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SDM A319/A320 MAINTENANCE PROGRAM
COVER PAGE
COVER PAGE
SDM AIRBUS 320 FAMILY MAINTENANCE PROGRAM
— “Rossiya airlines” OJSC —
18/4 Pilotov Street.
St. Petersburg, 196210
Russia
Continuing airworthiness is managed by
Produced by Operator’s Engineering Department
OTAR 39 Subpart F CAMO BDA/SF/018
Approved by BDCA
SDM A319/A320 MAINTENANCE PROGRAM
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c~ !.'..~~ ~.~J!
SOM A319/A320 MAINTENANCE PROGRAM
OPERATOR'S CERTIFICATION STATEMENT
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OPERATOR'S CERTIFICATION STATEMENT
In the preparation of this Maintenance Program to meet the requirements of EASA part M, OTAR Part 39 and IOSA standards, the recommendations
made by the airframe constructors and engine and equipment manufacturers have been evaluated and, where appropriate, have been incorporated.
It is accepted that any inspection requirements specified by the Director of Airworthiness Authority shall be incorporated.
This Maintenance Program lists the tasks and identifies the practices and procedures specified by the applicable Type Certificate Holder (s), which
form the basis for the scheduled maintenance of the aircrafts. The operator undertakes to ensure that these aircraft will be maintained in accordance
with this Maintenance Program.
The data contained in this Maintenance Program will be reviewed for continued validity at least annually in the light of operating experience.
It is accepted that this Maintenance Program does not prevent the necessity for complying with any new or amended regulations published by the
Authority where these new or amended regulations may override elements of this Maintenance Program.
It is understood that compliance with this Maintenance Program does not release the Operator from ensuring that the Maintenance Program reflects
the maintenance needs of the aircraft, such that continuing safe operation can be assured.
It is further understood that the Regulatory Authority, hereinafter referred as SOM Airworthiness Authorities, reserves the right to suspend, vary or
cancel approval of the Maintenance Program if they have evidence that requirements of the Maintenance Program are not being followed or that
standards of airworthiness are not being maintained.
For and behalf of the operator: SOM ("Rossiya airlines" OJSC)
Name: Alexander Sidorov,
Position: Posthold'ef fVr e'~n~n~ng Airworthiness
Signed:
DATE:
CJ{! ,4~ ~
,..-/
~·Jv-rm!(
f b'. 10. Q() (I(
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LIST OF CONCORDANCE
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SDM A319/A320 MAINTENANCE PROGRAM
AIRWORTHINESS AUTHORITIES APPROVAL
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SDM A319/A320 MAINTENANCE PROGRAM
CONTENTS
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CONTENTS
COVER PAGE ................................................................................................................................................................................................................. 1
OPERATOR’S CERTIFICATION STATEMENT ............................................................................................................................................................... 3
LIST OF CONCORDANCE .............................................................................................................................................................................................. 5
AIRWORTHINESS AUTHORITIES APPROVAL .............................................................................................................................................................. 7
CONTENTS ..................................................................................................................................................................................................................... 9
LIST OF EFFECTIVE PAGES AND RECORDING PROCEDURE ................................................................................................................................. 13
RECORDS AND REVISION HIGHLIGHTS .................................................................................................................................................................... 20
I.
A.
DISTRIBUTION LIST .......................................................................................................................................................................................... 20
B.
PROCEDURE OF REVISIONS ........................................................................................................................................................................... 21
C.
PROCEDURE OF TEMPORARY REVISIONS .................................................................................................................................................... 23
D.
REVISION HIGHLIGHTS .................................................................................................................................................................................... 24
1.
NEW TASKS ................................................................................................................................................................................................... 29
2.
DELETED TASKS ........................................................................................................................................................................................... 29
3.
REVISED APPLICABILITIES ........................................................................................................................................................................... 29
4.
REVISED INTERVALS .................................................................................................................................................................................... 29
5.
REVISED TASKS ............................................................................................................................................................................................ 29
6.
MOVED TASK ................................................................................................................................................................................................. 29
INTRODUCTION ..................................................................................................................................................................................................... 29
A.
MAINTENANCE PROGRAM DESCRIPTION ...................................................................................................................................................... 29
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B.
MAINTENANCE PROGRAM DOCUMENTS ....................................................................................................................................................... 29
C.
FLEET EFFECTIVITY, UTILIZATION AND LIMIT OF VALIDITY (LOV) .............................................................................................................. 31
D.
INTERVALS AND CHECKS ................................................................................................................................................................................ 34
1.
TASK INTERVALS .......................................................................................................................................................................................... 34
2.
MAINTENANCE CHECKS ............................................................................................................................................................................... 35
3.
SINGLE RUNNING TASKS (SRTs) ................................................................................................................................................................. 36
4.
ESCALATION OF ESTABLISHED PERIODS .................................................................................................................................................. 37
5.
VARIATIONS TO MAINTENANCE PERIODS ................................................................................................................................................. 37
6.
IMPLEMENTATION PERIODS ........................................................................................................................................................................ 39
E.
INCORPORATED MAINTENANCE PROGRAMS ............................................................................................................................................... 42
1.
SYSTEM/APU AND POWER PLANT INSPECTION PROGRAM ..................................................................................................................... 42
2.
STRUCTURAL INSPECTION PROGRAM ....................................................................................................................................................... 43
3.
ZONAL ISPECTION PROGRAM ..................................................................................................................................................................... 54
4.
TIME CONTROLLED ITEMS ........................................................................................................................................................................... 58
5.
ADDITIONAL PROGRAMS ............................................................................................................................................................................. 58
F.
STANDARDS, DEFINITIONS AND ABBREVATIONS ......................................................................................................................................... 66
1.
GENERAL STANDARD ................................................................................................................................................................................... 66
2.
GLOSSARY ..................................................................................................................................................................................................... 68
3.
ABBREVIATIONS ............................................................................................................................................................................................ 73
4.
ATA CHAPTERS ............................................................................................................................................................................................. 76
5.
TASK CODES AND MAINTENANCE OPERATIONS ...................................................................................................................................... 77
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TASK INFORMATION ..................................................................................................................................................................................... 78
G.
ZONAL DIAGRAMS ............................................................................................................................................................................................ 79
H.
MAINTENANCE PROGRAM LAYOUT ................................................................................................................................................................ 86
1.
REV ................................................................................................................................................................................................................. 87
2.
TASK NUMBER ............................................................................................................................................................................................... 87
3.
ZONE COLUMN .............................................................................................................................................................................................. 87
4.
DESCRIPTION COLUMN ................................................................................................................................................................................ 88
5.
SKILL CODE ................................................................................................................................................................................................... 88
6.
TASK CODE .................................................................................................................................................................................................... 89
7.
INTERVALS..................................................................................................................................................................................................... 89
8.
SOURCE ......................................................................................................................................................................................................... 91
9.
TPS – TEMPORARY PROTECTION SYSTEM ............................................................................................................................................... 92
10.
REFERENCEs ............................................................................................................................................................................................. 93
11.
MEN AND MH COLUMNS ........................................................................................................................................................................... 94
12.
APPLICABILITY COLUMN ........................................................................................................................................................................... 94
II.
SCHEDULED MAINTENANCE PROGRAM .......................................................................................................................................................... 1
III.
TIME CONTROLLED ITEMS ................................................................................................................................................................................ 1
IV.
MOD CONTROLLED ITEMS ................................................................................................................................................................................. 1
V.
INDIVIDUAL STRUCTURAL INSPECTIONS ........................................................................................................................................................ 1
A.
1.
STRUCTURAL INSPECTIONS LAYOUT .............................................................................................................................................................. 1
MSN .................................................................................................................................................................................................................. 1
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2.
ITEM .................................................................................................................................................................................................................. 1
3.
REASON ........................................................................................................................................................................................................... 1
4.
FURTHER ACTION ........................................................................................................................................................................................... 1
5.
PERIODIC INSPection ...................................................................................................................................................................................... 1
6.
LIMIT ................................................................................................................................................................................................................. 2
B.
INSPECTIONS MAINTNENANCE PROGRAM ..................................................................................................................................................... 2
APPENDIX I. EASA REQUIREMENTS REFERENCES ................................................................................................................................................... 1
APPENDIX II. BDCA AW 287 REFERENCES ................................................................................................................................................................. 1
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Upon receipt of a revision, each Maintenance Program hardcopy holder will be responsible for inserting the revised pages in its manual. The revisions
are made either by changing, adding or deleting the pages.
The revisions are identified by a number and the date of revision (this information is shown right-top corner of the page). They come with a modified list
of effective pages and a record of revisions (List of updates).
In order to avoid any risks of loss or omission, upon receipt of a revision, each MP Manual holder must check the pages according to the list of
effective pages. If any error was found, the holder shall claim the missing revisions to the Engineering department manager of the SDM.
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II-2
285
06-Oct-2014
III-1
1
06-Oct-2014
II-2
223
06-Oct-2014
II-2
244
06-Oct-2014
II-2
265
06-Oct-2014
II-2
286
06-Oct-2014
III-2
1
06-Oct-2014
II-2
224
06-Oct-2014
II-2
245
06-Oct-2014
II-2
266
06-Oct-2014
II-2
287
06-Oct-2014
III-2
2
06-Oct-2014
II-2
225
06-Oct-2014
II-2
246
06-Oct-2014
II-2
267
06-Oct-2014
II-2
288
06-Oct-2014
III-2
3
06-Oct-2014
II-2
226
06-Oct-2014
II-2
247
06-Oct-2014
II-2
268
06-Oct-2014
II-2
289
06-Oct-2014
III-2
4
06-Oct-2014
II-2
227
06-Oct-2014
II-2
248
06-Oct-2014
II-2
269
06-Oct-2014
II-2
290
06-Oct-2014
III-2
5
06-Oct-2014
II-2
228
06-Oct-2014
II-2
249
06-Oct-2014
II-2
270
06-Oct-2014
II-2
291
06-Oct-2014
III-2
6
06-Oct-2014
II-2
229
06-Oct-2014
II-2
250
06-Oct-2014
II-2
271
06-Oct-2014
II-2
292
06-Oct-2014
III-2
7
06-Oct-2014
II-2
230
06-Oct-2014
II-2
251
06-Oct-2014
II-2
272
06-Oct-2014
II-2
293
06-Oct-2014
III-2
8
06-Oct-2014
II-2
231
06-Oct-2014
II-2
252
06-Oct-2014
II-2
273
06-Oct-2014
II-2
294
06-Oct-2014
III-2
9
06-Oct-2014
II-2
232
06-Oct-2014
II-2
253
06-Oct-2014
II-2
274
06-Oct-2014
II-2
295
06-Oct-2014
III-2
10
06-Oct-2014
II-2
233
06-Oct-2014
II-2
254
06-Oct-2014
II-2
275
06-Oct-2014
II-2
296
06-Oct-2014
III-2
11
06-Oct-2014
II-2
234
06-Oct-2014
II-2
255
06-Oct-2014
II-2
276
06-Oct-2014
II-2
297
06-Oct-2014
III-2
12
06-Oct-2014
II-2
235
06-Oct-2014
II-2
256
06-Oct-2014
II-2
277
06-Oct-2014
II-2
298
06-Oct-2014
III-2
13
06-Oct-2014
II-2
236
06-Oct-2014
II-2
257
06-Oct-2014
II-2
278
06-Oct-2014
II-2
299
06-Oct-2014
IV-1
1
06-Oct-2014
II-2
237
06-Oct-2014
II-2
258
06-Oct-2014
II-2
279
06-Oct-2014
II-2
300
06-Oct-2014
IV-2
1
06-Oct-2014
II-2
238
06-Oct-2014
II-2
259
06-Oct-2014
II-2
280
06-Oct-2014
II-2
301
06-Oct-2014
IV-2
2
06-Oct-2014
II-2
239
06-Oct-2014
II-2
260
06-Oct-2014
II-2
281
06-Oct-2014
II-2
302
06-Oct-2014
IV-2
3
06-Oct-2014
II-2
240
06-Oct-2014
II-2
261
06-Oct-2014
II-2
282
06-Oct-2014
II-2
303
06-Oct-2014
IV-2
4
06-Oct-2014
II-2
241
06-Oct-2014
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06-Oct-2014
II-2
283
06-Oct-2014
II-2
304
06-Oct-2014
IV-2
5
06-Oct-2014
Page 18 of 94
MP-REF: SDM.A320.BDCA
SECTION: I
REV: 03 DATE: 06-Oct-2014
SDM A319/A320 MAINTENANCE PROGRAM
LIST OF EFFECTIVE PAGES AND RECORDING PROCEDURE
Sec
Page
Date
Sec
Page
Date
Sec
Page
Date
Sec
Page
Date
Sec
Page
Date
V-1
1
06-Oct-2014
V-2
6
06-Oct-2014
V-2
13
06-Oct-2014
VI
4
06-Oct-2014
VII
5
06-Oct-2014
V-1
2
06-Oct-2014
V-2
7
06-Oct-2014
V-2
14
06-Oct-2014
VI
5
06-Oct-2014
VII
6
06-Oct-2014
V-2
1
06-Oct-2014
V-2
8
06-Oct-2014
V-2
15
06-Oct-2014
VI
6
06-Oct-2014
VII
7
06-Oct-2014
V-2
2
06-Oct-2014
V-2
9
06-Oct-2014
V-2
16
06-Oct-2014
VII
1
06-Oct-2014
VII
8
06-Oct-2014
V-2
3
06-Oct-2014
V-2
10
06-Oct-2014
VI
1
06-Oct-2014
VII
2
06-Oct-2014
VII
9
06-Oct-2014
V-2
4
06-Oct-2014
V-2
11
06-Oct-2014
VI
2
06-Oct-2014
VII
3
06-Oct-2014
VII
10
06-Oct-2014
V-2
5
06-Oct-2014
V-2
12
06-Oct-2014
VI
3
06-Oct-2014
VII
4
06-Oct-2014
Page 19 of 94
SDM A319/A320 MAINTENANCE PROGRAM
RECORDS AND REVISION HIGHLIGHTS
MP-REF: SDM.A320.BDCA
SECTION: I
REV: 03 DATE: 06-Oct-2014
RECORDS AND REVISION HIGHLIGHTS
A.
DISTRIBUTION LIST
No
Distribution form
Title of Holder
1
Hard Copy
2
PDF version
RCAA North-West Regional Territorial Department for Civil Aviation Airworthiness
4
PDF version
Bermuda Aviation Authorities
3
PDF version
“Rossiya airlines” OJSC internal server
SDM Engineering Department
Page 20 of 94
SDM A319/A320 MAINTENANCE PROGRAM
RECORDS AND REVISION HIGHLIGHTS
B.
MP-REF: SDM.A320.BDCA
SECTION: I
REV: 03 DATE: 06-Oct-2014
PROCEDURE OF REVISIONS
The data contained in this Maintenance Program will be reviewed at least annually by SDM to ensure that the detailed requirements continue to be
valid in the light of operating experience and OEM requirements. Each amendment/change to this maintenance program is submitted to SDM
Authorities approval prior to incorporation in the Maintenance Program as a revision and publication.
Mandatory information such as Airworthiness Limitations and Certification Maintenance Requirements will be reviewed and implemented into the
Maintenance Program by SDM before actual compliance is required.
The updating of this A319/A320 SDM Maintenance Program will be initiated by SDM basing on the related Technical Documentation to reflect the
following (but not limited to) changes:







MRBR revision
MPD revision
Type certificate holder's recommendations
Maintenance Publication Documentation revisions
Aircraft Modifications
Operator in service experience
Requirement changes issued by EASA and/or SDM Authorities
Revision bars are marked to the left of the affected text, task number revision level is indicated in the revision column.
The system of revisions is applicable throughout all sections of this Maintenance Program. All revisions will be issued in the form of printed revision
pages. Handwritten revisions are not permitted.
Each revision will be numbered and distributed after the SDM Authorities approval. The Revision must be reported in the Record of revisions
paragraph.
Page 21 of 94
SDM A319/A320 MAINTENANCE PROGRAM
RECORDS AND REVISION HIGHLIGHTS
MP-REF: SDM.A320.BDCA
SECTION: I
REV: 03 DATE: 06-Oct-2014
Record of revisions
Revisions to the Maintenance Program are allocated consecutive revision numbers.
Rev No. Document Reference
Revision Date Remarks
First ISS SDM.A320.MS
21-Mar-2007
Initial MP for SDM A320 fleet
01
SDM.A319.MS
26-Jun-2008
BDCA approved. VP-BIU only
02
SDM.A319.MS
01-Dec-2008
BDCA approved
00
SDM.A320.FAM
15-Dec-2009
MPD Rev 32. The first maintenance program produced by Airbus SAS
03
SDM.A320.FAM
16-Aug-2010
MPD Rev 33. The last common maintenance program for BDCA and IRISH fleet
00
SDM.A320.BDCA
20-Mar-2013
Maintenace program layout changed. New OMP is only for VQ/VP-registered
aircrafts.
01
SDM.A320.BDCA
29-Jan-2014
MPD 39 implemented. MSN 1200, MSN 1379, MSN 2151 introduced. Reliability
decisions implementation.
02
SDM.A320.BDCA
17-Jul-2014
MSN 2163 introduced. Minor changes
03
SDM.A320.BDCA
06-Oct-2014
MSN 0649 APU Type change
Page 22 of 94
MP-REF: SDM.A320.BDCA
SECTION: I
REV: 03 DATE: 06-Oct-2014
SDM A319/A320 MAINTENANCE PROGRAM
RECORDS AND REVISION HIGHLIGHTS
C.
PROCEDURE OF TEMPORARY REVISIONS
Maintenance Program temporary revisions are used as interim minor update.
A Temporary Revision should be sent to the SDM and Aviation Authorities as a notification.
Record of temporary revisions
Signature of publication holder confirms that TEMPORARY REVISION has been incorporated:
TR No.
Document Reference
Issue Date
Date Inserted
Remarks
Page 23 of 94
SDM A319/A320 MAINTENANCE PROGRAM
RECORDS AND REVISION HIGHLIGHTS
D.
MP-REF: SDM.A320.BDCA
SECTION: I
REV: 03 DATE: 06-Oct-2014
REVISION HIGHLIGHTS
Maintenance program revision represents minor changes and applicability changes due to the fleet configuration evolution.
Section V. INDIVIDUAL STRUCTURAL INSPECTIONS layout change due to change of the publishing system
The following tables represent tasks changes highlights.
1. NEW TASKS
There are no new TC in this revision.
2. DELETED TASKS
Task Number
Change
272400-03-1
TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS.
324100-03-1
TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS
491200-01-1
TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS
491200-02-1
TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS
491300-01-1
TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS.
491600-01-1
TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS
491600-03-1
TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS
491600-04-1
TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS
492000-01-1
TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS
493100-01-1
TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS
493400-01-1
TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS
494141-01-1
TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS
Page 24 of 94
SDM A319/A320 MAINTENANCE PROGRAM
RECORDS AND REVISION HIGHLIGHTS
Task Number
Change
494251-01-1
TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS
494251-02-1
TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS
495100-01-1
TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS
498100-04-1
TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS
499100-02-1
TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS
ZL-315-01-3
TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS
MP-REF: SDM.A320.BDCA
SECTION: I
REV: 03 DATE: 06-Oct-2014
3. REVISED APPLICABILITIES
Task Number
Change
256300-01-1
IN APPLICABILITY MSN 0649 REMOVED DUE TO CAM Z050H0003010, is not equipped with EVAC
(AIRBUS LETTER)
272400-03-1
IN APPLICABILITY MSN "0649, 1200, 1379, 1488, 1560, 1578, 1657, 1743, 1761, 1767, 1851, 1863,
1876, 1890, 2151, 2163" REMOVED DUE TO GREASE 04-037 IS USED
272400-05-1
IN APPLICABILITY MSN "1130" REMOVED AND "ALL" ADDED DUE TO GREASE 04-037 USED
323000-17-1
IN APPLICABILITY MSN 1890 ADDED DUE TO SB 32-1346 EMBODIED.
323000-17-1
IN APPLICABILITY MSN 1200 DELETED DUE TO PRE MOD 37866.
324100-03-1
IN APPLICABILITY MSN 1761, 1851, 1863, 1876, 1890 REMOVED DUE TO APPL MPD REV 39.
361100-09-1
IN APPLICABILITY 1743, 1863, 1560 REMOVED DUE TO SB 71-1032 EMBODIED(NEW STATUS OF
RA32036-10)
361100-10-1
IN APPLICABILITY 1743, 1863, 1560 REMOVED DUE TO SB 71-1032 EMBODIED(NEW STATUS OF
RA32036-10)
491200-01-1
IN APPLICABILITY 0649 REMOVED DUE TO SB 49-1069 EMBODIED
491200-02-1
IN APPLICABILITY 0649 REMOVED DUE TO SB 49-1069 EMBODIED
Page 25 of 94
SDM A319/A320 MAINTENANCE PROGRAM
RECORDS AND REVISION HIGHLIGHTS
Task Number
Change
491200-B1-1
IN APPLICABILITY 0649 ADDED DUE TO SB 49-1069 EMBODIED
491200-B2-1
IN APPLICABILITY 0649 ADDED DUE TO SB 49-1069 EMBODIED
491300-01-1
IN APPLICABILITY 0649 REMOVED DUE TO SB 49-1069 EMBODIED
491300-B1-1
IN APPLICABILITY 0649 ADDED DUE TO SB 49-1069 EMBODIED
491600-01-1
IN APPLICABILITY 0649 REMOVED DUE TO SB 49-1069 EMBODIED
491600-03-1
IN APPLICABILITY 0649 REMOVED DUE TO SB 49-1069 EMBODIED
491600-04-1
IN APPLICABILITY 0649 REMOVED DUE TO SB 49-1069 EMBODIED
491600-B1-1
IN APPLICABILITY 0649 ADDED DUE TO SB 49-1069 EMBODIED
491600-B5-1
IN APPLICABILITY 0649 ADDED DUE TO SB 49-1069 EMBODIED
491600-B6-1
IN APPLICABILITY 0649 ADDED DUE TO SB 49-1069 EMBODIED
492000-01-1
IN APPLICABILITY 0649 REMOVED DUE TO SB 49-1069 EMBODIED
493000-B1-1
IN APPLICABILITY 0649 ADDED DUE TO SB 49-1069 EMBODIED
493100-01-1
IN APPLICABILITY 0649 REMOVED DUE TO SB 49-1069 EMBODIED
493400-01-1
IN APPLICABILITY 0649 REMOVED DUE TO SB 49-1069 EMBODIED
493400-B1-1
IN APPLICABILITY 0649 ADDED DUE TO SB 49-1069 EMBODIED
494000-B2-1
IN APPLICABILITY 0649 ADDED DUE TO SB 49-1069 EMBODIED
494000-B3-1
IN APPLICABILITY 0649 ADDED DUE TO SB 49-1069 EMBODIED
494000-B3-2
IN APPLICABILITY 0649 ADDED DUE TO SB 49-1069 EMBODIED
494000-B4-1
IN APPLICABILITY 0649 ADDED DUE TO SB 49-1069 EMBODIED
494141-01-1
IN APPLICABILITY 0649 REMOVED DUE TO SB 49-1069 EMBODIED
494251-01-1
IN APPLICABILITY 0649 REMOVED DUE TO SB 49-1069 EMBODIED
MP-REF: SDM.A320.BDCA
SECTION: I
REV: 03 DATE: 06-Oct-2014
Page 26 of 94
SDM A319/A320 MAINTENANCE PROGRAM
RECORDS AND REVISION HIGHLIGHTS
Task Number
Change
494251-02-1
IN APPLICABILITY 0649 REMOVED DUE TO SB 49-1069 EMBODIED
495100-01-1
IN APPLICABILITY 0649 REMOVED DUE TO SB 49-1069 EMBODIED
498000-B1-1
IN APPLICABILITY 0649 ADDED DUE TO SB 49-1069 EMBODIED
498100-04-1
IN APPLICABILITY 0649 REMOVED DUE TO SB 49-1069 EMBODIED
499100-02-1
IN APPLICABILITY 0649 REMOVED DUE TO SB 49-1069 EMBODIED
499100-B2-1
IN APPLICABILITY 0649 ADDED DUE TO SB 49-1069 EMBODIED
499100-B4-1
IN APPLICABILITY 0649 ADDED DUE TO SB 49-1069 EMBODIED
ZL-315-01-1
IN APPLICABILITY 0649 ADDED DUE TO SB 49-1069 EMBODIED
ZL-315-01-3
IN APPLICABILITY 0649 REMOVED DUE TO SB 49-1069 EMBODIED
MP-REF: SDM.A320.BDCA
SECTION: I
REV: 03 DATE: 06-Oct-2014
4. REVISED INTERVALS
Task Number
Change
336000-02-1-SDM
100% INTERVAL CHANGED FROM: "6000 FH and 18 MO", TO: "7500 FH and 24 MO".
336000-03-1-SDM
100% INTERVAL CHANGED FROM: "6000 FH and 18 MO", TO: "7500 FH OR 24 MO".
336000-04-1-SDM
100% INTERVAL CHANGED FROM: "12000 FH and 36 MO", TO: "90 DY".
5. REVISED TASKS
Task Number
Change
000001-01-1-SDM
IN REFERENCES "AAR EU OPS 1.605" DELETED AND "EU PART CAT (EU) No 965/2012" ADDED
252841-01-1-SDM
IN TASK TITLE “AND EEPMS" ADDED.
313300-01-1-SDM
IN DESCRIPTION "EU OPS 1" REMOVED AND "COMMISSION REGULATION (EU) No 965/2012"
ADDED.
336000-01-1-SDM
TASK TITLE CHANGED FROM: "GENERAL VISUAL INSPECTION AND SERVICING", TO: "SYSTEM
Page 27 of 94
SDM A319/A320 MAINTENANCE PROGRAM
RECORDS AND REVISION HIGHLIGHTS
Task Number
MP-REF: SDM.A320.BDCA
SECTION: I
REV: 03 DATE: 06-Oct-2014
Change
CHARGING".
336000-02-1-SDM
IN TASK TITLE: "6000 FH OR 18MO " DELETED.
336000-03-1-SDM
IN TASK TITLE: "6000 FH OR 18MO " DELETED.
336000-04-1-SDM
TASK TITLE CHANGED FROM: "12000 FH OR 36 MO INSPECTION AND FUNCTIONAL CHECK", TO: "
GENERAL VISUAL INSPECTION" .
336000-05-1-SDM
IN TASK TITLE: "10 YEAR " DELETED.
252841-01-1-SDM
IN DESCRIPTION "AND EMERGENCY ESCAPE PATH MARKING SYSTEM (IF INSTALLED)" ADDED.
336000-01-1-SDM
DESCRIPTION CHANGED "VISUAL INSPECTION OF FLOOR MOUNTED COMPONENTS, INTERIOR
LIGHTING AND SERVICE SYSTEM" TO "PERFORM INITIAL DAILY CHARGE PER APPROVED
PROCEDURES BY ACTIVATING CABIN LIGHTING".
336000-01-1-SDM
TASK CODE CHANGED FROM: "GVI", TO: "SVC"
336000-04-1-SDM
DESCRIPTION CHANGED FROM "INSPECTION AND FUNCTIONAL CHECK TEST COUPON (FWD RH
CABIN)" TO "GVI OF FLOOR MOUNTED COMPONENTS AND INTERIOR LIGHTING"
336000-04-1-SDM
TASK CODE CHANGED FROM: "FNC", TO: "GVI"
753120-01-1-SDM
IN DESCRIPTION " ONLY PN 3282970-4 AND PN 3282970-4" REMOVED AND " PN 3282970-4" ADDED
6. MOVED TASK
There are no moved TC in this revision.
Page 28 of 94
SDM A319/A320 MAINTENANCE PROGRAM
I.
MP-REF: SDM.A320.BDCA
SECTION: I
REV: 03 DATE: 06-Oct-2014
INTRODUCTION
A.
MAINTENANCE PROGRAM DESCRIPTION
The “ROSSIYA AIRLINES” OJSC (SDM) A319/A320 Maintenance Program provides maintenance instructions necessary for the safe, airworthy and
reliable operation of the aircraft in regard of its specific use. The SDM Maintenance Program is based on, and reflects, the manufacturer’s Aircraft
Maintenance Schedule, tailored to the “ROSSIYA AIRLINES” OJSC equipment and specifications, and approved by the SDM Authorities. Unscheduled
and off-wing maintenance tasks are not included in this SDM A319/A320 Maintenance Program. For unscheduled and off-wing maintenance, the
contracted Part-145 Maintenance Organization must follow the relevant manufacturer's instructions for continuing airworthiness.
The Maintenance Program is made up of Systems, Structures and Zonal requirements. The Systems Program gives task, arising from the MSG-3
Systems and Power Plant/APU the MSG-3 analysis. The Structures Program lists specific, directed inspections of each Structural Significant Item
developed through the MSG-3 Structures analysis of their fatigue, environment and accidental damage characteristics. The Zonal Program lists
general visual inspections of system installations and structure on a zone by zone basis. This program has been developed in conjunction with the
other programs to avoid duplication, and to ensure complete coverage of the aircraft systems and structure.
B.
MAINTENANCE PROGRAM DOCUMENTS
The following source documents are referenced to the latest issue in this maintenance program:











A318/A319/A320/A321 Maintenance Review Board Report (MRBR) Rev 18 dated 01 March 2013.
Airbus Maintenance Planning Document (MPD) Rev. 39 dated 01 July 2013.
A318/A319/A320/A321 ALS Part 2 – Damage Tolerant Airworthiness Limitation items document, Revision 02 from 28 May 2013.
A318/A319/A320/A321 ALS Part 3– Certification Maintenance Requirements items document, Revision 01 from 15 June 2012
A318/A319/A320/A321 ALS Part 4– ASM items document, Revision 01 from 15 June 2012
A318/A319/A320/A321 ALS Part 5 – Fuel Airworthiness Limitations items document, Revision 00 from 14 Sep 2012.
SDM CAME Issue 02, Revision 11 from April 2014
STC ST00788SE, BERG-151-701 Rev B from 05-Jul-2013. Live TV installation
STC ST02292AT, L67-10 Rev H from 15-May-2014. SAFTGLO Emergency Escape path parking
ICA_M090001115_JTU_20032014 Rev 0 from 20.03.2014 A320 MCD Installation
ICA_M090001109_BCA_17022014 Rev 0 from 25.02.2014 A320 MSN2151 2163 LH and RH Windscreen Installation
Page 29 of 94
SDM A319/A320 MAINTENANCE PROGRAM
INTRODUCTION







MP-REF: SDM.A320.BDCA
SECTION: I
REV: 03 DATE: 06-Oct-2014
Engine Shop Manuals (ESM) for CFM56–5A and CFM56–5B engines
APU Honeywell 131-9(A) Engine Manual
Inspection Service Bulletins (ISB)
Vendor Service Bulletins (VSB)
Service Information Letter (SIL)
Alert Operators Transmission (AOT)
Airworthiness Directives (AD)
Page 30 of 94
MP-REF: SDM.A320.BDCA
SECTION: I
REV: 03 DATE: 06-Oct-2014
SDM A319/A320 MAINTENANCE PROGRAM
INTRODUCTION
C.
FLEET EFFECTIVITY, UTILIZATION AND LIMIT OF VALIDITY (LOV)
The Certificate of Registration holder for the aircraft listed in this Maintenance System (Maintenance Program) is “ROSSIYA AIRLINES” OJSC .
This Maintenance Program is applicable to the aircraft, engines and APU listed hereunder (aircrafts under TC EASA.A.064):
Reg.
VP-BIU
VQ-BDR
VQ-BCG
VQ-BFM
VQ-BAR
VQ-BAQ
VQ-BBM
VQ-BDY
VQ-BAV
VP-BIT
VQ-BDQ
VQ-BAU
Type
A319-114
EASA A.064
A320-214
EASA A.064
A320-214
EASA A.064
A320-214
EASA A.064
A319-111
EASA A.064
A319-111
EASA A.064
A320-214
EASA A.064
A320-214
EASA A.064
A319-111
EASA A.064
A319-111
EASA A.064
A320-214
EASA A.064
A319-111
EASA A.064
MSN
DOM
Engine Type
APU
WV
GROUP
LOV
0649
17.01.1997 CFM56-5A5
131-9(A)
001
19-1A
48000 FC OR 60000 FH
1130
02.11.1999 CFM56-5B4/P
131-9(A)
010
N/A
48000 FC OR 60000 FH
1200
17.03.2000 CFM56-5B4/P
131-9(A)
010
N/A
48000 FC OR 60000 FH
1379
05.12.2000 CFM56-5B4/P
131-9(A)
010
N/A
48000 FC OR 60000 FH
1488
10.04.2001 CFM56-5B5/P
131–9(A)
002
19-1B
48000 FC OR 60000 FH
1560
26.07.2001 CFM56-5B5/P
131–9(A)
002
19-1B
48000 FC OR 60000 FH
1578
30.08.2001 CFM56-5B4/P
131–9(A)
010
N/A
48000 FC OR 60000 FH
1657
15.11.2001 CFM56-5B4/P
131-9(A)
010
N/A
48000 FC OR 60000 FH
1743
08.05.2002 CFM56-5B5/P
131–9(A)
002
19-1B
48000 FC OR 60000 FH
1761
23.05.2002 CFM56-5B5/P
131–9(A)
001
19-1A
48000 FC OR 60000 FH
1767
20.03.2002 CFM56-5B4/P
131-9(A)
010
N/A
48000 FC OR 60000 FH
1851
31.10.2002 CFM56-5B5/P
131-9(A)
002
19-1B
48000 FC OR 60000 FH
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Reg.
VQ-BAS
VQ-BAT
VP-BIQ
VP-BWH
VP-BWI
Type
A319-111
EASA A.064
A319-111
EASA A.064
A319-111
EASA A.064
A320-214
EASA A.064
A320-214
EASA A.064
MSN
DOM
Engine Type
APU
WV
GROUP
LOV
1863
09.09.2002 CFM56-5B5/P
131-9(A)
002
19-1B
48000 FC OR 60000 FH
1876
26.11.2002 CFM56-5B5/P
131-9(A)
002
19-1B
48000 FC OR 60000 FH
1890
11.12.2002 CFM56-5B5/P
131-9(A)
001
19-1A
48000 FC OR 60000 FH
2151
01.12.2003 CFM56-5B4/P
131-9(A)
012
N/A
48000 FC OR 60000 FH
2163
21.01.2004 CFM56-5B4/P
131-9(A)
012
N/A
48000 FC OR 60000 FH
NOTE: The Operator has to follow the rules detailed in A318/A319/A320/A321 MPD — Structure Section: “WV groups are only stated where
necessary. In other cases the aircraft Model, e.g. A320, or aircraft model and series, e.g. A320-200, have been retained where these cover all
requirements. For A/C, that have been subject to a WV change through a service bulletin embodiment, the maintenance requirements that apply are
those with the lowest threshold and interval figures applicable to this A/C during service life regardless of the current WV of that subject aircraft.”
Limit of Validity (LOV). A320 Family aircrafts are certified against utilization limits expressed in FC and FH. The requirements developed and
published allow operation up to the Limit of Validity (LOV) expressed in FC or FH whichever occurs first. The relevant LOV values are stated in the
table above. The LOV reflects the limit of validity of the engineering data that supports the structural maintenance program.
Utilization. The periods and frequencies of the maintenance tasks and inspections in this Maintenance Program are based on an estimated yearly
utilization of:


3700 FH and 3.0FH/FC for A320 aircraft with tolerance +/- 25%
3500 FH and 2.5 FH/FC for A319 aircraft with tolerance +/- 25%
Low Utilization Recommendations (LUR) are considered and incorporated in this Maintenance Program. On tasks with multiple intervals, always the
“whichever occurs first” value is applicable.
If the annual utilization varies by more than 25% from that stated, the Operator will review this Maintenance Schedule in order that any necessary
adjustments to the maintenance tasks and periods may be made.
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Fleet limit of validity status
As of 06.10.2014
50000
45000
40000
35000
FC
30000
25000
VQ-BFM
20000
VQ-BCG
15000
VP-BWI
VP-BIU
VQ-BAR
VQ-BAQ
VP-BIQ VQ-BAV
VQ-BAT
VP-BIT
VQ-BDQ
VQ-BAU
VQ-BBM
VQ-BDY
VP-BWH VQ-BDR
10000
5000
0
20000
25000
30000
35000
40000
45000
50000
55000
60000
FH
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INTERVALS AND CHECKS
1. TASK INTERVALS
a) General rules
When two intervals are assigned to a task, the interval expiring first shall apply.
Unless otherwise specified in delivery documentation, the maintenance clock may be set at zero at the Transfer of Title date to the first owner.
However, the following exceptions to this rule apply:
 ADs must be performed when due, refer to the compliance paragraph of any AD applicable.
 Life Limits, ALIs and CMRs: they count from First Flight.
 The TBO for Landing Gears may be counted from the date of delivery, if the concerned aircraft is delivered within three months after the First
Flight, otherwise the TBO clock counts from the date of the First Flight.
 Time Controlled Items: the starting point may be defined by the Supplier as the date of manufacturing.
The Operator will:
 Adjust this Maintenance Program in accordance with National Requirements.
 Comply with existing rules with respect to reporting to their Airworthiness Authorities and to the Manufacturer events having effects on the
continued airworthiness of the aircraft.
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b) Intervals
Intervals should be expressed in parameters:
Intervals - Operational usage parameters
Flight hours (FH)
Elapsed time between wheel lift off and wheel touchdown.
Flight cycles (FC)
A complete take-off and landing sequence.
Cycle (CY)
Engine cycle.
Intervals - Calendar units
Hour (HR)
One Calendar hour elapsed.
Day (DY)
24 Calendar hours elapsed. “DY” interval may be counted from 00:00 o’clock of next day
(has not to include remaining day time since task completion)
Day (DY)
One Calendar Day.
Month (MO)
One Calendar month.
Year (YE)
One Calendar year.
Other Intervals
National Requirement (NR)
Interval value may be affected by a local National Requirement
Vendor Requirement (VR)
Interval value dependent on the Vendor Recommendation
The MRB Report Section B Note 13 allows task interval parameters expressed in the MRB Report to be converted to an individual operators desired
units (FH, Cycle or Calendar Time), provided this conversion does not result in the operator exceeding the initial requirements of the MRB Report.
2. MAINTENANCE CHECKS
“A” events are performed as block. “C” events are performed as block.
a) Preflight Check
These checks are to be carried out in accordance with Flight Crew Operation Manual and accomplished by the Flight Crew before each flight.
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b) Transit Check
The Transit check shall be accomplished in accordance with Check List after arrival to the base parking apron. At ramp position the Transit Check has
to be done not earlier than two hours before take-off.
c) Daily Check
The Daily Check shall be performed once per calendar day (accomplishment not to exceed 48 elapsed calendar hours). Content of Daily Check is
supplied in SDM Line Check List document. "36 HR", "3 DY" tasks available in Maintenance Program section 3 are planned within “Daily Check”
package of Line Check List.
Day 1
Day 2
Once per day
Day 3
Maximum 48 hours
d) Weekly Check
The Weekly Check shall be performed once every 7 days (Accomplishment not to exceed 8 calendar days). Content of Weekly Check is supplied in
SDM Line Check List document. "8 DY", "120 FH", and "150 FH” tasks available in Maintenance Program section 3 are planned within “Weekly Check”
package of Line Check List.
e) “A”-Events and “C”-Events
Items “750 FH / 750 FC / 4 MO” + Out Of Phase tasks from this Maintenance Program may be comprised into packages which will be performed
together. Eventually, these groups may be given familiar letter check abbreviations as A-Check and are planned every 750 FH.
C-Checks are planned every 24 MO and are mainly comprised of “7500 FH / 5000 FC / 24 MO“ tasks +Out Of Phase tasks and their multiples of the
basic check intervals stated above where appropriate.
However, the maximum interval given in this first Maintenance Program issue must not be exceeded.
3. SINGLE RUNNING TASKS (SRTS)
SRTs are special inspections to be performed at intervals different from the scheduled maintenance checks. They can be performed either separately
or in the work package together with the maintenance checks.
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4. ESCALATION OF ESTABLISHED PERIODS
The initial maintenance requirements are outlined in the Maintenance Review Board (MRB) Report. No escalation is foreseen unless in accordance
with the manufacturer’s recommendations. “ROSSIYA AIRLINES” OJSC will not change the scheduled inspection program at any time. Nevertheless
changes and additions recommended or mandated by manufacturers and/or authorities will be incorporated into the A319/A320 SDM Maintenance
Program with approval from the SDM Airworthiness Authorities.
NOTE: CMR “One star” tasks. Task intervals quoted in the CMR document cannot be increased unless advised by the manufacturer following
approval by the appropriate Type Certification Authority.
NOTE: CMR “Two star” tasks. Task intervals quoted in the CMR document may be increased only in accordance with escalation practices
approved by the operator’s Maintenance Authority
5. VARIATIONS TO MAINTENANCE PERIODS
A permitted variation to a period required by the Maintenance Program may be granted by the SDM Quality Manager (Airworthiness Authorities always
notified) on a case by case basis on occasions where “ROSSIYA AIRLINES” OJSC or the contracted Part-145 approved/accepted maintenance
organization facility, does not have the ability to perform the required maintenance within the prescribed limits.
A permitted variation applies for a unique occasion.
A permitted variation should not be understood to be a maintenance planning tool, but as an exceptional means to allow “ROSSIYA AIRLINES” OJSC
to fly for a limited period of time until the required maintenance is performed. It therefore follows that acceptable reason for requesting a permitted
variation may include unforeseen workload peak in the maintenance organization, so that it is not physically possible to perform the required
maintenance on time.
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Maximum allowable variations by the operator are indicated below:
INTERVAL/THRESHOLD
MAXIMUM EXTENSION
Flight hours intervals
I ≤ 5 000 FH
±10%
I > 5 000 FH
500 FH
Flight cycles intervals
I ≤ 500 FC
±5% not more than 25 FC
I > 500 FC
±5% not more than 250 FC
Calendar intervals
I ≤ 1 YE
±10% not more than 1 month
1 YE < I ≤ 3 YE
not more than 2 months
I > 3 YE
not more than 3 months
Mixed limits intervals
For items controlled by more than one limit e.g. items controlled by flying hours and calendar time or flying hours
and landings/cycles, the more restricted limit shall be applied.
An application for a permitted variation should at least include the following information:
1.
Aircraft identification, by registration marks.
2.
Justification of the need for such a variation.
3.
Proposed extension in the appropriate figure (flight hours, cycles, etc.)
4.
Current inspection status of the aircraft.
5.
List of aircraft deferred defects which are affected by the variation.
6.
Confirmation that continued compliance with mandatory life limitation is not affected by the variation such as AD’s, life limited parts, CMR’s,
ALI’s etc.
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Compensation tasks (i.e. additional maintenance tasks undertaken to be performed before the new proposed limit).
Permitted variations do not apply to: Life Limitations, Airworthiness Directives, CMR unless specified otherwise in the MRB Report and agreed by
the Authority (ref. “Two star” CMR’s from ACJ 25.1309).
6. IMPLEMENTATION PERIODS
The IMPLEMENTATION PERIOD is a Grace period for the first time accomplishment of new tasks added to a Maintenance Program of an aircraft
already in service.
Since the origin of the maintenance program tasks varies from “mandatory” (CMRs, ALIs, Ads) to “potential economic benefit” It is not appropriate to
have a common policy regarding 'implementation period' that can be applied to all tasks. For the different sources the following Implementation rules
applies:
a)
Airworthiness Directives
The compliance date and implementation period is identified in the AD document. SDM may start a process to discuss Alternate Means of Compliance
with the Airworthiness Authorities.
b) ALI – ALS Part 2. Damage Tolerant Airworthiness Limitation Items
Airbus plan to publish ALIs at least two years before they become due on the first aircraft. In cases where this two year period is not achieved, it is
recognized that it may be difficult (or impossible) to schedule the task on a particular airframe before it comes due. In such cases, Airbus will review
the particular utilization and type of operation to determine if an alternate means of compliance can be developed.
Airbus is not normally able to issue a generic grace period for ALIs. ALI grace periods must be handled on a case by case basis, using specific
utilization data from concerned aircraft. SDM should ensure it does not exceed the limitation without prior agreement with the manufacturer,
the local airworthiness authority and the certificating authority. In exceptional circumstances an ALI may be issued which is already overdue on a
particular aircraft. In such cases Airbus will provide guidance in the transmittal letter. Operators may also contact Airbus for specific advice.
c) Certification Maintenance Requirements (CMR) – ALS Part 3
In theory, a CMR cannot be added, or an existing CMR made more restrictive, to an in-service aircraft. All CMRs should be published before the
subject design feature enters service, whether this is on the basic aircraft or as a result of a modification. If delays occur in CMR document approval it
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is possible that a CMR becomes valid after enters into service. In this case, the CMR document transmittal letter will advise an appropriate grace
period before first time accomplishment.
d) ALI – ALS Part 4. Aging System Maintenance
ALS Part 4 tasks are being established in order to allow operation of aircraft systems beyond their original qualification. Beyond this point, ageing
effects may affect the characteristics leading to an increased potential for failure. The Part 4 of the Airworthiness Limitations Section (ALS) therefore
contains the maintenance actions together with their limitation to help to qualify the systems for continued operation.
e) ALI – ALS Part 5. Fuel Airworthiness Limitation Items (FAL)
On aircraft that have already exceeded the task threshold, Airbus recommends that the FAL tasks are performed at the operator's next scheduled
structural inspection at 6 YE or 12 YE.
f)
MRB Report and MRB temporary revisions
Engineering judgment that is based on the Reliability Data is required for the new tasks that were driven by MRB revision. But Airbus recommended
rules are:
Systems/APU/Power Plant and ZIP tasks
Perform at the next due interval. This might not be the next interval (for which the planning may be completed) but it would be expected in the following
one.
NOTE: If task elapsed time is short and any possible corrective action is easily addressed, operator should consider first performance of at least the
FEC 5 and 8 tasks in the next convenient 750 FH / 750 FC / 100 days package. It is recognized that in some cases access for tasks with higher
interval (e.g. 24000 FH, 80 MO) is not available at the next C1 or C2 check events (where typically tasks with intervals 7500 FH / 15000 FH, 5000 FC /
10000 FC, 24 MO / 48 MO are performed), for example, fuel tank entry, galley or lavatory removal. In these cases, unless stated otherwise in the MRB
Report transmittal letter, Airbus recommend accomplishment at the next due interval that is typically a 6 YE check event.
Structure Tasks with CALENDAR threshold/ interval
A revised CALENDAR requirement is normally associated with findings from environmental impacts like corrosion, water ingress etc. In case of
overruns, the concerned operator needs to consider his local operating conditions in order to assess the potential for environmental damage in this
area on his particular aircraft. It is recommended to perform the task as soon as possible on at least one aircraft in the fleet in order to help make this
assessment. Delay in accomplishment may lead to higher repair costs but not to a loss of continued airworthiness. Note that if a safety concern exists,
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a new CALENDAR task recommendation on an in service aircraft would be promulgated by ISB (and possibly AD) in addition to inclusion in the MRB
Report.
EWIS tasks
On aircraft that have already exceeded the task threshold, Airbus recommend that the ATA 20 tasks with (EWIS) after task description are performed
at the operator's next convenient check opportunity unless access is assessed as insufficient to perform the task without exceeding the scheduled outof-service period. In this case, the task should be performed at the next suitable access opportunity (e.g. a structural inspection at 6 YE or 12 YE) but
not exceeding the task interval counting from the MRBR Rev. 12 approval date (April 2007).
g) Inspection Service Bulletins / All Operator Telexes
As for AD, these documents normally include a recommended compliance time. Where this is not stated, it is recommended that operators follow the
same guidance as for the MRB Report.
h) Service Information Letters
It is recommended that operators follow the same guidance as for the MRB Report.
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INCORPORATED MAINTENANCE PROGRAMS
1. SYSTEM/APU AND POWER PLANT INSPECTION PROGRAM
The System/APU and Power Plant Inspection Program covers all systems of ATA 20 up to and including ATA 80. It includes scheduled maintenance
tasks such as:
 visual checks and inspections,
 servicing and lubrication task,
 operational and functional checks,
 on A/C maintenance tasks.
These tasks have to be accomplished on 100% basis unless otherwise stated.
Discard, restoration and tasks to be normally performed in the shop are included in Section 04 of this Maintenance Program.
Engine and APU Program: contains the scheduled maintenance tasks related to:
 the power plants CFM 56-5A and CFM 56-5B (including engine and accessories, engine mounts, cowlings and thrust reversers)
 the Auxiliary Power Unit APU “Honeywell 131–9(A)”.
These scheduled maintenance tasks have to be accomplished on aircraft or may be accomplished at opportunity of an engine/APU change.
The inspection and restoration tasks specified in the engine and APU shop manuals will be performed at the opportunity of the engine removals and
disassembly in workshop. These tasks are not considered as scheduled maintenance in this A319/A320 SDM Maintenance Program.
Life limits defined by the Engine manufacturer and APU manufacturer are respectively specified in:
 “CFM 56-5A Engine Manual Chapter 5.”
 “CFM 56-5B Engine Manual Chapter 5.”
 “Honeywell 131–9(A) APU Component Maintenance Manual”
and are not attached to this Maintenance Program. They are linked to engine serial numbers ESN and not to Aircraft MSN. These items are tracked for
each engine ESN.
Off-wing maintenance tasks are not included in the Maintenance Program.
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2. STRUCTURAL INSPECTION PROGRAM
The purpose of this Program is to maintain the continuous airworthiness of the aircraft structure and to control corrosion to level 1 or better (refer to:
Paragraph f. Corrosion Prevention and Control Program (CPCP) for definition of level 1 corrosion).
The Structure Program is to be used in conjunction with the Zonal Program.
NOTE: Structure Significant Items (SSI) tasks required by the MRB Report Section D that are transferred to the Zonal Inspection Program, do not
require a dedicated task in the Structure Program for the initial scheduling. They are considered adequately covered by the Zonal Program.
a) Inspection thresholds and intervals
The following inspection thresholds and intervals apply to the Structure Program:
Fatigue related tasks:
Threshold: 24000 FC or 42000 FH, Subsequent intervals: no general interval, refer to each task
Environmental damage related tasks: Threshold: 6 YE or 12 YE, Subsequent intervals: 6 YE or 12 YE
Accidental damage related tasks: No general interval, refer to each task
b) Inspection levels
According to the analysis procedure, for each Structural Significant Item (SSI), various Inspection levels have been considered with the aim of
selecting the lowest inspection level compatible with the type of damage and the expected damage growth. Therefore, one or more of the following
inspection levels have been selected for each SSI:



General Visual Inspection (GVI)
Detailed Inspection (DI)
Special Detailed Inspection (SDI)
For definition of inspection levels refer to “STANDARDS, DEFINITIONS AND ABBREVATIONS” Chapter.
c) Types of damages considered
This Program has been developed by considering the following sources of damage:
Metallics:
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

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Fatigue Damage (FD).
Environmental Deterioration (ED).
Accidental Damage (AD).
Fatigue Damage (FD)
For FD, the damage initiation and subsequent damage growth is primarily dependent on the ground-air-ground loading variation, which occurs once
per flight. Therefore, flight cycles (FC) are used as the unit for thresholds and repeat intervals. Some fatigue related SSIs are also sensitive to flight
duration. For these SSIs, a FH limit is stated in addition to the FC limit. The inspection is to be performed at whichever limit is reached first.
The structure inspection tasks selected for fatigue are derived from damage tolerance evaluation according to the criteria defined by FAR/JAR 25.571
(EASA) Amendment 45, with the aim of ensuring timely damage detection. The FC and FH data is based on a combination of calculation, full-scale
fatigue test teardown results, and in-service experience (where available).
Environmental Deterioration (ED)
For ED, since the deterioration caused by the environment (e.g. corrosion, stress corrosion) is mainly time dependent, inspection intervals and
thresholds are based on calendar time (Years).
Accidental Damage (AD)
For deterioration caused by accidental damage, it is considered that major damage such as that caused by bird impact, or ground handling equipment,
will be detected by routine inspections.
AD consists of minor damage which could result in fatigue and/or corrosion damage, and which could propagate undetected. In the analysis, the
fatigue and environmental effects of the accidental damage are considered. A dedicated AD task is not selected; the AD requirement is consolidated
into either the ED or the FD task, or both, according to the AD consequences. AD is therefore subject to maintenance requirements expressed in FC
(and FH) or calendar time or both.
Non-Metallics:


Ageing Deterioration
Accidental Damage
Ageing Deterioration
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Deterioration caused by ageing considers loading conditions and environmental conditions. Inspection intervals and thresholds are based on calendar
time.
Accidental Damage
Deterioration caused by accidental damage is subject to inspection intervals based on calendar time.
The frequency of inspection is dependent on static strength reduction caused by the selected damage, combined with the likelihood of the selected
damage occurring more than once during the basic interval.
As this kind of deterioration is random in nature, inspections shall be applied to all aircraft at each repeat interval without threshold.
d) Inspection categories
Structure program inspections fall into the following three categories: 100% Tasks, Sampling Tasks, and Sampling Tasks that become 100% for the
non-sampling aircraft at the 100% Threshold.
The inspections performed on sampling fleet aircraft prevent performing the sampling inspections on 100% of one operator's fleet at the listed sampling
threshold as per task. In case an operator does not define a sampling fleet, it is the Airbus recommendation to perform applicable sampling inspection
requirements on all aircraft of the operator’s fleet.
100% TASKS
Fatigue tasks where calculation and/or test indicate high fatigue sensitivity. These tasks are not selected for Sampling. These tasks have a 100%
Threshold only.
Fatigue or corrosion tasks where Accidental Damage is likely. These tasks are not selected for Sampling. These tasks have a 100% Threshold only.
Environmental Deterioration (corrosion) tasks where in-service experience indicates that Accidental Damage is likely. These tasks are not selected for
Sampling. These tasks have a 100% Threshold only.
100% Tasks are indicated by an entry in the “100% THRESHOLD INTERVAL” column only.
SAMPLING TASKS THAT BECOME 100%
Fatigue tasks where calculation and/or test indicate a medium fatigue sensitivity. These tasks are selected for sampling. These tasks have a Sampling
Threshold and a 100% Threshold. All aircraft not inspected as sampling aircraft must be inspected at the 100% Threshold latest.
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Corrosion tasks where in-service experience indicates that damage is not likely are selected for sampling. These tasks have a Sampling Threshold and
a 100% Threshold. All aircraft not inspected as sampling aircraft must be inspected at the 100% Threshold.
Sampling Tasks that become 100% are indicated by an entry in the “SAMPLING THRESHOLD INTERVAL” and an entry in the “100% THRESHOLD
INTERVAL” column.
SAMPLING TASKS
Fatigue tasks where calculation and/or test indicate low fatigue sensitivity. These items are selected for sampling.
Sampling Tasks are indicated by an entry in the “SAMPLING THRESHOLD INTERVAL” column only.
e) Sampling Program
Sampling program is not applicable to the SDM fleet.
f)
Corrosion Prevention and Control Program
The Structures Program includes requirements to control corrosion to Level 1 or better on all structural details, elements or assemblies which
contribute significantly to carrying flight, ground, pressure or control loads, and whose failure could affect the structural integrity necessary for the
safety of the aircraft
All Corrosion Prevention and Control Program (CPCP) requirements are indicated by the code ‘CPCP’ in the “SOURCE” column.
Some calendar-time tasks are also covered by the Sampling Program, i.e. they have a Sample Threshold/Interval. For these tasks, the 100%
Threshold is the time at which the task becomes a CPCP task.
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CORROSION LEVEL DEFINITIONS
The definitions for the various Levels of corrosion are as follows:
Level 1 Corrosion
Corrosion occurring between successive inspections that can be reworked/blended-out within allowable limits as defined by the manufacturer (SRM,
SB, etc.)
Level 2 Corrosion
Corrosion occurring between successive inspections that require a single rework/blend-out, which exceeds allowable limits as defined by the
manufacturer (SRM, SB, etc.), requiring a repair/reinforcement or complete or partial replacement of applicable structure.
Level 3 Corrosion
Corrosion found during first or subsequent inspection(s), which is determined (normally by the operator) to be an urgent airworthiness concern
requiring expeditious action.
CPCP RULES
The effectiveness of the Corrosion Prevention and Control Program is determined by following the General Rules applicable to the Structures Program
(refer to Paragraph 8) and the rules listed below (Refer also to CPCP Flow Chart and Decision Steps on following pages).
Level 1 Corrosion Findings
Should inspections consistently reveal corrosion Level 1 findings for a given area during repeat inspections on particular aircraft operated in similar
conditions, then the existing program is considered effective for the concerned area, and no change to the program is necessary.
Level 2 Corrosion Findings
Should inspections reveal that corrosion is Level 2 for a given area during repeat inspections, then the existing program is not effective for the
concerned area of the particular fleet.
In order to control corrosion to Level 1 or better, consideration should be given to one or more of the following corrective actions:


Decreasing the inspection threshold/interval
Considering a higher inspection level
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


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Re-considering the Program Concept
Application/More frequent application of Temporary Protection System
Embodiment of preventive modifications, where applicable
Installation of parts with improved protection standard, where applicable
In this way, the program is self-regulating and will adjust itself to the optimum program.
Level 3 Corrosion Findings
Should inspections reveal that corrosion is Level 3 in a given area, then the existing
program is not effective for the concerned area.
In addition to the considerations given for Level 2 corrosion, an action plan calling for a onetime inspection of the concerned area should be expeditiously agreed with the local Aviation
Authority and carried out on all aircraft of a similar age or older.
Airbus may be consulted to determine whether or not the airworthiness is affected. In this
case all details of findings are to be promptly reported for detailed evaluation and the
assistance required clearly expressed.
A periodic review of the Structures Program, with particular attention to reported fleet data
shall be scheduled to maintain the target of this program to control corrosion to Level 1 or
better on all structural details, elements or assemblies which contribute significantly to
carrying flight, ground, pressure or control loads, and whose failure could affect the
structural integrity necessary for the safety of the aircraft.
EXPLANATION ON FLOW CHART DECISION STEPS
DECISION STEP A - CORROSION FINDING
There is a corrosion finding which is considered to be more than a negligible finding.
DECISION STEP B - BEYOND ALLOWABLE LIMITS
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The corrosion defect noticed on the considered aircraft is beyond the allowable limits as defined by the manufacturer (e.g. SRM, SB, etc.).
DECISION STEP C - AIRWORTHINESS AFFECTED
The corrosion defect is beyond the allowable limits which prevent the aircraft from flying in a safe condition.
When significant corrosion findings occur which could affect the structural integrity of the airplane Airbus can be consulted to determine whether or not
the airworthiness is affected. In this case all details of findings are to be promptly reported for detailed evaluation and the assistance required clearly
expressed.
DECISION STEP D - DUE TO A NON TYPICAL EVENT
For the purpose of the flow chart, a non-typical event is an event which is considered to be not representative of the events which normally occurs or
could occur in the concerned area.
As examples:


mercury spillage
corrosive fluid spillages when they are demonstrated to be exceptional, however when they are noticed to be systematic they cannot be
considered as non-typical.
DECISION STEP E - CUMULATIVE CORROSION
The corrosion in this area has been blended out previously and only at latest inspection the cumulative blend out now exceeds allowable limits as
defined by the manufacturer (e.g. SRM, SB, etc.).
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1.
2.
3.
4.
5.
6.
7.
8.
9.
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g) General rules applicable to the Structure Program
The Maintenance tasks are to be carried out” at or before" the limits stated for threshold, interval and 100% limit.
The Threshold is the time at which the first maintenance task is due.
 For items in FC or FH, the thresholds and 100% limits are counted from first flight.
 For items in Years, the thresholds and 100% limits are counted from date of initial delivery from manufacturer, unless otherwise stated.
For repeat maintenance tasks, the interval starts at the time of the last maintenance task performed.
The thresholds and intervals quoted in calendar time in this Program include aircraft time in and out of service. In other words, operators will not,
in general, be allowed to take credit for time out of service or storage periods to extend corrosion inspection intervals.
It is assumed that the structure to be inspected is in a state of cleanliness, which shall allow a satisfactory inspection to be carried out at the
required inspection level. Where existing Temporary Protection (TPS) permits un-obscured assessment of the condition of the structure, then
that Temporary Protection may remain in place for the inspection.
If damage is found or suspected (such as bulding skin) then the full extent of any damage must be clearly identified using appropriate inspection
techniques and/or disassembly when necessary. This may require additional access to that stated for the maintenance task.
All damage is to be evaluated and repaired in accordance with documentation acceptable to the relevant Airworthiness Authority.
If inspections indicate evidence of deterioration, appropriate further actions must be taken to prevent similar deteriorations from occurring in
Operator’s fleet.
For corrosion findings refer to § 5.2.3.5, Corrosion Prevention an Control Program, of this Introduction.
Inspection results related to SSIs to be reported to the manufacturer in accordance with the A318/A320/A320/A321 Structure Reporting System.
Ensure that all drain holes and drainage paths are clear from obstruction.
The following applies to Temporary Protection System application:

Prior to application of TPS, perform an inspection of the area at the inspection level for the task quoted in years.

Prior to re-fitting/re-connecting/re-installing parts removed to gain access to the inspection area, Temporary Protection System is to be
applied to each SSI as quoted in the task description (PDF Format) or in the TPS column (Excel Format), at least as frequently as the
calendar time threshold and interval columns of the respective SSI-task.
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CAUTION:
DO NOT APPLY TEMPORARY PROTECTIONS ON OXYGEN SYSTEMS, CONTROL CABLES, PULLEYS. TEFLON BEARINGS
AND LUBRICATED SURFACES MUST BE SHIELDED WHEN TEMPORARY PROTECTIONS ARE BEING APPLIED IN THESE AREAS. DRAIN
VALVES AND ALL OPEN ORIFICES ARE TO BE PROTECTED FROM INGRESS PRIOR TO TEMPORARY PROTECTION BEING APPLIED.
NOTE: The Type and Grade of TPS to be applied is indicated below the task description (PDF Format) or in thee TPS column (Excel Format) of the
Structures Program. Details of partial application of Temporary Protection System are provided as a Note in the TASK DESCRIPTION column when
applicable.
10. The access column may contain one of the following instructions concerning insulation blankets:

Insulation = Insulation to be removed from the inspection area.

Note 1 = Insulation to be displaced as required to complete the required maintenance task

Ensure wet insulation blankets are dried prior to re-installation, or replaced with new
11. The requirements quoted in years have been established by assuming aircraft operation in a "typical" environment. Operators who routinely
deviate from operation in a "typical" environment e.g. by transporting seafood products, should make appropriate adjustments to their program.
12. Inspection intervals recommended for surveillance of deterioration caused by the environment in fuel tank area (microbiological corrosion)
should be adjusted by individual operators, considering their own in-service experience and operational environment.
13. Based on reports made through the A318/A320/A320/A321 Structure Reporting System, AIRBUS will:

Inform all operators of any significant discrepancies discovered on the A318/A320/A320/A321 Fleet.

Make the appropriate recommendations.
14. Additional information concerning SSI inspections is provided in AIRBUS supporting publications for the A318/A320/A320/A321 aircraft:

– Maintenance Planning Document (MPD)

– Aircraft Maintenance Manual (AMM)

– Non-Destructive Testing Manual (NTM)

– Structure Repair Manual (SRM)

– Consumable Material List (CML)
15. All SSIs with "CPCP" quoted in the CPCP/ALI column are to be considered as CPCP SSIs.
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16. The condition of the paint system should be verified during the inspections. Re-protection should be applied where necessary.
17. “Touch and Go” Flight Cycles can be neglected if they are less than 5% of the total number of Flight Cycles up to threshold inspection or
between two consecutive inspections.
Each “Touch and Go” cycle above 5% is to be counted as one Flight Cycle, up to threshold inspection or between two consecutive inspections.

WEIGHT VARIANT APPLICABILITY

Some SSIs have different fatigue inspection requirements for the various Weight Variants (WV) of an aircraft type. The Weight Variant
represents the delivery standard of each aircraft.

The applicable Weight Variant for each individual aircraft can be found in Table 1 of the “Aircraft Allocation List” in the Structure Repair
Manual (SRM) introduction.

Table 2 of the “Aircraft Allocation List“ gives additional data for aircraft which have the Weight Variant status amended due to
modifications or Service Bulletin embodiment.

To minimize the number of individual inspection requirements, the Weight Variant requirements have been grouped where they are
similar. The Group number is stated in the Structures Program “APPLICABILITY“ column. Refer to the details below:

WV groups are only stated where necessary. In other cases the aircraft Model, e.g. A319, or aircraft model and series, e.g. A319–100,
have been retained where these cover all requirements.
MODEL/SERIES
GROUP
WEIGHT VARIANTS
A319-111
19-1A
001
A319-111
19-1B
002
A319-114
19- 1A
001
A320-214
N/A
010
A320-214
N/A
012
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h) Structure Program Reporting System
Operators shall report any findings to the manufacturer via the inspection reporting system on Airbus World/Maintenance and Engineering/Prepare
Maintenance/Optimize maintenance management/Optimize maintenance program/Report my check records.
The following rules apply to the reporting:
1.
2.
A completed Structural Inspection Report is required any time a structurally significant defect occurs.
The responsibility for reporting rests with the operator in accordance with SDM CAME section 1.16
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3. ZONAL ISPECTION PROGRAM
Where the term “Area” or “Zonal” is used in this document, this is to be interpreted to mean that a general visual inspection is made for general
condition, security and leaks in the structure, power plant, systems and components and their installation in the specified area or zone. The inspection
must be of sufficient depth to establish that any significant deterioration is identified and rectified to ensure that the general quality/condition of the
area/zone is satisfactory until the next higher inspection becomes due.
The inspections are specified by quoting the relevant zone number, zone description, access requirement, intervals and applicability.
The extent of the inspection is defined by the preparation and access requirements identification of access doors, positioning of surfaces, removal of
linings and the zone is to be inspected as visible with the relevant access open.
There are zones that will require more than one inspection at different intervals, because the depth at which the zone is to be examined may
necessitate differing levels of accessibility.
The inspection tasks check:




Structures by looking for signs of accidental damage, chafing, corrosion, cracks and for general condition of fasteners.
Systems installations for proper attachment and security (components, wiring, ducting, tubing, pulleys bearings electrical bonding, leaks,
chafing marks, etc.).
The general condition of any fairings, panels or other items which are removed/opened to gain access to a particular zone.
The items in the zone are to be visually inspected, from within touching distance where physically possible, unless otherwise stated.
a)
Interval of the Zonal Program
For the Zonal tasks the basic intervals are 4 months and multiples, 24 months and 48 months, 6 Years and 12 Years.
b) Zonal Program rules
Inspections are to be accomplished on each aircraft.
The routine content of inspections with frequencies below 4 MO be included in the Line Check List.
It is recognized that these inspections are of a lesser intensity than a General Visual Inspection, since they are to be performed 'from the ground, as far
as visible'.
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TASK N°
ZL-100-01-1
ZL-200-01-1
ZL-300-01-1
ZL-400-01-1
ZL-500-01-1
ZL-500-02-1
ZL-700-01-1
ZL-800-01-1
ZL-123-01-1
ZL-147-01-1
ZL-571-01-1
DESCRIPTION
Lower half of fuselage
Upper half of fuselage
Empennage and fuselage tail
Power plants, nacelles and pylons
Wings, L/H and R/H
Wing lower surface
Landing gear & landing gear doors
Doors
Nose Landing gear well
Main gear wheel hydraulic compartment
LH & RH main landing gear
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RECOMMENDED CALENDAR INTERVAL
36 hours (DAILY)
36 hours (DAILY)
36 hours (DAILY)
36 hours (DAILY)
36 hours (DAILY)
8 days (WEEKLY)
36 hours (DAILY)
36 hours (DAILY)
8 days (WEEKLY)
8 days (WEEKLY)
8 days (WEEKLY)
c) Guidance for accomplishment of a Zonal General Visual Inspection
A Zonal GVI requires a visual examination to detect obvious unsatisfactory conditions and discrepancies. It shall be performed from within touching
distance unless otherwise noted, that being the distance from the examiner’s eye to the area/item being inspected.
Flashlights and mirrors may be required to provide an adequate view of all surfaces.
There is no requirement for equipment removal or displacement unless this is specifically called for in the access instructions. However, should
unsatisfactory conditions be suspected, additional items may need to be removed or displaced in order to permit proper assessment.
Paint and/or sealant removal is not necessary and should be avoided unless condition is suspect.
It is expected that the area to be inspected is clean enough to minimize the possibility that accumulated dirt or grease might hide unsatisfactory
conditions that would otherwise be obvious. Any cleaning that is considered necessary should be performed in accordance with approved procedures
in order to minimize the possibility of the cleaning process itself introducing anomalies.
In general, the person performing the inspection is expected to identify degradation due to wear, vibration, moisture, contamination, excessive heat,
aging, etc. and make an assessment as to what actions are appropriate to address the noted discrepancy. In making this assessment, the person
performing the inspection shall take into account potential influence on adjacent system installations, particularly if these include wiring.
The following list is intended to clarify the type of deterioration that constitutes a discrepancy that is expected to be found and corrected. The list is not
intended to be exhaustive and may be amended or expanded as considered appropriate
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Structural Items/Assemblies
General: Deformations e.g. bulging skin joint, Corrosion, Cracks, Delamination or disbanding, Obstructed drain holes, Damage to hinges or latches,
Evidence of fluid spillage or pooled liquids
Accidental Damage: Dents, Impact marks, Scratches or gouges, Evidence of hail damage, Evidence of lightning strike, Evidence of FOD/bird strike
Fasteners: General condition of fasteners, Missing or broken fasteners
Surface Protection: Damaged, detached or missing sealant, Damaged, blistering or missing paint, Severely discoloured paint (evidence of corrosive
fluid spillage), Accumulation of contaminants (dirt, grease, skydrol etc …)
Repairs: Deterioration of previous repairs
Electrical installation (also refer to AMM Chapter 20 Standard Practices)
Wire/Wire Harnesses: Wire bundle/wire bundle or wire bundle/structure contact/chafing, Wire bundle sagging or badly secured, Wires damaged (large
scale damage due to mechanical impact, overheat, localized chafing etc.), Lacing tape and/or ties missing/incorrectly installed, Wiring protection
sheath/conduit deformity or incorrectly installed, End of sheath rubbing on end attachment device, Grommet missing or damaged, Dust and lint
accumulation, Surface contamination by metal shavings/swarf , Contamination by liquids, Deterioration of previous repairs
Connectors: External corrosion on receptacles, Backshell tail broken, Rubber pad or packing on backshell missing, No backshell wire securing device,
Fool proofing chain broken, Missing or broken safety wire, Discoloration/evidence of overheat on terminal lugs/blocks, Torque stripe misalignment
Switches: Rear protection cap damaged,
Ground points: Corrosion
Bonding braid/bonding jumper: Braid broken or disconnected, Multiple strands corroded, Multiple strands broken,
Wiring clamps or brackets: Corroded, Broken/missing, Bent or twisted, Faulty attachment (bad attachment or fastener missing), Unstuck/detached,
Protection/cushion damaged
Supports (rails or tubes/conduit): Broken, Deformed, Fastener missing, Missing edge protection on rims of feed through holes, Racetrack cushion
damaged
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The following item could be considered to be covered by the ZIP if access to the electrical power center, relay boxes etc. are added in the access
requirements:
Circuit breakers, contactors or relays: Signs of overheat
Hydraulic/Fuel/Water Waste/Oxygen/Fire Detection/Fire Suppression system installation
Seepage/leakage of liquid, Broken or incorrect wire locking, Pipes badly secured, Pipe/pipe or pipe/structure contact (check for chafing and restore
separation), Missing or broken clamps, Crushed/damaged pipes, Broken/disconnected bonding leads/jumpers, Deterioration of previous repairs,
Obstruction of smoke detectors, Plugged or damaged distribution nozzles
Air systems installation
Evidence of leakage on adjacent structure/components, Crushed/split ducts, Misaligned, missing or broken clamps, Ducting badly secured,
Mechanical systems installation
Bent/crushed control rods, Sagging control cables, Excessively worn, frayed or kinked control cables, Excessively worn fairleads, Extruded bearing
liners, Broken or incorrect wire locking, Significant corrosion on cables, threads
Cargo Systems
Split/holed compartment liners, Seal damage, Excessively worn rollers (sign of jamming and resultant overheat), Missing/damaged stops/latches,
Damaged cargo net restraining attachments
Engines/Pylons
Blade damage (e.g., nicks, cracks), Blades rub (on rubstrip), Vane damage, Cowling damage, Loose or migrating fasteners and bushings (due to
vibration), Discoloration (due to heat damage), Foreign Object Damage (FOD), Damage due to bird strike/ingestions,
General
Illegible labels, Condensation in windows, Window crazing, Oil canning
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4. TIME CONTROLLED ITEMS
This section contains tasks extracted from the section 3 (of this Scheduled Maintenance Program) covering “Time Control Items”. The list of Life
Limitation Items (e.g. landing gear life limited parts) is provided as part of the Airworthiness Limitation Section (ALS): Part 1: Safe Life Airworthiness
Limitation Items




Part 2: Damage-Tolerant Airworthiness Limitation Items
Part 3: Certification Maintenance Requirements
o CMR document - EASA version
o CMR document - FAA version
Part 4: For Ageing System Maintenance
Part 5: A318 / A319 / A320 / A321 Fuel Airworthiness Limitations
The above documents are available on Airbus World e-site via “Maintenance & Engineering/Prepare Maintenance/Prepare Maintenance
Program/Review Airbus maintenance requirements”. The Airworthiness Limitation Section (ALS) revision follow up is under operator responsibility.
Engine and APU Life Limited parts are available in separate documents (applicability of the parts associated to engine and APU, not to aircraft MSN).
5. ADDITIONAL PROGRAMS
a) Tasks related to Mandatory Life Limitations, Certification Maintenance Requirements (CMR) and Airworthiness Limitation
Items (ALI)
This Maintenance Program includes all maintenance requirements, including frequencies, arising from aircraft certification activities.
CMR tasks and task intervals resulting from systems safety assessment are given in AIRBUS Document ALS Part 3.
Fatigue related structural inspections (ALI) arising from the damage tolerance evaluation are given in AIRBUS Document ALS Part 2.
When applicable, these tasks are included in this A319/A320 SDM Maintenance Program and are identified in the “SOURCE” column.
b) Tasks related to Enhanced Zonal Analysis Procedures (EZAP)
The Enhanced Zonal Analysis procedure (EZAP) permits appropriate attention to electrical wiring installation within a zone. The Enhanced Zonal
Analysis procedure must be performed for all zones containing wiring where both of the following criteria are met:
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Presence of combustible material
Potential for arcing in case of wiring insulation damage prone to cause fire ignition
Tasks arising from the Enhanced Zonal Analysis Procedure (EZAP), comprised of GVI tasks not fully covered by Zonal tasks and DI/RS tasks are
included within ATA 20 and have no Failure Effect Category (FEC) quoted. The tasks are identified with “(EZAP)” following the task description.
NOTE: The term “wiring” in the task description of ATA 20 tasks includes all electrical wiring installations (e.g. cables, conduits, clamps, etc. …) .
NOTE: ATA 20 tasks must not be deleted from the operators maintenance program.
c) Tasks related to Airworthiness Directives
Airworthiness Directives (AD) and Consignes de Navigabilité (CN) are mandatory instructions issued by the prime Certification Authority,


when it considers that an unsafe condition exists in a product
that condition is likely to exist or develop in other products of the same type design
No person may operate a product to which AD or CN applies except in accordance with the requirements of the AD or CN.
AD and CN are issued by the Authority to regularly address airworthiness or safety issues. These requirements generally require inspection or
modification of aircraft, aircraft component or changes to procedures within a specific period of time.
When applicable, repetitive AD’s and CN’s are included in this A319/A320 SDM Maintenance Program and are identified in the “SOURCE” column.
d) Tasks related to SDM requirements
SDM issues additional maintenance requirements. Procedures are in place to assess all applicable SDM requirements on a continuing basis for
applicability to aircraft maintained to this Maintenance Program.
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e) Reliability Program
The initial maintenance requirements are outlined in the Maintenance
Review Board (MRB) Report. The intervals specified may be escalated by
the operator in accordance with the following procedure:
Step 1: Determine desired interval
The desired interval should be assessed in consideration of various factors
including utilization, availability, resources, environment, and experience.
Step 2: Review program for exceptions
The program should be reviewed for the more obvious exceptions to the
proposed interval increase such as inspections required by CMR’s, ALI’s,
AD, national requirements, life limited items.
Special attention to be given to items with intervals given with an MRB FEC
8 and 5.
Step 3 : Maintenance program findings
List findings from previous checks and decide, in view of the findings, which
items have potential for interval increase.
Findings analysis may also conduct to downgrade to lower interval or to
maintain the existing one.
Provide justification for items with potential for interval increase.
Step 4: Review reliability program
Review reliability program for findings associated with scheduled and
unscheduled maintenance. Classify findings against check item and decide,
in view of the findings, which items have potential for interval increase.
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Provide justification for items with potential for interval increase.
Step 5 : Assemble information
Assemble information obtained through previous steps. This should contain:


background data such as checks previously performed, fleet statistics, reliability statistics etc. …
justification data in form of tables listing all concerned tasks giving :
o MRB reference and MRB interval
o current airline reference and interval
o findings arising from maintenance
o findings arising from reliability program
o proposal - interval increase or exception
o justification against task interval increase proposal where there are findings from maintenance or from reliability program.
Step 6: Internal approval
The interval increase should be internally approved on the basis of the information given.
Step 7: Submit to SDM Airworthiness Authorities for approval
The request for internal increase is then submitted to the operator’s regulatory authorities for formal approval.
Step 8: Substantiation
Once interval increases are implemented, the maintenance and the reliability program should be monitored for adverse effects or trends resulting from
interval.
f) Engine Health Monitoring
Engine parameters like EGT, Fuel Flow, N2 and N1, will be recorded by the Aircraft Condition Monitoring System and sent to a ground station. The
parameters are continually analyzed and, if necessary, will result in a corrective maintenance action. For the complete procedure refer to SDM CAME
1.26.9 Engine condition monitoring program.
The purpose of the engine performance trend monitoring is to:
 Assess engine performance and health
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




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Provide engine indicating system fault detection
Prevent an unexpected engine problem
Reduce unscheduled maintenance
Monitor the engine guaranties
Reduce operational overhaul costs
The record of flight data in takeoff and cruise condition is performed automatically through an on board system.
g) Maintenance applicable to specific aircraft operations
The Maintenance Program contains the necessary tasks required to ensure continued compliance with special authorizations.
All Weather Operations
The objective of CAT2 and CAT3 operations is to provide a level of safety when landing in low visibility conditions. This possibility is achieved thanks to
different systems installed on aircraft.
Indeed the Single Aisle aircraft are fitted with automatic landing systems able to control the aircraft to touchdown (CAT 3A) or through rollout (CAT 3B),
and with monitoring systems able to determine the landing capability and downgrade.
Depending on the equipment/systems available, the monitoring function will provide the crew with the landing capability through a displayed on FMA
and/or ECAM (if case of failure), and also with a downgrade capability. The crew will be thus warned about a possible downgrade of the aircraft
possibilities.
To determine that an aircraft can operate CAT 3 condition Airbus considers that the LAND test (AMM 22.97.00.710) is sufficient.
RVSM Maintenance Practices
RVSM capabilities are inherent functions of the basic standard of the aircraft. Scheduled tasks necessary for these operations have been considered in
the development of this program. MSG-3 analysis has confirmed that neither scheduled maintenance tasks nor specific recommendations on RVSM
involved parts are needed on any aircraft type to hold their RVSM capability. Additional information is available in Airbus Service Information Letter 34064.
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ETOPS
ETOPS capabilities are inherent functions of the basic standard of the aircraft. Schedule tasks necessary for these operations have been considered in
the development of this program. ETOPS related task coming from the ETOPS Configuration, Maintenance and Procedures (CMP) Document have
been implemented in this program and highlighted in the source column as "CMP".
The basic aircraft is capable of 180 min single engine diversion time.
Modifications concern the supply of some systems in electrical emergency conditions and their reliability as required by the applicable ETOPS
Configuration Maintenance and Procedure (CMP) document at the time of aircraft delivery.
ETOPS operation authorization can only be obtained through application by the operator to its national authority. During the operational life of the
aircraft, additional modifications may be necessary to maintain systems reliability at the required level.
h) Maintenance applicable to Customer furnished equipment
This maintenance program contains the necessary tasks required to ensure continued airworthiness of equipment specified or furnished by other than
the constructor. The need for routine tasks has been assessed in accordance with the CMM.
i)
Vital points and control systems
Whenever inspections are made or work is undertaken on vital points, flying or engine control systems, a detailed investigation must be made on
completion of the task to ensure that all tools, rags or loose articles which could impede the free movement or safe operation of the system(s) have
been removed and that the system(s) and installation in the aircraft zone are clean and unobstructed.
If, as a result of the application of tasks associated with the Program, any part of either the main or any associated system is dismantled, isolated,
adjusted, repaired or renewed, that part of the system(s) which has been disturbed shall be subjected to a duplicate inspection, with free movement,
range, direction and tension checks and shall be certified in the Technical Log.
j)
Engine maintenance policy - Twin engine aircraft
The twin-engine maintenance policy adopted by Operator is designed to ensure continued airworthiness of the fleet and covers the aircraft fuel feed
system as well as the engines. Staggered maintenance is the separation of similar tasks on the same systems or components of both engines or fuel
systems.
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k) Parking and Storage procedures
For parking and prolonged parking procedures: refer to AMM Chapter 10. For the return to service procedure: refer to AMM Chapter 10.
l) Special maintenance
Special Inspections have to be performed after exceptional conditions such as but not limited to:
– Hard or overweight landing
– Lightning strike
– Hail
– Flight in excessive turbulence or in excess of VMO/MMO
– Bird strikes
All these inspections are defined in the AMM Chapter 05.
m) Inter season maintenance
Special maintenance is required to transit AC between cold and warm seasons in SDM operating environment. This maintenance is covered by JIC
A320-00-04 and A320-00-04-2 (to be done prior winter operations only).
n) Aircraft weighing
General
Weighing requirements are defined according to SDM/EU Part CAT requirements and performed by means of MP task 000001-01-1-SDM
New production aircraft weighed at the manufacturer are eligible to be placed into operations without reweighing if no or minor change and equipment
installation are accomplished by the operator.
Each airplane must be weighed after major repair or modification unless reliable data allowing analytical calculation of weight and balance change are
available.
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Weighing periods and procedure
The weighing task interval is 48 months specified by EU PART CAT (EU) No 965/2012 and 60 months specified by BDCA OTAR 39.81. The strictest
interval is used. Also aircraft will be weighed after major repair or after major alteration unless reliable data allowing analytical calculation of weight and
balance change are available.
The weighing procedure will be carried out according to AMM Chapter 08. Weighing, results will be calculated in accordance with A319/A320 SDM
procedures.
o) Test flights (non-revenue flights following maintenance actions)
Aircraft Maintenance Manual Chap 5 and A319/A320 SDM procedures define the procedures that require a subsequent Check Flight after
maintenance.
Check flights following maintenance actions are not required by AIRBUS except for actions involving items that cannot be properly ground tested to
verify that the aircraft operational characteristics have not been adversely affected.
p) Individual structural inspections
Aircrafts that have individual limitations and inspections driven by structural damages or repairs are listed in the dedicated section V of the
maintenance program.
q) Periodical inspections driven by STC modifications and supplemental requirements
Continued airworthiness instructions that require periodical inspections that are part of modifications (not repair) are included in the current
maintenance program with the reference to the STC document.
r)
Human factors and Critical Task Control
SDM uses Airbus Job Cards and AMM references for the maintenance events where all of the human factors best practices already implemented.
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STANDARDS, DEFINITIONS AND ABBREVATIONS
1. GENERAL STANDARD
Unless otherwise stated, all inspection requirements are to be applied without removing an item from the aircraft or dismantling the item, group or subassembly unless dismantling is considered essential in order to ensure airworthiness. Where dismantling is required by this Program, this is stated
against the item concerned. If the inspection requires clarification, the following inspection standards shall apply:
a) Check/Inspect
The term “Check/Inspect” as used in this document, is construed to mean a maintenance action requiring thorough examination of an item, component
or structure for general condition, as applicable, with special emphasis directed to the following areas:
Proper attachment, safety wiring, cotter pins, fasteners, clamps, latches, tubing, plumbing, electrical wiring and connections, linkages, bearings,
alignment, clearance, lubrication, obvious damage, cracks, delamination, fraying, operating pressure, fluid leakage, excess wear or play, corrosion,
evidence of overheating, rubbing, aging, preservative coating or finish, cleanliness and general appearance.
Inspections to the above requirements must comply with the minimum standards set out in regard to the material from which the item is made and
applying these standards wherever physically possible. The depth or degree of application being at the discretion of the signatory.
b) Metal Parts
e.g. applicable to all metal parts, bodies or casings of units in systems and in electrical, instrument and radio installations, metal pipes, ducting, tubes,
rods, levers.
Inspect for: Cleanliness, external evidence of damage, leaks, overheating or discharge. Fluid ingress. Obstruction of drainage or vent holes or overflow
pipe orifices. Correct seating of fairings and serviceability of fasteners.
Free from: Distortion, dents, scores, chafing, pulled or missing fasteners, rivets, bolts, screws. Evidence of cracks and wear. Separation of bond,
failure of welds and spot welds. Deterioration of protective treatment and corrosion. Security of attachments, fasteners, connections, locking and
bonding.
c) Rubber, Fabric, Glass Fibre and Plastic Parts
e.g. coverings, ducting, flexible pipes, flexible mountings, seals, insulation of electrical cables, windows, etc.
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Inspect for: Cleanliness, cracks, cuts, chafing, kinking, twisting, crushing, contraction - sufficient free length. Deterioration. Crazing. Loss of flexibility
(other than fabric covered components), overheating. Fluid soakage. Security of attachment (supports, packing and electrical bonding correctly
positioned, serviceable and secure) connections and locking.
d) Control System Components
Inspect for: Correct alignment - no fouling. Free movement. Distortion. Evidence of bowing. Scores. Chafing. Fraying. Kinking. Evidence of wear.
Flattening. Cracks, loose rivets. Deterioration of protective treatment and corrosion. Electrical bonding correctly positioned, undamaged and secure.
Attachments, end connections and locking secure.
e) Electric Motors, Alternators, Generators and Actuators
Inspect for: Cleanliness, obvious damage, evidence of overheating, corrosion and security of attachments and connections. If protective covers are
required to be removed: Cleanliness, scoring, pitting, brushes free in holders, nor excessively worn and correct bedding. Adequate spring tension.
Overheating. Fluid ingress.
f)
Relays, Solenoids and Contactors
Inspect for: Cleanliness, obvious damage, evidence of overheating, corrosion and security of attachments and connections. If protective covers are
required to be removed: Cleanliness, pitting or burning of contacts, evidence of overheating and security of contacts exposed.
g) Critical Design Configuration Control Limitations (CDCCLs)
A CDCCL is a limitation requirement to preserve a critical ignition source prevention feature of the fuel system design that is necessary to prevent the
occurrence of an unsafe condition.
The purpose of the CDCCL is to provide instructions to retain the critical ignition source prevention feature during configuration change that may be
caused by alterations, repairs, or maintenance actions. For details refer to ALS Part 5, FAL document, latest revision (see chapter 1 Item B).
A critical ignition source prevention feature may exist in the fuel system and its related installation or in systems that, if a failure condition were to
develop, could interact with the fuel system in such a way that an unsafe condition would develop in the fuel system without this limitation.
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Operators are responsible for ensuring that their internal documentation is amended to reflect the data contained within this section and provides
appropriate text to highlight the existence of each CDCCL. Such identification is necessary in the instructions used by the person performing an
installation, alteration, repair or modification so as to minimize the risk that the work performed compromises the original design criteria.
Regulatory oversight of the operator’s compliance with this mandatory requirement is based on the appropriate identification of the CDCCL in the
accomplishment instructions associated with the installation, alteration, repair or modification.
2. GLOSSARY
For the purpose of this Maintenance Program the following glossary terms apply:
Accidental Damage (AD)
Physical deterioration an item caused by contact or impact with an object or influence, which is not a part of the aircraft, or by human error
during manufacturing, operation of the aircraft, or maintenance practices.
AD-HOC JIC
Job instruction card that have its own time requirements and period of accomplishment. AD-HOC JIC can only be linked to the finding
Workorder (workorder raised to record and plan for the rectification of finding).
AMOS
Information system solution developed by Swiss-AS (http://swiss-as.com/) for the customers solve the Continuing Airworthiness, Maitenance,
Logistics and Resources management. All SDM maintenance planning, accomplishment and reporting activities are held in this system.
Airworthiness Limitations
A section of the Instructions for Continued Airworthiness that contains each mandatory replacement time, structural inspection interval, and
related structural inspection procedure. The information contained in the Airworthiness Limitations section may be changed to reflect service and/or
test experience or new analysis methods.
APU Change (APUC)
The interval term "APU Change" means the opportunity arising at some time between initiating removal of an APU and completing installation
of an APU, irrespective of whether the same APU is reinstalled or it is replaced by a new or overhauled one.
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APU Cycle(s) (APU CY)
A complete APU cycle.
APU Hour(s) (APU HR)
The APU operating time from start-up to shutdown.
Calendar Times (MO, YE)
Month(s): a period of 30 or 31 consecutive days depending on the month. Year(s): a period of 12 consecutive months.
Certification Maintenance Requirement (CMR)
A maintenance task with particular limitations arising from the Type Certification process.
Condition Monitoring (C/M)
“Condition Monitoring” (C/M) is a maintenance control process that relies on routine surveillance and evaluation of airplane system and/or
component performance as its primary criteria for continuing component service. Condition Monitoring Programs consist of data collection and analysis
systems which an operator uses to identify failure trends and attempts to identify corrective action that would preclude the continuation of
unsatisfactory service experience of a particular component or system. Simply, operators must collect and analyze component or system failure data
and implement corrective maintenance actions when set alert levels are surpassed.
This evaluation Program may be based on data collected but is not limited to the following sources: flight and/or cabin crews, airplane Built-in
Test Equipment (BITE), Airborne Indicating Detection Systems (AIDS), and equipment for ground check out of system performance may be used for
C/M. Other basic elements of a C/M Program may include data on: Unscheduled removals, maintenance log entries, pilot reports, sampling
inspections, functional checks, bench checks, shop findings and other sources of data pertinent to the determination of continued service. Operators
should bear in mind that failure of components which utilize C/M as their maintenance control process must not have direct adverse effects on
operating safety.
Damage Tolerant
A qualification standard for aircraft structure. An item is judged to be damage tolerant if it can sustain damage and the remaining structure can
withstand reasonable loads without structural failure or excessive structural deformation until the damage is detected.
Engine Change (EC)
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The interval term "Engine Change" means the opportunity arising at some time between initiating removal of an Engine and completing
installation of an Engine, irrespective of whether the same Engine is reinstalled or it is replaced by a new or overhauled one.
Engine Cycle(s) (CY)
A complete engine thermal cycle which includes the application of take-off power.
Environmental Deterioration (ED)
Physical deterioration of an item’s strength or resistance to failure as a result of chemical interaction with its climate or environment.
Fatigue Damage (FD)
The initiation of a crack or cracks due to cyclic loading and subsequent propagation.
Flight Cycle(s) (FC)
A complete take-off and landing sequence.
Flight Time
The Flight Time period referenced in this Maintenance Program is based on “Airborne Time” or “Time in Service”.
Fuel Conservation
When applicable, the repetitive scheduled tasks related to fuel conservation are included in this maintenance Program. In order to carry out
more efficiently the water drain at required interval especially during winter season AMM task 123228-281-001 (tank water drain) provides two
alternatives to de-ice water drain valves.
1. Use of air heater directly on the water drain valve. This procedure in mainly for isolated case event and is not useful for an entire fleet.
2. Alternatively it is recommended to refuel the aircraft with "warm" fuel, 2 to 3 hours prior the first flight of the day. This would allow ice to
melt and water to settle down for efficient drainage.
In addition as alternative procedure, use an anti-icing additive in the fuel (as per AMM 123128-660-001) to prevent any water in the fuel
freezing. The water drain procedure may therefore be carried out more efficiently at the required interval.
Interval
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The period expressed in Letter code, cycles, hours and/or calendar time, between successive accomplishments of a specific task.
Landing
An operation of an aircraft touching the runway and coming to a complete stop or performing a "touch an go".
Maintenance Task
An action or set of actions required to achieve a desired outcome which maintains an item (component, system/sub-system, structure) in or
restores an item to serviceable condition. This term includes inspection and determination of condition.
Maintenance Significant Item: (MSI)
Item identified by the manufacturer, whose failure:




Could affect safety (ground or flight), and/or
Is undetectable during operation, and/or
Could have significant operational economic impact, and/or
Could have significant non-operational economic impact.
MSG-3
Maintenance Steering Group 3. A task-oriented methodology used to develop an initial maintenance program.
NDT-Inspection: (NDT)
Non-destructive inspection procedure, e.g. eddy current, ultra sonic, X-ray, thermography…
Normal duties
Those duties associated with the routine operation of the aircraft, on a daily basis, to include the following:


Procedures and check performed during aircraft operation
Recognition of abnormalities or failures by the operating crew through the use of normal physical senses (e.g., odour, noise, vibration,
temperature, visual observation of damage or failure, changes in physical input force requirements, etc.).
Repeat Interval
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The maximum permitted period (for all tasks not performed on a sampling basis) that can separate total completion of a task from its next
accomplishment.
Operating Crew
Qualified cockpit and cabin attendant personnel who are on duty.
Other Structure
Structure which is judged not to be a Structural Significant item. “Other Structure” is defined both externally and internally within zonal
boundaries.
Replacement: (RAR)
The action whereby an item is removed and another new or restored item is installed in its place.
Safe Life Structure
Structure with is not practical to design or qualify as damage tolerant: its reliability is protected by discard limits which remove items from
service before failures are expected.
Sampling: (SPL)
The monitoring and/or withdrawal of selected devices from service to permit determination of their condition at predetermined progressive
intervals.
Sampling Inspection Program
Inspection of specific aircraft selected from those which have the highest age to identify the first evidence of deterioration in their condition
caused by corrosion or fatigue damage.
Scheduled Maintenance Check
Any of the maintenance opportunities with are pre-packaged and are accomplished on a regular basis.
Service
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The term “Service” implies that a component or system should be checked and serviced with fuel, oil, grease, water, oxygen, etc., to a level or
condition specified by the applicable manufacturer, vendor and/or by the Operator. “Service” may also be used to indicate that filter cleaning or
replacement is recommended.
Structure Significant Item: (SSI)
A structural detail, structural element or structural assembly which is judged significant by the manufacturers because of the reduction in aircraft
residual strength or loss of structural function which are consequences of its failure.
Task - Maintenance
An action or set of actions to achieve a desired outcome which restores an item to or maintains an item in serviceable condition, including
inspection and determination of condition.
Threshold: (TH)
Limit deadline for all tasks not performed on a sampling basis at which the task must be accomplished for the first time (subsequent
accomplishment deadlines are obtained by adding the repeat interval and its multiples to the threshold).
Touch and Go
A "Touch and Go" is a landing in which an aircraft touches the runway and does not come to a full stop prior to commencing an additional flight.
Workorder
Document with the unique number raised in the SDM AMOS system. Workorder contains maintenance actions either scheduled or
unscheduled, have FH/FC/Days limit and can be in status Closed or Opened.
3. ABBREVIATIONS
JIC
:
Job Instruction Card
NDT
:
Non Destructive Testing
NLG
:
Nose Landing Gear
NR
:
National Requirements
NRV
:
Non Return Valve
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NT
:
Note
NTM
:
Non Destructive Testing Manual
OEM
:
Original Equipment Manufacturer
OP
:
Operational Check
PCU
:
Power Control Unit
PFD
:
Primary Flight Display
POB
:
Pressure off Brakes
PTT
:
Press to Test
PTU
:
Power Transfer Unit
QAD
:
Quick Attach Detach
RAT
:
Ram Air Turbine
RH
:
Right Hand
RMP
:
Radio Management Panel
RS
:
Restoration
RSVR
:
Reservoir
RVSM
:
Reduced Vertical Separation Minima
SB
:
Service Bulletin
SDI
:
Special Detailed Inspection
SIL
:
Service Information Letter
SMR
:
Scheduled Maintenance Report (engine)
SOV
:
Shut off Valve
SSI
:
Structure Significant Item
ST(G)R
:
Stringer
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SV
:
Servicing
STC
:
Supplemental Type Certificate
SYS
:
System
TBD
:
To Be Determined
TCAS
:
Traffic Collision Avoidance System
TE
:
Trailing edge
THS
:
Trimmable Horizontal Stabilizer
TPS
:
Temporary Protection System
TR
:
Temporary Revision
ULB
:
Underwater Locating Beacon
VC
:
Visual Check
VHF
:
Very High Frequency
VR
:
Vendor Recommendation
YE
:
Year
SRT
:
Single-Running Task
OEM
:
Original Equipment Manufacturer
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4. ATA CHAPTERS
12
Servicing
32
Landing Gear (Mechanical)
56
Windows
20
Control Cables
33
Lights
57
Wings
21
Air Conditioning & Pressurization
34
Navigation
70
Standard Practices - Engine
22
Auto Flight
35
Oxygen
71
Power plant
23
Communications
36
Pneumatic
72
Engine
24
Electrical Power
38
Water/Waste
73
Engine Fuel & Control
25
Equipment & Furnishings
47
Inert Gas System
74
Ignition
26
Fire Protection
49
Airborne Auxiliary Power Unit (APU)
75
Air
27
Flight Controls
51
Fuselage Drains
76
Engine Controls
28
Fuel
52
Doors (Mechanical)
77
Engine Indicating
29
Hydraulic Power
53
Fuselage
78
Exhaust
30
Ice & Rain Protection
54
Nacelles/Pylons
79
Oil
31
Indicating & Recording System
55
Stabilizers
80
Starting
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5. TASK CODES AND MAINTENANCE OPERATIONS
TASK
CODE
DEFINITION
BSI
Borescope Inspection
CHK
Check. Task performed to ensure that a system or component is still serviceable or that pressures or fluid levels are correct.
Check for condition, leaks, circuit continuity, Check fluid reserve on item, Check tension and pointer, Check fluid level, Check detector,
Check charge pressure, Leak Check / Test.
DET
Detailed inspection. An intensive examination of a specific item, installation or assembly to detect damage, failure or irregularity. Available
lighting is normally supplemented with a direct source of good lighting at an intensity deemed appropriate. Inspection aids such as mirrors,
magnifying lenses etc. may be necessary. Surface cleaning and elaborate access procedures may be required.
DIS
Discard. The removal from service of an item at a specified life limit.
FNC
Functional Check. A quantitative check to determine if one or more functions of a system/sub-system or component performs, within
specified limits. This task may call for the use of special test equipment.
GVI
General Visual Inspection. A visual examination of an interior or exterior area, installation or assembly to detect obvious damage, failure or
irregularity. This level of inspection is made from within touching distance unless otherwise specified. A mirror may be necessary to ensure
visual access to all surfaces in the inspection area. This level of inspection is made under normally available lighting conditions such as
daylight, hangar lighting, flashlight or drop-light and may require removal or opening of access panels or doors. Stands, ladders or platforms
may be required to gain proximity to the area being checked.
LUB
Lubrication. Term covering all types of lubrication (grease gun, squirt can, spray, brush or hand application) for the purpose of maintaining
the inherent design operating capabilities of an item.
OPC
Operational Check. A task to determine that an item is fulfilling its intended purpose. Do not require quantitative tolerances. This is a failure
finding task.
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DEFINITION
RST
Restoration. That work (on/off the aircraft) necessary to return the item to a specific standard. Restoration may vary from cleaning or
replacement of single parts up to a complete overhaul.
SDI
Special Detailed Inspection. An intensive examination of a specific item, installation, or assembly to detect damage, failure or irregularity.
The examination is likely to make extensive use of specialized Inspection Techniques and/or equipment. Intricate cleaning and substantial
access or disassembly procedure may be required. When such inspections are required, detailed NDT procedures are described in the
A318/A320/A320/A321 Nondestructive Testing Manual (NTM).
SVC
Servicing. The term “Servicing” implies that a component or system should be checked and serviced with fuel, oil, grease, water, oxygen,
etc., to a level or condition specified by the applicable manufacturer, vendor and/or by the Operator. “Service” may also be used to indicate
that filter cleaning or replacement is recommended.
TPS
Temporary Protection System application.
VCK
Visual Check. An observation to determine that an item is fulfilling its intended purpose. Does not require quantitative tolerances. This is a
failure finding task.
6. TASK INFORMATION
Manufacturer's and vendors recommendations and/or requirements are published through Service Bulletin (SB), Service Information Letter (SIL), Alert
Operator Transmission (AOT), Component Maintenance Manual (CMM) and other documents dealing with maintenance.
For engines, APU, and main components, manufacturer's manuals for additional tasks once the engines or the components are in the shop should
also be considered.
Refer to Airbus technical publications (Aircraft Maintenance Manual, Non Destructive Testing Manual) for maintenance practices and procedures.
For Operator/Airbus common benefit significant maintenance information should be reported to manufacturer in view of further development of the
Maintenance Planning Document.
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ZONAL DIAGRAMS
The main aircraft zones are defined in the following pages. Refer to AMM: 06-20-00 for the details

MAJOR ZONES, A/C: A320

MAJOR ZONES A/C A319
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
MAJOR SUB-ZONES A/C A320, Fuselage and Vertical Stabilizer

MAJOR SUB-ZONES FUSELAGE AND VERTICAL STABILIZER, A/C: A319
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
MAJOR SUB-ZONES – WING AND NCALLE (LEFT AND RIGHT)
A/C A320

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MAJOR SUB-ZONES, WING AND NACELLE (LEFT AND RIGHT),
A/C A319
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
ZONES - FUSELAGE AND VERTICAL STABILIZER, A/C A320

ZONES - FUSELAGE AND VERTICAL STABILIZER, A/C A319
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
ZONES – DOORS, A/C A320

ZONES - DOORS A/C A319
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
ZONES – WING AND HORIZONTAL STABILIZER (LEFT AND
RIGHT SIDES), A/C: A320

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ZONES – WING AND HORIZONTAL STABILIZER (LEFT AND
RIGHT SIDES), A/C: A319
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
ZONES – LANDING GEAR, A/C: ALL

ZONES – NACELLES – LEFT AND RIGHT SIDES, A/C: ALL
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MAINTENANCE PROGRAM LAYOUT
The tasks are listed per increasing ATA chapter.
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1. REV
Revision code column shows revision status of the task: R- revised; N - new task; D – deleted task.
2. TASK NUMBER
A specific task number identifies each task. When a task applies to two specific main zones located symmetrically to either side of the aircraft centre
line, the task is assigned a single task number, both LH and RH zones are indicated in «ZONE» column.
The task number comprises 9 to 10 digits organized as follows: XX XX XX—XX—(X)X—SDM—LH/RH/CTR
First 6 digits
=
ATA reference or zone
Next 2 digits
=
Sequence number identifier
Single or 2 last digit
=
Applicability index
3 letter suffix —SDM
=
Specific Operator task identifier
LH/RH/CTR
=
Left Right or Center
Sequence number: Apart from a few cases, the sequence number is used to discriminate between different tasks relating to the same hardware.
Applicability index: The applicability index identifies successive developments of a task, introduced by modifications or specific requirements. As a
general rule, tasks with the same first 8 digits in the task number, have the same work description in the AMM.
Zonal tasks:
The zone number is preceded by the letter code «ZL». For task affecting symmetrical zones, the LH side zone number is used (for ATA 100 zoning to
AMM chapter 06-20)
3. ZONE COLUMN
Zone allocation has been made according to the following rules:

If task involves only one zone, the relevant zone number is indicated. If task involves two distinct symmetric zones, both LH and RH zone
numbers are indicated.

If task involves a zone or compartment equally displaced around the aircraft center line, which is normally quoted by its LH and RH side
zone numbers (e.g. 131/132 : FWD Cargo Compartment), only the left hand zone number (i.e. 131) is indicated but the task description
clearly covers both side of the zone or compartment.
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If task involves several zones for access, action and result, the most appropriate zone number(s) will be indicated.
4. DESCRIPTION COLUMN
This column provides the following information:

Task title: Identifies the system/sub-system/component/zone/structural significant item concerned by the task.

Task description: Gives a concise description of the test or inspection to be performed.

Task preparation data (where applicable ) : Specifies the preliminary steps to be performed prior the maintenance task itself.

Access (where applicable ) : Specifies the identifiers of the access panels, linings or doors to be opened or removed for accomplishment of the
task.

Floor panels of passenger cabin and cargo holds are not designated by their identifiers but by the frame numbers between which the floor
panels have to be removed.
5. SKILL CODE
Skill codes, specifying the type of skill required for task accomplishment:
Skill Code
Definition
AF
AIRFRAME:
AV
INSTRUMENT:
Comments
Hydro-mechanical, environmental, fuel, oxygen and cargo systems.
Associated servicing requiring a certain qualification such as:
 Flaps/Slats
 Landing Gear
 THS actuator
 Structure Visual Inspection
 ZONAL GVI including EWIS





Autopilot.
Instruments.
Digital equipment.
Fire protection
Lighting, windscreen ice and rain
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Comments
CA
Cabin/Utility
Furnishing, galleys
EL
ELECTRICAL:
Electrical generation, distribution and associated services and components.
EN
Power Plant:
NDT
NON DESTRUCTIVE
TESTING :
RA
RADIO:
UT
UTILITY:


Engines and APU accessories
Associated services
All Non-destructive test inspection and borescope inspection.


Radio and radio navigation.
Audio interphone, CVR, Pax address.
Toilets water, waste water.
6. TASK CODE
Task Code: Codes defining the type of task to be carried out. Ref to the part “TASK CODES AND MAINTENANCE OPERATIONS” for the details
7. INTERVALS
This column provides the following information:
100% Inspection Threshold:
This information, preceded by the letter «T», gives a specific value defining the first accomplishment deadline of the task. When threshold is equal to
the interval, the letter “T” may not show.
When the threshold is expressed in several units, the conjunction “OR” separate the different indications.
100% Inspection Task interval:
This information, preceded by the letter «I», gives a specific value defining the maximum time that can separate two complete accomplishments of the
task. When the interval is expressed in several units, the conjunction “OR” separates the different indications.
Sample Inspection Threshold:
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This information, preceded by the letter “ST”, gives a specific value defining the first accomplishment deadline of the task. When threshold is equal to
the interval, the letter “ST” may not show.
When the threshold is expressed in several units, the conjunction “0
OR” separates the different indications.
Sample Inspection Interval:
This information, preceded by the letter “SI”, gives a specific value defining the maximum time that can separate two complete accomplishments of the
task. When the interval is expressed in several units, the conjunction “OR” separates the different indications.
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8. SOURCE
CPCP
:
Task originated from Corrosion Prevention and Control Program.
EZAP
:
Enhanced Zonal Analysis Procedure requirements.
FAL
:
Task originated from Fuel Airworthiness Limitation
AD/CN
:
Task originated from an Airworthiness Directive.
ALI, ALI WFD
:
Task originated by Airworthiness Limitation Section (ALS) Part 2 - Airworthiness Limitation Items
arising from fatigue and damage tolerance evaluation of damage tolerant structural elements
whose failure could contribute to catastrophic failure of the aircraft (FAR/JAR 25.571) and
Airworthiness Limitation Items arising from an initial evaluation of Widespread Fatigue Damage
ASM
:
Task originated by Airworthiness Limitation Section (ALS) Part 4 - Ageing System Maintenance
CMR*
:
Task is an Airworthiness Limitation Section (ALS) Part 3 task – Certification Maintenance
Requirement. Its interval cannot be escalated by an Operator, without the concurrence of the
Primary Certification Authority (EASA). Cannot be changed or deleted from operator maintenance
program, without the concurrence of the Primary Certification Authority (EASA).
CMR**
:
Task is an Airworthiness Limitation Section (ALS) Part 3 task – Certification Maintenance
Requirement. Its interval may be changed in accordance with an Operator's approved escalation
practices or an approved reliability program. Cannot be changed or deleted from operator
maintenance program, without the concurrence of the Primary Certification Authority (EASA).
CMP
:
Task originated by CMP (Configuration Maintenance and Procedures). This document lists the
standards for ETOPS.
LUR
:
“Low Utilization Recommendation” identifier (“LUR” is not a source document but identifies tasks
having additional low utilization calendar time values).
MRB
:
Task originated by the MRB Report. For tasks resulting from a system/power plant analysis, the
three letters «MRB» are followed by the corresponding Functional Failure Effect category (5 to 9).
5: Evident Safety
6: Evident Operational
7: Evident Economic
8: Hidden Safety
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9: Hidden Non- Safety
SB, SIL, AOT
:
Task originated by an Inspection Service Bulletin, a Service Information Letter, an Alert Operator
Transmission
SPECI
:
“ROSSIYA AIRLINES” OJSC originated task
S-ICA
:
Task originated by Supplemental Instructions for Continuing Airworthiness of the non-OEM
modifications (STC, Minor changes)
9. TPS – TEMPORARY PROTECTION SYSTEM

Specifies the type of Temporary Protection System (TPS) to be applied as indicated below:
“1”
:
Type 1 Grade 2 or Grade 3 TPS is to be applied.
“2”
:
Type 2 Grade 2 TPS is to be applied.
“1+2”
:
Type 1 TPS plus a subsequent application of Type 2 TPS is to be applied.
“No”
:
TPS must not be applied in the area (example: inside fuel tank, pylon).
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10. REFERENCES
This column is divided on two parts.
The first is used to provide the reference of technical publications where task accomplishment instructions are available and also the reference to the
source document when the task has not originated from the MRBR. Refer to below:

AMM reference: AMTOSS number of the task in the A320 Aircraft Maintenance Manual.

FCOM reference indicating that task may alternatively be performed by the FLIGHT CREW.

Appendix 7: Based on MRB Report revision 15 issued in order to reflect results from dedicated ATA 32 working group activities, a new
APPENDIX 7 is provided for identification of shop procedures related to Landing Gear Overhaul. Those procedures are NOT to be covered in
the AMM and “APPENDIX 7” is stated in the reference column of the related MPD tasks

Other References to technical publications such as:

AD: Airworthiness Directives

CN: Consigne de Navigabilité (French Airworthiness Directives)

ICA: Instructions for continuing airworthiness for non-OEM modifications (STC and etc.)

STC Supplemental Type Certificate reference

DOA: Design Office Approval. Minor changes that are not under STC

ISB: Inspection Service Bulletin

SIL: Service Information Letter

OIT: Operator Information Telex

AOT: Alert Operators Transmission

CMP (ETOPS related Task)

JIC: Job Instruction Card (SDM produced AMOS jobcard)
The second part that goes after “SOURCE:” sign contains references to the source documents of the requirement that task represents
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11. MEN AND MH COLUMNS
Specifies:

The number of personnel and the corresponding labor hours required to carry out the task in each zone concerned (man-hours are expressed
in hours and hundredth of hours).
o Preceded by a «*», the labor hours required to open and close the listed access panels.
o Preceded by a «*», the labor hours required to perform the specific preparation.
All the labor hours estimates quoted are provided for planning guidance only and should be adjusted.
The figures quoted do not include:

Preparatory work such as aircraft cleaning, positioning work stands, procuring consumable materials, connecting ground power carts, etc.

Correction of defects found during task accomplishment.

Correction for dead time and labor efficiency.
12. APPLICABILITY COLUMN
When the task is applicable to the fleet, ALL is printed. When the task is applicable to part of the fleet, the Manufacturer Serial Number (MSN) of the
aircraft to which the task is applicable is printed.
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SCHEDULED MAINTENANCE PROGRAM
This section includes all scheduled maintenance tasks related to the aircraft systems including the tasks for power plants, auxiliary power unit, zonal
and structure. The list of all applicable tasks provided hereafter.
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SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
TASK
E
NUMBER
V
R 000001-01-1-SDM
ZONE
100
DESCRIPTION
AIRCRAFT WEIGHING
SKILL TASK
CODE CODE
INTERVALS
SOURCE
511
520
611
620
HIRF/LIGHTNING PROTECTION-WING
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
AF
FNC
I:
4 YE
SPECI
081000-200-001
JIC A320-08-00
EU PART CAT (EU) No
965/2012
OTAR 39.81
4
TBD
ALL
EL
FNC
I:
72 MO
MRB
249200-210-023
1
1
1
1
0.50
0.50
0.50
0.50
ALL
1
1
0.15
0.15
ALL
1
0.15
ALL
1
0.15
ALL
WEIGHING OF THE AIRCRAFT
200001-02-1
TPS
CHECK THAT THE CONNECTOR IS CORRECTLY TIGHTENED
BY MEASUREMENT OF THE RESISTANCE WITH A LOOP
TESTER:
- 4005VC, 4007VC, 4009VC, 4011VC, LH SIDE
- 4013VC, 4015VC, 4017VC, 4019VC, LH SIDE
- 4006VC, 4008VC, 4010VC, 4012VC, RH SIDE
- 4014VC, 4016VC, 4018VC, 4020VC, RH SIDE
SOURCE:
L/HIRF
20-00-01-2
L/HIRF
20-00-01-3
PREPARATION: SLATS FULLY EXTENDED;
200002-01-1
334
344
ACCESS PANELS: 521EB, 521GB, 522AB, 621EB, 621GB, 622AB
HIRF/LIGHTNING PROTECTION-THS T/E
EL
GVI
I:
36 MO
MRB
GENERAL VISUAL INSPECTION OF ELEMENTS FITTED ON
THE FOLLOWING HARNESSES:
- 405VB, 406VB, 407VB, 408VB, 409VB, LH SIDE
- 400VB, 401VB, 402VB, 403VB, 404VB, RH SIDE
200003-01-1
321
ACCESS PANELS: 334AB, 334BB, 334CB, 334DB, 334EB, 344AB, 344BB, 344CB,
344DB, 344EB
HIRF/LIGHTNING PROTECTION-VERTICAL FIN
SOURCE:
L/HIRF
20-00-02-1
EL
GVI
I:
72 MO
MRB
GENERAL VISUAL INSPECTION OF ELEMENTS FITTED ON
THE FOLLOWING HARNESSES:
- 4202VB, 4204VB
200003-02-1
322
ACCESS PANELS: 321AL
HIRF/LIGHTNING PROTECTION-VERTICAL FIN
GENERAL VISUAL INSPECTION OF ELEMENTS FITTED ON
THE FOLLOWING HARNESSES:
- 4202VB, 4204VB
249200-210-018
249200-210-019
SOURCE:
L/HIRF
20-00-03-1
EL
GVI
I:
72 MO
MRB
249200-210-020
SOURCE:
L/HIRF
20-00-03-2
ACCESS PANELS: 322BL
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R
E
V
TASK
NUMBER
200003-03-1
ZONE
324
DESCRIPTION
HIRF/LIGHTNING PROTECTION-VERTICAL FIN
SKILL TASK
CODE CODE
EL
GVI
INTERVALS
I:
72 MO
SOURCE
MRB
GENERAL VISUAL INSPECTION OF ELEMENTS FITTED ON
THE FOLLOWING HARNESSES:
- 4202VB, 4204VB
200121-01-1
121
122
ACCESS PANELS: 324AT
FORWARD AVIONIC COMPARTMENT
121
122
ACCESS PANELS: 121AF, 121AL, 121BF, 121CF, 811, 122BF
FORWARD AVIONIC COMPARTMENT
AF
RST
I:
48 MO
MRB
121
122
ACCESS PANELS: 121AF, 121AL, 121BF, 121CF, 122BF, 811
FORWARD AVIONIC COMPARTMENT
EL
GVI
I:
48 MO
MRB
121
122
ACCESS PANELS: 121AL, 811, 812, 822
FORWARD AVIONIC COMPARTMENT
TASKM. APPLICABI
H.
LITY
1
0.15
ALL
249200-100-004
1
1
0.30
0.30
ALL
249200-210-027
1
1
0.25
0.25
ALL
1
1
0.50
0.50
ALL
1
1
0.25
0.25
ALL
1
1
0.30
0.30
ALL
SOURCE:
MRB 20.0.121/02
AF
GVI
I:
72 MO
MRB
GENERAL VISUAL INSPECTION OF 90, 108, 109 VU
IN THE FORWARD AVIONIC COMPARTMENT (EWIS)
200121-04-1
249200-210-021
MEN
SOURCE:
MRB 20.0.121/01
GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE
FORWARD AVIONIC COMPARTMENT (EWIS)
200121-03-1
REFERENCES
SOURCE:
L/HIRF
20-00-03-3
CLEANING OF EWIS INSTALLED IN THE FORWARD AVIONIC
COMPARTMENT (ONLY IF CONTAMINATED)(EWIS)
200121-02-1
TPS
249200-210-028
SOURCE:
MRB 20.0.121/03
AF
DET
I:
72 MO
MRB
DETAILED INSPECTION OF G, E AND P ROUTES IN THE
FORWARD AVIONIC COMPARTMENT (EWIS)
249200-220-005
SOURCE:
MRB 20.0.121/04
PREPARATION: FLOOR PANELS FROM FR 1 TO FR 9 REMOVED;
200125-01-1
125
126
ACCESS PANELS: 121AF, 121AL, 121BF, 121CF, 811, 122BF
LATERAL AVIONIC COMPARTMENT
CLEANING OF EWIS INSTALLED IN THE LATERAL AVIONIC
COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
AF
RST
I:
72 MO
MRB
249200-100-031
SOURCE:
MRB 20.0.125/01
PREPARATION: 813 IF INSTALLED;
ACCESS PANELS: 812, 831, 822, 824
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SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
200125-03-1
ZONE
125
126
DESCRIPTION
LATERAL AVIONIC COMPARTMENT
SKILL TASK
CODE CODE
EL
GVI
INTERVALS
I:
48 MO
SOURCE
MRB
GENERAL VISUAL INSPECTION OF EWIS INSTALLED
IN THE LATERAL AVIONIC COMPARTMENT (EWIS)
TPS
REFERENCES
249200-210-808
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.25
0.25
ALL
1
1
0.25
0.25
ALL
1
1
0.25
0.25
ALL
1
1
0.30
0.30
ALL
1
1
0.25
0.25
ALL
1
1
0.25
0.25
ALL
SOURCE:
MRB 20.0.125/03
PREPARATION: 813 IF INSTALLED;
200125-05-1
125
126
ACCESS PANELS: 812, 831, 822, 824
LATERAL AVIONIC COMPARTMENT
AF
GVI
I:
72 MO
MRB
GENERAL VISUAL INSPECTION OF 105, 106, 103, 107
AND 70 VUS INSTALLED IN THE LATERAL AVIONIC
COMPARTMENT (EWIS)
249200-210-030
SOURCE:
MRB 20.0.125/05
PREPARATION: 103VU; 105VU; 106VU; 107VU;
200125-06-1
125
126
ACCESS PANELS: 812, 831, 822
LATERAL AVIONIC COMPARTMENT
AF
DET
I:
72 MO
MRB
DETAILED INSPECTION OF G, E AND P ROUTES INSTALLED
IN THE LATERAL AVIONIC COMPARTMENT (EWIS)
249200-220-008
SOURCE:
MRB 20.0.125/06
PREPARATION: FLOOR PANELS FROM FR 9 TO FR 16; 813 IF INSTALLED;
200127-02-1
127
128
ACCESS PANELS: 812, 831, 822, 824
REAR AVIONIC COMPARTMENT
AF
RST
I:
72 MO
MRB
CLEANING OF EWIS INSTALLED IN THE REAR AVIONIC
COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
200127-04-1
127
128
ACCESS PANELS: 127BF, 127BG, 127CF, 127DF, 131AW, 131BW, 131CW, 131DW,
128CF, 128EG, 132BW, 132EW, 824, 825
REAR AVIONIC COMPARTMENT
AF
SOURCE:
MRB 20.0.127/02
GVI
I:
48 MO
MRB
GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE
REAR AVIONIC COMPARTMENT (EWIS)
200127-05-1
127
128
ACCESS PANELS: 127BF, 127BG, 127CF, 127DF, 131AW, 131BW, 131CW, 131DW,
128CF, 128EG, 132BW, 132EW, 824, 825
REAR AVIONIC COMPARTMENT
AF
GENERAL VISUAL INSPECTION OF 80, 63, 187, 188 VU
INSTALLED IN THE REAR AVIONIC COMPARTMENT (EWIS)
249200-100-013
249200-210-033
SOURCE:
MRB 20.0.127/04
GVI
I:
72 MO
MRB
249200-210-034
SOURCE:
MRB 20.0.127/05
PREPARATION: PARTITION WALL PANELS ON FR 24A; 63VU;
ACCESS PANELS: 824, 825
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SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
200127-07-1
ZONE
127
128
DESCRIPTION
REAR AVIONIC COMPARTMENT
SKILL TASK
CODE CODE
EL
DET
INTERVALS
I:
72 MO
SOURCE
MRB
DETAILED INSPECTION OF G, E AND P ROUTES INSTALLED
IN THE REAR AVIONIC COMPARTMENT (EWIS)
TPS
REFERENCES
249200-220-007
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.25
0.25
ALL
1
1
0.25
0.25
ALL
1
1
0.25
0.25
ALL
1
1
0.25
0.25
ALL
1
1
0.15
0.15
ALL
SOURCE:
MRB 20.0.127/07
PREPARATION: FLOOR PANELS FROM FR 20 TO FR 24;
200131-01-1
131
132
ACCESS PANELS: 127BF, 127BG, 127CF, 127DF, 131AW, 131BW, 131CW, 131DW,
128CF, 128EG, 132BW, 132EW, 824, 825
FORWARD CARGO COMPARTMENT
AF
RST
I:
72 MO
MRB
CLEANING OF EWIS INSTALLED IN THE FORWARD CARGO
COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
249200-100-025
SOURCE:
MRB 20.0.131/01
PREPARATION: SIDEWALL AND CEILING PANELS REMOVED;
200131-02-1
131
132
ACCESS PANELS: 825
FORWARD CARGO COMPARTMENT
AF
GVI
I:
144 MO
MRB
GENERAL VISUAL INSPECTION OF G, E AND P ROUTES
INSTALLED IN THE FORWARD CARGO COMPARTMENT (EWIS)
249200-210-805
SOURCE:
MRB 20.0.131/02
PREPARATION: SIDEWALL AND CEILING PANELS REMOVED;
200133-01-1
133
134
ACCESS PANELS: 825
UNDERFLOOR BAY OF FWD CARGO COMPARTMENT
AF
RST
I:
72 MO
MRB
CLEANING OF EWIS INSTALLED IN
THE UNDERFLOOR BAY OF FORWARD CARGO
COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
249200-100-024
SOURCE:
MRB 20.0.133/01
PREPARATION: FLOOR PANELS REMOVED;
200137-01-1
137
138
ACCESS PANELS: 133AL, 134AR, 825
BAY BEHIND FWD CARGO COMPARTMENT
CLEANING OF EWIS INSTALLED IN THE BAY BEHIND FWD
CARGO COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
AF
RST
I:
72 MO
MRB
249200-100-029
SOURCE:
MRB 20.0.137/01
PREPARATION: ACT(S) NO.4 AND NO.6 REMOVED (IF INSTALLED);
ACCESS PANELS: 131NW, 131PW, 132PW, 825
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SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
200141-01-1
ZONE
141
142
DESCRIPTION
WING CENTRE BOX
SKILL TASK
CODE CODE
AF
GVI
INTERVALS
I:
144 MO
SOURCE
MRB
GENERAL VISUAL INSPECTION OF EXPOSED EWIS
INSTALLED IN THE WING CENTRE BOX (EWIS)
200145-01-1
145
146
ACCESS PANELS: 147AZ, 734, 148AZ, 744
ZONE UNDER CABIN FLOOR
TPS
REFERENCES
249200-210-026
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.25
0.25
ALL
1
1
0.15
0.15
ALL
1
1
0.25
0.25
ALL
1
1
0.15
0.15
ALL
1
1
0.15
0.15
ALL
SOURCE:
MRB 20.0.141/01
AF
RST
I:
72 MO
MRB
CLEANING OF EWIS INSTALLED IN THE ZONE UNDER CABIN
FLOOR (ONLY IF CONTAMINATED) (EWIS)
249200-100-015
SOURCE:
MRB 20.0.145/01
PREPARATION: FLOOR PANELS FROM FR 36 TO FR 46;
200151-01-1
151
152
ACCESS PANELS: 832, 842
AFT CARGO COMPARTMENT
EL
RST
I:
72 MO
MRB
CLEANING OF EWIS INSTALLED IN THE AFT CARGO
COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
249200-100-026
SOURCE:
MRB 20.0.151/01
PREPARATION: SIDEWALL PANELS FROM FR 46 TO FR 59; ACT(S) REMOVED (IF
INSTALLED);
200151-02-1
151
152
ACCESS PANELS: 826
AFT CARGO COMPARTMENT
EL
GVI
I:
144 MO
MRB
GENERAL VISUAL INSPECTION OF P ROUTES INSTALLED IN
AFT CARGO COMPARTMENT (EWIS)
249200-210-806
SOURCE:
MRB 20.0.151/02
PREPARATION: ACT(S) REMOVED (IF INSTALLED); CEILING PANELS FROM FR 46
TO FR 59; SIDEWALL PANELS FROM FR 46 TO FR 59;
200161-01-1
161
162
ACCESS PANELS: 826
BULK CARGO COMPARTMENT
CLEANING OF EWIS INSTALLED IN THE BULK CARGO
COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
AF
RST
I:
72 MO
MRB
249200-100-030
SOURCE:
MRB 20.0.161/01
PREPARATION: SIDEWALL PANELS FROM FR 59 TO FR 65; ACT(S) REMOVED (IF
INSTALLED);
ACCESS PANELS: 826
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SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
200171-01-1
ZONE
171
172
DESCRIPTION
AFT CABIN UNDERFLOOR COMPARTMENT
SKILL TASK
CODE CODE
EL
RST
INTERVALS
I:
144 MO
SOURCE
MRB
CLEANING OF EWIS INSTALLED IN THE AFT CABIN
UNDERFLOOR COMPARTMENT (ONLY IF CONTAMINATED)(EWIS)
TPS
REFERENCES
249200-100-001
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
ALL
1
1
0.15
0.15
ALL
1
1
0.30
0.30
ALL
1
1
0.30
0.30
ALL
1
1
0.25
0.25
ALL
SOURCE:
MRB 20.0.171/01
PREPARATION: ACT NO.5 REMOVED (IF INSTALLED); CABIN FLOOR PANELS
FROM FR 65 TO FR 70;
200191-01-1
191
192
ACCESS PANELS: 161DW, 171AL, 162DW, 172AR, 826
AIR CONDITIONING COMPARTMENT AND
FAIRINGS
AF
RST
I:
72 MO
MRB
SOURCE:
MRB 20.0.191/01
CLEANING OF EWIS INSTALLED IN THE AIR CONDITIONING
COMPARTMENT AND FAIRINGS (ONLY IF CONTAMINATED)
(EWIS)
200211-01-1
211
212
ACCESS PANELS: 191AB, 191AT, 191BT, 191CT, 191DT, 191EB, 191ET, 191GB,
191HB, 191JB, 191KB, 191LB, 192AB, 192AT, 192BT, 192CT, 192DT, 192EB, 192ET,
192FB, 192KB, 192LB, 192MB
COCKPIT
AF
RST
I:
144 MO
MRB
CLEANING OF EWIS INSTALLED IN THE COCKPIT
(ONLY IF CONTAMINATED) (EWIS)
200211-02-1
211
212
ACCESS PANELS: 211BC, 211FC, 211HC, 831, 212BC, 212FC, 212KW, 841
COCKPIT
249200-100-027
249200-100-016
SOURCE:
MRB 20.0.211/01
AF
RST
I:
72 MO
MRB
CLEANING OF EWIS INSTALLED IN 49VU AND 120VU
(ONLY IF CONTAMINATED) (EWIS)
249200-100-017
SOURCE:
MRB 20.0.211/02
PREPARATION: 120VU; 49VU;
200211-03-1
211
212
ACCESS PANELS: 831, 841
COCKPIT
GENERAL VISUAL INSPECTION OF EWIS
OF 49VU AND THE 120VU (EWIS)
AF
GVI
I:
144 MO
MRB
249200-210-035
SOURCE:
MRB 20.0.211/03
PREPARATION: 120VU; 49VU;
ACCESS PANELS: 831, 841
Sub 2 - Page 6 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
200221-01-1
ZONE
221
222
DESCRIPTION
FORWARD CABIN UTILITY AREA
SKILL TASK
CODE CODE
AF
RST
INTERVALS
I:
144 MO
SOURCE
MRB
CLEANING OF EWIS INSTALLED IN THE FORWARD
CABIN UTILITY AREA (ONLY IF CONTAMINATED) (EWIS)
TPS
REFERENCES
249200-100-007
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.25
0.25
ALL
1
1
0.20
0.20
ALL
1
1
0.25
0.25
ALL
1
1
0.25
0.25
ALL
SOURCE:
MRB 20.0.221/01
PREPARATION: DOOR FRAME LINING REMOVED; FLOOR PANELS FROM FR 12
TO FR 20; FURNISHINGS FROM FR 12 TO FR 20; GALLEYS AND TOILETS
REMOVED; SEATS REMOVED;
200223-01-1
223
224
ACCESS PANELS: 831, 841
FORWARD CABIN OVERHEAD COMPARTMENT
AF
RST
I:
144 MO
MRB
CLEANING OF EWIS INSTALLED IN THE FORWARD
CABIN OVERHEAD COMPARTMENT (ONLY IF CONTAMINATED)
(EWIS)
249200-100-010
SOURCE:
MRB 20.0.223/01
PREPARATION: CEILING PANELS FROM FR 12 TO FR 20; GALLEYS AND TOILETS
REMOVED; OVERHEAD STOWAGE COMPARTMENTS REMOVED;
200223-02-1
223
224
ACCESS PANELS: 831, 841
FORWARD CABIN OVERHEAD COMPARTMENT
AF
GVI
I:
144 MO
MRB
GENERAL VISUAL INSPECTION OF EWIS
OF THE 2000VU (EWIS)
249200-210-029
SOURCE:
MRB 20.0.223/02
PREPARATION: 2000VU;
200231-01-1
231
232
ACCESS PANELS: 831
FORWARD PASSENGER COMPARTMENT
CLEANING OF EWIS INSTALLED IN THE FORWARD
PASSENGER COMPARTMENT (ONLY IF CONTAMINATED)
(EWIS)
AF
RST
I:
144 MO
MRB
249200-100-002
SOURCE:
MRB 20.0.231/01
PREPARATION: DOOR FRAME LINING REMOVED; FURNISHINGS; GALLEYS;
SEATS REMOVED; SIDEWALL PANELS FROM FR 20 TO FR 35; TOILET
REMOVAL/INSTALLATION ;
ACCESS PANELS: 831, 841
Sub 2 - Page 7 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
200231-03-1
ZONE
231
232
DESCRIPTION
FORWARD PASSENGER COMPARTMENT
SKILL TASK
CODE CODE
AF
GVI
INTERVALS
I:
72 MO
SOURCE
MRB
GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS,
ATTACHMENT POINTS AND ELECTRICAL CONNECTORS BETWEEN
SEAT AND A/C INSTALLED IN THE FORWARD PASSENGER
COMPARTMENT (EWIS)
NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH
SEATS AND WITH EWIS BETWEEN SEAT AND A/C ONLY
TPS
REFERENCES
249200-210-036
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.25
0.25
ALL
1
1
0.25
0.25
ALL
1
1
0.25
0.25
ALL
1
1
0.25
0.25
ALL
SOURCE:
MRB 20.0.231/03
PREPARATION: SEAT COVERS REMOVED IF NECESSARY;
200233-01-1
233
234
ACCESS PANELS: 831, 841
FORWARD PASSENGER COMPARTMENT OVERHEAD
COMPARTMENT
AF
RST
I:
144 MO
MRB
249200-100-005
SOURCE:
MRB 20.0.233/01
CLEANING OF EWIS INSTALLED IN THE FORWARD
PASSENGER COMPARTMENT OVERHEAD COMPARTMENT
(ONLY IF CONTAMINATED) (EWIS)
PREPARATION: CEILING PANELS FROM FR 20 TO FR 35; GALLEYS AND TOILETS
REMOVED; OVERHEAD STOWAGE COMPARTMENTS REMOVED;
200233-03-1
233
234
ACCESS PANELS: 831, 841
FORWARD PASSENGER COMPARTMENT OVERHEAD
COMPARTMENT
AF
GVI
I:
144 MO
MRB
249200-210-810
SOURCE:
MRB 20.0.233/03
GENERAL VISUAL INSPECTION OF ALL G & P ROUTES
INSTALLED IN THE FORWARD PASSENGER
COMPARTMENT OVERHEAD COMPARTMENT (EWIS)
PREPARATION: CEILING PANELS FROM FR 20 TO FR 35; GALLEYS AND TOILETS
REMOVED; OVERHEAD STOWAGE COMPARTMENTS REMOVED;
200241-01-1
241
242
ACCESS PANELS: 831, 841
CENTER PASSENGER COMPARTMENT
CLEANING OF EWIS INSTALLED IN THE CENTER
PASSENGER COMPARTMENT (ONLY IF CONTAMINATED)
(EWIS)
EL
RST
I:
144 MO
MRB
249200-100-003
SOURCE:
MRB 20.0.241/01
PREPARATION: FURNISHINGS; GALLEYS; SEATS REMOVED; SIDEWALL PANELS
FROM FR 35 TO FR 47; TOILET REMOVAL/INSTALLATION ;
ACCESS PANELS: 832, 842
Sub 2 - Page 8 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
200241-03-1
ZONE
241
242
DESCRIPTION
CENTER PASSENGER COMPARTMENT
SKILL TASK
CODE CODE
EL
GVI
INTERVALS
I:
144 MO
SOURCE
MRB
GENERAL VISUAL INSPECTION OF G ROUTES INSTALLED
AT FR 47 (EWIS)
TPS
REFERENCES
249200-210-031
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.15
0.15
ALL
1
1
0.25
0.25
ALL
1
1
0.20
0.20
ALL
1
1
0.15
0.15
ALL
SOURCE:
MRB 20.0.241/03
PREPARATION: GALLEYS AND TOILETS REMOVED; LINING AT FR 47, RH ONLY;
ACCESS PANELS: 832, 842
200241-04-1
241
242
CENTER PASSENGER COMPARTMENT
EL
GVI
I:
72 MO
MRB
GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS,
ATTACHMENT POINTS AND ELECTRICAL CONNECTORS BETWEEN
SEATS AND A/C INSTALLED IN THE CENTER PASSENGER
COMPARTMENT (EWIS)
NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH
SEATS AND WITH EWIS BETWEEN SEAT AND A/C ONLY
249200-210-037
SOURCE:
MRB 20.0.241/04
PREPARATION: SEAT COVERS REMOVED IF NECESSARY;
200243-01-1
243
244
ACCESS PANELS: 832, 842
CENTER PASSENGER OVERHEAD COMPARTMENT
EL
RST
I:
144 MO
MRB
CLEANING OF EWIS INSTALLED IN THE CENTER
PASSENGER OVERHEAD COMPARTMENT (ONLY IF CONTAMINATED)
(EWIS)
249200-100-009
SOURCE:
MRB 20.0.243/01
PREPARATION: CEILING PANELS FROM FR 35 TO FR 47; GALLEYS AND TOILETS
REMOVED; OVERHEAD STOWAGE BINS FROM FR 35 TO FR 47;
200243-03-1
243
244
ACCESS PANELS: 832, 842
CENTER PASSENGER OVERHEAD COMPARTMENT
GENERAL VISUAL INSPECTION OF G AND P ROUTES
INSTALLED IN THE CENTER PASSENGER OVERHEAD
COMPARTMENT (EWIS)
EL
GVI
I:
144 MO
MRB
249200-210-041
SOURCE:
MRB 20.0.243/03
PREPARATION: CEILING PANELS REMOVED; OVERHEAD STOWAGE BINS FROM
FR 35 TO FR 47;
ACCESS PANELS: 832, 842
Sub 2 - Page 9 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
200251-02-1
ZONE
251
252
DESCRIPTION
AFT PASSENGER COMPARTMENT
SKILL TASK
CODE CODE
EL
RST
INTERVALS
I:
144 MO
SOURCE
MRB
CLEANING OF EWIS INSTALLED IN THE AFT PASSENGER
COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
TPS
REFERENCES
249200-100-019
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.25
0.25
ALL
1
1
0.25
0.25
ALL
1
1
0.20
0.20
ALL
1
1
0.15
0.15
ALL
SOURCE:
MRB 20.0.251/02
PREPARATION: GALLEYS AND TOILETS REMOVED; SIDEWALL PANELS FROM
FR 47 TO FR 64 REMOVED;
200251-03-1
251
252
ACCESS PANELS: 832, 842
AFT PASSENGER COMPARTMENT
EL
GVI
I:
72 MO
MRB
GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS,
ATTACHMENT POINTS AND ELECTRICAL CONNECTORS BETWEEN
SEATS AND A/C INSTALLED IN THE AFT PASSENGER
COMPARTMENT (EWIS)
NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH
SEATS AND WITH EWIS BETWEEN SEAT AND A/C ONLY
249200-210-039
SOURCE:
MRB 20.0.251/03
PREPARATION: SEAT COVERS REMOVED IF NECESSARY;
200253-01-1
253
254
ACCESS PANELS: 832, 842
AFT PASSENGER OVERHEAD COMPARTMENT
EL
RST
I:
144 MO
MRB
CLEANING OF EWIS INSTALLED IN THE AFT PASSENGER
OVERHEAD COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
249200-100-021
SOURCE:
MRB 20.0.253/01
PREPARATION: CEILING PANELS REMOVED; GALLEYS AND TOILETS REMOVED;
OVERHEAD STOWAGE BINS FROM FR 47 TO FR 64 REMOVED;
200253-02-1
253
254
ACCESS PANELS: 832, 842
AFT PASSENGER OVERHEAD COMPARTMENT
GENERAL VISUAL INSPECTION OF G AND P ROUTES INSTALLED
IN THE AFT PASSENGER OVERHEAD COMPARTMENT (EWIS)
EL
GVI
I:
144 MO
MRB
249200-210-042
SOURCE:
MRB 20.0.253/02
PREPARATION: CEILING PANELS REMOVED; OVERHEAD STOWAGE BINS FROM
FR 47 TO FR 64 REMOVED;
ACCESS PANELS: 832, 842
Sub 2 - Page 10 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
200261-01-1
ZONE
261
262
DESCRIPTION
AFT CABIN UTILITY AREA
SKILL TASK
CODE CODE
EL
RST
INTERVALS
I:
144 MO
SOURCE
MRB
CLEANING OF EWIS INSTALLED IN THE AFT CABIN
UTILITY AREA (ONLY IF CONTAMINATED) (EWIS)
TPS
REFERENCES
249200-100-022
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.25
0.25
ALL
1
1
0.33
0.33
ALL
1
1
0.25
0.25
ALL
1
1
0.20
0.20
ALL
SOURCE:
MRB 20.0.261/01
PREPARATION: GALLEYS AND TOILETS REMOVED; SEATS REMOVED;
SIDEWALL PANELS FROM FR 64 TO FR 70;
200261-02-1
261
262
ACCESS PANELS: 832, 842
AFT CABIN UTILITY AREA
EL
GVI
I:
144 MO
MRB
GENERAL VISUAL INSPECTION OF P ROUTES INSTALLED
IN THE AFT CABIN UTILITY AREA (EWIS)
249200-210-044
SOURCE:
MRB 20.0.261/02
PREPARATION: GALLEYS AND TOILETS REMOVED; LINING AT FR 67;
200261-03-1
261
262
ACCESS PANELS: 832, 842
AFT CABIN UTILITY AREA
EL
GVI
I:
72 MO
MRB
GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS,
ATTACHMENT POINTS AND ELECTRICAL CONNECTORS BETWEEN
SEATS AND A/C INSTALLED IN THE AFT CABIN UTILITY
AREA (EWIS)
NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH
SEATS AND WITH EWIS CONNECTIONS BETWEEN SEAT AND A/C
ONLY
249200-210-040
SOURCE:
MRB 20.0.261/03
PREPARATION: SEAT COVERS REMOVED IF NECESSARY;
200263-01-1
263
264
ACCESS PANELS: 832, 842
AFT CABIN OVERHEAD COMPARTMENT
CLEANING OF EWIS INSTALLED IN THE AFT CABIN OVERHEAD COMPARTMENT
(ONLY IF CONTAMINATED) (EWIS)
EL
RST
I:
144 MO
MRB
249200-100-023
SOURCE:
MRB 20.0.263/01
PREPARATION: CEILING PANELS REMOVED; GALLEYS AND TOILETS REMOVED;
OVERHEAD STOWAGE BINS FROM FR 64 TO FR 70;
ACCESS PANELS: 832, 842
Sub 2 - Page 11 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
200263-02-1
ZONE
263
264
DESCRIPTION
AFT CABIN OVERHEAD COMPARTMENT
SKILL TASK
CODE CODE
EL
GVI
INTERVALS
I:
144 MO
SOURCE
MRB
GENERAL VISUAL INSPECTION OF G AND P ROUTES INSTALLED IN THE AFT
CABIN OVERHEAD COMPARTMENT (EWIS)
TPS
REFERENCES
249200-210-043
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.15
0.15
ALL
1
1
0.20
0.20
ALL
1
1
0.10
0.10
ALL
1
1
1
1
0.13
0.13
0.13
0.13
ALL
1
1
1
1
0.13
0.13
0.13
0.13
ALL
1
1
1
1
0.13
0.13
0.13
0.13
ALL
SOURCE:
MRB 20.0.263/02
PREPARATION: CEILING PANELS REMOVED; OVERHEAD STOWAGE BINS FROM
FR 64 TO FR 70;
200263-03-1
263
264
ACCESS PANELS: 832, 842
AFT CABIN OVERHEAD COMPARTMENT
EL
GVI
I:
144 MO
MRB
GENERAL VISUAL INSPECTION OF ALL EWIS OF 2001 VU
(EWIS)
249200-210-045
SOURCE:
MRB 20.0.263/03
PREPARATION: CIRCUIT BREAKER PANEL;
200315-01-1
315
316
ACCESS PANELS: 832, 842
TAIL CONE AND APU ACCESSORY COMPARTMENT
EL
GVI
I:
24 MO
MRB
GENERAL VISUAL INSPECTION OF G AND P ROUTES INSTALLED
IN THE TAIL CONE AND APU ACCESSORY COMPARTMENT (EWIS)
200413-01-1
200435-01-1
200453-01-1
413
414
423
424
435
436
445
446
453
454
463
464
ACCESS PANELS: 315AL, 316AR
UPPER FORWARD PYLON
SOURCE:
MRB 20.0.315/01
EL
DET
I:
24 MO
MRB
DETAILED INSPECTION OF EWIS INSTALLED
IN THE UPPER FORWARD PYLON (EWIS)
DET
I:
24 MO
MRB
DETAILED INSPECTION OF EWIS IN THE FAN AND
ACCESSORY GEAR BOX (EWIS)
DETAILED INSPECTION OF EWIS INSTALLED
IN THE HOT SECTION (EWIS)
249200-220-001
SOURCE:
MRB 20.0.413/01
ACCESS PANELS: 413AL, 413BL, 413CL, 413DL, 413EL, 414AR, 414AZ, 414BR,
414CR, 414FR, 423AL, 423AZ, 423BL, 423CL, 423DL, 423FL, 424AR, 424BR, 424CR,
424ER
FAN AND ACCESSORY GEAR BOX
EL
ACCESS PANELS: 437AL, 438AR, 447AL, 448AR
HOT SECTION
249200-210-025
249200-220-003
SOURCE:
MRB 20.0.435/01
EL
DET
I:
24 MO
MRB
249200-220-004
SOURCE:
MRB 20.0.453/01
ACCESS PANELS: 451AL, 452AR, 461AL, 462AR
Sub 2 - Page 12 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
200540-02-1
ZONE
540
640
DESCRIPTION
WING FUEL TANK
SKILL TASK
CODE CODE
EL
GVI
INTERVALS
I:
144 MO
SOURCE
MRB
GENERAL VISUAL INSPECTION OF EXPOSED EWIS
WITHIN THE WING FUEL TANK (EWIS)
TPS
REFERENCES
249200-210-801
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.30
0.30
ALL
1
1
0.25
0.25
ALL
1
1
0.15
0.15
ALL
1
1
0.25
0.25
ALL
1
1
1
1
1
0.20
0.20
0.20
0.20
0.20
ALL
SOURCE:
MRB 20.0.540/02
ACCESS PANELS: 521AZ, 521BZ, 540AB, 540AZ, 540BB, 540BZ, 540CB, 540DB,
540EB, 540FB, 540GB, 540HB, 540JB, 540KB, 540LB, 540MB, 540NB, 540PB, 540QB,
540RB, 621AZ, 621BZ, 640AB, 640AZ, 640BB, 640BZ, 640CB, 640DB, 640EB, 640FB,
640GB, 640HB, 640JB, 640KB, 640LB, 640MB, 640NB, 640PB, 640QB, 640RB
200550-01-1
550
650
VENT SURGE TANK
AF
GVI
I:
144 MO
MRB
GENERAL VISUAL INSPECTION OF EXPOSED EWIS
WITHIN THE VENT SURGE TANK (EWIS)
249200-210-802
SOURCE:
MRB 20.0.550/01
ACCESS PANELS: 550AB, 550BB, 550CB, 550DB, 650AB, 650BB, 650CB, 650DB
200560-01-1
560
660
DRY BAY (OUTBOARD)
AF
GVI
I:
144 MO
MRB
GENERAL VISUAL INSPECTION OF EXPOSED EWIS
WITHIN THE DRY BAY (OUTBOARD) (EWIS)
200571-01-1
571
671
ACCESS PANELS: 560AB, 660AB
MLG BAY
SOURCE:
MRB 20.0.560/01
AF
GVI
I:
144 MO
MRB
GENERAL VISUAL INSPECTION OF P ROUTE PUMP
FEEDER (EWIS)
202800-01-1
300
500
600
700
800
PREPARATION: PUMP WIRING FAIRINGS;
ELECTRICAL BONDING
DETAILED INSPECTION OF BONDING LEADS LOCATED ON THE FOLLOWING
MOVABLE SURFACES: ELEVATOR, RUDDER, FLAPS, FLAP TRACK FAIRINGS,
SLATS, SPOILERS, AILERONS, LANDING GEAR DOORS AND PASSENGER/CREW
DOORS
249200-210-803
249200-210-804
SOURCE:
MRB 20.0.571/01
EL
DET
I:
24 MO
SIL
249200-210-024
SIL 20-020
ACCESS PANELS: 325BL; 325BR; 325CL; 325CR; 325DL; 325DR; 325EL; 325ER;
334BB; 334DB; 334FB; 334GB; 334HB; 344BB; 344DB; 344FB; 344GB; 344HB;
521AB; 522AB; 522FB; 522NB; 522SB; 571AB; 573AB; 573BB; 573CB; 575AB; 575AT;
575BB; 575CB; 575DB; 575EB; 575FB; 575GB; 575KB; 575LB; 575MB; 590AB;
590BB; 621AB; 622AB; 622FB; 622NB; 622SB; 671AB; 673AB; 673BB; 673CB; 675AB;
675AT; 675BB; 675CB; 675DB; 675EB; 675FB; 675GB; 675KB; 675LB; 675MB;
690AB; 690BB; 831FZ; 831GZ; 832FZ; 832GZ; 841FZ; 841GZ; 842FZ; 842GZ
Sub 2 - Page 13 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
212100-01-1
ZONE
131
DESCRIPTION
AIR DISTRIBUTION AND RECIRCULATION
SKILL TASK
CODE CODE
AF
RST
CLEAN COCKPIT AIR SUPPLY DUCTING GRID
212100-01-2
131
ACCESS PANELS: 131MW, 131PW, 825
AIR DISTRIBUTION AND RECIRCULATION
AF
RST
CLEAN COCKPIT AIR SUPPLY DUCTING GRID
212100-02-1
212141-01-1
200
ACCESS PANELS: 131SW, 825
AIR DISTRIBUTION AND RECIRCULATION
130
GENERAL VISUAL INSPECTION OF RISER DUCTS IN THE
PASSENGER COMPARTMENT
RECIRCULATION FILTER
AF
AF
GVI
DIS
DISCARD FILTER ELEMENTS OF RECIRCULATION SYSTEM
212300-01-1
212300-02-1
210
220
230
240
250
260
200
ACCESS PANELS: 131PW, 132PW
LAVATORY AND GALLEY VENTILATION
AF
GVI
LAVATORY AND GALLEY VENTILATION
AF
DIS
AVIONICS EQUIPMENT VENTILATION
AF
OPC
OPERATIONAL CHECK OF SYSTEM VIA MCDU
212600-02-1
212600-03-1
I:
24000 FH
OR
160 MO
MRB 9
LUR
I:
24000 FH
OR
160 MO
MRB 9
LUR
I:
12 YE
MRB 9
210
AVIONICS EQUIPMENT VENTILATION
210
OPERATIONAL CHECK OF OVERRIDE FUNCTION (BLOWER AND
EXTRACT)
AVIONICS EQUIPMENT VENTILATION
OPERATIONAL CHECK OF SMOKE CONFIGURATION CONTROL
CIRCUIT
TPS
REFERENCES
212149-100-001
AF
AF
OPC
OPC
TASKM. APPLICABI
H.
LITY
0.20
1130 1200
1379 1578
1657 1767
2151 2163
1
0.20
212000-210-001
1
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
ALL
SOURCE:
MRB 21.21.00/04
212141-920-002
1
0.05
ALL
1
1
1
1
1
1
1
0.25
0.25
0.25
0.25
0.25
0.25
0.20
ALL
212600-710-001
1
0.10
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
ALL
SOURCE:
MRB 21.26.00/02
MRB 26.15.00/01
212600-710-002
1
0.10
ALL
SOURCE:
MRB 21.26.00/03
212600-710-003
1
0.10
ALL
SOURCE:
MRB 21.21.00/05
212149-100-001
SOURCE:
MRB 21.21.00/05
I:
5000 FH
OR
36 MO
MRB 9
LUR
I:
12 YE
MRB 7
SOURCE:
MRB 21.21.00/02
I:
1000 FH
OR
12 MO
NOTE
MRB 7
LUR
I:
750 FH
OR
6 MO
MRB 9
LUR
I:
24 MO
MRB 9
I:
7500 FH
OR
50 MO
MEN
1
212000-210-002
SOURCE:
MRB 21.23.00/02
NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY
BE USED.
210
SOURCE
GENERAL VISUAL INSPECTION OF LAVATORY AND GALLEY
VENTILATION DUCTING IN ZONES 210 THROUGH 260
DISCARD LAVATORY AIR EXTRACTION FILTER ELEMENT
212600-01-1
INTERVALS
212300-600-001
SOURCE:
MRB 21.23.00/03
MRB 8
LUR
SOURCE:
MRB 21.26.00/04
Sub 2 - Page 14 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
212600-04-1
212600-05-1
ZONE
DESCRIPTION
210
AVIONICS EQUIPMENT VENTILATION
120
OPERATIONAL CHECK OF DITCHING CONFIGURATION CONTROL
CIRCUIT
AVIONICS EQUIPMENT VENTILATION
SKILL TASK
CODE CODE
AF
AF
OPC
DET
DETAILED INSPECTION OF SKIN HEAT EXCHANGER DRAIN HOSE
CONNECTION AREA
212600-07-1
128
ACCESS PANELS: 812, 822
AVIONICS EQUIPMENT VENTILATION
INTERVALS
SOURCE
I:
15000 FH
OR
100 MO
I:
24000 FH
OR
160 MO
MRB 9
LUR
MRB 9
LUR
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
212600-710-004
1
0.10
ALL
SOURCE:
MRB 21.26.00/05
212642-200-003
1
0.40
ALL
SOURCE:
MRB 21.26.00/06
AF
DET
I:
24000 FH
OR
160 MO
SIL
LUR
212642-210-002
SIL 21-074
1
0.08
ALL
AF
OPC
I:
24 MO
MRB 9
212656-280-002
1
0.10
ALL
I:
40 MO
NOTE
MRB 9
SOURCE:
MRB 21.26.00/16
122113-100-002
1
0.30
ALL
I:
3600 FH
OR
24 MO
MRB 6
LUR
1
0.10
1200 1379
1578
I:
6 YE
MRB 9
1
0.10
ALL
DETAILED INSPECTION OF ELBOW DRAIN HOSE CONNECTION AREA
DOWNSTREAM OF BLOWER FAN
PREPARATION: ELBOW DUCT DOWNSTREAM OF BLOWER FAN;
212600-08-1
127
ACCESS PANELS: 824
AVIONICS EQUIPMENT VENTILATION
OPERATIONAL CHECK OF AIR INLET CHECK VALVE 2150 HM
212600-09-1
120
AVIONICS EQUIPMENT VENTILATION
AF
RST
CLEAN GRID OF RELAY BOX VU PANELS
212600-11-1
127
NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY
BE USED.
AVIONICS EQUIPMENT VENTILATION
AF
DIS
DISCARD DEMISTER FILTER ELEMENT AND FILTER CARTRIDGE
(LE BOZEC)
212641-01-1
128
ACCESS PANELS: 824
AVIONICS EQUIPMENT VENTILATION
DETAILED INSPECTION OF CHECK VALVE FLAPPERS FOR
CONDITION AND OPERATION
AF
DET
SOURCE:
MRB 21.26.00/19
212643-600-016
SOURCE:
MRB 21.26.00/21
212641-210-001
SOURCE:
MRB 21.26.00/07
ACCESS PANELS: 824
Sub 2 - Page 15 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
212643-07-1
ZONE
120
DESCRIPTION
AVIONICS VENTILATION DUST SEPARATOR
SKILL TASK
CODE CODE
AF
DIS
DISCARD FILTER CARTRIDGE (PALL)
INTERVALS
I:
1200 FH
NOTE
SOURCE
MRB 6
TPS
REFERENCES
212643-920-001
SIL 21-078
MEN
TASKM. APPLICABI
H.
LITY
1
0.16
0649 1130
1488 1560
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
1
0.16
1
0.16
1
0.10
0649 1130
1488 1560
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
0649 1130
1488 1560
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
1200 1379
213100-710-002
1
0.10
ALL
SOURCE:
MRB 21.31.00/02
213100-710-003
1
0.10
ALL
SOURCE:
MRB 21.26.00/13
NOTE: DISCARD INTERVAL FOR FILTER CARTRIDGE (PALL) IS SPECIFIED BY
P/N:
- P/N QB0511: 1600 FH
- P/N QB0639: 2400 FH
- P/N QB0776: 3000 FH
DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A
LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED.
NOTE. TRIAL INTERVAL REDUCTION TO IMPROVE RELIABILITY. ORIGINAL MPD
INTERVAL MAY BE APPLIED FOR THE PLANNING PURPOSES
212643-09-1
120
AVIONICS VENT. WATER/MOISTURE SEP.
EL
OPC
OPERATIONAL CHECK OF NRV FOR FREE MOVEMENT AND
CONFIRM THE BOWL IS CLEAN
212643-10-1
120
NOTE: THIS TASK IS CANCELLED AFTER REPLACEMENT OF PAL
FILTER BY LE BOZEC FILTER PER MOD 32877 (SB 21-1139).
AVIONICS VENT. WATER/MOISTURE SEP.
EL
DET
INSPECTION OF THE SIPHON ASSEMBLY (STRAINER) FOR
CLEANLINESS
212800-01-1
213100-01-1
210
210
NOTE: THIS TASK IS CANCELLED AFTER REPLACEMENT OF PAL
FILTER BY LE BOZEC FILTER PER MOD 32877 (SB 21-1139).
CARGO COMPARTMENT, VENTILATION AND HEATING AND AFT CARGO
COMPARTMENT GROUND COOLING SYSTEM
OPERATIONAL CHECK TO VERIFY CLOSING OF OUTLET ISOLATION VALVE OF
FWD CARGO COMPARTMENT IN CASE OF DITCHING
PRESSURE CONTROL AND MONITORING
AF
AF
OPC
OPC
OPERATIONAL CHECK OF SYSTEM VIA MCDU
213100-02-1
210
PRESSURE CONTROL AND MONITORING
OPERATIONAL CHECK OF MANUAL MODE SELECTION AND MANUAL MODE
PRESSURE CONTROL AND FUNCTIONAL CHECK OF MANUAL MODE CABIN
ALTITUDE INDICATION AND OUTFLOW VALVE POSITION INDICATION
AF
FNC
I:
1500 FH
OR
12 MO
MRB 9
LUR
I:
3000 FH
OR
24 MO
MRB 9
LUR
I:
12000 FH
OR
80 MO
MRB 9
LUR
I:
9000 FH
OR
60 MO
I:
9000 FH
OR
60 MO
MRB 9
LUR
212643-710-001
SIL 21-078
SOURCE:
MRB 21.26.00/14
212643-100-001
SIL 21-100
SOURCE:
MRB 21.26.00/15
212800-710-004
SOURCE:
MRB 21.28.00/02
MRB 6,9
LUR
SOURCE:
MRB 21.31.00/03
Sub 2 - Page 16 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
213100-03-1
213100-04-1
215000-02-1
ZONE
DESCRIPTION
210
PRESSURE CONTROL AND MONITORING
210
OPERATIONAL CHECK OF OUTFLOW VALVE CLOSING IN
DITCHING CONFIGURATION
PRESSURE CONTROL AND MONITORING
130
190
OPERATIONAL CHECK OF OUTFLOW VALVE PARTIAL OPENING BY
EMERGENCY RAM AIR SWITCH
AIR COOLING AND TEMPERATURE CONTROL
SKILL TASK
CODE CODE
AF
AF
AF
OPC
OPC
DET
DETAILED INSPECTION OF PACK AIR CHECK VALVES FLAPPERS
FOR CONDITION AND OPERATION
215000-03-2
215000-04-2
215200-07-1
190
ACCESS PANELS: 131PW, 132PW, 191BB, 192FB
PACK RAM AIR INLET
190
DETAILED INSPECTION OF ACTUATOR MECHANISM AND INLET
FLAP FOR EXCESSIVE PLAY AND CHECK GAP BETWEEN INLET
NOSE AND DIFFUSER RAMP
PACK RAM AIR OUTLET
191
192
DETAILED INSPECTION OF RAM AIR OUTLET FLAP AND CHECK
FOR EXCESSIVE BACKLASH OF OUTLET FLAP
AIR COOLING AND TEMPERATURE CONTROL
AF
AF
AF
DET
DET
DIS
DISCARD COMBO SEALS AND PERISEALS ON HOT AIR INLET DUCTING, PACK
DUCTING AND TRIM AIR DUCTING.
INTERVALS
SOURCE
I:
22500 FH
OR
150 MO
I:
22500 FH
OR
150 MO
I:
24000 FH
OR
120 MO
MRB 9
LUR
I:
6000 FH
OR
48 MO
MRB 9
LUR
I:
12000 FH
OR
80 MO
I:
12000 FH
OR
48 MO
NOTE
MRB 9
LUR
I:
12000 FH
OR
48 MO
NOTE
MRB 6,9
SIL
MRB 9
LUR
MRB 9
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
213100-710-004
1
0.10
ALL
SOURCE:
MRB 21.31.00/04
213100-710-005
1
0.05
ALL
1
1
0.30
0.30
ALL
1
1.00
ALL
1
1.00
0649
1
1
2.50
2.50
0649
1
1
2.50
2.50
ALL
SOURCE:
MRB 21.31.00/05
215243-210-001
SOURCE:
MRB 21.50.00/06
216151-200-001
SOURCE:
MRB 21.50.00/14
MRB 6,9
SIL
216152-200-001
SOURCE:
MRB 21.50.00/21
215200-920-001
SIL 21-039
SIL 36-047
SOURCE:
MRB 21.50.00/17
NOTE:
DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A
LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED.
TASK MAY BE COMBINED WITH TASK 361100-05-1.
ACCESS PANELS: 191KB, 192KB
215200-08-1
191
192
AIR COOLING AND TEMPERATURE CONTROL
DISCARD O-RING SEALS ON HOT AIR INLET DUCTING, PACK DUCTING AND
TRIM AIR DUCTING.
NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
AF
DIS
215200-920-002
SIL 21-039
SIL 36-047
SOURCE:
MRB 21.50.00/17
ACCESS PANELS: 191KB, 192KB
Sub 2 - Page 17 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
215242-01-1
215500-01-1
ZONE
191
192
210
DESCRIPTION
SKILL TASK
CODE CODE
INJECTOR - WATER
AF
GVI
GENERAL VISUAL INSPECTION OF WATER INJECTOR NOZZLES
FOR EROSION.
EMERGENCY RAM AIR INLET
AF
OPC
OPERATIONAL CHECK OF EMERGENCY RAM AIR INLET SYSTEM
215500-02-1
210
EMERGENCY RAM AIR INLET
AF
OPC
OPERATIONAL CHECK OF EMERGENCY RAM AIR INLET AND FLOW
CONTROL VALVE CLOSING IN DITCHING CONFIGURATION
215541-01-1
137
EMERGENCY RAM AIR INLET CHECK VALVE
AF
DET
DETAILED INSPECTION OF EMERGENCY RAM AIR/LP GROUND
AIR CHECK VALVE FLAPPERS FOR CONDITION AND OPERATION
216000-01-1
200
ACCESS PANELS: 131PW
AIR COOLING AND TEMPERATURE CONTROL
AF
DET
DETAILED INSPECTION OF CABIN SENSOR DUCT AND
TEMPERATURE SENSOR FOR CONTAMINATION
216000-02-1
216000-03-2
210
ACCESS PANELS: 231CC, 251CC
AIR COOLING AND TEMPERATURE CONTROL
130
OPERATIONAL CHECK OF ZONE CONTROLLER (BACK UP SWITCHING) VIA
CFDS/MCDU
TEMPERATURE CONTROL
DISCARD TRIM AIR PRESSURE REGULATING VALVE (TAPRV) FILTER
NOTE: ACCORDING TO SIL 21-134, TASK IS APPLICABLE TO AIRCRAFT FITTED
WITH TAPRV P/N 746A0000-06 ONLY.
AF
AF
OPC
DIS
INTERVALS
SOURCE
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
I:
24000 FH
OR
160 MO
I:
15000 FH
OR
100 MO
I:
15000 FH
OR
100 MO
SIL
LUR
215200-200-012
SIL 21-128
1
1
0.30
0.30
ALL
MRB 9
LUR
215500-710-001
1
0.10
ALL
1
0.10
ALL
I:
24000 FH
OR
160 MO
MRB 9
LUR
1
0.50
ALL
I:
7500 FH
OR
50 MO
MRB 9
LUR
2
0.20
ALL
I:
9000 FH
OR
60 MO
I:
12000 FH
OR
80 MO
NOTE
MRB 9
LUR
1
0.10
ALL
1
1.50
ALL
MRB 9
LUR
SOURCE:
MRB 21.50.00/04
215500-710-002
SIL 21-060
SOURCE:
MRB 21.50.00/11
215541-210-001
SOURCE:
MRB 21.50.00/07
216317-210-001
SOURCE:
MRB 21.50.00/02
SIL
LUR
216300-710-002
SOURCE:
MRB 21.50.00/03
216300-920-001
SIL 21-134
NOTE: INTERVAL MAY BE ADJUSTED IN ACCORDANCE WITH
OPERATORS EXPERIENCE
ACCESS PANELS: 131NW, 131PW
Sub 2 - Page 18 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
216242-01-1
ZONE
191
DESCRIPTION
AIR COOLING AND TEMPERATURE CONTROL
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF TRIM AIR CHECK VALVES FLAPPERS
FOR CONDITION AND OPERATION
INTERVALS
SOURCE
I:
9000 FH
OR
60 MO
MRB 9
LUR
I:
15000 FH
OR
100 MO
I:
22500 FH
OR
150 MO
I:
750 FH
OR
6 MO
I:
7500 FH
OR
50 MO
I:
7500 FH
OR
50 MO
I:
28 DY
NOTE
MRB 9
LUR
I:
7500 FH
OR
50 MO
MRB 9
LUR
I:
15000 FH
OR
100 MO
MRB 9
LUR
TPS
REFERENCES
216342-210-001
MEN
TASKM. APPLICABI
H.
LITY
1
0.20
ALL
221000-710-002
1
0.25
ALL
SOURCE:
MRB 22.10.00/01
223000-710-003
1
0.25
ALL
SOURCE:
MRB 22.30.00/01
226000-710-002
1
0.25
ALL
SOURCE:
MRB 22.60.00/01
226000-710-001
1
0.25
ALL
SOURCE:
MRB 22.60.00/02
226000-710-003
1
0.25
ALL
1
TBD
ALL
231300-710-002
1
0.10
ALL
SOURCE:
MRB 23.13.00/01
MRB 34.36.00/01
MRB 34.51.00/01
MRB 34.53.00/01
MRB 34.55.00/01
235100-710-003
1
0.10
ALL
SOURCE:
MRB 21.50.00/05
PREPARATION: CHECK VALVE;
221000-01-1
223000-01-1
226000-01-1
210
ACCESS PANELS: 191BB, 192FB
AUTO PILOT/FLIGHT DIRECTOR (AP/FD)
210
OPERATIONAL CHECK OF AP DISENGAGEMENT AND LOCKING
DEVICES OF SIDE STICK CONTROLLER AND RUDDER PEDALS
AUTOTHRUST
210
OPERATIONAL CHECK OF ENGINE/AUTOTHRUST SYSTEM
ISOLATION
FLIGHT AUGMENTATION (FAC)
AV
AV
AV
OPC
OPC
OPC
OPERATIONAL CHECK OF AUTOMATIC CHANGEOVER (AFS TEST)
226000-02-1
210
FLIGHT AUGMENTATION (FAC)
AV
OPC
OPERATIONAL CHECK OF FAC 2 FUNCTIONS
226000-03-1
210
FLIGHT AUGMENTATION (FAC)
AV
OPC
OPERATIONAL CHECK OF "RETURN TO LOWSPEED" FUNCTION
227100-01-1-SDM
210
FLIGHT MANAGEMENT SYSTEM (FMS)
AV
SVC
INTERVAL NOTE: INTERVAL DEPENDS ON THE DATABASE DELIVERY DATE AND
MAY BE HIGHER OR LOWER ESNURING THE LATEST FM DATA VERSION IS
INSTALLED
RADIO MANAGEMENT
RA
OPC
LOAD NAVIGATION DATA BASE AND UPDATE IDLE/PERF VALUE
231300-01-1
210
OPERATIONAL CHECK OF RADIO NAVIGATION SELECTION IN
STANDBY MODE USING RMP 1 AND 2
235100-01-1
210
AUDIO MANAGEMENT
OPERATIONAL CHECK OF CAPT. AND F/O AUDIO CONTROL
PANELS SWITCHING TO THIRD AUDIO CONTROL PANEL
RA
OPC
MRB 9
LUR
MRB 9
LUR
MRB 9
LUR
MRB 9
LUR
SPECI
SOURCE:
MRB 22.60.00/03
227000-610-008
JIC A320-22-83-00
SOURCE:
MRB 23.50.00/01
Sub 2 - Page 19 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
236142-01-1
237100-01-1
ZONE
300
500
600
210
DESCRIPTION
STATIC DISCHARGER RETAINER
RESISTANCE CHECK TIP TO RETAINER. BONDING CHECK
RETAINER TO STRUCTURE
COCKPIT VOICE RECORDER
SKILL TASK
CODE CODE
RA
RA
FNC
OPC
OPERATIONAL CHECK OF CVR AND CVR-CHANNEL RECORDING
237100-02-1
237135-02-1
237300-01-1
237300-02-1
210
COCKPIT VOICE RECORDER
312
OPERATIONAL CHECK OF CVR RECORDING LOGIC INCLUDING
TIME DELAY RELAY
COCKPIT VOICE RECORDER
RA
OPC
210
OPERATIONAL CHECK FOR SECONDARY POWER SUPPLY TO
DIRECTORS AND DECODER/ENCODER UNITS, AND
DECODER/ENCODER UNITS-A CUT OFF FUNCTION
CABIN INTERCOMMUNICATION DATA SYSTEM
RA
RA
OPC
OPC
OPC
CABIN INTERCOMMUNICATION DATA SYSTEM
RA
OPC
ACCESS PANELS: 831, 841
CABIN INTERCOMMUNICATION DATA SYSTEM
RA
OPC
OPERATIONAL CHECK OF CABIN BULB SIGNS VIA MCDU
240000-04-1
521
621
236100-200-001
ALL
1
0.40
ALL
1
0.50
ALL
1
0.15
ALL
1
0.30
ALL
237300-710-015
1
0.30
SOURCE:
MRB 23.73.00/02
237300-710-036
1
0.20
1130 1200
1379 1578
1657 1767
2151 2163
ALL
237300-710-802
1
0.10
0649
SOURCE:
MRB 23.73.00/09
249200-210-003
SIL 24-067
1
1
0.50
0.50
ALL
SOURCE:
MRB 23.71.00/01
237100-710-002
MRB 9
LUR
ELECTRICAL POWER
EL
TPS
MRB 9
I:
22500 FH
OR
150 MO
MRB 9
LUR
I:
22500 FH
OR
150 MO
I:
7500 FH
OR
50 MO
MRB 9
LUR
I:
1500 FH
OR
10 MO
I:
24 MO
MRB 9
LUR
TASKM. APPLICABI
H.
LITY
0.60
0.60
0.60
SOURCE:
MRB 23.60.00/01
237100-710-001
MRB 9
LUR
MEN
1
1
1
SOURCE:
MRB 23.71.00/04
ACCESS PANELS: 312AR
CABIN INTERCOMMUNICATION DATA SYSTEM
200
MRB 9
REFERENCES
CVRP/N 980-6022-001, VENDOR: HONEYWELL INTERNATIONAL INC
ULB: P/N DK120, VENDOR DUKANE
AV
OPERATIONAL CHECK OF LOUDSPEAKERS VIA MCDU
237300-09-1
I:
7500 FH
OR
50 MO
I:
15000 FH
OR
100 MO
I:
2 YE
TPS
OPERATIONAL CHECK OF ULB
210
200
I:
20 MO
SOURCE
SOURCE:
MRB 23.71.00/02
237100-720-001
CMM 23-70-03
CMM 23-70-44
OPERATIONAL CHECK OF POWER TRANSFER FUNCTION
237300-03-1
INTERVALS
237300-710-002
SOURCE:
MRB 23.73.00/01
MRB 9
LUR
SOURCE:
MRB 23.73.00/03
SIL
2
APPLY TEMPORARY PROTECTION TO END FITTINGS OF
ELECTRICAL CONDUITS IN WING INBOARD LEADING
EDGE
NOTE : SAME INTERVAL AND ACCESS AS FOR TASK
ZL-521-01-1
ACCESS PANELS: 471CL, 521GB, 482CR, 621GB
Sub 2 - Page 20 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
240000-05-1
ZONE
522
622
DESCRIPTION
ELECTRICAL POWER
SKILL TASK
CODE CODE
INTERVALS
SOURCE
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
EL
TPS
I:
24 MO
SIL
2
249200-210-004
SIL 24-067
1
1
0.40
0.40
ALL
EL
TPS
I:
24 MO
SIL
2
249200-210-014
SIL 24-067
1
1
1
1
0.25
0.25
0.25
0.25
ALL
EL
TPS
I:
24 MO
SIL
2
249200-210-006
SIL 24-067
1
1
0.50
0.50
ALL
ACCESS PANELS: 575BB, 575CB, 575DB, 575EB, 575FB, 575GB, 575HB, 575KB,
575LB, 575MB, 675BB, 675CB, 675DB, 675EB, 675FB, 675GB, 675HB, 675KB, 675LB,
675MB
ELECTRICAL POWER
EL
TPS
I:
24 MO
SIL
2
249200-210-013
SIL 24-067
1
1
0.25
0.25
ALL
TPS
I:
6 YE
SIL
2
249200-210-005
SIL 24-067
1
1
0.75
0.75
ALL
APPLY TEMPORARY PROTECTION TO END FITTINGS OF
ELECTRICAL CONDUITS IN WING OUTBOARD LEADING
EDGE
NOTE : SAME INTERVAL AND ACCESS AS FOR TASK
ZL-522-01-1
240000-06-1
240000-07-1
571
574
671
674
575
675
ACCESS PANELS: 522AB, 622AB
ELECTRICAL POWER
APPLY TEMPORARY PROTECTION TO END FITTINGS OF
ELECTRICAL CONDUITS IN MAIN LANDING GEAR BAY
AND FALSE SPAR BOX
NOTE : SAME INTERVAL AND ACCESS AS FOR TASK
ZL-574-01-1
ACCESS PANELS: 574AB, 574BB, 674AB, 674BB
ELECTRICAL POWER
APPLY TEMPORARY PROTECTION TO END FITTINGS OF
ELECTRICAL CONDUITS IN WING OUTBOARD TRAILING
EDGE
240000-08-1
531
631
APPLY TEMPORARY PROTECTION TO END FITTINGS OF
ELECTRICAL CONDUITS IN FLAP TRACK NUMBER 2
FAIRING
NOTE : SAME INTERVAL AND ACCESS AS FOR TASK
ZL-531-01-1
240000-09-1
534
634
ACCESS PANELS: 531AT, 631AT
ELECTRICAL POWER
EL
APPLY TEMPORARY PROTECTION TO END FITTINGS OF
ELECTRICAL CONDUITS IN WING TIP
NOTE : SAME INTERVAL AND ACCESS AS FOR TASK
ZL-534-01-1 AND ZL-534-01-2
ACCESS PANELS: 534AB, 634AB
Sub 2 - Page 21 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
240000-10-1
ZONE
560
660
DESCRIPTION
ELECTRICAL POWER
SKILL TASK
CODE CODE
INTERVALS
SOURCE
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
EL
TPS
I:
12 YE
SIL
2
249200-210-015
SIL 24-067
1
1
0.75
0.75
ALL
EL
TPS
I:
6 YE
SIL
2
249200-210-007
SIL 24-067
1
1
0.75
0.75
ALL
ACCESS PANELS: 191AB, 191AT, 191BB, 191BT, 191CB, 191CT, 191DB, 191DT,
191EB, 191ET, 191GB, 191HB, 191JB, 191KB, 191LB, 192AB, 192AT, 192BT, 192CT,
192DT, 192EB, 192ET, 192FB, 192KB, 192LB, 192MB
ELECTRICAL POWER
EL
TPS
I:
24 MO
SIL
2
249200-210-010
SIL 24-067
1
1
0.50
0.50
ALL
EL
TPS
I:
24 MO
SIL
2
249200-210-008
SIL 24-067
1
0.60
ALL
EL
TPS
I:
12 YE
SIL
2
249200-210-012
SIL 24-067
1
1
1
0.75
0.75
0.75
ALL
APPLY TEMPORARY PROTECTION TO END FITTINGS OF
ELECTRICAL CONDUITS IN DRY BAY (OUTBOARD)
NOTE : SAME INTERVAL AND ACCESS AS FOR TASK
ZL-560-01-1
240000-11-1
191
192
ACCESS PANELS: 560AB, 660AB
ELECTRICAL POWER
APPLY TEMPORARY PROTECTION TO END FITTINGS OF
ELECTRICAL CONDUITS IN AIR CONDITIONING
COMPARTMENT
NOTE : SAME INTERVAL AND ACCESS AS FOR TASK
ZL-191-02-1
240000-12-1
311
312
APPLY TEMPORARY PROTECTION TO END FITTINGS OF
ELECTRICAL CONDUITS IN FUSELAGE TAIL AREA
NOTE : SAME INTERVAL AND ACCESS AS FOR TASK
ZL-311-01-1, ZL-315-01-1
240000-13-1
325
ACCESS PANELS: 315AL, 312AR, 314AR, 316AR
ELECTRICAL POWER
APPLY TEMPORARY PROTECTION TO END FITTINGS OF
ELECTRICAL CONDUITS IN VERTICAL STABILIZER
TRAILING EDGE
NOTE : SAME INTERVAL AND ACCESS AS FOR TASK
ZL-325-01-1
240000-15-1
321
322
324
ACCESS PANELS: 325BL, 325BR, 325CL, 325DL
ELECTRICAL POWER
APPLY TEMPORARY PROTECTION TO END FITTINGS OF
ELECTRICAL CONDUITS IN VERTICAL STABILIZER
LEADING EDGE
NOTE : SAME INTERVAL AND ACCESS AS FOR TASK
ZL-321-01-1, ZL-322-01-1, ZL 324-01-1
ACCESS PANELS: 321AL, 322BL, 324AT
Sub 2 - Page 22 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
240000-16-1
ZONE
334
344
DESCRIPTION
ELECTRICAL POWER
SKILL TASK
CODE CODE
INTERVALS
SOURCE
EL
TPS
I:
24 MO
SIL
EL
OPC
T:
24 MO
I:
36 MO
EL
OPC
TPS
2
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
249200-210-011
SIL 24-067
1
1
0.40
0.40
ALL
SIL
240000-200-004
SIL 20-017
1
1
0.05
0.05
ALL
I:
750 FH
OR
6 MO
MRB 9
LUR
244100-740-002
1
0.10
I:
800 FH
OR
6 MO
NOTE
CMP
MRB 6
LUR
1
1
0.40
0.40
1488 1560
1743 1761
1851 1863
1876 1890
2151 2163
1488 1560
1743 1761
1851 1863
1876 1890
2151 2163
I:
2400 FH
OR
24 MO
MRB 6
LUR
1
1
0.30
0.30
APPLY TEMPORARY PROTECTION TO END FITTINGS OF
ELECTRICAL CONDUITS IN TRIMMABLE HORIZONTAL
STABILIZER
NOTE : SAME INTERVAL AND ACCESS AS FOR TASK
ZL-334-01-1
240000-17-1
100
200
ACCESS PANELS: 334CB, 334DB, 334EB, 344CB, 344DB, 344EB
ELECTRICAL POWER
ELECTRICAL POWER, OPENING AND CLOSING OF ALL CIRCUIT
BREAKERS.
242000-01-1
210
PREPARATION: ELECTRICAL POWER OFF.;
AC GENERATION
OPERATIONAL CHECK OF GAPCU VIA CFDS
242000-21-1
438
448
AC GENERATION
EN
DIS
- REMOVE AND DISCARD SCAVENGE AND CHARGE
FILTER ELEMENTS,
- DRAIN AND REPLENISH OIL SYSTEM
SOURCE:
MRB 24.20.00/19
242100-920-040
SIL SUN 236
SOURCE:
CMP 24-2-0000-001
MRB 24.20.00/20
NOTE: - REPLACE FILTER ELEMENTS, DRAIN IDG OIL AND
REPLENISH AT 150 FH OR 1 MO AFTER AIRCRAFT
DELIVERY. THEREAFTER REFER TO INTERVAL.
- INTERVAL MAY BE ADJUSTED IN ACCORDANCE
WITH SIL SUN 236.
242100-01-1
438
448
ACCESS PANELS: 438AR, 448AR
INTEGRATED DRIVE GENERATOR
CHECK TORQUE OF QUICK-ATTACH-DETACH (QAD)
TENSION BOLT
EN
FNC
242100-210-043
ALL
SOURCE:
MRB 24.20.00/07
ACCESS PANELS: 438AR, 448AR
Sub 2 - Page 23 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
242100-02-1
ZONE
438
448
DESCRIPTION
INTEGRATED DRIVE GENERATOR
SKILL TASK
CODE CODE
EN
DET
-CHECK OIL LEVEL OF INTEGRATED DRIVE GENERATOR (GREEN RANGE) AND
REPLENISH IF NECESSARY
-CHECK FILTER DIFFERENTIAL PRESSURE INDICATOR ( POP OUT NOT
PROTRUDING )
INTERVALS
SOURCE
I:
150 FH
OR
1 MO
NOTE
MRB 6
LUR
I:
800 FH
OR
6 MO
NOTE
CMP
MRB 6
LUR
I:
7500 FH
OR
50 MO
I:
120 FH
OR
1 MO
MRB 9
LUR
I:
15000 FH
OR
100 MO
I:
7500 FH
OR
50 MO
I:
8000 FH
OR
60 MO
MRB 9
LUR
TPS
REFERENCES
242100-210-046
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.02
0.02
ALL
1
1
0.40
0.40
0649 1130
1200 1379
1578 1657
1767
242200-710-002
1
0.10
ALL
SOURCE:
MRB 24.20.00/08
242400-710-001
1
0.02
ALL
SOURCE:
CMR 242000-00002-1-C
MRB 24.20.00/15
MRB 24.30.00/08
MRB 24.50.00/06
242400-710-002
1
0.10
ALL
SOURCE:
MRB 24.20.00/10
242500-710-001
1
0.10
ALL
SOURCE:
MRB 24.20.00/09
242600-710-001
1
0.10
0649
SOURCE:
MRB 24.20.00/05
NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY
BE USED.
242100-03-1
438
448
ACCESS PANELS: 438AR, 448AR
INTEGRATED DRIVE GENERATOR
EN
DIS
- REMOVE AND DISCARD SCAVENGE FILTER ELEMENT
- DRAIN AND REPLENISH OIL SYSTEM
SOURCE:
CMP 24-2-0000-001
MRB 24.20.00/06
NOTE:
INTERVAL MAY BE ADJUSTED IN ACCORDANCE WITH SIL
SUN 236.
242200-01-1
210
ACCESS PANELS: 438AR, 448AR
AC GENERATION
EL
OPC
OPERATIONAL CHECK OF TRANSFER INHIBITION
242400-01-2
210
AC EMERGENCY GENERATION
EL
OPC
OPERATIONAL CHECK OF EMERGENCY GENERATING SYSTEM
242400-02-1
210
AC GENERATION
EL
OPC
OPERATIONAL CHECK OF EMERGENCY GCU VIA CFDS
242500-01-1
210
AC GENERATION
EL
OPC
OPERATIONAL CHECK OF AC ESS GENERATION SWITCHING
242600-01-1
210
AC GENERATION
OPERATIONAL CHECK OF MANUAL AND AUTOMATIC GALLEY
SHEDDING
EL
OPC
242100-920-040
SIL SUN 236
CMR*
MRB 8
LUR
MRB 9
LUR
MRB 8
LUR
SOURCE:
MRB 24.20.00/13
Sub 2 - Page 24 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
242600-02-1
ZONE
210
DESCRIPTION
AC GENERATION
SKILL TASK
CODE CODE
EL
OPC
OPERATIONAL CHECK OF MANUAL AND AUTOMATIC GALLEY AND
BUS SHEDDING
242800-01-2
210
STATIC INVERTER
EL
OPC
OPERATIONAL CHECK OF STATIC INVERTER
242800-01-3
210
STATIC INVERTER
EL
OPC
OPERATIONAL CHECK OF STATIC INVERTER
243200-01-1
210
DC GENERATION
EL
OPC
OPERATIONAL CHECK OF DC GENERATION SWITCHING
243400-01-1
210
DC GENERATION
EL
OPC
OPERATIONAL CHECK OF "DC EMERG. CONFIG" CAUTION
243800-01-1
244100-01-1
210
DC MAIN GENERATION
210
OPERATIONAL CHECK OF BATTERY CHARGE LIMITER NO 1 AND
NO 2 VIA CFDS
AC EXTERNAL POWER CONTROL
EL
EL
OPC
OPC
OPERATIONAL CHECK OF GPCU VIA CFDS
245100-01-1
210
AC/DC ELECTRICAL LOAD DISTRIBUTION
OPERATIONAL CHECK OF GENERATOR LINE CONTACTOR OPENING
EL
OPC
INTERVALS
SOURCE
TPS
REFERENCES
I:
15000 FH
OR
100 MO
MRB 8
LUR
242600-710-002
I:
750 FH
OR
6 MO
CMR**
MRB 8
LUR
242800-710-001
I:
90 FH
OR
1 MO
CMR*
MRB 8
LUR
I:
6000 FH
OR
48 MO
I:
7500 FH
OR
50 MO
I:
750 FH
OR
6 MO
I:
750 FH
OR
6 MO
I:
15000 FH
OR
100 MO
MRB 9
LUR
MEN
TASKM. APPLICABI
H.
LITY
1
0.10
1
0.10
242800-710-001
1
0.10
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
0649 1130
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890 2151
2163
1200 1379
SOURCE:
CMR 242000-00001-1-C
MRB 24.20.00/18
MRB 24.30.00/11
MRB 24.50.00/09
243200-710-001
1
0.15
ALL
SOURCE:
MRB 24.30.00/04
243400-710-001
1
0.15
ALL
SOURCE:
MRB 24.30.00/06
243800-710-001
1
0.10
ALL
SOURCE:
MRB 24.30.00/03
244100-740-004
1
0.10
SOURCE:
MRB 24.20.00/03
242200-710-001
1
0.30
0649 1130
1200 1379
1578 1657
1767
ALL
SOURCE:
MRB 24.20.00/14
MRB 9
LUR
MRB 9
LUR
MRB 9
LUR
MRB 8
LUR
SOURCE:
CMR 242000-00001-2-C
MRB 24.20.00/17
MRB 24.30.00/10
MRB 24.50.00/08
SOURCE:
MRB 24.50.00/04
Sub 2 - Page 25 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
245100-02-1
ZONE
210
DESCRIPTION
AC/DC ELECTRICAL LOAD DISTRIBUTION
SKILL TASK
CODE CODE
EL
OPC
OPERATIONAL CHECK OF COMMERCIAL ELECTRIC LOAD
SHEDDING
251000-01-1-SDM
251100-01-1
251100-02-1
252100-01-1-SDM
SOURCE
I:
15000 FH
OR
100 MO
MRB 9
LUR
COCKPIT
CA
GVI
I:
400 FH
SPECI
210
GENERAL VISUAL INSPECTION OF THE COCKPIT INCLUDING SEATS, SEAT
COVERS, CEILING, SIDEWALL PANELS AND FLOOR MATERIAL FOR CONDITION
CLEANLINESS AND SECURITY OF INSTALLATION
COCKPIT SEATS
AF
DET
MRB 9
LUR
210
DETAILED INSPECTION OF SEAT STRUCTURE AND SEAT
ATTACHMENT OF ALL FLIGHT DECK SEATS
COCKPIT SEATS
I:
24000 FH
OR
160 MO
I:
7500 FH
OR
50 MO
I:
15000 FH
OR
100 MO
I:
8 DY
I:
15000 FH
OR
100 MO
I:
7500 FH
MRB 9
LUR
AF
FNC
200
PASSENGER COMPARTMENT SEATS
200
DETAILED INSPECTION OF SEAT TO FLOOR ATTACHMENT AND
GENERAL VISUAL INSPECTION OF SEAT STRUCTURE
PASSENGER SEATS
AF
DET
CA
GVI
AF
DET
TPS
REFERENCES
245100-710-001
MEN
1
TASKM. APPLICABI
H.
LITY
0.10
SOURCE:
MRB 24.50.00/05
200
CHECK OF ADJUSTMENT OF SEAT CONTROL CABLES
252100-01-1
INTERVALS
MRB 6,9
LUR
MRB 9
LUR
1
TBD
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
ALL
251100-200-001
1
0.30
ALL
SOURCE:
MRB 25.11.00/01
251151-200-002
1
0.30
ALL
SOURCE:
MRB 25.11.00/02
252100-210-001
1
2.00
ALL
SOURCE:
MRB 25.21.00/01
SPECI
1
TBD
ALL
GENERAL VISUAL INSPECTION OF SEATS FOR CLEANLINESS AND CONDITION
INCLUDING:
- BUMBER STRIPS (CORNERS) FOR DAMAGE
- ALL ARMPADS AND FOOTBAR PADS FOR EXCESSIVE WEAR
- BOTTOM CUSIONS AND BACK CUSHION INSERTS CORRECT INSTALLATION
- ALL FOLDING ARMRESTS FOR CORRECT FRICTION
252100-02-1
252100-02-1-SDM
200
PASSENGER COMPARTMENT SEATS
200
DETAILED INSPECTION OF SEAT BELT ATTACHMENT, SEAT
BELT AND LOCK. CHECK OF LOCK
PASSENGER SEATS
CA
DET
252100-210-002
1
1.60
ALL
SOURCE:
MRB 25.21.00/02
SPECI
1
TBD
ALL
DETALIED INSPECTION OF PASSENGER SEATS INCLUDING:
- BUSHINGS (SEAT BACKS, SPREADERS, EYEBOLTS AND ETC.) FOR
EXCESSIVE WEAR OR LOOSENESS;
- TRACK FITTINGS FOR LOSENESS, CORROSION OR DAMAGE;
- SPREADERS AND LEGS FOR LOSENESS, CRACKS OR OTHER DAMAGE;
- ALL WEAR SURFACES (SLIDES, FOODTABLE SLIDES, COCKTAIL TRAYS, INARM FOOD TABLES) FOR LOSENESS AND EXCESSIVE WEAR
Sub 2 - Page 26 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
252100-03-1-SDM
252100-04-1-SDM
252142-01-1-SDM
252161-01-1-SDM
252200-01-1
252200-02-1
252331-01-1
252340-01-1-SDM
252341-01-1-SDM
ZONE
DESCRIPTION
SKILL TASK
CODE CODE
INTERVALS
SOURCE
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
200
PASSENGER SEATS
CA
DET
I:
750 FH
SPECI
1
TBD
ALL
200
DETAILED INSPECTION OF PASSENGER SEATS CUSHIONS, FIREBLOCKING
AND DRESS COVERS FOR EXCESSIVE WEAR
PASSENGER SEATS
CA
DET
I:
750 FH
SPECI
1
TBD
ALL
200
DETAILED INSPECTION OF FOOD TRAYS IN SEAT BACKS AND IAT FOR CRACKS
AND DELAMINATION
PASSENGER SEAT BELTS
CA
DET
I:
750 FH
SPECI
1
TBD
ALL
200
DETAILED INSPECTION OF PASSENGER SEAT BELTS FOR: CUT OR WORN
EDGES, DAMAGED STITCHING, BROKEN FABRIC THREADS, EXCESSIVE CHAFE
MARKS, EXCESSIVE WEAR/FUSING
PASSENGER SEATS - SEB
CA
DET
I:
750 FH
SPECI
1
TBD
1130 1578
1657 1767
200
DETAILED INSPECTION OF SEAT-TO-SEAT CABLES CONNECTED TO SEAT
ELECTRONIC BOXES (SEB) FOR CORRECT INSTALLATION
CABIN ATTENDANT SEATS
DET
MRB 9
LUR
200
DETAILED INSPECTION OF SEAT ATTACHMENT AND GENERAL
VISUAL INSPECTION OF SEAT STRUCTURE
CABIN ATTENDANT SEATS
200
DETAILED INSPECTION OF SEAT BELT ATTACHMENT, SEAT
BELT AND LOCK. CHECK OF LOCK
PANELS - LOWER SIDEWALL
AF
DET
I:
15000 FH
OR
100 MO
I:
15000 FH
OR
100 MO
I:
24 MO
200
DETAILED INSPECTION OF LOWER SIDE WALL PANEL
AND OF AREA BEHIND LOWER SIDE WALL PANEL
FOR FOREIGN MATERIAL ACCUMULATION.
NOTE : - ONE LOWER SIDE WALL PANEL IN FWD, MID
AND AFT PASSENGER CABIN SHOULD BE
REMOVED, (APPROX 2.5 MH)
- ALTERNATE SIDEWALL PANEL IS
RECOMMENDED AT NEXT INSPECTION
- INTERVAL MAY BE ADJUSTED ACCORDING TO
OPERATOR EXPERIENCE
PASSENGER COMPARTMENT SIDEWALL PANELS
CA
GVI
I:
400 FH
SPECI
1
TBD
ALL
200
GENERAL VISUAL INSPECTION INSPECTION OF PASSENGER COMPARTMENT
UPPER AND LOWER SIDEWALL PANELS
NOTE: PAY SPECIAL ATTENTION TO THE ZONES NEAR SEATS
PASSENGER COMPARTMENT CEILING PANELS
CA
GVI
I:
400 FH
SPECI
1
TBD
ALL
AF
AF
DET
MRB 9
LUR
SIL
252200-210-001
1
0.30
ALL
SOURCE:
MRB 25.22.00/01
252200-210-002
1
0.25
ALL
1
0.30
ALL
SOURCE:
MRB 25.22.00/02
252344-210-001
SIL 25-085
GENERAL VISUAL INSPECTION OF PASSENGER COMPARTMENT CEILING
PANELS FOR CONDITION AND SECURITY OF INSTALLATION
Sub 2 - Page 27 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
252343-01-1-SDM
252400-01-1-SDM
252410-01-1-SDM
ZONE
DESCRIPTION
SKILL TASK
CODE CODE
INTERVALS
SOURCE
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
200
PASSENGER COMPARTMENT WINDOWS BLINDS
CA
DET
I:
400 FH
SPECI
1
TBD
ALL
200
DETAILED INSPECTION OF PASSENGER COMPARTMENT WINDOW BLINDES
FOR CONDITION AND PROPER OPERATION
PASSENGER COMPARTMENT OVERHEAD BINS
CA
GVI
I:
400 FH
SPECI
1
TBD
ALL
230
GENERAL VISUAL INSPECTION OF PASSENGER COMPARTMENT OVERHEAD
STOWAGE BINS FROM INSIDE AND OUTSIED FOR CONDITION AND PROPER
OPERATION
MOVEABLE CLASS DIVIDER ASSEMBLY
AF
GVI
I:
750 FH
S-ICA
DOA M090001115.05032014
ICA
M09000115_JTU_20032014
1
0.50
2151 2163
AF
DET
I:
12000 FH
OR
80 MO
S-ICA
DOA M090001115.05032014
ICA
M09000115_JTU_20032014
1
1.00
2151 2163
DOA M090001109.25112013
ICA
M090001109_BCA_17022014
1
0.50
2151 2163
GENERAL VISUAL INSPECTION OF MOVEABLE CLASS DIVIDER ASSEMBLY
CONDITION INCLUDING PARTS:
- CENTER AND SIDE BODY
- SUPPORT BRACKET
- SECURING PINS
- BEARINGS
- CURTAINS
- EXIT SIGN
- QUICK LOCKS
252410-02-1-SDM
TPS
230
NOTE: LUBRICATION OF PARTS ON CONDITION (LUBRICATION MATERIAL IAW
CMM). CLEANING/REPLACEMENT OF PARTS ON DEMAND
MOVEABLE CLASS DIVIDER ASSEMBLY
DETAILED INSPECTION OF PSU RAIL ATTACHING PARTS INCLUDING SCREWS
NOTE: CLEANING/REPLACEMENT OF PARTS ON DEMAND
252410-03-1-SDM
252600-01-1-SDM
R 252841-01-1-SDM
230
CABIN WINDSCREEN
AF
GVI
S-ICA
200
GENERAL VISUAL INSPECTION OF THE LH AND RH WINDSCREENS FOR:
- CORRECT ATTACHMENT TO THE SEAT TRACK AND MOUNTING BRACKET
- CORRECT ATTACHMENT OF MOUNTING ATTACHMENTS TO THE OHSC
- CORRECT ATTACHMENT OF LITERATURE POCKETS, MAGAZINE
- DAMAGE, WEAR, TEAR AND CLEANLINESS
PASSENGER COMPARTMENT CURTAINS
I:
750 FH
OR
12 MO
CA
DET
I:
400 FH
SPECI
1
TBD
ALL
200
DETAILED INSPECTION OF PASSENGER COMPARTMENT CURTAINS FOR
CONDITION AND LABEL PRESENCE. REPLACE CURTAIN IN CASE LABEL
ABSENCE OR WASHING REQUIRED
PASSENGER COMPARTMENT TEXTILE FLOOR CARPET
CA
GVI
I:
400 FH
SPECI
1
TBD
ALL
GENERAL VISUAL INSPECTION OF PASSENGER COMPARTMENT TEXTILE
FLOOR CARPET AND EMERGENCY ESCAPE PATH MARKING SYSTEM (IF
INSTALLED) FOR CONDITION CLEANLINESS AND SECURITY OF INSTALLATION.
CLEAN OR REPLACE IF NECESSARY
Sub 2 - Page 28 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
253000-01-1
ZONE
200
DESCRIPTION
BUFFET AND GALLEY
SKILL TASK
CODE CODE
CA
DET
INTERVALS
I:
6 YE
SOURCE
MRB 9
DETAILED INSPECTION OF ATTACHMENT POINTS
253000-01-1-SDM
253000-02-1
253300-01-1-SDM
254000-01-1
200
GALLEYS
CA
DET
I:
8 DY
SPECI
200
DETAILED INSPECTION OF ALL GALLEYS FOR CLEANLINESS AND CONDITION
INCLUDING:
- ENSURE SINKS ARE NOT BLOCKED
- WATER TRAPS OPERATE CORRECTLY
- DOORS AND LATCHES OPERATE CORRECTLY
BUFFET AND GALLEY
AF
DIS
I:
5500 FH
OR
40 MO
NOTE
MRB 7
LUR
1
TASKM. APPLICABI
H.
LITY
0.30
ALL
1
253000-920-001
1
TBD
0.20
ALL
ALL
SOURCE:
MRB 25.30.00/04
200
GVI
I:
400 FH
SPECI
1
TBD
ALL
200
GENERAL VISUAL INSPECTION OF FWD GALLEY INCLUDING EQUIPMENT,
VENTS, CEILING AND WALL PANELS FOR CONDITION AND SECURITY OF
INSTALLATION. ENSURE FLOOR MAT AND COVERING DO NOT HAVE CRACKS
OR DISBONDING
AFT GALLEY
CA
GVI
I:
400 FH
SPECI
1
TBD
ALL
200
GENERAL VISUAL INSPECTION OF AFT GALLEY INCLUDING EQUIPMENT,
VENTS, CEILING AND WALL PANELS FOR CONDITION AND SECURITY OF
INSTALLATION. ENSURE FLOOR MAT AND COVERING DO NOT HAVE CRACKS
OR DISBONDING
LAVATORIES
CA
DET
I:
1000 FH
FAA AD
MRB 9
LUR
200
NOTE: INTERVAL IS 1000 FH FOR OPERATOR FLYING UNDER FAA
REGULATIONS AS PER FAA AD 74-08-09.
LAVATORIES
200
LAVATORIES
DETAILED INSPECTION OF ATTACHMENT POINTS
254000-210-001
FAA AD 74-08-09
1
0.20
ALL
0649 1130
1200 1379
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890 2151
2163
SOURCE:
MRB 25.40.00/01
CA
DET
I:
5 YE
MRB 9
254000-210-002
1
0.30
MRB 9
SOURCE:
MRB 25.40.00/02
254000-210-002
1
0.30
DETAILED INSPECTION OF ATTACHMENT POINTS
254000-02-2
253000-210-001
MEN
NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY
BE USED.
FORWARD GALLEY
CA
DETAILED INSPECTION OF WASTE COMPARTMENT INCLUDING
WASTE FLAP AND OPERATIONAL CHECK OF WASTE FLAP
254000-02-1
REFERENCES
SOURCE:
MRB 25.30.00/01
REMOVE AND DISCARD FILTER ELEMENT
253100-01-1-SDM
TPS
CA
DET
I:
80 MO
SOURCE:
MRB 25.40.00/03
Sub 2 - Page 29 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
254000-04-1
ZONE
200
DESCRIPTION
LAVATORIES
SKILL TASK
CODE CODE
CA
DET
INTERVALS
I:
6000 FH
SOURCE
MRB 9
DETAILED INSPECTION OF LAVATORY FLOOR PAN
254000-04-2
200
LAVATORIES
255000-02-1
130
150
160
130
150
CARGO COMPARTMENTS
CA
DET
I:
7500 FH
254000-210-004
MRB 9
254000-210-004
MRB 8
SOURCE:
MRB 25.40.00/05
255000-200-002
AF
VCK
I:
8 DY
VISUAL CHECK OF CARGO COMPARTMENT DECOMPRESSION,
LINING, FLOOR PANELS AND PRESSURE COMPENSATION VALVE
(AS FAR AS VISIBLE, IF ACT(S) INSTALLED)
ACCESS PANELS: 825, 826
LOWER DECK CARGO LOADING
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
1
1.50
1
1.50
1
1
1
0.20
0.20
0.20
1
1
0.20
0.20
1200 1379
2151 2163
1
1
0.20
0.20
1200 1379
2151 2163
SOURCE:
MRB 25.40.00/04
DETAILED INSPECTION OF LAVATORY FLOOR PAN
255000-01-1
TPS
SOURCE:
MRB 25.50.00/01
AF
DET
PERFORM OPERATIONAL CHECK AND DETAILED INSPECTION OF XZ-LATCHES
I:
8000 FH
OR
53 MO
MRB 8
LUR
I:
4000 FH
OR
12 MO
MRB 8
255000-210-001
0649 1130
1200 1379
1560 1578
1657 1767
1876 1890
1488 1743
1761 1851
1863 2151
2163
ALL
SOURCE:
MRB 25.50.00/03
ACCESS PANELS: 825, 826
255000-03-1
130
150
CARGO COMPARTMENTS
AF
DET
PERFORM OPERATIONAL CHECK AND DETAILED INSPECTION OF YZ DOOR
SILL LATCHES
255000-07-1
130
150
ACCESS PANELS: 825, 826
LOWER DECK CARGO LOADING
130
150
ACCESS PANELS: 825, 826
CARGO COMPARTMENTS
VISUAL CHECK OF XZ-LATCHES AND DOOR SILL LATCHES
SOURCE:
MRB 25.50.00/02
AF
DET
I:
2000 FH
OR
400 DY
SIL
LUR
255000-200-018
SIL 25-099
1
1
0.50
0.50
1200 1379
2151 2163
AF
VCK
I:
750 FH
OR
6 MO
MRB 8
LUR
255000-200-016
1
1
0.25
0.25
1200 1379
2151 2163
DETAILED INSPECTION OF PDU ROLLERS FOR WEAR AND DAMAGE
NOTE : IT IS RECOMMENDED TO ENSURE CLEANLINESS IN THE VICINITY OF
THE PDU ROLLERS
255000-11-1
255000-210-002
SOURCE:
MRB 25.50.00/17
NOTE: FOR A319 DOOR SILL LATCHES ONLY TO BE CHECKED IN FWD CC
ACCESS PANELS: 825, 826
Sub 2 - Page 30 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
255000-16-1
255000-25-1
ZONE
130
150
160
130
150
DESCRIPTION
CARGO COMPARTMENTS
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF DIVIDER NETS, DOOR NETS
AND NET ATTACHMENT POINTS
NOTE: THE NUMBER OF AFFECTED ZONES MAY VARY ACCORDING
TO THE CARGO SYSTEMS INSTALLED.
CARGO COMPARTMENTS
AF
DET
REMOVE XZ-LATCHES FOR DETAILED INSPECTION
256000-01-1-SDM
200
ACCESS PANELS: 825, 826
LIFE VESTS
INTERVALS
SOURCE
I:
750 FH
OR
6 MO
MRB 9
LUR
I:
24000 FH
OR
160 MO
MRB 8
LUR
TPS
REFERENCES
255000-200-025
SOURCE:
MRB 25.50.00/04
255000-200-802
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
0.20
0.20
0.20
ALL
1
1
0.67
0.67
1200 1379
2151 2163
SOURCE:
MRB 25.50.00/25
CA
VCK
I:
6 MO
SPECI
JIC A320-25-60-01
1
TBD
ALL
CA
VCK
I:
4 MO
SPECI
JIC A320-25-60-00
1
0.10
ALL
AF
DET
I:
6 YE
MRB 8
256141-200-001
1
0.20
ALL
1
0.10
ALL
CHECK LIFE VESTS AVAILABLE AND SERVICE LIFE NOT EXPIRED
256000-01-5-SDM
260
NOTE: REPLACE LIFE VEST OR OPEN DEFERRED ITEM IF LIFE VEST EXPIRES
IN LESS THAN 7 MO
FIRST AID KIT
CHECK FIRST AID KIT AND DOCTORS KIT FOR EXPIRATION DATE
256141-01-1
210
NOTE: REPLACE KITS OR OPEN DEFERRED ITEM IF THEY EXPIRES IN LESS
THAN 5 MO
DESCENT DEVICE EMERGENCY
DETAILED INSPECTION OF EMERGENCY ESCAPE ROPE AND ROPE
ATTACHMENT
256241-01-1
800
ACCESS PANELS: 211EC, 212EC
DOOR ESCAPE SLIDE
CHECK DOOR AND OFFWING ESCAPE SLIDE/RAFT INFLATION RESERVOIR
PRESSURE.
SOURCE:
MRB 25.61.41/01
AF
VCK
I:
750 FH
OR
6 MO
MRB 8
LUR
256200-210-001
SOURCE:
MRB 25.62.00/01
NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW
DOORS / EMERGENCY EXITS. DEPENDING ON AIRCRAFT CONFIGURATION,
ALTERNATIVE ACCESS PANELS ARE: -151CW AND 152CW (A320 & A321) OR 151SW AND 152SW (A319 & A318) OR ACCESS TO OVERHEAD STOWAGE
COMP. (FOR A/C WITH ACT) SEE AMM FOR ACCESS PANELS TO BE OPENED.
ACCESS PANELS: 151KW, 152KW
Sub 2 - Page 31 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
256241-05-1
R 256300-01-1
ZONE
221
222
261
262
200
DESCRIPTION
DOOR ESCAPE SLIDE
SKILL TASK
CODE CODE
AF
RST
CLEAN DOOR GIRT BAR FITTING STOP LEVERS
NOTE:
INTERVAL TO BE ADJUSTED ACCORDING TO DOOR USAGE
EVACUATION SIGNALLING EQUIPMENT
CA
OPC
OPERATIONAL CHECK OF EVAC FUNCTION
256551-01-1
256551-02-1
200
200
MEGAPHONE BATTERIES
CA
SOURCE
I:
1110 FC
OR
400 DY
NOTE
MRB 9
SIL
LUR
I:
22500 FH
OR
150 MO
MRB 9
LUR
I:
1 YE
MRB 9
210
210
128
256300-710-001
TASKM. APPLICABI
H.
LITY
1
1
1
1
0.10
0.10
0.10
0.10
ALL
2
0.20
1
0.20
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
ALL
DISCARD MEGAPHONE BATTERIES
MEGAPHONE
MRB 9
SOURCE:
MRB 25.65.51/01
256551-710-002
1
0.10
ALL
MRB 8
SOURCE:
MRB 25.65.51/02
261200-710-001
1
0.10
ALL
SOURCE:
MRB 26.12.00/01
MRB 26.21.00/01
261300-710-001
1
0.10
ALL
SOURCE:
MRB 26.13.00/01
MRB 26.22.00/01
261500-100-001
1
0.10
ALL
OPC
ENGINE FIRE AND OVERHEAT DETECTION
EL
OPC
APU FIRE AND OVERHEAT DETECTION
EL
OPC
OPERATIONAL CHECK OF LOOP/SQUIB
261500-03-1
531100-210-034
SIL 53-054
MEN
SOURCE:
MRB 23.73.00/05
I:
24 MO
I:
750 FH
OPERATIONAL CHECK OF LOOP/SQUIB
261300-01-1
REFERENCES
SOURCE:
MRB 52.10.00/07
OPERATIONAL CHECK OF MEGAPHONE
261200-01-1
TPS
256551-920-001
JIC A320-25-65-51
CMM 25-65-04
CA
DIS
INTERVALS
AVIONICS COMPARTMENT SMOKE DETECTION
CLEAN AVIONICS SMOKE DETECTION PICCOLO TUBES
NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY
BE USED.
AF
RST
I:
750 FH
OR
6 MO
MRB 8
LUR
I:
11000 FH
OR
73 MO
NOTE
MRB 9
LUR
SOURCE:
MRB 26.15.00/03
ACCESS PANELS: 824
Sub 2 - Page 32 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
261600-03-1
ZONE
210
DESCRIPTION
CARGO COMPARTMENT SMOKE DETECTION
SKILL TASK
CODE CODE
EL
OPC
OPERATIONAL CHECK OF CARGO COMPARTMENT SMOKE
DETECTION BY PTT
261600-04-1
210
CARGO COMPARTMENT SMOKE DETECTION
EL
OPC
OPERATIONAL CHECK OF CARGO COMPARTMENT SMOKE
DETECTION BY CFDS TO CONFIRM ISOLATION VALVES
LATCHING CIRCUIT INTEGRITY.
261600-05-1
261700-03-1
262100-02-1
262100-03-1
130
150
160
CARGO COMPARTMENT SMOKE DETECTION
RST
REMOVE CARGO COMPARTMENT SMOKE DETECTORS FOR CLEANING
210
ACCESS PANELS: 825, 826
LAVATORY SMOKE DETECTION
210
OPERATIONAL CHECK OF LAVATORY SMOKE DETECTION BY CFDS
TO CONFIRM WARNINGS CAN BE DISPLAYED
ENGINE FIRE EXTINGUISHING
415
425
AV
OPERATIONAL CHECK OF BOTTLE LOW PRESSURE INDICATING
CIRCUIT
ENGINE FIRE EXTINGUISHING
EL
EL
EL
OPC
OPC
OPC
CHECK FIRING CIRCUIT CONTINUITY
262100-04-1
415
425
ACCESS PANELS: 415BR, 425BR
ENGINE FIRE EXTINGUISHING
AF
FNC
CHECK DISTRIBUTION PIPING FOR LEAKAGE AND OBSTRUCTION
262100-05-1
210
ACCESS PANELS: 415BL, 415BR, 437AL, 438AR, 451AL, 452AR, 425BL, 425BR,
447AL, 448AR, 461AL, 462AR
ENGINE FIRE EXTINGUISHING
OPERATIONAL CHECK OF FIRE CONTROL PUSH BUTTON SWITCH
SUB FUNCTIONS RELATED TO ENGINE SHUTDOWN AND
ISOLATION
EL
OPC
INTERVALS
SOURCE
I:
750 FH
OR
6 MO
MRB 8
LUR
I:
750 FH
OR
6 MO
MRB 8
LUR
I:
18000 FH
OR
120 MO
MRB 8
LUR
I:
800 FH
OR
6 MO
I:
7500 FH
OR
50 MO
I:
15000 FH
OR
100 MO
MRB 9
LUR
I:
8000 FH
OR
72 MO
MRB 8
LUR
I:
15000 FH
OR
100 MO
MRB 8
LUR
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
261600-710-001
1
0.10
ALL
SOURCE:
MRB 26.16.00/01
MRB 26.23.00/02
261600-710-003
1
0.10
1
1
1
0.20
0.20
0.20
1130 1200
1379 1488
1560 1578
1743 1761
1767 1851
1863 1876
1890 2151
2163
ALL
261700-710-001
1
0.10
ALL
SOURCE:
MRB 26.17.00/01
262100-710-002
1
0.20
ALL
2
2
0.20
0.20
ALL
2
2
1.00
1.00
ALL
1
0.50
ALL
SOURCE:
MRB 21.28.00/06
MRB 26.16.00/02
261615-100-001
SOURCE:
MRB 26.16.00/05
MRB 9
LUR
MRB 9
LUR
SOURCE:
MRB 26.21.00/02
262100-720-001
SOURCE:
MRB 26.21.00/03
262100-720-003
SOURCE:
MRB 26.21.00/04
262100-710-004
SOURCE:
MRB 26.21.00/08
MRB 36.00.00/06
ACCESS PANELS: 413DL, 423DL
Sub 2 - Page 33 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
262142-01-1-SDM
ZONE
415
425
DESCRIPTION
ENGINE FIRE EXTINGUISHER BOTTLE - CARTRIDGE
SKILL TASK
CODE CODE
CA
VCK
INTERVALS
I:
24 MO
SOURCE
SPECI
CHECK ENGINE EXTINGUISHER SQUIBS FOR EXPIRATION DATE
262200-02-1
210
APU FIRE EXTINGUISHING
EL
OPC
OPERATIONAL CHECK OF AUTOMATIC FIRE EXTINGUISHING
CIRCUIT AND TEST APU LP FUEL VALVE OPERATION USING
EACH INDIVIDUAL MOTOR IN TURN AND TEST APU EMERGENCY
SHUTDOWN CIRCUIT
262200-03-1
210
APU FIRE EXTINGUISHING
EL
OPC
CHECK FIRING CIRCUIT CONTINUITY
262200-04-1
313
ACCESS PANELS: 314AR
APU FIRE EXTINGUISHING
AF
DET
DETAILED INSPECTION OF DISTRIBUTION PIPING
262200-05-1
210
ACCESS PANELS: 314AR
APU FIRE EXTINGUISHING
EL
OPC
OPERATIONAL CHECK OF LOW PRESSURE INDICATING CIRCUIT
262200-06-1
210
ACCESS PANELS: 314AR
APU FIRE EXTINGUISHING
EL
OPC
OPERATIONAL CHECK OF APU FIRE PUSH BUTTON SWITCH
FUNCTIONS (IN SINGLE CHANNEL CONFIGURATION) AND TEST
APU LP FUEL VALVE OPERATION USING EACH INDIVIDUAL
MOTOR IN TURN AND TEST APU EMERGENCY SHUTDOWN CIRCUIT
262242-01-1-SDM
313
APU FIRE EXTINGUISHER BOTTLE - CARTRIDGE
CHECK APU EXTINGUISHER SQUIBS FOR EXPIRATION DATE
CA
VCK
TPS
REFERENCES
262141-920-001
MEN
TASKM. APPLICABI
H.
LITY
1
1
TBD
TBD
ALL
SOURCE:
MRB 26.21.00/06
262200-710-002
1
0.10
ALL
SOURCE:
MRB 23.42.00/01
MRB 26.22.00/02
MRB 28.29.00/01
MRB 28.29.00/03
MRB 49.62.00/01-13
MRB 49.62.00/01-32
MRB 49.62.00/01-36
MRB 49.62.00/03-13
MRB 49.62.00/03-32
MRB 49.62.00/03-36
262200-720-001
2
0.33
ALL
1
0.20
ALL
2
0.20
ALL
I:
3000 FH
OR
20 MO
MRB 8
LUR
I:
15000 FH
OR
100 MO
MRB 8
LUR
I:
15000 FH
OR
100 MO
MRB 8
LUR
I:
15000 FH
OR
100 MO
MRB 8
LUR
I:
24000 FH
OR
80 MO
MRB 8
262200-710-004
1
0.30
ALL
I:
24 MO
SPECI
SOURCE:
MRB 26.22.00/09
MRB 49.62.00/02-13
MRB 49.62.00/02-32
MRB 49.62.00/02-36
262242-920-001
1
TBD
ALL
SOURCE:
MRB 26.22.00/07
262200-210-001
SOURCE:
MRB 26.22.00/05
262200-710-003
SOURCE:
MRB 26.22.00/06
SOURCE:
MRB 26.22.00/04
Sub 2 - Page 34 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
262300-02-1
ZONE
132
DESCRIPTION
CARGO COMPARTMENT FIRE EXTINGUISHING
SKILL TASK
CODE CODE
EL
OPC
CHECK FIRING CIRCUIT CONTINUITY
262300-02-3
132
ACCESS PANELS: 132SW, 825
CARGO COMPARTMENT FIRE EXTINGUISHING
EL
OPC
CHECK FIRING CIRCUIT CONTINUITY
262300-03-1
132
ACCESS PANELS: 132MW, 825
CARGO COMPARTMENT FIRE EXTINGUISHING
CA
FNC
CHECK FIRE EXTINGUISHING LINES FOR LEAKAGE AND
OBSTRUCTION
262300-03-3
132
ACCESS PANELS: 132SW, 825
CARGO COMPARTMENT FIRE EXTINGUISHING
CA
FNC
CHECK FIRE EXTINGUISHING LINES FOR LEAKAGE AND
OBSTRUCTION
INTERVALS
SOURCE
TPS
REFERENCES
I:
12000 FH
OR
80 MO
CMR**
MRB 8
LUR
I:
12000 FH
OR
80 MO
CMR**
MRB 8
LUR
I:
18000 FH
OR
120 MO
CMR**
MRB 8
LUR
I:
18000 FH
OR
120 MO
CMR**
MRB 8
LUR
262300-200-001
MEN
TASKM. APPLICABI
H.
LITY
262300-720-001
2
0.20
SOURCE:
CMR 262300-00001-1-C
MRB 26.23.00/03
262300-720-001
2
0.20
SOURCE:
CMR 262300-00001-1-C
MRB 26.23.00/03
262300-200-001
2
1.00
0649 1488
1560 1743
1761 1851
1863 1876
1890
2
1.00
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
CMR 262300-00002-1-C
MRB 26.23.00/04
SOURCE:
CMR 262300-00002-1-C
MRB 26.23.00/04
0649 1488
1560 1743
1761 1851
1863 1876
1890
1130 1200
1379 1578
1657 1767
2151 2163
262300-04-1-SDM
132
ACCESS PANELS: 132MW, 825
CARGO FIRE EXTINGUISHER BOTTLE - CARTRIDGE
CA
VCK
I:
24 MO
SPECI
JIC A320-26-23-00
1
0.10
ALL
262441-01-1
200
CHECK CARGO FIRE EXTINGUISHER SQUIB FOR EXPIRATION DATE
PORTABLE FIRE EXTINGUISHER
CA
VCK
I:
750 FH
OR
6 MO
MRB 9
LUR
262400-210-002
1
0.10
I:
48 MO
MRB 9
262500-200-002
1
0.10
0649 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
ALL
MRB 9
SOURCE:
MRB 26.25.00/01
262500-200-005
1
0.10
ALL
SOURCE:
MRB 26.25.00/04
279600-710-007
1
0.10
ALL
CHECK PRESSURE GAUGE READING
262541-01-1
262541-04-1
271400-01-1
200
LAVATORY FIRE EXTINGUISHER
200
GENERAL VISUAL INSPECTION OF LAVATORY FIRE
EXTINGUISHER FOR SIGNS OF LEAKAGE/DISCHARGE
LAVATORY FIRE EXTINGUISHING
210
VISUAL CHECK OF FIRE EXTINGUISHER BOTTLE PRESSURE
READING
AILERON AND HYDRAULIC ACTUATION
OPERATIONAL CHECK OF DAMPING MEASUREMENT BY BITE
CA
AF
EL
GVI
VCK
OPC
I:
4 MO
I:
4000 FH
OR
36 MO
SOURCE:
MRB 26.24.00/01
CMR**
MRB 8
LUR
SOURCE:
CMR 271400-00001-1-C
MRB 27.14.00/01
Sub 2 - Page 35 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
271400-02-2
ZONE
575
675
DESCRIPTION
AILERON AND HYDRAULIC ACTUATION
SKILL TASK
CODE CODE
AF
FNC
CHECK AILERON SERVO CONTROL AND HINGE BEARINGS FOR EXCESSIVE
PLAY AND CONDITION
INTERVALS
SOURCE
TPS
REFERENCES
I:
18000 FH
OR
120 MO
MRB 9
LUR
271400-220-001
I:
15000 FH
OR
100 MO
CMR**
MRB 8
LUR
271400-220-002
I:
1500 FH
OR
12 MO
I:
72 MO
OR
24000 FH
MRB 9
LUR
I:
72 MO
OR
24000 FH
MRB 6
I:
18000 FH
OR
72 MO
MRB 8
I:
18000 FH
OR
72 MO
MRB 6,8
I:
20 MO
MRB 6
MEN
TASKM. APPLICABI
H.
LITY
2
2
1.00
1.00
ALL
1
1
0.20
0.20
ALL
272200-710-001
1
0.10
ALL
SOURCE:
MRB 27.21.00/01
272100-210-002
1
0.30
ALL
1
0.10
ALL
2
0.40
ALL
1
0.10
ALL
1
0.10
ALL
SOURCE:
MRB 27.14.00/04
ACCESS PANELS: 575KB, 575MB, 590AB, 590BB, 675KB, 675MB, 690AB, 690BB
271400-03-1
575
675
AILERON AND HYDRAULIC ACTUATION
AF
OPC
CHECK FLUID RESERVE PISTON POSITION WITH HYDRAULIC
RESERVOIR DEPRESSURIZED
272100-01-1
210
ACCESS PANELS: 575KB, 675KB
RUDDER MECHANICAL CONTROL
AF
OPC
OPERATIONAL CHECK OF RESET FUNCTION
272100-02-1
100
RUDDER MECHANICAL CONTROL
AF
DET
DETAILED INSPECTION OF RUDDER MECHANICAL CONTROL CABLES INCLUDING ZONE 311-
272100-03-1
145
ACCESS PANELS: 131AC, 131BC, 131CC, 131PW, 151AC, 151BC, 151CC, 151DC,
161AC, 161BC, 162DW, 241FF, 241KF, 312AR, 812, 824, 825, 826
RUDDER MECHANICAL CONTROL
AF
FNC
CHECK TENSION OF RUDDER MECHANICAL CONTROL CABLES USING
TENSIOMETER
272100-05-1
210
ACCESS PANELS: 131BC, 811, 825
RUDDER MECHANICAL CONTROL
AF
OPC
OPERATIONAL CHECK OF CENTERING SPRING ROD
272100-07-1
325
ACCESS PANELS: 325CL, 325CR
RUDDER MECHANICAL CONTROL
AF
DET
DETAILED INSPECTION OF MECHANICAL CONTROL LINKAGE IN
FIN
MRB 6
SOURCE:
CMR 271400-00002-1-C
MRB 27.14.00/02
SOURCE:
MRB 27.21.00/03
272100-220-001
SOURCE:
MRB 27.21.00/03
272100-710-001
SOURCE:
MRB 27.21.00/05
272100-210-003
SOURCE:
MRB 27.21.00/07
ACCESS PANELS: 325AL, 325AR, 325BL, 325BR, 325CL, 325CR, 325DL, 325DR
272100-08-1
210
RUDDER MECHANICAL CONTROL
LUBRICATION OF RUDDER PEDAL ADJUSTMENT MECHANISM
AF
LUB
272143-600-001
SOURCE:
MRB 27.21.00/09
Sub 2 - Page 36 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
272100-10-1
ZONE
320
DESCRIPTION
RUDDER MECHANICAL CONTROL
SKILL TASK
CODE CODE
AF
FNC
FUNCTIONAL CHECK OF RUDDER SERVOCONTROL ACTUATING
SPRING RODS
INTERVALS
SOURCE
I:
24000 FH
OR
80 MO
MRB 8
I:
24000 FH
OR
80 MO
MRB 9
I:
40 MO
MRB 9
TPS
REFERENCES
272149-200-001
MEN
TASKM. APPLICABI
H.
LITY
2
1.50
ALL
1
0.67
ALL
1
0.33
ALL
272400-710-002
1
0.10
ALL
SOURCE:
MRB 27.24.00/01
MRB 29.10.00/15
MRB 29.30.00/01
MRB 29.30.00/02
272400-200-001
2
1.00
ALL
1
0.10
SOURCE:
MRB 27.21.00/10
ACCESS PANELS: 325BL, 325BR, 325CL, 325CR, 325DL, 325DR, 325EL, 325ER
272100-11-1
325
RUDDER MECHANICAL CONTROL
AF
DET
DETAILED INSPECTION OF RUDDER SERVOCONTROL ACTUATING
SPRING RODS AND RUDDER SERVOCONTROL FEEDBACK ROD
ATTACHMENTS
272145-01-1
125
ACCESS PANELS: 325CL
RUDDER CABLE TENSION REGULATOR
AF
OPC
SOURCE:
MRB 27.21.00/11
CHECK TENSION REGULATOR POINTER IS WITHIN THE LIMITS
272400-01-1
210
ACCESS PANELS: 811
RUDDER HYDRAULIC ACTUATION
325
RUDDER HYDRAULIC ACTUATION
AF
OPC
AF
FNC
CHECK RUDDER SERVOCONTROL AND HINGE BEARINGS FOR EXCESSIVE
PLAY AND CONDITION
D 272400-03-1
325
ACCESS PANELS: 325BL, 325CL, 325DL, 325EL
RUDDER HYDRAULIC ACTUATION
LUBRICATION OF RUDDER HINGE BEARING NO 6 WITH GREASE
MAT. NO. 04-004
272100-220-002
SOURCE:
MRB 27.21.00/02
OPERATIONAL CHECK OF RUDDER SERVOCONTROLS WITH
INDIVIDUAL HYDRAULIC SYSTEMS
272400-02-1
272100-220-004
AF
LUB
I:
750 FH
OR
6 MO
MRB 8
LUR
I:
18000 FH
OR
120 MO
MRB 9
LUR
I:
5500 FH
OR
15 MO
MRB 9
SOURCE:
MRB 27.24.00/02
122255-640-001
SOURCE:
MRB 27.24.00/03
NOTE: ALTERNATIVELY TASK 272400-05-1 CAN BE APPLIED.
ACCESS PANELS: 325DL, 325DR
Sub 2 - Page 37 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
TASK
E
NUMBER
V
R 272400-05-1
ZONE
325
DESCRIPTION
RUDDER HYDRAULIC ACTUATION
SKILL TASK
CODE CODE
AF
LUB
LUBRICATION OF RUDDER HINGE BEARING NO 6 WITH GREASE
MAT. NO. 04-037
INTERVALS
SOURCE
I:
5500 FH
OR
20 MO
MRB 9
T:
10000 FH
OR
72 MO
I:
750 FH
OR
6 MO
I:
4000 FH
OR
36 MO
SIL
LUR
CMR**
MRB 8
LUR
I:
20 MO
OR
12000 FH
EASA AD
FAA AD
MRB 9
TPS
REFERENCES
122255-640-002
MEN
TASKM. APPLICABI
H.
LITY
1
0.10
ALL
272651-200-001
SIL 27-127
1
0.20
0649 1488
1578 1657
279600-710-008
1
0.10
ALL
2
2
1.00
1.00
ALL
1
1
0.20
0.20
ALL
1
1
0.20
0.20
ALL
SOURCE:
MRB 27.24.00/03
NOTE: THIS IS AN ALTERNATIVE TASK TO 272400-03-1.
272651-01-1
325
ACCESS PANELS: 325DL 325DR
YAW DAMPER ACTUATION
AF
VCK
EL
OPC
INSPECTION OF RUDDER YAW DAMPER SERVO-ACTUATOR
FOR LEAKAGE
ACCESS PANELS: 325BL, 325BR
273400-01-1
210
ELEVATOR AND HYDRAULIC ACTUATION
OPERATIONAL CHECK OF DAMPING MEASUREMENT BY BITE
273400-02-1
334
344
ELEVATOR AND HYDRAULIC ACTUATION
AF
FNC
CHECK ELEVATOR SERVO CONTROL AND HINGE BEARINGS FOR
EXCESSIVE PLAY AND CONDITION
ACCESS PANELS: 334BB, 334DB, 334FB, 334HB, 344BB, 344DB, 344FB, 344HB
273400-03-1
334
344
ELEVATOR AND HYDRAULIC ACTUATION
AF
OPC
CHECK FLUID RESERVE PISTON POSITION WITH HYDRAULIC
RESERVOIR DEPRESSURIZED.
273400-04-2
334
344
ACCESS PANELS: 334DB, 344DB
ELEVATOR AND HYDRAULIC ACTUATION
CHECK OF THE DIFFERENTIAL PRESSURE INDICATOR AND
POSITION OF FLUID RESERVE PISTON OF ELEVATOR
SERVO CONTROLS
AF
VCK
I:
15000 FH
OR
100 MO
CMR**
MRB 8
LUR
I:
24000 FH
OR
160 MO
MRB 8
LUR
SOURCE:
CMR 273400-00001-1-C
MRB 27.34.00/01
273400-200-001
EASA AD
2007-0163
FAA AD
2001-16-09
FAA AD
2010-02-09
SOURCE:
MRB 27.34.00/03
273400-220-001
SOURCE:
CMR 273400-00002-1-C
MRB 27.34.00/02
273400-220-002
SOURCE:
MRB 27.34.00/04
ACCESS PANELS: 334DB, 344DB
Sub 2 - Page 38 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
273400-06-1
ZONE
334
344
DESCRIPTION
ELEVATOR AND HYDRAULIC ACTUATION
SKILL TASK
CODE CODE
INTERVALS
SOURCE
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
AF
CHK
I:
80 MO
SIL
273400-200-003
SIL 27-152
1
1
4.00
4.00
ALL
AF
LUB
I:
5500 FH
OR
15 MO
MRB 9
122253-640-001
1
0.10
0649 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
I:
750 FH
CMR**
MRB 8
274400-710-002
1
0.10
ALL
SOURCE:
CMR 274000-00002-1-C
MRB 27.40.00/01
274400-710-001
1
0.10
ALL
279600-710-006
1
0.10
ALL
SOURCE:
MRB 27.40.00/06
122253-640-002
1
0.10
1130
1
1
0.40
0.40
ALL
1
0.20
ALL
CHECK OF ELEVATOR NEUTRAL POSITION AND SERVO CONTROLS
INSTALLATION
274000-01-1
310
ACCESS PANELS: 334DB, 344DB
TRIMMABLE HORIZONTAL STABILIZER
LUBRICATE THS BEARINGS AND ATTACHMENT FITTINGS WITH
GREASE MAT. NO. 04-004
SOURCE:
MRB 27.40.00/04
NOTE: ALTERNATIVE TASK 274000-07-1 CAN BE APPLIED.
274000-02-1
210
ACCESS PANELS: 314AR
TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
OPC
OPERATIONAL CHECK OF THS ACTUATOR WITH INDIVIDUAL
HYDRAULIC SYSTEMS
274000-03-1
210
TRIMMABLE HORIZONTAL STABILIZER (THS)
AF
OPC
OPERATIONAL CHECK OF THS ACTUATOR JAMMING PROTECTION
DEVICE
274000-04-1
274000-07-1
210
ACCESS PANELS: 312AR
TRIMMABLE HORIZONTAL STABILIZER
310
OPERATIONAL CHECK OF THS ACTUATOR WITH ELECTRICAL
MOTOR NO 3
TRIMMABLE HORIZONTAL STABILIZER
AF
AF
OPC
LUB
LUBRICATE THS BEARINGS AND ATTACHMENT FITTINGS WITH
GREASE MAT. NO. 04-037
I:
4000 FH
OR
80 MO
CMR**
MRB 8
LUR
I:
15000 FH
OR
100 MO
I:
5500 FH
OR
20 MO
MRB 9
LUR
I:
72 MO
OR
24000 FH
MRB 6
I:
72 MO
OR
24000 FH
MRB 6
MRB 9
SOURCE:
CMR 274000-00003-1-C
MRB 27.40.00/02
SOURCE:
MRB 27.40.00/04
NOTE: THIS IS AN ALTERNATIVE TASK TO 274000-01-1
274100-01-1
100
310
ACCESS PANELS: 314AR
THS MECHANICAL CONTROL
AF
DET
DETAILED INSPECTION OF THS MECHANICAL CONTROL
274100-02-1
145
PREPARATION: CEILING PANELS REMOVED; FLOOR PANELS REMOVED;
THS MECHANICAL CONTROL
CHECK THS MECHANICAL CONTROL CABLES FOR CORRECT TENSION
AF
FNC
274100-210-001
SOURCE:
MRB 27.40.00/12
274100-220-002
SOURCE:
MRB 27.40.00/13
ACCESS PANELS: 241FF
Sub 2 - Page 39 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
274100-03-1
ZONE
120
310
DESCRIPTION
THS MECHANICAL CONTROL
SKILL TASK
CODE CODE
AF
LUB
LUBRICATION OF THS MECHANICAL CONTROL CHAINS AND REAR CABLE
(AREA OF TENSION REGULATOR)
274142-01-1
310
ACCESS PANELS: 811, 312AR
THS TRIM CTL CABLE TENSION COMPENSATOR
AF
FNC
INTERVALS
SOURCE
I:
30 MO
OR
11000 FH
MRB 6
I:
40 MO
MRB 6
310
ACCESS PANELS: 312AR
THS HYDRAULIC ACTUATION
274400-03-1
310
ACCESS PANELS: 312AR
THS HYDRAULIC ACTUATION
310
FUNCTIONAL CHECK OF THS ACTUATOR OVER FULL TRAVEL
RANGE BY REFERENCE TO MECHANICAL INDICATOR
THS ACTUATOR
AF
FNC
AF
AF
FNC
OPC
OPERATIONAL CHECK OF THS ACTUATOR NO-BACK DEVICE
274451-01-1
310
ACCESS PANELS: 312AR
THS ACTUATOR
AF
LUB
LUBRICATE THS ACTUATOR BALL SCREW NUT
274451-02-1
310
ACCESS PANELS: 312AR
THS ACTUATOR
AF
SVC
CHECK OIL LEVEL OF THS ACTUATOR GEARBOX
274451-03-1
310
ACCESS PANELS: 312AR
THS ACTUATOR
CHECK INDICATOR OF THS ACTUATOR NO-BACK WEAR
DETECTION DEVICE
122227-640-007
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.10
0.10
ALL
1
0.05
ALL
1
0.30
ALL
274100-720-001
2
0.20
ALL
SOURCE:
MRB 27.40.00/15
274451-710-001
1
0.30
ALL
1
0.10
ALL
1
0.05
ALL
1
0.07
ALL
274100-220-001
SOURCE:
MRB 27.40.00/07
FUNCTIONAL CHECK OF THS ACTUATOR PRESSURE OFF BRAKE
(APPLY TORQUE TO MANUAL CRANKING INPUT)
274400-02-1
REFERENCES
SOURCE:
MRB 27.40.00/20
CHECK POINTER ON TENSION COMPENSATOR SCALE WITHIN
LIMITS
274400-01-1
TPS
AF
DET
I:
24000 FH
OR
160 MO
MRB 9
LUR
I:
24000 FH
OR
160 MO
I:
18000 FH
OR
120 MO
MRB 9
LUR
I:
1600 FH
OR
12 MO
MRB 6
LUR
I:
3000 FH
OR
24 MO
MRB 6,9
LUR
I:
12000 FH
OR
80 MO
MRB 6
LUR
274454-720-001
SOURCE:
MRB 27.40.00/14
MRB 8
LUR
SOURCE:
MRB 27.40.00/18
122227-640-003
SOURCE:
MRB 27.40.00/03
274451-210-004
SOURCE:
MRB 27.40.00/05
274451-210-003
SOURCE:
MRB 27.40.00/08
ACCESS PANELS: 312AR
Sub 2 - Page 40 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
274451-04-1
ZONE
310
DESCRIPTION
THS ACTUATOR
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF THS ACTUATOR BALL SCREW NUT
BODY AND SCREW AND CLAW STOPS
274451-06-1
310
ACCESS PANELS: 312AR
THS ACTUATOR
AF
VCK
VISUAL CHECK OF THS ACTUATOR THREADED NUT (FAIL SAFE
NUT)
274451-07-1
310
ACCESS PANELS: 312AR
THS ACTUATOR
AF
FNC
CHECK BACKLASH BETWEEN THS ACTUATOR BALL SCREW NUT
AND SCREW
274451-08-1
310
ACCESS PANELS: 312AR
THS ACTUATOR
AF
FNC
CHECK INTEGRITY OF THS ACTUATOR BALL SCREW SHAFT
(PRIMARY AND SECONDARY LOAD PATH)
274451-09-1
310
ACCESS PANELS: 312AR
THS ACTUATOR
AF
SVC
DRAIN AND REFILL THS ACTUATOR GEARBOX
274451-11-1
310
ACCESS PANELS: 312AR
THS ACTUATOR
INTERVALS
SOURCE
MRB 6,9
LUR
ACCESS PANELS: 312AR
FLAPS
OPERATIONAL CHECK OF WTB/POB
NOTE : FLAP SURFACES MOVE AUTOMATICALLY
274451-220-001
I:
12000 FH
OR
80 MO
MRB 8
LUR
I:
15000 FH
OR
100 MO
MRB 6,8
LUR
I:
12000 FH
OR
80 MO
CMR*
MRB 8
LUR
274451-280-001
I:
18000 FH
OR
120 MO
MRB 9
LUR
274451-610-001
MEN
TASKM. APPLICABI
H.
LITY
1
0.15
ALL
1
0.05
ALL
1
0.40
ALL
1
0.10
ALL
1
0.50
ALL
SOURCE:
MRB 27.40.00/09
274451-210-002
SOURCE:
MRB 27.40.00/11
274451-200-001
SOURCE:
MRB 27.40.00/17
SOURCE:
CMR 274000-00001-1-C
MRB 27.40.00/16
SOURCE:
MRB 27.40.00/21
AF
DET
I:
10 MO
EASA AD
FAA AD
ISB
274451-220-004
EASA AD
2008-0150
FAA AD
2007-06-02
ISB 27-1164
1
3.50
ALL
AF
OPC
I:
7500 FH
OR
50 MO
CMR**
MRB 6,8
LUR
275100-710-001
2
0.30
ALL
NOTE: PERFORM INSPECTION PRIOR TO TASK 274451-05-1 (IF PLANNED AT
THE SAME TIME) AND PRIOR TO ANY CLEANING.
INTERVAL STARTING POINT IS THE AIRCRAFT FIRST FLIGHT AND NOT
DELIVERY FLIGHT.
210
REFERENCES
I:
12000 FH
OR
80 MO
DETAILED INSPECTION OF THSA UPPER ATTACHMENTS FOR SECONDARY
LOAD PATH LOADING
275100-01-2
TPS
SOURCE:
CMR 275000-00001-1-C
MRB 27.50.00/04
MRB 27.50.01/04
ACCESS PANELS: 575DB, 575EB, 575FB, 675DB, 675EB, 675FB
Sub 2 - Page 41 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
275100-02-1
ZONE
210
DESCRIPTION
FLAPS
SKILL TASK
CODE CODE
AF
OPC
OPERATIONAL CHECK OF FLAP INTERCONNECTING STRUT AND
FLAP DISCONNECT PROXIMITY SENSORS
275100-03-1
575
675
FLAPS
AF
DET
CHECK OF FLAPS TRANSMISSION SHAFTING INTEGRITY,
INCLUDING INSPECTION OF SEAL WITNESS DRAINS.
275100-06-1
275144-01-1
575
675
580
680
570
670
SOURCE
I:
8000 FH
OR
72 MO
MRB 8
LUR
I:
7500 FH
OR
50 MO
CMR**
MRB 6,8
LUR
530
630
SOURCE:
MRB 27.50.00/05
MRB 27.50.01/05
275400-210-002
TASKM. APPLICABI
H.
LITY
1
0.10
ALL
1
1
0.40
0.40
ALL
SOURCE:
CMR 275000-00001-1-C
MRB 27.50.00/04
MRB 27.50.01/04
I:
600 FH
SIL
275400-210-005
SIL 27-121
1
1
0.20
0.20
0649
CHECK FLAP ATTACHMENT BEARING NO.1 FOR LINER
MIGRATION
NOTE : IF BOTH FLAP ATTACHMENT PENDULUM ASSEMBLIES
ARE REPLACED BY NEW PENDULUM ASSEMBLY P/N D575-7224000400, THE INSPECTION IS NO LONGER APPLICABLE.
FLAP INTERCONNECTING STRUT
AF
DET
I:
8000 FH
OR
72 MO
MRB 8
LUR
275144-200-001
1
1
0.30
0.30
ALL
I:
24000 FH
OR
80 MO
MRB 6
1
1
1.00
1.00
ALL
I:
10 MO
OR
1800 FC
MRB 6,9
122227-640-004
1
1
0.40
0.40
ALL
I:
22000 FH
MRB 6,9
SOURCE:
MRB 27.50.00/02
MRB 27.50.01/02
275446-200-001
1
1
0.30
0.30
ALL
PREPARATION: FLAPS EXTENDED; SLATS FULLY EXTENDED;
FLAP TRANSMISSION ASSY
AF
DET
ACCESS PANELS: 734
FLAP TRACKS
AF
LUB
LUBRICATE ALL CARRIAGE ROLLERS ON ALL FLAP TRACKS
275446-02-1
275100-710-002
MEN
CHK
SOURCE:
MRB 27.50.00/06
MRB 27.50.01/06
PREPARATION: FLAPS EXTENDED; SLATS FULLY EXTENDED;
FLAP TRACKS
DETAILED INSPECTION OF TRACKS, ROLLERS AND SPHERICAL
BEARINGS (AS FAR AS VISIBLE).
AF
DET
275400-200-001
SOURCE:
MRB 27.50.00/08
MRB 27.50.01/08
PREPARATION: FLAPS EXTENDED; SLATS FULLY EXTENDED;
530
630
REFERENCES
AF
DETAILED INSPECTION OF TRANSMISSION ASSY
275446-01-1
TPS
ACCESS PANELS: 571AB, 573AB, 573BB, 573CB, 575AB, 575BB, 575CB, 575DB,
575EB, 575FB, 575GB, 734, 671AB, 673AB, 673BB, 673CB, 675AB, 675BB, 675CB,
675DB, 675EB, 675FB, 675GB, 744
FLAPS
DETAILED INSPECTION OF INTERCONNECTING STRUT AND
ATTACHMENTS
275400-01-1
INTERVALS
SOURCE:
MRB 27.50.00/09
PREPARATION: FLAPS EXTENDED; SLATS FULLY EXTENDED;
Sub 2 - Page 42 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
275449-03-1
ZONE
575
675
DESCRIPTION
ACTUATOR ASSEMBLY
SKILL TASK
CODE CODE
AF
SVC
DRAIN AND REFILL OFFSET GEARBOXES OF ROTARY ACTUATORS WITH SEMIFLUID
INTERVALS
SOURCE
I:
72 MO
OR
24000 FH
MRB 6
I:
72 MO
OR
18000 FC
OR
24000 FH
MRB 6
SIL
I:
72 MO
OR
24000 FH
MRB 6
I:
24 MO
MRB 6
TPS
REFERENCES
121327-612-004
MEN
TASKM. APPLICABI
H.
LITY
1
1
1.00
1.00
0649 1130
1200
1
1
4.00
4.00
0649 1130
1200
1
1
4.00
4.00
1
0.10
1200 1379
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890 2151
2163
ALL
1
1
0.25
0.25
ALL
2
2
1.40
1.40
ALL
1
1
0.10
0.10
ALL
SOURCE:
MRB 27.50.00/12
MRB 27.50.01/11
PREPARATION: FLAPS EXTENDED;
275449-05-1
575
675
ACCESS PANELS: 573AB, 575BB, 575CB, 575FB, 575GB, 673AB, 675BB, 675CB,
675FB, 675GB
ACTUATOR ASSEMBLY
AF
LUB
REMOVE FLAP ROTARY ACTUATOR ASSEMBLIES FOR REGREASING.
PREPARATION: FLAPS EXTENDED;
275449-06-1
575
675
ACCESS PANELS: 573AB, 575BB, 575CB, 575FB, 575GB, 673AB, 675BB, 675CB,
675FB, 675GB
ACTUATOR ASSEMBLY
AF
SVC
DRAIN AND REFILL FLAP ACTUATOR ASSEMBLIES WITH SEMI-FLUID
275451-01-1
147
FLAP POWER CONTROL UNIT
AF
SVC
SOURCE:
MRB 27.50.00/15
MRB 27.50.01/13
575
675
ACCESS PANELS: 734
SPOILER AND HYDRAULIC ACTUATION
AF
LUB
LUBRICATE SPOILER NO 1 TO 5 ACTUATOR ATTACHMENTS
276400-02-1
575
675
PREPARATION: FLAPS EXTENDED; SLATS FULLY EXTENDED;
SPOILER AND HYDRAULIC ACTUATION
AF
FNC
CHECK SPOILER SERVOCONTROL BEARING AND HINGE BEARINGS
FOR EXCESSIVE PLAY AND CONDITION
278100-03-1
520
620
PREPARATION: FLAPS EXTENDED; SLATS FULLY EXTENDED;
SLATS
OPERATIONAL CHECK OF WTB/POB
AF
OPC
121327-612-005
SOURCE:
MRB 27.50.00/13
MRB 27.50.01/12
REPLENISH PCU GEARBOX TO CONFIRM FLUID LEVEL
276400-01-1
122227-640-008
SIL 27-126
I:
2000 FH
OR
15 MO
MRB 9
LUR
I:
18000 FH
OR
120 MO
MRB 9
LUR
I:
7500 FH
OR
48 MO
CMR**
MRB 6,8
121327-612-002
SOURCE:
MRB 27.50.00/03
MRB 27.50.01/03
122227-640-005
SOURCE:
MRB 27.64.00/02
276400-200-001
SOURCE:
MRB 27.64.00/03
278100-710-001
SOURCE:
CMR 278000-00001-1-C
MRB 27.80.00/04
Sub 2 - Page 43 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
278100-04-1
ZONE
520
620
DESCRIPTION
SLATS
SKILL TASK
CODE CODE
AF
DET
CHECK OF SLATS TRANSMISSION SHAFTING INTEGRITY,
INCLUDING INSPECTION OF SEAL WITNESS DRAINS
278400-01-1
278451-01-1
147
190
520
620
147
ACCESS PANELS: 191EB, 191KB, 521AT, 521CB, 521EB, 521GB, 521HB, 522AB,
522CB, 522EB, 522FB, 522LB, 522NB, 522QB, 522SB, 522UB, 734, 192EB, 192KB,
621AT, 621CB, 621EB, 621GB, 621HB, 622AB, 622CB, 622EB, 622FB, 622LB, 622NB,
622QB, 622SB, 622UB, 744
SLAT TRANSMISSION ASSY
AF
DET
DETAILED INSPECTION OF TRANSMISSION ASSY
ACCESS PANELS: 734, 191BB, 191BT, 192BT, 192FB, 521BT, 522AB, 522CB,
522FB, 522JB, 522KB, 522LB, 522NB, 522QB, 522SB, 522UB, 621BT, 622AB, 622CB,
622FB, 622JB, 622KB, 622LB, 622NB, 622QB, 622SB, 622UB
SLAT POWER CONTROL UNIT
AF
SVC
INTERVALS
SOURCE
I:
7500 FH
OR
48 MO
CMR**
MRB 6,8
I:
24000 FH
OR
80 MO
MRB 6
I:
24 MO
MRB 6
520
620
ACCESS PANELS: 734
SLAT TRACKS
278468-02-1
520
620
AF
LUB
AF
DET
DETAILED INSPECTION OF SLAT TRACKS, ROLLER BEARINGS,
PINION BEARINGS AND CURVED RACK GEARS - AS VISIBLE.
I:
20 MO
OR
4500 FC
MRB 6,9
279000-05-1
210
OPERATIONAL CHECK :
- OF THE LOGICS ACTIVATING ELAC 1, ELAC 2 AND SEC.1
STANDBY POWER SUPPLIES
- TO CONFIRM ABILITY OF SEC.1 AND SEC.2 TO ACHIEVE
PITCH CONTROL
- TO CONFIRM ABILITY OF SIDESTICK PRIORITY FUNCTION
TASKM. APPLICABI
H.
LITY
1
1
0.10
0.10
ALL
0.50
0.50
0.50
0.50
ALL
SOURCE:
MRB 27.80.00/06
1
1
1
1
121327-612-003
1
0.10
ALL
1
1
0.50
0.50
ALL
1
1
1.00
1.00
ALL
2
0.40
ALL
278400-200-001
I:
6 YE
OR
22000 FH
MRB CPCP
MRB 6,9
AV
OPC
I:
400 FH
OR
80 DY
CMR*
MRB 8
LUR
122227-640-006
SOURCE:
MRB 27.80.00/02
278400-210-001
SOURCE:
MRB 27.80.00/07
MRB 574206-01-1
MRB 574306-01-1
MRB 574406-01-1
MRB 574506-01-1
MRB 574606-01-1
PREPARATION: FLAPS EXTENDED; SLATS FULLY EXTENDED;
ACCESS PANELS: 521AB, 521CB, 521EB, 522AB, 522CB, 522FB, 522KB, 522LB,
522NB, 522QB, 522SB, 522UB, 621AB, 621CB, 621EB, 622AB, 622CB, 622FB,
622KB, 622LB, 622NB, 622QB, 622SB, 622UB
ELECTRICAL FLIGHT CONTROL SYSTEM (EFCS)
278400-210-002
MEN
SOURCE:
MRB 27.80.00/03
LUBRICATE ALL TRACK ROLLERS AND PINIONS
ACCESS PANELS: 521AB, 521CB, 521EB, 522AB, 522CB, 522FB, 522KB, 522LB,
522NB, 522QB, 522SB, 522UB, 621AB, 621CB, 621EB, 622AB, 622CB, 622FB,
622KB, 622LB, 622NB, 622QB, 622SB, 622UB
SLAT TRACKS
REFERENCES
SOURCE:
CMR 278000-00001-1-C
MRB 27.80.00/04
REPLENISH PCU GEARBOX TO CONFIRM FLUID LEVEL
278468-01-1
TPS
279600-710-018
SOURCE:
CMR 279000-00001-1-C
MRB 27.90.00/02
MRB 27.90.00/05
Sub 2 - Page 44 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
281100-01-2
ZONE
190
500
600
DESCRIPTION
TANKS
SKILL TASK
CODE CODE
AF
SVC
DRAIN WATER CONTENT
INTERVALS
SOURCE
I:
36 HR
NOTE
MRB 9
I:
750 FH
OR
6 MO
MRB 9
LUR
TPS
REFERENCES
123228-281-001
SOURCE:
MRB 28.11.00/01
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
0.10
0.10
0.10
ALL
1
0.05
ALL
1
1
1
0.10
0.10
0.10
ALL
2
2
0.10
0.10
ALL
1
1
0.10
0.10
ALL
1
1
0.02
0.02
ALL
NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUEN INITIAL INTERVAL MAY
BE USED.
281100-02-1
196
ACCESS PANELS: 195BB, 196BB
TANKS
AF
OPC
CHECK LEAK MONITOR FOR EVIDENCE OF FUEL LEAKAGE AND
CORRECT CLOSURE OF THE VALVE
281100-04-2
281142-01-1
190
500
600
540
640
TANKS
AF
SVC
SIL
SAMPLE FUEL FOR MICROBIOLOGICAL CONTAMINATION ANALYSIS
NOTE : INTERVAL DEPENDING ON EACH INDIVIDUAL OPERATOR´S
ENVIRONMENT
TANK FLAP VALVES
I:
24 MO
NOTE
AF
OPC
I:
160 MO
MRB 9
CHECK FOR FULL AND FREE MOVEMENT OF CLACK VALVES
281100-200-002
SOURCE:
MRB 28.11.00/02
MRB 28.13.00/02
MRB 28.21.00/01
MRB 28.25.00/01
123228-281-003
SIL 28-079
281100-200-001
SOURCE:
MRB 28.11.00/03
PREPARATION: TANK DEFUELING;
281200-01-1
500
600
ACCESS PANELS: 540AB, 640AB
TANK VENTING SYSTEM
AF
VCK
I:
750 FH
MRB 9
281200-210-001
MRB 9
SOURCE:
MRB 28.12.00/02
281247-200-001
MRB 9
SOURCE:
MRB 28.12.00/01
281300-200-001
1
0.08
ALL
SOURCE:
MRB 28.13.00/01
MRB 28.22.00/03
281500-710-002
1
0.10
ALL
VISUAL CHECK OF VENT SURGE TANK BURST DISC (EXTERNAL)
281247-01-1
550
650
NACA VENT INTAKE
AF
VCK
I:
24 MO
VISUAL CHECK OF NACA INTAKE FOR SIGNS OF BLOCKAGE
281343-01-1
148
DRAIN MAST
AF
VCK
I:
4 MO
VISUAL CHECK OF DRAIN MAST FOR OBSTRUCTION
281500-01-1
210
INTERCELL TRANSFER SYSTEM
OPERATIONAL CHECK OF INDIVIDUAL TRANSFER VALVES TO
ENSURE VALVE SHAFT ROTATES VALVE TO OPEN POSITION
AF
OPC
I:
7500 FH
OR
50 MO
CMR**
MRB 8
LUR
SOURCE:
CMR 281500-00001-1-C
MRB 28.15.00/02
Sub 2 - Page 45 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
281600-01-1
281800-01-1
ZONE
471
481
137
138
DESCRIPTION
FUEL RECIRCULATION COOLING
OPERATIONAL CHECK OF PYLON CHECK VALVE TO ENSURE
VALVE NOT FAILED OPEN
IGNITION PREVENTION
SKILL TASK
CODE CODE
AF
AF
OPC
FNC
FUNCTIONAL CHECK OF TANK VAPOUR SEAL AND VENT DRAIN SYSTEM
(SFAR88)
281800-02-1
191
192
PREPARATION: FOR PRE 21003 - 241AF OR 131NW,FOR POST 21003 - 131NW,
132PW(REMOVE POTABLE WATER TANK);
IGNITION PREVENTION
AF
DET
INTERVALS
I:
7500 FH
SOURCE
MRB 8
I:
24000 FH
OR
72 MO
FAL
MRB 8
I:
72 MO
FAL
MRB 8
DETAILED INSPECTION OF VAPOUR SEAL (SFAR88)
281800-03-1
281800-04-1
140
540
550
640
650
140
540
550
640
650
ACCESS PANELS: 191KB, 192KB
IGNITION PREVENTION
AF
DET
I:
144 MO
MRB 9
DETAILED INSPECTION OF TANK BONDING LEADS (SFAR88)
TPS
REFERENCES
281600-710-002
SOURCE:
MRB 28.16.00/01
281800-700-001
SOURCE:
FAL 281800-00001-1-F
MRB 28.13.00/03
MRB 28.13.00/05
MRB 28.18.00/04
281800-200-001
SOURCE:
FAL 281800-00002-1-F
MRB 28.18.00/03
281800-200-002
SOURCE:
MRB 28.18.00/01
PREPARATION: 147AZ (PRE 25467) OR 147BZ (POST 25467);
ACCESS PANELS: 148AZ, 540AB, 540BB, 540CB, 540DB, 540EB, 540FB, 540GB,
540HB, 540JB, 540KB, 540LB, 540MB, 540NB, 540PB, 540QB, 540RB, 550AB,
550BB, 550CB, 550DB, 640AB, 640BB, 640CB, 640DB, 640EB, 640FB, 640GB,
640HB, 640JB, 640KB, 640LB, 640MB, 640NB, 640PB, 640QB, 640RB, 650AB,
650BB, 650CB, 650DB
IGNITION PREVENTION
AF
GVI
I:
144 MO
MRB 9
GENERAL VISUAL INSPECTION OF INTERNAL TANK WIRING AND PROBE
ATTACHMENTS (SFAR88)
281844-210-001
SOURCE:
MRB 28.18.00/02
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.10
0.10
ALL
1
1
1.00
1.00
ALL
1
1
0.40
0.40
ALL
1
1
1
1
1
10.00
10.00
10.00
10.00
10.00
ALL
1
1
1
1
1
1.60
1.60
1.60
1.60
1.60
ALL
1
1
0.05
0.05
ALL
PREPARATION: 147AZ (PRE 25467) OR 147BZ (POST 25467);
281800-05-1
137
138
ACCESS PANELS: 148AZ, 540AB, 540BB, 540CB, 540DB, 540EB, 540FB, 540GB,
540HB, 540JB, 540KB, 540LB, 540MB, 540NB, 540PB, 540QB, 540RB, 550AB,
550BB, 550CB, 550DB, 640AB, 640BB, 640CB, 640DB, 640EB, 640FB, 640GB,
640HB, 640JB, 640KB, 640LB, 640MB, 640NB, 640PB, 640QB, 640RB, 650AB,
650BB, 650CB, 650DB
IGNITION PREVENTION
GENERAL VISUAL INSPECTION OF CENTER TANK FWD CARGO BAY ISOLATION
MATS (SFAR88)
AF
GVI
I:
72 MO
MRB 9
281852-210-001
SOURCE:
MRB 28.18.00/05
ACCESS PANELS: 131NW, 131PW, 132PW
Sub 2 - Page 46 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
281800-06-1
ZONE
145
146
DESCRIPTION
IGNITION PREVENTION
SKILL TASK
CODE CODE
AF
GVI
INTERVALS
I:
144 MO
SOURCE
MRB 9
GENERAL VISUAL INSPECTION OF WIRING HARNESSES ABOVE CENTER TANK
(SFAR88)
281800-07-1
520
570
620
670
PREPARATION: FLOOR PANELS FROM FR 36 TO FR 46;
IGNITION PREVENTION
TPS
REFERENCES
281842-210-001
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.05
0.05
ALL
1
1
1
1
0.50
0.50
0.50
0.50
ALL
1
1
0.10
0.10
ALL
1
1
1
1.50
1.50
1.50
ALL
SOURCE:
MRB 28.18.00/06
AF
GVI
I:
144 MO
MRB 9
GENERAL VISUAL INSPECTION OF WING LEADING EDGE AND
TRAILING EDGE ELECTRICAL WIRING AND CONNECTIONS
(SFAR88)
281841-210-001
SOURCE:
MRB 28.18.00/07
ACCESS PANELS: 521AB, 521BB, 521BT, 521CB, 521EB, 521GB, 521HB, 522AB,
522AT, 522CB, 522EB, 522FB, 522HB, 522JB, 522KB, 522LB, 522NB, 522QB, 522SB,
522UB, 572AB, 572BB, 573AB, 573BB, 573CB, 573DB, 573EB, 573FB, 574AB, 574BB,
575AB, 575AT, 575BB, 575CB, 575DB, 575EB, 575FB, 575GB, 575HB, 575KB, 575LB,
575MB, 621AB, 621BB, 621BT, 621CB, 621EB, 621GB, 621HB, 622AB, 622AT,
622CB, 622EB, 622FB, 622HB, 622JB, 622KB, 622LB, 622NB, 622QB, 622SB, 622UB,
672AB, 672BB, 673AB, 673BB, 673CB, 673DB, 673EB, 673FB, 674AB, 674BB, 675AB,
675AT, 675BB, 675CB, 675DB, 675EB, 675FB, 675GB, 675HB, 675KB, 675LB, 675MB
281800-08-1
540
640
IGNITION PREVENTION
AF
GVI
I:
144 MO
MRB 9
GENERAL VISUAL INSPECTION OF WING FUEL PUMP
ELECTRICAL CONNECTIONS AND UNDERWING ELECTRICAL
SUPPLY CABLE (SFAR88)
281800-09-1
281800-10-1
140
540
640
122
PREPARATION: FUEL PUMP FAIRINGS;
IGNITION PREVENTION
SOURCE:
MRB 28.18.00/08
AF
GVI
I:
144 MO
MRB 9
GENERAL VISUAL INSPECTION OF FUEL PUMP CANISTERS
(SFAR88)
ACCESS PANELS: 147AZ, 148AZ, 540AB, 640AB
IGNITION PREVENTION
282100-02-1
210
MAIN FUEL PUMP SYSTEM
140
OPERATIONAL CHECK OF WING TANK PUMP PRESSURE SENSE
LINE CHECK VALVES
MAIN FUEL PUMP SYSTEM
OPERATIONAL CHECK OF CENTER TANK PUMP CANISTER CHECK
VALVES
281851-210-001
SOURCE:
MRB 28.18.00/09
AF
OPC
I:
24 MO
MRB 8
281800-710-801
1
0.12
ALL
MRB 9
SOURCE:
MRB 28.18.00/10
282100-710-002
1
0.10
ALL
SOURCE:
MRB 28.21.00/04
282100-710-003
2
0.10
ALL
OPERATIONAL CHECK OF CENTRE TANK FUEL PUMP GFI (SFAR88)
282100-01-1
281843-210-001
AF
AF
OPC
OPC
I:
24000 FH
I:
15000 FH
OR
100 MO
MRB 8
LUR
SOURCE:
MRB 28.21.00/05
Sub 2 - Page 47 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
282100-03-1
282100-04-1
ZONE
DESCRIPTION
210
MAIN FUEL PUMP SYSTEM
210
OPERATIONAL CHECK OF AIR RELEASE VALVES TO ENSURE
ADEQUATE FUEL FLOW UNDER SUCTION FEED CONDITIONS
MAIN FUEL PUMP SYSTEM
SKILL TASK
CODE CODE
AF
AF
OPC
OPC
INTERVALS
I:
15000 FH
OR
100 MO
I:
6500 FH
SOURCE
MRB 8
LUR
CMR**
MRB 8
OPERATIONAL CHECK TO ENSURE THAT BOTH CENTER TANK
PUMPS FEED FOR 2 MINUTES AFTER ENGINE START
282100-05-1
410
420
520
620
FUEL PUMP SYSTEM
AF
VCK
VISUAL CHECK OF PIPES, COUPLINGS AND LP VALVE EXTERNAL TO TANK
FROM FRONT SPAR TO DISCONNECT PANEL FOR LEAKS WITH BOOSTER
PUMP ON AND LP VALVE OPEN
I:
7500 FH
OR
50 MO
MRB 9
LUR
I:
24000 FH
OR
160 MO
I:
80 MO
OR
24000 FH
OR
18000 FC
I:
750 FH
MRB 9
LUR
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
282100-710-008
1
0.10
ALL
SOURCE:
MRB 28.21.00/08
282100-710-005
2
1.00
ALL
1
1
1
1
0.05
0.05
0.05
0.05
ALL
1
1
0.02
0.02
ALL
SOURCE:
MRB 28.21.00/09
282000-960-001
SIL 28-073
2
2
2.00
2.00
ALL
282200-210-001
1
0.10
ALL
SOURCE:
MRB 28.22.00/01
282300-720-001
1
0.10
ALL
1
0.10
ALL
SOURCE:
CMR 282100-00001-1-C
MRB 28.21.00/03
282100-790-002
SOURCE:
MRB 28.21.00/02
ACCESS PANELS: 413AL, 413CL, 413EL, 414AZ, 414FR, 437AL, 471AL, 472AR,
423AL, 423AZ, 423CL, 423FL, 424ER, 447AL, 481AL, 482AR, 522AB, 622AB
282100-06-1
540
640
MAIN FUEL PUMP SYSTEM
AF
OPC
CHECK SUCTION VALVES FOR FULL AND FREE MOVEMENT
282100-07-1
470
480
MAIN FUEL PUMP SYSTEM
AF
DIS
AF
OPC
DISCARD "O" RINGS ON PYLON ENGINE FUEL FEED PIPE
CONNECTORS AND REPLACE BY NEW "O" RINGS
282200-02-1
282300-01-2
148
ACCESS PANELS: 414FR, 471AL, 472AR, 423FL, 481AL, 482AR
APU FUEL PUMP SYSTEM
210
CHECK FOR LEAKAGE FROM SHROUD DRAIN MAST AND APU
COMPARTMENT DRAIN MAST WITH APU FUEL PUMP RUNNING
CROSSFEED SYSTEM
AF
OPC
OPERATIONAL CHECK OF CROSSFEED VALVE USING INDIVIDUAL
MOTORS AND CHECK FUEL FLOW IN "OPEN" AND FUEL SHUT
OFF IN "CLOSED" POSITIONS
282400-01-1
210
ACCESS PANELS: 734
ENGINE LOW PRESSURE SHUT OFF
OPERATIONAL CHECK OF LP SHUT OFF VALVES AND THEIR
CONTROLS TO ENSURE NO FLOW WHEN SELECTED CLOSED WITH
BOOSTER PUMP ON
AF
OPC
SIL
MRB 9
I:
7500 FH
OR
50 MO
MRB 8
LUR
I:
15000 FH
OR
100 MO
NOTE
MRB 8
LUR
282100-280-001
SOURCE:
MRB 28.23.00/01
282400-790-003
SOURCE:
MRB 28.24.00/01
MRB 28.24.00/02
NOTE: TASK MAY BE PERFORMED AT OPPORTUNITY OF ENGINE
REMOVAL PROVIDED INTERVAL NOT EXCEEDED
Sub 2 - Page 48 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
282541-01-1
ZONE
622
DESCRIPTION
COUPLING REFUEL/DEFUEL
SKILL TASK
CODE CODE
AF
DET
INTERVALS
I:
5000 FC
SOURCE
MRB 6
DETAILED INSPECTION OF COUPLING REFUEL/DEFUEL.
TPS
REFERENCES
282541-200-001
MEN
TASKM. APPLICABI
H.
LITY
1
0.10
1
1
0.10
0.10
1
0.20
ALL
1
1
0.02
0.02
ALL
1
0.06
ALL
SOURCE:
MRB 28.25.00/02
ACCESS PANELS: 622HB
282541-01-2
522
622
COUPLING REFUEL/DEFUEL
AF
DET
I:
5000 FC
MRB 6
DETAILED INSPECTION OF COUPLING REFUEL/DEFUEL.
282900-02-1
210
ACCESS PANELS: 522HB, 622HB
APU LOW PRESSURE FUEL SHUT OFF
SOURCE:
MRB 28.25.00/02
AF
OPC
OPERATIONAL CHECK OF APU LP FUEL VALVE FOR EVIDENCE
OF INTERNAL LEAKAGE WITH LEFT WING TANK PUMP ON
290000-02-1
435
445
ACCESS PANELS: 315AL
HYDRAULIC POWER
AF
VCK
CHECK CLOGGING INDICATOR ON ENGINE DRIVEN PUMP
(EDP) CASE DRAIN FILTER
( POP OUT NOT PROTRUDING )
290000-05-1
100
ACCESS PANELS: 437AL, 447AL
HYDRAULIC POWER
CHECK CLOGGING INDICATORS OF THE FOLLOWING
FILTERS(POP OUT NOT PROTRUDING)
-HIGH PRESSURE DELIVERY
-GROUND SERVICING (RESERVOIR FILLING)
-RETURN (LOW PRESSURE)
-BLUE HYDRAULIC SYSTEM ELECTRICAL PUMP CASE
DRAIN
-RESERVOIR PRESSURIZATION FILTER
-WATER SEPARATOR
282541-200-001
AF
VCK
I:
24000 FH
OR
160 MO
MRB 9
LUR
I:
1000 FH
OR
12 MO
MRB 9
LUR
I:
1000 FH
OR
12 MO
MRB 9
LUR
282900-710-002
1130 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
0649 1200
1379 2151
2163
SOURCE:
MRB 28.29.00/02
291000-200-007
SOURCE:
MRB 29.10.00/06
MRB 29.10.00/28
291000-210-002
SOURCE:
MRB 29.10.00/28
ACCESS PANELS: 195BB, 196BB, 197CB, 197FB, 734
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SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
290000-07-1
ZONE
100
DESCRIPTION
HYDRAULIC SYSTEM SEALS
SKILL TASK
CODE CODE
INTERVALS
SOURCE
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
AF
VCK
I:
24 MO
SIL
291000-200-025
SIL 29-064
1
0.33
ALL
AF
DET
I:
8 DY
MRB 6
LUR
291000-200-001
1
0.10
ALL
1
0.10
ALL
292300-710-002
1
0.10
ALL
SOURCE:
MRB 29.10.00/38
291400-680-001
1
0.10
ALL
292300-710-003
1
0.10
ALL
SOURCE:
MRB 29.10.00/37
291000-720-002
2
0.30
ALL
VISUAL CHECK OF HIGH AND LOW PRESSURE MANIFOLDS AND
GROUND SERVICE PANELS AND MANIFOLDS FOR SIGNS OF
EXTERNAL LEAKAGE.
291000-01-1
100
NOTE: THE INTERVAL IS SELECTED TO FIT WITH THE
CURRENT C EQUIVALENT CALENDAR TIME AS DEFINED IN
A318/A319/A320/A321 MPD GENERAL INTRODUCTION. THE
INTERVAL MAY BE ADAPTED TO AN INDIVIDUALLY ACHIEVED
INTERVAL ESCALATION HENCE ALLOWING TO PERFORM THE
TASK DURING THE TYPICAL C TASK PACKAGE.
MAIN HYDRAULIC POWER
CHECK FLUID LEVEL ON RESERVOIR INDICATORS
291000-02-1
100
ACCESS PANELS: 196BB, 197FB, 744
MAIN HYDRAULIC POWER
SOURCE:
MRB 29.10.00/01
AF
DET
CHECK RESERVOIR AIR PRESSURE ON RESERVOIR GAUGE
291000-04-1
210
ACCESS PANELS: 196BB, 197FB, 744
MAIN HYDRAULIC POWER
AF
FNC
FUNCTIONAL CHECK OF PTU GREEN TO YELLOW
291000-05-1
195
MAIN HYDRAULIC POWER
AF
SVC
DRAIN WATER SEPARATOR
291000-06-1
210
ACCESS PANELS: 195BB
MAIN HYDRAULIC POWER
AF
FNC
FUNCTIONAL CHECK OF PTU YELLOW TO GREEN
291000-08-1
210
MAIN HYDRAULIC POWER
FUNCTIONAL CHECK OF PRIORITY VALVES IN GREEN, BLUE
AND YELLOW SYSTEM
AF
FNC
I:
750 FH
OR
6 MO
MRB 6
LUR
I:
22000 FH
OR
144 MO
I:
2250 FH
OR
24 MO
MRB 6
LUR
I:
7500 FH
OR
50 MO
I:
36000 FH
OR
144 MO
MRB 6
LUR
291000-200-002
SOURCE:
MRB 29.10.00/02
MRB 9
LUR
SOURCE:
MRB 29.10.00/13
MRB 6,8
SOURCE:
MRB 29.10.00/19
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SECTION: II
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SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
291000-09-1
ZONE
210
DESCRIPTION
MAIN HYDRAULIC POWER
SKILL TASK
CODE CODE
AF
OPC
OPERATIONAL CHECK OF HYDRAULIC FIRE SHUT OFF
VALVES AND ASSOCIATED INDICATING SYSTEM.
291000-10-1
574
674
NOTE: APPLICABLE FOR PRE 22155 IF ACTUATOR
P/N E0 1100 AMENDMENT A, OR P/N E0 1100
AMENDMENT AB, OR P/N E0 1100 AMENDMENT AC, OR
P/N E0 1100 AMENDMENT BC, OR P/N E0 1100
AMENDMENT C, OR P/N A06 A00 IS INSTALLED
MAIN HYDRAULIC POWER
AF
FNC
FUNCTIONAL CHECK OF HYDRAULIC FIRE SHUT OFF VALVES
INTERVALS
SOURCE
I:
10000 FH
OR
72 MO
MRB 8
LUR
I:
16000 FH
OR
144 MO
MRB 8
LUR
I:
600 FH
OR
6 MO
MRB 9
LUR
I:
7500 FH
OR
24 MO
NOTE
MRB 9
SIL
I:
1500 FH
OR
12 MO
MRB 9
LUR
I:
24 MO
MRB 9
TPS
REFERENCES
291000-710-001
MEN
TASKM. APPLICABI
H.
LITY
1
0.10
ALL
2
2
0.20
0.20
ALL
1
0.10
ALL
1
0.30
ALL
1
0.30
ALL
291000-710-004
1
0.25
ALL
SOURCE:
MRB 29.10.00/36
291200-710-001
1
0.05
ALL
SOURCE:
MRB 29.10.00/14
291000-720-001
SOURCE:
MRB 29.10.00/20
NOTE: TASK MAY BE PERFORMED AT OPPORTUNITY OF ENGINE
REMOVAL PROVIDED INTERVAL NOT EXCEEDED
291000-14-1
100
ACCESS PANELS: 574AB, 674AB
MAIN HYDRAULIC POWER
AF
FNC
CHECK NITROGEN CHARGE PRESSURE ON HYDRAULIC POWER
ACCUMULATORS
291000-15-1
100
ACCESS PANELS: 196BB, 744
MAIN HYDRAULIC POWER
AF
DET
ANALYZE HYDRAULIC FLUID
NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY
BE USED.
291000-18-1
148
ACCESS PANELS: 734, 744
MAIN HYDRAULIC POWER
AF
SVC
DRAIN RECOVERY TANK
291000-20-1
210
ACCESS PANELS: 734, 744
MAIN/AUXILIARY POWER
AF
OPC
SOURCE:
MRB 29.10.00/22
210
BLUE MAIN HYDRAULIC POWER
FUNCTIONAL CHECK OF BLUE ELECTRICAL PUMP PRESSURE BY
READING ECAM INDICATION
AF
FNC
I:
7500 FH
OR
50 MO
123229-281-001
JIC A320-29-10-00
SIL 29-081
SOURCE:
MRB 29.10.00/23
291700-680-001
SOURCE:
MRB 29.10.00/32
OPERATIONAL CHECK OF EDP DEPESSURIZATION
291200-01-1
291000-200-008
SIL 29-092
MRB 6
LUR
SOURCE:
MRB 29.10.00/10
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SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
291900-01-1
291900-02-1
ZONE
DESCRIPTION
210
GROUND INTERNAL LEAK TEST SYSTEM
210
FUNCTIONAL CHECK TO MONITOR INTERNAL LEAK RATE OF
YELLOW AND GREEN HYDRAULIC SYSTEMS
GROUND INTERNAL LEAK TEST SYSTEM
SKILL TASK
CODE CODE
AF
AF
FNC
FNC
FUNCTIONAL CHECK TO MONITOR INTERNAL LEAK RATE OF
BLUE HYDRAULIC SYSTEM
292000-04-1
190
AUXILIARY HYDRAULIC POWER
AF
FNC
OPERATIONAL CHECK OF RAT MANUAL DEPLOYMENT AND
FUNCTIONAL CHECK OF RAT USING GROUND TEST UNIT,
FOLLOWED BY CHECK OF FILTER INDICATOR
292000-05-1
210
ACCESS PANELS: 195BB, 197EB
AUXILIARY HYDRAULIC POWER
AF
OPC
OPERATIONAL CHECK OF RAM AIR TURBINE (RAT) AUTOMATIC
DEPLOYMENT
292000-07-1
190
ACCESS PANELS: 197EB
AUXILIARY HYDRAULIC POWER
AF
FNC
INTERVALS
SOURCE
I:
24000 FH
OR
144 MO
I:
7500 FH
OR
50 MO
MRB 6,9
I:
3600 FH
OR
18 MO
CMR*
MRB 8
I:
3600 FH
OR
18 MO
CMR*
MRB 8
I:
72 MO
MRB 8
CMR*
MRB 8
LUR
190
ACCESS PANELS: 197EB
AUXILIARY HYDRAULIC POWER
AF
DET
I:
3600 FH
OR
18 MO
CMR*
MRB 8
RAM AIR TURBINE
TASKM. APPLICABI
H.
LITY
291000-220-001
2
0.40
ALL
SOURCE:
MRB 29.10.00/18
291000-220-002
2
0.30
ALL
SOURCE:
CMR 291000-00003-1-C
MRB 29.10.00/05
MRB 29.10.00/12
292200-720-003
2
1.00
ALL
SOURCE:
CMR 291000-00001-2-C
CMR 291000-00001-3-C
MRB 24.50.00/10
MRB 29.10.00/29
292200-710-006
2
0.10
ALL
2
0.10
ALL
1
0.40
0649
1
0.30
ALL
1
0.30
ALL
292200-280-002
AF
DET
I:
20 MO
MRB 8
292200-220-002
SOURCE:
CMR 291000-00001-2-C
MRB 29.10.00/34
ACCESS PANELS: 195BB, 197EB
195
MEN
SOURCE:
MRB 29.10.00/27
DETAILED INSPECTION OF RAT BLADES FOR EVIDENCE OF PLATING CRACKS
292251-02-1
REFERENCES
SOURCE:
CMR 291000-00002-1-C
MRB 29.10.00/08
FUNCTIONAL CHECK OF ANTI-ICING DEVICE MAGNETS
292000-09-1
TPS
DETAILED INSPECTION OF RAT ASSEMBLY AND DOORS IN
DEPLOYED POSITION
292251-200-003
SOURCE:
MRB 29.10.00/09
PREPARATION: RAM AIR TURBINE EXTENSION;
293100-01-1
190
ACCESS PANELS: 195BB, 197EB
HYDRAULIC FLUID QUANTITY INDICATING
FUNCTIONAL CHECK OF RESERVOIR LOW LEVEL WARNING
AF
FNC
I:
24000 FH
MRB 9
293100-710-001
SOURCE:
MRB 29.30.00/05
ACCESS PANELS: 197CB, 197EB, 198CB
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
293400-01-1
301151-01-2
ZONE
210
522
622
DESCRIPTION
RESERVOIR PRESSURIZATION INDICATING
OPERATIONAL CHECK OF RESERVOIR LOW AIR PRESSURE
WARNING
WING ANTI-ICE CONTROL VALVE
SKILL TASK
CODE CODE
AF
AF
OPC
DIS
INTERVALS
I:
7500 FH
OR
50 MO
I:
22000 FH
SOURCE
MRB 9
LUR
MRB 6
REPLACE WING ANTI-ICING FILTER
302100-01-1
210
ACCESS PANELS: 522AB, 622AB
ENGINE AIR INTAKE ICE PROTECTION
438
448
ACCESS PANELS: 438AR, 448AR
ENGINE AIR INTAKE ANTI-ICE DUCT
AF
OPC
120
ACCESS PANELS: 438AR, 452AR, 448AR, 462AR
PROBE ICE PROTECTION
FUNCTIONAL CHECK OF THE INSULATION RESISTANCE OF THE PITOT PROBE
HEATER
293400-710-001
SOURCE:
MRB 29.30.00/04
301151-960-001
MEN
TASKM. APPLICABI
H.
LITY
1
0.10
ALL
1
1
0.50
0.50
ALL
I:
48 MO
MRB 9
302100-710-001
1
0.30
ALL
1
1
0.20
0.20
ALL
1
0.25
ALL
SOURCE:
MRB 30.21.00/02
AF
DET
DETAILED INSPECTION OF INLET COWL ANTI-ICE SUPPLY
DUCTS AND ASSOCIATED HARDWARE IN THE CORE COMPARTMENT
303100-01-1
REFERENCES
SOURCE:
MRB 30.11.00/03
OPERATIONAL CHECK OF ENGINE ANTI-ICE SYSTEM FAULT
WARNING
302149-01-1
TPS
EL
FNC
I:
6000 FH
OR
40 MO
MRB 6
LUR
I:
24 MO
MRB 9
302149-200-001
SOURCE:
MRB 30.21.00/01
303100-720-001
SIL 34-084
SOURCE:
MRB 30.31.00/02
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
313000-01-1
ZONE
210
DESCRIPTION
CFDS AND DATA RECORDING SYSTEM
SKILL TASK
CODE CODE
AV
OPC
READ CENTRALIZED FAULT DISPLAY SYSTEM (CFDS)
FOR CLASS 3 FAULTS
R 313300-01-1-SDM
120
SOLID STATE FLIGHT DATA RECORDER (SSFDR)
AV
SVC
INTERVALS
SOURCE
I:
750 FH
OR
6 MO
MRB 9
LUR
I:
24 MO
SPECI
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
313200-869-002
1
0.10
ALL
SOURCE:
MRB 21.21.00/01
MRB 21.26.00/01
MRB 21.28.00/01
MRB 21.31.00/01
MRB 21.50.00/01
MRB 24.20.00/04
MRB 24.40.00/01
MRB 26.12.00/02
MRB 26.13.00/02
MRB 27.50.00/01
MRB 27.50.01/01
MRB 27.80.00/01
MRB 28.15.00/01
MRB 28.28.00/10
MRB 28.42.00/01
MRB 28.46.00/01
MRB 29.30.00/03
MRB 30.31.00/01
MRB 30.42.00/01
MRB 32.40.00/04
MRB 36.00.00/01
MRB 49.40.00/01-13
MRB 49.40.00/01-32
MRB 49.40.00/01-36
MRB 49.51.20/01-36
MRB 49.61.00/01-36
MRB 49.70.00/01-32
MRB 49.70.00/01-36
MRB 49.90.00/01-32
MRB 49.91.00/01-13
313300-710-009
1
1.00
ALL
SSFDR READOUT AND PARAMETER VERIFICATION IN ACCORDANCE TO
COMMISSION REGULATION (EU) No 965/2012
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
313300-03-1
ZONE
312
DESCRIPTION
DFDR SYSTEM INTERCONNECTION
SKILL TASK
CODE CODE
AV
OPC
OPERATIONAL CHECK OF ULB
INTERVALS
I:
24 MO
NOTE
SOURCE
MRB 9
FOR UNDERWATER LOCATOR:
- P/N DK120/DK100 (BATTERY: P/N 810-2007K), VENDOR
DUKANE OR
- P/N N15F210B, VENDOR DUKANE (BATTERY: P/N
810-418A, VENDOR AVIQUIPO INC) OR
- P/N ELP 362D, VENDOR: DATASONIC OR
- P/N 266E0305-00/01/02, VENDOR: L-3 COMMUNICATION
313300-04-1
210
ACCESS PANELS: 312AR
DFDR SYSTEM INTERCONNECTION
315000-02-1
315000-04-1
316000-01-1
210
210
210
210
CENTRAL WARNING SYSTEMS/ELECTRONIC
INSTRUMENT SYSTEM (EIS)
OPERATIONAL CHECK OF CORRECT OPERATION OF PFD-ND AND
ECAM-ND MANUAL TRANSFER
CENTRAL WARNING SYSTEMS/ELECTRONIC
INSTRUMENT SYSTEM (EIS)
OPERATIONAL CHECK OF CORRECT OPERATION OF EFIS AND
ECAM DMC AUTOMATIC AND MANUAL TRANSFER
CENTRAL WARNING SYSTEMS/ELECTRONIC
INSTRUMENT SYSTEM (EIS)
OPERATIONAL CHECK OF DMC3 POWER SUPPLY TRANSFER WHEN
BUSBAR 101XP IS LOST
ELECTRONIC INSTRUMENT SYSTEM
OPERATIONAL CHECK OF EFIS/ECAM SWITCHING FUNCTIONS:
- MANUAL DMC 1 + 2 TO DMC 3 SWITCHING
- MANUAL PFD/ND TRANSFER
- MANUAL ECAM/ND TRANSFER
- AUTOMATIC UPPER DU/LOWER DU TRANSFER
- AUTOMATIC PFD/ND TRANSFER
REFERENCES
313300-710-015
CMM 31-31-36
CMM 31-30-40
MEN
TASKM. APPLICABI
H.
LITY
1
0.15
ALL
313300-710-006
1
0.10
ALL
SOURCE:
MRB 31.33.00/05
316000-740-005
1
0.20
2151 2163
1
0.40
2151 2163
1
0.20
2151 2163
1
0.30
0649 1130
1200 1379
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
SOURCE:
MRB 31.33.00/04
AV
OPC
I:
24 MO
MRB 9
OPERATIONAL CHECK OF DFDR VIA MCDU
315000-01-1
TPS
AV
AV
AV
AV
OPC
OPC
OPC
OPC
I:
7500 FH
OR
50 MO
MRB 9
LUR
I:
7500 FH
OR
50 MO
MRB 9
LUR
I:
7500 FH
OR
50 MO
MRB 9
LUR
I:
6000 FH
OR
48 MO
MRB 9
LUR
SOURCE:
MRB 31.60.01/02
316000-710-005
SOURCE:
MRB 31.60.01/04
316000-710-006
SOURCE:
MRB 31.60.01/03
316000-710-002
SOURCE:
MRB 31.50.00/01
MRB 31.60.00/01
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SECTION: II
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SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
316000-02-1
ZONE
210
DESCRIPTION
ELECTRONIC INSTRUMENT SYSTEM
SKILL TASK
CODE CODE
EL
OPC
PERFORM ELECTRONIC INSTRUMENT SYSTEM (EIS) INPUT TEST
316322-01-1
210
DISPLAY UNIT
210
321000-01-1
711
731
741
731
741
I:
7500 FH
OR
50 MO
MRB 9
LUR
321100-15-1
731
741
316000-740-002
MEN
TASKM. APPLICABI
H.
LITY
1
0.15
SOURCE:
MRB 31.60.00/02
0649 1130
1200 1379
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
0649 1130
1200 1379
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
0649 1130
1200 1379
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
SIL
LUR
316322-400-002
SIL 31-025
JIC A320-31-63-00
1
0.25
AF
FNC
SIL
LUR
316322-200-001
SIL 31-030
1
0.25
NLG AND MLG CYLINDER CLEANING
AF
LUB
T:
6000 FH
OR
48 MO
I:
1200 FH
OR
12 MO
NOTE
I: 8 DY
SPECI
322100-100-051
321100-100-052
1
CLEAN THE CHROMIUM SURFACES OF NLG AND MLG CYLINDERS
MAIN LANDING GEAR AND DOORS
AF
LUB
I:
4 MO
OR
500 FC
MRB 5,8
122232-640-001
2
2
0.50
0.50
ALL
1
1
0.20
0.20
ALL
0
0
N/A
N/A
ALL
DISPLAY UNIT
MLG LUBRICATION
AF
LUB
I:
8 DY
SPECI
SOURCE:
MRB 32.11.00/02
MRB 32.11.00/18
MRB 32.30.00/03
122232-640-001
MLG LOWER BEARING 3 POINTS LUBRICATION
MAIN GEAR
AF
SDI
I:
20000 FC
OR
120 MO
MRB 5,8
321100-220-006
ACCESS PANELS: 734, 744
731
741
REFERENCES
I:
2400 FH
OR
24 MO
NOTE
LUBRICATION OF MAIN LANDING GEAR AND DOORS
321000-01-2-SDM
TPS
CHK
FUNCTIONAL CHECK OF DISPLAY UNITS BRIGHTNESS
NOTE : INTERVAL MAY BE ADJUSTED IN ACCORDANCE
WITH OPERATOR EXPERIENCE
320000-01-1-SDM
SOURCE
EL
REPOSITION ALL CATHODE RAY TUBES BY SWAPPING
ALL DISPLAY UNITS FROM ONE POSITION(PFD,ND,
UPPER ECAM,LOWER ECAM)TO ANOTHER
NOTE : INTERVAL MAY BE ADJUSTED IN ACCORDANCE
TO OPERATOR´S EXPERIENCE
316322-02-1
INTERVALS
SPECIAL DETAILED INSPECTION OF BUSHINGS AND BEARINGS IN MLG
AIRFRAME ATTACHMENT FITTINGS
TBD
ALL
SOURCE:
MRB 32.11.00/15
PREPARATION: AIRCRAFT JACKING; MAIN LANDING GEAR REMOVAL;
ACCESS PANELS: 734, 744
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
321101-01-2
ZONE
731
741
DESCRIPTION
MAIN GEAR
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF MAIN LANDING GEAR, SLIDING
TUBE (TWIN WHEEL), BRAKE ATTACHMENT FLANGE, UPPER AND
LOWER TORQUE LINKS, UPPER AND LOWER TORQUE LINK PINS
AND APEX PIN & NUT - EXTERNAL SURFACES, EXCEPT WHERE
COVERED BY DRESSINGS AND BUSH FLANGES.
321101-01-3-SDM
731
741
321103-01-1
731
741
321111-03-1
731
741
731
741
731
741
731
741
MRB CPCP
731
741
321100-200-008
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.40
0.40
ALL
SOURCE:
MRB 321101-01-2
I:
8 DY
SPECI
JIC A320-32-11-13
SB 32A1374
1
1
0.20
0.20
ALL
CLEAN AND EXAMINE THE MLG SLIDING TUBE
MAIN GEAR
AF
DET
T:
6 YE
I:
6 YE
MRB CPCP
321100-200-009
1
1
0.40
0.40
ALL
I:
1500 FC
OR
18 MO
I:
10000 FC
OR
80 MO
MRB 6,9
LUR
1
1
0.10
0.10
ALL
2
2
1.00
1.00
ALL
I:
5000 FC
OR
24 MO
I:
10000 FC
MRB 6
121432-614-003
1
1
0.40
0.40
ALL
MRB 6
SOURCE:
MRB 32.11.00/03
321127-200-001
1
1
0.20
0.20
ALL
MRB CPCP
SOURCE:
MRB 32.11.00/05
321100-200-018
1
1
0.60
0.60
ALL
DETAILED INSPECTION OF MAIN LANDING GEAR, MAIN
FITTING, FORWARD PINTLE PIN, FORWARD PINTLE PIN LOCK/
STUB BOLTS, REAR PINTLE PIN & NUT, RETRACTION
ACTUATOR ATTACHMENT PINS & UPPER DIAPHRAGM CROSS PIN
- EXTERNAL SURFACES, EXCEPT WHERE COVERED BY
DRESSINGS & BUSH FLANGES.
MAIN LANDING GEAR
AF
FNC
MAIN LANDING GEAR SHOCK ABSORBER
AF
FNC
PREPARATION: AIRCRAFT JACKING;
MAIN LANDING GEAR SHOCK ABSORBER
AF
FNC
MAIN LANDING GEAR TORQUE LINK
AF
DET
SOURCE:
MRB 321103-01-1
MRB 6
MAIN LANDING GEAR PARTS
DETAILED INSPECTION OF MAIN LANDING GEAR, RETRACTION ACTUATOR EXTERNAL SURFACE, EXCEPT WHERE COVERED BY DRESSINGS & BUSH
FLANGES.
AF
DET
T:
6 YE
I:
6 YE
321111-200-001
SOURCE:
MRB 32.11.00/13
121232-611-004
SOURCE:
MRB 32.11.00/04
CHECK OF MLG TORQUE LINKS FOR EXCESSIVE PLAY
321146-01-1
NO
REFERENCES
DET
CHECK OF MLG SHOCK ABSORBER CHARGE PRESSURE
321127-01-1
T:
6 YE
I:
6 YE
TPS
AF
CHECK OF MLG SHOCK ABSORBER FLUID LEVEL
321113-04-1
SOURCE
PREPARATION: AIRCRAFT JACKED, SLIDING TUBE FULLY EXTENDED.;
MLG SLIDING TUBE (CHROME EXTERNAL FASE)
CHECK OF MLG TORQUE LINK DAMPER FLUID LEVEL
321113-03-1
INTERVALS
SOURCE:
MRB 321146-01-1
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SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
321156-01-1
321156-01-2
322000-01-1
ZONE
731
741
731
741
710
DESCRIPTION
MAIN LANDING GEAR PARTS
DETAILED INSPECTION OF MAIN LANDING GEAR, UPPER &
LOWER SIDESTAY, UPPER & LOWER CARDANS AND NUTS, UPPER
& LOWER LOCK LINKS, LOCKSTAY CARDAN, LOCKSTAY CARDAN
BRACKET & BOLTS, CUFF, TRIANGULATION LINK, BANANA
LINKS, UPPER & LOWER CARDAN PINS, SIDESTAY PIVOT PIN,
UPPER PIN (SPRINGS), LOCKSTAY CARDAN PIN, UPPER &
LOWER LOCK LINK PINS, LOCK LINK CENTER PIN,
TRIANGULATION LINK PINS, LOCK LINK/BANANA LINK PIN,
CUFF PINS & LOWER (SPRINGS) PIN - EXTERNAL SURFACES,
EXCEPT WHERE COVERED BY DRESSINGS, BUSH FLANGES &
FITTINGS.
MAIN LANDING GEAR PARTS
DETAILED INSPECTION OF MAIN LANDING GEAR, UPPER &
LOWER SIDESTAY, UPPER & LOWER CARDANS AND NUTS,UPPER
& LOWER LOCK LINKS, LOCKSTAY CARDAN, CUFF,
TRIANGULATION LINK, BANANA LINKS, UPPER & LOWER
CARDAN PINS, SIDESTAY PIVOT PIN, UPPER PIN (SPRINGS),
LOCKSTAY CARDAN PIN, UPPER & LOWER LOCK LINK PINS,
LOCK LINK CENTER PIN, TRIANGULATION LINK PINS, LOCK
LINK/BANANA LINK PIN, CUFF PINS & LOWER (SPRINGS) PIN
- EXTERNAL SURFACES, EXCEPT WHERE COVERED BY
DRESSINGS, BUSH FLANGES & FITTINGS.
NOSE LANDING GEAR AND DOORS
SKILL TASK
CODE CODE
AF
AF
AF
DET
DET
LUB
LUBRICATION OF NOSE LANDING GEAR AND DOORS
INTERVALS
SOURCE
T:
6 YE
I:
6 YE
MRB CPCP
T:
6 YE
I:
6 YE
MRB CPCP
I:
4 MO
OR
500 FC
MRB 5,8
TPS
REFERENCES
321100-200-019
TASKM. APPLICABI
H.
LITY
1
1
0.67
0.67
0649
1
1
0.67
0.67
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
122232-640-002
2
0.50
ALL
1
0
SOURCE:
MRB 321156-01-1
321100-200-019
SOURCE:
MRB 321156-01-2
322000-01-1-SDM
711
NLG LUBRICATION
AF
LUB
I: 8 DY
SPECI
SOURCE:
MRB 32.21.00/01
MRB 32.30.00/03
MRB 32.50.00/01
122232-640-002
322100-07-1
710
NLG LOWER BEARING 2 POINTS LUBRICATION
NOSE GEAR
AF
SDI
I:
120 MO
OR
20000 FC
MRB 5,8
322100-200-016
ACCESS PANELS: 713, 714
SPECIAL DETAILED INSPECTION OF BUSHINGS AND BEARINGS IN NLG
AIRFRAME ATTACHMENT FITTINGS.
MEN
TBD
N/A
ALL
ALL
SOURCE:
MRB 32.21.00/07
PREPARATION: NLG REMOVED; AIRCRAFT JACKING;
ACCESS PANELS: 713, 714
Sub 2 - Page 58 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
322113-01-1
ZONE
711
DESCRIPTION
NOSE LANDING GEAR SHOCK ABSORBER
SKILL TASK
CODE CODE
AF
FNC
CHECK OF NLG SHOCK ABSORBER CHARGE PRESSURE
AND FLUID LEVEL.
322127-01-1
711
ACCESS PANELS: 713, 714
NOSE LANDING GEAR TORQUE LINK
AF
FNC
INTERVALS
SOURCE
I:
5000 FC
OR
24 MO
MRB 6
I:
5000 FC
ISB
MRB 6
TPS
REFERENCES
121232-610-002
MEN
TASKM. APPLICABI
H.
LITY
1
0.40
ALL
1
0.60
ALL
SOURCE:
MRB 32.21.00/03
322100-200-003
ISB 32-1252
CHECK OF NLG TORQUE LINKS FOR EXCESSIVE PLAY
322128-01-1
711
NOTE: INCLUDING CHECK OF TORQUE LINK APEX PIN FOR
CRACKS, WHERE APPLICABLE
NOSE LANDING GEAR
SOURCE:
MRB 32.21.00/02
AF
GVI
AF
DET
INSPECTION FOR BARREL WEAR
322141-01-1
711
NOSE LANDING GEAR PARTS
DETAILED INSPECTION OF NOSE LANDING GEAR, BARREL,
SLIDING TUBE AND TURNING TUBE EXTERNAL SURFACES,
EXCEPT WHERE COVERED BY DRESSINGS AND BUSH FLANGES.
322142-01-1
322143-01-1
322144-01-1
711
PREPARATION: AIRCRAFT JACKED, SLIDING TUBE FULLY EXTENDED.;
NOSE LANDING GEAR PARTS
711
DETAILED INSPECTION OF NOSE LANDING GEAR, TORQUE
LINKS - EXTERNAL SURFACES, EXCEPT WHERE COVERED BY
DRESSINGS AND BUSH FLANGES.
NOSE LANDING GEAR PARTS
711
DETAILED INSPECTION OF NOSE LANDING GEAR, FORESTAY
UPPER PANEL, LOWER LINK AND UNIVERSAL JOINT EXTERNAL SURFACES, EXCEPT WHERE COVERED BY DRESSINGS
AND BUSH FLANGES.
NOSE LANDING GEAR PARTS
DETAILED INSPECTION OF NOSE LANDING GEAR, LOCK LINK
UPPER AND LOCK LINK LOWER - EXTERNAL SURFACES, EXCEPT
WHERE COVERED BY DRESSINGS AND BUSH FLANGES.
AF
AF
AF
DET
DET
DET
I:
4500 FC
OR
20 MO
T:
6 YE
I:
6 YE
ISB
JIC A320-32-21-00
ISB 32-1323
1
1.50
0649 1200
1761
MRB CPCP
322100-200-018
1
0.18
ALL
T:
6 YE
I:
6 YE
MRB CPCP
1
0.13
ALL
T:
6 YE
I:
6 YE
MRB CPCP
1
0.20
ALL
T:
6 YE
I:
6 YE
MRB CPCP
1
0.20
ALL
SOURCE:
MRB 322141-01-1
322100-200-013
SOURCE:
MRB 322142-01-1
322100-200-014
SOURCE:
MRB 322143-01-1
322100-200-012
SOURCE:
MRB 322144-01-1
Sub 2 - Page 59 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
322145-01-1
322151-01-1
323000-01-1
323000-16-1
R 323000-17-1
ZONE
DESCRIPTION
711
NOSE LANDING GEAR PARTS
711
DETAILED INSPECTION OF NOSE LANDING GEAR, UPPER
BARREL HINGE PINS, FORESTAY BARREL PIN, ACTUATING
CYLINDER PINS, RETAINING NUT SHOCK ASSY, TORQUE LINK
PINS, TORQUE LINK APEX PIN AND NUT, UPPER PANEL TO
STRUCTURE PINS, UPPER PANEL TO UNIVERSAL JOINT PIN,
LOCK LINK CENTRE PIN, LOWER LOCK LINK PIN, LOWER LOCK
LINK TO UNIVERSAL JOINT PIN AND CROSS PIN - EXTERNAL
SURFACES, EXCEPT WHERE COVERED BY DRESSINGS AND BUSH
FLANGES.
NOSE LANDING GEAR PARTS
711
731
741
711
731
741
210
DETAILED INSPECTION OF NOSE LANDING GEAR, ACTUATING
CYLINDER - EXTERNAL SURFACES, EXCEPT WHERE COVERED BY
DRESSINGS AND BUSH FLANGES.
NORMAL EXTENSION AND RETRACTION
VISUAL CHECK OF NLG AND MLG DOWNLOCK SPRINGS AND
ATTACHMENTS.
NORMAL EXTENSION AND RETRACTION
SKILL TASK
CODE CODE
AF
AF
AF
AF
DET
DET
VCK
SDI
SPECIAL DETAILED INSPECTION OF MLG AND NLG DOOR HINGE
BEARINGS, ATTACHMENT LUG BUSHINGS AND PINS AND DOOR
ACTUATING CYLINDERS ATTACHMENT LUG BUSHINGS AND PINS.
ACCESS PANELS: 713, 714, 734, 744
NORMAL EXTENSION AND RETRACTION
AF
FNC
FUNCTIONAL CHECK OF LGCIU POWER SUPPLY RELAYS.
323000-19-1
323100-01-1
711
731
741
210
NORMAL EXTENSION AND RETRACTION
AF
GVI
GENERAL VISUAL INSPECTION OF L/G EXTENSION /
RETRACTION SYSTEM COMPONENTS
ACCESS PANELS: 713, 714, 734, 744
NORMAL EXTENSION AND RETRACTION
BITE CHECK OF LANDING GEAR CONTROL INTERFACE UNIT
(LGCIU) USING MCDU (TO ENSURE THAT CONTINUOUS BITE IS
OPERATIVE)
EL
OPC
INTERVALS
SOURCE
TPS
REFERENCES
T:
6 YE
I:
6 YE
MRB CPCP
322100-200-009
T:
6 YE
I:
6 YE
MRB CPCP
I:
750 FH
OR
4 MO
I:
120 MO
OR
20000 FC
MRB 8
323000-200-002
MRB 5,8
SOURCE:
MRB 32.30.00/01
528100-220-002
I:
4000 FH
OR
26 MO
I:
750 FH
OR
6 MO
MRB 8
LUR
I:
750 FH
OR
6 MO
MRB 9
LUR
MEN
TASKM. APPLICABI
H.
LITY
1
0.73
ALL
1
0.33
ALL
1
1
1
0.02
0.02
0.02
ALL
1
1
1
0.50
0.50
0.50
ALL
1
0.18
1
1
1
0.80
0.80
0.80
0649 1560
1767 1863
1890 2151
2163
ALL
1
0.10
SOURCE:
MRB 322145-01-1
322100-200-015
SOURCE:
MRB 322151-01-1
SOURCE:
MRB 32.30.00/16
MRB 32.30.00/18
MRB 6
LUR
323100-720-008
SOURCE:
MRB 32.30.00/17
323100-210-002
SOURCE:
MRB 32.30.00/19
326900-740-001
ALL
SOURCE:
MRB 32.30.00/02
Sub 2 - Page 60 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
323100-02-1
323100-03-1
ZONE
711
731
741
210
DESCRIPTION
NORMAL EXTENSION AND RETRACTION
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF GEAR UPLOCK AND DOOR UPLOCK
UNITS AND ROLLERS.
ACCESS PANELS: 713, 714, 734, 744
NORMAL EXTENSION AND RETRACTION
AF
OPC
OPERATIONAL CHECK OF RETRACTION INHIBITION BAULK
323100-04-1
210
NORMAL EXTENSION AND RETRACTION
AF
OPC
OPERATIONAL CHECK TO ENSURE SAFETY VALVE CLOSES AT
260 KTS
323100-05-1
120
PREPARATION: APU RUNNING;
NORMAL EXTENSION AND RETRACTION
AF
DET
DETAILED INSPECTION OF NOSE GEAR DOOR OPERATING
MECHANISM
323100-06-1
323100-07-1
210
ACCESS PANELS: 713, 714
NORMAL EXTENSION AND RETRACTION
210
BITE CHECK USING MCDU TO ENSURE "GEAR NOT DOWN FOR
LANDING" WARNINGS OPERATIVE
NORMAL EXTENSION AND RETRACTION
AF
OPC
EL
OPC
AF
VCK
INTERVALS
SOURCE
I:
3500 FC
OR
24 MO
MRB 5,8
I:
18000 FC
OR
144 MO
I:
15000 FH
OR
72 MO
MRB 9
MRB 8
I:
5000 FC
OR
24 MO
MRB 5
I:
7500 FH
OR
50 MO
I:
15000 FH
MRB 9
LUR
T:
800 FC
I:
8 DY
AOT
EASA AD
FAA AD
ISB
TPS
REFERENCES
323100-200-001
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
0.60
0.60
0.60
ALL
323100-710-001
2
0.10
ALL
SOURCE:
MRB 32.30.00/11
323100-710-005
2
0.40
ALL
1
0.30
ALL
1
0.10
ALL
2
0.10
1
0.75
0649 1130
1200 1488
1560 1578
1657 1767
1130 1200
1379 1578
1657 1767
1851 1876
1890 2163
SOURCE:
MRB 32.30.00/07
SOURCE:
MRB 32.30.00/12
323000-200-001
SOURCE:
MRB 32.30.00/06
ISB
326100-710-001
SOURCE:
MRB 32.30.00/05
323100-710-008
ISB 32-1225
OPERATIONAL CHECK TO ENSURE SAFETY VALVE CLOSURE
323105-03-1
210
NORMAL EXTENSION AND RETRACTION
CHECK CFDS (PFR) FOR SLOW DOOR OPENING/CLOSING MESSAGES
JIC A320-32-51-01
AOT 32A1390
AOT A32N001-13
EASA AD 2013-0288
FAA AD 2013-16-09
ISB 32-1390
Sub 2 - Page 61 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
323112-01-1
ZONE
711
DESCRIPTION
SELECTOR VALVE - LG
SKILL TASK
CODE CODE
323300-01-1
100
200
SOURCE
323300-01-2
100
200
323300-03-1
700
JIC A320-32-31-00
EASA AD
2007-0065
ISB 32-1290
1
0.50
1200 1379
1578 1761
1851 1890
2151 2163
AF
DET
I:
72 MO
MRB 8
323300-200-002
1
1
0.50
0.50
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
4
0.60
ALL
1
0.05
ALL
4
0.40
ALL
SOURCE:
MRB 32.30.00/09
AF
DET
I:
72 MO
MRB 8
ACCESS PANELS: 713, 714
LANDING GEAR FREE FALL EXTENSION
AF
FNC
I:
15000 FC
OR
80 MO
MRB 8
AF
FNC
I:
72 MO
MRB 8
210
ACCESS PANELS: 131AC, 241EF, 242FF, 242LF, 713, 714, 734, 744, 822, 825
LANDING GEAR FREE FALL EXTENSION
OPERATIONAL CHECK OF FREE-FALL MECHANICAL CONTROL
323300-720-003
SOURCE:
MRB 32.11.00/17
MRB 32.21.00/08
MRB 32.30.00/13
CHECK OF FREE-FALL MECHANISM CABLE TENSION
323300-05-1
323300-200-002
SOURCE:
MRB 32.30.00/09
PREPARATION: AIRCRAFT JACKING;
100
TASKM. APPLICABI
H.
LITY
EASA AD
ISB
FUNCTIONAL CHECK OF FREE-FALL SYSTEM
323300-04-1
MEN
T:
REFER TO
ISB / AD
I:
20000 FC
OR
89 MO
DETAILED INSPECTION OF FREE-FALL MECHANISM INCLUDING
CABLES
ACCESS PANELS: 131MC, 131NC, 132PW, 241EF, 241FF, 241KF, 241LF, 241MF,
242FF, 242KF, 242LF, 242MF, 713, 714, 734, 744, 822, 824, 825, 241EF, 241FF,
241KF, 241LF, 241MF, 242FF, 242KF, 242LF, 242MF
LANDING GEAR FREE FALL EXTENSION
REFERENCES
VCK
DETAILED INSPECTION OF FREE-FALL MECHANISM INCLUDING
CABLES
ACCESS PANELS: 131AC, 131BC, 131CC, 132PW, 241EF, 241FF, 241KF, 241LF,
241MF, 242FF, 242KF, 242LF, 242MF, 713, 714, 734, 744, 822, 824, 825, 211FF,
211JF
LANDING GEAR FREE FALL EXTENSION
TPS
AF
INSPECTION OF SELECTOR VALVES.
NOTE: APPLICABILITY IAW SB 32-1290 / AD 2007-0065. AIRCRAFT MSN 2389,
2392, 2393, 2396, 2398, 2403, 2405, 2407, 2409, 2410, 2411, FROM 2413 TO 2439,
2441, AND MSN ABOVE 2441 ON WHICH NO REPLACEMENT OF
THE LANDING GEAR (LG) SELECTOR VALVE 40GA OR OF THE LG DOOR
SELECTOR VALVE 41GA HAS BEEN PERFORMED SINCE AIRCRAFT DELIVERY
FROM AIRBUS ARE COMPLIANT WITH THE REQUIREMENTS OF AD. AIRCRAFT
ON WHICH LG SELECTOR VALVE 40GA AND LG DOOR SELECTOR VALVE 41GA
HAVE THE DUPLICATE INSPECTION "DI" OR DI-BE RECORDED ON THEIR
AMENDMENT PLATES ARE COMPLIANT WITH THE
REQUIREMENTS OF AD.
LANDING GEAR FREE FALL EXTENSION
INTERVALS
323300-200-001
SOURCE:
MRB 32.30.00/15
AF
OPC
I:
24 MO
MRB 8
323300-710-001
SOURCE:
MRB 32.30.00/08
ACCESS PANELS: 713, 714, 734, 744
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
324000-14-1
324000-17-1
ZONE
210
730
744
190
DESCRIPTION
WHEELS AND BRAKES
SKILL TASK
CODE CODE
AF
FNC
FUNCTIONAL CHECK OF THE AUTOMATIC REACTIVATION OF THE
NORMAL BRAKING MODE (PARKING BRAKE APPLIED)
PREPARATION: HYDRAULIC GROUND POWER;
WHEELS AND BRAKES
AF
FNC
FUNCTIONAL CHECK OF BRAKE ACCUMULATOR SYSTEM.
324100-01-1
700
WHEELS
AF
FNC
INTERVALS
SOURCE
I:
5000 FC
OR
48 MO
MRB 8
I:
5000 FC
OR
7500 FH
OR
50 MO
I:
3 DY
MRB 9
LUR
324200-03-1
700
731
741
WHEELS
CHECK CORRECT OPERATION OF WHEEL MOUNTED TIRE
PRESSURE INDICATORS
LANDING GEAR WHEELS AND BRAKES
AF
OPC
731
741
PREPARATION: MLG FIXED LEG FAIRING;
MAIN LANDING GEAR BRAKES
324300-01-1
210
324300-02-1
210
NOTE: TASK MAY BE ACCOMPLISHED AT BRAKE CHANGE.
ALTERNATE BRAKING SYSTEM
122
LOW PRESSURE BRAKE RESERVOIR
1
0.40
SOURCE:
MRB 32.40.00/11
JIC A320-32-42-00
ISB 32-1282
1761 1851
1863 1876
1890
1
1
3.00
3.00
ALL
1
1
0.02
0.02
ALL
324300-710-001
1
0.20
ALL
SOURCE:
CMR 324000-00001-1-C
MRB 32.40.00/08
324200-710-003
1
0.10
ALL
SOURCE:
MRB 32.40.00/09
324311-210-001
1
0.02
ALL
MRB 6
I:
6000 FH
OR
40 MO
CMR*
MRB 9
LUR
I:
10000 FC
MRB 9
CHECK FLUID LEVEL OF LOW PRESSURE BRAKE RESERVOIR
AF
FNC
I:
1500 FC
OR
18 MO
ALL
MRB 9
324227-210-003
SOURCE:
MRB 32.40.00/02
OPERATIONAL CHECK OF ANTISKID INHIBITION
324311-01-1
0.50
SOURCE:
MRB 32.40.00/01
324100-210-004
I:
36 HR
NOTE
OPC
1
ALL
FNC
AF
ALL
0.10
AF
OPERATIONAL CHECK OF ALTERNATE BRAKING SYSTEM
1.50
1.50
1.50
1
ISB
OPC
2
2
2
324100-210-003
T:
7500 FC
I:
2000 FC
NOTE : DEPENDING ON OPERATORS EXPERIENCE, A HIGHER INITIAL INTERVAL
MAY BE USED.
ALTERNATE BRAKING SYSTEM
AF
324400-720-002
TASKM. APPLICABI
H.
LITY
MRB 6,9
DET
FUNCTIONAL CHECK OF BRAKE HEAT PACK FOR WEAR BY USE OF THE WEAR
INDICATOR (PARKING BRAKE APPLIED)
324200-720-004
MEN
SOURCE:
MRB 32.40.00/17
AF
DETAILED INSPECTION OF THE NORMAL BRAKE MANIFOLD
324227-01-1
I:
4 MO
REFERENCES
SOURCE:
MRB 32.40.00/14
CHECK TIRE PRESSURE
D 324100-03-1
TPS
MRB 6
LUR
SOURCE:
MRB 32.40.00/06
ACCESS PANELS: 811
Sub 2 - Page 63 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
324314-01-1
ZONE
148
DESCRIPTION
ALTERNATE BRAKE DIST. - DUAL VALVE
SKILL TASK
CODE CODE
AF
RST
INTERVALS
I:
13 MO
SOURCE
MRB 6
DRAIN ACCUMULATED WATER FROM THE BRAKE DUAL DISTRIBUTION VALVE
(BDDV)
324411-01-1
148
ACCESS PANELS: 148FB, 734, 744
BRAKE ACCUMULATOR
148
ACCESS PANELS: 744
PARKING/ULTIMATE EMERGENCY BRAKING
SYSTEM
AF
FNC
AF
OPC
OPERATIONAL CHECK OF THE PARKING BRAKE SYSTEM
324500-03-2
324500-04-1
324900-01-1
190
190
210
PARKING/ULTIMATE EMERGENCY BRAKING
SYSTEM
FUNCTIONAL CHECK OF BRAKE ACCUMULATOR SYSTEM
PARKING/ULTIMATE EMERGENCY BRAKING
SYSTEM
INSPECTION OF THE ACCUMULATOR OF THE ALTERNATE
BRAKING SYSTEM FOR PRESSURE DECREASE.
TIRE PRESSURE INDICATING SYSTEM
AF
FNC
331400-01-1
ALL
1
0.02
ALL
1
0.20
ALL
1
0.50
1
2.00
1130 1200
1379 1578
1657 1767
2151 2163
ALL
324900-720-001
1
0.12
1200 1379
SOURCE:
MRB 32.40.00/03
JIC A320-32-51-01
1
0.3
ALL
331400-710-001
1
0.10
ALL
SOURCE:
MRB 23.13.00/02
MRB 27.90.00/01
MRB 31.50.00/07
MRB 33.14.00/01
MRB 34.48.00/03
335100-710-001
1
0.12
ALL
MRB 9
LUR
324500-710-001
SIL 32-091
I:
60000 FH
CMR*
SOURCE:
MRB 32.40.00/13
324400-720-002
AF
FNC
I:
750 FC
OR
9 MO
I:
4 MO
MRB 9
LUR
I:
750 FH
OR
6 MO
MRB 9
LUR
I:
8 DY
MRB 8
AF
DET
210
DETAILED INSPECTION OF NLG UPPER ELECTRICAL HARNESS CONNECTORS
FOR SIGNS OF CORROSION AND DETERIORATION
ANNUNCIATOR LIGHT TEST AND DIMMING
EL
OPC
OPERATIONAL CHECK OF EMERGENCY LIGHTS
0.20
I:
2000 FC
OR
24 MO
ISB
NLG UPPER ELECTRICAL HARNESS CONNECTORS
CABIN EMERGENCY LIGHTING
TASKM. APPLICABI
H.
LITY
EL
OPC
324411-200-001
SOURCE:
CMP 32-2-0000-001
MRB 32.40.00/05
I:
7500 FH
OR
5000 FC
711
210
MEN
1
CMP
MRB 6,9
FNC
OPERATIONAL CHECK OF LIGHTS TEST SYSTEM
335100-01-1
324314-200-002
I:
750 FH
OR
4 MO
AF
CROSSCHECK OF TPIS READING AND TIRE PRESSURE GAUGE
325101-01-1-SDM
REFERENCES
SOURCE:
MRB 32.40.00/12
FUNCTIONAL CHECK OF PARKING/EMERGENCY BRAKE
ACCUMULATOR BY READING THE CHARGE PRESSURE ON THE
ACCUMULATOR GAUGE
324500-01-1
TPS
SPECI
SOURCE:
CMR 324000-00002-1-C
JIC A320-32-45-00
ISB 32-1279
SOURCE:
MRB 33.51.00/01
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SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
335100-01-1-SDM
335100-02-1
ZONE
DESCRIPTION
SKILL TASK
CODE CODE
SOURCE
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
200
LHT EMERGENCY ESCAPE PATH. CABIN EMERGENCY LIGHTING
AF
GVI
I:
3 MO
S-ICA
1
0.20
1200 1379
2151 2163
220
VISUAL INSPECTION OF PHOTOLUMINESCENT FLOOR PATH MARKING FOR
CRACKS AND PROPER INSTALLATION
CABIN EMERGENCY LIGHTING
JIC A320-33-51-00
STC 10014013
ICA A320-EB33-0300
EL
OPC
I:
750 FH
OR
6 MO
I:
400 DY
MRB 9
LUR
335100-710-002
1
0.05
1130 1578
1
0.10
ALL
1
0.30
1130 1578
1
0.05
ALL
1
0.70
ALL
0649 1130
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
0649 1130
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
OPERATIONAL CHECK OF EMERGENCY ESCAPE PATH MARKING LIGHTS
335100-03-1
INTERVALS
220
CABIN EMERGENCY LIGHTING
EL
OPC
MRB 9
SOURCE:
MRB 33.51.00/02
335100-710-003
SIL 33-033
CHECK BATTERY CAPACITY
335100-04-1
200
CABIN EMERGENCY LIGHTING
EL
RST
I:
18 MO
MRB 9
REMOVE POWER SUPPLY UNITS OF EMERGENCY ESCAPE PATH MARKING
LIGHTS AND RESTORE BATTERIES TO REQUIRED STANDARD BY CAPACITY
CHECK
335100-05-1
335100-06-1
R 336000-01-1-SDM
200
NOTE:
P/N 5822-21 VENDOR: LOCTITE LUMINESCENT SYSTEM
CABIN EMERGENCY LIGHTING
220
CHECK MANUAL OPERATION FROM BOTH CONTROL PANELS AND
CHECK ALL CABIN LIGHTS AND SIGNS ILLUMINATED BY
BATTERIES
CABIN EMERGENCY LIGHTING
200
CHECK OF DOOR SWITCH POWER SUPPLIED BY EMERGENCY
LIGHTS SYSTEM AND CHECK DOOR SWITCH OPERATION TO
ACTIVATE THE EXTERIOR LIGHTS
SAFTGLO. DAILY SYSTEM CHARGING.
SOURCE:
MRB 33.51.00/04
EL
EL
OPC
OPC
I:
15000 FH
OR
100 MO
MRB 9
LUR
I:
24000 FH
MRB 9
200
SAFTGLO. INSPECTION AND SERVICING-CLEANING.
INSPECTION OF FLOOR MOUNTED COMPONENTS:
TOP COVER/CASING, BOTTOM TRACK,PHOTOLUMINESCENT ELEMENTS, EXIT
INDICATORS (ARROWS, ETC.) AT MID-CABIN EXITS, END INDICATORS (DOT
MARKERS), END CAPS OR RAMPS. CLEANING OF TOP COVER AND
PHOTOLUMINESCENT INSERT.
335100-710-004
SOURCE:
MRB 33.51.00/05
335100-720-001
SOURCE:
MRB 33.51.00/06
AF
SVC
I:
DY
S-ICA
JIC A320-33-60-00
STC ST02292AT
ICA L67-10
1
TBD
AF
SVC
I:
7500 FH
OR
24 MO
S-ICA
JIC A320-33-60-01
STC ST02292AT
ICA L67-10
1
TBD
PERFORM INITIAL DAILY CHARGE PER APPROVED PROCEDURES BY
ACTIVATING CABIN LIGHTING.
R 336000-02-1-SDM
SOURCE:
MRB 33.51.00/03
335139-920-001
CMM 33-51-02
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SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
TASK
E
NUMBER
V
R 336000-03-1-SDM
ZONE
200
DESCRIPTION
SAFTGLO. FUNCTIONAL CHECK.
SKILL TASK
CODE CODE
200
SAFTGLO. GENERAL VISUAL INSPECTION
SOURCE
200
SAFTGLO. 10 YEAR INSPECTION AND FUNCTIONAL CHECK.
341300-02-1
210
AIR DATA
210
OPERATIONAL CHECK OF OVERSPEED WARNING VMO/MMO
USING CFDS.
AIR DATA
341300-04-1
210
AIR DATA
210
OPERATIONAL CHECK OF OVERSPEED WARNINGS VFE/VLE
USING CFDS.
AIR DATA
JIC A320-33-60-02
STC ST02292AT
ICA L67-10
1
TBD
AF
GVI
I:
90 DY
S-ICA
JIC A320-33-60-03
STC ST02292AT
ICA L67-10
1
TBD
AF
FNC
I:
10 YE
S-ICA
JIC A320-33-60-04
STC ST02292AT
ICA L67-10
1
TBD
RA
OPC
I:
15000 FH
OR
100 MO
I:
15000 FH
OR
100 MO
I:
15000 FH
OR
100 MO
I:
7500 FH
OR
50 MO
I:
12000 FH
OR
80 MO
MRB 9
LUR
341300-710-002
1
0.20
0649 1130
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
0649 1130
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
0649 1130
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
ALL
SOURCE:
MRB 34.13.00/01
341300-710-001
1
0.10
ALL
SOURCE:
MRB 34.13.00/02
341300-710-007
1
0.20
ALL
SOURCE:
MRB 34.13.00/01
341300-710-003
1
0.10
ALL
SOURCE:
MRB 34.13.00/04
341000-710-009
1
0.20
ALL
RA
OPC
RA
RA
OPC
OPC
OPERATIONAL CHECK OF ALTITUDE COMPARISON WARNING
341300-05-1
210
AIR DATA
OPERATIONAL CHECK OF THE 5-MINUTE TIME DELAY OF ADIRU
2 AND 3 POWER DISCONNECTION IN EMERGENCY
CONFIGURATION
TASKM. APPLICABI
H.
LITY
S-ICA
OPERATIONAL CHECK OF AIR DATA SWITCHING FUNCTION
341300-03-1
MEN
I:
7500FH
OR
24 MO
INSPECTION AND FUNCTIONAL CHECK TEST COUPON (FWD RH CABIN).
341300-01-1
REFERENCES
FNC
GVI OF FLOOR MOUNTED COMPONENTS AND INTERIOR LIGHTING
R 336000-05-1-SDM
TPS
AF
INSPECTION INTERIOR LIGHTING: OVERALL CEILING LIGHTING, INOPERATIVE
CEILING LAMPS AT LIFE RAFT AREA, MISSING ELECTRICALLY ILLUMINATED
EXIT MARKER.
R 336000-04-1-SDM
INTERVALS
AV
OPC
MRB 9
LUR
MRB 9
LUR
MRB 9
LUR
MRB 9
LUR
SOURCE:
MRB 34.14.00/03
Sub 2 - Page 66 of 305
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SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
341300-07-1
ZONE
120
DESCRIPTION
AIR DATA
SKILL TASK
CODE CODE
AV
RST
341300-11-1
120
341400-01-1
210
RA
342100-01-1
210
ATTITUDE, HEADING AND POSITION
120
OPERATIONAL CHECK OF ATTITUDE AND HEADING COMPARISON
WARNING
STANDBY ALTITUDE AND AIRSPEED
RA
RA
I:
750 FH
OR
4 MO
SIL
OPC
I:
7500 FH
OR
50 MO
I:
7500 FH
OR
50 MO
I:
12000 FH
OR
80 MO
MRB 9
LUR
MRB 6
LUR
SOURCE:
MRB 34.14.00/02
342100-790-001
SIL 34-084
I:
6000 FH
OR
20 MO
NOTE
MRB 6
SIL
SOURCE:
MRB 34.21.00/01
341000-170-003
SIL 34-084
I:
6000 FH
OR
48 MO
MRB 9
LUR
OPC
FNC
LOW RANGE LEAK TEST OF STANDBY PNEUMATIC CIRCUITS
342100-02-1
120
ACCESS PANELS: 811
STANDBY ALTITUDE AND AIRSPEED
RA
SVC
DRAINING AND FLUSHING OF STANDBY PNEUMATIC CIRCUITS
NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY
BE USED.
342200-01-1
210
ACCESS PANELS: 811, 812
STANDBY COMPASS
OPERATIONAL CHECK OF THE STANDBY COMPASS INCLUDING LIGHT TEST
AND VISUAL CHECK
RA
REFERENCES
RST
OPERATIONAL CHECK OF ATT/HDG SWITCHING FUNCTION
341400-02-1
TPS
MRB 6
SIL
CLEANING OF 1 OUT OF 3 PITOT PROBES.
NOTE: TASK TO BE PERFORMED ALTERNATELY ON PITOT 1, 2
AND 3.
ATTITUDE, HEADING AND POSITION
SOURCE
I:
6000 FH
OR
20 MO
NOTE
FLUSHING OF TOTAL PRESSURE LINES
NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY
BE USED.
AIR DATA
AV
INTERVALS
OPC
341000-170-001
SIL 34-084
MEN
TASKM. APPLICABI
H.
LITY
1
0.20
ALL
341000-170-004
SIL 34-084
1
0.58
ALL
341400-710-003
1
0.10
ALL
SOURCE:
MRB 34.14.00/01
341400-710-004
1
0.20
ALL
2
0.20
ALL
1
0.75
ALL
1
0.10
ALL
SOURCE:
MRB 34.13.00/06
MRB 9
LUR
SOURCE:
MRB 34.21.00/02
342200-710-001
SOURCE:
MRB 34.22.00/01
NOTE: THIS NOTE FOR SDM BASE ONLY: AMTOSS REF 342200-710-001-A01 IS
NOT REQUIRED TO BE PERFORMED. ONLY -A
Sub 2 - Page 67 of 305
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SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
344100-02-1
ZONE
120
DESCRIPTION
WEATHER RADAR SYSTEM
SKILL TASK
CODE CODE
152
SOURCE
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
RA
RST
I:
72 MO
OR
30000 FH
NOTE
SIL
344100-100-801
SIL 34-102
1
0.42
NOTE: DEPENDING ON OPERATING ENVIRONMENT AND THE OPERATOR'S
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY
BE USED.
RADIO ALTIMETER
RA
DET
I:
4000 FH
OR
48 MO
NOTE
MRB 9
LUR
344200-750-001
1
0.20
1130 1200
1379 1488
1560 1578
1743 1761
1767 1851
1863 1876
1890 2151
2163
ALL
REMOVE WEATHER RADAR TRANSCEIVER MOUNTING TRAY FILTER FOR
CLEANING
344200-01-1
INTERVALS
OPERATIONAL CHECK AND DETAILED INSPECTION FOR CONTAMINATION OF
RADIO ALTIMETER FAN
SOURCE:
MRB 34.42.00/01
NOTE: DEPENDING ON OPERATING ENVIRONMENTAND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY
BE USED.
344200-03-1
150
ACCESS PANELS: 152GW
RADIO ALTIMETER
RA
RST
I:
6 MO
SIL
344211-615-001
SIL 34-099
1
0.40
ALL
344800-01-1
210
RADIO ALTIMETER ANTENNAS EXTERNAL SURFACE CLEANING
GROUND PROXIMITY WARNING SYSTEM
RA
OPC
I:
7500 FH
OR
50 MO
MRB 9
LUR
344800-710-001
CMM 34-45-30
CMM 34-45-36
1
0.20
ALL
345200-720-006
1
0.10
ALL
MRB 8
SOURCE:
MRB 34.52.00/02
351241-710-001
1
0.10
ALL
MRB 8
SOURCE:
MRB 35.10.00/01
351241-100-001
1
0.10
ALL
MRB 8
SOURCE:
MRB 35.10.00/07
351000-720-001
1
0.12
ALL
OPERATIONAL CHECK OF GROUND SELF TEST SYSTEM
345200-02-1
210
MSN 1130, 1200, 1379, 1488, 1560, 1578, 1657, 1743, 1761, 1767, 1851, 1863, 1876,
1890: P/N 965-0976-003-206-206, VENDOR: HONEYWELL
MSN 0649: P/N 965-0676-020, VENDOR: SUNDSTRAND
ATC SYSTEM
SOURCE:
MRB 34.48.00/01
RA
FNC
FUNCTIONAL CHECK OF ATC ANTENNAS
351000-01-1
210
CREW OXYGEN SYSTEM
AF
OPC
I:
15000 FH
OR
100 MO
I:
24 MO
MRB 9
LUR
OPERATIONAL CHECK OF FLIGHT CREW OXYGEN SYSTEM
351000-07-1
210
CREW OXYGEN MASKS
AF
RST
I:
24 MO
CLEANING OF OXYGEN MASKS
351000-08-1
210
CREW OXYGEN
FUNCTIONAL CHECK OF ECAM OXYGEN CYLINDER CONTENTS
INDICATION COMPARED WITH CYLINDER PRESSURE GAUGE
AF
FNC
I:
24 MO
OR
6500 FH
SOURCE:
MRB 35.10.00/08
Sub 2 - Page 68 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
351241-01-1
351351-01-1
352000-01-1
ZONE
DESCRIPTION
210
CREW OXYGEN MASKS
210
DETAILED INSPECTION OF OXYGEN MASKS (OUT OF BOX)
WITH HARNESS INFLATED
OXYGEN SUPPLY VALVE
200
OPERATIONAL CHECK OF LP SOLENOID VALVE CONTROL
(CLOSING MODE) AND LP INDICATION
PASSENGER OXYGEN (CHEMICAL)
SKILL TASK
CODE CODE
AF
EL
AF
DET
OPC
OPC
OPERATIONAL CHECK OF MANUAL MASK RELEASE
352000-02-1
200
PASSENGER OXYGEN (CHEMICAL)
AF
FNC
FUNCTIONAL CHECK OF AUTOMATIC MASK RELEASE, DETAILED INSPECTION
OF MASKS AND VISUAL CHECK OF CHEMICAL OXYGEN GENERATORS
INTERVALS
I:
24 MO
I:
24 MO
SOURCE
0.25
ALL
MRB 9
SOURCE:
MRB 35.10.00/03
351200-710-001
1
0.10
ALL
SOURCE:
MRB 35.10.00/02
352300-710-001
1
0.10
ALL
SOURCE:
CMR 352000-00001-1-C
MRB 35.20.00/01
352300-720-003
1
1.40
ALL
1
12.00
ALL
353242-210-002
1
0.17
ALL
SOURCE:
MRB 35.30.00/01
353242-210-001
1
0.20
ALL
1
0.20
ALL
MRB 9
SOURCE:
MRB 35.30.00/04
353000-220-001
1
0.20
ALL
SPECI
SOURCE:
MRB 35.30.00/06
JIC A320-35-30-01
1
0.20
ALL
I:
8500 FH
OR
80 MO
CMR**
MRB 8
LUR
I:
72 MO
OR
24000 FH
CMR**
MRB 9
AF
RST
I:
24 MO
SPECI
353000-01-1
200
CLEAN CABIN OXYGEN MASKS
PORTABLE OXYGEN CYLINDERS
AF
VCK
I:
4 MO
MRB 9
CHECK PRESSURE ON CYLINDER PRESSURE GAUGES
AF
VCK
VISUAL CHECK OF CYLINDER ATTACHMENTS
353000-05-1
200
PROTECT. BREATHING EQPT (CKPT & CABIN)
AF
VCK
I:
24000 FH
OR
160 MO
I:
100 DY
MRB 9
LUR
MRB 8
VISUAL CHECK OF THE TAMPER SEAL/SERVICEABILITY INDICATION OF THE
PROTECTIVE BREATHING EQUIPMENT
353000-07-1
200
PORTABLE OXYGEN
AF
DET
I:
24 MO
DETAILED INSPECTION OF PORTABLE OXYGEN MASK
353000-07-1-SDM
200
PORTABLE OXYGEN MASKS
CA
DET
I:
4 MO
TASKM. APPLICABI
H.
LITY
1
CABIN OXYGEN MASKS
PORTABLE OXYGEN
MEN
351241-200-001
200
200
REFERENCES
MRB 9
352143-01-1-SDM
353000-04-1
TPS
SOURCE:
CMR 352000-00002-1-C
MRB 35.20.00/02
352143-100-001
JIC A320-35-21-01
SOURCE:
MRB 35.30.00/03
353000-210-006
JIC A320-35-30-00
CHECK PORTABLE OXYGEN MASKS FOR EXPIRATION DATE
NOTE: REPLACE OXYGEN MASK OR OPEN DEFERRED ITEM IF IT EXPIRES IN
LESS THAN 5 MO
Sub 2 - Page 69 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
361100-01-1
ZONE
450
460
DESCRIPTION
ENGINE BLEED AIR SUPPLY SYSTEM
SKILL TASK
CODE CODE
AF
FNC
FUNCTIONAL CHECK OF OVERPRESSURE VALVE.
INTERVALS
SOURCE
I:
5 YE
OR
22000 FH
MRB 9
I:
12000 FH
OR
48 MO
NOTE
MRB 6
SIL
TPS
REFERENCES
361153-720-001
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.10
0.10
ALL
4
4
4.00
4.00
0649 1130
1578 1657
1767
SOURCE:
MRB 36.00.00/05
ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR
361100-05-1
191
192
ENGINE BLEED AIR SUPPLY SYSTEM
AF
DIS
REMOVE AND REPLACE COMBO SEALS ON PACK INLET INCL. ON SLEEVES
DOWNSTREAM AND UPSTREAM OF FLOW CONTROL VALVE
361241-920-001
SIL 21-039
SIL 36-047
SOURCE:
MRB 36.00.00/12
NOTE:
DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A
LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED.
TASK MAY BE COMBINED WITH TASK 215200-07-1.
ACCESS PANELS: 191BB, 192BB
361100-06-1
361100-07-1
361100-08-1
R 361100-09-1
410
420
190
520
620
450
460
450
460
ENGINE BLEED AIR SUPPLY SYSTEM
AF
CHK
I:
40 MO
SIL
361100-790-002
SIL 36-047
2
2
0.10
0.10
ALL
PERFORM LEAK CHECK ON THE COMBO SEALS ON THE
PYLON DUCT SLEEVES (DOWNSTREAM PRECOOLER)
NOTE : DEPENDING ON OPERATING ENVIRONMENT AND
OPERATOR´S EXPERIENCE,A LESS OR A MORE
FREQUENT INITIAL INTERVAL MAY BE USED
ENGINE BLEED AIR SUPPLY SYSTEM
AF
CHK
I:
40 MO
SIL
361148-790-002
SIL 36-047
1
1
1
1.00
1.00
1.00
0649 1130
ACCESS PANELS: 191BT, 192BT, 521AB, 521AT, 621AB, 621AT
ENGINE BLEED AIR SUPPLY SYSTEM
AF
DET
VSB
LUR
361149-200-004
VSB RA32036-13
1
1
0.10
0.10
DETAILLED INSPECTION OF HIGH PRESSURE BLEED AIR
DUCT BEND RADIUS.
ENGINE BLEED AIR SUPPLY SYSTEM
AF
DET
I:
1800 FC
OR
24 MO
I:
750 FC
OR
9 MO
ISB
LUR
JIC A320-36-11-00
ISB 36-1041
1
1
1.00
1.00
1130 1200
1379 1578
1657 1761
2151 2163
1488 1767
1851 1876
1890
PERFORM LEAK CHECK ON
- THE FLEXIBLE SEALS ON THE PYLON TO WING
DUCTING
- THE WING TO FUSELAGE FLEXIBLE ´S-DUCT´
NOTE : DEPENDING ON OPERATING ENVIRONMENT AND
OPERATOR´S EXPERIENCE,A LESS OR A MORE
FREQUENT INITIAL INTERVAL MAY BE USED
DETAILED INSPECTION OF UPPER HIGH PRESSURE BLEED AIR DUCT BEND
RADIUS
Sub 2 - Page 70 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
TASK
E
NUMBER
V
R 361100-10-1
361141-03-1
ZONE
450
460
453
463
DESCRIPTION
SKILL TASK
CODE CODE
413
423
SOURCE
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
ENGINE BLEED AIR SUPPLY SYSTEM
AF
DET
I:
24 MO
ISB
JIC A320-36-11-00
ISB 36-1041
1
1
2.00
2.00
DETAILED INSPECTION OF UPPER HIGH PRESSURE BLEED AIR
DUCT SUPPORT LINK DOUBLER AND ITS ASSOCIATED LINKS
IP BLEED CHECK VALVE
1488 1767
1851 1876
1890
EN
DET
I:
5500 FH
OR
36 MO
MRB 6
LUR
361141-200-001
1
1
0.25
0.25
ALL
I:
6000 FH
OR
40 MO
MRB 6
SIL
LUR
1
1
0.50
0.50
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
I:
6000 FH
OR
40 MO
MRB 6
LUR
1
1
0.50
0.50
0649
I:
22000 FH
OR
144 MO
MRB 6
SIL
LUR
1
1
0.50
0.50
ALL
REMOVE AND CHECK INTERMEDIATE PRESSURE BLEED CHECK VALVE FOR
CONDITION
361143-01-1
INTERVALS
ACCESS PANELS: 437AL, 451AL, 447AL, 461AL
THERMOSTAT - FAN AIR VALVE CONTROL
AF
RST
REMOVE THE THERMOSTAT-FILTER OF THE FAN AIR
VALVE-CONTROL FOR CLEANING.
SOURCE:
MRB 36.00.00/02
361143-100-001
SIL 36-055
SOURCE:
MRB 36.00.00/17
NOTE: - DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS OR A MORE FREQUENT INITIAL INTERVAL MAY BE USED
ACCESS PANELS: 413DL, 423DL
361143-02-1
413
423
THERMOSTAT - FAN AIR VALVE CONTROL
AF
RST
CLEANING OF FAN AIR VALVE TEMPERATURE CONTROL
THERMOSTAT (TCT) FILTER
361143-100-002
SOURCE:
MRB 36.00.00/17
NOTE: - DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS OR A MORE FREQUENT INITIAL INTERVAL MAY BE USED
ACCESS PANELS: 413DL, 423DL
361148-01-1
500
600
AIR BLEED DUCTS,WING
PERFORM LEAK CHECK ON BLEED AIR DUCTING IN WING AREA BETWEEN
BLEED AIR PRECOOLER, WING ANTI ICE VALVE AND WING/FUSELAGE
CONNECTION
EN
FNC
361148-790-001
SIL 36-047
SOURCE:
MRB 36.00.00/10
NOTE:
- TASK MAY BE COMBINED WITH TASKS 361200-02-1(A319) OR 361200-022(A320) OR 361200-02-3 (A321) OR 361200-02-4(A318) AND 361200-03-1
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATOR´S
EXPERIENCE,A LESS OR A MORE FREQUENT INITIAL INTERVAL MAY BE USED
ACCESS PANELS: 521AB, 521CB, 521EB, 621AB, 621CB, 621EB
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
361200-01-1
ZONE
210
DESCRIPTION
AIR BLEED AIR SUPPLY & CROSSBLEED SYST
SKILL TASK
CODE CODE
AF
OPC
INTERVALS
I:
50 MO
SOURCE
MRB 9
OPERATIONAL CHECK OF CROSSBLEED VALVE IN MANUAL MODE
361200-02-1
361200-02-2
150
160
190
310
147
148
151
161
198
312
314
315
APU BLEED AIR SUPPLY & CROSSBLEED SYST
EN
FNC
PERFORM LEAK CHECK ON APU BLEED AIR DUCTING (UPSTREAM THE APU
BLEED CHECK VALVE)
NOTE :
- TASK MAY BE COMBINED WITH TASKS 361148-01-1 AND 361200-03-1
ACCESS PANELS: 151BW, 151SW, 151TW, 151UW, 151VW, 161AW, 161BW,
161CW, 161DW, 312AR, 314AR
APU BLEED AIR SUPPLY & CROSSBLEED SYST
EN
FNC
PERFORM LEAK CHECK ON APU BLEED AIR DUCTING
(UPSTREAM THE APU BLEED CHECK VALVE)
NOTE :
- TASK MAY BE COMBINED WITH TASKS
361148-01-1 AND 361200-03-1
I:
22000 FH
OR
144 MO
MRB 6
SIL
LUR
I:
22000 FH
OR
144 MO
MRB 6
SIL
LUR
I:
22000 FH
OR
144 MO
MRB 6
SIL
LUR
I:
24000 FH
OR
160 MO
MRB 6,9
LUR
TPS
REFERENCES
361200-710-002
MEN
TASKM. APPLICABI
H.
LITY
1
0.10
ALL
1
1
1
1
0.50
0.50
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
MRB 36.00.00/15
1
1
1
1
1
1
1
1
0.50
0.50
0.50
0.50
0.50
0.50
0.50
0.50
1130 1200
1379 1578
1657 1767
2151 2163
361200-790-003
SIL 36-047
1
1
0.50
0.50
ALL
1
0.50
ALL
SOURCE:
MRB 36.00.00/03
361200-790-002
SIL 36-047
SOURCE:
MRB 36.00.00/15
361200-790-002
SIL 36-047
PREPARATION: ACT(S) REMOVED (IF INSTALLED);
361200-03-1
191
192
ACCESS PANELS: 734, 744, 151CW, 151DW, 151EW, 151HW, 151JW, 161AW,
161BW, 161CW, 312AR, 314AR
APU BLEED AIR SUPPLY & CROSSBLEED SYST
EN
FNC
LEAK CHECK OF BLEED AIR DUCTING IN FUSELAGE AREA
BETWEEN APU BLEED CHECK VALVE, AIR CONDITIONING
PACK AND WING/FUSELAGE CONNECTION
NOTE:
- TASK MAY BE COMBINED WITH TASKS
361148-01-1 AND 361200-02-1(A319) OR 361200-02-2
(A320) OR 361200-02-3(A321) OR 361200-02-4(A318)
- DEPENDING ON OPERATING ENVIRONMENT AND
OPERATOR´S EXPERIENCE,A LESS OR A MORE
FREQUENT INITIAL INTERVAL MAY BE USED
361251-01-1
192
ACCESS PANELS: 191KB, 192KB
APU BLEED CHECK VALVE
REMOVE AND CHECK AUXILIARY POWER UNIT BLEED
CHECK VALVE FOR CONDITION
AF
DET
SOURCE:
MRB 36.00.00/11
361251-200-001
SIL 36-038
SOURCE:
MRB 36.00.00/04
ACCESS PANELS: 197BB
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
381000-01-1
ZONE
171
DESCRIPTION
POTABLE WATER SYSTEM
SKILL TASK
CODE CODE
CA
RST
STERILIZATION OF POTABLE WATER SYSTEM AND DISCARD OF WATER FILTER
ELEMENTS, IF INSTALLED
INTERVALS
SOURCE
I:
100 DY
OR
NR
NOTE
MRB 6,9
I:
100 DY
OR
NR
NOTE
MRB 6,9
I:
15000 FH
OR
100 MO
MRB 9
LUR
I:
6000 FH
OR
24 MO
MRB 9
I:
6000 FH
OR
24 MO
NOTE
MRB 6
SIL
TPS
REFERENCES
381000-670-002
MEN
TASKM. APPLICABI
H.
LITY
2
3.00
0649 1488
1560 1743
1761 1851
1863 1876
1890
2
3.00
1130 1200
1379 1578
1657 1767
2151 2163
1
0.75
1130 1200
1379 1578
1657 1767
2151 2163
2
0.50
ALL
1
0.50
ALL
SOURCE:
MRB 38.10.00/01
NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY
BE USED.
381000-01-2
171
ACCESS PANELS: 133AL, 171AL
POTABLE WATER SYSTEM
CA
RST
STERILIZATION OF POTABLE WATER SYSTEM AND DISCARD OF WATER FILTER
ELEMENTS, IF INSTALLED
381000-670-002
SOURCE:
MRB 38.10.00/01
NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY
BE USED.
381000-02-1
138
ACCESS PANELS: 133AL, 171AL, 192NB
POTABLE WATER SYSTEM
UT
GVI
GENERAL VISUAL INSPECTION OF POTABLE WATER TANK
383100-02-1
170
ACCESS PANELS: 131NW, 131PW, 132PW, 825
VACUUM TOILET SYSTEM
UT
DET
INSPECT WATER SEPARATOR AND ASSOCIATED FILTER
ELEMENT, AND CLEAN AS NECESSARY
383100-05-1
172
ACCESS PANELS: 161DW, 162DW
VACUUM TOILET SYSTEM
DETAILED INSPECTION OF CLEANLINESS INSIDE WASTE TANK
NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY
BE USED.
UT
DET
381141-200-001
SOURCE:
MRB 38.10.00/03
383167-610-001
SIL 38-020
SOURCE:
MRB 38.31.01/03
383161-210-001
SIL 38-020
SOURCE:
MRB 38.31.01/06
ACCESS PANELS: 161DW, 162DW
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
383100-06-1
ZONE
200
DESCRIPTION
VACUUM TOILET SYSTEM
SKILL TASK
CODE CODE
AF
RST
383100-07-1
200
MRB 7
SIL
LUR
RST
I:
7500 FH
OR
48 MO
NOTE
SIL
LUR
RST
I:
1500 FH
OR
24 MO
NOTE
MRB 7
LUR
I:
6500 FH
OR
48 MO
I:
24000 FH
OR
72 MO
SIL
LUR
I:
24000 FH
OR
72 MO
NOTE
MRB 6,9
CORRECTIVE VACUUM WASTE LINE CLEANING.
383200-01-1
200
NOTE:INTERVAL MAY BE ADJUSTED ACCORDING TO
OPERATOR EXPERIENCE.
WASTE WATER DRAIN
UT
CLEAN FILTER ELEMENT OF WASHBASIN DRAIN VALVES
NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY
BE USED.
383200-02-1
200
SINK DRAIN AIR STOP VALVE
UT
RST
CA
DIS
REMOVE FOR CLEANING THE SINK DRAIN AIR STOP VALVE.
384142-01-1
171
AIR FILTER
DISCARD SYSTEM FILTER ELEMENT
NOTE : DEPENDING ON EACH INDIVIDUAL OPERATOR´S
ENVIRONMENT A MORE FREQUENT INTERVAL
MAY BE USED
384142-01-2
137
ACCESS PANELS: 161DW, 826
AIR FILTER
DISCARD SYSTEM FILTER ELEMENT
NOTE : DEPENDING ON EACH INDIVIDUAL OPERATOR´S
ENVIRONMENT A MORE FREQUENT INTERVAL
MAY BE USED
CA
SOURCE
I:
150 FH
OR
2 MO
NOTE
CLEANING OF VACUUM WASTE LINES WITH CHEMICAL CLEANING AGENT AND
CRUSHED ICE
NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY
BE USED.
VACUUM TOILET SYSTEM
AF
INTERVALS
DIS
TPS
REFERENCES
383100-100-018
SIL 38-020
MEN
TASKM. APPLICABI
H.
LITY
1
0.30
ALL
383100-100-004
SIL 38-020
2
10.00
ALL
383200-100-002
SIL 38-029
1
0.10
1
0.30
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
0649
1
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.10
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
MRB 38.31.01/05
SOURCE:
MRB 38.32.00/02
MRB 6,9
383200-100-003
TFU
38.32.00.005
SIL 38-029
384100-610-001
SOURCE:
MRB 38.40.00/01
384100-610-001
SOURCE:
MRB 38.40.00/01
ACCESS PANELS: 131PW, 825
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
384241-01-2
ZONE
172
DESCRIPTION
AIR SUPPLY
SKILL TASK
CODE CODE
CA
DET
DETAILED INSPECTION OF COMPRESSOR INLET FILTER.
NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY
BE USED.
384242-01-3
171
ACCESS PANELS: 162DW, 826
AIR SUPPLY
CA
DIS
DISCARD COMPRESSOR OUTLET FILTER ELEMENT.
D 491200-01-1
315
ACCESS PANELS: 161DW, 826
APU MOUNTS
AF
DET
DETAILED INSPECTION OF APU SUSPENSION RODS, VIBRATION ISOLATOR
STRUCTURE INCLUDING BRACKETS AND VISIBLE PART OF STRUCTURE
ATTACHMENT FITTINGS
D 491200-02-1
315
316
NOTE : TASK MAY BE ACCOMPLISHED AT OPPORTUNITY OF APU CHANGE
APU MOUNTS
AF
GVI
INTERVALS
SOURCE
I:
12000 FH
OR
80 MO
NOTE
MRB 9
LUR
I:
24000 FH
OR
72 MO
MRB 9
I:
80 MO
NOTE
MRB 9
I:
20 MO
MRB 9
315
ACCESS PANELS: 315AL, 316AR
APU MOUNTS
REFERENCES
384200-210-001
MEN
TASKM. APPLICABI
H.
LITY
1
0.05
0649
1
0.10
0649
1
0.30
1
1
0.55
0.55
1
0.30
ALL
1
1
0.55
0.55
ALL
SOURCE:
MRB 38.40.00/03
384200-610-001
SOURCE:
MRB 38.40.00/02
491200-210-001
SOURCE:
MRB 49.12.00/01-36
GENERAL VISUAL INSPECTION OF APU SUSPENSION SYSTEM
FOR CONDITION AND SECURITY.
R 491200-B1-1
TPS
491200-210-002
SOURCE:
MRB 49.12.00/02-36
EN
DET
DETAILED INSPECTION OF APU SUSPENSION RODS, VIBRATION
ISOLATOR STRUCTURE INCLUDING BRACKETS AND VISIBLE
PART OF STRUCTURE ATTACHMENT FITTINGS
I:
80 MO
NOTE
MRB 9
I:
20 MO
MRB 9
491200-210-007
SOURCE:
MRB 49.12.00/02-13
NOTE : TASK MAY BE ACCOMPLISHED AT OPPORTUNITY OF
APU CHANGE
R 491200-B2-1
315
316
ACCESS PANELS: 315AL, 316AR
APU MOUNTS
GENERAL VISUAL INSPECTION OF APU SUSPENSION SYSTEM FOR CONDITION
AND SECURITY.
AF
GVI
491200-210-804
SOURCE:
MRB 49.12.00/01-13
ACCESS PANELS: 315AL, 316AR
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
TASK
E
NUMBER
V
D 491300-01-1
ZONE
310
DESCRIPTION
FIRE SEALS
SKILL TASK
CODE CODE
EN
GVI
INTERVALS
I:
20 MO
SOURCE
MRB 8
GENERAL VISUAL INSPECTION OF ALL APU COMPARTMENT FIRE WALLS AND
SEALS:
- COMPARTMENT DOORS
- FWD AND AFT FIRE WALLS
- SIDE FIRE WALLS
- UPPER FIRE WALL
R 491300-B1-1
310
ACCESS PANELS: 315AL, 316AR
FIRE SEALS
310
ACCESS PANELS: 315AL, 316AR
AIR INTAKE SYSTEM
EN
GVI
I:
20 MO
MRB 8
310
ACCESS PANELS: 314AR, 315AL, 316AR
AIR INTAKE SYSTEM
AF
DET
I:
40 MO
MRB 9
310
ACCESS PANELS: 315AL, 316AR
APU AIR INTAKE SYSTEM
313
315
ACCESS PANELS: 315AL, 316AR
AIR INTAKE SYSTEM
DETAILED INSPECTION OF APU AIR INTAKE,
DIFFUSER ELBOW, SEALS AND FELT METAL
1
1.42
491300-200-003
1
1.42
491600-210-001
1
0.30
AF
RST
I:
2400 FH
EASA AD
ISB
491600-100-001
EASA AD
2006-0153
ISB 49-1068
1
1.50
EN
GVI
I:
600 FH
EASA AD
ISB
491600-210-004
EASA AD
2006-0153
ISB 49-1068
1
0.20
EN
DET
I:
40 MO
MRB 9
491600-200-002
1
1
0.15
0.15
GENERAL VISUAL INSPECTION OF APU AIR INLET PLENUM
AND APU AIR INTAKE.
R 491600-B1-1
TASKM. APPLICABI
H.
LITY
ALL
SOURCE:
MRB 49.16.00/02-36
CLEANING OF APU AIR INTAKE
D 491600-04-1
491300-200-001
MEN
SOURCE:
MRB 49.13.00/01-13
DETAILED INSPECTION OF APU AIR INTAKE,
DIFFUSER ELBOW, SEALS AND FELT METAL
D 491600-03-1
REFERENCES
SOURCE:
MRB 49.13.00/01-36
GENERAL VISUAL INSPECTION OF ALL APU COMPARTMENT FIRE
WALLS AND SEALS:
- COMPARTMENT DOORS
- FWD AND AFT FIRE WALLS
- SIDE FIRE WALLS
- UPPER FIRE WALL
D 491600-01-1
TPS
ALL
SOURCE:
MRB 49.16.00/01-13
ACCESS PANELS: 314AR, 316AR, 315AL
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
TASK
E
NUMBER
V
R 491600-B5-1
ZONE
315
DESCRIPTION
AIR INTAKE SYSTEM
SKILL TASK
CODE CODE
INTERVALS
SOURCE
AF
RST
I:
2400 FH
EASA AD
FAA AD
ISB
EN
GVI
I:
600 FH
EASA AD
FAA AD
ISB
EN
DET
I:
750 FH
OR
6 MO
MRB 7
LUR
I:
8500 FH
OR
72 MO
MRB 9
LUR
I:
1500 FH
OR
12 MO
MRB 9
LUR
I:
24 MO
MRB 9
MRB 9
CLEANING OF APU AIR INTAKE
ACCESS PANELS: 315AL, 316AR
R 491600-B6-1
310
APU AIR INTAKE SYSTEM
GENERAL VISUAL INSPECTION OF APU AIR INLET PLENUM AND APU AIR
INTAKE.
D 492000-01-1
310
ACCESS PANELS: 315AL, 316AR
ENGINE
DETAILED INSPECTION OF MAGNETIC CHIP DETECTOR
R 493000-B1-1
315
ACCESS PANELS: 315AL, 316AR
ENGINE FUEL AND CONTROL
EN
DIS
DISCARD FUEL INLET FILTER ELEMENT
D 493100-01-1
310
ACCESS PANELS: 315AL, 316AR
FUEL DISTRIBUTION
EN
VCK
VISUAL CHECK OF FUEL FILTER DIFFERENTIAL PRESSURE
INDICATOR.
D 493400-01-1
210
ACCESS PANELS: 315AL
APU FUEL LOW PRESSURE WARNING
EN
OPC
210
APU FUEL LOW PRESSURE WARNING
EN
OPC
I:
24 MO
315
ACCESS PANELS: 315AL, 316AR
IGNITION AND STARTING
DETAILED INSPECTION OF IGNITER PLUG
491600-100-003
EASA AD
2006-0153
FAA AD
2007-13-08
ISB 49-1068
491600-210-802
EASA AD
2006-0153
FAA AD
2007-13-08
ISB 49-1068
499142-200-001
MEN
TASKM. APPLICABI
H.
LITY
1
1.50
0649 1130
1657 1767
1
0.20
0649 1130
1657 1767
1
0.10
1
0.15
1
0.02
493100-710-001
1
0.10
SOURCE:
MRB 49.34.00/01-36
493100-710-003
1
0.10
ALL
1
0.20
ALL
493241-920-001
ALL
SOURCE:
MRB 49.30.00/02-13
493211-210-001
SOURCE:
MRB 49.31.00/01-36
OPERATIONAL CHECK OF APU FUEL LOW PRESSURE CIRCUIT
R 494000-B2-1
REFERENCES
SOURCE:
MRB 49.20.00/01-36
OPERATIONAL CHECK OF APU FUEL LOW PRESSURE CIRCUIT
R 493400-B1-1
TPS
SOURCE:
MRB 49.34.00/01-13
EN
DET
I:
6000 FH
OR
40 MO
MRB 7
LUR
494141-220-001
SOURCE:
MRB 49.40.00/02-13
ACCESS PANELS: 315AL, 316AR
Sub 2 - Page 77 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
TASK
E
NUMBER
V
R 494000-B3-1
ZONE
315
DESCRIPTION
IGNITION AND STARTING
SKILL TASK
CODE CODE
INTERVALS
SOURCE
EN
VCK
I:
600 FH
EASA AD
FAA AD
ISB
EN
VCK
I:
750 FH
OR
6 MO
SIL
LUR
EN
OPC
I:
600 FH
EASA AD
FAA AD
ISB
EN
DET
I:
6000 FH
OR
40 MO
MRB 7
LUR
CHECK WEAR INDICATOR OF STARTER MOTOR BRUSH
ACCESS PANELS: 315AL
R 494000-B3-2
315
IGNITION AND STARTING
CHECK WEAR INDICATOR OF STARTER MOTOR BRUSH
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
494251-200-008
EASA AD
2006-0153
FAA AD
2007-13-08
ISB 49-1068
494251-200-008
SIL 49-043
1
0.10
0649 1130
1657 1767
1
0.10
494251-700-002
EASA AD
2006-0153
FAA AD
2007-13-08
ISB 49-1068
494141-220-002
1
0.50
0649 1200
1379 1488
1560 1578
1743 1761
1851 1863
1876 1890
2151 2163
0649 1130
1657 1767
1
0.20
ACCESS PANELS: 315AL
R 494000-B4-1
315
IGNITION AND STARTING
TEST OF CLUTCH OF APU STARTER MOTOR
ACCESS PANELS: 315AL, 316AR
D 494141-01-1
316
IGNITER PLUG
DETAILED INSPECTION OF IGNITER PLUG
D 494251-01-1
315
ACCESS PANELS: 315AL, 316AR
STARTER MOTOR
SOURCE:
MRB 49.40.00/03-36
EN
VCK
I:
600 FH
EASA AD
ISB
494251-200-005
EASA AD
2006-0153
ISB 49-1068
1
0.10
EN
OPC
I:
600 FH
EASA AD
ISB
494251-700-001
EASA AD
2006-0153
ISB 49-1068
1
0.50
AF
RST
I:
2250 FH
OR
24 MO
MRB 7
LUR
495152-600-001
1
0.30
I:
24 MO
MRB 9
1
0.10
CHECK WEAR INDICATOR OF STARTER MOTOR BRUSH
D 494251-02-1
315
ACCESS PANELS: 315AL
STARTER MOTOR
TEST OF CLUTCH OF APU STARTER MOTOR
D 495100-01-1
315
ACCESS PANELS: 315AL, 316AR
LOAD COMPRESSOR SURGE/REVERSE FLOW
PROTECTION
CLEAN SURGE VALVE FILTER
R 498000-B1-1
310
ACCESS PANELS: 315AL, 316AR
EXHAUST
VISUAL CHECK OF APU COMPARTMENT EXHAUST MUFFLER
INSULATION COVERS AND BELLOWS
EN
VCK
SOURCE:
MRB 49.51.20/02-36
498100-200-017
ALL
SOURCE:
MRB 49.80.00/01-13
ACCESS PANELS: 315AL, 316AR
Sub 2 - Page 78 of 305
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REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
TASK
E
NUMBER
V
D 498100-04-1
ZONE
310
DESCRIPTION
EXHAUST SYSTEM
SKILL TASK
CODE CODE
EN
DET
INTERVALS
I:
24 MO
SOURCE
MRB 9
VISUAL CHECK OF APU COMPARTMENT EXHAUST MUFFLER
INSULATION COVERS AND BELLOWS
D 499100-02-1
310
ACCESS PANELS: 315AL, 316AR
STORAGE AND DISTRIBUTION
TPS
REFERENCES
498100-200-015
MEN
TASKM. APPLICABI
H.
LITY
1
0.10
SOURCE:
MRB 49.80.00/04-36
EN
VCK
I:
7500 FH
OR
50 MO
AOT
SIL
LUR
490000-790-001
AOT 49-03
SIL 49-032
1
0.60
AF
DIS
I:
3000 FH
OR
24 MO
NOTE
SIL
LUR
499141-200-002
SIL 49-051
1
0.20
ALL
EN
VCK
I:
7500 FH
OR
50 MO
SIL
LUR
490000-790-008
SIL 49-032
1
0.60
ALL
AF
FNC
I:
8 DY
MRB 8
521000-210-004
1
1
1
1
0.02
0.02
0.02
0.02
ALL
1
1
1
1
0.05
0.05
0.05
0.05
ALL
CHECK APU COMPARTMENT AND AIR INTAKE DUCT FOR OIL CONTAMINATION
ACCESS PANELS: 314AR, 315AL, 316AR
R 499100-B2-1
315
STORAGE AND DISTRIBUTION
REMOVE AND DISCARD OIL FILTER ELEMENTS (8069KM)
AND (8076KM).
NOTE: DEPENDING ON OPERATING ENVIROMENT AND
OPERATORS EXPERIENCE A HIGHER INITIAL
INTERVAL MAY BE USED
R 499100-B4-1
310
ACCESS PANELS: 315AL, 316AR
STORAGE AND DISTRIBUTION
CHECK APU COMPARTMENT AND AIR INTAKE DUCT FOR
OIL CONTAMINATION
521000-01-1
521000-02-1
831
832
841
842
831
832
841
842
ACCESS PANELS: 314AR, 315AL, 316AR
PASSENGER/CREW DOOR
CHECK EMERGENCY CYLINDER/ACCUMULATOR PRESSURE
NOTE : TASK IS NOT APPLICABLE FOR DEACTIVATED
PASSENGER/CREW DOORS
PASSENGER/CREW DOOR
FUNCTIONAL CHECK OF DOOR SUSPENSION
ACCESS PANELS: 831, 831FZ, 831GZ, 832, 832FZ, 832GZ, 841, 841FZ, 841GZ, 842,
842FZ, 842GZ
SOURCE:
MRB 52.10.00/01
AF
FNC
I:
15000 FH
OR
10000 FC
OR
80 MO
MRB 6,9
521000-720-001
SOURCE:
MRB 52.10.00/02
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
521000-03-1
ZONE
831
832
841
842
DESCRIPTION
PASSENGER/CREW DOOR
SKILL TASK
CODE CODE
AF
DET
INTERVALS
I:
48 MO
SOURCE
MRB 6
DETAILED INSPECTION OF DOOR SEALS
TPS
REFERENCES
521000-220-006
SOURCE:
MRB 52.10.00/06
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
0.05
0.05
0.05
0.05
ALL
1
1
1
1
0.10
0.10
0.10
0.10
ALL
1
1
1
1
0.10
0.10
0.10
0.10
ALL
1
1
1
1
0.20
0.20
0.20
0.20
ALL
1
1
1
1
0.10
0.10
0.10
0.10
ALL
NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED
PASSENGER/CREW DOORS
521000-04-1
831
832
841
842
ACCESS PANELS: 831, 832, 841, 842
PASSENGER/CREW DOOR
AF
DET
DETAILED INSPECTION OF PASSENGER/CREW
DOOR FOR INTEGRITY AND GOOD ADJUSTMENT OF
MECHANISMS (INCLUDING GIRT BAR)
I:
15000 FH
OR
10000 FC
OR
80 MO
MRB 6,9
I:
15000 FH
OR
10000 FC
OR
80 MO
I:
15000 FH
OR
10000 FC
OR
80 MO
MRB 6,9
I:
15000 FH
OR
10000 FC
OR
80 MO
MRB 6,9
521000-200-002
SOURCE:
MRB 52.10.00/02
PREPARATION: INSULATION REMOVED;
521000-05-1
831
832
841
842
ACCESS PANELS: 831AZ, 831BZ, 831CZ, 831DZ, 831EZ, 831FZ, 831GZ, 832AZ,
832BZ, 832CZ, 832DZ, 832EZ, 832FZ, 832GZ, 841AZ, 841BZ, 841CZ, 841DZ, 841EZ,
841FZ, 841GZ, 842AZ, 842BZ, 842CZ, 842DZ, 842EZ, 842FZ, 842GZ
PASSENGER/CREW DOOR
AF
FNC
FUNCTIONAL CHECK OF LOCKING MECHANISM
ACCESS PANELS: 831, 832, 841, 842
521000-06-1
521000-07-1
831
832
841
842
831
832
841
842
PASSENGER/CREW DOOR
AF
FNC
FUNCTIONAL CHECK OF ESCAPE SLIDE RELEASE
MECHANISM
NOTE : ONLY FWD DOORS FOR POST 37807 (IF AFT DOORS
FULLY DEACTIVATED).
PASSENGER/CREW DOOR
CHECK OF DOOR STOPS ADJUSTMENT
ACCESS PANELS: 831, 832, 841, 842
AF
FNC
521000-720-003
SOURCE:
MRB 52.10.00/02
MRB 6,9
521000-720-005
SOURCE:
MRB 52.10.00/02
521000-200-001
SOURCE:
MRB 52.10.00/02
Sub 2 - Page 80 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
521000-08-1
ZONE
831
832
841
842
DESCRIPTION
PASSENGER/CREW DOOR
SKILL TASK
CODE CODE
AF
OPC
OPERATIONAL CHECK OF INTERLOCK MECHANISM TO
ENSURE THAT EMERGENCY ESCAPE HANDLE STAYS IN
DISARMED POSITION WHEN DOOR IS UP AND OUTSIDE
OF FRAME
INTERVALS
SOURCE
I:
15000 FH
OR
10000 FC
OR
80 MO
MRB 6,9
I:
15000 FH
OR
10000 FC
OR
80 MO
I:
15000 FH
OR
10000 FC
OR
80 MO
MRB 6,9
I:
15000 FH
OR
10000 FC
OR
80 MO
MRB 6,9
I:
15000 FH
OR
10000 FC
OR
80 MO
MRB 6,9
TPS
REFERENCES
521000-710-002
SOURCE:
MRB 52.10.00/02
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
0.10
0.10
0.10
0.10
ALL
1
1
1
1
0.10
0.10
0.10
0.10
ALL
1
1
1
1
0.05
0.05
0.05
0.05
ALL
1
1
1
1
0.05
0.05
0.05
0.05
ALL
1
1
1
1
0.05
0.05
0.05
0.05
ALL
NOTE : ONLY FWD DOORS FOR POST 37807 (IF AFT DOORS
FULLY DEACTIVATED).
521000-09-1
521000-10-1
831
832
841
842
831
832
841
842
ACCESS PANELS: 831, 832, 841, 842
PASSENGER/CREW DOOR
AF
FNC
FUNCTIONAL CHECK OF MECHANICAL LOCKING
INDICATION
ACCESS PANELS: 831, 832, 841, 842
PASSENGER/CREW DOOR
AF
OPC
OPERATIONAL CHECK OF DAMPING DURING
OPENING/CLOSING
NOTE : ONLY FWD DOORS FOR POST 37807 (IF AFT DOORS
FULLY DEACTIVATED).
521000-11-1
831
832
841
842
ACCESS PANELS: 831, 832, 841, 842
PASSENGER/CREW DOOR
AF
OPC
OPERATIONAL CHECK OF STRIKER MECHANISM
NOTE : ONLY FWD DOORS FOR POST 37807 (IF AFT DOORS
FULLY DEACTIVATED).
521000-12-1
831
832
841
842
ACCESS PANELS: 831, 832, 841, 842
PASSENGER/CREW DOOR
OPERATIONAL CHECK OF ESCAPE SLIDE DISARMING
WHEN DOOR IS OPENED FROM THE OUTSIDE
NOTE : ONLY FWD DOORS FOR POST 37807 (IF AFT DOORS
FULLY DEACTIVATED).
AF
OPC
521000-720-004
SOURCE:
MRB 52.10.00/02
MRB 6,9
521000-710-001
SOURCE:
MRB 52.10.00/02
521000-710-003
SOURCE:
MRB 52.10.00/02
521000-720-002
SOURCE:
MRB 52.10.00/02
ACCESS PANELS: 831, 832, 841, 842
Sub 2 - Page 81 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
521000-14-1
521101-01-1
ZONE
831
832
841
842
831
841
DESCRIPTION
PASSENGER/CREW DOOR
SKILL TASK
CODE CODE
AF
LUB
521104-01-1
831
841
831
841
I:
20 MO
SOURCE
MRB 9
SIL
TPS
REFERENCES
122252-640-016
SIL 53-076
LUBRICATION OF HINGE ARM SUPPORT FITTING BEARINGS
NOTE : TASK IS NOT APPLICABLE FOR DEACTIVATED
PASSENGER/CREW DOORS
FWD PAX/CREW DOOR STOP ASSEMBLIES
SOURCE:
MRB 52.10.00/05
AF
DET
DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ON
FORWARD PASSENGER/CREW DOOR, LH/RH
521103-01-1
INTERVALS
ACCESS PANELS: 831, 841
FWD PAX/CREW DOOR SKIN EXTERNAL SURFACE
GENERAL VISUAL INSPECTION OF FORWARD PASSENGER/CREW
DOOR SKIN, EXTERNAL SURFACE, LH/RH
FWD PAX/CREW DOOR INTERNAL STRUCTURE
AF
AF
GVI
DET
DETAILED INSPECTION OF FORWARD PASSENGER/CREW DOOR,
INTERNAL STRUCTURE, LH/RH
T:
12 YE
I:
12 YE
MRB CPCP
T:
14800 FC
I:
14800 FC
T:
12 YE
I:
6 YE
ALI
I:
20 MO
MRB 6
521100-200-001
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
0.10
0.10
0.10
0.10
ALL
1
1
0.23
0.23
ALL
1
1
0.15
0.15
ALL
1
1
0.50
0.50
ALL
1
1
1
1
0.10
0.10
0.10
0.10
ALL
1
1
1
1
0.10
0.10
0.10
0.10
ALL
1
1
0.23
0.23
ALL
SOURCE:
MRB 521101-01-1
MRB CPCP
521100-210-002
SOURCE:
ALI 521103-01-1
1+2 521100-200-002
SOURCE:
MRB 521104-01-1
PREPARATION: LINING REMOVED; INSULATION REMOVED;
521121-01-1
521121-02-1
831
832
841
842
831
832
841
842
ACCESS PANELS: 831, 841
PASSENGER / CREW DOOR
AF
LUB
LUBRICATION OF EXTERIOR CONTROL HANDLE AND TELESCOPIC
ARM
NOTE : TASK IS NOT APPLICABLE FOR DEACTIVATED
PASSENGER/CREW DOORS
PASSENGER / CREW DOOR
122252-640-006
SOURCE:
MRB 52.10.00/03
AF
LUB
I:
36 MO
MRB 6
LUBRICATION OF SAFETY PIN GUIDE FITTING AND DOOR
ARMING/DISARMING MECHANISM
122252-640-014
AOT 52A1103
SOURCE:
MRB 52.10.00/04
NOTE : TASK IS NOT APPLICABLE FOR DEACTIVATED
PASSENGER/CREW DOORS
521301-01-1
832
842
ACCESS PANELS: 831BZ, 831CZ, 831DZ, 832BZ, 832CZ, 832DZ, 841BZ, 841CZ,
841DZ, 842BZ, 842CZ, 842DZ
AFT PAX/CREW DOOR STOP ASSEMBLIES
DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ON AFT
PASSENGER/CREW DOOR, LH/RH
AF
DET
T:
12 YE
I:
12 YE
MRB CPCP
521300-200-001
SOURCE:
MRB 521301-01-1
ACCESS PANELS: 832, 842
Sub 2 - Page 82 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
521303-01-1
521304-01-1
ZONE
832
842
832
842
DESCRIPTION
AFT PAX/CREW DOOR SKIN EXTERNAL SURFACE
GENERAL VISUAL INSPECTION OF AFT PASSENGER/CREW DOOR
SKIN, EXTERNAL SURFACE, LH/RH
AFT PAX/CREW DOOR INTERNAL STRUCTURE
SKILL TASK
CODE CODE
AF
AF
GVI
DET
DETAILED INSPECTION OF AFT PASSENGER/CREW DOOR,
INTERNAL STRUCTURE, LH/RH
INTERVALS
SOURCE
T:
14800 FC
I:
14800 FC
T:
12 YE
I:
6 YE
ALI
I:
9000 FH
OR
60 MO
MRB 8
LUR
I:
9000 FH
OR
60 MO
MRB 8
LUR
I:
12000 FH
OR
80 MO
MRB 8
LUR
I:
12000 FH
OR
80 MO
MRB 8
LUR
MRB CPCP
TPS
REFERENCES
521300-210-002
SOURCE:
ALI 521303-01-1
1+2 521300-200-002
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.15
0.15
ALL
1
1
0.50
0.50
ALL
2
2
2
2
2
2
0.20
0.20
0.20
0.20
0.20
0.20
1130 1200
1379 1578
1657 1767
2151 2163
2
2
2
2
0.20
0.20
0.20
0.20
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
1
1
1
1
0.20
0.20
0.20
0.20
0.20
0.20
1130 1200
1379 1578
1657 1767
1
1
1
1
0.20
0.20
0.20
0.20
0649 1488
1560 1743
1761
SOURCE:
MRB 521304-01-1
PREPARATION: LINING REMOVED; INSULATION REMOVED;
522100-01-1
522100-01-2
151
152
833
834
843
844
151
152
834
844
ACCESS PANELS: 832, 842
PASSENGER COMPARTMENT EMERGENCY EXIT
AF
OPC
OPERATIONAL CHECK OF UNLOCKING AND OPENING FROM
INSIDE IN ARMED MODE.
522100-710-003
SOURCE:
MRB 52.21.00/01
NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED
EMERGENCY EXITS
ACCESS PANELS: 151CW, 152CW, 826, 833BZ, 834BZ, 843BZ, 844BZ
PASSENGER COMPARTMENT EMERGENCY EXIT
AF
OPC
OPERATIONAL CHECK OF UNLOCKING AND OPENING FROM
INSIDE IN ARMED MODE
522100-710-003
SOURCE:
MRB 52.21.00/01
NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED
EMERGENCY EXITS
522100-02-1
522100-02-2
151
152
833
834
843
844
151
152
834
844
ACCESS PANELS: 151CW, 152CW, 826, 834BZ, 844BZ
PASSENGER COMPARTMENT EMERGENCY EXIT
AF
FNC
FUNCTIONAL CHECK OF MANUAL AND AUTOMATIC SLIDE
RELEASE SIGNAL.
522100-720-001
SOURCE:
MRB 52.21.00/02
NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED
EMERGENCY EXITS
ACCESS PANELS: 151CW, 152CW, 826, 833BZ, 834BZ, 843BZ, 844BZ
PASSENGER COMPARTMENT EMERGENCY EXIT
FUNCTIONAL CHECK OF MANUAL AND AUTOMATIC SLIDE RELEASE SIGNAL
AF
FNC
522100-720-001
SOURCE:
MRB 52.21.00/02
NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED EMERGENCY EXITS
ACCESS PANELS: 151CW, 152CW, 826, 834BZ, 844BZ
Sub 2 - Page 83 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
522100-02-5
522100-02-6
ZONE
151
152
833
834
843
844
151
152
834
844
DESCRIPTION
PASSENGER COMPARTMENT EMERGENCY EXIT
SKILL TASK
CODE CODE
AF
FNC
FUNCTIONAL CHECK OF MANUAL AND AUTOMATIC SLIDE
RELEASE SIGNAL.
INTERVALS
SOURCE
I:
15000 FH
OR
100 MO
MRB 8
LUR
I:
15000 FH
OR
100 MO
MRB 8
LUR
I:
12000 FH
OR
80 MO
MRB 8
LUR
I:
12000 FH
OR
80 MO
MRB 8
LUR
I:
15000 FH
OR
100 MO
MRB 8
LUR
TPS
REFERENCES
522100-720-001
SOURCE:
MRB 52.21.00/04
NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED
EMERGENCY EXITS
ACCESS PANELS: 151CW, 152CW, 826, 833BZ, 834BZ, 843BZ, 844BZ
PASSENGER COMPARTMENT EMERGENCY EXIT
AF
FNC
FUNCTIONAL CHECK OF MANUAL AND AUTOMATIC SLIDE RELEASE SIGNAL
522100-720-001
SOURCE:
MRB 52.21.00/04
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
1
1
0.20
0.20
0.20
0.20
0.20
0.20
2151 2163
1
1
1
1
0.20
0.20
0.20
0.20
1851 1863
1876 1890
2
2
2
2
2
2
0.20
0.20
0.20
0.20
0.20
0.20
1130 1200
1379 1578
1657 1767
2
2
2
2
0.20
0.20
0.20
0.20
0649 1488
1560 1743
1761
2
2
2
2
2
2
0.20
0.20
0.20
0.20
0.20
0.20
2151 2163
NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED EMERGENCY EXITS
ACCESS PANELS: 151CW, 152CW, 826, 834BZ, 844BZ
522100-07-1
522100-07-2
151
152
833
834
843
844
151
152
834
844
PASSENGER COMPARTMENT EMERGENCY EXIT
AF
OPC
OPERATIONAL CHECK OF UNLOCKING AND OPENING FROM
OUTSIDE IN ARMED MODE.
522100-710-004
SOURCE:
MRB 52.21.00/02
NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED
EMERGENCY EXITS
ACCESS PANELS: 151CW, 152CW, 826, 833BZ, 834BZ, 843BZ, 844BZ
PASSENGER COMPARTMENT EMERGENCY EXIT
AF
OPC
OPERATIONAL CHECK OF UNLOCKING AND OPENING FROM OUTSIDE IN
ARMED MODE
522100-710-004
SOURCE:
MRB 52.21.00/02
NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED EMERGENCY EXITS
522100-07-5
151
152
833
834
843
844
ACCESS PANELS: 151CW, 152CW, 826, 834BZ, 844BZ
PASSENGER COMPARTMENT EMERGENCY EXIT
OPERATIONAL CHECK OF UNLOCKING AND OPENING FROM
OUTSIDE IN ARMED MODE.
NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED
EMERGENCY EXITS
AF
OPC
522100-710-004
SOURCE:
MRB 52.21.00/04
ACCESS PANELS: 151CW, 152CW, 826, 833BZ, 834BZ, 843BZ, 844BZ
Sub 2 - Page 84 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
522100-07-6
ZONE
151
152
834
844
DESCRIPTION
PASSENGER COMPARTMENT EMERGENCY EXIT
SKILL TASK
CODE CODE
AF
OPC
OPERATIONAL CHECK OF UNLOCKING AND OPENING FROM
OUTSIDE IN ARMED MODE
INTERVALS
SOURCE
I:
15000 FH
OR
100 MO
MRB 8
LUR
I:
15000 FH
OR
100 MO
MRB 9
LUR
I:
15000 FH
OR
100 MO
MRB 9
LUR
T:
12 YE
OR
39300 FC
I:
6 YE
OR
11400 FC
ALI
MRB CPCP
TPS
REFERENCES
522100-710-004
SOURCE:
MRB 52.21.00/04
MEN
TASKM. APPLICABI
H.
LITY
2
2
2
2
0.20
0.20
0.20
0.20
1851 1863
1876 1890
2
2
2
2
2
2
0.20
0.20
0.20
0.20
0.20
0.20
1130 1200
1379 1578
1657 1767
2151 2163
2
2
2
2
0.20
0.20
0.20
0.20
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
1
1
1.00
1.00
1.00
1.00
1130 1200
1379 1578
1657 1767
2151 2163
NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED
EMERGENCY EXITS
522100-08-1
151
152
833
834
843
844
ACCESS PANELS: 151CW, 152CW, 826, 834BZ, 844BZ
PASSENGER COMPARTMENT EMERGENCY EXIT
AF
OPC
- OPERATIONAL CHECK OF UNLOCKING AND OPENING
FROM INSIDE AND OUTSIDE IN DISARMED POSITION
- OPERATIONAL CHECK OF CLOSING AND LOCKING FROM
INSIDE
- OPERATIONAL CHECK OF ESCAPE SLIDE ARMING AND
DISARMING.
522100-710-005
SOURCE:
MRB 52.21.00/03
NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED
EMERGENCY EXITS
522100-08-2
151
152
834
844
ACCESS PANELS: 151CW, 152CW, 826, 833BZ, 834BZ, 843BZ, 844BZ
PASSENGER COMPARTMENT EMERGENCY EXIT
AF
OPC
- OPERATIONAL CHECK OF UNLOCKING AND OPENING
FROM INSIDE AND OUTSIDE IN DISARMED POSITION
- OPERATIONAL CHECK OF CLOSING AND LOCKING FROM
INSIDE
- OPERATIONAL CHECK OF ESCAPE SLIDE ARMING AND
DISARMING
522100-710-005
SOURCE:
MRB 52.21.00/03
NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED
EMERGENCY EXITS
522102-01-1
833
834
843
844
ACCESS PANELS: 151CW, 152CW, 826, 834BZ, 844BZ
EMERGENCY EXITS STRUCTURE
DETAILED INSPECTION OF EMERGENCY EXITS, INTERNAL
STRUCTURE AND LOAD TRANSMITTING PROFILE, LH/RH
PREPARATION: LINING REMOVED; INSULATION REMOVED;
ACCESS PANELS: 833, 834, 843, 844
AF
DET
1
522100-200-001
SOURCE:
ALI 522102-01-1
MRB 522102-01-1
Sub 2 - Page 85 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
522102-01-2
ZONE
834
844
DESCRIPTION
EMERGENCY EXITS STRUCTURE
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF EMERGENCY EXITS, INTERNAL
STRUCTURE AND LOAD TRANSMITTING PROFILE, LH/RH
PREPARATION: LINING REMOVED; INSULATION REMOVED;
522103-01-1
833
834
843
844
ACCESS PANELS: 834, 844
EMERGENCY EXITS STRUCTURE
NDT
SDI
AF
LUB
SPECIAL DETAILED INSPECTION OF OVERWING EMERGENCY EXIT FRAME.
INTERVALS
SOURCE
T:
12 YE
OR
39300 FC
I:
6 YE
OR
11400 FC
T:
24000 FC
I:
4500 FC
ALI
MRB CPCP
ISB
I:
18 MO
OR
4500 FC
MRB 6,9
I:
18 MO
OR
4500 FC
MRB 6,9
I:
18000 FC
OR
72 MO
MRB 6,9
T:
12500 FC
OR
25000 FH
I:
12500 FC
OR
25000 FH
ALI
TPS
1
REFERENCES
522100-200-001
MEN
TASKM. APPLICABI
H.
LITY
1
1
1.00
1.00
0649 1488
1560 1743
1761 1851
1863 1876
1890
522100-200-003
ISB 52-1145
1
1
1
1
2.00
2.00
2.00
2.00
1200 1379
2151 2163
122252-640-002
1
1
0.20
0.20
ALL
1
1
0.10
0.10
ALL
2
0.20
ALL
1
0.10
ALL
SOURCE:
ALI 522102-01-2
MRB 522102-01-2
PREPARATION: LINING REMOVED;
INSULATION REMOVED;
523000-01-1
825
826
ACCESS PANELS: 833, 834, 843, 844
CARGO COMPARTMENT DOOR, FWD AND AFT
LUBRICATION OF CARGO DOOR
523000-03-1
825
826
ACCESS PANELS: 825, 825AR, 826, 826AR
CARGO COMPARTMENT DOOR
AF
LUB
LUBRICATION OF EXTERIOR CARGO DOOR HANDLE
523100-01-1
825
NOTE : INTERVAL MAY NEED TO BE MORE FREQUENT
WHEN OPERATING IN HOSTILE ENVIRONMENTS
FORWARD CARGO COMPARTMENT DOOR
AF
FNC
FUNCTIONAL CHECK OF FORWARD CARGO COMPARTMENT
DOOR, COMPRISING FUNCTIONAL CHECKS OF:
- LOCKING MECHANISM
- INTERLOCK MECHANISM
- DRIFT PIN MECHANISM
- SAFETY MECHANISM
523101-01-1
825
ACCESS PANELS: 825, 825AR
FWD CARGO COMPARTMENT DOOR SKIN
GENERAL VISUAL INSPECTION OF FORWARD CARGO
COMPARTMENT DOOR SKIN, EXTERNAL SURFACE
AF
GVI
SOURCE:
MRB 52.31.00/01
122252-640-009
SOURCE:
MRB 52.31.00/01
523100-720-001
SOURCE:
MRB 52.31.00/02
523111-200-011
SOURCE:
ALI 523101-01-1
Sub 2 - Page 86 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
523103-01-1
ZONE
825
DESCRIPTION
FWD CARGO DOOR INTERNAL STRUCTURE
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT
DOOR, INTERNAL STRUCTURE
INTERVALS
SOURCE
T:
12 YE
I:
6 YE
MRB CPCP
T:
5300 FC
I:
5300 FC
MRB
T:
12 YE
OR
51200 FC
OR
102400 FH
I:
12 YE
OR
14500 FC
OR
29000 FH
ST:
55100 FC
OR
110200 FH
SI:
5900 FC
OR
11800 FH
T:
12 YE
I:
6 YE
T:
10300 FC
OR
20700 FH
I:
10300 FC
OR
20700 FH
ALI
MRB CPCP
TPS
1
REFERENCES
523111-200-001
MEN
TASKM. APPLICABI
H.
LITY
1
1.50
ALL
1
0.33
ALL
1
0.30
ALL
1
0.50
ALL
1
0.30
ALL
SOURCE:
MRB 523103-01-1
PREPARATION: LINING REMOVED; INSULATION REMOVED;
523105-01-3
825
ACCESS PANELS: 825
FWD CARGO COMPARTMENT DOOR ACTUATOR
AF
GVI
GENERAL VISUAL INSPECTION OF FORWARD CARGO
COMPARTMENT DOOR, ACTUATOR ATTACH FITTINGS
523108-01-1
825
ACCESS PANELS: 825
FWD CARGO DOOR FITTINGS EXTERNAL AREA
AF
DET
DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT
DOOR, HINGE FITTINGS AND ATTACHMENT AREA, EXTERNAL
NOTE: APPLICATION OF TPS IS LIMITED TO THE INNER SIDE
OF HINGE FITTINGS
ACCESS PANELS: 825
523109-01-1
825
FWD CARGO DOOR LOCKING HOOKS
AF
DET
DETAILED INSPECTION OF LOCKING HOOKS AND FORK
FITTINGS OF FORWARD CARGO COMPARTMENT DOOR AT ALL
FRAMES, BETWEEN LONGERON 4 AND LONGERON 5 (6 PLACES)
ACCESS PANELS: 825, 825AR
523109-02-1
825
FWD CARGO DOOR LOCKING HOOKS
GENERAL VISUAL INSPECTION OF LOCKING HOOKS AND FORK
FITTINGS OF FORWARD CARGO COMPARTMENT DOOR AT ALL
FRAMES, BETWEEN LONGERON 4 AND LONGERON 5 (6 PLACES)
ACCESS PANELS: 825
AF
GVI
523111-200-022
SOURCE:
MRB 523105-01-3
1
523111-200-004
SOURCE:
ALI 523108-01-1
MRB 523108-01-1
MRB CPCP
1
523111-200-005
SOURCE:
MRB 523109-01-1
ALI
523111-200-013
SOURCE:
ALI 523109-02-1
Sub 2 - Page 87 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
523111-01-1
ZONE
826
DESCRIPTION
AFT CARGO DOOR SKIN
SKILL TASK
CODE CODE
AF
GVI
GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT
DOOR SKIN, EXTERNAL SURFACE
523113-01-1
826
AFT CARGO DOOR INTERNAL STRUCTURE
AF
DET
DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR,
INTERNAL STRUCTURE
INTERVALS
SOURCE
T:
12500 FC
OR
25000 FH
I:
12500 FC
OR
25000 FH
T:
12 YE
I:
6 YE
ALI
T:
5300 FC
I:
5300 FC
MRB
T:
12 YE
OR
51200 FC
OR
102400 FH
I:
12 YE
OR
14500 FC
OR
29000 FH
ST:
55100 FC
OR
110200 FH
SI:
5900 FC
OR
11800 FH
T:
12 YE
I:
6 YE
ALI
MRB CPCP
TPS
REFERENCES
523211-200-011
MEN
TASKM. APPLICABI
H.
LITY
1
0.10
1130 1200
1379 1578
1657 1767
2151 2163
1
1.50
1130 1200
1379 1578
1657 1767
2151 2163
1
0.10
1130 1200
1379 1578
1657 1767
2151 2163
1
0.30
1130 1200
1379 1578
1657 1767
2151 2163
1
0.50
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
ALI 523111-01-1
MRB CPCP
1
523211-200-001
SOURCE:
MRB 523113-01-1
PREPARATION: LINING REMOVED; INSULATION REMOVED;
523115-01-3
826
ACCESS PANELS: 826
AFT CARGO DOOR ACTUATOR ATTACH FITTINGS
AF
GVI
GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT
DOOR ACTUATOR ATTACH FITTINGS
523118-01-2
826
ACCESS PANELS: 826
AFT CARGO DOOR FITTINGS EXTERNAL AREA
AF
DET
DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR,
HINGE FITTINGS AND ATTACHMENT AREA, EXTERNAL
NOTE: APPLICATION OF TPS IS LIMITED TO THE INNER SIDE
OF HINGE FITTINGS
ACCESS PANELS: 826
523119-01-2
826
AFT CARGO DOOR LOCKING HOOKS
DETAILED INSPECTION OF LOCKING HOOKS AND FORK
FITTINGS OF AFT CARGO COMPARTMENT DOOR AT ALL FRAMES,
BETWEEN LONGERON 4 AND LONGERON 5 (6 PLACES)
ACCESS PANELS: 826, 826AR
AF
DET
523211-200-022
SOURCE:
MRB 523115-01-3
1
523211-200-005
SOURCE:
ALI 523118-01-2
MRB 523118-01-2
MRB CPCP
1
523211-200-006
SOURCE:
MRB 523119-01-2
Sub 2 - Page 88 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
523119-02-2
ZONE
826
DESCRIPTION
AFT CARGO DOOR LOCKING HOOKS
SKILL TASK
CODE CODE
AF
GVI
GENERAL VISUAL INSPECTION OF LOCKING HOOKS AND FORK
FITTINGS OF AFT CARGO COMPARTMENT DOOR AT ALL FRAMES,
BETWEEN LONGERON 4 AND LONGERON 5 (6 PLACES)
ACCESS PANELS: 826
523130-01-1
825
826
FWD / AFT CARGO DOOR HANDLE
AF
DET
AF
FNC
DETAILED INSPECTION OF BEARING HOUSING OF THE
FORWARD / AFT CARGO DOOR LOCKING HANDLE
523200-01-1
826
ACCESS PANELS: 825, 825AR, 826, 826AR
AFT CARGO COMPARTMENT DOOR
FUNCTIONAL CHECK OF AFT CARGO COMPARTMENT
DOOR, COMPRISING FUNCTIONAL CHECKS OF:
- LOCKING MECHANISM
- INTERLOCK MECHANISM
- DRIFT PIN MECHANISM
- SAFETY MECHANISM
523211-01-1
826
ACCESS PANELS: 826, 826AR
AFT CARGO DOOR SKIN EXTERNAL
AF
GVI
GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT
DOOR SKIN, EXTERNAL SURFACE
523213-01-1
826
AFT CARGO DOOR INTERNAL STRUCTURE
AF
DET
DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR,
INTERNAL STRUCTURE
INTERVALS
SOURCE
T:
10300 FC
OR
20700 FH
I:
10300 FC
OR
20700 FH
T:
4500 FC
I:
4500 FC
ALI
ISB
I:
18000 FC
OR
72 MO
MRB 6,9
T:
4500 FC
I:
4500 FC
ALI
T:
12 YE
I:
6 YE
MRB CPCP
T:
5300 FC
I:
5300 FC
MRB
TPS
REFERENCES
523211-200-012
MEN
TASKM. APPLICABI
H.
LITY
1
0.30
1130 1200
1379 1578
1657 1767
2151 2163
523000-220-001
ISB 52-1127
1
1
0.40
0.40
0649
523200-720-001
2
0.20
ALL
1
0.30
1
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.30
SOURCE:
ALI 523119-02-2
SOURCE:
MRB 52.31.00/02
523211-200-013
SOURCE:
ALI 523211-01-1
1
523211-200-007
SOURCE:
MRB 523213-01-1
PREPARATION: LINING REMOVED; INSULATION REMOVED;
523215-01-1
826
ACCESS PANELS: 826
AFT CARGO DOOR ACTUATOR ATTACH FITTINGS
GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT
DOOR ACTUATOR ATTACH FITTINGS
AF
GVI
523211-200-014
SOURCE:
MRB 523215-01-1
0649 1488
1560 1743
1761 1851
1863 1876
1890
ACCESS PANELS: 826
Sub 2 - Page 89 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
523217-01-1
ZONE
826
DESCRIPTION
AFT CARGO DOOR FITTINGS INTERNAL AREA
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR,
HINGE FITTINGS ATTACHMENT AREA, INTERNAL
PREPARATION: LINING REMOVED; INSULATION REMOVED;
523218-01-1
826
ACCESS PANELS: 826
AFT CARGO DOOR FITTINGS EXTERNAL AREA
AF
DET
DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR
HINGE FITTINGS AND ATTACHMENT AREA, EXTERNAL.
NOTE: APPLICATION OF TPS IS LIMITED TO THE INNER SIDE
OF HINGE FITTING
ACCESS PANELS: 826
523219-01-1
826
AFT CARGO DOOR FITTINGS EXTERNAL AREA
AF
DET
DETAILED INSPECTION OF LOCKING HOOKS AND FORK
FITTINGS OF AFT CARGO COMPARTMENT DOOR AT ALL FRAMES,
BETWEEN LONGERON 4 AND LONGERON 5 (6 PLACES)
ACCESS PANELS: 826, 826AR, 826BR, 826CR
523219-02-1
826
AFT CARGO DOOR LOCKING HOOKS AND FORK
FITTINGS
AF
GVI
GENERAL VISUAL INSPECTION OF LOCKING HOOKS AND FORK
FITTINGS OF AFT CARGO COMPARTMENT DOOR AT ALL FRAMES,
BETWEEN LONGERON 4 AND LONGERON 5 (6 PLACES)
523300-01-1
827
ACCESS PANELS: 826
BULK CARGO COMPARTMENT DOOR
LUBRICATION OF BULK CARGO COMPARTMENT DOOR HANDLE AND
HINGE ARM BEARINGS
AF
LUB
INTERVALS
ST:
30000 FC
SI:
15000 FC
T:
35200 FC
I:
15000 FC
T:
12 YE
OR
48000 FC
OR
60000 FH
I:
12 YE
OR
14500 FC
OR
29000 FH
ST:
48000 FC
OR
60000 FH
SI:
5900 FC
OR
11800 FH
T:
12 YE
I:
6 YE
T:
10300 FC
OR
20700 FH
I:
10300 FC
OR
20700 FH
I:
18 MO
OR
4500 FC
SOURCE
TPS
ALI
MRB
REFERENCES
523211-200-010
MEN
TASKM. APPLICABI
H.
LITY
1
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.10
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
ALI 523217-01-1
MRB 523217-01-1
ALI
MRB CPCP
1
523211-200-008
SOURCE:
ALI 523218-01-1
MRB 523218-01-1
MRB CPCP
1
523211-200-009
SOURCE:
MRB 523219-01-1
ALI
523211-200-015
SOURCE:
ALI 523219-02-1
MRB 6,9
122252-640-007
SOURCE:
MRB 52.33.00/01
NOTE: INTERVAL MAY NEED TO BE MORE FREQUENT
WHEN OPERATING IN HOSTILE ENVIRONMENTS
Sub 2 - Page 90 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
523301-01-1
523303-01-1
ZONE
DESCRIPTION
827
BULK CARGO DOOR SKIN EXTERNAL
827
GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT
DOOR SKIN, EXTERNAL SURFACE
BULK CARGO DOOR INTERNAL
SKILL TASK
CODE CODE
AF
AF
GVI
DET
DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR,
INTERNAL STRUCTURE
INTERVALS
SOURCE
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
T:
7500 FC
I:
7500 FC
T:
12 YE
I:
6 YE
ALI
523311-200-004
1
0.10
MRB CPCP
SOURCE:
ALI 523301-01-1
523311-200-003
1
0.20
T:
12 YE
I:
12 YE
MRB CPCP
1
0.75
1130 1200
1379 1578
1657 1767
2151 2163
I:
10000 FC
OR
72 MO
MRB 9
1
0.20
1200 1379
2151 2163
I:
48 MO
MRB 9
1
1
1
1
0.05
0.05
0.05
0.05
ALL
1
1
1
1
0.05
0.05
0.05
0.05
ALL
1
SOURCE:
MRB 523303-01-1
1130 1200
1379 1578
1657 1767
2151 2163
1130 1200
1379 1578
1657 1767
2151 2163
PREPARATION: LINING REMOVED; INSULATION REMOVED;
523305-01-1
827
ACCESS PANELS: 827
BULK CARGO DOOR FITTINGS AREA
AF
DET
DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR
STOP FITTINGS AND ATTACHMENT AREA, EXTERNAL AND
INTERNAL
1
523311-200-002
SOURCE:
MRB 523305-01-1
PREPARATION: LINING REMOVED; INSULATION REMOVED;
523500-01-1
100
ACCESS PANELS: 827
CARGO COMPARTMENT DOOR - ELECTRICAL CONTROL SYSTEM AND
HYDRAULIC SYSTEM
AF
OPC
OPERATIONAL CHECK OF DOOR CLOSING INHIBITION BY DOOR SILL LATCH
SWITCH
524100-01-1
524100-02-1
811
812
822
824
811
812
822
824
ACCESS PANELS: 826
ACCESS DOORS
AF
DET
SOURCE:
MRB 52.35.00/01
DETAILED INSPECTION OF DOOR SEALS
ACCESS PANELS: 811, 812, 822, 824
ACCESS DOORS
LUBRICATION OF EXTERIOR AVIONIC COMPARTMENT DOOR
HANDLE
NOTE: INTERVAL MAY NEED TO BE MORE FREQUENT
WHEN OPERATING IN HOSTILE ENVIRONMENTS
523500-710-001
524100-210-001
SOURCE:
MRB 52.41.00/01
AF
LUB
I:
20 MO
NOTE
MRB 9
122252-640-008
SOURCE:
MRB 52.41.00/02
ACCESS PANELS: 811, 812, 822, 824
Sub 2 - Page 91 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
524111-01-1
ZONE
811
DESCRIPTION
FWD AVIONIC DOOR INTERNAL STRUCTURE
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF FORWARD AVIONICS COMPARTMENT
ACCESS DOOR, INTERNAL STRUCTURE, INCLUDING HINGE ARMS
INTERVALS
SOURCE
T:
12 YE
I:
12 YE
MRB CPCP
T:
12 YE
I:
6 YE
MRB CPCP
T:
12 YE
I:
6 YE
MRB CPCP
T:
12 YE
I:
6 YE
MRB CPCP
I:
15000 FH
OR
100 MO
I:
15000 FH
OR
48 MO
I:
15000 FH
OR
48 MO
I:
15000 FH
OR
48 MO
MRB 6,9
LUR
TPS
1
REFERENCES
524111-200-001
MEN
TASKM. APPLICABI
H.
LITY
1
0.30
ALL
1
0.20
ALL
1
0.20
ALL
1
0.20
ALL
525100-220-001
1
0.25
ALL
MRB 9
SOURCE:
MRB 52.51.11/01
525100-720-002
1
0.15
ALL
MRB 9
SOURCE:
MRB 52.51.11/02
525100-710-005
1
0.05
ALL
MRB 9
SOURCE:
MRB 52.51.11/02
525100-710-006
1
0.05
ALL
SOURCE:
MRB 524111-01-1
PREPARATION: DOOR FLOOR PANELS REMOVED;
524121-01-1
824
ACCESS PANELS: 811
AFT AVIONIC DOOR INTERNAL STRUCTURE
AF
DET
DETAILED INSPECTION OF AFT AVIONICS COMPARTMENT
ACCESS DOOR, INTERNAL STRUCTURE
524131-01-1
822
ACCESS PANELS: 824
LATERAL RIGHT AVIONIC DOOR
AF
DET
DETAILED INSPECTION OF LATERAL RIGHT AVIONICS
COMPARTMENT ACCESS DOOR, INTERNAL STRUCTURE
1
524114-200-001
SOURCE:
MRB 524121-01-1
1
524113-200-001
SOURCE:
MRB 524131-01-1
PREPARATION: LINING REMOVED; INSULATION REMOVED;
524141-01-1
812
ACCESS PANELS: 822
LATERAL LEFT AVIONIC DOOR
AF
DET
DETAILED INSPECTION OF LATERAL LEFT AVIONICS
COMPARTMENT ACCESS DOOR, INTERNAL STRUCTURE
1
524112-200-001
SOURCE:
MRB 524141-01-1
PREPARATION: LINING REMOVED; INSULATION REMOVED;
525111-01-1
525111-02-1
525111-04-1
525111-05-1
220
ACCESS PANELS: 812
COCKPIT DOOR
220
DETAILED INSPECTION OF MECHANICAL PARTS OF DOOR
LOCKING SYSTEMS
COCKPIT DOOR
220
OPERATIONAL CHECK OF ALL PRESSURE SENSING CHANNELS
FOR RAPID DECOMPRESSION.
COCKPIT DOOR
220
OPERATIONAL CHECK OF DOOR OPENING IN CASE OF
POWER OFF.
COCKPIT DOOR
OPERATIONAL CHECK OF DOOR OPENING BY USING THE
EMERGENCY CODE.
AF
AF
AF
AF
DET
OPC
OPC
OPC
SOURCE:
MRB 52.51.11/02
Sub 2 - Page 92 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
525111-06-1
ZONE
220
DESCRIPTION
COCKPIT DOOR
SKILL TASK
CODE CODE
INTERVALS
SOURCE
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
AF
FNC
I:
20 MO
SIL
525100-720-003
SIL 52-061
1
3.00
AF
OPC
I:
12000 FH
OR
80 MO
I:
72 MO
MRB 9
LUR
525100-710-008
1
0.05
0649 1130
1200 1379
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
2151 2163
MRB 9
SOURCE:
MRB 52.51.11/04
525100-710-010
1
0.13
ALL
I:
7500 FH
OR
40 MO
MRB 9
SOURCE:
MRB 52.51.11/05
527100-710-001
1
0.05
ALL
I:
18 MO
MRB 9
0.05
0.05
0.05
0.05
ALL
SOURCE:
MRB 52.71.00/02
1
1
1
1
527300-710-003
1
0.10
ALL
FUNCTIONAL CHECK OF THE CORRECT ADJUSTMENT OF THE
COCKPIT DOOR, ELECTRICAL RELEASE STRIKES AND LATCH
MECHANISM
525111-07-1
220
COCKPIT DOOR
OPERATIONAL CHECK OF DEADBOLT
525111-08-1
220
COCKPIT DOOR
AF
OPC
OPERATIONAL CHECK OF MANUAL RELEASE OF PIP-PINS
527100-01-1
210
DOOR WARNING
EL
OPC
OPERATIONAL CHECK OF DOOR WARNING SYSTEM
527100-02-1
831
832
841
842
NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED
PASSENGER/CREW DOORS / EMERGENCY EXITS
DOOR WARNING
AF
LUB
SOURCE:
MRB 52.71.00/01
LUBRICATION OF DOOR WARNING PROXIMITY SWITCH ACTUATING
MECHANISM
122252-640-005
NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW
DOORS
527300-01-1
210
ACCESS PANELS: 831, 841, 832, 842
EMERGENCY ESCAPE SLIDE RELEASE AND
OVERPRESSURE WARNING SYSTEMS
OPERATIONAL CHECK OF EMERGENCY ESCAPE SLIDE RELEASE
WARNING
EL
OPC
I:
7500 FH
OR
40 MO
MRB 9
SOURCE:
MRB 52.73.00/01
NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED
PASSENGER/CREW DOORS / EMERGENCY EXITS
Sub 2 - Page 93 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
527300-02-1
ZONE
122
DESCRIPTION
EMERGENCY ESCAPE SLIDE RELEASE AND
OVERPRESSURE WARNING SYSTEMS
SKILL TASK
CODE CODE
AF
FNC
OPERATIONAL CHECK OF RESIDUAL CABIN PRESSURE WARNING
AND FUNCTIONAL CHECK OF DIFFERENTIAL PRESSURE SWITCH
INTERVALS
SOURCE
I:
18000 FC
OR
80 MO
MRB 9
T:
6 YE
I:
6 YE
MRB CPCP
T:
18800 FC
I:
3600 FC
MRB
T:
49100 FC
I:
2800 FC
ALI
T:
6 YE
I:
6 YE
MRB CPCP
TPS
REFERENCES
527300-720-003
MEN
TASKM. APPLICABI
H.
LITY
1
0.10
ALL
1
1
0.15
0.15
ALL
1
1
1.00
1.00
ALL
1
1
0.15
0.15
ALL
1
1
0.15
0.15
ALL
SOURCE:
MRB 52.73.00/02
NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED
PASSENGER/CREW DOORS
528101-01-1
734
744
ACCESS PANELS: 811
MLG DOOR FWD AND AFT FITTING
AF
DET
DETAILED INSPECTION OF MLG DOOR, FORWARD AND AFT
FITTINGS, LH/RH
528106-01-1
734
744
ACCESS PANELS: 734, 744
MAIN GEAR DOORS
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC & US) OF MLG DOOR ACTUATOR LUGS,
LH/RH
1
528100-200-001
SOURCE:
MRB 528101-01-1
528100-280-801
NTM 52-81-06
SOURCE:
MRB 528106-01-1
NOTE: FOR PRE 24903 AIRCRAFT RETROFITTED, THRESHOLD IS TO BE
COUNTED FROM SB 52-1073 EMBODIMENT
PREPARATION: ACTUATOR REMOVED;
528107-01-1
730
740
ACCESS PANELS: 734, 744
MAIN GEAR DOORS
AF
GVI
GENERAL VISUAL INSPECTION OF MLG DOOR FWD FITTING JOINT TO HINGE
FITTING, LH/RH
528100-210-801
SOURCE:
ALI 528107-01-1
NOTE: FOR PRE 24428 OR PRE 24903 AIRCRAFT RETROFITTED, THRESHOLD IS
TO BE COUNTED FROM SB 52-1058 OR SB 52-1073 EMBODIMENT
ACCESS PANELS: 734, 744
528211-01-1
713
714
NLG MAIN DOOR HINGES
DETAILED INSPECTION OF NLG, MAIN DOOR HINGES, LH/RH
AF
DET
1
528200-200-001
SOURCE:
MRB 528211-01-1
ACCESS PANELS: 713, 714
Sub 2 - Page 94 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
528221-01-1
ZONE
715
716
DESCRIPTION
NLG SECONDARY DOOR HINGES
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF NLG, SECONDARY DOOR HINGES,
LH/RH
528223-01-1
715
716
ACCESS PANELS: 715, 716
NOSE GEAR DOORS
AF
DET
DETAILED INSPECTION OF NLG AFT DOOR AFT FITTINGS, LH/RH
530000-01-1
531101-01-1
100
ACCESS PANELS: 715, 716
FUSELAGE DRAINAGE
220
REMOVE AND DETAILED INSPECTION OF PISTON TYPE DRAIN
VALVES IN LOWER FUSELAGE SHELL
FWD PAX/CREW DOOR
AF
AF
DET
DET
DETAILED INSPECTION OF FWD PASSENGER/CREW DOOR
CUTOUT, INTERCOSTALS FITTINGS N°7 BETWEEN FR15-16
AND FR20-21, LH/RH
INTERVALS
SOURCE
T:
6 YE
I:
6 YE
MRB CPCP
T:
26000 FC
I:
7500 FC
MRB
I:
6 YE
MRB 9
T:
36500 FC
I:
3800 FC
ALI
T:
6 YE
OR
22000 FC
I:
6 YE
OR
13600 FC
ST:
30000 FC
SI:
16800 FC
T:
48000 FC
I:
16800 FC
ALI
MRB CPCP
TPS
1
REFERENCES
528200-200-002
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.15
0.15
ALL
1
1
0.17
0.17
ALL
530000-210-001
1
0.40
ALL
SOURCE:
MRB 53.19.00/03
531100-220-802
1
0.40
ALL
1
0.30
ALL
1
1
0.93
0.93
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
MRB 528221-01-1
528200-220-801
SOURCE:
MRB 528223-01-1
SOURCE:
ALI 531101-01-1
PREPARATION: CEILING PANELS REMOVED; INSULATION REMOVED; LINING
REMOVED;
531102-01-1
220
ACCESS PANELS: 831, 841
FWD PAX/CREW DOOR
AF
DET
DETAILED INSPECTION OF FORWARD PASSENGER/CREW DOOR
FRAME, UPPER CORNERS, EXTERNAL SURFACE, LH/RH
ACCESS PANELS: 831, 841
531103-01-1
221
222
MAIN STRUCTURE
SPECIAL DETAILED INSPECTION (ROTO) OF FWD PASSENGER/CREW DOOR
CUTOUT, STOP FITTINGS HOLES ON THE FR20, LH/RH
NOTE: 100% THRESHOLD/INTERVAL ONLY FOR AIRCRAFT A320-200 PRE
160000.
NDT
SDI
531100-210-001
SOURCE:
ALI 531102-01-1
MRB 531102-01-1
ALI
MRB
531100-210-819
NTM 53-11-03
SOURCE:
ALI 531103-01-1
MRB 531103-01-1
PREPARATION: INSULATION REMOVED; LINING REMOVED; CEILLING PANELS
REMOVED; STOP FITTING BOLT REMOVED; GALLEY & TOILET IF INSTALLED;
ACCESS PANELS: 831, 841
Sub 2 - Page 95 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
531104-01-1
ZONE
220
DESCRIPTION
DOOR FRAME FWD LOWER CORNER
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF FORWARD PASSENGER/CREW DOOR
FRAME, FORWARD LOWER CORNER UNDERNEATH THE SCUFF
PLATE, LH/RH
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531104-02-1
531104-02-1
220
PREPARATION: FWD CORNER SCUFF PLATE REMOVED;
DOOR FRAME EXTERNAL SURFACE
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF FORWARD
PASSENGER/CREW DOOR FRAME, FORWARD LOWER CORNER
UNDERNEATH THE SCUFF PLATES, LH/RH
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531104-01-1
531105-01-1
211
212
PREPARATION: FWD CORNER SCUFF PLATE REMOVED;
MAIN STRUCTURE
AF
DET
DETAILED INSPECTION OF LATERAL WINDOW FRAME STIFFENER, UPPER
AREA, LH/RH
NOTE: THIS TASK IS AN ALTERNATIVE INSPECTION TO TASK 531105-02-1
100% THRESHOLD/INTERVAL APPLY ONLY TO AIRCRAFT A320-200 PRE 160000.
PREPARATION: SLIDING WINDOW OPENED;
531105-02-1
211
212
MAIN STRUCTURE
SPECIAL DETAILED INSPECTION (HFEC) OF LATERAL WINDOW FRAME
STIFFENER, UPPER AREA, LH/RH
NOTE: THIS TASK IS AN ALTERNATIVE INSPECTION TO TASK 531105-01-1
100% THRESHOLD/INTERVAL APPLY ONLY TO AIRCRAFT A320-200 PRE 160000.
PREPARATION: SLIDING WINDOW OPENED;
NDT
SDI
INTERVALS
SOURCE
ST:
48000 FC
OR
96000 FH
SI:
8000 FC
OR
16000 FH
MRB
ST:
48000 FC
OR
96000 FH
SI:
16100 FC
OR
32200 FH
MRB
ST:
30000 FC
SI:
800 FC
T:
48000 FC
NOTE
I:
800 FC
NOTE
ALI
MRB
ST:
30000 FC
SI:
1600 FC
T:
48000 FC
NOTE
I:
1600 FC
NOTE
ALI
MRB
TPS
REFERENCES
531100-210-002
MEN
TASKM. APPLICABI
H.
LITY
1
0.20
ALL
1
0.50
ALL
1
1
0.30
0.30
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.50
0.50
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
MRB 531104-01-1
531100-210-028
NTM 53-11-04
SOURCE:
MRB 531104-02-1
531100-220-806
SOURCE:
ALI 531105-01-1
MRB 531105-01-1
531100-220-809
NTM 53-11-05
SOURCE:
ALI 531105-02-1
MRB 531105-02-1
Sub 2 - Page 96 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
531107-01-1
ZONE
110
DESCRIPTION
FWD PRESSURE BULKHEAD
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF FORWARD FACE OF PRESSURE
BULKHEAD, VERTICAL ANGLE (Y=675) AT CROSSING AREAS
WITH HORIZONTAL STIFFENERS (Z=1 AND Z=1329), LH/RH
INTERVALS
SOURCE
ST:
30000 FC
SI:
20000 FC
MRB
ST:
30000 FC
OR
60000 FH
SI:
17200 FC
OR
34400 FH
T:
48000 FC
OR
96000 FH
NOTE
I:
17200 FC
OR
34400 FH
NOTE
ST:
30000 FC
OR
60000 FH
SI:
14400 FC
OR
28900 FH
T:
38900 FC
OR
77900 FH
I:
14400 FC
OR
28900 FH
T:
1500 FC
I:
1500 FC
ALI
MRB
TPS
REFERENCES
531100-210-003
MEN
TASKM. APPLICABI
H.
LITY
1
0.20
ALL
1
0.37
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.13
0.13
ALL
1
0.20
ALL
SOURCE:
MRB 531107-01-1
PREPARATION: UPPER PROTECTIVE SHIELD;
531108-01-1
123
ACCESS PANELS: 110AL
MAIN STRUCTURE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTO) OF HOLES AT FWD CORNERS OF NLG
BAY, FR9
NOTE: 100% THRESHOLD/INTERVAL APPLY ONLY TO AIRCRAFT A320-200 PRE
160000
PREPARATION: BOLTS REMOVED;
ACCESS PANELS: 713, 714
531110-01-2
125
126
NOSE FORWARD FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTO) OF CROSSBEAM SPLICING, FR16 AND
FR20, LH/RH
PREPARATION: BOLTS REMOVED; INSULATION REMOVED;
AIR CONDITIONING DUCTS REMOVED;
ACCESS PANELS: 812, 824
531111-01-1
100
AVIONICS DOORS SURROUND
GENERAL VISUAL INSPECTION OF AVIONICS COMPARTMENT
DOORS, SURROUND CORNERS, EXTERNAL SURFACE (4 DOORS)
AF
GVI
531100-220-804
NTM 53-11-08
SOURCE:
ALI 531108-01-1
MRB 531108-01-1
ALI
MRB
531100-220-803
NTM 53-11-10
SOURCE:
ALI 531110-01-2
MRB 531110-01-2
ALI
531100-210-809
SOURCE:
ALI 531111-01-1
Sub 2 - Page 97 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
531112-01-1
ZONE
100
DESCRIPTION
FUSELAGE LOWER PANEL EXTERNAL SURFACE
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF FUSELAGE LOWER PANEL AT NLG
BAY AFT CORNERS, EXTERNAL SURFACE, LH/RH
531113-01-1
531114-01-1
531117-01-1
531118-01-1
200
FUSELAGE SKIN ATTACHMENT
200
GENERAL VISUAL INSPECTION OF ATTACHMENT TO SKIN PANEL, FR16, STG 3
LH/RH
FUSELAGE SKIN EXTERNAL SURFACE
200
DETAILED INSPECTION OF FUSELAGE SKIN ABOVE
WINDSHIELD, BETWEEN FR 4 AND FR 12, EXTERNAL SURFACE,
LH/RH
FUSELAGE SIDE PANEL
200
GENERAL VISUAL INSPECTION OF FUSELAGE SIDE PANEL,
BELOW COCKPIT SIDE WINDOWS, BETWEEN FR 1 AND FR 12,
EXTERNAL SURFACE, LH/RH
FUSELAGE SIDE PANEL
AF
AF
AF
AF
GVI
DET
GVI
GVI
GENERAL VISUAL INSPECTION OF AREA FORWARD OF
WINDSHIELD, ABOVE SIDE PANEL, FROM FR 0 TO FR
4, EXTERNAL SURFACE, LH/RH
531119-01-1
100
NOTE:
THRESHOLD BASED ON EASA AD 2010-0071 ISSUE DATE (MAR
15/10)
LOWER LAP JOINT EXTERNAL SURFACE
AF
DET
DETAILED INSPECTION OF UPPER SKIN OF LOWER LONGITUDINAL LAP JOINT,
BETWEEN FR 9 AND FR 20, EXTERNAL SURFACE, LH/RH
NOTE: 100% THRESHOLD/INTERVAL NOT APPLICABLE TO A321-100 POST
30748.
531119-01-2
100
LOWER LAP JOINT EXTERNAL SURFACE
DETAILED INSPECTION OF UPPER SKIN OF LOWER
LONGITUDINAL LAP JOINT, BETWEEN FR 9 AND FR 20,
EXTERNAL SURFACE, LH/RH
AF
DET
INTERVALS
SOURCE
T:
16300 FC
OR
32600 FH
I:
16300 FC
OR
32600 FH
T:
41400 FC
I:
7400 FC
T:
5700 FC
I:
5700 FC
ALI
T:
14500 FC
I:
14500 FC
ALI
T:
100 DY
NOTE
I:
4300 FC
ALI
ST:
30000 FC
SI:
12600 FC
T:
41000 FC
I:
12600 FC
ST:
30000 FC
SI:
11700 FC
T:
35300 FC
I:
11700 FC
ALI
MRB
TPS
REFERENCES
531100-210-005
MEN
TASKM. APPLICABI
H.
LITY
1
0.30
ALL
SOURCE:
ALI 531112-01-1
ALI
531100-210-818
1
0.25
ALL
ALI
SOURCE:
ALI 531113-01-1
531100-210-006
1
0.50
ALL
1
0.10
ALL
1
0.25
ALL
1
0.60
0649 1130
1200 1379
1488
1
0.60
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
SOURCE:
ALI 531114-01-1
531100-210-810
SOURCE:
ALI 531117-01-1
531100-210-811
SOURCE:
ALI 531118-01-1
531100-210-007
SOURCE:
ALI 531119-01-1
MRB 531119-01-1
ALI
MRB
531100-210-007
SOURCE:
ALI 531119-01-2
MRB 531119-01-2
Sub 2 - Page 98 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
531120-01-1
531121-01-1
531123-01-1
ZONE
DESCRIPTION
200
UPPER LAP JOINT EXTERNAL SURFACE
100
DETAILED INSPECTION OF UPPER SKIN OF UPPER
LONGITUDINAL LAP JOINT, BETWEEN FR 15 AND FR 16 AND
FR 20 AND FR 24, EXTERNAL SURFACE, LH/RH
LAT LAP JOINT FR 11-14, FR 20-24
100
DETAILED INSPECTION OF OUTER SKIN OF LATERAL
LONGITUDINAL LAP JOINT, BETWEEN FR 11 AND FR 14 AND
FR 20 AND FR 24, LH/RH
LAT LAP JOINT FR 01-24
SKILL TASK
CODE CODE
AF
AF
AF
DET
DET
DET
DETAILED INSPECTION OF OUTER SKIN OF LATERAL
LONGITUDINAL LAP JOINT, BETWEEN FR 1 AND FR 24, LH/RH
531124-01-1
127
128
SPLICE AT FR 20
AF
DET
DETAILED INSPECTION OF FR 20 SPLICE, BETWEEN STRINGER
30 AND STRINGER 32, LH/RH
PREPARATION: INSULATION DISPLACED;
531124-01-2
127
128
ACCESS PANELS: 824
SPLICE AT FR 20
AF
DET
DETAILED INSPECTION OF FR 20 SPLICE, BETWEEN STRINGER
30 AND STRINGER 32, LH/RH
INTERVALS
SOURCE
ST:
30000 FC
SI:
18500 FC
MRB
ST:
30000 FC
SI:
16600 FC
MRB
ST:
6 YE
SI:
6 YE
T:
24 YE
I:
6 YE
ST:
30000 FC
SI:
8300 FC
T:
35600 FC
I:
8300 FC
T:
33600 FC
I:
7900 FC
MRB CPCP
ST:
33000 FC
SI:
29800 FC
MRB
TPS
REFERENCES
531100-210-008
MEN
TASKM. APPLICABI
H.
LITY
1
0.30
ALL
1
0.30
ALL
1
1.00
ALL
1
1
0.15
0.15
0649 1130
1200 1379
1488
1
1
0.15
0.15
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
1
1
0.17
0.17
ALL
SOURCE:
MRB 531120-01-1
531100-210-009
SOURCE:
MRB 531121-01-1
531100-210-010
SOURCE:
MRB 531123-01-1
ALI
MRB
531100-210-011
SOURCE:
ALI 531124-01-1
MRB 531124-01-1
ALI
531100-210-011
SOURCE:
ALI 531124-01-2
PREPARATION: INSULATION DISPLACED;
531125-02-1
211
212
ACCESS PANELS: 824
NOSE FORWARD FUSELAGE
DETAILED INSPECTION OF CENTRAL/LATERAL WINDOW FRAME AROUND
FASTENER HOLE, UPPER AREA, LH/RH
AF
DET
531100-220-805
SOURCE:
MRB 531125-02-1
PREPARATION: SLIDING WINDOW OPENED;
Sub 2 - Page 99 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
531127-01-1
ZONE
211
212
DESCRIPTION
MAIN STRUCTURE
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF LATERAL SPLICING, FR11, LH/RH
PREPARATION: INSULATION REMOVED; LINING REMOVED;
531129-02-2
211
212
WINDSHIELD CTR POST LWR ATTACHMENT
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF WINDSHIELD CENTER POST,
LOWER ATTACHMENT AREA, INTERNAL SIDE
PREPARATION: LH/RH WINDSHIELDS REMOVED;
DISPLAY UNIT 4WT1 REMOVED;
ANCHOR NUT SHIMS REMOVED;
531129-02-3
211
212
ACCESS PANELS: 211LW, 211MW
WINDSHIELD CTR POST LWR ATTACHMENT
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF WINDSHIELD CENTER POST,
LOWER ATTACHMENT AREA, INTERNAL SIDE
INTERVALS
SOURCE
ST:
30000 FC
SI:
9900 FC
T:
42400 FC
I:
9900 FC
ST:
30000 FC
SI:
9500 FC
T:
36600 FC
I:
9500 FC
ALI
MRB
T:
34600 FC
I:
9000 FC
ALI
ST:
30000 FC
SI:
13800 FC
T:
48000 FC
I:
13800 FC
ST:
30000 FC
SI:
20000 FC
ALI
MRB
TPS
REFERENCES
531100-220-807
NTM 53-11-27
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.28
0.28
ALL
1
1
0.50
0.50
0649 1130
1200 1379
1488
1
1
0.50
0.50
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
1
1
0.15
0.15
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.20
0.20
ALL
SOURCE:
ALI 531127-01-1
MRB 531127-01-1
ALI
MRB
531100-220-001
NTM 53-11-29
SOURCE:
ALI 531129-02-2
MRB 531129-02-2
531100-220-001
NTM 53-11-29
SOURCE:
ALI 531129-02-3
PREPARATION: LH/RH WINDSHIELDS REMOVED;
DISPLAY UNIT 4WT1 REMOVED;
ANCHOR NUT SHIMS REMOVED;
531130-02-1
211
212
ACCESS PANELS: 211LW, 211MW
NOSE FORWARD FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF LATERAL FORWARD CORNER OF
SLIDING WINDOW FRAME AT FR4, LH/RH
PREPARATION: SLIDING WINDOW OPENED;
531131-01-1
211
212
ACCESS PANELS: 211NW, 211PW, 212NW, 212PW
WINDSHIELD CTR POST UPR ATTACHMENT
DETAILED INSPECTION OF WINDSHIELD CENTER POST, UPPER
ATTACHMENT AREA, INTERNAL SIDE
AF
DET
531100-220-808
NTM 53-11-30
SOURCE:
ALI 531130-02-1
MRB 531130-02-1
MRB
531100-210-013
SOURCE:
MRB 531131-01-1
ACCESS PANELS: 211LC, 211MC, 211MW, 212LC
Sub 2 - Page 100 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
531133-01-1
ZONE
211
212
DESCRIPTION
WINDSHIELD SIDE POST LWR ATTACHMENT
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF WINDSHIELD SIDE POST AT FR 4,
LOWER ATTACHMENT, INTERNAL SIDE, LH/RH
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531133-02-1
INTERVALS
SOURCE
T:
26700 FC
I:
2700 FC
ALI
T:
26700 FC
I:
5700 FC
ALI
T:
28800 FC
I:
11500 FC
ALI
T:
28800 FC
I:
11000 FC
ALI
ST:
30000 FC
SI:
9200 FC
MRB
TPS
REFERENCES
531100-210-014
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
ALL
1
1
0.50
0.50
ALL
1
1
0.50
0.50
0649 1130
1200 1379
1488
1
1
0.50
0.50
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
1
0.20
ALL
SOURCE:
ALI 531133-01-1
PREPARATION: SLIDING WINDOW OPENED;
531133-02-1
211
212
ACCESS PANELS: 211NW, 211PW, 212NW, 212PW
WINDSHIELD SIDE POST LWR ATTACHMENT
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF WINDSHIELD SIDE
POST AT FR 4, LOWER ATTACHMENT, INTERNAL SIDE, LH/RH
531100-210-029
NTM 53-11-33
SOURCE:
ALI 531133-02-1
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531133-01-1
PREPARATION: SLIDING WINDOW OPENED;
531135-01-1
211
212
ACCESS PANELS: 211NW, 211PW, 212NW, 212PW
WINDSHIELD SIDE POST UPR ATTACHMENT
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTO) OF WINDSHIELD SIDE
POST AT FR 4, UPPER ATTACHMENT, INTERNAL SIDE, LH/RH
531100-210-026
NTM 53-11-35
SOURCE:
ALI 531135-01-1
PREPARATION: BOLTS REMOVED; SLIDING WINDOW OPENED;
ACCESS PANELS: 211BC, 211KC, 211LC, 211NW, 212BC, 212KC, 212LC, 212NW
531135-01-2
211
212
WINDSHIELD SIDE POST UPR ATTACHMENT
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTO) OF WINDSHIELD SIDE
POST AT FR 4, UPPER ATTACHMENT, INTERNAL SIDE, LH/RH
531100-210-026
NTM 53-11-35
SOURCE:
ALI 531135-01-2
PREPARATION: BOLTS REMOVED; SLIDING WINDOW OPENED;
ACCESS PANELS: 211BC, 211KC, 211LC, 211NW, 212BC, 212KC, 212LC, 212NW
531141-01-1
200
SIDE WINDOW STRUCTURE
DETAILED INSPECTION OF SIDE WINDOW STRUCTURE, UPPER
JUNCTION, BETWEEN FORWARD AND REAR FR, EXTERNAL
SURFACE, LH/RH
AF
DET
531100-210-015
SOURCE:
MRB 531141-01-1
Sub 2 - Page 101 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
531151-01-1
ZONE
221
222
DESCRIPTION
DOOR STOP FITTINGS
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF DOOR STOP FITTINGS ON FR 16
AND FR 20, LH/RH
INTERVALS
SOURCE
T:
12 YE
I:
12 YE
MRB CPCP
ST:
30000 FC
SI:
17700 FC
MRB
T:
27700 FC
I:
10300 FC
ALI
T:
24000 FC
I:
7300 FC
ALI
T:
24000 FC
I:
7000 FC
ALI
TPS
REFERENCES
531100-210-017
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.40
0.40
ALL
1
1
1.00
1.00
ALL
1
1
1.00
1.00
ALL
1
1
0.75
0.75
0649 1130
1200 1379
1488
1
1
0.75
0.75
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
SOURCE:
MRB 531151-01-1
PREPARATION: LINING REMOVED;
531153-02-1
221
222
ACCESS PANELS: 831, 841
DOOR STOPS AT FR 16
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF DOOR FR 16, AT
DOUBLE JOGGLE AREA IN OUTER FLANGE OF FR, AT DOOR
STOPS NUMBER 1 AND 7 LOCATION, LH/RH.
531100-210-025
NTM 53-11-53
SOURCE:
MRB 531153-02-1
PREPARATION: BOLTS REMOVED; LINING REMOVED; INSULATION REMOVED;
ACCESS PANELS: 831, 841
531155-02-1
221
222
DOOR STOPS AT FR 20
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC AND ROTO) OF DOOR
FR 20, AT DOUBLE JOGGLE AREA IN OUTER FLANGE OF FR,
AT DOOR STOPS NUMBER 1 AND 7 LOCATION, LH/RH
531100-210-027
NTM 53-11-55
SOURCE:
ALI 531155-02-1
PREPARATION: BOLTS REMOVED; LINING REMOVED; INSULATION REMOVED;
ACCESS PANELS: 831, 841
531157-01-1
127
128
CONTINUITY AND ANGLE FITTINGS
AF
DET
DETAILED INSPECTION OF CONTINUITY FITTING BETWEEN FR
20 AND FR 21, AND ANGLE FITTING, BOTH SIDES OF FR 21,
AT STRINGER 41 LOCATION, LH/RH
531100-210-021
SOURCE:
ALI 531157-01-1
PREPARATION: FLOOR PANELS REMOVED; LADDER;
531157-01-2
127
128
ACCESS PANELS: 824
CONTINUITY AND ANGLE FITTINGS
DETAILED INSPECTION OF CONTINUITY FITTING BETWEEN FR
20 AND FR 21, AND ANGLE FITTING, BOTH SIDES OF FR 21,
AT STRINGER 41 LOCATION, LH/RH
AF
DET
531100-210-021
SOURCE:
ALI 531157-01-2
PREPARATION: FLOOR PANELS REMOVED; LADDER;
ACCESS PANELS: 824
Sub 2 - Page 102 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
531161-01-1
ZONE
123
DESCRIPTION
NLG BAY ALL PANELS
SKILL TASK
CODE CODE
AF
GVI
GENERAL VISUAL INSPECTION OF NLG BAY, ALL PANELS,
LH/RH
531162-01-1
127
128
ACCESS PANELS: 713, 714
NLG BAY
AF
DET
DETAILED INSPECTION OF NLG BAY, REAR PANEL AFT FACE,
LOWER CORNERS, LH/RH
PREPARATION: LADDER REMOVED; FLOOR PANEL REMOVED;
ACCESS PANELS: 824
531162-01-2
127
128
NLG BAY
AF
DET
DETAILED INSPECTION OF NLG BAY, REAR PANEL AFT FACE,
LOWER CORNERS, LH/RH
PREPARATION: LADDER REMOVED; FLOOR PANEL REMOVED;
ACCESS PANELS: 824
531163-01-1
221
222
FWD PAX/CREW DOOR SURROUND
DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND
FORWARD PASSENGER/CREW DOOR, ABOVE CABIN FLOOR LEVEL,
BETWEEN FR 15 AND FR 21 AND BETWEEN STRINGER 8 AND
STRINGER 23, LH/RH, EXCLUDING THE LOWER CORNERS OF
THE DOOR ENTRANCE AREA AT FR 16 AND FR 20, BETWEEN
STRINGER 22 AND 23, LH/RH
AF
DET
INTERVALS
SOURCE
T:
6 YE
I:
6 YE
MRB CPCP
ST:
30000 FC
OR
60000 FH
SI:
20000 FC
OR
40000 FH
MRB
ST:
30000 FC
OR
60000 FH
SI:
19100 FC
OR
38300 FH
MRB
T:
6 YE
I:
6 YE
MRB CPCP
TPS
1
REFERENCES
531100-210-803
MEN
TASKM. APPLICABI
H.
LITY
1
0.20
ALL
1
1
0.45
0.45
0649 1130
1200 1379
1488
1
1
0.45
0.45
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
1
1
0.80
0.80
ALL
SOURCE:
MRB 531161-01-1
531100-210-018
SOURCE:
MRB 531162-01-1
531100-210-018
SOURCE:
MRB 531162-01-2
1
531100-210-019
SOURCE:
MRB 531163-01-1
NOTE: EXCLUDED AREA COVERED BY TASKS 531166-01-1 AND
531166-01-2
PREPARATION: CEILING PANELS REMOVED; LINING REMOVED; INSULATION
REMOVED;
ACCESS PANELS: 831, 841
Sub 2 - Page 103 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
531164-01-1
ZONE
125
126
DESCRIPTION
FUSELAGE FR 15-21
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
BELOW FORWARD PASSENGER/CREW DOOR AND CABIN FLOOR
LEVEL, FROM FR 15 TO FR 21 AND BETWEEN STRINGER 28 LH
AND STRINGER 28 RH.
INTERVALS
SOURCE
T:
6 YE
I:
6 YE
MRB CPCP
T:
5 YE
I:
5 YE
MRB CPCP
T:
6 YE
I:
6 YE
MRB CPCP
T:
6 YE
I:
6 YE
MRB CPCP
T:
6 YE
I:
6 YE
MRB CPCP
TPS
1
REFERENCES
531100-210-801
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.50
0.50
ALL
1
1
0.80
0.80
0649
1
1
0.80
0.80
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
1
0.20
ALL
1
1
1.50
1.50
ALL
SOURCE:
MRB 531164-01-1
PREPARATION: INSULATION REMOVED;
531166-01-1
221
222
ACCESS PANELS: 812, 824
FUSELAGE FR 16-20
AF
DET
DETAILED INSPECTION OF FWD PASSENGER/CREW DOOR CUTOUT
LOWER CORNERS INTERNAL STRUCTURE ABOVE CABIN FLOOR
LEVEL, AT FR 16 AND FR 20 FROM STRINGER 22 TO
STRINGER 23 AND AROUND GIRT BAR FITTINGS, LH/RH.
1+2 531100-220-006
SOURCE:
MRB 531166-01-1
PREPARATION: GIRT BAR FITTING REMOVED; BLANKING PLATE REMOVED;
531166-01-2
221
222
ACCESS PANELS: 831, 841
FUSELAGE FR 16-20
AF
DET
DETAILED INSPECTION OF FWD PASSENGER/CREW DOOR CUTOUT
LOWER CORNERS INTERNAL STRUCTURE ABOVE CABIN FLOOR
LEVEL, AT FR 16 AND FR 20 FROM STRINGER 22 TO
STRINGER 23 AND AROUND GIRT BAR FITTINGS, LH/RH.
1+2 531100-220-006
SOURCE:
MRB 531166-01-2
PREPARATION: GIRT BAR FITTING REMOVED; BLANKING PLATE REMOVED;
531167-01-1
126
ACCESS PANELS: 831, 841
AREA BELOW BATTERIES
AF
DET
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
BELOW BATTERIES, BETWEEN FR 10 AND FR 16, RH
531169-01-1
125
126
ACCESS PANELS: 822
FUSELAGE FR 12-15
GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL
STRUCTURE, BELOW GALLEY AND TOILET, BETWEEN FR 12 AND
FR 15 AND BETWEEN STRINGER 23 LH AND STRINGER 23 RH
AF
GVI
1
531100-210-036
SOURCE:
MRB 531167-01-1
1
531100-210-804
SOURCE:
MRB 531169-01-1
PREPARATION: INSULATION REMOVED;
ACCESS PANELS: 812, 822
Sub 2 - Page 104 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
531170-01-1
ZONE
200
DESCRIPTION
COCKPIT WINDSHIELD LOWER FRONT FTG
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF COCKPIT WINDSHIELD, LOWER FRONT FITTING AT
FR 4, LOWER ATTACHMENT, EXTERNAL SURFACE, LH/RH
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531170-02-1
100% THRESHOLD/INTERVAL IS NOT APPLICABLE TO A321-100 POST 30748.
531170-01-2
200
PREPARATION: LOWER RETAINERS;
COCKPIT WINDSHIELD LOWER FRONT FTG
AF
DET
DETAILED INSPECTION OF COCKPIT WINDSHIELD, LOWER FRONT FITTING AT
FR 4, LOWER ATTACHMENT, EXTERNAL SURFACE, LH/RH
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531170-02-2
531170-02-1
200
PREPARATION: LOWER RETAINERS;
COCKPIT WINDSHIELD LOWER FRONT FTG
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF COCKPIT WINDSHIELD, LOWER
FRONT FITTING AT FR 4, LOWER ATTACHMENT, EXTERNAL SURFACE, LH/RH
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531170-01-1.
100% THRESHOLD/INTERVAL IS NOT APPLICABLE TO A321-100 POST 30748.
INTERVALS
SOURCE
ST:
30000 FC
SI:
5700 FC
T:
36700 FC
I:
5700 FC
ALI
MRB
ST:
30000 FC
SI:
5500 FC
T:
36700 FC
I:
5500 FC
ST:
30000 FC
SI:
15600 FC
T:
36700 FC
I:
15600 FC
ALI
MRB
ST:
30000 FC
SI:
15000 FC
T:
36700 FC
I:
15000 FC
ALI
MRB
T:
6 YE
I:
6 YE
MRB CPCP
ST:
30000 FC
SI:
14000 FC
MRB
TPS
REFERENCES
531100-210-038
MEN
TASKM. APPLICABI
H.
LITY
1
0.30
0649 1130
1200 1379
1488
1
0.30
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
1
1.00
0649 1130
1200 1379
1488
1
1.00
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
1
1
0.20
0.20
ALL
1
0.50
ALL
SOURCE:
ALI 531170-01-1
MRB 531170-01-1
531100-210-038
SOURCE:
ALI 531170-01-2
MRB 531170-01-2
ALI
MRB
531100-210-039
NTM 53-11-70
SOURCE:
ALI 531170-02-1
MRB 531170-02-1
PREPARATION: LOWER RETAINERS;
531170-02-2
200
COCKPIT WINDSHIELD LOWER FRONT FTG
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF COCKPIT
WINDSHIELD, LOWER FRONT FITTING AT FR 4, LOWER
ATTACHMENT, EXTERNAL SURFACE, LH/RH
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK
531170-01-2.
531171-01-1
123
124
PREPARATION: LOWER RETAINERS;
NLG SECONDARY DOOR HINGE SUPPORTS
AF
DET
DETAILED INSPECTION OF NLG, SECONDARY DOOR HINGE
SUPPORTS ON FUSELAGE, LH/RH
531172-01-1
100
ACCESS PANELS: 715, 716
SKIN FR21-23 & FR17-18 FROM STGR 31-36
DETAILED INSPECTION OF FUSELAGE SKIN, BETWEEN FR 21
AND FR 23 LH AND FR 17 AND FR 18 RH, FROM STRINGER 31
TO STRINGER 36
AF
DET
531100-210-039
NTM 53-11-70
SOURCE:
ALI 531170-02-2
MRB 531170-02-2
1
531100-210-020
SOURCE:
MRB 531171-01-1
531100-210-032
SOURCE:
MRB 531172-01-1
Sub 2 - Page 105 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
531175-01-1
ZONE
110
DESCRIPTION
FWD FACE OF FRONT PRESSURE BULKHEAD
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF FORWARD FACE OF FRONT PRESSURE
BULKHEAD ATTACHED TO FR 1
PREPARATION: PROTECTIVE SHIELD;
531176-01-1
531177-01-1
200
ACCESS PANELS: 110AL
COCKPIT SIDE WINDOWS FRAMEWORK
200
DETAILED INSPECTION OF COCKPIT SIDE WINDOWS, EXTERNAL
VISIBLE PORTION OF FRAMEWORK, BETWEEN FR 4 AND FR 12,
LH/RH
COCKPIT WINDSHIELD FRAME
AF
AF
DET
DET
DETAILED INSPECTION OF COCKPIT WINDSHIELD, EXTERNAL
PORTION OF FRAMEWORK COVERED BY RETAINERS
531178-01-1
531180-01-1
200
PREPARATION: WINDSHIELD RETAINERS;
COCKPIT WINDSHIELD RETAINERS
100
DETAILED INSPECTION OF COCKPIT WINDSHIELD, EXTERNAL
VISIBLE PORTION OF RETAINERS
FWD PAX/CREW DOOR UNDER SCUFF-PLATE
AF
AF
DET
DET
DETAILED INSPECTION OF FORWARD PASSENGER/CREW DOOR
CUTOUT, UNDERNEATH THE SCUFF-PLATE, LH/RH
INTERVALS
SOURCE
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
T:
6 YE
I:
6 YE
MRB CPCP
T:
12 YE
I:
12 YE
MRB CPCP
T:
6 YE
I:
6 YE
T:
12 YE
I:
12 YE
MRB CPCP
MRB CPCP
T:
6 YE
I:
6 YE
MRB CPCP
TPS
REFERENCES
531100-210-040
MEN
TASKM. APPLICABI
H.
LITY
1
0.30
ALL
1
0.30
ALL
1
0.30
ALL
531100-210-043
1
0.30
ALL
SOURCE:
MRB 531178-01-1
531100-210-044
1
0.20
ALL
1
0.30
ALL
SOURCE:
MRB 531175-01-1
MRB CPCP
531100-210-041
SOURCE:
MRB 531176-01-1
NO
531100-210-042
SOURCE:
MRB 531177-01-1
NO
SOURCE:
MRB 531180-01-1
PREPARATION: SCUFF PLATES REMOVED;
531181-01-1
129
ACCESS PANELS: 831, 841
FUSELAGE INTL STRUCT FR15-21, STR23-28
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE
AND LOWER SURFACE OF CABIN FLOOR STRUCTURE FROM FR 15
TO FR 21, BETWEEN STRINGER 23 AND STRINGER 28 LH/RH
NOTE: TII TPS MAY BE LIMITED TO LOWER SURFACE OF
CABIN FLOOR STRUCTURE BETWEEN FR15 AND FR21
AF
DET
1+2 531100-210-035
SOURCE:
MRB 531181-01-1
PREPARATION: CABIN FLOOR PANELS REMOVED; STAIRS DEPLOYED (IF
INSTALLED);
ACCESS PANELS: 812, 813, 824
Sub 2 - Page 106 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
531184-01-2
ZONE
211
212
DESCRIPTION
FWD PRESSURE BULKHEAD VERTICAL POSTS
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF CENTRAL AND ADJACENT VERTICAL
POSTS OF FORWARD PRESSURE BULKHEAD AND WEB ASSEMBLY,
UPPER PORTION
INTERVALS
SOURCE
T:
34000 FC
I:
13500 FC
ALI
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
T:
12 YE
I:
12 YE
MRB CPCP
TPS
REFERENCES
531100-210-045
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
ALL
1
1
1
1
1
1
1
1
1
1
1
1
0.08
0.08
0.08
0.08
0.08
0.08
0.08
0.08
0.08
0.08
1.00
1.00
ALL
1
1
1.00
1.00
ALL
1
1
1.50
1.50
ALL
SOURCE:
ALI 531184-01-2
PREPARATION: INSULATION REMOVED;
531185-01-1
531186-01-1
211
212
221
222
223
224
231
232
233
234
211
212
ACCESS PANELS: 811
FUSELAGE INTERNAL STRUCTURE
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL
STRUCTURE, FROM FR 1 TO FR 24, ABOVE CABIN FLOOR
LEVEL, AS FAR AS VISIBLE.
PREPARATION: AIR CONDITIONING DUCTS REMOVED; GALLEYS AND TOILETS
REMOVED; INSULATION DISPLACED; LINING AND CEILING PANELS REMOVED;
AFT FACE OF FWD PRESSURE BULKHEAD
AF
DET
DETAILED INSPECTION OF AFT FACE OF FORWARD PRESSURE
BULKHEAD, ABOVE COCKPIT FLOOR LEVEL, INCLUDING FR 1,
AS FAR AS VISIBLE
PREPARATION: INSULATION DISPLACED; WIRING BUNDLES DISPLACED;
531187-01-1
211
212
ACCESS PANELS: 811
COCKPIT WINDOW FRAMES
AF
DET
DETAILED INSPECTION OF COCKPIT WINDOW FRAMES AND
CLOSING PANELS, INTERNAL STRUCTURE (FR 12 AND
FORWARD).
PREPARATION: INSULATION DISPLACED; LINING REMOVED; ELECTRONIC
DEVICES DISPLACED;
531188-01-1
211
212
ACCESS PANELS: 811
COCKPIT FLOOR STRUCTURE
DETAILED INSPECTION OF COCKPIT FLOOR STRUCTURE,
BETWEEN FR 1 AND FR 12
AF
DET
531100-210-814
SOURCE:
MRB 531185-01-1
531100-210-046
ALL
SOURCE:
MRB 531186-01-1
531100-210-047
SOURCE:
MRB 531187-01-1
1
531100-210-048
SOURCE:
MRB 531188-01-1
PREPARATION: COCKPIT FLOOR PANELS; RUBBER LEVELLING STRIPS;
Sub 2 - Page 107 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
531189-01-1
531189-01-2
531190-01-1
531190-01-2
ZONE
211
212
221
222
231
232
211
212
221
222
231
232
221
222
231
232
221
222
231
232
DESCRIPTION
FLOOR STRUCTURE FR 12 TO 21
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BETWEEN
FR 12 AND FR 21
PREPARATION: CABIN FLOOR PANELS; GALLEYS; TOILET
REMOVAL/INSTALLATION ;
FLOOR STRUCTURE FR 12 TO 21
AF
DET
DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BETWEEN
FR 12 AND FR 21
INTERVALS
SOURCE
T:
5 YE
I:
5 YE
MRB CPCP
T:
6 YE
I:
6 YE
MRB CPCP
T:
10 YE
I:
10 YE
MRB CPCP
T:
12 YE
I:
12 YE
MRB CPCP
T:
12 YE
I:
12 YE
MRB CPCP
TPS
REFERENCES
1+2 531100-210-049
SOURCE:
MRB 531189-01-1
1+2 531100-210-049
SOURCE:
MRB 531189-01-2
PREPARATION: CABIN FLOOR PANELS; GALLEYS; TOILET
REMOVAL/INSTALLATION ;
FLOOR STRUCTURE FR 21 TO FR 24
AF
GVI
GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE,
EXCLUDING AREAS BELOW GALLEYS AND TOILETS, BETWEEN FR
21 AND FR 24
PREPARATION: CABIN FLOOR PANELS;
FLOOR STRUCTURE FR 21 TO FR 24
AF
GVI
GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE,
EXCLUDING AREAS BELOW GALLEYS AND TOILETS, BETWEEN FR
21 AND FR 24
1+2 531100-210-805
SOURCE:
MRB 531190-01-1
1+2 531100-210-805
SOURCE:
MRB 531190-01-2
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
1
1
0.25
0.25
0.25
0.25
0.25
0.25
0649
1
1
1
1
1
1
0.25
0.25
0.25
0.25
0.25
0.25
1
1
1
1
1.20
1.20
1.20
1.20
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
0649
1
1
1
1
1.20
1.20
1.20
1.20
1
1
1.50
1.50
PREPARATION: CABIN FLOOR PANELS;
531191-01-1
121
122
AFT FACE OF FWD PRESSURE BULKHEAD
DETAILED INSPECTION OF AFT FACE OF FORWARD PRESSURE
BULKHEAD, BELOW COCKPIT FLOOR LEVEL, INCLUDING FR 1
AND STRINGER CONNECTIONS.
NOTE: IF CORROSION IS FOUND ON THE PRESSURE BULKHEAD
ABOVE THE AVIONICS FLOOR PANELS THE COMPLETE AFT FACE
(UPPER AND LOWER AREAS) OF THE PRESSURE BULKHEAD IS
TO BE INSPECTED.
AF
DET
1
531100-220-002
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
ALL
SOURCE:
MRB 531191-01-1
PREPARATION: FORWARD AVIONICS BAY FLOOR PANELS REMOVED;
INSULATION DISPLACED; WIRING BUNDLES DISPLACED;
ACCESS PANELS: 811
Sub 2 - Page 108 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
531192-01-1
ZONE
121
122
125
126
DESCRIPTION
FUSELAGE FR 1 TO 12
SKILL TASK
CODE CODE
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL
STRUCTURE AND FLOOR STRUCTURE, INCLUDING NLG BAY
PANELS, BETWEEN FR 1 AND FR 12, BELOW COCKPIT FLOOR
PANELS
NOTE: TPS MAY BE LIMITED TO FUSELAGE INTERNAL
STRUCTURE BETWEEN FR1 AND FR12 AND AFT FACE OF
PRESSURE BULKHEAD, FROM STRINGER 32, LH/RH TO BOTTOM
CENTERLINE
INTERVALS
SOURCE
T:
12 YE
I:
12 YE
MRB CPCP
T:
12 YE
I:
12 YE
MRB CPCP
T:
6 YE
I:
6 YE
MRB CPCP
T:
10000 FC
I:
500 FC
ISB
TPS
1
REFERENCES
531100-210-806
SOURCE:
MRB 531192-01-1
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
1.00
1.00
1.00
1.00
ALL
1
1
0.30
0.30
ALL
1
1
1
1
0.30
0.30
0.30
0.30
1200 1379
1
1
0.50
0.50
0649 2151
2163
PREPARATION: AIR DUCT; FORWARD AVIONICS BAY FLOOR PANELS
REMOVED; INSULATION REMOVED;
531193-01-1
127
128
ACCESS PANELS: 811, 812, 822
FUSELAGE FR 21 TO 24
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL
STRUCTURE AND FLOOR STRUCTURE, INCLUDING NLG BAY AFT
FACE, BETWEEN FR 21 AND FR 24, BELOW CABIN FLOOR
PANELS
NOTE: TPS MAY BE LIMITED TO FUSELAGE INTERNAL
STRUCTURE BETWEEN FR 21 AND FR 24, FROM STRINGER 32,
LH/RH TO BOTTOM CENTERLINE
1
531100-210-807
SOURCE:
MRB 531193-01-1
PREPARATION: AVIONICS BAY FLOOR PANELS REMOVED;
531194-01-2
531197-01-1
221
222
231
232
123
124
ACCESS PANELS: 824
FLOOR STRUCTURE FR 21 TO 24
AF
DET
DETAILED INSPECTION OF CABIN FLOOR STRUCTURE, BELOW AND 0.5M
AROUND GALLEYS AND TOILETS, BETWEEN FR 21 AND FR 24
PREPARATION: CABIN FLOOR PANELS;
GALLEYS;
TOILET
REMOVAL/INSTALLATION
;
NLG BAY
DETAILED INSPECTION OF NOSE LANDING GEAR ACTUATOR FITTING
FASTENERS
AF
DET
1+2 531100-220-003
SOURCE:
MRB 531194-01-2
ISB 53-1180
ACCESS PANELS: 824
Sub 2 - Page 109 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
531257-01-1
ZONE
150
160
DESCRIPTION
TACK HOLES AT FR50-FR63
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF TACK HOLES AT FR50-FR63
BETWEEN P33-P39 (LH ONLY) IN CARGO FLOOR AREA.
531259-01-1
140
ACCESS PANELS: 151AE, 151AG, 151BE, 151BG, 151DE, 151EF, 151FE, 151FF,
151GE, 151HE, 151HF, 151JF, 151MF, 151NF, 151QF, 151RF, 151TF, 151TG, 151UF,
151UG, 161AF, 161BF, 161CF, 161EF, 161FF
TI-ANGLE CONNECTION BETWEEN BELLY FAIRING AND KEEL BEAM SIDE
AF
PANEL
DET
DETAILED INSPECTION OF OF TI-ANGLE CONNECTION BETWEEN BELLY
FAIRING AND KEEL BEAM SIDE PANEL FR41-FR42, RH/LH.
ACCESS PANELS: 147BZ 148AZ
531260-01-1
240
250
SPLICE PLATE OF FR47 BUTT JOINT CROSSING
AREA
NDT
SDI
AF
DET
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTO) OF SPLICE PLATE OF FR47 BUTT
JOINT CROSSING AREA P5-P7 (LH/RH).
ACCESS PANELS: 241FC, 251AC
531269-01-1
240
FRAME FOOT AT FR43
DETAILED INSPECTION OF FRAME FOOT AT FR43 RH/LH.
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531269-02-1.
531269-02-1
240
FRAME FOOT AT FR43
SPECIAL DETAILED INSPECTION OF FRAME FOOT AT FR43 RH/LH.
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531269-01-1.
INTERVALS
T:
38200 FC
OR
76400 FH
I:
5000 FC
OR
10000 FH
T:
30000 FC
OR
60000 FH
I:
5000 FC
OR
10000 FH
T:
30700 FC
OR
61400 FH
I:
14800 FC
OR
29600 FH
T:
40000 FC
OR
80000 FH
I:
10000 FC
OR
20000 FH
T:
40000 FC
OR
80000 FH
I:
20000 FC
OR
40000 FH
SOURCE
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
ISB
ISB 53-1257
1
1
12.00
12.00
ALL
EASA AD
ISB
JIC A320-54-12-00
EASA AD 2013-0122
ISB 53-1259
1
2.00
ALL
ISB
ISB 53-1260
1
1
21.00
21.00
1130 1200
1379 1578
1657
ISB
ISB 53-1269
1
1.00
ALL
ISB
ISB 53-1269
1
1.00
ALL
Sub 2 - Page 110 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
531277-01-1
ZONE
240
DESCRIPTION
EMERGENCY EXIT DOOR HATCHES IN SECTION 15
SKILL TASK
CODE CODE
NDT
SDI
AF
DET
SPECIAL DETAILED INSPECTION OF THE EMERGENCY EXIT DOOR HATCHES
(LH/RH) IN SECTION 15.
531900-01-1
220
FUSELAGE DRAINAGE
INTERVALS
T:
48000 FC
OR
96000 FH
I:
6000 FC
OR
12000 FH
I:
4 MO
SOURCE
TPS
120
FUSELAGE DRAINAGE
MEN
TASKM. APPLICABI
H.
LITY
ISB
ISB 53-1277
1
5.00
1130 1200
1379 1578
1657 1767
2151 2163
MRB 9
531900-210-001
1
0.10
2
0.60
1
1
1
0.20
0.20
0.20
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
ALL
2
2
1.50
1.50
ALL
1
1
0.08
0.08
ALL
INSPECTION OF THE COCKPIT GRID COLLECTOR ASSY
531900-02-1
REFERENCES
SOURCE:
MRB 53.19.00/06
AF
OPC
I:
24 MO
MRB 9
531900-710-001
OPERATIONAL CHECK OF THE COCKPIT DRAINAGE PIPE
SOURCE:
MRB 53.19.00/07
ACCESS PANELS: 824, 825
531900-03-1
532102-01-1
120
130
150
231
232
FUSELAGE DRAINAGE
OPERATIONAL CHECK OF PISTON TYPE DRAIN VALVES IN
LOWER FUSELAGE SHELL FROM OUTSIDE
FLOOR STRUCTURE FR 24-35
AF
AF
OPC
GVI
GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE,
EXCLUDING AREAS BELOW GALLEYS AND TOILETS (IF
INSTALLED), BETWEEN FR 24 AND FR 35
532104-01-1
131
132
PREPARATION: CABIN FLOOR PANELS;
FLOOR STRUCTURE
SPECIAL DETAILED INSPECTION (ROTO) OF ATTACHMENT AREA OF FR25 LH
TO FR34 LH AND FR29 RH TO FR34 RH TO CABIN FLOOR BEAMS, INTERNAL
STRUCTURE
PREPARATION: BOLTS REMOVED; CEILING PANELS REMOVED; INSULATION
DISPLACED; LINING REMOVED;
NDT
SDI
I:
24 MO
OR
5000 FC
T:
12 YE
I:
12 YE
MRB 9
531900-710-003
MRB CPCP
SOURCE:
MRB 53.19.00/08
532100-210-001
T:
43400 FC
OR
86900 FH
I:
35600 FC
OR
71200 FH
ALI WFD
1
SOURCE:
MRB 532102-01-1
532100-220-802
NTM 53-21-04
SOURCE:
ALI 532104-01-1
ACCESS PANELS: 825
Sub 2 - Page 111 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
532120-01-1
ZONE
231
232
DESCRIPTION
FRAME WEBS
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF FRAME WEBS AT STRINGER 18 LH/RH FOR FR 25,
26, 27, 28, 32, 33, 34
INTERVALS
SOURCE
ST:
30000 FC
SI:
9500 FC
MRB
ST:
30000 FC
SI:
9200 FC
MRB
ST:
30000 FC
SI:
9500 FC
MRB
ST:
30000 FC
SI:
9200 FC
MRB
ST:
30000 FC
OR
60000 FH
SI:
10400 FC
OR
20800 FH
MRB
TPS
REFERENCES
532100-200-001
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.30
0.30
1130 1200
1379
1
1
0.30
0.30
1578 1657
1767 2151
2163
1
1
0.25
0.25
0649 1488
1761 1890
1
1
0.25
0.25
1560 1743
1851 1863
1876
1
1
0.20
0.20
ALL
SOURCE:
MRB 532120-01-1
PREPARATION: LINING; INSULATION REMOVED;
532120-01-3
231
232
ACCESS PANELS: 831
FRAME WEBS
AF
DET
DETAILED INSPECTION OF FRAME WEBS AT STRINGER 18,
LH/RH FOR FR 25, 26, 27, 28, 32, 33, 34.
532100-200-001
SOURCE:
MRB 532120-01-3
PREPARATION: LINING; INSULATION REMOVED;
532120-02-1
231
232
ACCESS PANELS: 831
FRAME WEBS
AF
DET
DETAILED INSPECTION OF FRAME WEBS AT STRINGER 18
LH/RH FOR: FR 25, 26, 27, 28, 29, 30, 34
532100-200-030
SOURCE:
MRB 532120-02-1
PREPARATION: LINING AND INSULATION REMOVED;
532120-02-3
231
232
ACCESS PANELS: 831
FRAME WEBS
AF
DET
DETAILED INSPECTION OF FRAME WEBS AT STRINGER 18
LH/RH FOR: FR 25, 26, 27, 28, 29, 30, 34
532100-200-030
SOURCE:
MRB 532120-02-3
PREPARATION: LINING AND
INSULATION REMOVED;
532125-01-1
128
132
ACCESS PANELS: 831
JUNCTION FR 24/PAX FLOOR BEAM
DETAILED INSPECTION OF FR 24 JUNCTION WITH CABIN
FLOOR BEAM AT STRINGER 23, INTERNAL SIDE, RH
PREPARATION: INSULATION REMOVED;
ACCESS PANELS: 131HC, 132BW, 132EW, 825
AF
DET
532100-200-002
SOURCE:
MRB 532125-01-1
Sub 2 - Page 112 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
532132-01-1
ZONE
100
132
DESCRIPTION
FWD CARGO DOOR HINGE FITTING
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF FUSELAGE FORWARD CARGO DOOR
HINGE FITTING AND EXTERNAL ATTACHMENT AREA
532132-01-3
100
132
ACCESS PANELS: 825
FWD CARGO DOOR HINGE FITTING
AF
DET
DETAILED INSPECTION OF FUSELAGE FORWARD CARGO DOOR HINGE FITTING
AND EXTERNAL ATTACHMENT AREA
NOTE : TPS APPLICATION IS LIMITED TO THE INNER SIDE OF THE HINGE
FITTINGS
INTERVALS
SOURCE
T:
24000 FC
I:
13800 FC
ALI
T:
12 YE
I:
12 YE
MRB CPCP
T:
1200 FC
OR
2400 FH
OR
6 YE
I:
1200 FC
OR
2400 FH
OR
6 YE
T:
9700 FC
OR
19400 FH
I:
9700 FC
OR
19400 FH
ST:
30000 FC
OR
60000 FH
SI:
7100 FC
OR
14200 FH
ALI
MRB CPCP
TPS
REFERENCES
532100-200-027
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.45
0.45
ALL
1
1
0.45
0.45
ALL
1
0.30
ALL
1
1
0.25
0.25
ALL
1
1
0.50
0.50
0649 1130
1200 1379
1488
SOURCE:
ALI 532132-01-1
1
532100-200-027
SOURCE:
MRB 532132-01-3
PREPARATION: DOOR OPENED AND CLOSED;
532135-01-2
132
ACCESS PANELS: 825
FWD CARGO DOOR CUTOUT LATERAL FRAMES
AF
GVI
GENERAL VISUAL INSPECTION OF FORWARD CARGO DOOR
CUTOUT, VISIBLE PART OF LATERAL FR 24A AND FR 28
ACCESS PANELS: 825
532137-01-1
100
132
FWD CARGO DOOR CUTOUT PANELS
AF
DET
DETAILED INSPECTION OF FORWARD CARGO DOOR CUTOUT
PANELS, UPPER AND LOWER CORNERS, EXTERNAL SURFACE
ACCESS PANELS: 825
532140-01-1
132
232
FR 25, 26 AND 27 LOWER FITTINGS
DETAILED INSPECTION OF INSIDE RADIUS OF CROSS BEAM AT
FR 25, FR 26 AND FR 27 LOWER FITTINGS, LOCATED ABOVE
FORWARD CARGO DOOR, RH
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532140-02-1
PREPARATION: ACTUATOR DISCONNECTED; CEILING PANELS REMOVED;
AF
DET
1
532100-210-002
SOURCE:
ALI 532135-01-2
MRB 532135-01-1
ALI
532100-200-004
SOURCE:
ALI 532137-01-1
MRB
532100-200-016
SOURCE:
MRB 532140-01-1
ACCESS PANELS: 825
Sub 2 - Page 113 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
532140-01-2
ZONE
132
232
DESCRIPTION
FR 25, 26 AND 27 LOWER FITTINGS
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF INSIDE RADIUS OF CROSS BEAM AT
FR 25, FR 26 AND FR 27 LOWER FITTINGS, LOCATED ABOVE
FORWARD CARGO DOOR, RH
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532140-02-2
PREPARATION: ACTUATOR DISCONNECTED; CEILING PANELS REMOVED;
532140-02-1
132
232
ACCESS PANELS: 825
FR 25, 26 AND 27 LOWER FITTINGS
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF INSIDE RADIUS
OF CROSS BEAM AT FR 25, FR 26 AND FR 27 LOWER
FITTINGS, LOCATED ABOVE FORWARD CARGO DOOR, RH.
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532140-01-1
PREPARATION: ACTUATOR DISCONNECTED; CEILING PANELS REMOVED;
532140-02-2
132
232
ACCESS PANELS: 825
FR 25, 26 AND 27 LOWER FITTINGS
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF INSIDE RADIUS
OF CROSS BEAM AT FR 25, FR 26 AND FR 27 LOWER
FITTINGS, LOCATED ABOVE FORWARD CARGO DOOR, RH.
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532140-01-2
PREPARATION: ACTUATOR DISCONNECTED; CEILING PANELS REMOVED;
532145-01-1
131
132
ACCESS PANELS: 825
FR 29 TO 34 ATTACHMENT AREA
AF
DET
DETAILED INSPECTION OF ATTACHMENT AREA OF FR 29 TO FR
34, CARGO FLOOR BEAMS, LH/RH
INTERVALS
SOURCE
ST:
30000 FC
OR
60000 FH
SI:
6700 FC
OR
13500 FH
MRB
ST:
30000 FC
OR
60000 FH
SI:
17400 FC
OR
34800 FH
MRB
ST:
30000 FC
OR
60000 FH
SI:
16600 FC
OR
33200 FH
MRB
ST:
30000 FC
SI:
11700 FC
MRB
ST:
30000 FC
SI:
11100 FC
MRB
TPS
REFERENCES
532100-200-016
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.50
0.50
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
1
1
0.50
0.50
0649 1130
1200 1379
1488
1
1
0.50
0.50
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
1
1
0.50
0.50
0649 1130
1200 1379
1488
1
1
0.50
0.50
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
SOURCE:
MRB 532140-01-2
532100-200-017
NTM 53-21-40
SOURCE:
MRB 532140-02-1
532100-200-017
NTM 53-21-40
SOURCE:
MRB 532140-02-2
532100-200-009
SOURCE:
MRB 532145-01-1
PREPARATION: CARGO FLOOR PANELS REMOVED;
532145-01-2
131
132
ACCESS PANELS: 825
FR 29 TO 34 ATTACHMENT AREA
DETAILED INSPECTION OF ATTACHMENT AREA OF FR 29 TO FR
34, CARGO FLOOR BEAMS, LH/RH
PREPARATION: CARGO FLOOR PANELS REMOVED;
AF
DET
532100-200-009
SOURCE:
MRB 532145-01-2
ACCESS PANELS: 825
Sub 2 - Page 114 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
532155-01-1
ZONE
131
DESCRIPTION
FRAME SPLICES FR 24-34
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF FRAME SPLICES AT STRINGER 35
LH, FROM FR 24 TO FR 34
INTERVALS
SOURCE
T:
34000 FC
I:
11000 FC
ALI
T:
32400 FC
I:
10500 FC
ALI
ST:
48000 FC
SI:
13000 FC
MRB
T:
30000 FC
OR
60000 FH
I:
3100 FC
OR
6200 FH
T:
30000 FC
OR
60000 FH
I:
3300 FC
OR
6600 FH
T:
5400 FC
I:
5400 FC
MRB
TPS
REFERENCES
532100-200-012
MEN
TASKM. APPLICABI
H.
LITY
1
0.90
0649 1130
1200 1379
1488
1
0.90
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
1
1.10
ALL
1
2.57
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
3.52
1130 1200
1379 1578
1657 1767
2151 2163
1
0.40
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
ALI 532155-01-1
PREPARATION: CARGO FLOOR PANELS; INSULATION REMOVED;
532155-01-2
131
ACCESS PANELS: 825
FRAME SPLICES FR 24-34
AF
DET
DETAILED INSPECTION OF FRAME SPLICES AT STRINGER 35
LH, FROM FR 24 TO FR 34
532100-200-012
SOURCE:
ALI 532155-01-2
PREPARATION: CARGO FLOOR PANELS; INSULATION REMOVED;
532160-01-1
532164-01-4
200
ACCESS PANELS: 825
FUSELAGE SKIN BETWEEN FR 28 AND 35
200
DETAILED INSPECTION OF FUSELAGE SKIN AND VISIBLE PART
OF WINDOW FORGING DOUBLERS AROUND CABIN WINDOWS,
BETWEEN FR 28 AND FR 35 AND BETWEEN STRINGER 14 AND
STRINGER 18, EXTERNAL SURFACE, LH/RH
FORWARD FUSELAGE
AF
AF
DET
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL SURFACE, FROM
STRINGER 23 LH/RH TO CROWN CENTERLINE, EXCEPT AREAS COVERED BY
BELLY FAIRING
NOTE: INSPECTION BETWEEN FR 24 AND FR 35.
532164-01-5
200
FORWARD FUSELAGE
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL SURFACE, FROM
STRINGER 23 LH/RH TO CROWN CENTERLINE, EXCEPT AREAS COVERED BY
BELLY FAIRING
NOTE: INSPECTION BETWEEN FR 24 AND FR 35.
532165-01-1
100
FUSELAGE SKIN BETWEEN FR 24 AND 35
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL SURFACE, FROM
STRINGER 23 LH/RH TO BOTTOM CENTERLINE, EXCEPT AREAS COVERED BY
BELLY FAIRING
AF
GVI
532100-200-008
SOURCE:
MRB 532160-01-1
532100-210-802
SOURCE:
MRB 532164-01-4
MRB
532100-210-802
SOURCE:
MRB 532164-01-5
ALI
532100-210-005
SOURCE:
ALI 532165-01-1
NOTE: INSPECTION BETWEEN FR 24 AND FR 35.
CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 53216501-2.
Sub 2 - Page 115 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
532165-01-2
ZONE
100
DESCRIPTION
FUSELAGE SKIN BETWEEN FR 24 AND 35
SKILL TASK
CODE CODE
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL SURFACE, FROM
STRINGER 23 LH/RH TO BOTTOM CENTERLINE, EXCEPT AREAS COVERED BY
BELLY FAIRING
532166-01-1
137
138
NOTE: INSPECTION BETWEEN FR 24 AND FR 35.
CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 53216501-1
FUSELAGE SKIN AT FR 35
AF
DET
DETAILED INSPECTION OF FUSELAGE SKIN AT FR 35 AND 10
CM FORWARD, AT LEVEL OF STRINGER 30, INTERNAL SIDE,
LH/RH
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532166-02-1
PREPARATION: LINING REMOVED; INSULATION REMOVED;
532166-02-1
137
138
FORWARD FUSELAGE
SPECIAL DETAILED INSPECTION (ROTO) OF FUSELAGE SKIN AT FR 35 AND 10
CM FORWARD, AT LEVEL OF STRINGER 30, INTERNAL SIDE, LH/RH
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532166-01-1.
PREPARATION: BOLTS REMOVED; INSULATION REMOVED; LINING REMOVED;
NDT
SDI
INTERVALS
SOURCE
T:
5600 FC
I:
5600 FC
ALI
ST:
30000 FC
OR
60000 FH
SI:
5400 FC
OR
10800 FH
T:
43400 FC
OR
86900 FH
I:
5400 FC
OR
10800 FH
ST:
30000 FC
OR
60000 FH
SI:
18800 FC
OR
37700 FH
T:
43400 FC
OR
86900 FH
I:
18800 FC
OR
37700 FH
ALI
MRB
TPS
REFERENCES
532100-210-005
MEN
TASKM. APPLICABI
H.
LITY
1
0.40
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.50
0.50
ALL
1
1
0.32
0.32
ALL
SOURCE:
ALI 532165-01-2
532100-200-023
SOURCE:
ALI 532166-01-1
MRB 532166-01-1
ALI
MRB
532100-220-803
NTM 53-21-66
SOURCE:
ALI 532166-02-1
MRB 532166-02-1
Sub 2 - Page 116 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
532170-01-1
ZONE
132
DESCRIPTION
FWD CARGO DOOR LOCK FITTINGS AND SURROUNDING STRUCTURE
SKILL TASK
CODE CODE
AF
GVI
GENERAL VISUAL INSPECTION OF FORWARD CARGO DOOR LOCK FITTINGS
AND SURROUNDING STRUCTURE, EXTERNAL PORTION
NOTE: INSPECTION BETWEEN FR 25 AND FR 27A (6 PLACES).
532170-01-2
132
ACCESS PANELS: 825
FWD CARGO DOOR LOCK FITTINGS AND
SURROUNDING STRUCTURE
AF
GVI
GENERAL VISUAL INSPECTION OF FORWARD CARGO DOOR LOCK FITTINGS
AND SURROUNDING STRUCTURE, EXTERNAL PORTION
NOTE: INSPECTION BETWEEN FR 25 AND FR 27A (6 PLACES).
532175-01-1
132
232
ACCESS PANELS: 825
FWD CARGO DOOR CUT OUT
AF
DET
DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND
FORWARD CARGO DOOR CUTOUT, FROM FR 24 TO FR 29 AND
BETWEEN STRINGER 23 AND STRINGER 38, RH
INTERVALS
SOURCE
T:
9300 FC
OR
6 YE
I:
9300 FC
OR
6 YE
T:
9100 FC
OR
6 YE
I:
9100 FC
OR
6 YE
ALI
MRB CPCP
T:
12 YE
I:
6 YE
MRB CPCP
T:
6 YE
I:
6 YE
MRB CPCP
TPS
1
REFERENCES
532100-210-006
MEN
TASKM. APPLICABI
H.
LITY
1
0.30
0649 1130
1200 1379
1488
1
0.30
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
1
1
0.80
0.80
ALL
1
1
1
1
0.10
0.10
0.10
0.10
ALL
SOURCE:
ALI 532170-01-1
MRB 532170-01-4
ALI
MRB CPCP
1
532100-210-006
SOURCE:
ALI 532170-01-2
MRB 532170-01-4
1
532100-200-011
SOURCE:
MRB 532175-01-1
PREPARATION: CARGO FLOOR PANELS REMOVED; FWD ACT(S) REMOVED (IF
INSTALLED); LINING AND INSULATION REMOVED;
532180-01-2
133
134
137
138
ACCESS PANELS: 825
FUSELAGE FR 24-35
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE INCLUDING
FORWARD FACE OF PRESSURE BULKHEAD, FROM STRINGER 38 LH/RH TO
BOTTOM CENTERLINE
AF
DET
1+2 532100-200-013
SOURCE:
MRB 532180-01-2
NOTE: INSPECTION BETWEEN FR 24 AND FR 35. TYPE 2 TPS MAY BE LIMITED
TO FUSELAGE INTERNAL STRUCTURE FROM FR 34 TO FR 35, AND FORWARD
FACE OF PRESSURE BULKHEAD, FROM STRINGER 38, LH/RH TO BOTTOM
CENTERLINE.
PREPARATION: CARGO FLOOR PANELS REMOVED; FWD ACT(S) REMOVED (IF
INSTALLED);
ACCESS PANELS: 825
Sub 2 - Page 117 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
532186-01-1
ZONE
200
DESCRIPTION
CIRCUMFERENTIAL JOINT AT FR 35
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (LFEC) OF CIRCUMFERENTIAL JOINT AT FR 35,
BETWEEN STRINGER 10 LH AND STRINGER 10 RH, EXTERNAL SIDE
532186-01-2
200
CIRCUMFERENTIAL JOINT AT FR 35
NDT
SDI
SPECIAL DETAILED INSPECTION (LFEC) OF CIRCUMFERENTIAL JOINT AT FR 35,
BETWEEN STRINGER 10 LH AND STRINGER 10 RH, EXTERNAL SIDE.
532188-01-1
200
CIRCUMFERENTIAL JOINT AT FR 35
AF
DET
DETAILED INSPECTION OF SKIN OF CIRCUMFERENTIAL JOINT
AT FR 35, BETWEEN STRINGER 10 LH AND STRINGER 10 RH,
EXTERNAL SIDE
532190-01-1
532195-01-1
100
FUSELAGE SKIN BETWEEN FR 25 AND FR 29
132
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE AROUND WATER DRAIN PANEL CUTOUT, BETWEEN FR
25 AND FR 29 AT STRINGER 43 LH
FWD CARGO DOOR ACTUATOR
GENERAL VISUAL INSPECTION OF FORWARD CARGO DOOR
ACTUATOR ATTACH BRACKETS, BETWEEN CABIN FLOOR BEAMS,
FROM FR 25 TO FR 27
AF
AF
GVI
GVI
INTERVALS
SOURCE
T:
48000 FC
OR
96000 FH
I:
13300 FC
OR
26600 FH
ST:
30000 FC
OR
60000 FH
SI:
13300 FC
OR
34400 FH
T:
42700 FC
OR
60000 FH
I:
13300 FC
OR
34400 FH
ST:
30000 FC
OR
60000 FH
SI:
20000 FC
OR
42000 FH
ALI WFD
T:
48000 FC
I:
8100 FC
ALI
T:
16700 FC
I:
16700 FC
MRB
TPS
REFERENCES
532100-200-024
NTM 53-21-86
MEN
TASKM. APPLICABI
H.
LITY
1
3.42
1130 1200
1379 1578
1657 1767
2151 2163
1
3.42
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.10
ALL
1
0.10
ALL
SOURCE:
ALI 532186-01-1
ALI
MRB
532100-200-024
NTM 53-21-86
SOURCE:
ALI 532186-01-2
MRB 532186-01-2
MRB
532100-200-026
SOURCE:
MRB 532188-01-1
532100-210-007
SOURCE:
ALI 532190-01-1
532100-210-008
SOURCE:
MRB 532195-01-1
ACCESS PANELS: 131AC, 825
Sub 2 - Page 118 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
532196-01-1
ZONE
132
DESCRIPTION
FWD CARGO DOOR ECCENTRIC BOLTS
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF FORWARD CARGO DOOR ECCENTRIC
BOLTS OF LOCKING MECHANISM AT LOCK FITTINGS, BETWEEN
FR 25 AND FR 27A
PREPARATION: ECCENTRIC BOLTS REMOVED;
ACCESS PANELS: 825
533101-01-1
147
148
AFT PRESSURE BULKHEAD FWD FACE
AF
DET
DETAILED INSPECTION OF PRESSURE BULKHEAD AT FR 46,
FORWARD FACE
ACCESS PANELS: 734, 744
533101-01-3
147
148
AFT PRESSURE BULKHEAD FWD FACE
AF
DET
DETAILED INSPECTION OF PRESSURE BULKHEAD AT FR 46, FORWARD FACE.
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
533101-01-1.
ACCESS PANELS: 734, 744
533103-01-1
151
152
AFT PRESSURE BULKHEAD AFT FACE
DETAILED INSPECTION OF PRESSURE BULKHEAD AT FR 46, AFT FACE,
INCLUDING VERTICAL BEAMS, ABOVE CARGO FLOOR LEVEL
AF
DET
INTERVALS
SOURCE
ST:
12 YE
OR
37400 FC
SI:
12 YE
OR
9300 FC
T:
24 YE
I:
12 YE
ST:
30000 FC
OR
60000 FH
SI:
20000 FC
OR
40000 FH
MRB CPCP
ST:
30000 FC
OR
60000 FH
SI:
18800 FC
OR
37600 FH
MRB
T:
12 YE
I:
12 YE
MRB CPCP
TPS
NO
REFERENCES
532100-200-005
MEN
TASKM. APPLICABI
H.
LITY
1
1.00
ALL
1
1
0.50
0.50
1130 1200
1379 1578
1657 1767
2151 2163
1
1
1.00
1.00
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.50
0.50
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
MRB 532196-01-1
MRB
533100-210-002
SOURCE:
MRB 533101-01-1
533100-210-002
SOURCE:
MRB 533101-01-3
1
533100-210-008
SOURCE:
MRB 533103-01-1
PREPARATION: INSULATION REMOVED; ACT(S) REMOVED (IF INSTALLED);
ACCESS PANELS: 151AW, 151BW, 152BW
Sub 2 - Page 119 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
533103-01-5
ZONE
151
152
DESCRIPTION
AFT PRESSURE BULKHEAD AFT FACE
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF PRESSURE BULKHEAD AT FR 46, AFT FACE,
INCLUDING VERTICAL BEAMS, ABOVE CARGO FLOOR LEVEL.
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
533103-01-1.
PREPARATION: ACT(S) REMOVED (IF INSTALLED); INSULATION REMOVED;
ACCESS PANELS: 151AW, 151BW, 152BW
533105-01-1
147
148
MLG BAY SIDE PANELS
AF
DET
DETAILED INSPECTION OF MLG BAY FUSELAGE SIDE PANELS
INSIDE MLG BAY, BETWEEN FR 42 AND FR 46, INCLUDING
SLANTED FRAMES AND SIDE BOX, LH/RH
ACCESS PANELS: 734, 744
533105-01-2
147
148
MLG BAY SIDE PANELS
AF
DET
DETAILED INSPECTION OF MLG BAY FUSELAGE SIDE PANELS
INSIDE MLG BAY, BETWEEN FR 42 AND FR 46, INCLUDING
SLANTED FRAMES AND SIDE BOX, LH/RH
ACCESS PANELS: 734, 744
533107-01-1
147
148
MLG BAY SIDE PANELS OUTBOARD FACE
DETAILED INSPECTION OF MLG BAY FUSELAGE SIDE PANELS,
OUTBOARD FACE, BETWEEN FR 42 AND FR 47, FROM STRINGER
26 TO STRINGER 36, LH/RH
AF
DET
INTERVALS
ST:
35000 FC
OR
60000 FH
SI:
18000 FC
OR
40500 FH
T:
12 YE
I:
12 YE
ST:
12 YE
SI:
6 YE
T:
24 YE
OR
28400 FC
OR
60000 FH
I:
6 YE
OR
12900 FC
OR
35400 FH
ST:
12 YE
SI:
6 YE
T:
24 YE
I:
6 YE
ST:
48000 FC
SI:
20000 FC
SOURCE
MRB CPCP
TPS
1
REFERENCES
533100-210-008
MEN
TASKM. APPLICABI
H.
LITY
1
1
1.00
1.00
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.50
0.50
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
MRB 533103-01-5
ALI
MRB CPCP
533100-210-003
SOURCE:
ALI 533105-01-1
MRB 533105-01-1
MRB CPCP
533100-210-003
SOURCE:
MRB 533105-01-2
MRB
533100-210-004
SOURCE:
MRB 533107-01-1
ACCESS PANELS: 191ET, 193AT, 734, 192ET, 194AT, 744
Sub 2 - Page 120 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
533109-01-1
ZONE
145
146
DESCRIPTION
PRESSURE DECK MEMBRANES UPR SURFACE
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF UPPER SURFACES OF PRESSURE
DECK MEMBRANES AND SIDE BOXES, BETWEEN FR 42 AND FR
46, INCLUDING CONNECTIONS TO LONGITUDINAL BEAMS AND
SUPPORT RIBS, LH/RH
533110-01-1
145
146
PREPARATION: AIR DUCT; CABIN FLOOR PANELS; INSULATION REMOVED;
LONGITUDINAL FLOOR BEAMS
NDT
SDI
SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF UPPER
FLANGE OF LONGITUDINAL FLOOR BEAMS AT FR 42 AND FR
46, AS FAR AS VISIBLE
PREPARATION: CABIN FLOOR PANELS;
533110-01-2
145
146
LONGITUDINAL FLOOR BEAMS
NDT
SDI
SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF UPPER FLANGE OF
LONGITUDINAL FLOOR BEAMS AT FR 42 AND FR 46, AS FAR AS VISIBLE
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
533110-01-1.
533111-01-1
147
148
PREPARATION: CABIN FLOOR PANELS REMOVED;
PRESSURE DECK MEMBRANES LWR SURFACE
AF
DET
DETAILED INSPECTION OF LOWER SURFACE OF PRESSURE DECK
MEMBRANES, BETWEEN FR 42 AND FR 46, INCLUDING
CONNECTIONS TO LONGITUDINAL BEAMS, SIDE BOXES,
SUPPORT RIBS, REAR SPAR OF CENTER WING BOX AND
PRESSURE BULKHEAD, LH/RH
ACCESS PANELS: 734, 744
533121-01-1
200
CIRCUMFERENTIAL SPLICE AT FR 35
DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL SPLICE
AND STRINGER COUPLING AREA AT FR 35 FROM STRINGER 10,
LH/RH TO CROWN CENTERLINE, EXTERNAL SURFACE
AF
DET
INTERVALS
SOURCE
T:
20000 FC
OR
55000 FH
I:
12300 FC
OR
33800 FH
ST:
48000 FC
OR
96000 FH
SI:
15400 FC
OR
30800 FH
ALI
ST:
33500 FC
OR
60000 FH
SI:
12000 FC
OR
33000 FH
MRB
ST:
12 YE
SI:
6 YE
T:
24 YE
OR
24000 FC
OR
48000 FH
I:
6 YE
OR
8400 FC
OR
16800 FH
ST:
30000 FC
SI:
20000 FC
ALI
MRB CPCP
TPS
REFERENCES
533100-210-005
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.75
0.75
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
1.00
1.00
1130 1200
1379 1578
1657 1767
2151 2163
1
1
1.00
1.00
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.75
0.75
ALL
1
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
ALI 533109-01-1
MRB
533100-220-003
NTM 53-31-10
SOURCE:
MRB 533110-01-1
533100-220-003
NTM 53-31-00
SOURCE:
MRB 533110-01-2
533100-210-006
SOURCE:
ALI 533111-01-1
MRB 533111-01-1
MRB
533100-210-018
SOURCE:
MRB 533121-01-1
Sub 2 - Page 121 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
533122-01-2
533122-01-3
533128-01-2
ZONE
DESCRIPTION
200
CIRCUMFERENTIAL SPLICE AT FR 47
200
DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL SPLICE
AND STRINGER COUPLING AREA AT FR 47, FROM STRINGER
10, LH/RH TO CROWN CENTERLINE, EXTERNAL SURFACE
CIRCUMFERENTIAL SPLICE AT FR 47/51
200
DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL SPLICE
AND STRINGER COUPLING AREA AT FR 47/51, FROM STRINGER
10, LH/RH TO CROWN CENTERLINE, EXTERNAL SURFACE
EMERGENCY EXIT SKIN CUTOUTS
SKILL TASK
CODE CODE
AF
AF
AF
DET
DET
DET
DETAILED INSPECTION OF EMERGENCY EXIT SKIN CUTOUTS, UPPER AND
LOWER CORNERS, LH/RH
ACCESS PANELS: 833834843, 844
533128-01-3
200
EMERGENCY EXIT SKIN CUTOUTS
AF
DET
DETAILED INSPECTION OF EMERGENCY EXIT SKIN CUTOUTS, UPPER AND
LOWER CORNERS, LH/RH
ACCESS PANELS: 834, 844
533128-01-6
200
EMERGENCY EXIT SKIN CUTOUTS
AF
DET
DETAILED INSPECTION OF EMERGENCY EXIT SKIN CUTOUTS,
UPPER AND LOWER CORNERS, LH/RH
ACCESS PANELS: 833, 834, 843, 844
533129-01-1
241
242
EMERGENCY EXIT CUTOUTS
DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND
EMERGENCY EXIT CUTOUTS, BETWEEN FR 37 AND FR 41, BOTH
SIDES, FROM STRINGER 10 TO STRINGER 23, LH/RH
AF
DET
INTERVALS
SOURCE
T:
33000 FC
I:
9200 FC
ALI
T:
33300 FC
I:
11500 FC
ALI
T:
31100 FC
OR
62200 FH
I:
10900 FC
OR
21900 FH
T:
24000 FC
OR
60000 FH
I:
9800 FC
OR
24500 FH
T:
24000 FC
OR
60000 FH
I:
8700 FC
OR
21700 FH
T:
12 YE
I:
6 YE
ALI
TPS
REFERENCES
533100-210-019
MEN
TASKM. APPLICABI
H.
LITY
1
0.50
2151 2163
1
0.50
1
1.00
0649 1488
1560 1743
1761 1851
1863 1876
1890
1130 1200
1379 1578
1657 1767
1
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1.00
2151 2163
1
1
0.25
0.25
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
ALI 533122-01-2
533100-210-019
SOURCE:
ALI 533122-01-3
533100-210-016
SOURCE:
ALI 533128-01-2
ALI
533100-210-016
SOURCE:
ALI 533128-01-3
ALI
533100-210-016
SOURCE:
ALI 533128-01-6
MRB CPCP
1
533100-210-009
SOURCE:
MRB 533129-01-1
PREPARATION: CABIN AIR OUTLET ASSEMBLY; LINING REMOVED; RISER DUCT;
INSULATION REMOVED;
ACCESS PANELS: 833, 834, 843, 844
Sub 2 - Page 122 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
533129-01-2
ZONE
241
242
DESCRIPTION
EMERGENCY EXIT CUTOUTS
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND
EMERGENCY EXIT CUTOUTS, BETWEEN FR 39 AND FR 41,
BOTH SIDES, FROM STRINGER 10 TO STRINGER 23, LH/RH
INTERVALS
SOURCE
T:
12 YE
I:
6 YE
MRB CPCP
ST:
12 YE
OR
34900 FC
OR
69900 FH
SI:
12 YE
OR
21900 FC
OR
43900 FH
T:
24 YE
I:
12 YE
ST:
12 YE
SI:
12 YE
T:
24 YE
OR
30500 FC
I:
12 YE
OR
17000 FC
MRB CPCP
TPS
1
REFERENCES
533100-210-009
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.25
0.25
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.10
1130 1200
1379 1578
1657 1767
1
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
MRB 533129-01-2
PREPARATION: CABIN AIR OUTLET ASSEMBLY; LINING REMOVED; RISER DUCT;
INSULATION REMOVED;
533130-01-1
200
ACCESS PANELS: 834, 844
ANTI COLLISION LIGHT SKIN CUTOUT
AF
DET
DETAILED INSPECTION OF SKIN AROUND ANTI COLLISION
LIGHT CUTOUT, BETWEEN FR 40 AND FR 41 AND BETWEEN
STRINGER 1, LH/RH, EXTERNAL SURFACE
PREPARATION: COVER OF ANTI-COLLISION LIGHT AND ANTI-COLLISION LIGHT
REMOVED;
533130-01-2
200
ANTI COLLISION LIGHT SKIN CUTOUT
DETAILED INSPECTION OF SKIN AROUND ANTI COLLISION
LIGHT CUTOUT, BETWEEN FR 40 AND FR 41 AND BETWEEN
STRINGER 1, LH/RH, EXTERNAL SURFACE
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS
ACCOMPLISHMENT OF TASK 533130-01-1.
PREPARATION: COVER OF ANTI-COLLISION LIGHT AND ANTI-COLLISION LIGHT
REMOVED;
AF
DET
533100-210-010
SOURCE:
MRB 533130-01-1
ALI
MRB CPCP
533100-210-010
SOURCE:
ALI 533130-01-2
MRB 533130-01-2
Sub 2 - Page 123 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
533130-01-4
ZONE
200
DESCRIPTION
ANTI COLLISION LIGHT SKIN CUTOUT
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF SKIN AROUND ANTI COLLISION
LIGHT CUTOUT, BETWEEN FR 40 AND FR 41 AND BETWEEN
STRINGER 1, LH/RH, EXTERNAL SURFACE
PREPARATION: COVER OF
ANTI-COLLISION LIGHT
AND ANTI-COLLISION
LIGHT REMOVED;
533131-01-1
200
ADF1 ANTENNA SKIN CUTOUT
AF
DET
DETAILED INSPECTION OF SKIN AROUND ADF 1 ANTENNA CUTOUT, BETWEEN
FR 44 AND FR 45 AND BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE
PREPARATION: COVER OF ANTENNA AND ANTENNA REMOVED;
533131-01-5
200
ADF1 ANTENNA SKIN CUTOUT
AF
DET
DETAILED INSPECTION OF SKIN AROUND ADF 1 ANTENNA CUTOUT, BETWEEN
FR 44 AND FR 45 AND BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
533131-01-1.
PREPARATION: COVER OF ANTENNA AND ANTENNA REMOVED;
533132-01-3
200
WINDOW FORGINGS FR35-47/51
AF
DET
DETAILED INSPECTION OF VISIBLE PART OF WINDOW FORGINGS AND
FUSELAGE SKIN IN WINDOW FORGING AREA, LH/RH, EXTERNAL SURFACE
NOTE: INSPECTION BETWEEN FR 35 AND FR 47/51.
533133-01-5
200
CENTER FUSELAGE
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL SURFACE, BETWEEN
STRINGER 23, LH/RH TO CROWN CENTER LINE, EXCEPT AREAS COVERED BY
BELLY FAIRING NOTE: INSPECT FROM FR 35 TO FR 47.
AF
GVI
INTERVALS
ST:
12 YE
SI:
12 YE
T:
24 YE
OR
27800 FC
I:
12 YE
OR
11500 FC
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
ST:
12 YE
SI:
12 YE
T:
24 YE
OR
26300 FC
I:
12 YE
OR
15700 FC
ST:
30000 FC
SI:
9300 FC
T:
36300 FC
I:
9300 FC
T:
30000 FC
I:
5000 FC
SOURCE
ALI
MRB CPCP
TPS
REFERENCES
533100-210-010
MEN
TASKM. APPLICABI
H.
LITY
1
0.10
2151 2163
1
0.30
1130 1200
1379 1578
1657 1767
1
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
2.65
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
8.40
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
ALI 533130-01-4
MRB 533130-01-4
MRB CPCP
533100-210-011
SOURCE:
MRB 533131-01-1
ALI
MRB CPCP
533100-210-011
SOURCE:
ALI 533131-01-5
MRB 533131-01-5
ALI
MRB
533100-210-020
SOURCE:
ALI 533132-01-3
MRB 533132-01-3
MRB
533100-210-038
SOURCE:
MRB 533133-01-5
Sub 2 - Page 124 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
533133-01-7
ZONE
200
DESCRIPTION
CENTER FUSELAGE
SKILL TASK
CODE CODE
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL SURFACE, BETWEEN
STRINGER 23, LH/RH TO CROWN CENTER LINE, EXCEPT AREAS COVERED BY
BELLY FAIRING
533135-01-1
145
146
NOTE: INSPECT FROM FR 35 TO FR 47/51.
FUSELAGE FR 36-46
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL
STRUCTURE BELOW CABIN FLOOR PANELS, INCLUDING CABIN
FLOOR STRUCTURE BETWEEN FR 36 AND FR 46
NOTE: CAN BE PERFORMED AT SAME TIME AS TASK
571157-01-1
533136-01-1
147
148
PREPARATION: CABIN FLOOR PANELS; INSULATION REMOVED;
MAIN LANDING GEAR BAY
AF
GVI
GENERAL VISUAL INSPECTION OF MLG BAY, INCLUDING MLG
DOOR HINGES
533138-01-1
241
242
ACCESS PANELS: 734, 744
LONGITUDINAL LAP JOINT AT FR 42
AF
DET
DETAILED INSPECTION OF LOWER SKIN OF LONGITUDINAL LAP JOINT AT
STRINGER 18 LH AND STRINGER 18 RH, IN RUNOUT AREA AT FR 42, INTERNAL
NOTE: THIS TASK IS AN ALTERNATIVE INSPECTION TO TASK 533138-02-1
PREPARATION: LINING REMOVED; INSULATION REMOVED;
533138-01-2
241
242
LONGITUDINAL LAP JOINT AT FR 42
DETAILED INSPECTION OF LOWER SKIN OF LONGITUDINAL LAP JOINT AT
STRINGER 18 LH AND STRINGER 18 RH, IN RUNOUT AREA AT FR 42, INTERNAL
NOTE: THIS TASK IS AN ALTERNATIVE INSPECTION TO TASK 533138-02-2
PREPARATION: LINING AND INSULATION REMOVED;
AF
DET
INTERVALS
SOURCE
T:
30000 FC
I:
5000 FC
MRB
T:
12 YE
I:
12 YE
MRB CPCP
T:
6 YE
I:
6 YE
MRB CPCP
ST:
30000 FC
OR
60000 FH
SI:
17400 FC
OR
34900 FH
T:
40000 FC
OR
80000 FH
I:
17400 FC
OR
34900 FH
ST:
30000 FC
SI:
10000 FC
T:
40000 FC
I:
10000 FC
ALI
MRB
TPS
REFERENCES
533100-210-038
MEN
TASKM. APPLICABI
H.
LITY
1
8.40
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.50
0.50
ALL
1
1
0.10
0.10
ALL
1
1
0.25
0.25
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.25
0.25
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
MRB 533133-01-7
1
533100-210-031
SOURCE:
MRB 533135-01-1
1
533100-210-023
SOURCE:
MRB 533136-01-1
533100-210-027
SOURCE:
ALI 533138-01-1
MRB 533138-01-1
ALI
MRB
533100-210-027
SOURCE:
ALI 533138-01-2
MRB 533138-01-2
Sub 2 - Page 125 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
533138-02-1
ZONE
241
242
DESCRIPTION
LONGITUDINAL LAP JOINT AT FR 42
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF LOWER SKIN OF
LONGITUDINAL LAP JOINT AT STRINGER 18 LH AND STRINGER
18 RH, IN RUNOUT AREA AT FR 42, INTERNAL
NOTE: THIS TASK IS AN ALTERNATIVE INSPECTION TO TASK
533138-01-1
PREPARATION: LINING REMOVED; INSULATION REMOVED;
533138-02-2
241
242
LONGITUDINAL LAP JOINT AT FR 42
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF LOWER SKIN OF LONGITUDINAL
LAP JOINT AT STRINGER 18 LH AND STRINGER 18 RH, IN RUNOUT AREA AT FR
42, INTERNAL
NOTE: THIS TASK IS AN ALTERNATIVE INSPECTION TO TASK 533138-01-2
533139-01-1
241
242
PREPARATION: LINING AND INSULATION REMOVED;
FRAME FLANGES AT FR 38, 39, 40 AND 41
AF
DET
DETAILED INSPECTION OF FRAME FLANGES AT FR 38 AND 39,
AND AT FR 40 AND 41 BETWEEN STRINGER 12 AND STRINGER
21, LH/RH, AND LONGITUDINAL BEAM FLANGE AT STRINGER
20A LH AND STRINGER 20A RH, BETWEEN FR 38 AND FR 39
AND BETWEEN FR 40 AND FR 41
533139-01-2
241
242
PREPARATION: LINING REMOVED; INSULATION REMOVED;
FRAME FLANGES AT FR 40 AND 41
DETAILED INSPECTION OF FRAME FLANGES AT FR 40 AND
41, BETWEEN STRINGER 12 AND STRINGER 21, LH/RH, AND
LONGITUDINAL BEAM FLANGE AT STRINGER 20A LH AND
STRINGER 20A RH, BETWEEN FR 40 AND FR 41
AF
DET
INTERVALS
SOURCE
ST:
30000 FC
OR
60000 FH
SI:
31400 FC
OR
62800 FH
T:
40000 FC
OR
80000 FH
I:
31400 FC
OR
62800 FH
ST:
30000 FC
SI:
12000 FC
T:
40000 FC
I:
12000 FC
ALI
MRB
T:
27400 FC
OR
54800 FH
I:
7400 FC
OR
14900 FH
ALI
T:
24000 FC
I:
7400 FC
ALI
TPS
REFERENCES
533100-220-004
NTM 53-31-38
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.60
0.60
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.60
0.60
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.30
0.30
1130 1200
1379 1578
1657 1767
1
1
0.30
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
ALI 533138-02-1
MRB 533138-02-1
ALI
MRB
533100-220-004
NTM 53-31-38
SOURCE:
ALI 533138-02-2
MRB 533138-02-2
533100-210-028
SOURCE:
ALI 533139-01-1
533100-210-028
SOURCE:
ALI 533139-01-2
PREPARATION: LINING REMOVED; INSULATION REMOVED;
Sub 2 - Page 126 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
533139-01-3
ZONE
241
242
DESCRIPTION
FRAME FLANGES AT FR 38, 39, 40 AND 41
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF FRAME FLANGES AT FR 38 AND 39,
AND AT FR 40 AND 41 BETWEEN STRINGER 12 AND STRINGER
21, LH/RH, AND LONGITUDINAL BEAM FLANGE AT STRINGER
20A LH AND STRINGER 20A RH, BETWEEN FR 38 AND FR 39
AND BETWEEN FR 40 AND FR 41
533140-01-2
200
PREPARATION: LINING REMOVED;
INSULATION REMOVED;
SPLICE PLATE AT FR 47
NDT
SDI
SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE PLATE AT
CIRCUMFERENTIAL SKIN SPLICE AT FR 47, FROM STRINGER
10, LH/RH, TO CROWN CENTER LINE
533140-01-4
200
SPLICE PLATE AT FR 47/51
NDT
SDI
SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE PLATE AT
CIRCUMFERENTIAL SKIN SPLICE AT FR 47/51, FROM
STRINGER 10, LH/RH, TO CROWN CENTER LINE
533140-01-7
533140-01-8
200
SPLICE PLATE AT FR 47
200
SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE PLATE AT
CIRCUMFERENTIAL SKIN SPLICE AT FR 47, FROM STRINGER
10, LH/RH, TO CROWN CENTER LINE
SPLICE PLATE AT FR 47
SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE PLATE AT
CIRCUMFERENTIAL SKIN SPLICE AT FR 47, FROM STRINGER 10, LH/RH, TO
CROWN CENTER LINE
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
533140-01-2
NDT
NDT
SDI
SDI
INTERVALS
SOURCE
T:
24000 FC
I:
7400 FC
ALI
ST:
45900 FC
OR
91800 FH
SI:
26500 FC
OR
53100 FH
MRB
ST:
30000 FC
SI:
12800 FC
T:
38700 FC
I:
12800 FC
T:
31100 FC
I:
5200 FC
ALI
MRB
T:
40300 FC
OR
80700 FH
I:
14800 FC
OR
29700 FH
ALI WFD
TPS
REFERENCES
533100-210-028
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.30
0.30
2151 2163
1
1.00
1761
1
1.00
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1.00
2151 2163
1
1.00
1130 1200
1379 1578
1657
SOURCE:
ALI 533139-01-3
533100-220-006
NTM 53-31-40
SOURCE:
MRB 533140-01-2
533100-220-006
NTM 53-31-40
SOURCE:
ALI 533140-01-4
MRB 533140-01-4
ALI
533100-220-006
NTM 53-31-40
SOURCE:
ALI 533140-01-7
533100-220-006
NTM 53-31-40
SOURCE:
ALI 533140-01-8
Sub 2 - Page 127 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
533141-01-1
ZONE
190
DESCRIPTION
FUSELAGE SKIN BETWEEN FR 35 AND 36
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF FUSELAGE SKIN, BETWEEN FR 35
AND FR 36 AND BETWEEN STRINGER 25 AND STRINGER 30,
LH/RH, EXTERNAL SURFACE
ACCESS PANELS: 191BT, 191EB, 192BT, 192EB
533143-01-1
147
148
SIDE BOX BEAM IN AREA OF FR 46
AF
DET
DETAILED INSPECTION OF SIDE BOX BEAM IN AREA OF ATTACHMENT TO FR
46, LH/RH
ACCESS PANELS: 734, 744
533144-01-1
145
146
FRAME ATTACHMENTS TO PRESSURE FLOOR
AF
DET
DETAILED INSPECTION OF FRAME ATTACHMENTS TO PRESSURE FLOOR FROM
FR 42 TO FR 46, LH/RH
PREPARATION: LINING REMOVED; INSULATION REMOVED;
533151-01-1
147
148
191
192
195
196
KEELBEAM BOX
DETAILED INSPECTION OF KEELBEAM BOX
NOTE: INSPECTION BETWEEN FR 35 AND FR 47.
AF
DET
INTERVALS
ST:
30000 FC
OR
60000 FH
SI:
9800 FC
OR
19600 FH
T:
38600 FC
OR
77200 FH
I:
9800 FC
OR
19600 FH
T:
40000 FC
OR
80000 FH
I:
10600 FC
OR
21200 FH
T:
33100 FC
OR
66200 FH
I:
12800 FC
OR
25600 FH
T:
6 YE
I:
6 YE
SOURCE
TPS
ALI
MRB
REFERENCES
533100-210-025
MEN
TASKM. APPLICABI
H.
LITY
1
0.40
ALL
1
1
0.20
0.20
0649 1130
1200 1379
1488 1560
1578 1743
1761 1851
1863 1876
1890
1
1
0.30
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
1
1
1
1
0.30
0.30
0.30
0.30
0.30
0.30
1130 1200
1379 1578
1657 1767
SOURCE:
ALI 533141-01-1
MRB 533141-01-1
ALI
533100-210-029
SOURCE:
ALI 533143-01-1
ALI
533100-210-030
SOURCE:
ALI 533144-01-1
MRB CPCP
1
533100-210-007
SOURCE:
MRB 533151-01-1
ACCESS PANELS: 147AB, 147BB, 147EB, 147FB, 734, 148DB, 148FB, 744, 191BB,
191GB, 191HB, 191JB, 191KB, 192KB, 195AB, 196AB
Sub 2 - Page 128 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
533151-01-3
533151-01-6
533152-01-10
ZONE
147
148
191
192
195
196
147
148
191
192
195
196
137
138
DESCRIPTION
KEELBEAM BOX
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF KEELBEAM BOX
NOTE: INSPECTION BETWEEN FR 35 AND FR 47/51.
ACCESS PANELS: 147AB, 147BB, 147EB, 147FB, 734, 148DB, 148FB, 744, 191BB,
191GB, 191HB, 191JB, 191KB, 192KB, 195AB, 196AB
KEELBEAM BOX
AF
DET
DETAILED INSPECTION OF KEELBEAM BOX
NOTE: INSPECTION BETWEEN FR 35 AND FR 47.
ACCESS PANELS: 147AB, 147BB, 147EB, 147FB, 148DB, 148FB, 191BB, 191GB,
191HB, 191JB, 191KB, 192KB, 195AB, 196AB, 734, 744
PRESSURE BULKHEAD AT FR 35 FWD FACE
AF
DET
DETAILED INSPECTION OF PRESSURE BULKHEAD FORWARD FACE
NOTE: INSPECTION AT FR 35 AND PRESSURE DECK UPPER
SURFACE, BETWEEN FR 35 AND FR 36, INCLUDING
CONNECTIONS TO CENTER WING BOX AT FR 35 AND FR 36.
INTERVALS
SOURCE
ST:
48000 FC
SI:
10000 FC
T:
6 YE
I:
6 YE
ST:
48000 FC
SI:
10000 FC
T:
6 YE
I:
6 YE
T:
12 YE
OR
31000 FC
I:
6 YE
OR
9100 FC
MRB CPCP
T:
12 YE
OR
31000 FC
I:
6 YE
OR
9100 FC
ALI
MRB CPCP
TPS
1
REFERENCES
533100-210-007
SOURCE:
MRB 533151-01-3
MRB CPCP
1
533100-210-007
SOURCE:
MRB 533151-01-6
ALI
MRB CPCP
1
533100-210-012
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
1
1
0.30
0.30
0.30
0.30
0.30
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
1
1
1
1
0.30
0.30
0.30
0.30
0.30
0.30
2151 2163
1
1
0.75
0.75
2151 2163
1
1
0.75
0.75
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
ALI 533152-01-10
MRB 533152-01-10
PREPARATION: AIR CONDITIONING
DUCTS REMOVED;
RECIRCULATION FILTER
REMOVED;
INSULATION REMOVED;
POTABLE WATER TANK
REMOVED;
533152-01-4
137
138
ACCESS PANELS: 131NW, 131PW, 132PW, 825
PRESSURE BULKHEAD AT FR 35 FWD FACE
DETAILED INSPECTION OF PRESSURE BULKHEAD FORWARD FACE
NOTE: INSPECTION AT FR 35 AND PRESSURE DECK UPPER SURFACE,
BETWEEN FR 35 AND FR 36, INCLUDING CONNECTIONS TO CENTER WING BOX
AT FR 35 AND FR 36.
AF
DET
1
533100-210-012
SOURCE:
ALI 533152-01-4
MRB 533152-01-4
PREPARATION: AIR DUCT; RECIRCULATION FILTER REMOVED; INSULATION
REMOVED;
ACCESS PANELS: 131NW, 131PW, 132PW
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
533152-01-7
ZONE
137
138
DESCRIPTION
PRESSURE BULKHEAD AT FR 35 FWD FACE
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF PRESSURE BULKHEAD FORWARD FACE
INTERVALS
SOURCE
T:
12 YE
I:
6 YE
MRB CPCP
T:
6 YE
I:
6 YE
MRB CPCP
T:
6 YE
I:
6 YE
MRB CPCP
ST:
30000 FC
OR
60000 FH
SI:
17500 FC
OR
39300 FH
T:
38400 FC
OR
60000 FH
I:
17500 FC
OR
39300 FH
ALI
MRB
TPS
1
REFERENCES
533100-210-012
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.75
0.75
1130 1200
1379 1578
1657 1767
1
1
0.15
0.15
ALL
1
1
0.20
0.20
ALL
1
1
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
SOURCE:
MRB 533152-01-7
NOTE: INSPECTION AT AT FR 35 AND PRESSURE DECK UPPER SURFACE,
BETWEEN FR 35 AND FR 36, INCLUDING CONNECTIONS TO CENTER WING BOX
AT FR 35 AND FR 36.
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
533152-01-1.
PREPARATION: AIR DUCT; RECIRCULATION FILTER REMOVED; POTABLE
WATER TANK; INSULATION REMOVED;
533153-02-1
191
192
ACCESS PANELS: 131NW, 131PW, 132PW
PRESSURE BULKHEAD AT FR 35 AFT FACE
AF
GVI
GENERAL VISUAL INSPECTION OF PRESSURE BULKHEAD AFT FACE AND
LOWER SKIN OF RESSURE DECK LOWER SURFACE NOTE: INSPECTION AT FR
35 AND LOWER SKIN OF PRESSURE DECK LOWER SURFACE, BETWEEN FR 35
AND FR 36.
533154-01-1
147
148
ACCESS PANELS: 191BB, 191EB, 192EB, 192FB
MLG DOORS FITTINGS
AF
DET
DETAILED INSPECTION OF HINGE AND ACTUATOR FITTINGS
FOR MLG DOORS AT KEELBEAM
533155-03-1
147
148
ACCESS PANELS: 734, 744
KEEL BEAM BOX ELLIPTICAL CUTOUT
SPECIAL DETAILED INSPECTION (HFEC) OF KEELBEAM BOX
ELLIPTICAL CUTOUT AT FR 46, LH/RH
ACCESS PANELS: 734, 744
NDT
SDI
1
533100-210-032
SOURCE:
MRB 533153-02-1
1
533100-210-014
SOURCE:
MRB 533154-01-1
533100-220-007
NTM 53-31-55
SOURCE:
ALI 533155-03-1
MRB 533155-03-1
Sub 2 - Page 130 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
533174-02-1
ZONE
260
DESCRIPTION
FUSELAGE - CENTER SECTION
SKILL TASK
CODE CODE
INTERVALS
SOURCE
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
AF
DET
T:
3500 FC
I:
3500 FC
CN
FAA AD
ISB
CN
F-2003-147(B)
FAA AD
2005-01-01
ISB 53-1147
1
2.80
1130
NDT
SDI
T:
48100 FC
OR
96200 FH
I:
6100 FC
OR
12200 FH
ALI WFD
533100-220-803
NTM 53-31-80
1
1
1.60
1.60
1130 1200
1379 1578
1657 1767
2151 2163
T:
48500 FC
OR
97000 FH
I:
17200 FC
OR
34400 FH
ALI WFD
1
1
1.40
1.40
1130 1200
1379 1578
1657 1767
2151 2163
T:
48000 FC
OR
96000 FH
I:
20000 FC
OR
40000 FH
MRB
1
1
0.75
0.75
1130 1200
1379 1578
1657 1767
2151 2163
DETAILED INSPECTION OF OVERWING EMERGENCY EXIT DOOR
FRAMES
NOTE:
- REFER TO SB 53-1147 FOR APPLICABLE MSN
- ALTERNATIVE REMOVAL OF RIVETS, INSPECTION AND
REWORK OF RIVET HOLES AS PER SB 53-1147
TERMINATES THIS INSPECTION REQUIREMENT
533180-01-1
145
146
ACCESS PANELS: 833, 834, 843, 844
UPPER SURFACES OF PRESSURE DECK MEMBRANES AND SIDE BOXES,
BETWEEN FR 42 AND FR 46
SPECIAL DETAILED INSPECTION (HFEC) OF UPPER SURFACE OF PRESSURE
DECK MEMBRANES AND SIDE BOXES, BETWEEN FR 42 AND FR 46, AT
CONNECTIONS TO LONGITUDINAL BEAMS AND SUPPORT RIBS (INCLUDING
LATERAL OUTER PART OF CONNECTION PLATES) AT Y=+/- 254 MM, Y=+/- 765
MM, Y=+/- 1292 MM AND Y=+/- 1650 MM
SOURCE:
ALI 533180-01-1
PREPARATION: CABIN FLOOR PANELS REMOVED; INSULATION REMOVED;
533181-01-1
147
148
LONGITUDINAL BEAMS FLANGES AT ATTACHMENT AREA TO PRESSURE DECK NDT
MEMBRANE BETWEEN FR 42 AND FR 46
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF LONGITUDINAL BEAMS FLANGES
AT ATTACHMENT AREA TO PRESSURE DECK MEMBRANE BETWEEN FR 42 AND
FR 46 AT Y=+/- 254 MM, Y=+/- 765MM, Y=+/- 1292 MM AND SIDE BOX FLANGE
AT Y=+/- 1650 MM
533100-220-802
NTM 53-31-81
SOURCE:
ALI 533181-01-1
PREPARATION: CABIN FLOOR PANELS REMOVED; INSULATION REMOVED;
ACCESS PANELS: 734, 744
533182-01-1
145
146
CENTER FUSELAGE
DETAILED INSPECTION OF CONNECTION PLATES AT FR 43, (EXCLUDING
LATERAL OUTER PART OF CONNECTION PLATES) BETWEEN Y=+/- 254 MM, AND
BETWEEN Y=+ 765 MM AND Y=+1292 MM, AND BETWEEN Y=- 765 MM AND Y=1292 MM (3 PLACES)
PREPARATION: CABIN FLOOR PANELS REMOVED; INSULATION REMOVED;
NDT
DET
533100-210-802
SOURCE:
MRB 533182-01-1
Sub 2 - Page 131 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
533185-01-2
ZONE
137
138
DESCRIPTION
PRESSURE DECK MEMBRANE UPPER SURFACE TO CENTER WING BOX,
UNDER TITANIUM ANGLE CONNECTION AND CORNER BRACKETS AT FR 36
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (LFEC AND ROTO) OF PRESSURE DECK
MEMBRANE UPPER SURFACE TO CENTER WING BOX, UNDER TITANIUM ANGLE
CONNECTION AND CORNER BRAKETS, AT FR 36
PREPARATION: AIR CONDITIONING
DUCTS REMOVED;
BOLTS REMOVED;
RECIRCULATION FILTER
REMOVED;
INSULATION REMOVED;
POTABLE WATER TANK
REMOVED;
533186-01-1
147
148
ACCESS PANELS: 131NW, 131PW, 132PW, 825
FR 35 FORWARD FACE TO PRESSURE BULKHEAD ATTACHMENTS
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF FR 35 FORWARD FACE TO
RESSURE BULKHEAD ATTACHMENTS, AROUND RIVETS AND HOLES BETWEEN
STR 28 AND STR 31, LH/RH
PREPARATION: AIR CONDITIONING DUCTS REMOVED; RECIRCULATION FILTER
REMOVED; INSULATION REMOVED;
533188-01-1
191
192
ACCESS PANELS: 131PW, 132PW
PRESSURE BULKHEAD, AFT FACE, LOWER PART OF VERTICAL STRUTS
AF
DET
DETAILED INSPECTION OF PRESSURE BULKHEAD, AFT FACE, LOWER PART OF
VERTICAL STRUTS (200 MM FROM BOTTOM) AT Y= +/-765 MM (2 PLACES)
INTERVALS
SOURCE
T:
48000 FC
OR
96000 FH
I:
31200 FC
OR
62500 FH
ALI
T:
40000 FC
OR
80000 FH
I:
15000 FC
OR
30000 FH
ALI
T:
30300 FC
I:
8400 FC
ALI
T:
26900 FC
OR
53800 FH
I:
21500 FC
OR
43000 FH
ALI
TPS
REFERENCES
533100-220-804
NTM 53-31-85
MEN
TASKM. APPLICABI
H.
LITY
1
1
1.20
1.20
1130 1200
1379 1578
1657 1767
1
1
2.92
2.92
ALL
1
1
0.30
0.30
ALL
1
1
0.55
0.55
ALL
SOURCE:
ALI 533185-01-2
533100-220-805
NTM 53-31-86
SOURCE:
ALI 533186-01-1
533100-220-806
SOURCE:
ALI 533188-01-1
NOTE: PRESSURE BULKHEAD FR 35.
ACCESS PANELS: 191BB, 191EB, 192EB, 192FB
533189-01-1
191
192
ANGLE FITTING ATTACHMENT AT FR 36 AT STRINGER STR 30
SPECIAL DETAILED INSPECTION (LFEC) OF ANGLE FITTING FORWARD
ATTACHMENT, AT FRAME 36 AT STRINGER 30, LH/RH
PREPARATION: AIR CONDITIONING DUCTS REMOVED;
ACCESS PANELS: 191BT, 192BT
NDT
SDI
533100-220-807
NTM 53-31-89
SOURCE:
ALI 533189-01-1
Sub 2 - Page 132 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
533500-01-1-SDM
533900-01-1
534103-01-1
ZONE
147
148
191
192
193
194
195
196
197
198
140
200
DESCRIPTION
FAIRINGS
SKILL TASK
CODE CODE
534106-01-1
SOURCE
TPS
REFERENCES
AF
DET
I:
750 FH
SPECI
533500-200-002
FUSELAGE DRAINAGE
AF
OPC
I:
24 MO
MRB 9
OPERATIONAL CHECK OF RUBBER FLAP DRAIN VALVE HOLES IN
PRESSURE FLOOR FROM MLG BAY
WINDOW FORGINGS FR 47-65
ST:
48000 FC
OR
96000 FH
SI:
17300 FC
OR
34600 FH
MRB
ST:
33600 FC
SI:
20000 FC
MRB
T:
51300 FC
OR
102700 FH
I:
12900 FC
OR
25800 FH
ALI
AF
DET
200
WINDOW FORGINGS FR 47/51-65
252
DETAILED INSPECTION OF VISIBLE PART OF WINDOW
FORGINGS AND FUSELAGE SKIN IN WINDOW FORGING AREA,
BETWEEN FR 47/51 AND FR 65, LH/RH, EXTERNAL SURFACE.
FRAME SPLICES FR 53-56
DETAILED INSPECTION OF FRAME SPLICES AND ADJACENT AREA LOCATED
ABOVE STRINGER 18 RH
NOTE: INSPECT AREA FROM FR 53 TO FR 56.
PREPARATION: INSULATION REMOVED;
AF
AF
DET
DET
MEN
TASKM. APPLICABI
H.
LITY
TBD
TBD
TBD
TBD
TBD
TBD
TBD
TBD
TBD
TBD
0.10
ALL
533900-210-001
1
1
1
1
1
1
1
1
1
1
1
SOURCE:
MRB 53.19.00/01
534100-210-016
1
0.50
1130 1200
1379 1578
1657 1767
2151 2163
1
0.50
1
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890
1130 1200
1379 1578
1657 1767
INSPECTION OF THE WING TO FUSELAGE FAIRINGS AND BELLY
FAIRING ACCESS PANELS FOR MISSING FASTENERS
DETAILED INSPECTION OF VISIBLE PART OF WINDOW
FORGINGS AND FUSELAGE SKIN IN WINDOW FORGING AREA,
BETWEEN FR 47 AND FR 65, LH/RH, EXTERNAL SURFACE
534103-01-3
INTERVALS
SOURCE:
MRB 534103-01-1
534100-210-016
SOURCE:
MRB 534103-01-3
534100-210-011
SOURCE:
ALI 534106-01-1
ALL
ACCESS PANELS: 252HW, 252LW, 252PW
Sub 2 - Page 133 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534106-01-5
ZONE
252
DESCRIPTION
FRAME SPLICES FR 53-56
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF FRAME SPLICES AND ADJACENT AREA LOCATED
ABOVE STRINGER 18 RH
INTERVALS
SOURCE
ST:
48000 FC
SI:
13600 FC
MRB
ST:
48000 FC
SI:
20000 FC
MRB
T:
6 YE
I:
6 YE
MRB CPCP
T:
3000 FC
I:
3000 FC
ALI
T:
3000 FC
I:
3000 FC
ALI
TPS
REFERENCES
534100-210-011
MEN
TASKM. APPLICABI
H.
LITY
1
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
1
2.00
2.00
ALL
1
0.50
1130 1200
1379 1578
1657 1767
2151 2163
1
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
MRB 534106-01-5
NOTE: INSPECT AREA FROM FR 53 TO FR 56.
THIS TASK IS AN ALTERNATIVE INSPECTION TO TASK 534106-02-1.
PREPARATION: INSULATION REMOVED;
534106-02-1
252
ACCESS PANELS: 252HW, 252LW, 252PW
FRAME SPLICES FR 53-56
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF FRAME SPLICES AND ADJACENT
AREA LOCATED ABOVE STRINGER 18
534100-220-004
NTM 53-41-06
SOURCE:
MRB 534106-02-1
NOTE: INSPECT AREA FROM FR 53 TO FR 56. THIS TASK IS AN ALTERNATIVE
INSPECTION TO TASK 534106-01-5.
PREPARATION: INSULATION REMOVED;
534107-01-1
153
154
ACCESS PANELS: 252HW, 252LW, 252PW
FUSELAGE INTERNAL STRUCTURE FR 46-65
AF
DET
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, BETWEEN FR 46
AND FR 65, INCLUDING AFT FACE OF PRESSURE BULKHEAD FROM STRINGER
38, LH/RH TO BOTTOM CENTER LINE.
1+2 534100-210-014
SOURCE:
MRB 534107-01-1
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
534107-01-4.
534108-01-2
534108-01-4
100
PREPARATION: CARGO FLOOR PANELS REMOVED; ACT(S) REMOVED (IF
INSTALLED);
FUSELAGE EXTERNAL SURFACE FR 47-70
100
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, BETWEEN FR 47 AND FR 70, FROM STRINGER 23,
LH/RH TO BOTTOM CENTERLINE, EXCEPT AREA COVERED BY
BELLY FAIRING
FUSELAGE EXTERNAL SURFACE FR 47/51-70
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, BETWEEN FR 47/51 AND FR 70, FROM STRINGER
23, LH/RH TO BOTTOM CENTERLINE, EXCEPT AREA COVERED
BY BELLY FAIRING
AF
AF
GVI
GVI
534100-210-810
SOURCE:
ALI 534108-01-2
534100-210-810
SOURCE:
ALI 534108-01-4
Sub 2 - Page 134 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534109-01-1
ZONE
263
264
DESCRIPTION
UPPER SEGMENT OF FR 70
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF UPPER SEGMENT OF FR 70, FIN TO
FUSELAGE FORWARD ATTACHMENT FITTINGS AND AREA BETWEEN
FR 69 AND FR 70, FROM STRINGER 6, LH/RH TO CROWN
CENTER LINE, INTERNAL STRUCTURE
534110-01-1
200
323
PREPARATION: GALLEYS; INSULATION REMOVED; TOILET
REMOVAL/INSTALLATION ;
CIRCUMFERENTIAL SKIN SPLICE AT FR 70
AF
DET
DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL SPLICE
AT FR 70, BETWEEN STRINGER 10, LH/RH AND CROWN CENTER
LINE, INCLUDING CUTOUT CORNERS FOR FIN ATTACHMENTS,
EXTERNAL SURFACE
534111-01-1
200
ACCESS PANELS: 323AL, 323AR
ADF2 ANTENNA SKIN CUTOUT
AF
DET
DETAILED INSPECTION OF SKIN AROUND ADF2 ANTENNA CUTOUT, BETWEEN
STRINGER 1, LH/RH, EXTERNAL SURFACE
NOTE: INSPECTION BETWEEN FR 48 AND FR 49. FOR PRE 20053 AIRCRAFT
RETROFITTED, THRESHOLD IS TO BE COUNTED FROM SB EMBODIMENT.
534111-01-3
200
PREPARATION: COVER OF ANTENNA AND ANTENNA REMOVED;
ADF2 ANTENNA SKIN CUTOUT
DETAILED INSPECTION OF SKIN AROUND ADF2 ANTENNA CUTOUT, BETWEEN
STRINGER 1, LH/RH, EXTERNAL SURFACE
NOTE: INSPECTION BETWEEN FR 52 AND FR 53. FOR PRE 20053 AIRCRAFT
RETROFITTED, THRESHOLD IS TO BE COUNTED FROM SB EMBODIMENT.
PREPARATION: COVER OF ANTENNA AND ANTENNA REMOVED;
AF
DET
INTERVALS
SOURCE
ST:
48000 FC
SI:
20000 FC
MRB
ST:
48000 FC
SI:
20000 FC
MRB
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
ST:
12 YE
SI:
12 YE
T:
24 YE
OR
28800 FC
OR
60000 FH
I:
12 YE
OR
16700 FC
OR
41700 FH
ALI
MRB CPCP
TPS
REFERENCES
534100-210-036
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.30
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.30
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.30
1130 1578
1657 1767
1
0.30
0649 1743
1761 1890
SOURCE:
MRB 534109-01-1
534100-210-018
SOURCE:
MRB 534110-01-1
534100-210-002
SOURCE:
MRB 534111-01-1
534100-210-002
SOURCE:
ALI 534111-01-3
MRB 534111-01-3
Sub 2 - Page 135 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534111-01-7
ZONE
200
DESCRIPTION
ADF2 ANTENNA SKIN CUTOUT
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF SKIN AROUND ADF2 ANTENNA
CUTOUT, BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE
NOTE: INSPECTION BETWEEN FR 48 AND FR 49.
PREPARATION: COVER OF ANTENNA AND
ANTENNA REMOVED;
534112-01-1
200
VHF3 ANTENNA SKIN CUTOUT
AF
DET
DETAILED INSPECTION OF SKIN AROUND VHF 3 ANTENNA CUTOUT, BETWEEN
STRINGER 1, LH/RH, EXTERNAL SURFACE
NOTE: INSPECTION BETWEEN FR 52 AND FR 53.
534112-01-3
200
PREPARATION: ANTENNA REMOVED;
VHF3 ANTENNA SKIN CUTOUT
DETAILED INSPECTION OF SKIN AROUND VHF 3 ANTENNA CUTOUT, BETWEEN
STRINGER 1, LH/RH, EXTERNAL SURFACE
NOTE: INSPECTION BETWEEN FR 56 AND FR 57.
PREPARATION: ANTENNA REMOVED;
AF
DET
INTERVALS
ST:
12 YE
SI:
12 YE
T:
24 YE
OR
28800 FC
OR
60000 FH
I:
12 YE
OR
16700 FC
OR
41700 FH
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
ST:
12 YE
SI:
12 YE
T:
24 YE
OR
31200 FC
OR
60000 FH
I:
12 YE
OR
18700 FC
OR
56100 FH
SOURCE
ALI
MRB CPCP
TPS
REFERENCES
534100-210-002
MEN
TASKM. APPLICABI
H.
LITY
1
0.30
2151 2163
1
0.30
1130 1200
1379 1578
1657 1767
1
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
ALI 534111-01-7
MRB 534111-01-7
MRB CPCP
534100-210-019
SOURCE:
MRB 534112-01-1
ALI
MRB CPCP
534100-210-019
SOURCE:
ALI 534112-01-3
MRB 534112-01-3
Sub 2 - Page 136 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534112-01-7
ZONE
200
DESCRIPTION
VHF3 ANTENNA SKIN CUTOUT
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF SKIN AROUND VHF 3 ANTENNA
CUTOUT, BETWEEN STRINGER
1, LH/RH, EXTERNAL SURFACE
NOTE INSPECTION BETWEEN FR 52 AND FR 53.
CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF
TASK 534112-01-1.
PREPARATION: ANTENNA REMOVED;
534113-01-1
200
CIRCUMFERENTIAL SKIN SPLICE AT FR 64
AF
DET
DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL SPLICE
AND STRINGER COUPLING AREAS AT FR 64, FROM STRINGER
10, LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE
534118-01-4
200
REAR FUSELAGE
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL SURFACE, BETWEEN
STRINGER 23, LH/RH TO CROWN CENTER LINE
534118-01-5
200
NOTE: INSPECTION FROM FR 47 TO FR 70.
REAR FUSELAGE
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL SURFACE, BETWEEN
STRINGER 23, LH/RH TO CROWN CENTER LINE
534121-01-1
200
NOTE: INSPECTION FROM FR 47/51 TO FR 70.
CIRCUMFERENTIAL SKIN SPLICE AT FR 64
SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE PLATE AT
CIRCUMFERENTIAL SKIN SPLICE AT FR 64, FROM STRINGER
10, LH/RH TO CROWN CENTERLINE
NDT
SDI
INTERVALS
SOURCE
ST:
12 YE
SI:
12 YE
T:
24 YE
OR
31200 FC
OR
60000 FH
I:
12 YE
OR
18700 FC
OR
56100 FH
ST:
30000 FC
SI:
13500 FC
T:
40000 FC
I:
13500 FC
T:
30000 FC
I:
3000 FC
ALI
MRB CPCP
T:
30000 FC
I:
3000 FC
MRB
ST:
41300 FC
OR
82600 FH
SI:
15000 FC
OR
30000 FH
MRB
TPS
REFERENCES
534100-210-019
MEN
TASKM. APPLICABI
H.
LITY
1
0.30
2151 2163
1
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
0
N/A
1130 1200
1379 1578
1657 1767
2151 2163
0
N/A
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.70
1130 1200
1379 1578
1657
SOURCE:
ALI 534112-01-7
MRB 534112-01-7
ALI
MRB
534100-210-020
SOURCE:
ALI 534113-01-1
MRB 534113-01-1
MRB
534100-210-823
SOURCE:
MRB 534118-01-4
534100-210-823
SOURCE:
MRB 534118-01-5
534100-220-010
NTM 53-41-21
SOURCE:
MRB 534121-01-1
Sub 2 - Page 137 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534121-01-4
ZONE
200
DESCRIPTION
REAR FUSELAGE
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE PLATE AT
CIRCUMFERENTIAL SKIN SPLICE AT FR 64, FROM STRINGER 10, LH/RH TO
CROWN CENTERLINE
534123-01-2
261
262
263
264
REAR FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTO) OF FUSELAGE INTERNAL STRUCTURE,
FRAME 66 AND FRAME 68 INNER CAP JOINT TO GUSSETS PLATE FROM
STRINGER 10 TO STRINGER 16, LH/RH
PREPARATION: BOLTS REMOVED; INSULATION REMOVED; LINING REMOVED;
INTERVALS
SOURCE
ST:
30000 FC
SI:
15000 FC
T:
40000 FC
I:
15000 FC
ST:
30000 FC
OR
60000 FH
SI:
8300 FC
OR
16600 FH
ALI
MRB
ST:
40000 FC
OR
80000 FH
SI:
10600 FC
OR
21200 FH
MRB
T:
28300 FC
OR
56600 FH
I:
6600 FC
OR
13200 FH
ALI
T:
32700 FC
OR
65400 FH
I:
7500 FC
OR
15000 FH
ALI
TPS
REFERENCES
534100-220-010
NTM 53-41-21
MEN
TASKM. APPLICABI
H.
LITY
1
0.70
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
1
1
0.33
0.33
0.33
0.33
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
1
1
0.33
0.33
0.33
0.33
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.67
0.67
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.67
0.67
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
ALI 534121-01-4
MRB 534121-01-4
MRB
534100-220-802
NTM 53-41-23
SOURCE:
MRB 534123-01-2
ACCESS PANELS: 832, 842
534123-01-3
261
262
263
264
REAR FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTO) OF FUSELAGE INTERNAL STRUCTURE,
FRAME 66 AND FRAME 68 INNER CAP JOINT TO GUSSETS PLATE FROM
STRINGER 10 TO STRINGER 16, LH/RH
PREPARATION: BOLTS REMOVED; INSULATION REMOVED; LINING REMOVED;
534100-220-802
NTM 53-41-23
SOURCE:
MRB 534123-01-3
ACCESS PANELS: 832, 842
534124-01-2
263
264
REAR FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF AFT PASSENGER/CREW DOOR
CUTOUT, AFT UPPER CORNER BETWEEN STRINGER 8 AND STRINGER 10,
FRAME 68 WEB JOINT TO DOOR FRAME, AFT FACE, LH/RH
PREPARATION: INSULATION REMOVED; LINING REMOVED;
534124-01-3
263
264
ACCESS PANELS: 832, 842
REAR FUSELAGE
SPECIAL DETAILED INSPECTION (HFEC) OF AFT PASSENGER/
CREW DOOR CUTOUT, AFT UPPER CORNER BETWEEN STRINGER 8 AND
STRINGER 10, FRAME 68 WEB JOINT TO DOOR FRAME, AFT FACE, LH/RH
PREPARATION: INSULATION REMOVED; LINING REMOVED;
NDT
SDI
534100-220-808
NTM 53-41-24
SOURCE:
ALI 534124-01-2
534100-220-808
NTM 53-41-24
SOURCE:
ALI 534124-01-3
ACCESS PANELS: 832, 842
Sub 2 - Page 138 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534125-01-2
534125-01-3
ZONE
100
263
264
100
DESCRIPTION
REAR FUSELAGE
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE SKIN EXTERNAL
SURFACE AT WATER SERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND
FRAME 66 AT AND BELOW STRINGER 37, TWO UPPER RIVET ROWS AT SKIN TO
REINFORCEMENT JOINT, LH
REAR FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE SKIN EXTERNAL
SURFACE AT WATER SERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND
FRAME 66 AT AND BELOW STRINGER
37, TWO UPPER RIVET ROWS AT SKIN TO REINFORCEMENT
JOINT, LH
534126-01-2
100
REAR FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE SKIN EXTERNAL
SURFACE AT WASTE SERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND
FRAME 66 BELOW STRINGER 33, TWO UPPER RIVET ROWS AT SKIN TO
REINFORCEMENT JOINT, RH
534126-01-3
100
REAR FUSELAGE
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE SKIN EXTERNAL
SURFACE AT WASTE SERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND
FRAME 66 BELOW STRINGER 33, TWO UPPER RIVET ROWS AT SKIN TO
REINFORCEMENT JOINT, RH
NDT
SDI
INTERVALS
T:
32100 FC
OR
60000 FH
I:
3000 FC
OR
6000 FH
ST:
30000 FC
OR
60000 FH
SI:
3200 FC
OR
6400 FH
T:
36100 FC
OR
72200 FH
I:
3200 FC
OR
6400 FH
T:
28700 FC
OR
57400 FH
I:
2200 FC
OR
4400 FH
T:
30900 FC
OR
61800 FH
I:
2300 FC
OR
4600 FH
SOURCE
ALI WFD
TPS
REFERENCES
534100-220-809
NTM 53-41-25
MEN
TASKM. APPLICABI
H.
LITY
1
1.14
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1.14
1130 1200
1379 1578
1657 1767
2151 2163
1
1.30
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1.30
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
ALI 534125-01-2
ALI WFD
MRB
534100-220-809
NTM 53-41-25
SOURCE:
ALI 534125-01-3
MRB 534125-01-3
ALI WFD
534100-220-810
NTM 53-41-26
SOURCE:
ALI 534126-01-2
ALI WFD
534100-220-810
NTM 53-41-26
SOURCE:
ALI 534126-01-3
Sub 2 - Page 139 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534127-01-2
ZONE
263
264
DESCRIPTION
REAR FUSELAGE
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE
INTERNAL STRUCTURE, LATERAL FRAME 68 JOINT TO UPPER
FRAME 68 BETWEEN STRINGER 4 AND STRINGER 5, LH/RH
PREPARATION: INSULATION REMOVED; LINING REMOVED;
534127-01-3
263
264
ACCESS PANELS: 832, 842
REAR FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE INTERNAL STRUCTURE,
LATERAL FRAME 68 JOINT TO UPPER FRAME 68 BETWEEN STRINGER 4 AND
STRINGER 5, LH/RH
PREPARATION: INSULATION REMOVED; LINING REMOVED;
534128-01-4
200
ACCESS PANELS: 832, 842
FUSELAGE SKIN BETWEEN FR 64 AND 70
AF
DET
DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE BETWEEN
FRAME 64 AND FRAME 70 FROM STRINGER 6 TO CROWN CENTER LINE, LH/RH
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
534128-01-5
INTERVALS
SOURCE
T:
27700 FC
OR
55400 FH
I:
5700 FC
OR
11400 FH
ALI
T:
28700 FC
OR
57400 FH
I:
5800 FC
OR
11600 FH
ALI
ST:
47600 FC
OR
60000 FH
SI:
29300 FC
OR
58600 FH
MRB
ST:
48600 FC
OR
97200 FH
SI:
29500 FC
OR
59000 FH
MRB
TPS
REFERENCES
534100-220-811
NTM 53-41-27
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.20
0.20
1130 1200
1379 1578
1657 1767
2151 2163
1
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.30
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
ALI 534127-01-2
534100-220-811
NTM 53-41-27
SOURCE:
ALI 534127-01-3
534100-210-806
SOURCE:
MRB 534128-01-4
ACCESS PANELS: 321AL
534128-01-6
200
FUSELAGE SKIN BETWEEN FR 64 AND 70
DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE BETWEEN
FRAME 64 AND FRAME 70 FROM STRINGER 6 TO CROWN CENTER LINE, LH/RH
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
534128-01-1
AF
DET
534100-210-806
SOURCE:
MRB 534128-01-6
ACCESS PANELS: 321AL
Sub 2 - Page 140 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534129-01-2
ZONE
261
262
DESCRIPTION
REAR FUSELAGE
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTO) OF AFT PASSENGER/CREW DOOR
CUTOUT, DOOR STOP FITTINGS HOLES AT FRAME 66 WEB, LH/RH
PREPARATION: BOLTS REMOVED; LINING REMOVED;
ACCESS PANELS: 832, 842
534129-01-3
261
262
REAR FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTO) OF AFT PASSENGER/CREW DOOR
CUTOUT, DOOR STOP FITTINGS HOLES AT FRAME 66 WEB, LH/RH
PREPARATION: BOLTS REMOVED; LINING REMOVED;
ACCESS PANELS: 832, 842
534130-01-2
261
262
REAR FUSELAGE
SPECIAL DETAILED INSPECTION (ROTO) OF AFT
PASSENGER/CREW DOOR CUTOUT, DOOR STOP FITTINGS HOLES
AT FRAME 68 WEB, LH/RH
PREPARATION: BOLTS REMOVED; LINING REMOVED;
NDT
SDI
INTERVALS
ST:
30000 FC
OR
60000 FH
SI:
8300 FC
OR
16600 FH
T:
40200 FC
OR
60000 FH
I:
8300 FC
OR
16600 FH
ST:
30000 FC
OR
60000 FH
SI:
9700 FC
OR
19400 FH
T:
48000 FC
OR
96000 FH
I:
9700 FC
OR
19400 FH
T:
34100 FC
OR
60000 FH
I:
8300 FC
OR
16600 FH
SOURCE
ALI
MRB
TPS
REFERENCES
534100-220-812
NTM 53-41-29
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.47
0.47
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.47
0.47
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.47
0.47
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
ALI 534129-01-2
MRB 534129-01-2
ALI
MRB
534100-220-812
NTM 53-41-29
SOURCE:
ALI 534129-01-3
MRB 534129-01-3
ALI
534100-220-813
NTM 53-41-30
SOURCE:
ALI 534130-01-2
ACCESS PANELS: 832, 842
Sub 2 - Page 141 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534130-01-3
ZONE
261
262
DESCRIPTION
REAR FUSELAGE
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTO) OF AFT PASSENGER/CREW DOOR
CUTOUT, DOOR STOP FITTINGS HOLES AT FRAME 68 WEB, LH/RH
PREPARATION: BOLTS REMOVED; LINING REMOVED;
ACCESS PANELS: 832, 842
534131-01-1
100
200
FUSELAGE SKIN BETWEEN FR 65 AND 70
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AROUND AFT
PASSENGER/CREW DOOR CUTOUTS, BETWEEN FR 65 AND FR 70
AND FROM STRINGER 6 TO STRINGER 26, EXTERNAL SURFACE
(EXCEPT AREA UNDER SCUFF PLATE), LH/RH
534131-01-3
100
200
FUSELAGE SKIN BETWEEN FR 65 AND 70
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AROUND AFT
PASSENGER/CREW DOOR CUTOUTS, BETWEEN FR 65 AND FR 70
AND FROM STRINGER 6 TO STRINGER 26, EXTERNAL SURFACE
(EXCEPT AREA UNDER SCUFF PLATE), LH/RH
534132-01-4
260
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS
ACCOMPLISHMENT OF TASK 534131-01-1.
AFT PAX/CREW DOOR CUTOUT UPR CORNER
DETAILED INSPECTION OF AFT PASSENGER/CREW DOOR
CUTOUT, UPPER CORNERS, INCLUDING SKIN AND INTERNALLY
THE VISIBLE PORTION OF THE INTERNAL DOUBLER, LH/RH
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS
ACCOMPLISHMENT OF TASK 534132-01-1.
AF
DET
INTERVALS
SOURCE
ST:
30000 FC
OR
60000 FH
SI:
9700 FC
OR
19400 FH
T:
40900 FC
OR
81800 FH
I:
9700 FC
OR
19400 FH
T:
23800 FC
OR
47600 FH
I:
23800 FC
OR
47600 FH
T:
23100 FC
OR
46200 FH
I:
23100 FC
OR
46200 FH
ALI
MRB
T:
16300 FC
OR
32600 FH
I:
10300 FC
OR
20600 FH
ALI
TPS
REFERENCES
534100-220-813
NTM 53-41-30
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.47
0.47
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.50
0.50
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.15
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
ALI 534130-01-3
MRB 534130-01-3
ALI
534100-210-814
SOURCE:
ALI 534131-01-1
ALI
534100-210-814
SOURCE:
ALI 534131-01-3
534100-210-010
SOURCE:
ALI 534132-01-4
ACCESS PANELS: 832, 842
Sub 2 - Page 142 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534132-01-6
ZONE
260
DESCRIPTION
AFT PAX/CREW DOOR CUTOUT UPR CORNER
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF AFT PASSENGER/CREW DOOR
CUTOUT, UPPER CORNERS, INCLUDING SKIN AND INTERNALLY
THE VISIBLE PORTION OF THE INTERNAL DOUBLER, LH/RH
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS
ACCOMPLISHMENT OF TASK 534132-01-3.
534133-01-6
170
260
ACCESS PANELS: 832, 842
AFT PAX/CREW DOOR CUTOUT LWR CORNER
AF
DET
DETAILED INSPECTION OF AFT PASSENGER/CREW DOOR
CUTOUT, LOWER CORNERS, INCLUDING SKIN AND DOUBLER
UNDERNEATH THE SCUFF PLATE, LH/RH
PREPARATION: CORNER SCUFF PLATES REMOVED;
534133-02-2
170
260
ACCESS PANELS: 832, 842
REAR FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC & X-RAY) OF AFT PASSENGER/CREW
DOOR CUTOUT, LOWER CORNERS, INCLUDING SKIN AND DOUBLER
UNDERNEATH THE SCUFF PLATE, LH/RH
NOTE: SPECIAL DETAILED INSPECTION IS FOR DOUBLER WHICH IS NOT
VISIBLE WITH DETAILED INSPECTION.
INTERVALS
SOURCE
T:
12400 FC
OR
24800 FH
I:
7700 FC
OR
15400 FH
ALI
ST:
48000 FC
OR
60000 FH
SI:
23800 FC
OR
47600 FH
MRB
ST:
48000 FC
OR
60000 FH
SI:
39600 FC
OR
60000 FH
MRB
T:
12 YE
I:
12 YE
MRB CPCP
TPS
REFERENCES
534100-210-010
MEN
TASKM. APPLICABI
H.
LITY
1
0.15
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.25
0.25
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.60
0.60
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.25
0.25
ALL
SOURCE:
ALI 534132-01-6
534100-210-021
SOURCE:
MRB 534133-01-6
534100-220-008
NTM 53-41-33
SOURCE:
MRB 534133-02-2
PREPARATION: CORNER SCUFF PLATES REMOVED;
LINING AND INSULATION REMOVED;
534134-01-1
261
262
ACCESS PANELS: 832, 842
DOOR STOP FITTINGS FR 66 AND 68
DETAILED INSPECTION OF DOOR STOP FITTINGS ON FR 66
AND FR 68, LH/RH
AF
DET
534100-210-029
SOURCE:
MRB 534134-01-1
PREPARATION: LINING REMOVED;
ACCESS PANELS: 832, 842
Sub 2 - Page 143 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534135-01-4
ZONE
261
262
263
264
DESCRIPTION
AFT PAX/CREW DOOR CUTOUT
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND AFT
PASSENGER/CREW DOOR CUTOUT, ABOVE CABIN FLOOR LEVEL, BETWEEN
FR 65 AND FR 69 AND FROM STRINGER 6 TO STRINGER 23, LH/RH, EXCLUDING
THE LOWER CORNERS OF THE DOOR ENTRANCE AREA AT FR 66 AND FR 68,
BETWEEN STRINGER 22 AND 23, LH/RH
INTERVALS
SOURCE
T:
6 YE
I:
6 YE
MRB CPCP
T:
12 YE
I:
12 YE
MRB CPCP
ST:
30000 FC
OR
60000 FH
SI:
24900 FC
OR
49800 FH
T:
57700 FC
OR
115400 FH
I:
24900 FC
OR
49800 FH
ALI
MRB
TPS
1
REFERENCES
534100-210-003
MEN
TASKM. APPLICABI
H.
LITY
0.50
0.50
0.50
0.50
ALL
SOURCE:
MRB 534135-01-4
1
1
1
1
534100-210-041
1
0.30
ALL
1
0.25
1130 1200
1379 1578
1657 1767
2151 2163
NOTE: EXCLUDED AREA COVERED BY TASKS 534143-01-1 OR 534143-01-3.
PREPARATION: LINING AND INSULATION REMOVED;
534136-01-1
100
ACCESS PANELS: 832, 842
AFT PAX/CREW DOOR UNDER SCUFF-PLATE
AF
DET
DETAILED INSPECTION OF AFT PASSENGER/CREW DOOR
CUTOUT, UNDERNEATH THE SCUFF PLATE, LH/RH
SOURCE:
MRB 534136-01-1
PREPARATION: SCUFF PLATE;
534137-01-1
100
ACCESS PANELS: 832, 842
WASTE SERVICE PANEL CUTOUT
SPECIAL DETAILED INSPECTION (LFEC) OF INTERNAL
DOUBLER, FORWARD AND AFT OF WASTE SERVICE PANEL
CUTOUT, BETWEEN STRINGER 35 AND STRINGER 39, RH
NDT
SDI
534100-220-009
NTM 53-41-37
SOURCE:
ALI 534137-01-1
MRB 534137-01-1
Sub 2 - Page 144 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534137-01-3
ZONE
100
DESCRIPTION
REAR FUSELAGE
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (LFEC) OF INTERNAL
DOUBLER, FORWARD AND AFT OF WASTE SERVICE PANEL
CUTOUT, BETWEEN STRINGER 35 AND STRINGER 39, RH
534139-01-1
100
WATER SERVICE PANEL CUTOUT AFT DOUBLER
NDT
SDI
SPECIAL DETAILED INSPECTION (LFEC) OF INTERNAL
DOUBLER, FORWARD AND AFT OF WATER SERVICE PANEL
CUTOUT, BETWEEN STRINGER 38 AND STRINGER 42, LH
534139-01-2
100
REAR FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (LFEC) OF INTERNAL DOUBLER, FORWARD
AND AFT OF WATER SERVICE PANEL CUTOUT, BETWEEN STRINGER 38 AND
STRINGER 42, LH.
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
534139-01-1.
534140-01-6
100
FUSELAGE SKIN AROUND OUTFLOW VALVE CUTOUT
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AROUND OUTFLOW VALVE
CUTOUT, BETWEEN FR 65 AND FR 66 AND FROM STRINGER 26 TO STRINGER
31, RH, EXTERNAL SURFACE
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
534140-01-3.
AF
GVI
INTERVALS
SOURCE
ST:
30000 FC
OR
60000 FH
SI:
25500 FC
OR
51000 FH
T:
41900 FC
OR
60000 FH
I:
25500 FC
OR
51000 FH
ST:
60000 FC
OR
120000 FH
SI:
31400 FC
OR
62800 FH
ALI
MRB
ST:
48000 FC
OR
60000 FH
SI:
22800 FC
OR
45600 FH
MRB
T:
38400 FC
OR
60000 FH
I:
3000 FC
OR
6000 FH
ALI
TPS
REFERENCES
534100-220-009
NTM 53-41-37
MEN
TASKM. APPLICABI
H.
LITY
1
0.25
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.25
1130 1200
1379 1578
1657 1767
2151 2163
1
0.25
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.15
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
ALI 534137-01-3
MRB 534137-01-3
MRB
534100-220-007
NTM 53-41-39
SOURCE:
MRB 534139-01-1
534100-220-007
NTM 53-41-39
SOURCE:
MRB 534139-01-2
534100-210-815
SOURCE:
ALI 534140-01-6
Sub 2 - Page 145 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534140-01-8
ZONE
100
DESCRIPTION
FUSELAGE SKIN AROUND OUTFLOW VALVE CUTOUT
SKILL TASK
CODE CODE
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AROUND OUTFLOW VALVE
CUTOUT, BETWEEN FR 65 AND FR 66 AND FROM STRINGER 26 TO STRINGER
31, RH, EXTERNAL SURFACE
534141-01-5
100
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
534140-01-1 OR 534140-01-4.
FUSELAGE SKIN AROUND WATER SERVICE PANEL
CUTOUT
AF
DET
DETAILED INSPECTION OF FUSELAGE SKIN AROUND WATER
SERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND FRAME 66
AND FROM STRINGER 37 TO STRINGER 43, LH, EXTERNAL
SURFACE
534141-01-8
100
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS
ACCOMPLISHMENT OF TASK 534141-01-1.
FUSELAGE SKIN AROUND WATER SERVICE PANEL
CUTOUT
AF
DET
DETAILED INSPECTION OF FUSELAGE SKIN AROUND WATER
SERVICE PANEL CUTOUT, BETWEEN FRAME 65 AND FRAME 66
AND FROM STRINGER 37 TO STRINGER 43, LH, EXTERNAL
SURFACE
534142-01-8
100
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS
ACCOMPLISHMENT OF TASK 534141-01-4.
FUSELAGE SKIN AROUND WASTE SERVICE PANEL
CUTOUT
DETAILED INSPECTION OF FUSELAGE SKIN AROUND WASTE
SERVICE PANEL CUTOUT, BETWEEN FR 65 AND FR 66 AND
FROM STRINGER 33 TO STRINGER 40, RH, EXTERNAL SURFACE
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS
ACCOMPLISHMENT OF TASK 534142-01-4.
AF
DET
INTERVALS
SOURCE
T:
35600 FC
OR
71200 FH
I:
3200 FC
OR
6400 FH
T:
29600 FC
OR
59200 FH
I:
10700 FC
OR
21400 FH
ALI
T:
25700 FC
OR
51400 FH
I:
9500 FC
OR
19000 FH
ALI
T:
33000 FC
OR
60000 FH
I:
12900 FC
OR
25800 FH
ALI
TPS
REFERENCES
534100-210-815
MEN
TASKM. APPLICABI
H.
LITY
1
0.15
1130 1200
1379 1578
1657 1767
2151 2163
1
0.15
1130 1200
1379 1578
1657 1767
2151 2163
1
0.15
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.15
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
ALI 534140-01-8
ALI
534100-210-816
SOURCE:
ALI 534141-01-5
534100-210-816
SOURCE:
ALI 534141-01-8
534100-210-817
SOURCE:
ALI 534142-01-8
Sub 2 - Page 146 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534142-01-9
ZONE
100
DESCRIPTION
FUSELAGE SKIN AROUND WASTE SERVICE PANEL
CUTOUT
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF FUSELAGE SKIN AROUND WASTE
SERVICE PANEL CUTOUT, BETWEEN FR 65 AND FR 66 AND
FROM STRINGER 33 TO STRINGER 40, RH, EXTERNAL
SURFACE
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS
ACCOMPLISHMENT OF TASK 534142-01-5 OR 534142-01-1.
534143-01-1
261
262
FUSELAGE INTERNAL STRUCTURE FR 66-68
DETAILED INSPECTION OF AFT PASSENGER/CREW DOOR CUTOUT LOWER
CORNERS INTERNAL STRUCTURE, ABOVE CABIN FLOOR LEVEL, AT FR 66 AND
FR 68 FROM STRINGER 22 TO STRINGER 23 AND AROUND GIRT BAR FITTINGS,
LH/RH
AF
DET
INTERVALS
ST:
30000 FC
OR
60000 FH
SI:
13700 FC
OR
27400 FH
T:
35400 FC
OR
70800 FH
I:
13700 FC
OR
27400 FH
T:
5 YE
I:
5 YE
SOURCE
ALI
MRB
TPS
REFERENCES
534100-210-817
MEN
TASKM. APPLICABI
H.
LITY
1
0.15
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.20
0.20
0649 1130
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
SOURCE:
ALI 534142-01-9
MRB 534142-01-9
MRB CPCP
1+2 534100-210-834
SOURCE:
MRB 534143-01-1
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
534135-01-4 IN CASE THIS INSPECTION WAS PERFORMED PRIOR JUNE 2004.
PREPARATION: LINING AND INSULATION REMOVED; GIRT BAR FITTING
REMOVED; BLANKING PLATE REMOVED;
ACCESS PANELS: 832, 842
Sub 2 - Page 147 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534143-01-3
ZONE
261
262
DESCRIPTION
FUSELAGE INTERNAL STRUCTURE FR 66-68
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF AFT PASSENGER/CREW DOOR CUTOUT LOWER
CORNERS INTERNAL STRUCTURE, ABOVE CABIN FLOOR LEVEL, AT FR 66 AND
FR 68 FROM STRINGER 22 TO STRINGER 23 AND AROUND GIRT BAR FITTINGS,
LH/RH
INTERVALS
SOURCE
T:
6 YE
I:
6 YE
MRB CPCP
T:
6 YE
I:
6 YE
MRB CPCP
T:
12 YE
I:
12 YE
MRB CPCP
T:
12 YE
I:
12 YE
MRB CPCP
TPS
REFERENCES
1+2 534100-210-834
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
1200 1379
2151 2163
1
1
0.50
0.50
ALL
1
1
1
1
0.50
0.50
0.50
0.50
1130 1200
1379 1578
1657 1767
2151 2163
1
1
1
1
0.50
0.50
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
MRB 534143-01-3
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASKS
534135-01-4 OR 534143-01-1.
PREPARATION: LINING AND
INSULATION REMOVED;
GIRT BAR FITTING
REMOVED;
BLANKING PLATE
REMOVED;
534144-01-1
171
172
ACCESS PANELS: 832, 842
FUSELAGE INTERNAL STRUCTURE FR 65-70
AF
DET
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
BELOW CABIN FLOOR PANELS INCLUDING FLOOR STRUCTURE,
FROM FR 65 TO FR 70
1
534100-210-030
SOURCE:
MRB 534144-01-1
PREPARATION: INSULATION REMOVED;
534146-01-1
534146-01-2
251
252
261
262
251
252
261
262
ACCESS PANELS: 161DW, 162DW, 826
CABIN FLOOR STRUCTURE FR 47 TO FR 70
AF
GVI
GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE,
EXCLUDING AREAS BELOW GALLEYS AND TOILETS AND DOOR
ENTRANCE AREA, FROM FR 47 TO FR 70
PREPARATION: CABIN FLOOR PANELS;
CABIN FLOOR STRUCTURE FR 47/51 TO FR 70
GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE,
EXCLUDING AREAS BELOW GALLEYS AND TOILETS AND DOOR
ENTRANCE AREA, FROM FR 47/51 TO FR 70
AF
GVI
1
534100-210-801
SOURCE:
MRB 534146-01-1
1
534100-210-801
SOURCE:
MRB 534146-01-2
PREPARATION: CABIN FLOOR PANELS;
Sub 2 - Page 148 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534147-01-1
ZONE
251
252
261
262
DESCRIPTION
FLOOR STRUCTURE FR 47 TO 70
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF CABIN FLOOR STRUCTURE, BELOW
AND 0.5M AROUND GALLEYS AND TOILETS, FROM FR 47 TO
FR 70, EXCEPT AREA BETWEEN FR 66 AND FR 68 AND
LATERAL SHEAR PLATES BETWEEN FR 68 AND FR 70.
INTERVALS
SOURCE
T:
6 YE
I:
6 YE
MRB CPCP
T:
6 YE
I:
6 YE
MRB CPCP
T:
6 YE
I:
6 YE
MRB CPCP
T:
6 YE
I:
6 YE
MRB CPCP
TPS
REFERENCES
1+2 534100-210-037
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
1.50
1.50
1.50
1.50
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
MRB 534147-01-2
1
1
1
1
1.50
1.50
1.50
1.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
534100-210-802
1
4.00
1130 1200
1379 1578
1657 1767
2151 2163
1
4.00
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
MRB 534147-01-1
NOTE: TASK ONLY APPLICABLE IF GALLEYS/TOILETS
INSTALLED
534147-01-2
251
252
261
262
PREPARATION: CABIN FLOOR PANELS; GALLEYS; TOILET
REMOVAL/INSTALLATION ;
FLOOR STRUCTURE FR 47/51 TO 70
AF
DET
DETAILED INSPECTION OF CABIN FLOOR STRUCTURE, BELOW
AND 0.5M AROUND GALLEYS AND TOILETS, FROM FR 47/51 TO
FR 70, EXCEPT AREA BETWEEN FR 66 AND FR 68 AND
LATERAL SHEAR PLATES BETWEEN FR 68 AND FR 70.
1+2 534100-210-037
NOTE: TASK ONLY APPLICABLE IF GALLEYS/TOILETS
INSTALLED
534148-01-1
190
PREPARATION: CABIN FLOOR PANELS; GALLEYS; TOILET
REMOVAL/INSTALLATION ;
FUSELAGE UNDER BELLY FAIRING
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, AND BELLY FAIRING SUPPORT STRUCTURE BETWEEN
FR 30 AND FR 53, UNDER THE BELLY FAIRING
534148-01-3
190
PREPARATION: BELLY FAIRING;
FUSELAGE UNDER BELLY FAIRING
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, AND BELLY FAIRING SUPPORT STRUCTURE (AND
PORTION OF AFT CARGO DOOR COVERED BY BELLY FAIRING)
BETWEEN FR 27 AND FR 57, UNDER THE BELLY FAIRING
AF
GVI
1
SOURCE:
MRB 534148-01-1
1
534100-210-802
SOURCE:
MRB 534148-01-3
PREPARATION: BELLY FAIRING;
Sub 2 - Page 149 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534150-01-1
ZONE
152
DESCRIPTION
AFT CARGO DOOR CUTOUT
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE AROUND AFT
CARGO DOOR CUTOUT
INTERVALS
SOURCE
T:
12 YE
I:
6 YE
MRB CPCP
T:
12 YE
I:
6 YE
MRB CPCP
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
TPS
1
REFERENCES
534100-210-004
MEN
TASKM. APPLICABI
H.
LITY
1
0.50
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.60
1130 1200
1379 1578
1657 1767
2151 2163
1
0.60
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
MRB 534150-01-1
NOTE: INSPECTION FROM FR 52 TO FR 57 AND BETWEEN STRINGER 23 AND
STRINGER 38.
PREPARATION: ACT; INSULATION REMOVED;
534150-01-2
152
162
ACCESS PANELS: 152DW, 152EF, 152FF, 152HW, 152MF, 152NF
AFT CARGO DOOR CUTOUT
AF
DET
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE AROUND AFT
CARGO DOOR CUTOUT
1
534100-210-004
SOURCE:
MRB 534150-01-2
NOTE: INSPECTION FROM FR 55 TO FR 60 AND BETWEEN STRINGER 23 AND
STRINGER 38.
PREPARATION: ACT; INSULATION REMOVED;
534152-01-2
252
ACCESS PANELS: 152TW, 152WG, 152XG, 162AW, 162BF, 162CF
AFT CARGO DOOR HINGE FITTINGS INTERNAL
AF
DET
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE AT
INTERNAL ATTACHMENT AREA OF AFT CARGO DOOR HINGE
FITTINGS, FROM FR 52 TO FR 57, BETWEEN STRINGER 22
AND STRINGER 23
PREPARATION: REAR ACT REMOVED (IF INSTALLED); INSULATION REMOVED;
534100-210-005
SOURCE:
MRB 534152-01-2
ACCESS PANELS: 252GW, 252KW, 252NW
534152-01-4
252
AFT CARGO DOOR HINGE FITTINGS INTERNAL
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE AT
INTERNAL ATTACHMENT AREA OF AFT CARGO DOOR HINGE
FITTINGS, FROM FR 55 TO FR 60, BETWEEN STRINGER 22
AND STRINGER 23
PREPARATION: REAR ACT REMOVED (IF INSTALLED); INSULATION REMOVED;
AF
DET
534100-210-005
SOURCE:
MRB 534152-01-4
ACCESS PANELS: 252NW, 252RW, 252UW
Sub 2 - Page 150 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534153-01-1
ZONE
152
DESCRIPTION
AFT CARGO DOOR HINGE FITTINGS EXTERNAL
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF FUSELAGE AFT CARGO DOOR HINGE
FITTINGS AND EXTERNAL ATTACHMENT AREA
NOTE: APPLICATION OF TPS IS LIMITED TO THE INNER SIDE
OF HINGE FITTINGS
PREPARATION: ACT;
534153-01-2
152
ACCESS PANELS: 826
AFT CARGO DOOR HINGE FITTINGS EXTERNAL
AF
DET
DETAILED INSPECTION OF FUSELAGE AFT CARGO DOOR HINGE
FITTINGS AND EXTERNAL ATTACHMENT AREA
NOTE: APPLICATION OF TPS IS LIMITED TO THE INNER SIDE
OF HINGE FITTINGS
PREPARATION: ACT;
534154-01-1
152
ACCESS PANELS: 826
REAR FUSELAGE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTO) OF FUSELAGE STRUCTURE AT
ATTACHMENT AREA UNDER AFT CARGO DOOR OUTER HINGE FITTINGS FROM
FR 55 TO FR 56 BETWEEN STRINGER 22 AND STRINGER 23
PREPARATION: BOLTS REMOVED; CEILING PANELS REMOVED; INSULATION
REMOVED; LINING REMOVED; REAR ACT REMOVED (IF INSTALLED);
INTERVALS
SOURCE
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
T:
48000 FC
OR
96000 FH
I:
39000 FC
OR
78000 FH
ALI
ST:
12 YE
OR
48000 FC
SI:
12 YE
OR
12200 FC
T:
24 YE
I:
12 YE
MRB CPCP
TPS
1
REFERENCES
534100-210-006
MEN
TASKM. APPLICABI
H.
LITY
1
0.40
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.40
1130 1200
1379 1578
1657 1767
2151 2163
1
0.25
1130 1200
1379 1578
1657 1767
2151 2163
1
0.27
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
MRB 534153-01-1
1
534100-210-006
SOURCE:
MRB 534153-01-2
534100-220-815
NTM 53-41-54
SOURCE:
ALI 534154-01-1
ACCESS PANELS: 252NW, 826
534155-01-2
154
AFT CARGO DOOR ECCENTRIC BOLTS
DETAILED INSPECTION OF AFT CARGO DOOR ECCENTRIC BOLTS
OF LOCKING MECHANISM AT LOCK FITTINGS, BETWEEN FR 53
AND FR 55 A (6 PLACES)
PREPARATION: ECCENTRIC BOLTS REMOVED;
ACCESS PANELS: 826
AF
DET
534100-210-025
SOURCE:
MRB 534155-01-2
Sub 2 - Page 151 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534155-01-4
ZONE
154
DESCRIPTION
AFT CARGO DOOR ECCENTRIC BOLTS
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF AFT CARGO DOOR ECCENTRIC BOLTS
OF LOCKING MECHANISM AT LOCK FITTINGS, BETWEEN FR 56
AND FR 58A (6 PLACES)
PREPARATION: ECCENTRIC BOLTS REMOVED;
ACCESS PANELS: 826
534156-01-1
154
AFT CARGO DOOR LOCK FITTING
AF
DET
DETAILED INSPECTION OF AFT CARGO DOOR LOCK FITTINGS
AND SURROUNDING STRUCTURE, BETWEEN FR 53 AND FR 55 A,
FROM STRINGER 41 RH TO DOOR SILL, INTERNAL PORTION (6
PLACES)
NOTE: THIS TASK IS AN ALTERNATIVE INSPECTION TO TASK
534156-02-1
INTERVALS
SOURCE
ST:
12 YE
OR
48000 FC
SI:
12 YE
OR
13100 FC
T:
24 YE
I:
12 YE
ST:
48000 FC
SI:
8400 FC
MRB CPCP
ST:
48000 FC
SI:
8400 FC
MRB
TPS
REFERENCES
534100-210-025
MEN
TASKM. APPLICABI
H.
LITY
1
0.27
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.90
1130 1200
1379 1578
1657 1767
2151 2163
1
0.90
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
MRB 534155-01-4
MRB
534100-210-012
SOURCE:
MRB 534156-01-1
PREPARATION: REAR ACT; CARGO FLOOR PANELS;
534156-01-2
154
ACCESS PANELS: 826
AFT CARGO DOOR LOCK FITTING
DETAILED INSPECTION OF AFT CARGO DOOR LOCK FITTINGS
AND SURROUNDING STRUCTURE, BETWEEN FR 56 AND FR 58 A,
FROM STRINGER 41 RH TO DOOR SILL, INTERNAL PORTION (6
PLACES)
NOTE: THIS TASK IS AN ALTERNATIVE INSPECTION TO TASK
534156-02-2
AF
DET
534100-210-012
SOURCE:
MRB 534156-01-2
PREPARATION: ACT; CARGO FLOOR PANELS;
ACCESS PANELS: 826
Sub 2 - Page 152 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534156-02-1
ZONE
154
DESCRIPTION
AFT CARGO DOOR LOCK FITTING
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF AFT CARGO DOOR
LOCK FITTINGS AND SURROUNDING STRUCTURE, BETWEEN FR
53 AND FR 55 A, FROM STRINGER 41 RH TO DOOR SILL,
INTERNAL PORTION (6 PLACES)
NOTE: THIS TASK IS AN ALTERNATIVE INSPECTION TO TASK
534156-01-1
INTERVALS
SOURCE
ST:
48000 FC
SI:
9600 FC
MRB
ST:
48000 FC
SI:
9600 FC
MRB
T:
14100 FC
OR
28300 FH
OR
6 YE
I:
14100 FC
OR
28300 FH
OR
6 YE
T:
13100 FC
OR
6 YE
I:
13100 FC
OR
6 YE
ALI
MRB CPCP
TPS
REFERENCES
534100-220-011
NTM 53-41-56
MEN
TASKM. APPLICABI
H.
LITY
1
0.35
1130 1200
1379 1578
1657 1767
2151 2163
1
0.35
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.15
1130 1200
1379 1578
1657 1767
2151 2163
1
0.15
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
MRB 534156-02-1
PREPARATION: REAR ACT; CARGO FLOOR PANELS;
534156-02-2
154
ACCESS PANELS: 826
AFT CARGO DOOR LOCK FITTING
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF AFT CARGO DOOR
LOCK FITTINGS AND SURROUNDING STRUCTURE, BETWEEN FR
56 AND FR 58 A, FROM STRINGER 41 RH TO DOOR SILL,
INTERNAL PORTION (6 PLACES)
NOTE: THIS TASK IS AN ALTERNATIVE INSPECTION TO TASK
534156-01-2
534100-220-011
NTM 53-41-56
SOURCE:
MRB 534156-02-2
PREPARATION: ACT; CARGO FLOOR PANELS;
534157-01-4
152
ACCESS PANELS: 826
AFT CARGO DOOR LOCK FITTING
AF
GVI
GENERAL VISUAL INSPECTION OF AFT CARGO DOOR LOCK
FITTINGS AND SURROUNDING STRUCTURE, BETWEEN FR 53 AND
FR 55A, EXTERNAL PORTION (6 PLACES)
ACCESS PANELS: 826
534157-01-5
152
AFT CARGO DOOR LOCK FITTING
GENERAL VISUAL INSPECTION OF AFT CARGO DOOR LOCK
FITTINGS AND SURROUNDING STRUCTURE, BETWEEN FR 56 AND
FR 58A, EXTERNAL PORTION (6 PLACES)
ACCESS PANELS: 826
AF
GVI
1
534100-210-038
SOURCE:
ALI 534157-01-4
MRB 534157-01-1
ALI
MRB CPCP
1
534100-210-038
SOURCE:
ALI 534157-01-5
MRB 534157-01-2
Sub 2 - Page 153 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534159-01-1
ZONE
152
154
252
DESCRIPTION
AFT CARGO DOOR CUTOUT UPR/LWR CORNERS
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, UPPER
AND LOWER CORNERS, EXTERNAL SURFACE
ACCESS PANELS: 826
534159-01-3
152
154
252
AFT CARGO DOOR CUTOUT UPR/LWR CORNERS
AF
DET
DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, UPPER
AND LOWER CORNERS, EXTERNAL SURFACE
INTERVALS
SOURCE
T:
13400 FC
OR
26800 FH
I:
13400 FC
OR
26800 FH
T:
12000 FC
I:
12000 FC
ALI
T:
6 YE
I:
6 YE
MRB CPCP
T:
6 YE
I:
6 YE
MRB CPCP
T:
1400 FC
OR
2800 FH
I:
1400 FC
OR
2800 FH
ALI
TPS
REFERENCES
534100-210-031
SOURCE:
ALI 534159-01-1
ALI
534100-210-031
SOURCE:
ALI 534159-01-3
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
0.20
0.20
0.20
1130 1200
1379 1578
1657 1767
2151 2163
1
1
1
0.20
0.20
0.20
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.15
1130 1200
1379 1578
1657 1767
2151 2163
1
0.15
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.50
1130 1200
1379 1578
1657 1767
2151 2163
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS
ACCOMPLISHMENT OF TASK 534159-01-1
534160-01-3
152
ACCESS PANELS: 826
AFT CARGO DOOR CUTOUT LATERAL FRAMES
AF
GVI
GENERAL VISUAL INSPECTION OF AFT CARGO DOOR CUTOUT, VISIBLE PART
OF LATERAL FRAMES.
1
534100-210-803
SOURCE:
MRB 534160-01-1
NOTE: INSPECTION OF FR 52A AND FR 56.
534160-01-4
152
ACCESS PANELS: 826
AFT CARGO DOOR CUTOUT LATERAL FRAMES
AF
GVI
GENERAL VISUAL INSPECTION OF AFT CARGO DOOR CUTOUT, VISIBLE PART
OF LATERAL FRAMES
1
534100-210-803
SOURCE:
MRB 534160-01-2
NOTE: INSPECTION OF FR 55A AND FR 59.
534160-02-1
152
ACCESS PANELS: 826
AFT CARGO DOOR CUTOUT LATERAL FRAMES
DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, VISIBLE PART OF
LATERAL FRAMES
NOTE: INSPECTION OF FR 52A AND FR 56.
ACCESS PANELS: 826
AF
DET
534100-220-803
SOURCE:
ALI 534160-02-1
Sub 2 - Page 154 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534160-02-2
ZONE
152
DESCRIPTION
AFT CARGO DOOR CUTOUT LATERAL FRAMES
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, VISIBLE PART OF
LATERAL FRAMES
NOTE: INSPECTION OF FR 55A AND FR 59.
534163-01-1
152
ACCESS PANELS: 826
AFT CARGO DOOR ACTUATOR ATTACH BRACKET
AF
GVI
GENERAL VISUAL INSPECTION OF AFT CARGO DOOR ACTUATOR
ATTACH BRACKET
INTERVALS
SOURCE
T:
1000 FC
OR
2100 FH
I:
1000 FC
OR
2100 FH
T:
16700 FC
I:
16700 FC
ALI
T:
16700 FC
I:
16700 FC
MRB
T:
12 YE
I:
6 YE
MRB CPCP
TPS
REFERENCES
534100-220-803
MEN
TASKM. APPLICABI
H.
LITY
1
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.10
1130 1200
1379 1578
1657 1767
2151 2163
1
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.50
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
ALI 534160-02-2
MRB
534100-210-819
SOURCE:
MRB 534163-01-1
NOTE: INSPECTION BETWEEN FLOOR BEAMS AT FR 53, FR 54 AND FR 55.
PREPARATION: ACT;
534163-01-2
152
ACCESS PANELS: 151CC
AFT CARGO DOOR ACTUATOR ATTACH BRACKET
AF
GVI
GENERAL VISUAL INSPECTION OF AFT CARGO DOOR ACTUATOR ATTACH
BRACKET
534100-210-819
SOURCE:
MRB 534163-01-2
NOTE: INSPECTION BETWEEN FLOOR BEAMS AT FR 56, FR 57 AND FR 58.
PREPARATION: ACT;
534164-01-1
162
ACCESS PANELS: 151GC
BULK CARGO DOOR CUTOUT
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
AROUND BULK CARGO DOOR CUTOUT, FROM FR 59 TO FR 63
AND BETWEEN STRINGER 23 AND STRINGER 38
AF
DET
1
534100-210-028
SOURCE:
MRB 534164-01-1
PREPARATION: INSULATION REMOVED;
ACCESS PANELS: 162BW, 162EW
Sub 2 - Page 155 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534167-02-1
ZONE
162
DESCRIPTION
BULK CARGO DOOR STOP FITTING
SKILL TASK
CODE CODE
AF
GVI
GENERAL VISUAL INSPECTION OF BULK CARGO DOOR STOP
FITTINGS INCLUDING VISIBLE PART OF LATERAL FR 60 AND
FR 62.
NOTE: TPS APPLICATION IS LIMITED TO THE VISIBLE PART
OF THE LATERAL BULK CARGO DOOR FRAMES.
INTERVALS
SOURCE
T:
6 YE
I:
6 YE
MRB CPCP
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
T:
21000 FC
OR
42100 FH
I:
21000 FC
OR
42100 FH
MRB CPCP
T:
15300 FC
OR
30600 FH
OR
6 YE
I:
15300 FC
OR
30600 FH
OR
6 YE
ALI
MRB CPCP
TPS
REFERENCES
1+2 534100-210-805
MEN
TASKM. APPLICABI
H.
LITY
1
0.10
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.10
0.10
1130 1200
1379 1578
1657 1767
2151 2163
1
0.20
1130 1200
1379 1578
1657 1767
2151 2163
1
0.10
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
MRB 534167-02-1
PREPARATION: INSULATION REMOVED;
534169-01-1
162
164
ACCESS PANELS: 827
FUSELAGE SKIN UNDER SCUFF PLATE
AF
DET
DETAILED INSPECTION OF FUSELAGE SKIN UNDERNEATH BULK
CARGO DOOR SCUFF PLATE
PREPARATION: SCUFF PLATES REMOVED;
534171-01-2
162
ACCESS PANELS: 827
BULK CARGO DOOR CUTOUT UPR CORNERS
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE SKIN OF BULK CARGO
DOOR CUTOUT AT UPPER CORNERS
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
534171-01-3.
534172-01-2
162
ACCESS PANELS: 827
BULK CARGO DOOR CUTOUT SEALING PROFILE
GENERAL VISUAL INSPECTION OF SEALING PROFILE OF BULK CARGO DOOR
CUTOUT AT UPPER CORNERS
NOTE: TPS TO BE APPLIED AT THRESHOLD/INTERVAL NOT EXCEEDING 6 YE.
ACCESS PANELS: 827
AF
GVI
NO
534100-210-007
SOURCE:
MRB 534169-01-1
ALI
534100-210-008
NTM 53-41-71
SOURCE:
ALI 534171-01-2
1
534100-210-804
SOURCE:
ALI 534172-01-2
MRB 534172-01-1
Sub 2 - Page 156 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534195-01-1
ZONE
261
262
DESCRIPTION
CABIN FLOOR STRUCTURE AFT ENTRANCE AREA
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF CABIN FLOOR STRUCTURE AND STRUCTURE
BELOW AFT ENTRANCE AREA; BETWEEN FRAME 66 AND FRAME 68 AND
LATERAL SHEAR PLATES BETWEEN FRAME 68 AND FRAME 70.
INTERVALS
SOURCE
T:
5 YE
I:
5 YE
MRB CPCP
T:
6 YE
I:
6 YE
MRB CPCP
TPS
REFERENCES
1+2 534100-210-835
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.33
0.33
0649 1130
1200 1379
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
1
1
0.33
0.33
2151 2163
SOURCE:
MRB 534195-01-1
NOTE: IN CASE SUFFICIENT ACCESS TO LATERAL SHEAR WEBS IS NOT
POSSIBLE DUE TO GALLEY CONFIGURATION, THE GALLEY MUST BE REMOVED
TO GET ACCESS TO THE INSPECTION AREA.
PREPARATION: CABIN ATTENDANT SEAT REMOVED; FLOOR PANELS FROM FR
66 TO FR 68; LATERAL GALLEY LINING REMOVED; LOWER DOOR FRAME LINING
REMOVED;
534195-01-2
261
262
ACCESS PANELS: 832, 842
CABIN FLOOR STRUCTURE AFT ENTRANCE AREA
AF
DET
DETAILED INSPECTION OF CABIN FLOOR STRUCTURE AND STRUCTURE
BELOW AFT ENTRANCE AREA; BETWEEN FRAME 66 AND FRAME 68 AND
LATERAL SHEAR PLATES BETWEEN FRAME 68 AND FRAME 70.
1+2 534100-210-835
SOURCE:
MRB 534195-01-2
NOTE: IN CASE SUFFICIENT ACCESS TO LATERAL SHEAR WEBS IS NOT
POSSIBLE DUE TO GALLEY CONFIGURATION, THE GALLEY MUST BE REMOVED
TO GET ACCESS TO THE INSPECTION AREA.
PREPARATION: CABIN ATTENDANT SEAT REMOVED;
FLOOR PANELS FROM FR 66 TO FR 68;
LATERAL GALLEY
LINING REMOVED;
LOWER DOOR FRAME
LINING REMOVED;
534199-01-1-SDM
253
254
ACCESS PANELS: 832, 842
LIVETV RADOME INSTL AREA-FRAME C52 TO C56 & STR 5L TO 5R
AF
DET
T:
24000 FC
I:
15000 FC
S-ICA
STC ST00788SE
ICA BERG-151-701
1
1
TBD
TBD
1488 1560
1743 1761
1851 1863
1876 1890
AF
DET
T:
24000 FC
I:
11000 FC
S-ICA
STC ST00788SE
ICA BERG-151-701
1
1
TBD
TBD
1488 1560
1743 1761
1851 1863
1876 1890
INTERNAL DETAILED VISUAL INSPECTION OF THE SKIN AT THE WIRING
PENETRATION
534199-02-1-SDM
253
254
PREPARATION: LINING AND INSULATION REMOVED;
OVERHEAD STOWAGE COMPARTMENTS REMOVED;
LIVETV RADOME INST AREA-FRAME C52 TO C56 & STR 5L TO 5R
INTERNAL DETAILED VISUAL INSPECTION OF THE SKIN AROUND ANTENNA
ATTACHEMENT FITTINGS F1 TO F6.
PREPARATION: LINING AND INSULATION REMOVED;
OVERHEAD STOWAGE COMPARTMENTS REMOVED;
Sub 2 - Page 157 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
534199-03-1-SDM
ZONE
253
254
DESCRIPTION
LIVETV RADOME INST AREA-FRAME C52 TO C56 & STR 5L TO 5R
SKILL TASK
CODE CODE
253
254
253
254
253
254
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
T:
24000 FC
I:
15000 FC
S-ICA
STC ST00788SE
ICA BERG-151-701
1
1
TBD
TBD
1488 1560
1743 1761
1851 1863
1876 1890
AF
DET
T:
24000 FC
I:
7000 FC
S-ICA
STC ST00788SE
ICA BERG-151-701
1
1
TBD
TBD
1488 1560
1743 1761
1851 1863
1876 1890
AF
DET
T:
24000 FC
I:
15000 FC
S-ICA
STC ST00788SE
ICA BERG-151-701
1
1
TBD
TBD
1488 1560
1743 1761
1851 1863
1876 1890
AF
DET
T:
24000 FC
I:
7000 FC
S-ICA
STC ST00788SE
ICA BERG-151-701
1
1
TBD
TBD
1488 1560
1743 1761
1851 1863
1876 1890
AF
DET
T:
24000 FC
I:
24000 FC
NOTE
S-ICA
STC ST00788SE
ICA BERG-151-701
1
1
TBD
TBD
1488 1560
1743 1761
1851 1863
1876 1890
LIVETV LNA INSTALLATION - STRINGERS P4 AND P5 BETWEEN FRAME C59 AND AF
C60
DET
T:
24000 FC
I:
24000 FC
NOTE
S-ICA
STC ST00788SE
ICA BERG-151-701
1
1
TBD
TBD
1488 1560
1743 1761
1851 1863
1876 1890
PREPARATION: LINING AND INSULATION REMOVED;
OVERHEAD STOWAGE COMPARTMENTS REMOVED;
LIVETV RADOME INSTL AREA-FRAME C52 TO C56 & STR 5L TO 5R
PREPARATION: COVER OF ANTENNA AND ANTENNA REMOVED;
BLANKING PLATE REMOVED;
LIVETV RADOME INST AREA-FRAME C52 TO C56 & STR 5L TO 5R
DETAILED VISUAL INSPECTION OF INTERNAL SUPPORT STRUCTURE FOR
LIVETV INSTALLATION.
534199-06-1-SDM
TPS
DET
EXTERNAL DETAILED VISUAL INSPECTION OF SKIN COVERED BY RADOME.
534199-05-1-SDM
SOURCE
AF
INTERNAL DETAILED VISUAL INSPECTION OF THE SKIN AT THE CENTER POINT
DOUBLER.
534199-04-1-SDM
INTERVALS
PREPARATION: LINING AND INSULATION REMOVED;
OVERHEAD STOWAGE COMPARTMENTS REMOVED;
LIVETV RADOME INST AREA-FRAME C52 TO C56 & STR 5L TO 5R
EXTERNAL DETAILED VISUAL INSPECTION OF RADOME ATTACHMENT SITES:
RADOME, BASEPLATE, RADOME TO BASEPLATE FITTINGS, BASEPLATE TO
SKIN BODY FITTINGS, AND OTHER CONNECTING ELEMENTS.
PREPARATION: COVER OF ANTENNA AND ANTENNA REMOVED;
BLANKING PLATE REMOVED;
534199-08-1-SDM
253
254
LIVETV WADL ANTENNA INSTL - FRAME C60 TO C61 & STR P´1L TO P1
INTERNAL SURFACE EDDY CURRENT INSPECTION OF AIRCRAFT SKIN AROUND
FIRST FASTENER RIVET ROW WITH A DETECTABLE CRACK LENGTH OF 0.10
INCHES
NOTE: INTERVAL : 24000 FC (BASED ON AVERAGE FLIGHT LENGTH OF 1 HOUR)
534199-09-1-SDM
253
254
INTERNAL DETAILED VISUAL INSPECTION (DET) OF THE STRINGER SECTION
FOR FAILED EDGE LIGAMENT
NOTE: INTERVAL : 24000 FC (BASED ON AVERAGE FLIGHT LENGTH OF 1 HOUR)
Sub 2 - Page 158 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
535101-01-1
ZONE
311
312
DESCRIPTION
REAR PRESSURE BULKHEAD AFT FACE
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF REAR PRESSURE BULKHEAD
COMPLETE AFT FACE, AND FUSELAGE INTERNAL STRUCTURE,
BETWEEN FR 70 AND FR 71, FROM STRINGER 26, LH/RH TO
BOTTOM CENTER LINE
NOTE: TPS MAY BE LIMITED TO FUSELAGE INTERNAL
STRUCTURE FROM FR 70 TO FR 71, AND AFT FACE OF
PRESSURE BULKHEAD, FROM STRINGER 26, LH/RH TO BOTTOM
CENTERLINE
INTERVALS
SOURCE
T:
6 YE
I:
6 YE
MRB CPCP
T:
17500 FC
OR
35000 FH
I:
17500 FC
OR
35000 FH
ST:
48000 FC
SI:
15700 FC
ALI
ST:
48000 FC
OR
60000 FH
SI:
8700 FC
OR
26100 FH
MRB
T:
12 YE
I:
12 YE
MRB CPCP
TPS
REFERENCES
1+2 535100-210-001
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.60
0.60
ALL
1
0.15
ALL
1
1
0.30
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.75
0.75
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.20
0.20
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
MRB 535101-01-1
PREPARATION: PROTECTIVE SHIELD;
535103-01-2
300
ACCESS PANELS: 312AR
FUSELAGE SKIN AROUND CUTOUT FOR TAIL
COMPARTMENT ACCESS DOOR
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AROUND
CUTOUT FOR TAIL COMPARTMENT ACCESS DOOR, BETWEEN FR
70 AND FR 73 AND BETWEEN STRINGER 25 RH AND BOTTOM
CENTER LINE, EXTERNAL SURFACE
535105-01-4
311
312
REAR PRESSURE BULKHEAD SPLICE
AF
DET
DETAILED INSPECTION OF REAR PRESSURE BULKHEAD AFT
FACE, REINFORCEMENT SPLICE AT FORWARD FIN ATTACHMENT
AREA
535107-01-1
311
312
ACCESS PANELS: 312AR
CIRCUMFERENTIAL JOINT AT FR70
AF
DET
DETAILED INSPECTION OF RING FRAME AT CIRCUMFERENTIAL
JOINT OF REAR PRESSURE BULKHEAD SKIN AT FR 70, AFT
FACE
ACCESS PANELS: 312AR
535113-01-1
311
312
FUSELAGE SKIN AT THS CUTOUT
DETAILED INSPECTION OF FUSELAGE SKIN AT HORIZONTAL
STABILIZER CUTOUT AT FORWARD, UPPER AND LOWER
CORNERS, LH/RH
AF
DET
535100-210-019
SOURCE:
ALI 535103-01-2
MRB
535100-210-014
SOURCE:
MRB 535105-01-4
535100-210-003
SOURCE:
MRB 535107-01-1
1
535100-210-004
SOURCE:
MRB 535113-01-1
ACCESS PANELS: 333AB, 333AT, 343AB, 343AT
Sub 2 - Page 159 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
535113-01-5
ZONE
311
312
DESCRIPTION
FUSELAGE SKIN AT THS CUTOUT
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF FUSELAGE SKIN AT HORIZONTAL STABILIZER
CUTOUT AT FORWARD, UPPER AND LOWER CORNERS, LH/RH
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
535113-01-1.
535115-01-1
311
312
ACCESS PANELS: 333AB, 333AT, 343AB, 343AT
FRAME 74 SPLICES
AF
DET
DETAILED INSPECTION OF FR 74, SPLICES AT STRINGER 12
AND STRINGER 19, LH/RH, INTERNAL STRUCTURE
535117-01-1
311
312
ACCESS PANELS: 312AR
HORIZONTAL STABILIZER ATTACHMENT
AF
DET
DETAILED INSPECTION OF HORIZONTAL STABILIZER
ATTACHMENT AND BACK UP STRUCTURE AT FR 77, FROM
STRINGER 8 TO STRINGER 21, LH/RH
535117-01-5
311
312
ACCESS PANELS: 312AR, 314AR
HORIZONTAL STABILIZER ATTACHMENT
AF
DET
DETAILED INSPECTION OF HORIZONTAL STABILIZER ATTACHMENT AND BACK
UP STRUCTURE AT FR 77, FROM STRINGER 8 TO STRINGER 21, LH/RH
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
535117-01-1.
INTERVALS
SOURCE
ST:
48000 FC
SI:
17300 FC
T:
12 YE
I:
12 YE
MRB CPCP
T:
12 YE
I:
12 YE
MRB CPCP
T:
12 YE
I:
12 YE
MRB CPCP
ST:
48000 FC
SI:
18000 FC
T:
12 YE
I:
12 YE
MRB CPCP
T:
33100 FC
OR
66200 FH
I:
9500 FC
OR
19100 FH
T:
6 YE
I:
6 YE
ALI WFD
TPS
1
REFERENCES
535100-210-004
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.90
0.90
ALL
1
1
0.90
0.90
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.90
0.90
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.40
0.40
0649 1130
1200 1379
1488 1560
1578
1
1
0.60
0.60
ALL
SOURCE:
MRB 535113-01-5
1
535100-210-005
SOURCE:
MRB 535115-01-1
1
535100-210-007
SOURCE:
MRB 535117-01-1
1
535100-210-007
SOURCE:
MRB 535117-01-5
PREPARATION: 312AR 314AR;
535119-01-1
311
312
SHEAR TIES/FRAME CLIPS AT FR 72 AND 74
AF
DET
DETAILED INSPECTION OF SHEAR TIES AND FRAME CLIPS AT
FR 72 AND FR 74, BETWEEN STRINGER 3 AND STRINGER 9,
LH/RH, INTERNAL STRUCTURE
ACCESS PANELS: 312AR
535121-01-1
171
172
REAR PRESSURE BULKHEAD BLW CABIN FLOOR
DETAILED INSPECTION OF REAR PRESSURE BULKHEAD,
FORWARD FACE, BELOW CABIN FLOOR LEVEL
AF
DET
535100-210-017
SOURCE:
ALI 535119-01-1
MRB CPCP
1
535100-210-002
SOURCE:
MRB 535121-01-1
ACCESS PANELS: 162DW
Sub 2 - Page 160 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
535123-01-1
ZONE
261
262
DESCRIPTION
REAR PRESSURE BULKHEAD ABV CABIN FLOOR
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF REAR PRESSURE BULKHEAD,
FORWARD FACE, ABOVE CABIN FLOOR LEVEL
535126-01-1
323
PREPARATION: GALLEYS; INSULATION REMOVED; TOILET
REMOVAL/INSTALLATION ;
FUSELAGE AND VERT STAB ATTACH FITTINGS
AF
GVI
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE AND VERTICAL STABILIZER ATTACHMENT FITTING,
UNDERNEATH VERTICAL STABILIZER/FUSELAGE FAIRINGS
535151-01-1
311
312
313
314
PREPARATION: FAIRINGS;
TAIL CONE ATTACH FITTINGS
AF
DET
DETAILED INSPECTION OF TAIL CONE ATTACHMENT FITTINGS
AT FR 77 AND FR 78
ACCESS PANELS: 314AR
535162-01-1
323
FIN/FUSELAGE ATTACH FITTINGS OUTSIDE
AF
DET
DETAILED INSPECTION OF FIN TO FUSELAGE, FORWARD, MID
AND AFT ATTACH FITTINGS, OUTSIDE FUSELAGE, LH/RH
ACCESS PANELS: 323AL, 323AR
535162-01-2
323
FIN/FUSELAGE ATTACH FITTINGS OUTSIDE
AF
DET
DETAILED INSPECTION OF FIN TO FUSELAGE, FORWARD, MID AND AFT
ATTACH FITTINGS, OUTSIDE FUSELAGE, LH/RH
535900-01-1
535900-02-1
310
ACCESS PANELS: 323AL, 323AR
FUSELAGE DRAINAGE
827
OPERATIONAL CHECK OF SINGLE DRAIN PIPE AFT OF FR 70
FROM OUTSIDE
FUSELAGE DRAINAGE
OPERATIONAL CHECK OF RUBBER FLAP DRAIN VALVE AT BULK
CARGO COMPARTMENT DOOR FROM OUTSIDE
AF
AF
OPC
OPC
INTERVALS
SOURCE
T:
12 YE
I:
12 YE
MRB CPCP
T:
12 YE
I:
12 YE
MRB CPCP
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
ST:
34300 FC
OR
68600 FH
SI:
31300 FC
OR
62600 FH
MRB CPCP
T:
34100 FC
I:
14400 FC
ALI
I:
8 MO
MRB 9
MRB 9
I:
24 MO
TPS
1
REFERENCES
535100-210-008
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.40
0.40
ALL
1
0.20
ALL
0.30
0.30
0.30
0.30
ALL
SOURCE:
MRB 535151-01-1
1
1
1
1
535100-210-012
1
1.20
1130 1200
1379 1578
1657 1767
2151 2163
1
1.20
0649 1488
1560 1743
1761 1851
1863 1876
1890
535900-210-001
1
0.05
ALL
SOURCE:
MRB 53.19.00/02
535900-210-002
1
0.10
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
MRB 535123-01-1
1
535100-210-018
SOURCE:
MRB 535126-01-1
MRB
535100-210-009
SOURCE:
MRB 535162-01-1
535100-210-012
SOURCE:
ALI 535162-01-2
SOURCE:
MRB 53.19.00/05
Sub 2 - Page 161 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
545000-01-1
ZONE
410
420
DESCRIPTION
PYLONS
SKILL TASK
CODE CODE
AF
GVI
INTERVALS
I:
24 MO
SOURCE
MRB 8
GENERAL VISUAL INSPECTION OF COMPARTMENT A AND F
PYLON DRAIN SYSTEM
TPS
REFERENCES
545000-200-001
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.10
0.10
ALL
2
2
0.10
0.10
ALL
SOURCE:
MRB 54.50.00/01
NOTE: ACCESS 482AR 482BR 486AR OR 471CL 481BR 481CR 485AR OR 425BL
ARE ALTERNATIVE DEPENDING ON CONFIGURATION
545000-02-1
410
420
ACCESS PANELS: 413AL, 415AL, 415BL, 471AL, 471BL, 471CL, 475AL, 423AL,
425BL, 425BR, 425AR, 481CR, 482AR, 482BR, 485AR, 486AR, 481BR
PYLONS
AF
FNC
I:
72 MO
MRB 8
FLOW CHECK OF INDIVIDUAL DRAIN LINES OF PYLON SYSTEM
545000-03-1
410
420
ACCESS PANELS: 413AL, 471AL, 471BL, 423AL, 482AR, 482BR
PYLON DRAINAGE
545000-200-002
SOURCE:
MRB 54.50.00/02
AF
DET
I:
24 MO
SIL
545000-220-001
SIL 54-029
1
1
0.10
0.10
ALL
AF
DET
I:
24 MO
MRB 8
545000-220-002
1
1
0.60
0.60
ALL
1
1
0.75
0.75
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.75
0.75
1130 1200
1379 1578
1657 1767
2151 2163
DETAILED INSPECTION OF THE CAF4 SEALANT IN PYLON
CANTILEVER ZONE "A"
545000-04-1
410
420
ACCESS PANELS: 413AL, 423AL
PYLONS
DETAILED INSPECTION OF PYLON COMPARTMENT C DRAIN
SYSTEM.
545101-01-1
415
425
PREPARATION: LOWER AFT PYLON FAIRING REMOVED;
PYLON FWD MOUNT FITTING
SOURCE:
MRB 54.50.00/03
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTO) OF PYLON FORWARD
MOUNT FITTING AND SPIGOT FITTING
PREPARATION: BOLTS REMOVED;
ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR
545101-01-2
415
425
PYLON FWD MOUNT FITTING
SPECIAL DETAILED INSPECTION (ROTO) OF PYLON FORWARD
MOUNT FITTING AND SPIGOT FITTING
PREPARATION: BOLTS REMOVED;
ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR
NDT
SDI
ST:
30000 FC
OR
60000 FH
SI:
8600 FC
OR
17200 FH
MRB
ST:
30000 FC
OR
60000 FH
SI:
17400 FC
OR
34800 FH
MRB
545100-200-001
NTM 54-51-01
SOURCE:
MRB 545101-01-1
545100-200-001
NTM 54-51-01
SOURCE:
MRB 545101-01-2
Sub 2 - Page 162 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
545102-01-10
ZONE
415
425
DESCRIPTION
PYLON FWD MOUNT FITTING
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF PYLON FORWARD
MOUNT FITTING, END OF LOWER ARMS, AFT OF RIB 1,
FORWARD AND AFT ATTACHMENT, BOLT HOLES
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS
ACCOMPLISHMENT OF TASK 545102-01-6
INTERVALS
SOURCE
T:
24000 FC
OR
42000 FH
I:
13500 FC
OR
27000 FH
ALI
T:
24000 FC
OR
42000 FH
I:
11100 FC
OR
30700 FH
ALI
T:
8300 FC
I:
8300 FC
ALI
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
TPS
REFERENCES
545100-200-002
NTM 54-51-02
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.75
0.75
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.75
0.75
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.20
0.20
ALL
1
1
0.50
0.50
ALL
SOURCE:
ALI 545102-01-10
ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR
545102-01-11
415
425
PYLON FWD MOUNT FITTING
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF PYLON FORWARD
MOUNT FITTING, END OF LOWER ARMS, AFT OF RIB 1,
FORWARD AND AFT ATTACHMENT, BOLT HOLES
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS
ACCOMPLISHMENT OF TASK 545102-01-6
545100-200-002
NTM 54-51-02
SOURCE:
ALI 545102-01-11
ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR
545103-01-2
415
425
PYLON FWD MOUNT FITTING
AF
DET
DETAILED INSPECTION OF PYLON FORWARD MOUNT FITTING,
FORWARD OF RIB 1
545100-200-003
SOURCE:
ALI 545103-01-2
ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR
545104-01-1
415
425
PYLON LOWER SPAR UPPER SURFACE
DETAILED INSPECTION OF PYLON, LOWER SPAR, UPPER
SURFACE, BETWEEN RIB 2 AND RIB 3, AND RIB 4 AND RIB 8
NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS
TASK 545104-02-1
ACCESS PANELS: 415AL, 415AR, 415BL, 415BR, 425AL, 425AR, 425BL, 425BR
AF
DET
NO
545100-200-027
SOURCE:
MRB 545104-01-1
Sub 2 - Page 163 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
545104-02-1
ZONE
415
425
DESCRIPTION
PYLON LOWER SPAR UPPER SURFACE
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF PYLON,
LOWER SPAR, UPPER SURFACE, BETWEEN RIB 1 AND RIB 2,
AND RIB 3 AND RIB 4, AND RIB 8 AND RIB 10.
NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS
TASK 545104-01-1
INTERVALS
SOURCE
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
ST:
12 YE
OR
30000 FC
OR
60000 FH
SI:
12 YE
OR
11600 FC
OR
23200 FH
T:
24 YE
OR
48000 FC
OR
80000 FH
I:
12 YE
OR
11600 FC
OR
23200 FH
MRB CPCP
TPS
NO
REFERENCES
545100-200-028
NTM 54-51-04
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.75
0.75
ALL
1
1
0.50
0.50
ALL
1
1
0.30
0.30
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
MRB 545104-02-1
ACCESS PANELS: 415AL, 415AR, 415BL, 415BR, 425AL, 425AR, 425BL, 425BR
545106-01-1
415
425
PYLON LWR SPAR
AF
DET
DETAILED INSPECTION OF PYLON, LOWER SPAR, BETWEEN RIB
1 AND RIB 10, LOWER SURFACE
ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 473AL, 473AR, 473BL, 473CL,
447AL, 448AR, 461AL, 462AR, 483AL, 483AR, 483BL, 483CL
545107-01-1
415
425
ENGINE AFT ATTACH BEAM
DETAILED INSPECTION OF ENGINE AFT ATTACHMENT BEAM
ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR
AF
DET
NO
545100-200-004
SOURCE:
MRB 545106-01-1
ALI
MRB CPCP
NO
545100-200-005
SOURCE:
ALI 545107-01-1
MRB 545107-01-1
Sub 2 - Page 164 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
545107-01-5
ZONE
415
425
DESCRIPTION
ENGINE AFT ATTACH BEAM
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF ENGINE AFT ATTACHMENT BEAM.
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
545107-01-1.
ACCESS PANELS: 437AL, 438AR, 447AL, 448AR, 451AL, 452AR, 461AL, 462AR
545114-01-1
415
425
PYLON/WING ATTACH FITTINGS LUGS RIB 4
AF
DET
DETAILED INSPECTION OF PYLON TO WING ATTACH FITTING
LUGS AT RIB 4
ACCESS PANELS: 414FR, 471AL, 472AR, 423FL, 481AL, 482AR
545114-01-2
415
425
PYLON/WING ATTACH FITTINGS LUGS RIB 4
DETAILED INSPECTION OF PYLON TO WING ATTACH FITTING LUGS AT RIB 4
ACCESS PANELS: 414FR, 471AL, 472AR, 423FL, 481AL, 482AR
AF
DET
INTERVALS
SOURCE
ST:
12 YE
OR
30000 FC
OR
60000 FH
SI:
12 YE
OR
15100 FC
OR
30200 FH
T:
24 YE
I:
12 YE
ST:
30000 FC
OR
60000 FH
SI:
12000 FC
OR
24000 FH
MRB CPCP
ST:
30000 FC
OR
60000 FH
SI:
13900 FC
OR
27800 FH
T:
48000 FC
OR
80000 FH
I:
13900 FC
OR
27800 FH
ALI
MRB
TPS
REFERENCES
545100-200-005
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.30
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.40
0.40
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.40
0.40
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
MRB 545107-01-5
MRB
545100-200-006
SOURCE:
MRB 545114-01-1
545100-200-006
SOURCE:
ALI 545114-01-2
MRB 545114-01-2
Sub 2 - Page 165 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
545115-01-1
ZONE
415
425
DESCRIPTION
PYLON/WING RIB 4
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF PYLON TO WING FORWARD
ATTACHMENT SHACKLES AT RIB 4
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545115-02-1
ACCESS PANELS: 414FR, 423FL, 471AL, 472AR, 481AL, 482AR, 521BT, 621BT
545115-01-2
415
425
PYLON/WING RIB 4
AF
DET
DETAILED INSPECTION OF PYLON TO WING FORWARD ATTACHMENT
SHACKLES AT RIB 4
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545115-02-2
ACCESS PANELS: 414FR, 423FL, 471AL, 472AR, 481AL, 482AR, 521BT, 621BT
545115-02-1
415
425
PYLON/WING RIB 4
SPECIAL DETAILED INSPECTION (US) OF PYLON TO WING
FORWARD ATTACHMENT SHACKLES AT RIB 4.
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK
545115-01-1.
ACCESS PANELS: 414FR, 423FL, 471AL, 472AR, 481AL, 482AR, 521BT, 621BT
NDT
SDI
INTERVALS
SOURCE
ST:
30000 FC
OR
60000 FH
SI:
5100 FC
OR
10200 FH
MRB
ST:
30000 FC
OR
60000 FH
SI:
5700 FC
OR
11400 FH
T:
48000 FC
OR
80000 FH
I:
5700 FC
OR
11400 FH
ST:
30000 FC
OR
60000 FH
SI:
7900 FC
OR
15800 FH
ALI
MRB
TPS
REFERENCES
545100-200-008
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.40
0.40
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.40
0.40
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.60
0.60
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
MRB 545115-01-1
545100-200-008
SOURCE:
ALI 545115-01-2
MRB 545115-01-2
MRB
545100-200-007
NTM 54-51-15
SOURCE:
MRB 545115-02-1
Sub 2 - Page 166 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
545115-02-2
ZONE
415
425
DESCRIPTION
PYLON/WING RIB 4
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF PYLON TO WING FORWARD
ATTACHMENT SHACKLES AT RIB 4.
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545115-01-2.
ACCESS PANELS: 414FR, 423FL, 471AL, 472AR, 481AL, 482AR, 521BT, 621BT
545116-01-1
415
425
PYLON/WING ATTACH FITTING RIB4
AF
DET
DETAILED INSPECTION OF SHACKLES, SLEEVES AND BOLTS OF
PYLON TO WING ATTACHMENT FITTINGS AT RIB 4
PREPARATION: BOLTS REMOVED; SHACKLES; SLEEVES; ENGINE REMOVED;
545117-01-1
415
425
PYLON SPIGOT
AF
DET
DETAILED INSPECTION OF PYLON SPIGOT RECEPTACLE UPPER
SURFACE, INCLUDING FITTING BORE, AND UPPER SPAR
SURROUNDING SURFACE
INTERVALS
SOURCE
ST:
30000 FC
OR
60000 FH
SI:
10800 FC
OR
21600 FH
T:
48000 FC
OR
80000 FH
I:
10800 FC
OR
21600 FH
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
T:
12 YE
I:
12 YE
ALI
MRB
ST:
30000 FC
OR
60000 FH
SI:
11000 FC
OR
22000 FH
MRB
TPS
REFERENCES
545100-200-007
NTM 54-51-15
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.60
0.60
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.30
0.30
ALL
1
1
0.70
0.70
ALL
1
1
0.20
0.20
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
ALI 545115-02-2
MRB 545115-02-2
MRB CPCP
NO
545100-200-009
SOURCE:
MRB 545116-01-1
MRB CPCP
NO
545100-200-010
SOURCE:
MRB 545117-01-1
PREPARATION: BALL JOINT;
545120-01-1
415
425
ACCESS PANELS: 415BL, 415BR, 471AL, 471BL, 472AR, 472BR, 425BL, 425BR,
481AL, 481BL, 482AR, 482BR
PYLON/WING ATTACH FITTINGS LUGS RIB 10
DETAILED INSPECTION OF PYLON TO WING ATTACH FITTING
LUGS AT RIB 10
ACCESS PANELS: 471CL, 472BR, 475BL, 476BR, 481BL, 482CR, 485BL, 486BR
AF
DET
545100-200-011
SOURCE:
MRB 545120-01-1
Sub 2 - Page 167 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
545120-01-2
ZONE
415
425
DESCRIPTION
PYLON/WING ATTACH FITTINGS LUGS RIB 10
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF PYLON TO WING ATTACH FITTING LUGS AT RIB 10
ACCESS PANELS: 471CL, 472BR, 475BL, 476BR, 481BL, 482CR, 485BL, 486BR
545123-01-1
415
425
PYLON/WING AFT ATTACHMENT SHACKLES AT
RIB 10
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF PYLON TO WING AFT
ATTACHMENT SHACKLES AT RIB 10.
ACCESS PANELS: 471CL, 472BR, 475AL, 475BL, 476AR, 476BR, 481BL, 482CR,
485AL, 485BL, 486AR, 486BR
545123-01-2
415
425
PYLON/WING AFT ATTACHMENT SHACKLES AT RIB 10
SPECIAL DETAILED INSPECTION (US) OF PYLON TO WING AFT ATTACHMENT
SHACKLES AT RIB 10.
ACCESS PANELS: 471CL, 472BR, 475AL, 475BL, 476AR, 476BR, 481BL, 482CR,
485AL, 485BL, 486AR, 486BR
NDT
SDI
INTERVALS
SOURCE
ST:
30000 FC
OR
60000 FH
SI:
13600 FC
OR
27200 FH
T:
48000 FC
OR
80000 FH
I:
13600 FC
OR
27200 FH
ST:
30000 FC
OR
60000 FH
SI:
9800 FC
OR
19600 FH
ALI
MRB
ST:
30000 FC
OR
60000 FH
SI:
13200 FC
OR
26400 FH
T:
48000 FC
OR
80000 FH
I:
13200 FC
OR
26400 FH
ALI
MRB
TPS
REFERENCES
545100-200-011
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.60
0.60
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.60
0.60
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
ALI 545120-01-2
MRB 545120-01-2
MRB
545100-220-001
NTM 54-51-23
SOURCE:
MRB 545123-01-1
545100-220-001
NTM 54-51-23
SOURCE:
ALI 545123-01-2
MRB 545123-01-2
Sub 2 - Page 168 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
545124-01-1
ZONE
415
425
DESCRIPTION
PYLON/WING AFT ATTACH FITTING SLEEVES
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF PYLON TO WING AFT ATTACHMENT
FITTING, SLEEVES AND BOLTS
PREPARATION: BOLTS REMOVED; SHACKLES; SLEEVES; ENGINE REMOVED;
545126-01-1
410
420
PYLON LATERAL PANELS FASTENERS AREAS
AF
DET
DETAILED INSPECTION OF PYLON, LATERAL PANELS, IN THE
AREAS OF FASTENERS SECURING THE SUPPORTS OF ACCESS
DOORS, BETWEEN RIB 5 AND RIB 6, LH/RH
545126-01-2
410
420
PYLON LATERAL PANELS FASTENERS AREAS
AF
DET
DETAILED INSPECTION OF PYLON, LATERAL PANELS, IN THE
AREAS OF FASTENERS SECURING THE SUPPORTS OF ACCESS
DOORS, BETWEEN RIB 5 AND RIB 6, LH/RH
545130-01-1
415
425
PYLON LATERAL PANELS EDGE OF CUTOUTS
AF
DET
DETAILED INSPECTION OF PYLON, LATERAL PANELS, AT THE
EDGE OF ACCESS DOOR CUTOUTS, BETWEEN RIB 5 AND RIB 6,
LH/RH
545131-01-1
410
420
ACCESS PANELS: 415BL, 415BR, 425BL, 425BR
PYLON LATERAL PANELS CUTOUT CORNERS
DETAILED INSPECTION OF PYLON, LATERAL PANEL, IN AREAS
OF FASTENERS AT DOOR CUTOUT CORNERS, BETWEEN RIB 2
AND RIB 3, EXTERNAL SURFACE, LH/RH
AF
DET
INTERVALS
SOURCE
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
ST:
30000 FC
OR
60000 FH
SI:
6000 FC
OR
12000 FH
MRB CPCP
ST:
30000 FC
OR
60000 FH
SI:
9500 FC
OR
19000 FH
MRB
T:
20000 FC
I:
20000 FC
ALI
ST:
30000 FC
OR
60000 FH
SI:
5000 FC
OR
10000 FH
MRB
TPS
NO
REFERENCES
545100-200-014
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
ALL
1
1
0.20
0.20
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.20
0.20
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.20
0.20
ALL
1
1
0.20
0.20
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
MRB 545124-01-1
MRB
545100-200-015
SOURCE:
MRB 545126-01-1
545100-200-015
SOURCE:
MRB 545126-01-2
545100-200-016
SOURCE:
ALI 545130-01-1
545100-200-017
SOURCE:
MRB 545131-01-1
Sub 2 - Page 169 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
545131-01-2
ZONE
410
420
DESCRIPTION
PYLON LATERAL PANELS CUTOUT CORNERS
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF PYLON, LATERAL PANEL, IN AREAS
OF FASTENERS AT DOOR CUTOUT CORNERS, BETWEEN RIB 2
AND RIB 3, EXTERNAL SURFACE, LH/RH
545133-01-1
415
425
PYLON LWR SPAR RIB 1 AND 4
AF
DET
DETAILED INSPECTION OF PYLON, LOWER SPAR, IN AREAS OF
FASTENERS AT JUNCTION WITH LATERAL PANEL, BETWEEN RIB
1 AND RIB 4, LH/RH
ACCESS PANELS: 415AL, 415AR, 425AL, 425AR
545134-01-1
415
425
PYLON UPR SPAR RIB 4 AND 10
AF
DET
DETAILED INSPECTION OF PYLON, UPPER SPAR, IN AREAS OF
FASTENERS AT JUNCTION WITH LATERAL PANEL, BETWEEN RIB
4 AND RIB 10, LH/RH
ACCESS PANELS: 471AL, 471BL, 471CL, 472AR, 472BR, 481AL, 481BL, 482AR,
482BR, 482CR
545134-01-2
415
425
PYLON UPR SPAR RIB 4 AND 10
AF
DET
DETAILED INSPECTION OF PYLON, UPPER SPAR, IN AREAS OF
FASTENERS AT JUNCTION WITH LATERAL PANEL, BETWEEN RIB
4 AND RIB 10, LH/RH
ACCESS PANELS: 471AL, 471BL, 471CL, 472AR, 472BR, 481AL, 481BL, 482AR,
482BR, 482CR
545156-01-1
415
425
PYLON UPPER SPARS UPPER SURFACE
DETAILED INSPECTION OF PYLON, UPPER SPARS, UPPER
SURFACE, FROM FORWARD OF RIB 1 TO RIB 10
AF
DET
INTERVALS
SOURCE
ST:
30000 FC
OR
60000 FH
SI:
9700 FC
OR
19400 FH
MRB
ST:
30000 FC
OR
60000 FH
SI:
13100 FC
OR
26200 FH
MRB
ST:
30000 FC
OR
60000 FH
SI:
6800 FC
OR
13600 FH
MRB
ST:
30000 FC
OR
60000 FH
SI:
9900 FC
OR
19800 FH
MRB
T:
10 YE
I:
10 YE
MRB CPCP
TPS
REFERENCES
545100-200-017
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.50
0.50
ALL
1
1
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.50
0.50
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.35
0.35
ALL
SOURCE:
MRB 545131-01-2
545100-200-018
SOURCE:
MRB 545133-01-1
545100-200-019
SOURCE:
MRB 545134-01-1
545100-200-019
SOURCE:
MRB 545134-01-2
NO
545100-200-021
SOURCE:
MRB 545156-01-1
PREPARATION: PRE-COOLER;
ACCESS PANELS: 413CL, 413DL, 413EL, 414CR, 414FR, 471AL, 471BL, 471CL,
472AR, 472BR, 423CL, 423DL, 423FL, 424CR, 424ER, 481AL, 481BL, 482AR, 482BR,
482CR
Sub 2 - Page 170 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
545161-01-1
ZONE
415
425
DESCRIPTION
PYLON UPPER SPAR LOWER SURFACE
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF PYLON, UPPER SPAR, LOWER
SURFACE, FORWARD OF RIB 1
INTERVALS
SOURCE
T:
10 YE
I:
10 YE
MRB CPCP
ST:
10 YE
SI:
10 YE
T:
24 YE
I:
10 YE
MRB CPCP
ST:
10 YE
SI:
10 YE
T:
24 YE
I:
10 YE
MRB CPCP
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
TPS
NO
REFERENCES
545100-200-022
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.50
0.50
ALL
1
1
0.60
0.60
ALL
1
1
0.75
0.75
ALL
1
1
0.10
0.10
ALL
1
1
0.15
0.15
ALL
SOURCE:
MRB 545161-01-1
ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR
545162-01-1
415
425
PYLON UPPER SPAR LOWER SURFACE
AF
DET
DETAILED INSPECTION OF PYLON, UPPER SPAR, LOWER
SURFACE, BETWEEN RIB 2 AND RIB 3, AND RIB 4 AND RIB 8
NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS
TASK 545162-02-1
ACCESS PANELS: 415AL, 415AR, 415BL, 415BR, 425AL, 425AR, 425BL, 425BR
545162-02-1
415
425
PYLON UPPER SPAR LOWER SURFACE
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF PYLON,
UPPER SPAR, LOWER SURFACE, BETWEEN RIB 1 AND RIB 2,
RIB 3 AND RIB 4, AND RIB 8 AND RIB 10.
NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS
TASK 545162-01-1.
NO
545100-200-023
SOURCE:
MRB 545162-01-1
NO
545100-200-024
NTM 54-51-62
SOURCE:
MRB 545162-02-1
ACCESS PANELS: 415AL, 415AR, 415BL, 415BR, 425AL, 425AR, 425BL, 425BR
545170-01-1
415
425
PYLON PYRAMID MATING FACE
AF
DET
DETAILED INSPECTION OF PYLON, PYRAMID MATING FACE
WITH THE ENGINE FORWARD MOUNT FITTING
PREPARATION: ENGINE REMOVED;
545171-01-1
415
425
PYLON ENGINE AFT ATTACHMENT BEAM
DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENT
BEAM MATING FACE WITH THE ENGINE AFT MOUNT FITTING
PREPARATION: ENGINE REMOVED;
AF
DET
NO
545100-200-025
SOURCE:
MRB 545170-01-1
MRB CPCP
NO
545100-200-026
SOURCE:
MRB 545171-01-1
Sub 2 - Page 171 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
545172-01-1
ZONE
475
476
485
486
DESCRIPTION
PYLON FWD CORNER FITTINGS
SKILL TASK
CODE CODE
INTERVALS
SOURCE
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
AF
DET
T:
6 YE
I:
6 YE
ISB
OIT
545400-220-002
ISB 54-1022
OIT 999.0037/11
1
1
1
1
1.00
1.00
1.00
1.00
AF
DET
T:
6 YE
I:
6 YE
MRB
551634-200-001
1
1
0.20
0.20
ST:
32000 FC
SI:
24000 FC
MRB
1
1
0.30
0.30
ALL
T:
6 YE
I:
6 YE
MRB
1
1
0.25
0.25
ALL
T:
12 YE
I:
12 YE
MRB
1
1
0.15
0.15
ALL
DETAILED INSPECTION OF AFT PYLON SECONDARY
STRUCTURE, FORWARD CORNER FITTINGS
ACCESS PANELS: 475AL, 476AR, 485AL, 486AR
551001-01-1
333
343
THS JACK FITTING
DETAILED INSPECTION OF HORIZONTAL STABILIZER, JACK
FITTING AND SURROUNDING EXTERNAL STRUCTURE
551002-01-1
333
343
ACCESS PANELS: 312AR
THS UPR JOINT FITTING REAR AREA
AF
DET
DETAILED INSPECTION OF HORIZONTAL STABILIZER, UPPER
AND LOWER JOINT FITTINGS, EXTERNAL SURFACES, 5
REARMOST ROWS OF FASTENERS
551010-01-1
333
343
ACCESS PANELS: 314AR
THS SUPPORT AND ATTACH FITTINGS
AF
DET
DETAILED INSPECTION OF HORIZONTAL STABILIZER, REAR
SUPPORT FITTINGS, UPPER AND LOWER ATTACH FITTINGS AND
SURROUNDING EXTERNAL STRUCTURE, LH/RH
551012-01-1
333
343
ACCESS PANELS: 314AR
THS SPARBOX INTERNAL STRUCTURE
DETAILED INSPECTION OF HORIZONTAL STABILIZER,
INTERNAL STRUCTURE OF TORQUE BOX, INBOARD OF
FUSELAGE FAIRINGS
AF
DET
0649 1130
1200 1379
1488 1560
1657 1743
1761 1767
1851 1863
1876 1890
ALL
SOURCE:
MRB 551001-01-1
551600-200-002
SOURCE:
MRB 551002-01-1
551600-200-001
SOURCE:
MRB 551010-01-1
551000-210-001
SOURCE:
MRB 551012-01-1
PREPARATION: PEELABLE HOLE COVERS REMOVED;
ACCESS PANELS: 312AR, 314AR
Sub 2 - Page 172 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
551019-01-1
ZONE
333
343
DESCRIPTION
THS TORQUE BOX INTERNAL STRUCTURE
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF HORIZONTAL STABILIZER,
INTERNAL STRUCTURE OF TORQUE BOX, OUTBOARD OF
FUSELAGE FAIRINGS, LH/RH
INTERVALS
SOURCE
T:
12 YE
I:
12 YE
MRB
T:
6 YE
I:
6 YE
MRB CPCP
T:
6 YE
I:
6 YE
MRB CPCP
T:
6 YE
I:
6 YE
MRB
TPS
REFERENCES
551000-210-002
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.30
0.30
ALL
1
1
0.75
0.75
ALL
1
1
0.75
0.75
ALL
1
1.00
ALL
1
1
0.75
0.75
ALL
SOURCE:
MRB 551019-01-1
PREPARATION: PEELABLE HOLE COVERS REMOVED;
551020-01-1
334
344
ACCESS PANELS: 331AB, 331BB, 331CB, 332AB, 334AB, 334AT, 334BB, 334BT,
334CB, 334CT, 334DB, 334DT, 334EB, 334FB, 334GB, 334HB, 341AB, 341BB,
341CB, 342AB, 344AB, 344AT, 344BB, 344BT, 344CB, 344CT, 344DB, 344DT, 344EB,
344FB, 344GB, 344HB
ELEVATOR HINGE SUPPORTS AND FITTINGS
AF
DET
DETAILED INSPECTION OF HORIZONTAL STABILIZER, HINGE
FITTINGS AND SUPPORT RIBS AND ACTUATOR FITTINGS FOR
THE ELEVATOR, LH/RH
552002-01-1
335
345
ACCESS PANELS: 334AT, 334BB, 334BT, 334CT, 334DB, 334DT, 334FB, 334HB,
344AT, 344BB, 344BT, 344CT, 344DB, 344DT, 344FB, 344HB
ELEVATOR HINGE SUPPORT AND ACT. FTG.
AF
DET
DETAILED INSPECTION OF ELEVATOR, HINGE FITTINGS AND
ACTUATOR FITTINGS, LH/RH
552004-01-1
300
ACCESS PANELS: 334BB, 334DB, 334FB, 334HB, 335AB, 335BB, 335CB, 335DB,
344BB, 344DB, 344FB, 344HB, 345AB, 345BB, 345CB, 345DB
ELEVATOR SKIN PANELS
NDT
SDI
SPECIAL DETAILED (TAP TEST) INSPECTION OF ELEVATOR,
TOP AND BOTTOM SKIN PANELS IN AREA OF HINGE SUPPORTS
2, 3 AND 4 AND ACTUATOR FITTINGS 1 AND 2, LH/RH
552005-01-1
335
345
ELEVATOR PANELS INTERNAL STRUCTURE
DETAILED INSPECTION OF ELEVATOR PANELS, INTERNAL
STRUCTURE AS FAR AS VISIBLE, LH/RH
AF
DET
T:
12 YE
I:
12 YE
1
551600-200-004
SOURCE:
MRB 551020-01-1
1
552000-200-003
SOURCE:
MRB 552002-01-1
MRB
552000-200-001
NTM 51-10-03
NTM 55-20-04
SOURCE:
MRB 552004-01-1
552000-200-002
SOURCE:
MRB 552005-01-1
PREPARATION: PEELABLE HOLE COVERS REMOVED;
ACCESS PANELS: 334AB, 334BB, 334CB, 334DB, 334EB, 334FB, 334GB, 334HB,
335AB, 335BB, 335CB, 335DB, 344AB, 344BB, 344CB, 344DB, 344EB, 344FB,
344GB, 344HB, 345AB, 345BB, 345CB, 345DB
Sub 2 - Page 173 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
552006-01-1
ZONE
335
345
DESCRIPTION
ELEVATOR OUTBOARD RIB
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF ELEVATOR OUTBOARD RIB, EXTERNAL SURFACE,
LH/RH
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
552005-01-1 IN CASE THIS INSPECTION WAS PERFORMED PRIOR JUNE 2004.
INTERVALS
SOURCE
T:
10 YE
I:
10 YE
MRB CPCP
T:
12 YE
I:
12 YE
MRB CPCP
T:
12 YE
NOTE
I:
6 YE
ALI
T:
12 YE
NOTE
I:
6 YE
ALI
TPS
REFERENCES
552000-200-005
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.30
0.30
0649 1130
1200 1379
1488 1560
1578 1657
1743 1761
1767 1863
1
1
0.30
0.30
1851 1876
1890 2151
2163
2
2
3.00
3.00
ALL
2
2
3.00
3.00
ALL
SOURCE:
MRB 552006-01-1
PREPARATION: ELEVATOR TIP;
ACCESS PANELS: 332AB, 342AB
552006-01-2
335
345
ELEVATOR OUTBOARD RIB
AF
DET
DETAILED INSPECTION OF ELEVATOR OUTBOARD RIB, EXTERNAL SURFACE,
LH/RH
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
552005-01-1 IN CASE THIS INSPECTION WAS PERFORMED PRIOR JUNE 2004.
552000-200-005
SOURCE:
MRB 552006-01-2
PREPARATION: ELEVATOR TIP;
ACCESS PANELS: 332AB, 342AB
552007-01-2
335
345
ELEVATOR TOP AND BOTTOM SKIN PANELS
NDT
SDI
SPECIAL DETAILED INSPECTION (THERMOGRAPHIC) OF
ELEVATOR TOP AND BOTTOM SKIN PANELS, LH/RH.
552007-01-4
335
345
NOTE: THRESHOLD IS 12 YEARS SINCE THE DATE OF THE
FIRST FLIGHT.
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK
552007-01-4.
ELEVATOR TOP AND BOTTOM SKIN PANELS
SPECIAL DETAILED INSPECTION (THERMOGRAPHIC) OF
ELEVATOR TOP AND BOTTOM SKIN PANELS, LH/RH.
NOTE: -THRESHOLD IS 12 YEARS SINCE THE DATE OF THE
FIRST FLIGHT.
NDT
SDI
552000-200-006
NTM 55-20-07
SIL 55-037
SOURCE:
ALI 552007-01-2
552000-200-006
NTM 55-20-07
SIL 55-037
SOURCE:
ALI 552007-01-4
-THIS TASK IS AN ALTERNATIVE TO TASK
552007-01-2.
PREPARATION: ELEVATOR REMOVED;
Sub 2 - Page 174 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
552600-01-1
ZONE
335
345
DESCRIPTION
ELEVATOR ATTACH FITTINGS
SKILL TASK
CODE CODE
INTERVALS
SOURCE
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
AF
CHK
I:
12 YE
SIL
552600-200-002
SIL 55-035
1
1
2.50
2.50
ALL
AF
DET
T:
12 YE
I:
12 YE
MRB
553000-200-001
0.75
0.75
0.75
0.75
ALL
SOURCE:
MRB 553003-01-1
1
1
1
1
T:
6 YE
I:
6 YE
MRB
553600-210-001
1
0.30
ALL
T:
6 YE
I:
6 YE
MRB CPCP
1
0.20
ALL
T:
6 YE
I:
6 YE
MRB CPCP
1
0.15
0649 1130
1200 1379
1488 1560
1578 1657
T:
6 YE
I:
6 YE
MRB CPCP
1
0.15
1743 1761
1767 1851
1863 1876
1890 2151
2163
CHECK OF ELEVATOR ATTACHMENT FITTINGS FOR WEAR,
LH/RH
PREPARATION: ELEVATOR REMOVED;
ACCESS PANELS: 334BB, 334DB, 334FB, 334HB, 344BB, 344DB, 344FB, 344HB
553003-01-1
321
322
323
324
VERT STABILIZER CENTER BOX
DETAILED INSPECTION OF VERTICAL STABILIZER, CENTER
BOX, INTERNAL STRUCTURE AS FAR AS VISIBLE, FRONT SPAR
FORWARD FACE AND UPPER CLOSING RIB, UPPER SURFACE
PREPARATION: PEELABLE HOLE COVERS REMOVED;
553004-01-1
323
ACCESS PANELS: 321AL, 322AL, 322BL, 322CL, 323AL, 323AR, 324AT, 325AL,
325AR, 325BL, 325BR, 325CL, 325CR, 325DL, 325DR, 325EL, 325ER
VERT STABILIZER ATTACH FITTINGS
AF
DET
DETAILED INSPECTION OF VERTICAL STABILIZER, ATTACH
FITTINGS, INCLUDING LOAD INTRODUCTION AREA AT SKIN
PANELS
553005-01-1
325
ACCESS PANELS: 323AL, 323AR
RUDDER HINGE ARMS AND ACTUATOR
AF
DET
DETAILED INSPECTION OF RUDDER HINGE ARM 1,2,3,4 AND 5
AND FIN ACTUATOR FITTINGS (ACTUATOR 1, 2 AND 3)
553006-01-1
325
ACCESS PANELS: 325BL, 325CL
RUDDER HINGE ARM 6 AND 7
AF
DET
DETAILED INSPECTION OF RUDDER HINGE ARM 6 AND 7
553006-01-2
325
ACCESS PANELS: 324AT, 325DL, 325EL
RUDDER HINGE ARM 6 AND 7
DETAILED INSPECTION OF RUDDER HINGE ARM 6 AND 7
ACCESS PANELS: 324AT, 325DL, 325EL, 326CT
AF
DET
SOURCE:
MRB 553004-01-1
1
553000-210-001
SOURCE:
MRB 553005-01-1
1
553000-210-002
SOURCE:
MRB 553006-01-1
1
553000-210-002
SOURCE:
MRB 553006-01-2
Sub 2 - Page 175 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
553600-01-1
ZONE
325
DESCRIPTION
RUDDER ATTACH FITTINGS
SKILL TASK
CODE CODE
INTERVALS
SOURCE
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
AF
CHK
T:
6 YE
I:
6 YE
SIL
554600-200-802
SIL 55-038
1
6.42
ALL
NDT
SDI
T:
6 YE
I:
6 YE
MRB
554000-210-001
NTM 55-40-03
1
1.00
ALL
T:
12 YE
I:
12 YE
MRB
1
0.50
ALL
T:
6 YE
I:
6 YE
MRB CPCP
1
0.20
ALL
T:
6 YE
I:
6 YE
MRB CPCP
1
0.15
ALL
CHECK OF RUDDER ATTACHMENT FITTINGS FOR WEAR
ACCESS PANELS: 325BL, 325BR, 325CL, 325CR, 325DL, 325DR, 325EL, 325ER
554003-01-1
554004-01-1
300
RUDDER SIDE PANELS
326
SPECIAL DETAILED INSPECTION (US) OF RUDDER SIDE
PANELS, IN AREA OF RUDDER BEARINGS, IN THE BOOSTER
AREA AND AROUND TRAILING EDGE FASTENERS AND HOISTING
POINTS, LH/RH.
RUDDER SIDE PANELS INTERNAL SURFACES
AF
DET
DETAILED INSPECTION OF RUDDER SIDE PANELS, INTERNAL
SURFACES
NOTE: ALTERNATIVE ACCESS: 325AR 325BR 325CR 325DR
325ER 326AT
SOURCE:
MRB 554003-01-1
554000-210-003
SOURCE:
MRB 554004-01-1
PREPARATION: PEELABLE HOLE COVERS REMOVED;
554005-01-1
326
ACCESS PANELS: 325AL, 325BL, 325CL, 325DL, 325EL, 326AT
RUDDER FITTINGS,ACT. ATTACH FITTINGS
AF
DET
DETAILED INSPECTION OF RUDDER ATTACH FITTING 1,2,3,4
AND 5 AND RUDDER ACTUATOR ATTACH FITTINGS (ACTUATOR
1, 2 AND 3)
1
554000-210-004
SOURCE:
MRB 554005-01-1
NOTE: ON A/C POST SB 55-1030 ONLY RUDDER ACTUATOR
ATTACH FITTINGS (ACTUATOR 1, 2 AND 3) TO BE
INSPECTED.
554006-01-1
326
ACCESS PANELS: 325BL, 325CL
RUDDER ATTACH FITTING 6 AND 7
DETAILED INSPECTION OF RUDDER ATTACH FITTING 6 AND 7
AF
DET
1
554000-210-005
SOURCE:
MRB 554006-01-1
ACCESS PANELS: 324AT, 325DL, 325EL
Sub 2 - Page 176 of 305
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SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
554008-01-1
ZONE
300
DESCRIPTION
RUDDER SIDE PANELS
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (THERMOGRAPHIC) OF THE
HONEYCOMB CORE OF THE RUDDER SIDE PANELS, LH / RH.
554009-01-1
300
NOTE: RUDDER WITH AN AGE OF 12 YE OR HIGHER, AT
APPROVAL DATE OF MRBR REVISION 16 (SEP 2011), SHOULD
TO BE INSPECTED NOT LATER THAN 12 MONTH AFTER
APPROVAL DATE OF MRBR REVISION 16 (SEP 2011).
RUDDER WITH AN AGE LOWER THAN 12 YE, AT APPROVAL DATE
OF MRBR REVISION 16 (SEP 2011), SHOULD PERFORM THE
INSPECTION WITHIN 24 MONTH AFTER APPROVAL DATE OF
MRBR REVISION 16 (SEP 2011), OR AT THE RUDDER
INSPECTION THRESHOLD DATE, WHICHEVER OCCURS THE
LATER.
RUDDER SIDE PANELS
NDT
SDI
SPECIAL DETAILED INSPECTION (ELCH TEST) OF THE
BONDING LAYERS BETWEEN RUDDER SIDE PANEL HONEYCOMB
STRUCTURE AND EXTERNAL SKINS OF THE RUDDER SIDE
PANELS, LH / RH.
561000-01-1
561000-02-1
561200-01-1
INTERVALS
SOURCE
T:
6 YE
I:
6 YE
MRB
T:
6 YE
I:
6 YE
MRB
TPS
REFERENCES
554000-220-001
NTM 55-40-08
MEN
TASKM. APPLICABI
H.
LITY
1
2.50
ALL
1
4.66
ALL
SOURCE:
MRB 554008-01-1
554000-210-006
NTM 55-40-09
SOURCE:
MRB 554009-01-1
210
NOTE: RUDDER WITH AN AGE OF 12 YE OR HIGHER, AT
APPROVAL DATE OF MRBR REVISION 16 (SEP 2011), SHOULD
TO BE INSPECTED NOT LATER THAN 12 MONTH AFTER
APPROVAL DATE OF MRBR REVISION 16 (SEP 2011).
RUDDER WITH AN AGE LOWER THAN 12 YE, AT APPROVAL DATE
OF MRBR REVISION 16 (SEP 2011), SHOULD PERFORM THE
INSPECTION WITHIN 24 MONTH AFTER APPROVAL DATE OF
MRBR REVISION 16 (SEP 2011), OR AT THE RUDDER
INSPECTION THRESHOLD DATE, WHICHEVER OCCURS THE
LATER.
COCKPIT WINDOWS
AF
DET
I:
4 MO
SIL
1
0.30
ALL
210
DETAILED INSPECTION OF ALL COCKPIT WINDOWS FROM
INSIDE.
COCKPIT WINDOWS
561000-200-003
JIC A320-56-10-00
SIL 56-017
AF
DET
I:
20 MO
SIL
561000-200-005
SIL 56-017
1
0.30
ALL
210
DETAILED INSPECTION OF ALL COCKPIT WINDOWS FROM
OUTSIDE
SLIDING WINDOWS
AF
DET
I:
48 MO
MRB 9
SIL
561200-220-001
SIL 56-017
1
0.10
ALL
DETAILED INSPECTION OF WINDOW SEALS
SOURCE:
MRB 56.12.00/02
Sub 2 - Page 177 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
561200-02-1
ZONE
210
DESCRIPTION
SLIDING WINDOWS
SKILL TASK
CODE CODE
AF
LUB
INTERVALS
I:
20 MO
SOURCE
TPS
MRB 6,8
122256-600-001
T:
6 YE
I:
6 YE
MRB
SOURCE:
MRB 56.12.00/01
562113-200-001
ST:
30000 FC
OR
60000 FH
SI:
20300 FC
OR
40600 FH
T:
37200 FC
OR
74400 FH
I:
20300 FC
OR
40600 FH
ST:
30000 FC
OR
60000 FH
SI:
15400 FC
OR
30900 FH
ALI
MRB
LUBRICATION OF COCKPIT SLIDING WINDOW TRACKS
562101-01-1
571101-02-1
221
222
231
232
241
242
251
252
261
262
147
148
WINDOW PANES
AF
DET
DETAILED INSPECTION OF CABIN WINDOW PANES, INCLUDING
WINDOW PANES IN DOORS
MAIN STRUCTURE
NDT
SDI
ACCESS PANELS: 734, 744
141
142
NO
SOURCE:
MRB 562101-01-1
ACCESS PANELS: 831
SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING BOX, REAR SPAR,
SYSTEM HOLES NEAR MAN HOLES
571106-01-2
REFERENCES
CENTER WING BOX LWR SKIN
SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING BOX
AT ENDS OF LOWER SKIN STIFFENERS, 8 TO 15, LH/RH.
PREPARATION: SEALANT REMOVED;
ACCESS PANELS: 147AZ, 734, 148AZ, 744
NDT
SDI
571000-220-802
NTM 57-11-01
MEN
TASKM. APPLICABI
H.
LITY
1
0.20
ALL
2
2
2
2
2
2
2
2
2
2
1
1
0.60
0.60
0.60
0.60
0.60
0.60
0.60
0.60
0.60
0.60
0.27
0.27
ALL
1
1
3.10
3.10
1130 1200
1379 1578
1657 1767
2151 2163
ALL
SOURCE:
ALI 571101-02-1
MRB 571101-02-1
MRB
571000-220-002
NTM 57-11-06
SOURCE:
MRB 571106-01-2
Sub 2 - Page 178 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
571106-01-4
ZONE
141
142
DESCRIPTION
CENTER WING BOX LWR SKIN
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING BOX AT ENDS OF
LOWER SKIN STIFFENERS, 8 TO 15, LH/RH.
PREPARATION: SEALANT REMOVED;
ACCESS PANELS: 147AZ, 734, 148AZ, 744
571106-01-7
141
142
CENTER WING
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING BOX AT ENDS OF
LOWER SKIN STIFFENERS, 8 TO 15, LH/RH.
PREPARATION: SEALANT REMOVED;
ACCESS PANELS: 147AZ, 148AZ, 734, 744
571109-01-1
147
148
CENTER WING BOX REAR SPAR
AF
DET
DETAILED INSPECTION OF CENTER WING BOX, REAR SPAR,
AROUND ACCESS DOOR CUTOUTS
571109-02-1
147
148
ACCESS PANELS: 147AZ, 734, 148AZ, 744
CENTER WING BOX REAR SPAR
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING
BOX, REAR SPAR, AROUND ACCESS DOOR CUTOUTS.
ACCESS PANELS: 147AZ, 734, 148AZ, 744
571109-02-2
147
148
CENTER WING BOX REAR SPAR
SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING
BOX, REAR SPAR, AROUND ACCESS DOOR CUTOUTS.
ACCESS PANELS: 147AZ, 734, 148AZ, 744
NDT
SDI
INTERVALS
SOURCE
ST:
34000 FC
OR
60000 FH
SI:
9900 FC
OR
27300 FH
MRB
ST:
30000 FC
OR
60000 FH
SI:
10600 FC
OR
29100 FH
MRB
T:
12 YE
I:
12 YE
MRB CPCP
ST:
48000 FC
OR
96000 FH
SI:
14500 FC
OR
38500 FH
MRB
ST:
48000 FC
OR
60000 FH
SI:
12700 FC
OR
33700 FH
MRB
TPS
REFERENCES
571000-220-002
NTM 57-11-06
MEN
TASKM. APPLICABI
H.
LITY
1
1
3.10
3.10
1488 1560
1743 1851
1863 1876
1
1
3.10
3.10
0649 1761
1890
1
1
0.19
0.19
ALL
1
1
0.60
0.60
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.60
0.60
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
MRB 571106-01-4
571000-220-002
NTM 57-11-06
SOURCE:
MRB 571106-01-7
NO
571000-200-004
SOURCE:
MRB 571109-01-1
571000-220-001
NTM 57-11-09
SOURCE:
MRB 571109-02-1
571000-220-001
NTM 57-11-09
SOURCE:
MRB 571109-02-2
Sub 2 - Page 179 of 305
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SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
571120-01-1
ZONE
137
138
DESCRIPTION
CENTER WING SPANWISE
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF CENTER WING SPANWISE FORMED
ANGLE, ALONG LOWER EDGE OF FRONT SPAR, FORWARD FACE
PREPARATION: LINING REMOVED; INSULATION REMOVED;
ACCESS PANELS: 825
571120-01-2
137
138
CENTER WING SPANWISE
AF
DET
DETAILED INSPECTION OF CENTER WING SPANWISE FORMED
ANGLE, ALONG LOWER EDGE OF FRONT SPAR, FORWARD FACE.
PREPARATION: LINING REMOVED; WATER TANK REMOVED (IF INSTALLED);
INSULATION REMOVED;
571120-01-4
137
138
ACCESS PANELS: 825
CENTER WING SPANWISE
AF
DET
DETAILED INSPECTION OF CENTER WING SPANWISE FORMED
ANGLE, ALONG LOWER EDGE OF FRONT SPAR, FORWARD FACE
PREPARATION: LINING REMOVED;
INSULATION REMOVED;
571122-01-1
147
148
ACCESS PANELS: 825
CENTER WING BOX REAR SPAR
AF
DET
DETAILED INSPECTION OF CENTER WING BOX, REAR SPAR AFT
FACE
571134-01-1
191
192
195
196
ACCESS PANELS: 734, 744
CENTER WING BOX SKIN STGR 11-15
DETAILED INSPECTION OF CENTER WING BOX, BOTTOM SKIN
LOWER SURFACE, FROM STRINGER 11 TO STRINGER 15,
BETWEEN Y=+/-1292, AS FAR AS VISIBLE
ACCESS PANELS: 191BB, 191CT, 191EB, 191KB, 191LB, 192CT, 192EB, 192FB,
192KB, 192LB, 195AB, 734, 196AB, 744
AF
DET
INTERVALS
SOURCE
ST:
30000 FC
OR
60000 FH
SI:
7500 FC
OR
20700 FH
MRB
ST:
48000 FC
OR
96000 FH
SI:
9600 FC
OR
19300 FH
MRB
ST:
48000 FC
OR
60000 FH
SI:
7000 FC
OR
19400 FH
MRB
T:
6 YE
I:
6 YE
MRB CPCP
T:
32800 FC
OR
65600 FH
I:
7200 FC
OR
14500 FH
ALI
TPS
REFERENCES
571000-200-006
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.13
0.13
0649 1761
1890
1
1
0.13
0.13
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.13
0.13
1488 1560
1743 1851
1863 1876
1
1
0.75
0.75
ALL
1
1
1
1
0.25
0.25
0.25
0.25
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
MRB 571120-01-1
571000-200-006
SOURCE:
MRB 571120-01-2
571000-200-006
SOURCE:
MRB 571120-01-4
1+2 571000-200-012
SOURCE:
MRB 571122-01-1
571000-200-013
SOURCE:
ALI 571134-01-1
Sub 2 - Page 180 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
571134-01-4
ZONE
191
192
195
196
DESCRIPTION
CENTER WING BOX SKIN STGR 11-15
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF CENTER WING BOX, BOTTOM SKIN
LOWER SURFACE, FROM STRINGER 11 TO STRINGER 15,
BETWEEN Y=+/-1292, AS FAR AS VISIBLE
ACCESS PANELS: 191BB, 191CT, 191EB, 191KB, 191LB, 192CT, 192EB, 192FB,
192KB, 192LB, 195AB, 734, 196AB, 744
571134-01-5
191
192
195
196
CENTER WING BOX SKIN STGR 11-15
AF
DET
DETAILED INSPECTION OF CENTER WING BOX, BOTTOM SKIN
LOWER SURFACE, FROM STRINGER 11 TO STRINGER 15,
BETWEEN Y=+/-1292, AS FAR AS VISIBLE
ACCESS PANELS: 191BB, 191CT, 191EB, 191KB 191LB, 192CT, 192EB, 192FB,
192KB, 192LB, 195AB, 734, 196AB, 744
571135-01-1
141
142
CENTER WING BOX SKIN STGR 6-11, 11-15
AF
DET
DETAILED INSPECTION OF CENTER WING BOX, BOTTOM SKIN
UPPER SURFACE, INCLUDING STRINGERS, FROM STRINGER 6
TO STRINGER 11, BETWEEN Y=+/-765 AND FROM STRINGER 11
TO STRINGER 15, BETWEEN Y=+/-1292
571135-01-4
141
142
ACCESS PANELS: 147AZ, 734, 148AZ, 744
CENTER WING BOX SKIN STGR 6-11, 11-15
AF
DET
DETAILED INSPECTION OF CENTER WING BOX, BOTTOM SKIN
UPPER SURFACE, INCLUDING STRINGERS, FROM STRINGER 6
TO STRINGER 11, BETWEEN Y=+/-765 AND FROM STRINGER 11
TO STRINGER 15, BETWEEN Y=+/-1292
ACCESS PANELS: 147AZ, 734, 148AZ, 744
571135-01-5
141
142
CENTER WING BOX SKIN STGR 6-11, 11-15
DETAILED INSPECTION OF CENTER WING BOX, BOTTOM SKIN
UPPER SURFACE, INCLUDING STRINGERS, FROM STRINGER 6
TO STRINGER 11, BETWEEN Y=+/-765 AND FROM STRINGER 11
TO STRINGER 15, BETWEEN Y=+/-1292
ACCESS PANELS: 147AZ, 734, 148AZ, 744
AF
DET
INTERVALS
SOURCE
ST:
42000 FC
OR
60000 FH
SI:
11600 FC
OR
32000 FH
MRB
ST:
47000 FC
OR
60000 FH
SI:
11100 FC
OR
30500 FH
MRB
T:
32800 FC
OR
65600 FH
I:
9500 FC
OR
19000 FH
ST:
42000 FC
OR
60000 FH
SI:
15200 FC
OR
41900 FH
ALI
ST:
47000 FC
OR
60000 FH
SI:
14900 FC
OR
41000 FH
MRB
TPS
REFERENCES
571000-200-013
SOURCE:
MRB 571134-01-4
571000-200-013
SOURCE:
MRB 571134-01-5
571000-200-014
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
0.25
0.25
0.25
0.25
0649 1761
1890
1
1
1
1
0.25
0.25
0.25
0.25
1488 1560
1743 1851
1863 1876
1
1
0.50
0.50
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.50
0.50
0649 1761
1890
1
1
0.50
0.50
1488 1560
1743 1851
1863 1876
SOURCE:
ALI 571135-01-1
MRB
571000-200-014
SOURCE:
MRB 571135-01-4
571000-200-014
SOURCE:
MRB 571135-01-5
Sub 2 - Page 181 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
571136-01-1
ZONE
141
142
DESCRIPTION
CENTER WING BOX DRAIN HOLES
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTO) OF CENTER WING
BOX, DRAIN HOLES ON STRINGER 13 AND STRINGER 14 ON
BOTTOM SKIN, UPPER SURFACE (12 PLACES)
ACCESS PANELS: 147AZ, 734, 148AZ, 744
571136-01-2
141
142
CENTER WING BOX DRAIN HOLES
NDT
SDI
SPECIAL DETAILED INSPECTION (ROTO) OF CENTER WING BOX, DRAIN HOLES
ON STRINGER 13 AND STRINGER 14 ON BOTTOM SKIN, UPPER SURFACE (12
PLACES)
ACCESS PANELS: 147AZ, 734, 148AZ, 744
571154-01-1
571155-01-1
191
192
195
196
191
192
195
196
CENTER WING BOX LOWER SKIN
AF
DET
DETAILED INSPECTION OF CENTER WING BOX, LOWER SKIN
LOWER SURFACE, FROM FR 36 TO FR 42, BETWEEN RIB 1 LH
AND RIB 1 RH, INCLUDING LOWER SPLICE AT RIB 1, AS FAR
AS VISIBLE
ACCESS PANELS: 191BB, 191CT, 191EB, 191LB, 192CT, 192EB, 192FB, 192LB,
195BB, 734, 196BB, 744
CENTER WING BOX LOWER SKIN
DETAILED INSPECTION OF CENTER WING BOX, LOWER SKIN
LOWER SURFACE, FROM FR 36 TO FR 42 BETWEEN RIB 1 LH
AND RIB 1 RH, COVERED BY VAPOR SEAL
PREPARATION: AIR CONDITIONING PACKS; VAPOR SEAL (IF INSTALLED); HEAT
SHIELDS REMOVED;
AF
DET
INTERVALS
SOURCE
ST:
30000 FC
OR
60000 FH
SI:
7900 FC
OR
15800 FH
T:
36900 FC
OR
73900 FH
I:
7900 FC
OR
15800 FH
T:
20000 FC
OR
41700 FH
I:
8600 FC
OR
23700 FH
T:
6 YE
I:
6 YE
ALI
MRB
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
TPS
REFERENCES
571000-220-003
NTM 57-11-36
MEN
TASKM. APPLICABI
H.
LITY
1
1
1.00
1.00
1130 1200
1379 1578
1657 1767
2151 2163
1
1
1.00
1.00
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
1
1
0.50
0.50
0.50
0.50
ALL
1
1
1
1
0.40
0.40
0.40
0.40
ALL
SOURCE:
ALI 571136-01-1
MRB 571136-01-1
ALI
571000-220-003
NTM 57-11-36
SOURCE:
ALI 571136-01-2
MRB CPCP
1
571000-200-019
SOURCE:
MRB 571154-01-1
571000-200-016
SOURCE:
MRB 571155-01-1
ACCESS PANELS: 191BB, 191CT, 191EB, 191KB, 191LB, 192CT, 192EB, 192FB,
192KB, 192LB, 195AB, 734, 196AB, 744
Sub 2 - Page 182 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
571156-01-1
ZONE
137
138
DESCRIPTION
CENTER WING BOX FRONT SPAR
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF CENTER WING BOX, FRONT SPAR,
FORWARD FACE
PREPARATION: FWD ACT(S) REMOVED (IF INSTALLED); LINING REMOVED;
INSULATION REMOVED;
571157-01-1
145
146
ACCESS PANELS: 825
CENTER WING BOX UPPER SKIN
AF
DET
DETAILED INSPECTION OF CENTER WING BOX, UPPER SKIN
UPPER SURFACE AND BEAMS, INCLUDING FRAME FEET BETWEEN
FR 36 AND FR 42.
INTERVALS
SOURCE
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
T:
12 YE
I:
12 YE
MRB CPCP
T:
34000 FC
OR
60000 FH
I:
9100 FC
OR
18200 FH
T:
21000 FC
OR
42000 FH
I:
9100 FC
OR
18200 FH
T:
NOTE
I:
NOTE
ALI
TPS
REFERENCES
571000-200-020
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.40
0.40
ALL
1
1
0.75
0.75
ALL
1
1
0.60
0.60
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.60
0.60
1130 1200
1379 1578
1657 1767
2151 2163
1
1
14.00
14.00
1130 1200
1379 1578
1657 1767
SOURCE:
MRB 571156-01-1
1
571000-200-021
SOURCE:
MRB 571157-01-1
NOTE: - CAN BE PERFORMED AT SAME TIME AS 533135-01-1
- TPS MAY BE LIMITED TO CENTER WING BOX, UPPER
SKIN BEAMS, BETWEEN FR 36 AND FR 42
571170-01-1
191
192
PREPARATION: CABIN FLOOR PANELS REMOVED;
INSPECTION OF CENTER WING BOX
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX, CRUCIFORM
FITTING, REAR SPAR AT THE LEVEL OF FRAME 42, LH/RH
ACCESS PANELS: 191DT, 191ET, 192DT, 192ET
571170-01-2
191
192
INSPECTION OF CENTER WING BOX
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX, CRUCIFORM
FITTING, REAR SPAR AT THE LEVEL OF FRAME 42, LH/RH.
ACCESS PANELS: 191DT, 191ET, 192DT, 192ET
571173-01-1
540
640
CENTER WING BOX
SPECIAL DETAILED INSPECTION OF LOWER STIFFENERS IN
CENTER AND OUTER WING BOX AT LEVEL OF RIB 1 JUNCTION
NOTE: REFER TO ISB 57-1129 FOR THRESHOLD/INTERVAL
AND APPLICABILITY.
NDT
SDI
571000-220-006
NTM 57-11-47
SOURCE:
ALI 571170-01-1
ALI
571000-220-006
NTM 57-11-47
SOURCE:
ALI 571170-01-2
EASA AD
FAA AD
ISB
NTM 57-11-73
NTM 57-11-74
EASA AD
2007-0067
FAA AD
2008-02-15
ISB 57-1129
ACCESS PANELS: 147AZ, 540AB, 540AZ, 540BZ, 148AZ, 640AB, 640AZ, 640BZ
Sub 2 - Page 183 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
571175-01-1
ZONE
191
192
DESCRIPTION
CENTER WING BOX - EXTERNAL
SKILL TASK
CODE CODE
INTERVALS
SOURCE
ACCESS PANELS: 147CB, 191LB, 148DB, 192LB
CENTER WING BOX TRIFORM FITTING
EASA AD
FAA AD
ISB
NTM 57-11-75
EASA AD
2007-0067
FAA AD
2008-02-15
ISB 57-1130
1
1
6.00
6.00
0649 1130
1200 1379
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
NDT
SDI
T:
29600 FC
OR
59300 FH
I:
29600 FC
OR
59300 FH
ALI
571000-200-023
NTM 57-11-81
1
1
1.00
1.00
1130 1200
1379 1578
1657 1767
2151 2163
ST:
30000 FC
OR
60000 FH
SI:
14400 FC
OR
39600 FH
MRB
1
1
1.00
1.00
0649 1488
1560 1743
1761 1851
1863 1876
1890
T:
29600 FC
OR
59300 FH
I:
14800 FC
OR
29700 FH
ALI WFD
1
1
1.00
1.00
1130 1200
1379 1578
1657 1767
2151 2163
ST:
30000 FC
OR
60000 FH
SI:
14400 FC
OR
39600 FH
MRB
1
1
1.00
1.00
0649 1488
1560 1743
1761 1851
1863 1876
1890
PREPARATION: SEALANT REMOVED;
141
142
ACCESS PANELS: 147AZ, 734, 148AZ, 744
CENTER WING BOX TRIFORM FITTING
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF CWB, UPPER
SURFACE OF TRIFORM FITTING (ON FIRST ROW OF FASTENERS
FROM RIB 1), BETWEEN STRINGER 8 AND FR 42, LH/RH
PREPARATION: SEALANT REMOVED;
571182-01-1
540
640
ACCESS PANELS: 147AZ, 734, 148AZ, 744
OUTER WING TRIFORM FITTING
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF OUTER WB, UPPER
SURFACE OF TRIFORM FITTING (ON FIRST ROW OF FASTENERS
FROM RIB 1), BETWEEN STRINGER 8 AND FR 42, LH/RH
PREPARATION: SEALANT REMOVED;
571182-01-4
540
640
ACCESS PANELS: 540AB, 540AZ, 540BZ, 640AB, 640AZ, 640BZ
OUTER WING TRIFORM FITTING
SPECIAL DETAILED INSPECTION (US) OF OUTER WB, UPPER
SURFACE OF TRIFORM FITTING (ON FIRST ROW OF FASTENERS
FROM RIB 1), BETWEEN STRINGER 8 AND FR 42, LH/RH
PREPARATION: SEALANT REMOVED;
TASKM. APPLICABI
H.
LITY
T:
NOTE
I:
NOTE
SPECIAL DETAILED INSPECTION (US) OF CWB, UPPER
SURFACE OF TRIFORM FITTING (ON FIRST ROW OF FASTENERS
FROM RIB 1), BETWEEN STRINGER 8 AND FR 42, LH/RH
571181-01-4
MEN
SDI
NOTE: REFER TO ISB 57-1130 FOR THRESHOLD/INTERVAL
AND APPLICABILITY.
141
142
REFERENCES
NDT
SPECIAL DETAILED INSPECTION OF LOWER PANELS IN
CENTER AND OUTER WING BOX AT LEVEL OF RIB 1 JUNCTION
571181-01-1
TPS
NDT
SDI
SOURCE:
ALI 571181-01-1
571000-200-023
NTM 57-11-81
SOURCE:
MRB 571181-01-4
571000-200-024
NTM 57-11-82
SOURCE:
ALI 571182-01-1
571000-200-024
NTM 57-11-82
SOURCE:
MRB 571182-01-4
ACCESS PANELS: 540AB, 540AZ, 540BZ, 640AB, 640AZ, 640BZ
Sub 2 - Page 184 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
571183-01-1
571183-01-4
ZONE
191
192
195
196
191
192
195
196
DESCRIPTION
CENTER WING BOX LOWER SPLICE AT RIB 1
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF CWB, LOWER SPLICE
ON LOWER SKIN LOWER SURFACE AT RIB 1 (AT TWO CENTRAL
ROWS OF FASTENERS), BETWEEN STRINGER 8 AND FR 42,
LH/RH
ACCESS PANELS: 191LB, 192LB, 734, 744
CENTER WING BOX LOWER SPLICE AT RIB 1
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF CWB, LOWER SPLICE
ON LOWER SKIN LOWER SURFACE AT RIB 1 (AT TWO CENTRAL
ROWS OF FASTENERS), BETWEEN STRINGER 8 AND FR 42,
LH/RH
ACCESS PANELS: 191LB, 192LB, 734, 744
571185-01-1
540
640
OUTER WING UPPER HALF OF VERTICAL TEE
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF OUTER WING BOX
(HOLES ON) UPPER HALF OF VERTICAL TEE FITTING AT
JUNCTION WITH RIB 1 AND REAR SPAR, LH/RH
PREPARATION: SEALANT REMOVED;
571185-01-8
540
640
ACCESS PANELS: 540AB, 540AZ, 540BZ, 640AB, 640AZ, 640BZ
CENTER WING
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF OUTER WB, (HOLES ON) UPPER HALF
OF VERTICAL TEE FITTING AT JUNCTION WITH RIB 1 AND REAR SPAR, LH/RH.
PREPARATION: SEALANT REMOVAL FROM FASTENERS;
ACCESS PANELS: 540AB, 540AZ, 540BZ, 640AB, 640AZ, 640BZ
571189-01-3
141
142
CENTER WING BOX STRINGER WEB
DETAILED INSPECTION OF CENTER WING BOX, STRINGER WEB AT JUNCTION
WITH STRUT ATTACH FITTINGS ON UPPER STRINGERS 2, 3, 8, 9, 15, 16
ACCESS PANELS: 147AZ, 734, 148AZ, 744
AF
DET
INTERVALS
SOURCE
T:
29600 FC
OR
59300 FH
I:
15200 FC
OR
30400 FH
ST:
30000 FC
OR
60000 FH
SI:
14400 FC
OR
39600 FH
ALI WFD
T:
29000 FC
OR
60000 FH
I:
11200 FC
OR
33000 FH
ALI
ST:
30000 FC
OR
60000 FH
SI:
10000 FC
OR
20100 FH
MRB
T:
22600 FC
OR
59900 FH
I:
13100 FC
OR
36000 FH
ALI
TPS
REFERENCES
571000-200-025
NTM 57-11-83
SOURCE:
ALI 571183-01-1
MRB
571000-200-025
NTM 57-11-83
SOURCE:
MRB 571183-01-4
571000-200-026
NTM 57-11-85
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
1.00
1.00
1.00
1.00
1130 1200
1379 1578
1657 1767
2151 2163
1
1
1
1
1.00
1.00
1.00
1.00
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.50
0.50
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
ALI 571185-01-1
571000-200-026
NTM 57-11-85
SOURCE:
MRB 571185-01-8
571000-200-017
SOURCE:
ALI 571189-01-3
Sub 2 - Page 185 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
571189-01-8
ZONE
141
142
DESCRIPTION
CENTER WING BOX STRINGER WEB
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF CENTER WING BOX, STRINGER WEB AT JUNCTION
WITH STRUT ATTACH FITTINGS ON UPPER STRINGERS 2, 3, 8, 9, 15, 16.
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF ALI
TASKS 571189-01-1 OR 571189-01-5.
INTERVALS
SOURCE
ST:
30000 FC
OR
60000 FH
SI:
26000 FC
OR
52000 FH
MRB
T:
17800 FC
OR
45400 FH
I:
11100 FC
OR
29600 FH
ALI
T:
12 YE
I:
12 YE
MRB CPCP
T:
12 YE
I:
6 YE
MRB CPCP
TPS
REFERENCES
571000-200-017
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.60
0.60
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.50
0.50
0649
1
1
0.25
0.25
ALL
1
1
0.50
0.50
ALL
SOURCE:
MRB 571189-01-8
ACCESS PANELS: 147AZ, 148AZ, 734, 744
571192-01-2
141
142
CENTER WING BOX REAR SPAR
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING
BOX, REAR SPAR, EDGE OF LOWER FLANGE AT CORNER
FITTING, LH/RH
PREPARATION: SEALANT REMOVED;
571199-01-1
540
640
ACCESS PANELS: 147AZ, 734, 148AZ, 744
OUTER WING BOX EXTERNAL SURFACE
AF
DET
DETAILED INSPECTION OF OUTER WING BOX, EXTERNAL
SURFACE OF RIB 1 AND UPPER SURFACE OF TRIFORM
FITTING, BETWEEN FRONT SPAR AND REAR SPAR
572001-01-1
521
621
ACCESS PANELS: 540AB, 540AZ, 540BZ, 640AB, 640AZ, 640BZ
OUTER WING FRONT SPAR FWD FACE
DETAILED INSPECTION OF OUTER WING, FRONT SPAR FORWARD
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING VICINITY OF
CUTOUTS FOR SLAT TRACKS 1,2,3 AND 4
AF
DET
571000-220-005
NTM 57-11-92
SOURCE:
ALI 571192-01-2
NO
571000-200-022
SOURCE:
MRB 571199-01-1
572000-220-004
SOURCE:
MRB 572001-01-1
ACCESS PANELS: 521AB, 521BT, 521CB, 521EB, 521GB, 621AB, 621BT, 621CB,
621EB, 621GB
Sub 2 - Page 186 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572002-01-1
ZONE
540
640
DESCRIPTION
OUTER WING FRONT SPAR ROOT JOINT FTG
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT
FACE, UPPER AND LOWER ROOT JOINT FITTING
ACCESS PANELS: 540AB, 540AZ, 640AB, 640AZ
572004-01-1
540
640
OUTER WING FRONT SPAR AFT FACE
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT
FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THE AREA
INSIDE THE DRY BAY
ACCESS PANELS: 540AB, 540AZ, 540BB, 540CB, 640AB, 640AZ, 640BB, 640CB
AF
DET
INTERVALS
ST:
12 YE
OR
48000 FC
OR
60000 FH
SI:
12 YE
OR
15000 FC
OR
24800 FH
T:
24 YE
I:
12 YE
ST:
30500 FC
OR
61000 FH
SI:
15000 FC
OR
30000 FH
T:
60000 FC
OR
120000 FH
I:
15000 FC
OR
30000 FH
SOURCE
MRB CPCP
TPS
NO
REFERENCES
572000-200-003
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
1
1.00
1.00
1130 1200
1379 1578
1657 1767
SOURCE:
MRB 572002-01-1
ALI
MRB
572000-200-004
SOURCE:
ALI 572004-01-1
MRB 572004-01-1
Sub 2 - Page 187 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572004-01-4
ZONE
540
640
DESCRIPTION
OUTER WING FRONT SPAR AFT FACE
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT FACE, BETWEEN
RIB 1 AND RIB 8, EXCLUDING THE AREA INSIDE THE DRY BAY
ACCESS PANELS: 540AB, 540AZ, 540BB, 540CB, 640AB, 640AZ, 640BB, 640CB
572007-01-2
571
671
OUTER WING REAR SPAR AFT FACE
AF
DET
DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT FACE, BETWEEN RIB
1 AND GEAR SUPPORT RIB 5, INCLUDING REAR SPAR ANGLE
572007-01-8
571
671
OUTER WING REAR SPAR AFT FACE
DETAILED INSPECTION OF OUTER WING, REAR SPAR, AFT FACE, BETWEEN
RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING REAR SPAR ANGLE
AF
DET
INTERVALS
ST:
30000 FC
OR
49700 FH
SI:
14700 FC
OR
24300 FH
T:
39800 FC
OR
60000 FH
I:
14700 FC
OR
24300 FH
T:
12 YE
OR
11900 FC
OR
23800 FH
I:
6 YE
OR
11900 FC
OR
23800 FH
T:
12 YE
OR
10600 FC
OR
17400 FH
I:
6 YE
OR
10600 FC
OR
17400 FH
SOURCE
ALI
MRB
TPS
REFERENCES
572000-200-004
MEN
TASKM. APPLICABI
H.
LITY
1
1
1.00
1.00
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
1
0.50
0.50
1130 1200
1379 1578
1657 1767
1
1
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
SOURCE:
ALI 572004-01-4
MRB 572004-01-4
ALI
MRB CPCP
1+2 572000-200-005
SOURCE:
ALI 572007-01-2
MRB 572007-01-2
ALI
MRB CPCP
1+2 572000-200-005
SOURCE:
ALI 572007-01-8
MRB 572007-01-8
Sub 2 - Page 188 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572008-01-1
ZONE
574
674
DESCRIPTION
OUTER WING REAR SPAR JOINT PLATE
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER
WING, REAR SPAR AFT FACE SPAR JOINT PLATE AT RIB 6.
ACCESS PANELS: 574AB, 574BB, 674AB, 674BB
572008-01-3
574
674
OUTER WING REAR SPAR JOINT PLATE
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER WING, REAR SPAR
AFT FACE SPAR JOINT PLATE AT RIB 6
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
572008-01-1
572009-01-1
540
640
ACCESS PANELS: 574AB, 574BB, 674AB, 674BB
OUTER WING REAR SPAR
SPECIAL DETAILED INSPECTION (US) OF OUTER WING, REAR SPAR FORWARD
FACE, AT THE ATTACHMENT HOLES OF GEAR SUPPORT RIB 5, MLG FORWARD
PINTLE FITTING AND RETRACTION JACK FITTING
ACCESS PANELS: 540AB, 540BB, 540BZ, 640AB, 640BB, 640BZ
NDT
SDI
INTERVALS
SOURCE
ST:
48000 FC
OR
96000 FH
SI:
15000 FC
OR
30000 FH
MRB
ST:
48000 FC
OR
60000 FH
SI:
9000 FC
OR
16400 FH
MRB
T:
48000 FC
OR
96000 FH
I:
12000 FC
OR
24000 FH
ALI
TPS
REFERENCES
572000-200-006
NTM 57-20-08
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.50
0.50
1130 1200
1379 1578
1657 1767
1
1
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
1
0.62
0.62
1130 1200
1379 1578
1657 1767
SOURCE:
MRB 572008-01-1
572000-200-006
NTM 57-20-08
SOURCE:
MRB 572008-01-3
572000-280-801
NTM 57-21-10
SOURCE:
ALI 572009-01-1
Sub 2 - Page 189 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572010-01-4
ZONE
540
640
DESCRIPTION
OUTER WING REAR SPAR ROOT JOINT FTG
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD
FACE, UPPER AND LOWER ROOT JOINT FITTINGS
ACCESS PANELS: 540AB, 540BZ, 640AB, 640BZ
SKILL TASK
CODE CODE
AF
DET
INTERVALS
ST:
12 YE
OR
30000 FC
OR
60000 FH
SI:
12 YE
OR
15000 FC
OR
30000 FH
T:
24 YE
OR
58600 FC
OR
117200 FH
I:
12 YE
OR
15000 FC
OR
30000 FH
SOURCE
ALI
MRB CPCP
TPS
NO
REFERENCES
572000-200-007
SOURCE:
ALI 572010-01-4
MRB 572010-01-4
MEN
1
1
TASKM. APPLICABI
H.
LITY
0.20
0.20
1130 1200
1379 1578
1657 1767
Sub 2 - Page 190 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572010-01-5
ZONE
540
640
DESCRIPTION
OUTER WING REAR SPAR ROOT JOINT FTG
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD
FACE, UPPER AND LOWER ROOT JOINT FITTINGS.
ACCESS PANELS: 540AB, 540BZ, 640AB, 640BZ
SKILL TASK
CODE CODE
AF
DET
INTERVALS
ST:
12 YE
OR
30000 FC
OR
58900 FH
SI:
12 YE
OR
11400 FC
OR
23600 FH
T:
24 YE
OR
36200 FC
OR
60000 FH
I:
12 YE
OR
11400 FC
OR
23600 FH
SOURCE
ALI
MRB CPCP
TPS
NO
REFERENCES
572000-200-007
SOURCE:
ALI 572010-01-5
MRB 572010-01-5
MEN
1
1
TASKM. APPLICABI
H.
LITY
0.20
0.20
0649 1488
1560 1743
1761 1851
1863 1876
1890
Sub 2 - Page 191 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572010-01-7
ZONE
540
640
DESCRIPTION
OUTER WING REAR SPAR ROOT JOINT FTG
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD
FACE, UPPER AND LOWER ROOT JOINT FITTINGS.
ACCESS PANELS: 540AB, 540BZ, 640AB, 640BZ
572011-01-2
540
640
OUTER WING REAR SPAR FWD FACE
AF
DET
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE,
BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION OF THE JOINT AT RIB 6
AND TOP AND BOTTOM FLANGES
ACCESS PANELS: 540AB, 540BB, 540BZ, 540CB, 640AB, 640BB, 640BZ, 640CB
572011-01-5
540
640
OUTER WING REAR SPAR FWD FACE
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD FACE,
BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION OF THE JOINT AT RIB 6
AND TOP AND BOTTOM FLANGES
ACCESS PANELS: 540AB, 540BB, 540BZ, 540CB, 640AB, 640BB, 640BZ, 640CB
AF
DET
INTERVALS
ST:
12 YE
OR
30000 FC
OR
58900 FH
SI:
12 YE
OR
11400 FC
OR
23600 FH
T:
24 YE
OR
35200 FC
OR
60000 FH
I:
12 YE
OR
11400 FC
OR
23600 FH
T:
32400 FC
OR
64800 FH
I:
9300 FC
OR
18600 FH
T:
32900 FC
OR
60000 FH
I:
9400 FC
OR
15300 FH
SOURCE
ALI
MRB CPCP
TPS
NO
REFERENCES
572000-200-007
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
2151 2163
1
1
1.00
1.00
1130 1200
1379 1578
1657 1767
1
1
1.00
1.00
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
ALI 572010-01-7
MRB 572010-01-7
ALI
572000-200-008
SOURCE:
ALI 572011-01-2
ALI
572000-200-008
SOURCE:
ALI 572011-01-5
Sub 2 - Page 192 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572011-01-6
ZONE
540
640
DESCRIPTION
OUTER WING REAR SPAR FWD FACE
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
ACCESS PANELS: 540AB, 540BB, 540BZ, 540CB, 640AB, 640BB, 640BZ, 640CB
572012-01-1
500
600
OUTER WING TOP SKIN UPR SURFACE
AF
DET
DETAILED INSPECTION OF OUTER WING, TOP SKIN UPPER
SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 1 AND RIB 8
572012-01-3
500
600
OUTER WING TOP SKIN UPR SURFACE
AF
DET
DETAILED INSPECTION OF OUTER WING, TOP SKIN UPPER
SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 1 AND RIB 8
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS
ACCOMPLISHMENT OF TASK 572012-01-1
572014-01-3
500
600
OUTER WING TOP SKIN
GENERAL VISUAL INSPECTION OF OUTER WING, TOP SKIN,
UPPER SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS
BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR
AF
GVI
INTERVALS
SOURCE
T:
32400 FC
OR
53300 FH
I:
9100 FC
OR
15000 FH
ST:
30000 FC
OR
60000 FH
SI:
15000 FC
OR
30000 FH
T:
59600 FC
OR
119200 FH
I:
15000 FC
OR
30000 FH
ST:
31000 FC
OR
50000 FH
SI:
15000 FC
OR
24000 FH
ALI
T:
48300 FC
OR
96600 FH
I:
15000 FC
OR
30000 FH
ALI
TPS
REFERENCES
572000-200-008
MEN
TASKM. APPLICABI
H.
LITY
1
1
1.00
1.00
2151 2163
1
1
0.50
0.50
1130 1200
1379 1578
1657 1767
1
1
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
1
1.25
1.25
1130 1200
1379 1578
1657 1767
SOURCE:
ALI 572011-01-6
ALI
MRB
572000-220-001
SOURCE:
ALI 572012-01-1
MRB 572012-01-1
MRB
572000-220-001
SOURCE:
MRB 572012-01-3
572000-210-802
SOURCE:
ALI 572014-01-3
Sub 2 - Page 193 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572019-01-1
ZONE
540
640
DESCRIPTION
OUTER WING TOP SKIN STGR CROWN FTG
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGER
CROWN FITTINGS AT ROOT JOINT, FROM FRONT SPAR TO REAR
SPAR
ACCESS PANELS: 540AB, 540AZ, 540BZ, 640AB, 640AZ, 640BZ
572019-01-3
540
640
OUTER WING TOP SKIN STGR CROWN FTG
AF
DET
DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGER
CROWN FITTINGS AT ROOT JOINT, FROM FRONT SPAR TO REAR
SPAR
ACCESS PANELS: 540AB, 540AZ, 540BZ, 640AB, 640AZ, 640BZ
572019-01-4
540
640
OUTER WING TOP SKIN STGR CROWN FTG
AF
DET
DETAILED INSPECTION OF OUTER WING, TOP SKIN, STRINGER
CROWN FITTINGS AT ROOT JOINT FROM FRONT SPAR TO REAR
SPAR
ACCESS PANELS: 540AB, 540AZ, 540BZ, 640AB, 640AZ, 640BZ
572020-01-1
540
640
OUTER WING TOP SKIN RIB 1 AND 8
AF
DET
DETAILED INSPECTION OF OUTER WING, TOP SKIN
STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS
AND AIR TRANSFER HOLES, STRINGER JOINTS, AND BUTT
STRAP, AT STRINGER 11, EXCLUDING THE AREA INSIDE THE
DRY BAY
INTERVALS
SOURCE
ST:
48000 FC
OR
60000 FH
SI:
20000 FC
OR
27900 FH
MRB
ST:
48000 FC
OR
60000 FH
SI:
17800 FC
OR
24900 FH
MRB
ST:
48000 FC
OR
96000 FH
SI:
17800 FC
OR
35600 FH
MRB
T:
33900 FC
OR
67800 FH
I:
11700 FC
OR
23400 FH
ALI
T:
33900 FC
OR
60000 FH
I:
10500 FC
OR
20400 FH
ALI
TPS
REFERENCES
572000-200-009
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.34
0.34
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.34
0.34
2151 2163
1
1
0.34
0.34
1130 1200
1379 1578
1657 1767
2
2
3.00
3.00
1130 1200
1379 1578
1657 1767
2
2
3.00
3.00
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
MRB 572019-01-1
572000-200-009
SOURCE:
MRB 572019-01-3
572000-200-009
SOURCE:
MRB 572019-01-4
572000-200-010
SOURCE:
ALI 572020-01-1
ACCESS PANELS: 540AB, 540AZ, 540BB, 540BZ, 640AB, 640AZ, 640BB, 640BZ
572020-01-3
540
640
OUTER WING TOP SKIN RIB 1 AND 8
DETAILED INSPECTION OF OUTER WING, TOP SKIN
STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS
AND AIR TRANSFER HOLES AND BUTT STRAP, AT STRINGER
11, EXCLUDING THE AREA INSIDE THE DRY BAY
ACCESS PANELS: 540AB, 540AZ, 540BB, 540BZ, 640AB, 640AZ, 640BB, 640BZ
AF
DET
572000-200-010
SOURCE:
ALI 572020-01-3
Sub 2 - Page 194 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572020-01-9
ZONE
540
640
DESCRIPTION
OUTER WING TOP SKIN RIB 1 AND 8
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, TOP SKIN
STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING
RUNOUTS AND AIR TRANSFER HOLES, STRINGER JOINTS,
AND BUTT STRAP, AT STRINGER 11, EXCLUDING THE AREA
INSIDE THE DRY BAY
INTERVALS
SOURCE
T:
33900 FC
OR
60000 FH
I:
11700 FC
OR
22600 FH
ALI
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
ST:
38500 FC
OR
54000 FH
SI:
25000 FC
OR
35000 FH
MRB CPCP
ST:
30000 FC
OR
60000 FH
SI:
19300 FC
OR
38600 FH
MRB
ST:
30000 FC
OR
43200 FH
SI:
19300 FC
OR
27000 FH
MRB
TPS
REFERENCES
572000-200-010
MEN
TASKM. APPLICABI
H.
LITY
2
2
3.00
3.00
2151 2163
1
1
1
1
0.15
0.15
0.15
0.15
ALL
1
1
1.00
1.00
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
1.00
1.00
1130 1200
1379 1578
1657 1767
1
1
1.00
1.00
2151 2163
SOURCE:
ALI 572020-01-9
ACCESS PANELS: 540AB, 540AZ, 540BB, 540BZ, 640AB, 640AZ, 640BB, 640BZ
572022-01-1
521
540
621
640
OUTER WING TOP SKIN LWR SURFACE
AF
DET
DETAILED INSPECTION OF OUTER WING, TOP SKIN, LOWER
SURFACE PYLON REINFORCING PLATE
ACCESS PANELS: 521BT, 540BB, 540CB, 621BT, 640BB, 640CB
572024-01-1
540
640
OUTER WING RIBS OUTBOARD FACE
AF
DET
DETAILED INSPECTION OF OUTER WING RIBS, OUTBOARD FACE OF RIB 2, RIB
3 AND RIB 4 AT SKIN ATTACHMENTS (INCLUDING CLEATS), SPAR
ATTACHMENTS, AND IN REGION OF STRINGER CUTOUTS.
ACCESS PANELS: 540AB, 640AB
572024-01-4
540
640
OUTER WING RIBS OUTBOARD FACE
AF
DET
DETAILED INSPECTION OF OUTER WING RIBS, OUTBOARD FACE OF RIB 2, RIB
3 AND RIB 4 AT SKIN ATTACHMENTS (INCLUDING CLEATS), SPAR
ATTACHMENTS, AND IN REGION OF STRINGER CUTOUTS.
ACCESS PANELS: 540AB, 640AB
572024-01-5
540
640
OUTER WING RIBS OUTBOARD FACE
DETAILED INSPECTION OF OUTER WING RIBS, OUTBOARD FACE
OF RIB 2, RIB 3 AND RIB 4 AT SKIN ATTACHMENTS
(INCLUDING CLEATS), SPAR ATTACHMENTS, AND IN REGION
OF STRINGER CUTOUTS.
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS
ACCOMPLISHMENT OF TASK 572024-01-4.
AF
DET
572000-200-011
SOURCE:
MRB 572022-01-1
MRB
572000-200-013
SOURCE:
MRB 572024-01-1
572000-200-013
SOURCE:
MRB 572024-01-4
572000-200-013
SOURCE:
MRB 572024-01-5
ACCESS PANELS: 540AB 640AB
Sub 2 - Page 195 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572026-01-1
ZONE
540
640
DESCRIPTION
OUTER WING BOLTED PANEL
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, RIB 5, AFT OF
BOLTED PANEL
ACCESS PANELS: 540AB, 540BB, 640AB, 640BB
572026-01-6
540
640
OUTER WING BOLTED PANEL
AF
DET
DETAILED INSPECTION OF OUTER WING, RIB 5, AFT OF BOLTED PANEL
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
572026-01-1
ACCESS PANELS: 540AB, 540BB, 640AB, 640BB
572027-01-1
540
640
OUTER WING RIB 5 AND RIB 6
AF
DET
DETAILED INSPECTION OF OUTER WING, RIB 5 AND RIB 6 AT SKIN
ATTACHMENTS (INCLUDING CLEATS) SPAR ATTACHMENTS, ACCESS CUTOUT
SURROUNDS AND IN REGION OF STRINGER CUTOUTS, EXCLUDING THE AREA
INSIDE THE DRY BAY
ACCESS PANELS: 540AB, 540BB, 640AB, 640BB
572027-01-2
540
640
OUTER WING RIB 5 AND RIB 6
DETAILED INSPECTION OF OUTER WING, RIB 5 AND RIB 6 AT SKIN
ATTACHMENTS (INCLUDING CLEATS) SPAR ATTACHMENTS, ACCESS CUTOUT
SURROUNDS AND IN REGION OF STRINGER CUTOUTS, EXCLUDING THE AREA
INSIDE THE DRY BAY
ACCESS PANELS: 540AB, 540BB, 640AB, 640BB
AF
DET
INTERVALS
SOURCE
ST:
30000 FC
OR
60000 FH
SI:
15000 FC
OR
30000 FH
MRB
ST:
30000 FC
OR
60000 FH
SI:
10800 FC
OR
25300 FH
T:
38300 FC
OR
60000 FH
I:
10800 FC
OR
25300 FH
ST:
48000 FC
OR
60000 FH
SI:
16900 FC
OR
27900 FH
ALI
MRB
ST:
30000 FC
OR
60000 FH
SI:
16000 FC
OR
32000 FH
MRB
TPS
REFERENCES
572000-200-014
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.50
0.50
1130 1200
1379 1578
1657 1767
1
1
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
1
0.70
0.70
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.70
0.70
1130 1200
1379 1578
1657 1767
SOURCE:
MRB 572026-01-1
572000-200-014
SOURCE:
ALI 572026-01-6
MRB 572026-01-6
MRB
572000-200-015
SOURCE:
MRB 572027-01-1
572000-200-015
SOURCE:
MRB 572027-01-2
Sub 2 - Page 196 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572027-01-4
ZONE
540
640
DESCRIPTION
OUTER WING RIB 5 AND RIB 6
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, RIB 5 AND RIB 6 AT
SKIN ATTACHMENTS (INCLUDING CLEATS) SPAR ATTACHMENTS,
ACCESS CUTOUT SURROUNDS AND IN REGION OF STRINGER
CUTOUTS, EXCLUDING THE AREA INSIDE THE DRY BAY
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS
ACCOMPLISHMENT OF TASK 572027-01-2
572028-01-1
540
640
ACCESS PANELS: 540AB, 540BB, 640AB, 640BB
OUTER WING RIB 7 AND 8
AF
DET
DETAILED INSPECTION OF OUTER WING, RIB 7 AND RIB 8
AND PYLON REAR FITTING EXCLUDING PICK-UP LUG
ACCESS PANELS: 540BB, 540CB, 640BB, 640CB
572028-01-2
540
640
OUTER WING RIB 7 AND 8
AF
DET
DETAILED INSPECTION OF OUTER WING, RIB 7 AND RIB 8 AND PYLON REAR
FITTING EXCLUDING PICK-UP LUG
ACCESS PANELS: 540BB, 540CB, 640BB, 640CB
572029-01-2
500
600
OUTER WING BOTTOM SKIN RIB 1-7
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT ATTACHMENT TO FRONT SPAR, BETWEEN RIB 1
AND RIB 7, EXCLUDING AREA COVERED BY PYLON FAIRING
AND PYLON REINFORCING
572029-01-5
500
600
OUTER WING BOTTOM SKIN RIB 1-7
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT ATTACHMENT TO FRONT SPAR, BETWEEN RIB 1
AND RIB 7, EXCLUDING AREA COVERED BY PYLON FAIRING
AND PYLON REINFORCING
AF
DET
INTERVALS
SOURCE
ST:
48000 FC
OR
60000 FH
SI:
16000 FC
OR
26500 FH
MRB
ST:
48000 FC
OR
96000 FH
SI:
20000 FC
OR
40000 FH
MRB
ST:
48000 FC
OR
60000 FH
SI:
20000 FC
OR
27900 FH
MRB
ST:
34700 FC
OR
69400 FH
SI:
15000 FC
OR
30000 FH
MRB
ST:
30000 FC
OR
41500 FH
SI:
12000 FC
OR
18000 FH
MRB
TPS
REFERENCES
572000-200-015
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.70
0.70
2151 2163
1
1
0.50
0.50
1130 1200
1379 1578
1657 1767
1
1
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
1
0.10
0.10
1130 1200
1379 1578
1657 1767
1
1
0.10
0.10
2151 2163
SOURCE:
MRB 572027-01-4
572000-200-016
SOURCE:
MRB 572028-01-1
572000-200-016
SOURCE:
MRB 572028-01-2
572000-200-017
SOURCE:
MRB 572029-01-2
572000-200-017
SOURCE:
MRB 572029-01-5
Sub 2 - Page 197 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572029-01-6
ZONE
500
600
DESCRIPTION
OUTER WING BOTTOM SKIN RIB 1-7
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT ATTACHMENT TO FRONT SPAR, BETWEEN RIB 1
AND RIB 7, EXCLUDING AREA COVERED BY PYLON FAIRING
AND PYLON REINFORCING
572031-01-1
411
421
500
600
OUTER WING BOTTOM SKIN LWR SURFACE
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT FRONT SPAR MASKED BY PYLON FAIRING AND
VISIBLE PORTION OF PYLON REINFORCING PLATE
PREPARATION: PYLON FAIRINGS REMOVED;
572032-01-1
500
600
OUTER WING BOTTOM SKIN/REAR SPAR
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 1 AND
RIB 8, EXCLUDING AREAS COVERED BY MLG REINFORCING
PLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING
572032-01-3
500
600
OUTER WING BOTTOM SKIN/REAR SPAR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 1 AND
RIB 8, EXCLUDING AREAS COVERED BY MLG REINFORCING
PLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING
AF
DET
INTERVALS
SOURCE
ST:
30000 FC
OR
41500 FH
SI:
14000 FC
OR
20000 FH
MRB
ST:
48000 FC
OR
60000 FH
SI:
15800 FC
OR
22000 FH
MRB
ST:
32200 FC
OR
64400 FH
SI:
7500 FC
OR
15000 FH
T:
60000 FC
OR
120000 FH
I:
7500 FC
OR
15000 FH
T:
18000 FC
OR
31200 FH
I:
6500 FC
OR
11300 FH
ALI
MRB
TPS
REFERENCES
572000-200-017
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.10
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
1
1
0.20
0.20
0.20
0.20
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
1
0.20
0.20
1130 1200
1379 1578
1657 1767
1
1
0.20
0.20
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
MRB 572029-01-6
572000-200-019
SOURCE:
MRB 572031-01-1
572000-200-020
SOURCE:
ALI 572032-01-1
MRB 572032-01-1
ALI
572000-200-020
SOURCE:
ALI 572032-01-3
Sub 2 - Page 198 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572032-01-5
ZONE
500
600
DESCRIPTION
OUTER WING BOTTOM SKIN/REAR SPAR
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 1 AND
RIB 8, EXCLUDING AREAS COVERED BY MLG REINFORCING
PLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING
572033-01-1
540
640
OUTER WING BOTTOM SKIN LDG PLATE
NDT
SDI
SPECIAL DETAILED INSPECTION (X-RAY) OF OUTER WING,
BOTTOM SKIN, FORWARD OF REAR SPAR IN AREA MASKED BY
MLG REINFORCING PLATE INCLUDING ATTACHMENT TO REAR
SPAR.
ACCESS PANELS: 540AB, 540BB, 640AB, 640BB
572033-01-3
540
640
OUTER WING BOTTOM SKIN LDG PLATE
NDT
SDI
SPECIAL DETAILED INSPECTION (X-RAY) OF OUTER WING,
BOTTOM SKIN, FORWARD OF REAR SPAR IN AREA MASKED BY
MLG REINFORCING PLATE INCLUDING ATTACHMENT TO REAR
SPAR.
ACCESS PANELS: 540AB, 540BB, 640AB, 640BB
572033-01-4
540
640
OUTER WING BOTTOM SKIN LDG PLATE
SPECIAL DETAILED INSPECTION (X-RAY) OF OUTER WING,
BOTTOM SKIN, FORWARD OF REAR SPAR IN AREA MASKED BY
MLG REINFORCING PLATE INCLUDING ATTACHMENT TO REAR
SPAR.
ACCESS PANELS: 540AB, 540BB, 640AB, 640BB
NDT
SDI
INTERVALS
SOURCE
T:
24000 FC
OR
42000 FH
I:
6500 FC
OR
11300 FH
ST:
30000 FC
OR
60000 FH
SI:
15000 FC
OR
30000 FH
T:
48000 FC
OR
96000 FH
I:
15000 FC
OR
30000 FH
ST:
48000 FC
OR
60000 FH
SI:
58000 FC
OR
81000 FH
ALI
ST:
34000 FC
OR
47000 FH
SI:
49000 FC
OR
69000 FH
MRB
TPS
REFERENCES
572000-200-020
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
2151 2163
1
1
0.50
0.50
1130 1200
1379 1578
1657 1767
1
1
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.50
0.50
2151 2163
SOURCE:
ALI 572032-01-5
ALI
MRB
572000-200-021
NTM 57-20-33
SOURCE:
ALI 572033-01-1
MRB 572033-01-1
MRB
572000-200-021
NTM 57-20-33
SOURCE:
MRB 572033-01-3
572000-200-021
NTM 57-20-33
SOURCE:
MRB 572033-01-4
Sub 2 - Page 199 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572034-01-1
ZONE
500
600
DESCRIPTION
OUTER WING BOTTOM SKIN LDG PLATE
SKILL TASK
CODE CODE
AF
GVI
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN
LOWER SURFACE MLG REINFORCING PLATE
572034-01-7
500
600
OUTER WING BOTTOM SKIN LDG PLATE
AF
GVI
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN
LOWER SURFACE MLG REINFORCING PLATE
572036-01-2
531
631
OUTER WING BOTTOM SKIN FLAP TRACK 2
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE, FORWARD OF REAR SPAR IN AREA COVERED BY FLAP
TRACK 2 FAIRINGS, INCLUDING ATTACHMENT TO REAR SPAR
ACCESS PANELS: 531AB, 531BB, 531CB, 631AB, 631BB, 631CB
AF
DET
INTERVALS
T:
31700 FC
OR
51400 FH
I:
10100 FC
OR
16300 FH
T:
25000 FC
OR
40500 FH
I:
8300 FC
OR
13300 FH
ST:
33800 FC
OR
67600 FH
SI:
10700 FC
OR
21400 FH
T:
60000 FC
OR
120000 FH
I:
10700 FC
OR
21400 FH
SOURCE
ALI
TPS
REFERENCES
572000-210-003
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.20
0.20
2151 2163
1
1
0.10
0.10
1130 1200
1379 1578
1657 1767
SOURCE:
ALI 572034-01-1
ALI
572000-210-003
SOURCE:
ALI 572034-01-7
ALI
MRB
572000-200-022
SOURCE:
ALI 572036-01-2
MRB 572036-01-2
Sub 2 - Page 200 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572036-01-5
ZONE
531
631
DESCRIPTION
OUTER WING BOTTOM SKIN FLAP TRACK 2
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE, FORWARD OF REAR SPAR IN AREA COVERED BY FLAP
TRACK 2 FAIRINGS, INCLUDING ATTACHMENT TO REAR SPAR
ACCESS PANELS: 531AB, 531BB, 531CB, 631AB, 631BB, 631CB
572036-01-7
531
631
OUTER WING
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE, FORWARD OF REAR SPAR IN AREA COVERED BY FLAP
TRACK 2 FAIRINGS. INCLUDING ATTACHMENT TO REAR SPAR.
ACCESS PANELS: 531AB, 531BB, 531CB, 631AB, 631BB, 631CB
572037-02-4
471
481
OUTER WING
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER
SURFACE ATTACHMENT TO REAR SPAR IN AREA COVERED BY
PYLON FAIRING.
PREPARATION: REMOVE PYLON FAIRINGS;
AF
DET
INTERVALS
ST:
30000 FC
OR
52100 FH
SI:
10200 FC
OR
17700 FH
T:
36500 FC
OR
60000 FH
I:
10200 FC
OR
17700 FH
ST:
30000 FC
OR
52100 FH
SI:
10700 FC
OR
18600 FH
T:
35800 FC
OR
60000 FH
I:
10700 FC
OR
18600 FH
ST:
32800 FC
OR
65600 FH
SI:
5300 FC
OR
10600 FH
SOURCE
ALI
MRB
TPS
REFERENCES
572000-200-022
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.10
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.10
0.10
2151 2163
1
1
0.50
0.50
1130 1200
1379 1578
1657 1767
SOURCE:
ALI 572036-01-5
MRB 572036-01-5
ALI
MRB
572000-200-022
SOURCE:
ALI 572036-01-7
MRB 572036-01-7
MRB
572000-220-804
SOURCE:
MRB 572037-02-4
Sub 2 - Page 201 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572037-02-5
ZONE
471
481
DESCRIPTION
OUTER WING
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER
SURFACE ATTACHMENT TO REAR SPAR IN AREA COVERED BY
PYLON FAIRING
PREPARATION: REMOVE PYLON FAIRINGS;
572038-01-1
500
600
OUTER WING BOTTOM SKIN RUNOUTS
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE AT
RUNOUTS OF STRINGER 2 (RIB BAY 5-6), STRINGER 9 (RIB BAYS 2-3 AND 6-7),
STRINGER 10 (RIB BAYS 2-3 AND 6-7), STRINGER 14 (RIB BAY 3-4) AND
STRINGER 15 (RIB BAY 2-3)
572038-01-4
500
600
OUTER WING BOTTOM SKIN RUNOUTS
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT RUNOUTS OF STRINGER 2 (RIB BAY 5-6),
STRINGER 9 (RIB BAYS 2-3 AND 6-7), STRINGER 10
(RIB BAYS 2-3 AND 6-7), STRINGER 14 (RIB BAY 3-4) AND
STRINGER 15 (RIB BAY 2-3)
572040-01-2
540
640
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS
ACCOMPLISHMENT OF TASK 572038-01-1
OUTER WING BOTTOM SKIN CUTOUTS
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, UPPER AND LOWER
SURFACES, AROUND ACCESS DOOR CUTOUTS IN RIB BAY 2-3 AND RIB BAY 6-7
AF
DET
INTERVALS
SOURCE
ST:
32800 FC
OR
57000 FH
SI:
5300 FC
OR
9200 FH
MRB
ST:
30000 FC
OR
60000 FH
SI:
5600 FC
OR
11200 FH
T:
54600 FC
OR
109200 FH
I:
5600 FC
OR
11200 FH
ST:
30000 FC
OR
52100 FH
SI:
5600 FC
OR
9700 FH
ALI
MRB
T:
12 YE
I:
6 YE
MRB CPCP
TPS
REFERENCES
572000-220-804
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.35
0.35
1130 1200
1379 1578
1657 1767
1
1
0.35
0.35
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
1
0.10
0.10
ALL
SOURCE:
MRB 572037-02-5
572000-200-023
SOURCE:
ALI 572038-01-1
MRB 572038-01-1
MRB
572000-200-023
SOURCE:
MRB 572038-01-4
NO
572000-200-001
SOURCE:
MRB 572040-01-2
ACCESS PANELS: 540AB, 540BB, 640AB, 640BB
Sub 2 - Page 202 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572040-03-2
ZONE
540
640
DESCRIPTION
OUTER WING BOTTOM SKIN CUTOUTS
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING, BOTTOM SKIN,
UPPER AND LOWER SURFACES, AROUND ACCESS DOOR CUTOUTS IN RIB BAY
2-3 AND RIB BAY 6-7
ACCESS PANELS: 540AB, 540BB, 640AB, 640BB
572040-03-4
540
640
OUTER WING BOTTOM SKIN CUTOUTS
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING, BOTTOM SKIN,
UPPER AND LOWER SURFACES, AROUND ACCESS DOOR CUTOUTS IN RIB BAY
2-3 AND RIB BAY 6-7
ACCESS PANELS: 540AB, 540BB, 640AB, 640BB
572040-03-6
540
640
OUTER WING
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,
BOTTOM SKIN, UPPER AND LOWER SURFACES, AROUND ACCESS
DOOR CUTOUTS IN RIB BAY 2-3 AND RIB BAY 6-7
ACCESS PANELS: 540AB, 540BB, 640AB, 640BB
572041-02-4
500
600
OUTER WING
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER
SURFACE AT ATTACHMENT TO RIBS AND STRINGERS
(EXCLUDING STRINGERS 8 AND 11) BETWEEN RIB 1 AND RIB
8 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS
COVERED BY FAIRINGS AND REINFORCING PLATES.
AF
DET
INTERVALS
SOURCE
ST:
30000 FC
OR
51300 FH
SI:
15000 FC
OR
25600 FH
MRB
ST:
30000 FC
OR
60000 FH
SI:
15000 FC
OR
30000 FH
T:
51900 FC
OR
103800 FH
I:
15000 FC
OR
30000 FH
ST:
30000 FC
OR
51300 FH
SI:
15000 FC
OR
25600 FH
ALI
MRB
T:
31200 FC
OR
62400 FH
I:
4900 FC
OR
9800 FH
ALI
TPS
REFERENCES
572000-200-032
NTM 57-20-40
MEN
TASKM. APPLICABI
H.
LITY
1
1
1.00
1.00
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
1.00
1.00
1130 1200
1379 1578
1657 1767
1
1
1.00
1.00
2151 2163
1
1
0.70
0.70
1130 1200
1379 1578
1657 1767
SOURCE:
MRB 572040-03-2
572000-200-032
NTM 57-20-40
SOURCE:
ALI 572040-03-4
MRB 572040-03-4
MRB
572000-200-032
NTM 57-20-40
SOURCE:
MRB 572040-03-6
572000-220-802
SOURCE:
ALI 572041-02-4
Sub 2 - Page 203 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572041-02-5
ZONE
500
600
DESCRIPTION
OUTER WING
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER
SURFACE AT ATTACHMENT TO RIBS AND STRINGERS
(EXCLUDING STRINGERS 8 AND 11) BETWEEN RIB 1 AND RIB
8 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS
COVERED BY FAIRINGS AND REINFORCING PLATES.
572041-02-7
500
600
OUTER WING
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER SURFACE AT
ATTACHMENT TO RIBS AND STRINGERS (EXCLUDING STRINGERS 8 AND 11)
BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR EXCLUDING
AREAS COVERED BY FAIRINGS AND REINFORCING PLATES.
572042-01-2
471
481
OUTER WING BOTTOM SKIN LOWER SURFACE
AF
GVI
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN
LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, IN
AREA COVERED BY PYLON FAIRING
PREPARATION: PYLON FAIRINGS REMOVED;
572042-01-7
471
481
OUTER WING BOTTOM SKIN LOWER SURFACE
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN
LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, IN
AREA COVERED BY PYLON FAIRING
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS
ACCOMPLISHMENT OF TASK 572042-01-2
AF
GVI
INTERVALS
T:
31200 FC
OR
50700 FH
I:
4900 FC
OR
7900 FH
ST:
30000 FC
OR
48700 FH
SI:
4900 FC
OR
7900 FH
T:
37600 FC
OR
60000 FH
I:
4900 FC
OR
7900 FH
T:
37300 FC
OR
74600 FH
I:
5300 FC
OR
10600 FH
T:
24000 FC
OR
42000 FH
I:
3800 FC
OR
6200 FH
SOURCE
ALI
TPS
REFERENCES
572000-220-802
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.70
0.70
2151 2163
1
1
0.70
0.70
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.15
0.15
1130 1200
1379 1578
1657 1767
1
1
0.15
0.15
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
SOURCE:
ALI 572041-02-5
ALI
MRB
572000-220-802
SOURCE:
ALI 572041-02-7
MRB 572041-02-7
ALI
572000-210-005
SOURCE:
ALI 572042-01-2
ALI
572000-210-005
SOURCE:
ALI 572042-01-7
PREPARATION: PYLON FAIRINGS REMOVED;
Sub 2 - Page 204 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572044-01-2
ZONE
500
600
DESCRIPTION
OUTER WING BOTTOM SKIN LOWER SURFACE
SKILL TASK
CODE CODE
AF
GVI
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN
LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS
COVERED BY REINFORCING PLATES AND FAIRINGS
572044-01-3
500
600
OUTER WING BOTTOM SKIN LOWER SURFACE
AF
GVI
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN
LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS
COVERED BY REINFORCING PLATES AND FAIRINGS
572044-01-7
500
600
OUTER WING BOTTOM SKIN LOWER SURFACE
AF
GVI
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN
LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS
COVERED BY REINFORCING PLATES AND FAIRINGS
572047-01-1
471
481
OUTER BOTTOM SKIN LOWER SURFACE
NDT
SDI
SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF OUTER
WING, BOTTOM SKIN, LOWER SURFACE AROUND AFT PYLON
ATTACHMENT FITTING CUTOUT.
PREPARATION: PYLON FAIRINGS REMOVED;
572047-01-3
471
481
OUTER BOTTOM SKIN LOWER SURFACE
SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF OUTER
WING, BOTTOM SKIN, LOWER SURFACE AROUND AFT PYLON
ATTACHMENT FITTING CUTOUT.
PREPARATION: PYLON FAIRINGS
REMOVED;
NDT
SDI
INTERVALS
SOURCE
T:
38000 FC
OR
76000 FH
I:
5800 FC
OR
11600 FH
T:
26300 FC
OR
42800 FH
I:
3800 FC
OR
6200 FH
T:
22600 FC
OR
36800 FH
I:
3800 FC
OR
6200 FH
ST:
30000 FC
OR
60000 FH
SI:
15000 FC
OR
30000 FH
ALI
ST:
30000 FC
OR
44900 FH
SI:
13300 FC
OR
19900 FH
MRB
TPS
REFERENCES
572000-210-004
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.10
0.10
1130 1200
1379 1578
1657 1767
1
1
0.10
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.10
0.10
2151 2163
1
1
0.30
0.30
1130 1200
1379 1578
1657 1767
1
1
0.30
0.30
2151 2163
SOURCE:
ALI 572044-01-2
ALI
572000-210-004
SOURCE:
ALI 572044-01-3
ALI
572000-210-004
SOURCE:
ALI 572044-01-7
MRB
572000-200-024
NTM 57-20-47
SOURCE:
MRB 572047-01-1
572000-200-024
NTM 57-20-47
SOURCE:
MRB 572047-01-3
Sub 2 - Page 205 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572047-01-4
ZONE
471
481
DESCRIPTION
OUTER BOTTOM SKIN LOWER SURFACE
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (EDDY CURRENT) OF OUTER WING, BOTTOM
SKIN, LOWER SURFACE AROUND AFT PYLON ATTACHMENT FITTING CUTOUT
PREPARATION: PYLON FAIRINGS REMOVED;
572049-01-4
500
600
OUTER WING BOTTOM SKIN DRAIN HOLES
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER SURFACE AT
DRAIN HOLES FOR TRACK CANS, 1,2,3,& 4 (RIB BAYS 1-2, 2-3, 4-5, 5-6), DRY BAY
DRAIN HOLE IN RIB BAY 6-7; MAGNETIC LEVEL INDICATOR HOLE ADJACENT TO
RIB 6; MLG PICK UP RAIL HOLE FORWARD OF REAR SPAR INBOARD OF RIB 5.
572050-01-1
540
640
OUTER WING, DRY BAY AREA
AF
DET
DETAILED INSPECTION OF OUTER WING, DRY BAY AREA
NOTE:
- THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-1.
- IF AN A/C HAS ALREADY EXCEEDED THE INSPECTION
THRESHOLD OF THIS TASK, THE INSPECTION SHOULD BE
PERFORMED AT THE NEXT DUE OF ANY APPLICABLE TASKS OF
SSI 572004 OR 572020 OR 572027 OR 572053. FROM THAT
TIME ONWARDS, APPLY THE INSPECTION INTERVAL OF THIS
TASK.
INTERVALS
SOURCE
ST:
30000 FC
OR
44900 FH
SI:
15000 FC
OR
22400 FH
MRB
T:
6 YE
I:
6 YE
MRB CPCP
T:
25000 FC
OR
44800 FH
I:
10600 FC
OR
20500 FH
ALI
T:
29800 FC
OR
59600 FH
I:
15000 FC
OR
30000 FH
ALI
TPS
REFERENCES
572000-200-024
NTM 57-20-47
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.30
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.10
0.10
ALL
1
1
0.60
0.60
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.60
0.60
1130 1200
1379 1578
1657 1767
SOURCE:
MRB 572047-01-4
574100-200-003
SOURCE:
MRB 572049-01-4
572000-200-034
SOURCE:
ALI 572050-01-1
ACCESS PANELS: 540AB, 540BB, 540CZ, 540DZ, 640AB, 640BB, 640CZ, 640DZ
572050-01-4
540
640
OUTER WING, DRY BAY AREA
DETAILED INSPECTION OF OUTER WING, DRY BAY AREA
NOTE:
- THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-4.
- IF AN A/C HAS ALREADY EXCEEDED THE INSPECTION
THRESHOLD OF THIS TASK, THE INSPECTION SHOULD BE
PERFORMED AT THE NEXT DUE OF ANY APPLICABLE TASKS OF
SSI 572004 OR 572020 OR 572027 OR 572053. FROM THAT
TIME ONWARDS, APPLY THE INSPECTION INTERVAL OF THIS
TASK.
AF
DET
572000-200-034
SOURCE:
ALI 572050-01-4
ACCESS PANELS: 540AB, 540BB, 540CZ, 540DZ, 640AB, 640BB, 640CZ, 640DZ
Sub 2 - Page 206 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572050-01-8
ZONE
540
640
DESCRIPTION
OUTER WING, DRY BAY AREA
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, DRY BAY AREA
NOTE:
- THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-8.
- IF AN A/C HAS ALREADY EXCEEDED THE INSPECTION
THRESHOLD OF THIS TASK, THE INSPECTION SHOULD BE
PERFORMED AT THE NEXT DUE OF ANY APPLICABLE TASKS OF
SSI 572004 OR 572020 OR 572027 OR 572053. FROM THAT
TIME ONWARDS, APPLY THE INSPECTION INTERVAL OF THIS
TASK.
INTERVALS
SOURCE
T:
25000 FC
OR
44800 FH
I:
11700 FC
OR
21100 FH
ALI
T:
25000 FC
OR
44800 FH
I:
10600 FC
OR
20500 FH
ALI
T:
29800 FC
OR
59600 FH
I:
15000 FC
OR
30000 FH
ALI
TPS
REFERENCES
572000-200-034
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.60
0.60
2151 2163
1
1
1.00
1.00
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
1.00
1.00
1130 1200
1379 1578
1657 1767
SOURCE:
ALI 572050-01-8
ACCESS PANELS: 540AB, 540BB, 540CZ, 540DZ, 640AB, 640BB, 640CZ, 640DZ
572050-02-1
521
621
OUTER WING, DRY BAY AREA
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER
WING, DRY BAY AREA
NOTE:
- THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-1.
- IF AN A/C HAS ALREADY EXCEEDED THE INSPECTION
THRESHOLD OF THIS TASK, THE INSPECTION SHOULD BE
PERFORMED AT THE NEXT DUE OF ANY APPLICABLE TASKS OF
SSI 572004 OR 572020 OR 572027 OR 572053. FROM THAT
TIME ONWARDS, APPLY THE INSPECTION INTERVAL OF THIS
TASK.
572050-02-4
521
621
ACCESS PANELS: 521AZ, 521BZ, 521EB, 621AZ, 621BZ, 621EB
OUTER WING, DRY BAY AREA
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER WING, DRY BAY
AREA
NOTE:
- THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-4.
- IF AN A/C HAS ALREADY EXCEEDED THE INSPECTION THRESHOLD OF THIS
TASK, THE INSPECTION SHOULD BE PERFORMED AT THE NEXT DUE OF ANY
APPLICABLE TASKS OF SSI 572004 OR 572020 OR 572027 OR 572053. FROM
THAT TIME ONWARDS, APPLY THE INSPECTION INTERVAL OF THIS TASK.
NDT
SDI
572000-220-011
NTM 57-20-50
SOURCE:
ALI 572050-02-1
572000-220-011
NTM 57-20-50
SOURCE:
ALI 572050-02-4
ACCESS PANELS: 521AZ, 521BZ, 521EB, 621AZ, 621BZ, 621EB
Sub 2 - Page 207 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572050-02-8
ZONE
521
621
DESCRIPTION
OUTER WING, DRY BAY AREA
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER
WING, DRY BAY AREA
NOTE:
- THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-8.
- IF AN A/C HAS ALREADY EXCEEDED THE INSPECTION
THRESHOLD OF THIS TASK, THE INSPECTION SHOULD BE
PERFORMED AT THE NEXT DUE OF ANY APPLICABLE TASKS OF
SSI 572004 OR 572020 OR 572027 OR 572053. FROM THAT
TIME ONWARDS, APPLY THE INSPECTION INTERVAL OF THIS
TASK.
572052-01-1
540
640
ACCESS PANELS: 521AZ, 521BZ, 521EB, 621AZ, 621BZ, 621EB
OUTER WING BOTTOM SKIN ROOT JOINT FTG
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN ROOT
JOINT FITTINGS ON STRINGER 8 AND STRINGER 11
ACCESS PANELS: 540AB, 540AZ, 540BZ, 640AB, 640AZ, 640BZ
572052-01-8
540
640
OUTER WING
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN ROOT JOINT FITTINGS
ON STRINGER 8 AND STRINGER 11
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
572052-01-1
ACCESS PANELS: 540AB, 540AZ, 540BZ, 640AB, 640AZ, 640BZ
AF
DET
INTERVALS
SOURCE
T:
25000 FC
OR
44800 FH
I:
11700 FC
OR
21100 FH
ALI
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
ST:
12 YE
OR
31500 FC
OR
53000 FH
SI:
12 YE
OR
31000 FC
OR
52500 FH
T:
24 YE
I:
12 YE
MRB CPCP
TPS
REFERENCES
572000-220-011
NTM 57-20-50
MEN
TASKM. APPLICABI
H.
LITY
1
1
1.00
1.00
2151 2163
1
1
0.10
0.10
1130 1200
1379 1578
1657 1767
1
1
0.10
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
ALI 572050-02-8
NO
572000-200-025
SOURCE:
MRB 572052-01-1
MRB CPCP
NO
572000-200-025
SOURCE:
MRB 572052-01-8
Sub 2 - Page 208 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572052-01-9
ZONE
540
640
DESCRIPTION
OUTER WING
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN ROOT
JOINT FITTINGS ON STRINGER 8 AND STRINGER 11
ACCESS PANELS: 540AB, 540AZ, 540BZ, 640AB, 640AZ, 640BZ
572053-01-2
540
640
OUTER WING BOTTOM SKIN STRINGERS
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN
STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING DRAIN
HOLES IN STRINGERS AND BUTT STRAP AT STRINGER 8 AND
STRINGER 11, EXCLUDING THE AREA INSIDE THE DRY BAY
ACCESS PANELS: 540AB, 540AZ, 540BB, 540BZ, 540CB, 640AB, 640AZ, 640BB,
640BZ, 640CB
572053-01-5
540
640
OUTER WING BOTTOM SKIN STRINGERS
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN
STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING DRAIN
HOLES IN STRINGERS AND BUTT STRAP AT STRINGER 8 AND
STRINGER 11, EXCLUDING THE AREA INSIDE THE DRY BAY
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS
ACCOMPLISHMENT OF TASK 572053-01-2
AF
DET
INTERVALS
ST:
12 YE
OR
30000 FC
OR
52100 FH
SI:
12 YE
OR
27000 FC
OR
46500 FH
T:
24 YE
I:
12 YE
ST:
30000 FC
OR
60000 FH
SI:
15000 FC
OR
30000 FH
T:
37300 FC
OR
74600 FH
I:
15000 FC
OR
30000 FH
T:
25000 FC
OR
44800 FH
I:
11800 FC
OR
21100 FH
SOURCE
MRB CPCP
TPS
NO
REFERENCES
572000-200-025
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.10
0.10
2151 2163
1
1
0.50
0.50
1130 1200
1379 1578
1657 1767
1
1
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
SOURCE:
MRB 572052-01-9
ALI
MRB
572000-200-026
SOURCE:
ALI 572053-01-2
MRB 572053-01-2
ALI
572000-200-026
SOURCE:
ALI 572053-01-5
ACCESS PANELS: 540AB, 540AZ, 540BB, 540BZ, 540CB, 640AB, 640AZ, 640BB,
640BZ, 640CB
Sub 2 - Page 209 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572054-01-1
ZONE
500
600
DESCRIPTION
OUTER WING BOTTOM SKIN PUMP APERTURES
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE AT
FUEL PUMP APERTURES BETWEEN RIB 1 AND RIB 2
PREPARATION: FUEL PUMP;
572054-01-6
500
600
OUTER WING BOTTOM SKIN PUMP APERTURES
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE AT
FUEL PUMP APERTURES BETWEEN RIB 1 AND RIB 2
PREPARATION: FUEL PUMP;
572054-02-1
500
600
OUTER WING BOTTOM SKIN PUMP APERTURES
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER SURFACE AT
HOLES ADJACENT TO FUEL PUMP APERTURES BETWEEN RIB 1 AND RIB 2
AF
DET
INTERVALS
ST:
12 YE
OR
30000 FC
OR
60000 FH
SI:
12 YE
OR
15000 FC
OR
30000 FH
T:
24 YE
OR
49700 FC
OR
99400 FH
I:
12 YE
OR
15000 FC
OR
30000 FH
ST:
12 YE
OR
44000 FC
OR
60000 FH
SI:
12 YE
OR
9600 FC
OR
17100 FH
T:
24 YE
I:
12 YE
T:
6 YE
I:
6 YE
SOURCE
ALI
MRB CPCP
TPS
NO
REFERENCES
572000-200-002
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.10
0.10
1130 1200
1379 1578
1657 1767
1
1
0.10
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
1
0.13
0.13
ALL
SOURCE:
ALI 572054-01-1
MRB 572054-01-1
MRB CPCP
NO
572000-200-002
SOURCE:
MRB 572054-01-6
MRB CPCP
572000-220-805
SOURCE:
MRB 572054-02-1
Sub 2 - Page 210 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572057-01-1
ZONE
471
481
DESCRIPTION
OUTER WING BOTTOM SKIN RIB BAY 7-8
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,
BOTTOM SKIN LOWER SURFACE, HOT FUEL RECIRCULATION
HOLE AT RIB BAY 7-8, BETWEEN STRINGER 4 AND STRINGER
5.
PREPARATION: PYLON FAIRINGS REMOVED;
572062-01-1
572063-01-1
571
574
671
674
500
600
OUTER WING FIXED TRAILING EDGE
AF
DET
DETAILED INSPECTION OF OUTER WING, FIXED TRAILING
EDGE, REAR SPAR AFT FACE, BETWEEN GEAR SUPPORT RIB 5
AND RIB 8
ACCESS PANELS: 574AB, 574BB, 674AB, 674BB
OUTER WING BOTTOM SKIN LWR SURFACE
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER
SURFACE, AREA COVERED BY FUEL PUMP WIRING HARNESS
FAIRINGS.
PREPARATION: FUEL PUMP FAIRINGS; WIRING HARNESS DISPLACED;
AF
DET
INTERVALS
SOURCE
ST:
48000 FC
OR
60000 FH
SI:
15000 FC
OR
24200 FH
MRB
T:
12 YE
I:
6 YE
MRB CPCP
ST:
6 YE
SI:
6 YE
T:
24 YE
I:
6 YE
MRB CPCP
TPS
REFERENCES
572000-200-027
NTM 57-20-57
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
1
1
1
0.10
0.10
0.10
0.10
ALL
1
1
0.10
0.10
ALL
SOURCE:
MRB 572057-01-1
572000-220-003
SOURCE:
MRB 572062-01-1
572000-200-031
SOURCE:
MRB 572063-01-1
Sub 2 - Page 211 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572101-01-1
ZONE
522
622
DESCRIPTION
OUTER WING FRT SPAR FWD FACE RIB 8-22
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, FRONT SPAR FORWARD FACE,
BETWEEN RIB 8 AND RIB 22, INCLUDING ALL CUTOUTS
ACCESS PANELS: 522AB, 522CB, 522EB, 522FB, 522HB, 522JB, 522KB, 522LB,
522NB, 522QB, 622AB, 622CB, 622EB, 622FB, 622HB, 622JB, 622KB, 622LB, 622NB,
622QB
572101-01-7
522
622
MAIN STRUCTURE
DETAILED INSPECTION OF OUTER WING, FRONT SPAR FORWARD FACE,
BETWEEN RIB 8 AND RIB 22, INCLUDING ALL CUTOUTS
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
572101-01-1.
ACCESS PANELS: 522AB, 522CB, 522EB, 522FB, 522HB, 522JB, 522KB, 522LB,
522NB, 522QB, 622AB, 622CB, 622EB, 622FB, 622HB, 622JB, 622KB, 622LB, 622NB,
622QB
AF
DET
INTERVALS
ST:
12 YE
OR
30000 FC
OR
60000 FH
SI:
12 YE
OR
15000 FC
OR
30000 FH
T:
24 YE
OR
43000 FC
OR
86000 FH
I:
12 YE
OR
15000 FC
OR
30000 FH
ST:
12 YE
SI:
12 YE
T:
24 YE
OR
33300 FC
OR
55100 FH
I:
12 YE
OR
11600 FC
OR
19100 FH
SOURCE
ALI
MRB CPCP
TPS
REFERENCES
572100-200-006
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.75
0.75
1130 1200
1379 1578
1657 1767
1
1
0.75
0.75
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
SOURCE:
ALI 572101-01-1
MRB 572101-01-1
ALI
MRB CPCP
572100-200-006
SOURCE:
ALI 572101-01-7
MRB 572101-01-7
Sub 2 - Page 212 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572106-01-1
ZONE
522
622
DESCRIPTION
OUTER WING FRT SPAR FWD FACE RIB 22-27
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, FRONT SPAR FORWARD
FACE, BETWEEN RIB 22 AND RIB 27, INCLUDING ALL
CUTOUTS
ACCESS PANELS: 522QB, 522SB, 522UB, 622QB, 622SB, 622UB
572106-01-5
522
622
OUTER WING FRT SPAR FWD FACE RIB 22-27
AF
DET
DETAILED INSPECTION OF OUTER WING, FRONT SPAR FORWARD
FACE, BETWEEN RIB 22 AND RIB 27, INCLUDING ALL
CUTOUTS
ACCESS PANELS: 522QB, 522SB, 522UB, 622QB, 622SB, 622UB
572106-01-6
522
622
OUTER WING FRT SPAR FWD FACE RIB 22-27
DETAILED INSPECTION OF OUTER WING, FRONT SPAR FORWARD
FACE, BETWEEN RIB 22 AND RIB 27, INCLUDING ALL
CUTOUTS
ACCESS PANELS: 522QB, 522SB, 522UB, 622QB, 622SB, 622UB
AF
DET
INTERVALS
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
ST:
12 YE
OR
30000 FC
OR
52500 FH
SI:
12 YE
OR
23500 FC
OR
32900 FH
T:
24 YE
I:
12 YE
ST:
12 YE
OR
41000 FC
OR
58000 FH
SI:
12 YE
OR
21100 FC
OR
29500 FH
T:
24 YE
I:
12 YE
SOURCE
MRB CPCP
TPS
REFERENCES
572100-200-007
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.30
0.30
1130 1200
1379 1578
1657 1767
1
1
0.30
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.30
0.30
2151 2163
SOURCE:
MRB 572106-01-1
MRB CPCP
572100-200-007
SOURCE:
MRB 572106-01-5
MRB CPCP
572100-200-007
SOURCE:
MRB 572106-01-6
Sub 2 - Page 213 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572108-01-2
ZONE
540
640
DESCRIPTION
OUTER WING FRT SPAR AFT FACE RIB 8-22
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT
FACE, BETWEEN RIB 8 AND RIB 22
ACCESS PANELS: 540CB, 540DB, 540EB, 540FB, 540GB, 540HB, 540JB, 540KB,
540LB, 540MB, 540NB, 540PB, 540QB, 540RB, 640CB, 640DB, 640EB, 640FB,
640GB, 640HB, 640JB, 640KB, 640LB, 640MB, 640NB, 640PB, 640QB, 640RB
572108-01-4
540
640
OUTER WING FRT SPAR AFT FACE RIB 8-22
AF
DET
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT
FACE, BETWEEN RIB 8 AND RIB 22
ACCESS PANELS: 540CB, 540DB, 540EB, 540FB, 540GB, 540HB, 540JB, 540KB,
540LB, 540MB, 540NB, 540PB, 540QB, 540RB, 640CB, 640DB, 640EB, 640FB,
640GB, 640HB, 640JB, 640KB, 640LB, 640MB, 640NB, 640PB, 640QB, 640RB
572108-01-5
540
640
OUTER WING FRT SPAR AFT FACE RIB 8-22
AF
DET
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT
FACE, BETWEEN RIB 8 AND RIB 22
ACCESS PANELS: 540CB, 540DB, 540EB, 540FB, 540GB, 540HB, 540JB, 540KB,
540LB, 540MB, 540NB, 540PB, 540QB, 540RB, 640CB, 640DB, 640EB, 640FB,
640GB, 640HB, 640JB, 640KB, 640LB, 640MB, 640NB, 640PB, 640QB, 640RB
572109-01-1
550
560
650
660
OUTER WING FRT SPAR AFT FACE RIB 22-27
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT FACE, BETWEEN
RIB 22 AND RIB 27
ACCESS PANELS: 550AB, 550BB, 550CB, 550DB, 650AB, 650BB, 650CB, 650DB,
560AB, 660AB
AF
DET
INTERVALS
SOURCE
ST:
30000 FC
OR
60000 FH
SI:
15000 FC
OR
30000 FH
T:
35700 FC
OR
71400 FH
I:
15000 FC
OR
30000 FH
T:
31000 FC
OR
51200 FH
I:
8800 FC
OR
14500 FH
ALI
MRB
T:
27100 FC
OR
44700 FH
I:
7800 FC
OR
13000 FH
ALI
ST:
39000 FC
OR
78000 FH
SI:
20000 FC
OR
40000 FH
MRB
TPS
REFERENCES
572100-200-008
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.50
0.50
1130 1200
1379 1578
1657 1767
1
1
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.50
0.50
2151 2163
1
1
1
1
0.20
0.20
0.20
0.20
1130 1200
1379 1578
1657 1767
SOURCE:
ALI 572108-01-2
MRB 572108-01-2
ALI
572100-200-008
SOURCE:
ALI 572108-01-4
572100-200-008
SOURCE:
ALI 572108-01-5
572100-200-009
SOURCE:
MRB 572109-01-1
Sub 2 - Page 214 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572109-01-4
ZONE
550
560
650
660
DESCRIPTION
MAIN STRUCTURE
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT FACE, BETWEEN
RIB 22 AND RIB 27
ACCESS PANELS: 550AB, 550BB, 550CB, 550DB, 560AB, 650AB, 650BB, 650CB,
650DB, 660AB
572111-01-1
574
575
674
675
OUTER WING REAR SPAR AFT FACE RIB 8-11
AF
DET
DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT
FACE, FROM RIB 8 TO RIB 11
ACCESS PANELS: 573CB, 573EB, 573FB, 575AB, 673CB, 673EB, 673FB, 675AB
572111-01-2
574
575
674
675
OUTER WING REAR SPAR AFT FACE RIB 8-11
AF
DET
DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT
FACE, FROM RIB 8 TO RIB 11
ACCESS PANELS: 573CB, 573EB, 573FB, 575AB, 673CB, 673EB, 673FB, 675AB
572111-01-6
574
575
674
675
OUTER WING REAR SPAR AFT FACE RIB 8-11
DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT FACE, FROM RIB 8
TO RIB 11
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
572111-01-1
ACCESS PANELS: 573CB, 573EB, 573FB, 575AB, 673CB, 673EB, 673FB, 675AB
AF
DET
INTERVALS
SOURCE
ST:
48000 FC
OR
60000 FH
SI:
20000 FC
OR
27900 FH
MRB
ST:
30000 FC
OR
60000 FH
SI:
15000 FC
OR
30000 FH
T:
12 YE
I:
6 YE
T:
12 YE
OR
21800 FC
OR
35800 FH
I:
6 YE
OR
11600 FC
OR
19000 FH
T:
12 YE
OR
21800 FC
OR
35800 FH
I:
6 YE
OR
11200 FC
OR
18400 FH
MRB CPCP
TPS
REFERENCES
572100-200-009
SOURCE:
MRB 572109-01-4
572100-200-002
SOURCE:
MRB 572111-01-1
ALI
MRB CPCP
572100-200-002
SOURCE:
ALI 572111-01-2
MRB 572111-01-2
ALI
MRB CPCP
572100-200-002
SOURCE:
ALI 572111-01-6
MRB 572111-01-6
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
0.20
0.20
0.20
0.20
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
1
1
1
0.10
0.10
0.10
0.10
1130 1200
1379 1578
1657 1767
1
1
1
1
0.10
0.10
0.10
0.10
0649 1761
1890
1
1
1
1
0.10
0.10
0.10
0.10
1488 1560
1743 1851
1863 1876
2151 2163
Sub 2 - Page 215 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572112-01-1
ZONE
575
675
DESCRIPTION
OUTER WING REAR SPAR AFT FACE RIB11-27
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT
FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT
PLATE AT RIB 22
ACCESS PANELS: 575BB, 575CB, 575DB, 575EB, 575FB, 575GB, 575HB, 575KB,
575LB, 575MB, 675BB, 675CB, 675DB, 675EB, 675FB, 675GB, 675HB, 675KB, 675LB,
675MB
572112-01-2
575
675
OUTER WING REAR SPAR AFT FACE RIB11-27
AF
DET
DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT
FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT
PLATE AT RIB 22
ACCESS PANELS: 575BB, 575CB, 575DB, 575EB, 575FB, 575GB, 575HB, 575JB,
575KB, 575LB, 575MB, 675BB, 675CB, 675DB, 675EB, 675FB, 675GB, 675HB, 675JB,
675KB, 675LB, 675MB
572112-01-6
575
675
OUTER WING REAR SPAR AFT FACE RIB11-27
AF
DET
DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT
FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT
PLATE AT RIB 22
ACCESS PANELS: 575BB, 575CB, 575DB, 575EB, 575FB, 575GB, 575HB, 575KB,
575LB, 575MB, 675BB, 675CB, 675DB, 675EB, 675FB, 675GB, 675HB, 675KB, 675LB,
675MB
572114-01-3
540
640
OUTER WING REAR SPAR FWD FACE RIB8-11
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD
FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND
BOTTOM FLANGES
ACCESS PANELS: 540CB, 540DB, 540EB, 640CB, 640DB, 640EB
AF
DET
INTERVALS
T:
12 YE
OR
21000 FC
OR
42000 FH
I:
6 YE
OR
15000 FC
OR
30000 FH
T:
12 YE
OR
22800 FC
OR
40300 FH
I:
6 YE
OR
12500 FC
OR
22100 FH
T:
12 YE
OR
21000 FC
OR
37200 FH
I:
6 YE
OR
11900 FC
OR
21000 FH
T:
30100 FC
OR
49400 FH
I:
9400 FC
OR
15300 FH
SOURCE
ALI
MRB CPCP
TPS
REFERENCES
572100-200-003
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.75
0.75
1130 1200
1379 1578
1657 1767
1
1
0.75
0.75
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.75
0.75
2151 2163
1
1
0.30
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
ALI 572112-01-1
MRB 572112-01-1
ALI
MRB CPCP
572100-200-003
SOURCE:
ALI 572112-01-2
MRB 572112-01-2
ALI
MRB CPCP
572100-200-003
SOURCE:
ALI 572112-01-6
MRB 572112-01-6
ALI
572100-200-010
SOURCE:
ALI 572114-01-3
Sub 2 - Page 216 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572114-01-4
ZONE
540
640
DESCRIPTION
OUTER WING REAR SPAR FWD FACE RIB8-11
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD
FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND
BOTTOM FLANGES
ACCESS PANELS: 540CB, 540DB, 540EB, 640CB, 640DB, 640EB
572114-01-6
540
640
OUTER WING REAR SPAR FWD FACE RIB8-11
AF
DET
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD
FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND
BOTTOM FLANGES
ACCESS PANELS: 540CB, 540DB, 540EB, 640CB, 640DB, 640EB
572115-01-1
572115-01-2
540
550
560
640
650
660
540
550
560
640
650
660
OUTER WING REAR SPAR FWD FACE RIB11-27
AF
DET
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD
FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT
RIB 22 AND TOP AND BOTTOM FLANGES
ACCESS PANELS: 540FB, 540GB, 540HB, 540JB, 540KB, 540LB, 540MB, 540NB,
540PB, 540QB, 540RB, 550AB, 550BB, 550CB, 550DB, 560AB, 640FB, 640GB,
640HB, 640JB, 640KB, 640LB, 640MB, 640NB, 640PB, 640QB, 640RB, 650AB,
650BB, 650CB, 650DB, 660AB
OUTER WING REAR SPAR FWD FACE RIB11-27
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD
FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT
RIB 22 AND TOP AND BOTTOM FLANGES
ACCESS PANELS: 540FB, 540GB, 540HB, 540JB, 540KB, 540LB, 540MB, 540NB,
540PB, 540QB, 540RB, 550AB, 550BB, 550CB, 550DB, 560AB, 640FB, 640GB,
640HB, 640JB, 640KB, 640LB, 640MB, 640NB, 640PB, 640QB, 640RB, 650AB,
650BB, 650CB, 650DB, 660AB
AF
DET
INTERVALS
SOURCE
T:
30100 FC
OR
60200 FH
I:
10100 FC
OR
20200 FH
T:
30100 FC
OR
49400 FH
I:
8500 FC
OR
13900 FH
ST:
30000 FC
OR
48900 FH
SI:
15500 FC
OR
25200 FH
ALI
ST:
30000 FC
OR
60000 FH
SI:
15000 FC
OR
30000 FH
T:
43200 FC
OR
86400 FH
I:
15000 FC
OR
30000 FH
ALI
MRB
TPS
REFERENCES
572100-200-010
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.30
0.30
1130 1200
1379 1578
1657 1767
1
1
0.30
0.30
2151 2163
1
1
1
1
1
1
0.11
0.11
0.11
0.11
0.11
0.11
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
1
1
1
1
0.11
0.11
0.11
0.11
0.11
0.11
1130 1200
1379 1578
1657 1767
SOURCE:
ALI 572114-01-4
ALI
572100-200-010
SOURCE:
ALI 572114-01-6
MRB
572100-200-011
SOURCE:
MRB 572115-01-1
572100-200-011
SOURCE:
ALI 572115-01-2
MRB 572115-01-2
Sub 2 - Page 217 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572115-01-6
572116-02-1
ZONE
540
550
560
640
650
660
500
600
DESCRIPTION
OUTER WING REAR SPAR FWD FACE RIB11-27
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD
FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT
RIB 22 AND TOP AND BOTTOM FLANGES
ACCESS PANELS: 540FB, 540GB, 540HB, 540JB, 540KB, 540LB, 540MB, 540NB,
540PB, 540QB, 540RB, 550AB, 550BB, 550CB, 550DB, 560AB, 640FB, 640GB,
640HB, 640JB, 640KB, 640LB, 640MB, 640NB, 640PB, 640QB, 640RB, 650AB,
650BB, 650CB, 650DB, 660AB
MAIN STRUCTURE
AF
DET
DETAILED INSPECTION OF OUTER WING, TOP SKIN, UPPER SURFACE AT
ATTACHMENT TO FRONT SPAR AND REAR SPAR BETWEEN RIB 8 AND RIB 22
572116-02-2
500
600
MAIN STRUCTURE
AF
DET
DETAILED INSPECTION OF OUTER WING, TOP SKIN, UPPER SURFACE AT
ATTACHMENT TO FRONT SPAR AND REAR SPAR BETWEEN RIB 8 AND RIB 22
572120-01-3
500
600
OUTER WING TOP SKIN
GENERAL VISUAL INSPECTION OF OUTER WING, TOP SKIN, UPPER SURFACE
AT ATTACHMENTS TO RIBS AND STRINGERS BETWEEN RIB 8 AND RIB 27 FROM
FRONT SPAR TO REAR SPAR
AF
GVI
INTERVALS
SOURCE
T:
24600 FC
OR
40100 FH
I:
15800 FC
OR
25700 FH
ALI
ST:
30000 FC
OR
60000 FH
SI:
15000 FC
OR
30000 FH
T:
58800 FC
OR
117600 FH
I:
15000 FC
OR
30000 FH
ST:
30000 FC
OR
53800 FH
SI:
15000 FC
OR
26900 FH
ALI
MRB
T:
51700 FC
OR
103400 FH
I:
15000 FC
OR
30000 FH
ALI
TPS
REFERENCES
572100-200-011
SOURCE:
ALI 572115-01-6
572100-220-801
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
1
1
0.11
0.11
0.11
0.11
0.11
0.11
2151 2163
1
1
0.60
0.60
1130 1200
1379 1578
1657 1767
1
1
0.60
0.60
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
1
0.40
0.40
1130 1200
1379 1578
1657 1767
SOURCE:
ALI 572116-02-1
MRB 572116-02-1
MRB
572100-220-801
SOURCE:
MRB 572116-02-2
572100-210-804
SOURCE:
ALI 572120-01-3
Sub 2 - Page 218 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572122-01-1
ZONE
500
600
DESCRIPTION
OUTER WING TOP SKIN RIB 19-20
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, TOP SKIN, UPPER
SURFACE AROUND MANUAL REFUELLING APERTURE, BETWEEN
RIB 19 AND RIB 20
PREPARATION: ADAPTOR RING;
572122-02-1
572123-01-1
500
600
540
640
OUTER WING TOP SKIN RIB 19-20
DETAILED INSPECTION OF OUTER WING TOP SKIN,
UPPER SURFACE AROUND MANUAL REFUELLING APERTURE
BETWEEN RIB 19 AND RIB 20
OUTER WING TOP SKIN STGR RIB 8-13
AF
AF
DET
DET
DETAILED INSPECTION OF OUTER WING, TOP SKIN, STRINGERS BETWEEN RIB
8 AND RIB 13, INCLUDING RUNOUTS AND AIR TRANSFER HOLES, STRINGERS
JOINT BETWEEN RIB 8 AND RIB 9 AND BUTT STRAP AT STRINGER 11
ACCESS PANELS: 540CB, 540DB, 540EB, 540FB, 540GB, 640CB, 640DB, 640EB,
640FB, 640GB
572123-01-3
540
640
OUTER WING TOP SKIN STGR RIB 8-13
DETAILED INSPECTION OF OUTER WING, TOP SKIN, STRINGERS BETWEEN RIB
8 AND RIB 13, INCLUDING RUNOUTS AND AIR TRANSFER HOLES, STRINGERS
JOINT BETWEEN RIB 8 AND RIB 9 AND BUTT STRAP AT STRINGER 11
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
572123-01-1
AF
DET
INTERVALS
SOURCE
ST:
48000 FC
OR
60000 FH
SI:
20000 FC
OR
32100 FH
MRB
T:
6 YE
I:
6 YE
MRB CPCP
ST:
30000 FC
OR
60000 FH
SI:
20000 FC
OR
40000 FH
T:
53200 FC
OR
106400 FH
I:
20000 FC
OR
40000 FH
ST:
30000 FC
OR
52500 FH
SI:
20000 FC
OR
29000 FH
ALI
MRB
TPS
REFERENCES
572100-200-001
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.10
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
1
0.10
0.10
ALL
2
2
2.00
2.00
1130 1200
1379 1578
1657 1767
2
2
2.00
2.00
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
SOURCE:
MRB 572122-01-1
572100-200-032
SOURCE:
MRB 572122-02-1
572100-200-012
SOURCE:
ALI 572123-01-1
MRB 572123-01-1
MRB
572100-200-012
SOURCE:
MRB 572123-01-3
ACCESS PANELS: 540CB, 540DB, 540EB, 540FB, 540GB, 640CB, 640DB, 640EB,
640FB, 640GB
Sub 2 - Page 219 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572124-01-3
ZONE
540
550
560
640
650
660
DESCRIPTION
OUTER WING TOP SKIN STGR RIB 13-27
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGERS, BETWEEN RIB
13 AND RIB 27, INCLUDING RUNOUTS, AIR TRANSFER HOLES AND BUTT STRAP
AT STRINGER 11, INCLUDING RUNOUT AT FRONT SPAR AT RIB 18
ACCESS PANELS: 540HB, 540JB, 540KB, 540LB, 540MB, 540NB, 540PB, 540QB,
540RB, 550AB, 550BB, 550CB, 550DB, 560AB, 640HB, 640JB, 640KB, 640LB, 640MB,
640NB, 640PB, 640QB, 640RB, 650AB, 650BB, 650CB, 650DB, 660AB
572124-01-4
540
550
560
640
650
660
OUTER WING TOP SKIN STGR RIB 13-27
DETAILED INSPECTION OF OUTER WING, TOP SKIN
STRINGERS, BETWEEN RIB 13 AND RIB 27, INCLUDING
RUNOUTS, AIR TRANSFER HOLES AND BUTT STRAP AT
STRINGER 11, INCLUDING RUNOUT AT FRONT SPAR AT RIB 18
ACCESS PANELS: 540HB, 540JB, 540KB, 540LB, 540MB, 540NB, 540PB, 540QB,
540RB, 550AB, 550BB, 550CB, 550DB, 560AB, 640HB, 640JB, 640KB, 640LB, 640MB,
640NB, 640PB, 640QB, 640RB, 650AB, 650BB, 650CB, 650DB, 660AB
AF
DET
INTERVALS
ST:
30000 FC
OR
60000 FH
SI:
17300 FC
OR
34600 FH
T:
53300 FC
OR
106600 FH
I:
17300 FC
OR
34600 FH
ST:
30000 FC
OR
52900 FH
SI:
17300 FC
OR
30500 FH
T:
44700 FC
OR
60000 FH
I:
17300 FC
OR
30500 FH
SOURCE
ALI
MRB
TPS
REFERENCES
572100-200-013
SOURCE:
ALI 572124-01-3
MRB 572124-01-3
ALI
MRB
572100-200-013
SOURCE:
ALI 572124-01-4
MRB 572124-01-4
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
1
1
0.67
0.67
0.67
0.67
0.67
0.67
1130 1200
1379 1578
1657 1767
1
1
1
1
1
1
0.67
0.67
0.67
0.67
0.67
0.67
0649 1488
1560 1743
1761 1851
1863 1876
1890
Sub 2 - Page 220 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572124-01-7
ZONE
540
550
560
640
650
660
DESCRIPTION
OUTER WING TOP SKIN STGR RIB 13-27
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, TOP SKIN
STRINGERS, BETWEEN RIB 13 AND RIB 27, INCLUDING
RUNOUTS, AIR TRANSFER HOLES AND BUTT STRAP AT
STRINGER 11, INCLUDING RUNOUT AT FRONT SPAR AT RIB 18
ACCESS PANELS: 540HB, 540JB, 540KB, 540LB, 540MB, 540NB, 540PB, 540QB,
540RB, 550AB, 550BB, 550CB, 550DB, 560AB, 640HB, 640JB, 640KB, 640LB, 640MB,
640NB, 640PB, 640QB, 640RB, 650AB, 650BB, 650CB, 650DB, 660AB
572125-01-1
575
675
TOP SKIN PANEL 2 OVERHANG BETWEEN RIB 22
AND RIB 27
NDT
SDI
AF
DET
SPECIAL DETAILED INSPECTION OF OUTER WING, TOP SKIN
PANEL 2 OVERHANG BETWEEN RIB 22 AND RIB 27
572126-01-1
540
550
560
640
650
660
NOTE : - FOR THRESHOLD REFER TO ISB 57-1154.
- REFER TO ISB 57-1154 FOR ALTERNATIVE TASK
TERMINATING THIS INSPECTION.
OUTER WING RIB9-27 AT SKIN ATTACHMENTS
DETAILED INSPECTION OF OUTER WING, RIB 9 TO RIB 27,
AT SKIN ATTACHMENTS, INCLUDING CLEATS, SPAR
ATTACHMENTS AND IN REGION OF STRINGER CUTOUTS
ACCESS PANELS: 540CB, 540DB, 540EB, 540FB, 540GB, 540HB, 540JB, 540KB,
540LB, 540MB, 540NB, 540PB, 540QB, 540RB, 650AB, 650BB, 650CB, 650DB,
560AB, 640CB, 640DB, 640EB, 640FB, 640GB, 640HB, 640JB, 640KB, 640LB, 640MB,
640NB, 640PB, 640QB, 640RB, 550AB, 550BB, 550CB, 550DB, 660AB
572126-01-3
540
550
560
640
650
660
OUTER WING RIB9-27 AT SKIN ATTACHMENTS
DETAILED INSPECTION OF OUTER WING, RIB 9 TO RIB 27, AT SKIN
ATTACHMENTS, INCLUDING CLEATS, SPAR ATTACHMENTS AND IN REGION OF
STRINGER CUTOUTS
ACCESS PANELS: 540CB, 540DB, 540EB, 540FB, 540GB, 540HB, 540JB, 540KB,
540LB, 540MB, 540NB, 540PB, 540QB, 540RB, 550AB, 550BB, 550CB, 550DB,
560AB, 640CB, 640DB, 640EB, 640FB, 640GB, 640HB, 640JB, 640KB, 640LB, 640MB,
640NB, 640PB, 640QB, 640RB, 650AB, 650BB, 650CB, 650DB, 660AB
AF
DET
INTERVALS
SOURCE
ST:
30000 FC
OR
52900 FH
SI:
17300 FC
OR
30500 FH
T:
43000 FC
OR
60000 FH
I:
17300 FC
OR
30500 FH
T:
NOTE
I:
40 MO
ALI
MRB
ISB
ST:
30000 FC
OR
60000 FH
SI:
20000 FC
OR
40000 FH
MRB
ST:
30000 FC
OR
52500 FH
SI:
20000 FC
OR
31900 FH
MRB
TPS
REFERENCES
572100-200-013
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
1
1
0.67
0.67
0.67
0.67
0.67
0.67
2151 2163
572100-270-001
ISB 57-1154
2
2
3.00
3.00
ALL
572100-200-014
1
1
1
1
1
1
0.53
0.53
0.53
0.53
0.53
0.53
1130 1200
1379 1578
1657 1767
1
1
1
1
1
1
0.53
0.53
0.53
0.53
0.53
0.53
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
SOURCE:
ALI 572124-01-7
MRB 572124-01-7
SOURCE:
MRB 572126-01-1
572100-200-014
SOURCE:
MRB 572126-01-3
Sub 2 - Page 221 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572127-01-1
ZONE
575
675
DESCRIPTION
TOP SKIN PANEL 2 OVERHANG BETWEEN RIB 4
AND RIB 22
SKILL TASK
CODE CODE
572129-01-1
500
600
500
600
OUTER WING BOTTOM SKIN ATTACH RIB 8-15
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT ATTACHMENTS TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 8 AND RIB 15, EXCLUDING AREAS COVERED BY
PYLON REINFORCING, PYLON FAIRING AND FLAP TRACK 3
FAIRING
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
SDI
T:
NOTE
I:
40 MO
ISB
572100-270-002
ISB 57-1155
2
2
8.00
8.00
ALL
AF
DET
T:
28900 FC
OR
50200 FH
I:
6300 FC
OR
10900 FH
ST:
30000 FC
OR
60000 FH
SI:
7300 FC
OR
14600 FH
T:
45700 FC
OR
91400 FH
I:
7300 FC
OR
14600 FH
ALI
572100-200-015
1
1
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.50
0.50
1130 1200
1379 1578
1657 1767
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT ATTACHMENTS TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 8 AND RIB 15, EXCLUDING AREAS COVERED BY
PYLON REINFORCING, PYLON FAIRING AND FLAP TRACK 3
FAIRING
572129-01-4
SOURCE
NDT
SPECIAL DETAILED INSPECTION OF OUTER WING, TOP SKIN
PANEL 2 OVERHANG BETWEEN RIB 4 AND RIB 22
NOTE : - FOR THRESHOLD REFER TO ISB 57-1155.
- REFER TO ISB 57-1155 FOR ALTERNATIVE TASK
TERMINATING THIS INSPECTION.
OUTER WING BOTTOM SKIN ATTACH RIB 8-15
INTERVALS
AF
DET
SOURCE:
ALI 572129-01-1
ALI
MRB
572100-200-015
SOURCE:
ALI 572129-01-4
MRB 572129-01-4
Sub 2 - Page 222 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572129-01-6
ZONE
500
600
DESCRIPTION
OUTER WING BOTTOM SKIN ATTACH RIB 8-15
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT ATTACHMENTS TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 8 AND RIB 15, EXCLUDING AREAS COVERED BY
PYLON REINFORCING, PYLON FAIRING AND FLAP TRACK 3
FAIRING
572130-01-2
500
600
OUTER WING BOTTOM SKIN ATTACH RIB15-22
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 15 AND RIB 22, EXCLUDING AREA COVERED BY
FLAP TRACK 4 FAIRING
572130-01-6
500
600
OUTER WING BOTTOM SKIN ATTACH RIB15-22
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 15 AND RIB 22, EXCLUDING AREA COVERED BY
FLAP TRACK 4 FAIRING
AF
DET
INTERVALS
SOURCE
ST:
30000 FC
OR
52100 FH
SI:
7300 FC
OR
12700 FH
T:
41400 FC
OR
60000 FH
I:
7300 FC
OR
12700 FH
ST:
31000 FC
OR
53900 FH
SI:
16200 FC
OR
28100 FH
ALI
MRB
ST:
30000 FC
OR
52100 FH
SI:
14100 FC
OR
24600 FH
T:
46000 FC
OR
60000 FH
I:
14100 FC
OR
24600 FH
ALI
MRB
TPS
REFERENCES
572100-200-015
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.50
0.50
2151 2163
1
1
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.50
0.50
2151 2163
SOURCE:
ALI 572129-01-6
MRB 572129-01-6
MRB
572100-200-016
SOURCE:
MRB 572130-01-2
572100-200-016
SOURCE:
ALI 572130-01-6
MRB 572130-01-6
Sub 2 - Page 223 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572130-01-7
ZONE
500
600
DESCRIPTION
OUTER WING BOTTOM SKIN ATTACH RIB15-22
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 15 AND RIB 22, EXCLUDING AREA COVERED BY
FLAP TRACK 4 FAIRING
572131-01-1
500
600
OUTER WING BOTTOM SKIN LWR SURFACE
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 22 AND RIB 27
572131-01-3
500
600
OUTER WING BOTTOM SKIN LWR SURFACE
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 22 AND RIB 27
AF
DET
INTERVALS
SOURCE
ST:
30000 FC
OR
60000 FH
SI:
14100 FC
OR
28200 FH
T:
46000 FC
OR
92000 FH
I:
14100 FC
OR
28200 FH
ST:
37000 FC
OR
60000 FH
SI:
16000 FC
OR
28000 FH
ALI
MRB
ST:
30000 FC
OR
52500 FH
SI:
13300 FC
OR
23100 FH
MRB
TPS
REFERENCES
572100-200-016
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.50
0.50
1130 1200
1379 1578
1657 1767
1
1
0.20
0.20
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.20
0.20
2151 2163
SOURCE:
ALI 572130-01-7
MRB 572130-01-7
MRB
572100-200-017
SOURCE:
MRB 572131-01-1
572100-200-017
SOURCE:
MRB 572131-01-3
Sub 2 - Page 224 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572134-01-2
ZONE
540
640
DESCRIPTION
OUTER WING BOTTOM SKIN TRACK 3 AND 4
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER
SURFACE IN AREAS OF FLAP TRACK 3 AND 4 FORWARD AND
AFT PICK UP FITTINGS, INCLUDING ATTACHMENT TO REAR
SPAR
ACCESS PANELS: 540FB, 540GB, 540NB, 540PB, 640FB, 640GB, 640NB, 640PB
572134-01-4
540
640
OUTER WING BOTTOM SKIN TRACK 3 AND 4
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER
SURFACE IN AREAS OF FLAP TRACK 3 AND 4 FORWARD AND
AFT PICK UP FITTINGS, INCLUDING ATTACHMENT TO REAR
SPAR
ACCESS PANELS: 540FB, 540GB, 540NB, 540PB, 640FB, 640GB, 640NB, 640PB
572134-01-7
540
640
OUTER WING BOTTOM SKIN TRACK 3 AND 4
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER
SURFACE IN AREAS OF FLAP TRACK 3 AND 4 FORWARD AND
AFT PICK UP FITTINGS, INCLUDING ATTACHMENT TO REAR
SPAR
ACCESS PANELS: 540FB, 540GB, 540NB, 540PB, 640FB, 640GB, 640NB, 640PB
AF
DET
INTERVALS
SOURCE
ST:
30000 FC
OR
60000 FH
SI:
8800 FC
OR
17600 FH
T:
53500 FC
OR
107000 FH
I:
8800 FC
OR
17600 FH
T:
32000 FC
OR
60000 FH
I:
10600 FC
OR
24200 FH
ALI
MRB
T:
29300 FC
OR
60000 FH
I:
7900 FC
OR
18100 FH
ALI
TPS
REFERENCES
572100-200-018
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
1130 1200
1379 1578
1657 1767
1
1
0.20
0.20
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.20
0.20
2151 2163
SOURCE:
ALI 572134-01-2
MRB 572134-01-2
ALI
572100-200-018
SOURCE:
ALI 572134-01-4
572100-200-018
SOURCE:
ALI 572134-01-7
Sub 2 - Page 225 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572137-01-2
ZONE
500
600
DESCRIPTION
OUTER WING BOTTOM SKIN RUNOUTS
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE AT
RUNOUT OF STRINGER 4 (RIB BAY 10-11), STRINGER 5 (RIB BAY 13-14),
STRINGER 13 (RIB BAY 8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIB BAY
19-20) AND STRINGER 12 (RIB BAY 17-18)
572137-01-4
500
600
OUTER WING BOTTOM SKIN RUNOUTS
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT RUNOUT OF STRINGER 4 (RIB BAY 10-11),
STRINGER 5 (RIB BAY 13-14), STRINGER 13 (RIB BAY
8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIB BAY
19-20) AND STRINGER 12 (RIB BAY 17-18)
572137-01-6
500
600
OUTER WING BOTTOM SKIN RUNOUTS
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT RUNOUT OF STRINGER 4 (RIB BAY 10-11),
STRINGER 5 (RIB BAY 13-14), STRINGER 13 (RIB BAY
8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIB BAY
19-20) AND STRINGER 12 (RIB BAY 17-18)
572139-01-2
500
540
600
640
OUTER WING BOTTOM SKIN RIB BAY CUTOUTS
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, UPPER
AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS IN RIB
BAYS 8-9, 9-10, 10-11, 11-12 AND 12-13
AF
DET
INTERVALS
ST:
30000 FC
OR
60000 FH
SI:
5500 FC
OR
11000 FH
T:
58200 FC
OR
116400 FH
I:
5500 FC
OR
11000 FH
T:
24000 FC
OR
42000 FH
I:
5000 FC
OR
8400 FH
T:
19700 FC
OR
33400 FH
I:
4700 FC
OR
7900 FH
T:
12 YE
I:
6 YE
SOURCE
TPS
ALI
MRB
REFERENCES
572100-200-019
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.12
0.12
1130 1200
1379 1578
1657 1767
1
1
0.12
0.12
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.12
0.12
2151 2163
1
1
1
1
0.13
0.13
0.13
0.13
ALL
SOURCE:
ALI 572137-01-2
MRB 572137-01-2
ALI
572100-200-019
SOURCE:
ALI 572137-01-4
ALI
572100-200-019
SOURCE:
ALI 572137-01-6
MRB CPCP
NO
572100-200-004
SOURCE:
MRB 572139-01-2
ACCESS PANELS: 540CB, 540DB, 540EB, 540FB, 540GB, 640CB, 640DB, 640EB,
640FB, 640GB
Sub 2 - Page 226 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572139-02-1
ZONE
500
540
600
640
DESCRIPTION
OUTER WING BOTTOM SKIN RIB BAY CUTOUTS
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,
BOTTOM SKIN, UPPER AND LOWER SURFACES AROUND ACCESS
DOOR CUTOUTS IN RIB BAYS 8-9, 9-10, 10-11, 11-12 AND
12-13.
ACCESS PANELS: 540CB, 540DB, 540EB, 540FB, 540GB, 640CB, 640DB, 640EB,
640FB, 640GB
572139-02-3
572139-02-5
500
540
600
640
500
540
600
640
OUTER WING BOTTOM SKIN RIB BAY CUTOUTS
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,
BOTTOM SKIN, UPPER AND LOWER SURFACES AROUND ACCESS
DOOR CUTOUTS IN RIB BAYS 8-9, 9-10, 10-11, 11-12 AND
12-13.
ACCESS PANELS: 540CB, 540DB, 540EB, 540FB, 540GB, 640CB, 640DB, 640EB,
640FB, 640GB
OUTER WING BOTTOM SKIN RIB BAY CUTOUTS
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,
BOTTOM SKIN, UPPER AND LOWER SURFACES AROUND ACCESS
DOOR CUTOUTS IN RIB BAYS 8-9, 9-10, 10-11, 11-12 AND
12-13
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS
ACCOMPLISHMENT OF TASK 572139-02-1
572140-01-2
500
540
550
560
600
640
650
660
ACCESS PANELS: 540CB, 540DB, 540EB, 540FB, 540GB, 640CB, 640DB, 640EB,
640FB, 640GB
OUTER WING BOTTOM SKIN CUTOUTS
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACES, AROUND ACCESS DOOR CUTOUTS IN ALL BAYS,
BETWEEN RIB 13 AND RIB 27
ACCESS PANELS: 540HB, 540JB, 540KB, 540LB, 540MB, 540NB, 540PB, 540QB,
540RB, 550AB, 550BB, 550CB, 550DB, 560AB, 640HB, 640JB, 640KB, 640LB, 640MB,
640NB, 640PB, 640QB, 640RB, 650AB, 650BB, 650CB, 650DB, 660AB
AF
DET
INTERVALS
SOURCE
ST:
30000 FC
OR
60000 FH
SI:
15000 FC
OR
30000 FH
T:
52800 FC
OR
105600 FH
I:
15000 FC
OR
30000 FH
ST:
30000 FC
OR
52100 FH
SI:
15000 FC
OR
26000 FH
ALI
MRB
ST:
30000 FC
OR
52100 FH
SI:
15000 FC
OR
26000 FH
MRB
T:
12 YE
I:
7.5 YE
MRB CPCP
TPS
REFERENCES
572100-200-020
NTM 57-21-39
SOURCE:
ALI 572139-02-1
MRB 572139-02-1
MRB
572100-200-020
NTM 57-21-39
SOURCE:
MRB 572139-02-3
572100-200-020
NTM 57-21-39
SOURCE:
MRB 572139-02-5
572100-200-021
SOURCE:
MRB 572140-01-2
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
0.30
0.30
0.30
0.30
1130 1200
1379 1578
1657 1767
1
1
1
1
0.30
0.30
0.30
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
1
1
0.30
0.30
0.30
0.30
2151 2163
1
1
1
1
1
1
1
1
0.10
0.10
0.10
0.10
0.10
0.10
0.10
0.10
ALL
Sub 2 - Page 227 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572140-02-4
572140-02-5
572142-01-2
ZONE
500
540
550
560
600
640
650
660
500
540
550
560
600
640
650
660
500
600
DESCRIPTION
OUTER WING BOTTOM SKIN CUTOUTS
SKILL TASK
CODE CODE
AF
GVI
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN
LOWER SURFACES, AROUND ACCESS DOOR CUTOUTS IN ALL
BAYS, BETWEEN RIB 13 AND RIB 27
OUTER WING BOTTOM SKIN CUTOUTS
AF
GVI
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN
LOWER SURFACES, AROUND ACCESS DOOR CUTOUTS IN ALL
BAYS, BETWEEN RIB 13 AND RIB 27
OUTER WING BOTTOM SKIN CUTOUTS
AF
GVI
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN
LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS,
BETWEEN RIB 8 AND RIB 15, FROM FRONT SPAR TO REAR
SPAR, EXCLUDING AREAS COVERED BY PYLON FAIRING AND
FLAP TRACK 3 FAIRING
572142-01-3
500
600
OUTER WING BOTTOM SKIN CUTOUTS
AF
GVI
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN
LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS,
BETWEEN RIB 8 AND RIB 15, FROM FRONT SPAR TO REAR
SPAR, EXCLUDING AREAS COVERED BY PYLON FAIRING AND
FLAP TRACK 3 FAIRING
572142-01-7
500
600
OUTER WING BOTTOM SKIN CUTOUTS
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN
LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS,
BETWEEN RIB 8 AND RIB 15, FROM FRONT SPAR TO REAR
SPAR, EXCLUDING AREAS COVERED BY PYLON FAIRING AND
FLAP TRACK 3 FAIRING
AF
GVI
INTERVALS
T:
42900 FC
OR
85800 FH
I:
3300 FC
OR
6600 FH
T:
34200 FC
OR
60000 FH
I:
3200 FC
OR
5700 FH
T:
48300 FC
OR
96600 FH
I:
5600 FC
OR
11200 FH
T:
24000 FC
OR
42000 FH
I:
4000 FC
OR
6800 FH
T:
24000 FC
OR
42000 FH
I:
3800 FC
OR
6400 FH
SOURCE
ALI
TPS
REFERENCES
572100-210-001
SOURCE:
ALI 572140-02-4
ALI
572100-210-001
SOURCE:
ALI 572140-02-5
ALI
572100-210-002
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
0.10
0.10
0.10
0.10
0.10
0.10
0.10
0.10
0.50
0.50
0.50
0.50
0.50
0.50
0.50
0.50
0.12
0.12
1130 1200
1379 1578
1657 1767
1
1
0.12
0.12
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.12
0.12
2151 2163
SOURCE:
ALI 572142-01-2
ALI
572100-210-002
SOURCE:
ALI 572142-01-3
ALI
572100-210-002
2151 2163
1130 1200
1379 1578
1657 1767
SOURCE:
ALI 572142-01-7
Sub 2 - Page 228 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572143-01-2
ZONE
532
533
632
633
DESCRIPTION
OUTER WING BOTTOM SKIN RIB/STGR ATTACH
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT ATTACHMENT TO RIBS AND STRINGERS IN AREA
COVERED BY FLAP TRACK 3 FAIRING AND FLAP TRACK 4
FAIRING.
ACCESS PANELS: 532AB, 532BB, 532CB, 532DB, 533AB, 533BB, 533CB, 533DB,
632AB, 632BB, 632CB, 632DB, 633AB, 633BB, 633CB, 633DB
572143-01-5
532
533
632
633
OUTER WING BOTTOM SKIN RIB/STGR ATTACH
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE AT
ATTACHMENT TO RIBS AND STRINGERS IN AREA COVERED BY FLAP TRACK 3
FAIRING AND FLAP TRACK 4 FAIRING
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
572143-01-2
572144-01-5
500
600
ACCESS PANELS: 532AB, 532BB, 532CB, 532DB, 533AB, 533BB, 533CB, 533DB,
632AB, 632BB, 632CB, 632DB, 633AB, 633BB, 633CB, 633DB
OUTER WING BOTTOM SKIN
AF
GVI
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT ATTACHMENT TO RIBS AND STRINGERS BETWEEN RIB 15 AND
RIB 27 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREA COVERED BY
FLAP TRACK 4 FAIRING.
572148-01-2
500
600
OUTER WING BOTTOM SKIN RIB/STGR ATTACH
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN
LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 8 AND RIB 18, EXCLUDING
AREAS COVERED BY PYLON FAIRING AND BY FLAP TRACK 3
FAIRING
AF
GVI
INTERVALS
SOURCE
ST:
30000 FC
OR
60000 FH
SI:
10900 FC
OR
21800 FH
T:
53500 FC
OR
107000 FH
I:
10900 FC
OR
21800 FH
T:
31700 FC
OR
54000 FH
I:
9400 FC
OR
16000 FH
ALI
MRB
T:
50800 FC
OR
101600 FH
I:
6700 FC
OR
13400 FH
T:
48300 FC
OR
96600 FH
I:
6000 FC
OR
12000 FH
ALI
TPS
REFERENCES
572100-200-022
SOURCE:
ALI 572143-01-2
MRB 572143-01-2
ALI
572100-200-022
SOURCE:
ALI 572143-01-5
572100-210-803
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
0.10
0.10
0.10
0.10
1130 1200
1379 1578
1657 1767
1
1
1
1
0.10
0.10
0.10
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
1
0.32
0.32
1130 1200
1379 1578
1657 1767
1
1
0.15
0.15
1130 1200
1379 1578
1657 1767
SOURCE:
ALI 572144-01-5
ALI
572100-210-003
SOURCE:
ALI 572148-01-2
Sub 2 - Page 229 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572148-01-3
ZONE
500
600
DESCRIPTION
OUTER WING BOTTOM SKIN RIB/STGR ATTACH
SKILL TASK
CODE CODE
AF
GVI
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN
LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 8 AND RIB 18, EXCLUDING
AREAS COVERED BY PYLON FAIRING AND BY FLAP TRACK 3
FAIRING
572148-01-9
500
600
OUTER WING BOTTOM SKIN RIB/STGR ATTACH
AF
GVI
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN
LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 8 AND RIB 18, EXCLUDING
AREAS COVERED BY PYLON FAIRING AND BY FLAP TRACK 3
FAIRING
572149-01-2
500
600
OUTER WING BOTTOM SKIN RIB/STGR ATTACH
AF
GVI
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN
LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 18 AND RIB 21, ADJACENT TO
FRONT SPAR AND REAR SPAR, EXCLUDING AREA COVERED BY
FLAP TRACK 4 FAIRING
572149-01-3
500
600
OUTER WING BOTTOM SKIN RIB/STGR ATTACH
AF
GVI
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN
LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 18 AND RIB 21, ADJACENT TO
FRONT SPAR AND REAR SPAR, EXCLUDING AREA COVERED BY
FLAP TRACK 4 FAIRING
572149-01-8
500
600
OUTER WING BOTTOM SKIN RIB/STGR ATTACH
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN
LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 18 AND RIB 21, ADJACENT TO
FRONT SPAR AND REAR SPAR, EXCLUDING AREA COVERED BY
FLAP TRACK 4 FAIRING
AF
GVI
INTERVALS
T:
24000 FC
OR
40400 FH
I:
3800 FC
OR
6100 FH
T:
21700 FC
OR
35300 FH
I:
3800 FC
OR
6100 FH
T:
56500 FC
OR
113000 FH
I:
6000 FC
OR
12000 FH
T:
25800 FC
OR
42000 FH
I:
5100 FC
OR
8300 FH
T:
22600 FC
OR
36700 FH
I:
5100 FC
OR
8300 FH
SOURCE
ALI
TPS
REFERENCES
572100-210-003
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.15
0.15
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.15
0.15
2151 2163
1
1
0.10
0.10
1130 1200
1379 1578
1657 1767
1
1
0.10
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.10
0.10
2151 2163
SOURCE:
ALI 572148-01-3
ALI
572100-210-003
SOURCE:
ALI 572148-01-9
ALI
572100-210-004
SOURCE:
ALI 572149-01-2
ALI
572100-210-004
SOURCE:
ALI 572149-01-3
ALI
572100-210-004
SOURCE:
ALI 572149-01-8
Sub 2 - Page 230 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572150-01-2
ZONE
532
632
DESCRIPTION
OUTER WING BOTTOM SKIN JOINTS RIB11-13
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 11 AND RIB 13 IN AREAS
COVERED BY FLAP TRACK 3 FAIRING
ACCESS PANELS: 532AB, 532BB, 532CB, 532DB, 632AB, 632BB, 632CB, 632DB
572150-01-3
532
632
OUTER WING BOTTOM SKIN JOINTS RIB11-13
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 11 AND RIB 13 IN AREAS
COVERED BY FLAP TRACK 3 FAIRING
ACCESS PANELS: 532AB, 532BB, 532CB, 532DB, 632AB, 632BB, 632CB, 632DB
572150-01-7
532
632
OUTER WING BOTTOM SKIN JOINTS RIB11-13
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 11 AND RIB 13 IN AREAS
COVERED BY FLAP TRACK 3 FAIRING
ACCESS PANELS: 532AB, 532BB, 532CB, 532DB, 632AB, 632BB, 632CB, 632DB
AF
DET
INTERVALS
SOURCE
ST:
30000 FC
OR
60000 FH
SI:
7800 FC
OR
15600 FH
T:
53500 FC
OR
107000 FH
I:
7800 FC
OR
15600 FH
T:
24000 FC
OR
42000 FH
I:
9400 FC
OR
16000 FH
ALI
MRB
T:
24000 FC
OR
42000 FH
I:
9400 FC
OR
16000 FH
ALI
TPS
REFERENCES
572100-200-023
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.10
0.10
1130 1200
1379 1578
1657 1767
1
1
0.10
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.10
0.10
2151 2163
SOURCE:
ALI 572150-01-2
MRB 572150-01-2
ALI
572100-200-023
SOURCE:
ALI 572150-01-3
572100-200-023
SOURCE:
ALI 572150-01-7
Sub 2 - Page 231 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572151-01-2
ZONE
533
633
DESCRIPTION
OUTER WING BOTTOM SKIN JOINTS RIB18-20
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 18 AND RIB 20 IN AREA
COVERED BY FLAP TRACK 4 FAIRING
ACCESS PANELS: 533AB, 533BB, 533CB, 533DB, 633AB, 633BB, 633CB, 633DB
572151-01-5
533
633
OUTER WING BOTTOM SKIN JOINTS RIB18-20
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 18 AND RIB 20 IN AREA
COVERED BY FLAP TRACK 4 FAIRING
NOTE: CREDIT CAN BR TAKEN FROM PREVIOUS
ACCOMPLISHMENT OF TASK 572151-01-2
INTERVALS
SOURCE
ST:
30000 FC
OR
60000 FH
SI:
10900 FC
OR
21800 FH
T:
56500 FC
OR
113000 FH
I:
10900 FC
OR
21800 FH
ST:
30000 FC
OR
48700 FH
SI:
10900 FC
OR
17700 FH
ALI
MRB
ST:
30000 FC
OR
48700 FH
SI:
10900 FC
OR
17700 FH
MRB
T:
6 YE
I:
6 YE
MRB CPCP
TPS
REFERENCES
572100-200-024
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.10
0.10
1130 1200
1379 1578
1657 1767
1
1
0.10
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.10
0.10
2151 2163
1
1
0.12
0.12
ALL
SOURCE:
ALI 572151-01-2
MRB 572151-01-2
MRB
572100-200-024
SOURCE:
MRB 572151-01-5
ACCESS PANELS: 533AB, 533BB, 533CB, 533DB, 633AB, 633BB, 633CB, 633DB
572151-01-7
533
633
OUTER WING BOTTOM SKIN JOINTS RIB18-20
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 18 AND RIB 20 IN AREA
COVERED BY FLAP TRACK 4 FAIRING
ACCESS PANELS: 533AB, 533DB, 633AB, 633DB
572153-01-1
500
600
OUTER WING BOTTOM SKIN DRAIN HOLES
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE, AT
DRAIN HOLES FOR SLAT CANS 5,6,7,8,9,10,11 AND 12 (RIB BAYS 9-10, 11-12, 1314, 16-17, 18-19, 21-22, 23-24 & 25-26) DRY BAY DRAIN HOLES IN RIB BAY
26-27 AND MAGNETIC LEVEL INDICATOR POSITIONS ADJACENT TO RIB 9 AND
RIB 12
AF
DET
572100-200-024
SOURCE:
MRB 572151-01-7
572100-200-025
SOURCE:
MRB 572153-01-1
Sub 2 - Page 232 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572153-01-2
ZONE
500
600
DESCRIPTION
OUTER WING BOTTOM SKIN DRAIN HOLES
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE, AT
DRAIN HOLES FOR SLAT CANS 5,6,7,8,9,10,11 AND 12 (RIB BAYS 9-10, 11-12, 1314, 16-17, 18-19, 21-22, 23-24 & 25-26) DRY BAY DRAIN HOLES IN RIB BAY 26-27
AND MAGNETIC LEVEL INDICATOR POSITIONS ADJACENT TO RIB 9 AND RIB 12
572153-01-3
500
600
OUTER WING BOTTOM SKIN DRAIN HOLES
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE, AT
DRAIN HOLES FOR SLAT CANS 5,6,7,8,9,10,11 AND 12 (RIB BAYS 9-10, 11-12, 1314, 16-17, 18-19, 21-22, 23-24 & 25-26) DRY BAY DRAIN HOLES IN RIB BAY 26-27
AND MAGNETIC LEVEL INDICATOR POSITIONS ADJACENT TO RIB 9 AND RIB 12
572155-01-1
540
640
OUTER WING BOTTOM SKIN RIB 8-21
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER
SURFACE BUTT STRAPS AT STRINGER 8 AND STRINGER 11,
BETWEEN RIB 8 AND RIB 21
ACCESS PANELS: 540CB, 540DB, 540EB, 540FB, 540GB, 540HB, 540JB, 540KB,
540LB, 540MB, 540NB, 540PB, 540QB, 640CB, 640DB, 640EB, 640FB, 640GB,
640HB, 640JB, 640KB, 640LB, 640MB, 640NB, 640PB, 640QB
572155-01-7
540
640
OUTER WING BOTTOM SKIN RIB 8-21
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER
SURFACE BUTT STRAPS AT STRINGER 8 AND STRINGER 11,
BETWEEN RIB 8 AND RIB 21
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS
ACCOMPLISHMENT OF TASK 572155-01-1
AF
DET
INTERVALS
SOURCE
ST:
34500 FC
OR
69000 FH
SI:
10500 FC
OR
21000 FH
MRB
ST:
41800 FC
OR
60000 FH
SI:
12700 FC
OR
21200 FH
MRB
ST:
30000 FC
OR
60000 FH
SI:
15000 FC
OR
30000 FH
T:
48300 FC
OR
96600 FH
I:
15000 FC
OR
30000 FH
T:
28700 FC
OR
54600 FH
I:
11200 FC
OR
21300 FH
ALI
MRB
TPS
REFERENCES
572100-200-025
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.12
0.12
1130 1200
1379 1578
1657 1767
1
1
0.12
0.12
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
1.00
1.00
1130 1200
1379 1578
1657 1767
1
1
1.00
1.00
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
SOURCE:
MRB 572153-01-2
572100-200-025
SOURCE:
MRB 572153-01-3
572100-200-026
SOURCE:
ALI 572155-01-1
MRB 572155-01-1
ALI
572100-200-026
SOURCE:
ALI 572155-01-7
ACCESS PANELS: 540CB, 540DB, 540EB, 540FB, 540GB, 540HB, 540JB, 540KB,
540LB, 540MB, 540NB, 540PB, 540QB, 640CB, 640DB, 640EB, 640FB, 640GB,
640HB, 640JB, 640KB, 640LB, 640MB, 640NB, 640PB, 640QB
Sub 2 - Page 233 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572157-01-1
ZONE
500
600
DESCRIPTION
OUTER WING BOTTOM SKIN RUNOUT
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (X-RAY) OF OUTER WING,
BOTTOM SKIN, RUNOUT OF BUTTSTRAP AT STRINGER 8,
BETWEEN RIB 20 AND RIB 21, ADJACENT TO FRONT SPAR AND
RUNOUT OF BUTTSTRAP AT STRINGER 11 ADJACENT TO RIB 21
AT REAR SPAR.
572157-01-5
500
600
ACCESS PANELS: 540PB, 540QB, 540RB, 640PB, 640QB, 640RB
OUTER WING BOTTOM SKIN RUNOUT
NDT
SDI
SPECIAL DETAILED INSPECTION (X-RAY) OF OUTER WING, BOTTOM SKIN,
RUNOUT OF BUTTSTRAP AT STRINGER 8, BETWEEN RIB 20 AND RIB 21,
ADJACENT TO FRONT SPAR AND RUNOUT OF BUTTSTRAP, AT STRINGER 11,
ADJACENT TO RIB 21 AT REAR SPAR
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
572157-01-1
572158-01-2
540
640
ACCESS PANELS: 540PB, 540QB, 540RB, 640PB, 640QB, 640RB
OUTER WING BOTTOM SKIN STGR RIB 8-18
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN STRINGERS
(INCLUDING DRAIN HOLES), BETWEEN RIB 8 AND RIB 18, COMPRISING
STRINGERS 4,5,6,7,8,11,12 AND 13
ACCESS PANELS: 540CB, 540DB, 540EB, 540FB, 540GB, 540HB, 540JB, 540KB,
540LB, 540MB, 640CB, 640DB, 640EB, 640FB, 640GB, 640HB, 640JB, 640KB, 640LB,
640MB
572158-01-5
540
640
OUTER WING BOTTOM SKIN STGR RIB 8-18
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN STRINGERS
(INCLUDING DRAIN HOLES), BETWEEN RIB 8 AND RIB 18, COMPRISING
STRINGERS 4,5,6,7,8,11,12 AND 13
ACCESS PANELS: 540CB, 540DB, 540EB, 540FB, 540GB, 540HB, 540JB, 540KB,
540LB, 540MB, 640CB, 640DB, 640EB, 640FB, 640GB, 640HB, 640JB, 640KB, 640LB,
640MB
AF
DET
INTERVALS
SOURCE
ST:
34000 FC
OR
68000 FH
SI:
20000 FC
OR
40000 FH
MRB
ST:
30000 FC
OR
52500 FH
SI:
20000 FC
OR
33200 FH
MRB
ST:
30000 FC
OR
60000 FH
SI:
15000 FC
OR
30000 FH
T:
48300 FC
OR
96600 FH
I:
15000 FC
OR
30000 FH
T:
29900 FC
OR
60000 FH
I:
11400 FC
OR
23000 FH
ALI
MRB
TPS
REFERENCES
572100-200-027
NTM 57-21-57
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.50
0.50
1130 1200
1379 1578
1657 1767
1
1
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
1
1.00
1.00
1130 1200
1379 1578
1657 1767
1
1
1.00
1.00
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
MRB 572157-01-1
572100-200-027
NTM 57-21-57
SOURCE:
MRB 572157-01-5
572100-200-028
SOURCE:
ALI 572158-01-2
MRB 572158-01-2
ALI
572100-200-028
SOURCE:
ALI 572158-01-5
Sub 2 - Page 234 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572158-01-9
ZONE
540
640
DESCRIPTION
OUTER WING BOTTOM SKIN STGR RIB 8-18
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN
STRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8 AND
RIB 18, COMPRISING STRINGERS 4,5,6,7,8,11,12 AND 13
572160-01-2
540
550
560
640
650
660
ACCESS PANELS: 540CB, 540DB, 540EB, 540FB, 540GB, 540HB, 540JB, 540KB,
540LB, 540MB, 640CB, 640DB, 640EB, 640FB, 640GB, 640HB, 640JB, 640KB, 640LB,
640MB
OUTER WING BOTTOM SKIN STGR RIB 18-27
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN
STRINGERS, BETWEEN RIB 18 AND RIB 27, COMPRISING
STRINGERS 7, 8 AND 11
ACCESS PANELS: 540NB, 540PB, 540QB, 540RB, 550AB, 550BB, 550CB, 550DB,
560AB, 640NB, 640PB, 640QB, 640RB, 650AB, 650BB, 650CB, 650DB, 660AB
572160-01-5
540
550
560
640
650
660
OUTER WING BOTTOM SKIN STGR RIB 18-27
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN
STRINGERS, BETWEEN RIB 18 AND RIB 27, COMPRISING
STRINGERS 7, 8 AND 11
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS
ACCOMPLISHMENT OF TASK 572160-01-2
INTERVALS
SOURCE
T:
28000 FC
OR
56500 FH
I:
11400 FC
OR
23000 FH
ALI
ST:
34000 FC
OR
68000 FH
SI:
15500 FC
OR
31000 FH
MRB
T:
34000 FC
OR
58700 FH
I:
15500 FC
OR
26800 FH
ALI
T:
12 YE
I:
12 YE
MRB CPCP
TPS
REFERENCES
572100-200-028
MEN
TASKM. APPLICABI
H.
LITY
1
1
1.00
1.00
2151 2163
1
1
1
1
1
1
0.67
0.67
0.67
0.67
0.67
0.67
1130 1200
1379 1578
1657 1767
1
1
1
1
1
1
0.67
0.67
0.67
0.67
0.67
0.67
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
1
1
1
1
1
0.10
0.10
0.10
0.10
0.10
0.10
1130 1200
1379 1578
1657 1767
SOURCE:
ALI 572158-01-9
572100-200-029
SOURCE:
MRB 572160-01-2
572100-200-029
SOURCE:
ALI 572160-01-5
ACCESS PANELS: 540NB, 540PB, 540QB, 540RB, 550AB, 550BB, 550CB, 550DB,
560AB, 640NB, 640PB, 640QB, 640RB, 650AB, 650BB, 650CB, 650DB, 660AB
572161-01-11
540
550
560
640
650
660
MAIN STRUCTURE
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, ACCESS DOORS
BETWEEN RIB 13 AND RIB 27
ACCESS PANELS: 540HB, 540JB, 540KB, 540LB, 540MB, 540NB, 540PB, 540QB,
540RB, 550AB, 550BB, 550CB, 550DB, 560AB, 640HB, 640JB, 640KB, 640LB, 640MB,
640NB, 640PB, 640QB, 640RB, 650AB, 650BB, 650CB, 650DB, 660AB
AF
DET
NO
572100-200-030
SOURCE:
MRB 572161-01-11
Sub 2 - Page 235 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572161-01-5
572164-01-1
572164-02-6
ZONE
DESCRIPTION
540
550
560
640
650
660
OUTER WING BOTTOM SKIN ACCESS DOORS
500
600
OUTER WING BOTTOM SKIN FUEL DRAIN
500
600
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN ACCESS DOORS,
BETWEEN RIB 13 AND RIB 27
ACCESS PANELS: 540HB, 540JB, 540KB, 540LB, 540MB, 540NB, 540PB, 540QB,
540RB, 550AB, 550BB, 550CB, 550DB, 560AB, 640HB, 640JB, 640KB, 640LB, 640MB,
640NB, 640PB, 640QB, 640RB, 650AB, 650BB, 650CB, 650DB, 660AB
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE AT
FUEL TANK WATER DRAIN HOLES BETWEEN RIB 15-16 AND RIB 22-23.
OUTER WING BOTTOM SKIN FUEL DRAIN
AF
AF
DET
GVI
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN
LOWER SURFACE AT FUEL TANK WATER DRAIN HOLES
BETWEEN RIB 15-16 AND RIB 22-23
572601-01-1
531
532
533
631
632
633
FLAP TRACK BEAMS UPR FLANGE RADII
AF
DET
DETAILED INSPECTION OF OUTER WING, FLAP TRACK BEAMS
2,3,4 TRACK UPPER FLANGE RADII
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572601-02-1
INTERVALS
SOURCE
ST:
48000 FC
OR
60000 FH
SI:
11800 FC
OR
20200 FH
T:
12 YE
I:
12 YE
T:
6 YE
I:
6 YE
T:
48000 FC
OR
96000 FH
I:
8300 FC
OR
16600 FH
ST:
48000 FC
SI:
7500 FC
MRB CPCP
ST:
48000 FC
SI:
4500 FC
MRB
TPS
NO
REFERENCES
572100-200-030
SOURCE:
MRB 572161-01-5
MRB CPCP
574100-200-005
ALI
SOURCE:
MRB 572164-01-1
572100-210-802
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
1
1
0.10
0.10
0.10
0.10
0.10
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
1
0.17
0.17
ALL
1
1
0.10
0.10
1130 1200
1379 1578
1657 1767
1
1
1
1
1
1
0.10
0.10
0.10
0.10
0.10
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
1
1
1
1
0.10
0.10
0.10
0.10
0.10
0.10
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
ALI 572164-02-6
MRB
572600-200-004
SOURCE:
MRB 572601-01-1
PREPARATION: FLAPS EXTENDED;
ACCESS PANELS: 531AB, 531BB, 531CB, 532AB, 532BB, 532CB, 533AB, 533BB,
533CB, 631AB, 631BB, 631CB, 632AB, 632BB, 632CB, 633AB, 633BB, 633CB
572601-01-3
531
532
533
631
632
633
FLAP TRACK BEAMS UPR FLANGE RADII
DETAILED INSPECTION OF OUTER WING, FLAP TRACK BEAMS
2,3,4 TRACK UPPER FLANGE RADII
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572601-02-3
AF
DET
572600-200-004
SOURCE:
MRB 572601-01-3
PREPARATION: FLAPS EXTENDED;
ACCESS PANELS: 531AB, 531BB, 531CB, 532AB, 532BB, 532CB, 533AB, 533BB,
533CB, 631AB, 631BB, 631CB, 632AB, 632BB, 632CB, 633AB, 633BB, 633CB
Sub 2 - Page 236 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572601-02-1
ZONE
531
532
533
631
632
633
DESCRIPTION
FLAP TRACK BEAMS UPR FLANGE RADII
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,
FLAP TRACK BEAMS 2,3,4 TRACK UPPER FLANGE RADII
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572601-01-1
INTERVALS
SOURCE
ST:
48000 FC
SI:
15000 FC
MRB
ST:
48000 FC
SI:
9300 FC
MRB
ST:
48000 FC
SI:
7500 FC
MRB
ST:
48000 FC
SI:
4300 FC
MRB
TPS
REFERENCES
572600-220-003
NTM 57-26-01
SOURCE:
MRB 572601-02-1
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
1
1
0.20
0.20
0.20
0.20
0.20
0.20
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
1
1
1
1
0.20
0.20
0.20
0.20
0.20
0.20
1130 1200
1379 1578
1657 1767
2151 2163
1
1
1
1
1
1
0.10
0.10
0.10
0.10
0.10
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
1
1
1
1
0.10
0.10
0.10
0.10
0.10
0.10
1130 1200
1379 1578
1657 1767
2151 2163
PREPARATION: FLAPS EXTENDED;
ACCESS PANELS: 531AB, 531BB, 531CB, 532AB, 532BB, 532CB, 533AB, 533BB,
533CB, 631AB, 631BB, 631CB, 632AB, 632BB, 632CB, 633AB, 633BB, 633CB
572601-02-3
531
532
533
631
632
633
FLAP TRACK BEAMS UPR FLANGE RADII
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,
FLAP TRACK BEAMS 2,3,4 TRACK UPPER FLANGE RADII
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572601-01-3
572600-220-003
NTM 57-26-01
SOURCE:
MRB 572601-02-3
PREPARATION: FLAPS EXTENDED;
ACCESS PANELS: 531AB, 531BB, 531CB, 532AB, 532BB, 532CB, 533AB, 533BB,
533CB, 631AB, 631BB, 631CB, 632AB, 632BB, 632CB, 633AB, 633BB, 633CB
572604-01-1
531
532
533
631
632
633
FLAP TRACK BEAMS LWR FLANGES
AF
DET
DETAILED INSPECTION OF OUTER WING, FLAP TRACK BEAMS
2,3,4 LOWER FLANGES AND LOWER CHANNEL
572600-200-005
SOURCE:
MRB 572604-01-1
PREPARATION: FLAPS EXTENDED;
ACCESS PANELS: 531AB, 531BB, 531CB, 532AB, 532BB, 532CB, 533AB, 533BB,
533CB, 631AB, 631BB, 631CB, 632AB, 632BB, 632CB, 633AB, 633BB, 633CB
572604-01-4
531
532
533
631
632
633
FLAP TRACK BEAMS LWR FLANGES
DETAILED INSPECTION OF OUTER WING, FLAP TRACK BEAMS
2,3,4 LOWER FLANGES AND LOWER CHANNEL
PREPARATION: FLAPS EXTENDED;
AF
DET
572600-200-005
SOURCE:
MRB 572604-01-4
ACCESS PANELS: 531AB, 531BB, 531CB, 532AB, 532BB, 532CB, 533AB, 533BB,
533CB, 631AB, 631BB, 631CB, 632AB, 632BB, 632CB, 633AB, 633BB, 633CB
Sub 2 - Page 237 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572607-01-1
572607-02-1
572610-01-1
ZONE
531
532
533
631
632
633
531
532
533
631
632
633
531
532
533
631
632
633
DESCRIPTION
FLAP TRACK BEAMS FWD SPIGOT ATTACH
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, FLAP TRACK BEAMS
2,3,4 FORWARD SPIGOT PINS, BOLTS AND FITTINGS.
ACCESS PANELS: 531AB, 531BB, 532AB, 532BB, 533AB, 533BB, 631AB, 631BB,
632AB, 632BB, 633AB, 633BB
FLAP TRACK BEAMS FWD SPIGOT ATTACH
AF
DET
DETAILED INSPECTION OF OUTER WING, FLAP TRACK BEAMS
2,3,4 FORWARD SPIGOT PINS, BOLTS AND FITTINGS
NOTE: REFER TO AMM FOR GAP CHECK
ACCESS PANELS: 531AB, 531BB, 532AB, 532BB, 533AB, 533BB, 631AB, 631BB,
632AB, 632BB, 633AB, 633BB
FLAP TRACK BEAMS AFT SPIGOT
AF
DET
DETAILED INSPECTION OF OUTER WING, FLAP TRACK BEAMS
2,3,4 AFT SPIGOT
NOTE: REFER TO AMM FOR TORQUE CHECK
INTERVALS
SOURCE
T:
6 YE
I:
6 YE
MRB CPCP
ST:
48000 FC
SI:
7100 FC
MRB
ST:
48000 FC
SI:
15000 FC
MRB
T:
6 YE
I:
6 YE
MRB CPCP
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
T:
6 YE
I:
6 YE
MRB CPCP
TPS
NO
REFERENCES
572600-200-006
SOURCE:
MRB 572607-01-1
572600-220-004
SOURCE:
MRB 572607-02-1
572600-220-005
SOURCE:
MRB 572610-01-1
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
1
1
0.10
0.10
0.10
0.10
0.10
0.10
ALL
1
1
1
1
1
1
0.25
0.25
0.25
0.25
0.25
0.25
ALL
1
1
1
1
1
1
0.10
0.10
0.10
0.10
0.10
0.10
ALL
1
1
1
1
1
1
0.10
0.10
0.10
0.10
0.10
0.10
ALL
1
1
0.20
0.20
ALL
1
1
0.10
0.10
ALL
PREPARATION: FLAPS EXTENDED;
572610-02-1
572650-01-1
531
532
533
631
632
633
571
671
ACCESS PANELS: 531CB, 532CB, 533CB, 631CB, 632CB, 633CB
FLAP TRACK BEAMS AFT SPIGOT
AF
DET
DETAILED INSPECTION OF OUTER WING, FLAP TRACK BEAMS
2,3,4 AFT SPIGOT
571
671
572600-200-010
SOURCE:
MRB 572610-02-1
PREPARATION: FLAPS EXTENDED;
ACCESS PANELS: 531CB, 532CB, 533CB, 631CB, 632CB, 633CB
OUTER WING REAR SPAR SIDESTAY FITTING
AF
DET
DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT FACE
SIDESTAY FITTING
572651-01-1
NO
OUTER WING REAR SPAR JACK FITTING
DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT FACE
RETRACTION JACK FITTING
AF
DET
572600-200-008
SOURCE:
MRB 572650-01-1
MRB CPCP
572600-200-007
SOURCE:
MRB 572651-01-1
PREPARATION: RETRACTION ANCHORAGE ACTUATOR REMOVED; BEARING
ASSEMBLY REMOVED;
Sub 2 - Page 238 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572653-01-1
ZONE
531
532
533
631
632
633
DESCRIPTION
FLAP TRACK 2 AFT ATTACH FITTINGS
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, FLAP TRACK 2, AFT
ATTACHMENT FITTINGS ON WING BOTTOM SKIN AT FALSE REAR
SPAR, AND FLAP TRACK 3 & 4, AFT ATTACHMENT FITTINGS
AT REAR SPAR
ACCESS PANELS: 531AB, 531BB, 531CB, 532AB, 532BB, 532CB, 533AB, 533BB,
533CB, 631AB, 631BB, 631CB, 632AB, 632BB, 632CB, 633AB, 633BB, 633CB
572654-01-1
521
621
OUTER WING PYLON FWD ATTACH FITTING
NDT
SDI
SPECIAL DETAILED INSPECTION (US AND EC) OF OUTER
WING, PYLON FORWARD ATTACHMENT FITTINGS
PREPARATION: BOLTS REMOVED; SHACKLES; SLEEVES; ENGINE REMOVED;
ACCESS PANELS: 521BT, 621BT
572654-01-3
521
621
OUTER WING PYLON FWD ATTACH FITTING
NDT
SDI
SPECIAL DETAILED INSPECTION (U/S + EDDY CURRENT) OF OUTER WING,
PYLON FORWARD ATTACHMENT FITTINGS
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
572654-01-1
572656-01-1
500
600
PREPARATION: ENGINE REMOVED; SHACKLES, SLEEVES; AND BOLTS
REMOVED;
OUTER WING PYLON SPIGOT
AF
DET
DETAILED INSPECTION OF OUTER WING, PYLON SPIGOT
FITTING
PREPARATION: BALL JOINT REMOVED; PYLON FAIRINGS REMOVED; SLEEVE
REMOVED;
572657-01-1
500
600
OUTER WING PYLON AFT FITTING LUG
DETAILED INSPECTION OF OUTER WING, AFT PYLON
ATTACHMENT FITTING LUG
PREPARATION: PYLON FAIRINGS REMOVED;
AF
DET
INTERVALS
SOURCE
ST:
48000 FC
SI:
20000 FC
T:
12 YE
I:
12 YE
MRB CPCP
ST:
48000 FC
OR
96000 FH
SI:
20000 FC
OR
40000 FH
MRB
ST:
48000 FC
OR
60000 FH
SI:
20000 FC
OR
27900 FH
MRB
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
TPS
NO
REFERENCES
572600-200-001
MEN
TASKM. APPLICABI
H.
LITY
0.10
0.10
0.10
0.10
0.10
0.10
ALL
SOURCE:
MRB 572653-01-1
1
1
1
1
1
1
572600-220-001
NTM 57-26-54
1
1
0.50
0.50
1130 1200
1379 1578
1657 1767
1
1
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
1
0.10
0.10
ALL
1
1
0.10
0.10
ALL
SOURCE:
MRB 572654-01-1
572600-220-001
NTM 57-26-54
SOURCE:
MRB 572654-01-3
572600-200-002
SOURCE:
MRB 572656-01-1
MRB CPCP
NO
572600-200-003
SOURCE:
MRB 572657-01-1
Sub 2 - Page 239 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
572658-01-1
572900-01-1
ZONE
531
532
533
631
632
633
500
600
DESCRIPTION
OUTER WING BOTTOM SKIN TRACK BEAM FTG
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE, FORWARD ATTACHMENT FITTING FOR FLAP TRACK
BEAMS 2,3 & 4
ACCESS PANELS: 531AB, 531BB, 532AB, 532BB, 533AB, 533BB, 631AB, 631BB,
632AB, 632BB, 633AB, 633BB
MISCELLANEOUS (DRAINS) FOR OUTER WING
AF
OPC
INTERVALS
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
I:
80 MO
SOURCE
MRB CPCP
534
634
WING TIP BOTTOM SKIN LWR SURFACE JOINT
AF
DET
DETAILED INSPECTION OF WING TIP, BOTTOM SKIN LOWER
SURFACE JOINT, OUTBOARD OF RIB 27
573101-01-4
534
634
WING TIP BOTTOM SKIN LWR SURFACE JOINT
AF
DET
DETAILED INSPECTION OF WING TIP, BOTTOM SKIN LOWER
SURFACE JOINT, OUTBOARD OF RIB 27
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS
ACCOMPLISHMENT OF TASK 573101-01-1
573900-01-1
530
630
MISCELLANEOUS (DRAINS) FOR WING TIP
CHECK OF DRAIN HOLES FOR CLOGGING
AF
OPC
ST:
34700 FC
OR
69400 FH
SI:
15000 FC
OR
30000 FH
T:
60000 FC
OR
120000 FH
I:
15000 FC
OR
30000 FH
T:
27900 FC
OR
39000 FH
I:
12400 FC
OR
17300 FH
I:
80 MO
REFERENCES
572600-200-009
SOURCE:
MRB 572658-01-1
MRB 9
CHECK OF DRAIN HOLES AND HOSES FOR CLOGGING
573101-01-1
TPS
ALI
MRB
572900-210-002
SOURCE:
MRB 57.29.00/01
573000-200-001
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
1
1
0.10
0.10
0.10
0.10
0.10
0.10
ALL
1
1
0.40
0.40
ALL
1
1
0.20
0.20
1130 1200
1379 1578
1657 1767
1
1
0.20
0.20
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
1
0.10
0.10
ALL
SOURCE:
ALI 573101-01-1
MRB 573101-01-1
ALI
573000-200-001
SOURCE:
ALI 573101-01-4
MRB 9
573900-200-002
SOURCE:
MRB 57.39.00/01
Sub 2 - Page 240 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
574101-01-1
ZONE
521
522
621
622
DESCRIPTION
FIXED LE ROLLER PIN HOLES
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, FIXED LEADING
EDGE, ROLLER PIN HOLES AND OTHER CUTOUTS IN TRACK RIB
1 TO 12
ACCESS PANELS: 521AB, 521CB, 521EB, 522AB, 522CB, 522FB, 522KB, 522LB,
522NB, 522QB, 522SB, 522UB, 621AB, 621CB, 621EB, 622AB, 622CB, 622FB,
622KB, 622LB, 622NB, 622QB, 622SB, 622UB
574101-01-3
521
522
621
622
FIXED LE ROLLER PIN HOLES
AF
DET
DETAILED INSPECTION OF OUTER WING, FIXED LEADING EDGE, ROLLER PIN
HOLES AND OTHER CUTOUTS IN TRACK RIB 1 TO 12
ACCESS PANELS: 521AB, 521CB, 521EB, 522AB, 522CB, 522FB, 522KB, 522LB,
522NB, 522QB, 522SB, 522UB, 621AB, 621CB, 621EB, 622AB, 622CB, 622FB,
622KB, 622LB, 622NB, 622QB, 622SB, 622UB
574102-01-1
522
622
FIXED LE FWD UPR ROLLER PIN HOLES
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,
FIXED LEADING EDGE, FORWARD UPPER ROLLER PIN HOLES IN
TRACK RIBS 5,6,7,8,9,10,11 AND 12.
PREPARATION: SLATS AND SLAT TRACKS REMOVED;
NDT
SDI
INTERVALS
ST:
30000 FC
OR
52500 FH
SI:
23000 FC
OR
32000 FH
T:
12 YE
I:
6 YE
ST:
30000 FC
OR
60000 FH
SI:
20600 FC
OR
41200 FH
T:
12 YE
OR
52200 FC
OR
104400 FH
I:
6 YE
OR
20600 FC
OR
41200 FH
ST:
48000 FC
OR
96000 FH
SI:
22500 FC
OR
45000 FH
SOURCE
MRB CPCP
TPS
REFERENCES
574100-200-012
SOURCE:
MRB 574101-01-1
ALI
MRB CPCP
574100-200-012
SOURCE:
ALI 574101-01-3
MRB 574101-01-3
MRB
574100-200-013
NTM 57-41-02
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
0.73
0.73
0.73
0.73
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
1
1
0.73
0.73
0.73
0.73
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.80
0.80
1130 1200
1379 1578
1657 1767
SOURCE:
MRB 574102-01-1
ACCESS PANELS: 522AB, 522CB, 522FB, 522KB, 522LB, 522NB, 522QB, 522SB,
522UB, 622AB, 622CB, 622FB, 622KB, 622LB, 622NB, 622QB, 622SB, 622UB
Sub 2 - Page 241 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
574102-01-4
ZONE
522
622
DESCRIPTION
FIXED LE FWD UPR ROLLER PIN HOLES
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,
FIXED LEADING EDGE, FORWARD UPPER ROLLER PIN HOLES IN
TRACK RIBS 5,6,7,8,9,10,11 AND 12.
PREPARATION: SLATS AND SLAT TRACKS REMOVED;
INTERVALS
SOURCE
ST:
48000 FC
OR
60000 FH
SI:
25500 FC
OR
31400 FH
MRB
ST:
46000 FC
OR
60000 FH
SI:
22500 FC
OR
31400 FH
MRB
ST:
12 YE
OR
30000 FC
OR
52500 FH
SI:
6 YE
OR
21000 FC
OR
29600 FH
T:
24 YE
I:
6 YE
MRB CPCP
TPS
REFERENCES
574100-200-013
NTM 57-41-02
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.80
0.80
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.80
0.80
2151 2163
1
1
1
1
0.10
0.10
0.10
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
MRB 574102-01-4
ACCESS PANELS: 522AB, 522CB, 522FB, 522KB, 522LB, 522NB, 522QB, 522SB,
522UB, 622AB, 622CB, 622FB, 622KB, 622LB, 622NB, 622QB, 622SB, 622UB
574102-01-5
522
622
FIXED LE FWD UPR ROLLER PIN HOLES
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,
FIXED LEADING EDGE, FORWARD UPPER ROLLER PIN HOLES IN
TRACK RIBS 5,6,7,8,9,10,11 AND 12.
PREPARATION: SLATS AND SLAT
TRACKS REMOVED;
574100-200-013
NTM 57-41-02
SOURCE:
MRB 574102-01-5
ACCESS PANELS: 522AB, 522CB, 522FB, 522KB, 522LB, 522NB, 522QB, 522SB,
522UB, 622AB, 622CB, 622FB, 622KB, 622LB, 622NB, 622QB, 622SB, 622UB
574106-01-1
521
522
621
622
FIXED LE BOTTOM ATTACH JOINT
DETAILED INSPECTION OF OUTER WING, FIXED LEADING
EDGE, BOTTOM ATTACHMENT JOINT ON TRACK RIB 1 TO 12
ACCESS PANELS: 521AB, 521CB, 521EB, 522AB, 522CB, 522FB, 522KB, 522LB,
522NB, 522QB, 522SB, 522UB, 621AB, 621CB, 621EB, 622AB, 622CB, 622FB,
622KB, 622LB, 622NB, 622QB, 622SB, 622UB
AF
DET
574100-200-014
SOURCE:
MRB 574106-01-1
Sub 2 - Page 242 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
574106-01-3
ZONE
521
522
621
622
DESCRIPTION
FIXED LE BOTTOM ATTACH JOINT
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, FIXED LEADING
EDGE, BOTTOM ATTACHMENT JOINT ON TRACK RIB 1 TO 12
ACCESS PANELS: 521AB, 521CB, 521EB, 522AB, 522CB, 522FB, 522KB, 522LB,
522NB, 522QB, 522SB, 522UB, 621AB, 621CB, 621EB, 622AB, 622CB, 622FB,
622KB, 622LB, 622NB, 622QB, 622SB, 622UB
574106-01-5
521
522
621
622
FIXED LE BOTTOM ATTACH JOINT
AF
DET
DETAILED INSPECTION OF OUTER WING, FIXED LEADING
EDGE, BOTTOM ATTACHMENT JOINT ON TRACK RIB 1 TO 12
ACCESS PANELS: 521AB, 521CB, 521EB, 522AB, 522CB, 522FB, 522KB, 522LB,
522NB, 522QB, 522SB, 522UB, 621AB, 621CB, 621EB, 622AB, 622CB, 622FB,
622KB, 622LB, 622NB, 622QB, 622SB, 622UB
574112-01-1
521
522
621
622
FIXED LE MAIN BOTTOM WING SKIN
DETAILED INSPECTION OF OUTER WING, FIXED LEADING
EDGE, BOTTOM WING SKIN, UPPER AND LOWER SURFACES,
FORWARD OF FRONT SPAR, FROM RIB 1 TO RIB 27,
INCLUDING SIGHTING ROD HOLES IN RIB BAY 8-9 AND RIB
BAY 26-27, LIFTING BEAM HOLES AND DRAIN HOLES
AF
DET
INTERVALS
ST:
12 YE
OR
48000 FC
OR
96000 FH
SI:
6 YE
OR
15400 FC
OR
30800 FH
T:
24 YE
I:
6 YE
ST:
12 YE
OR
30000 FC
OR
52500 FH
SI:
6 YE
OR
15400 FC
OR
21500 FH
T:
24 YE
I:
6 YE
ST:
12 YE
SI:
6 YE
T:
24 YE
I:
6 YE
SOURCE
MRB CPCP
TPS
REFERENCES
574100-200-014
SOURCE:
MRB 574106-01-3
MRB CPCP
574100-200-014
SOURCE:
MRB 574106-01-5
MRB CPCP
574100-200-015
SOURCE:
MRB 574112-01-1
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
0.10
0.10
0.10
0.10
1130 1200
1379 1578
1657 1767
1
1
1
1
0.10
0.10
0.10
0.10
2151 2163
1
1
1
1
0.25
0.25
0.25
0.25
ALL
ACCESS PANELS: 521AB, 521CB, 521EB, 522AB, 522CB, 522FB, 522KB, 522LB,
522NB, 522QB, 522SB, 522UB, 621AB, 621CB, 621EB, 622AB, 622CB, 622FB,
622KB, 622LB, 622NB, 622QB, 622SB, 622UB
Sub 2 - Page 243 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
574113-01-1
574114-01-1
ZONE
521
522
621
622
521
522
621
622
DESCRIPTION
FIXED LE TOP WING SKIN
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, FIXED LEADING EDGE
TOP WING SKIN, UPPER AND LOWER SURFACES, FORWARD OF
FRONT SPAR, FROM RIB 1 TO RIB 27
ACCESS PANELS: 521AB, 521CB, 521EB, 522AB, 522CB, 522FB, 522KB, 522LB,
522NB, 522QB, 522SB, 522UB, 621AB, 621CB, 621EB, 622AB, 622CB, 622FB,
622KB, 622LB, 622NB, 622QB, 622SB, 622UB
FIXED LE PINION FITTING
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,
FIXED LEADING EDGE PINION FITTING BOLTING AND
ACTUATOR BOLTING LOWER BOLT HOLES ON RIB
2,3,5,6,7,8,9,10,11 AND 12
ACCESS PANELS: 521CB, 521EB, 522AB, 522CB, 522FB, 522KB, 522LB, 522NB,
522QB, 522SB, 522UB, 621CB, 621EB, 622AB, 622CB, 622FB, 622KB, 622LB,
622NB, 622QB, 622SB, 622UB
574114-01-3
574145-01-1
521
522
621
622
521
621
FIXED LE PINION FITTING
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,
FIXED LEADING EDGE PINION FITTING BOLTING AND
ACTUATOR BOLTING LOWER BOLT HOLES ON RIB
2,3,5,6,7,8,9,10,11 AND 12
ACCESS PANELS: 521CB, 521EB, 522AB, 522CB, 522FB, 522KB, 522LB, 522NB,
522QB, 522SB, 522UB, 621CB, 621EB, 622AB, 622CB, 622FB, 622KB, 622LB,
622NB, 622QB, 622SB, 622UB
LEADING EDGE ACCESS PANEL LANDING AND ADJACENT AREA
DETAILED INSPECTION OF OUTER WING, LEADING EDGE, ACCESS PANEL
521EB/621EB, OUTBOARD AFT LANDING AND ADJACENT AREA FOR DAMAGE
AND CRACKING
NOTE: A REPAIR BY INSTALLATION OF THE POST 32664 LANDING ASSEMBLIES
(D5745018300000 AND D5745018300100) CANCELS THE INSPECTION
REQUIREMENTS.
ACCESS PANELS: 521EB, 621EB
AF
DET
INTERVALS
SOURCE
ST:
12 YE
SI:
6 YE
T:
24 YE
I:
6 YE
MRB CPCP
ST:
30000 FC
OR
41900 FH
SI:
12300 FC
OR
17100 FH
T:
36900 FC
OR
51600 FH
I:
12300 FC
OR
17100 FH
T:
33200 FC
OR
46500 FH
I:
12300 FC
OR
17100 FH
ALI
MRB
T:
750 FH
OR
750 FC
OR
4 MO
I:
15000 FH
OR
10000 FC
OR
48 MO
ISB
TPS
REFERENCES
574100-200-016
SOURCE:
MRB 574113-01-1
574100-200-017
NTM 57-41-14
SOURCE:
ALI 574114-01-1
MRB 574114-01-1
ALI
574100-200-017
NTM 57-41-14
SOURCE:
ALI 574114-01-3
JIC A320-57-41-00
ISB 57-1122
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
0.25
0.25
0.25
0.25
ALL
1
1
1
1
0.50
0.50
0.50
0.50
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
1
1
0.50
0.50
0.50
0.50
2151 2163
1
1
0.25
0.25
0649 1130
1200 1379
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
Sub 2 - Page 244 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
574201-01-1
ZONE
500
600
DESCRIPTION
SLAT 1, TRACKS 1-4
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF SLAT 1, TRACKS 1 TO 4 :
VISIBLE PART OF ROLLER CONTACT AREA WHEN SLAT IS
FULLY EXTENDED, LH/RH
PREPARATION: SLATS FULLY EXTENDED;
574202-01-1
500
600
SLAT 1 TRACKS 1-4 ATTACHMENTS
AF
DET
DETAILED INSPECTION OF SLAT 1, TRACKS 1 TO 4
ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS,
BOLTS, LINKS AND SIDE PLATES, LH/RH
INTERVALS
SOURCE
ST:
6 YE
SI:
6 YE
T:
24 YE
I:
6 YE
T:
12 YE
I:
6 YE
MRB CPCP
ST:
12 YE
OR
39000 FC
OR
78000 FH
SI:
12 YE
OR
16000 FC
OR
32000 FH
T:
24 YE
I:
12 YE
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
TPS
NO
REFERENCES
574100-200-002
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
ALL
1
1
0.20
0.20
ALL
1
1
0.20
0.20
ALL
1
1
0.40
0.40
ALL
SOURCE:
MRB 574201-01-1
MRB CPCP
NO
574200-200-001
SOURCE:
MRB 574202-01-1
PREPARATION: BOLTS SUCCESSIVELY REMOVED; SLATS FULLY EXTENDED;
574204-01-1
500
600
SLAT 1 SKIN CONNECTIONS
AF
DET
DETAILED INSPECTION OF SLAT 1, SKIN CONNECTIONS IN
AREA OF LOWER GIRDER AT TRACK RIB STATIONS, LH/RH.
NOTE: DETAILED INSPECTION IS OF EXTERNAL STRUCTURE OF
SLAT 1.
PREPARATION: SLATS FULLY EXTENDED;
574204-02-1
500
600
SLAT 1 SKIN CONNECTIONS
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF SLAT 1,
SKIN CONNECTIONS IN AREA OF LOWER GIRDER AT TRACK RIB
STATIONS, LH/RH.
NOTE: SDET INSPECTION IS OF INTERNAL STRUCTURE OF
SLAT 1 (ENDOSCOPE).
NDT
SDI
NO
574200-200-004
SOURCE:
MRB 574204-01-1
MRB CPCP
NO
574200-200-005
NTM 57-42-04
SOURCE:
MRB 574204-02-1
PREPARATION: SLATS FULLY EXTENDED;
Sub 2 - Page 245 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
574204-03-1
ZONE
500
600
DESCRIPTION
SLAT 1
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF SLAT 1, SKIN CONNECTIONS IN
AREA OF LOWER GIRDER AT TRACK RIB STATIONS 3 AND 4, LH/RH
NOTE: SDET INSPECTION IS OF EXTERNAL STRUCTURE OF SLAT 1
PREPARATION: SLAT FULLY EXTENDED;
574205-01-1
500
600
SLAT 1 TRAILING EDGE
AF
DET
DETAILED INSPECTION OF SLAT 1, TRAILING EDGE, LOWER
FACE, LH/RH
574301-01-1
500
600
PREPARATION: SLATS FULLY EXTENDED;
SLAT 2 TRACK 5-6 ROLLER CONTACT AREA
AF
DET
DETAILED INSPECTION OF SLAT 2, TRACKS 5 AND 6 :
VISIBLE PART OF ROLLER CONTACT AREA WHEN SLAT IS
FULLY EXTENDED, LH/RH
PREPARATION: SLATS FULLY EXTENDED;
574302-01-1
500
600
SLAT 2 TRACK 5-6 ATTACHMENTS
AF
DET
DETAILED INSPECTION OF SLAT 2, TRACKS 5 AND 6
ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS,
BOLTS, LINKS AND SIDE PLATES, LH/RH
INTERVALS
SOURCE
ST:
39000 FC
OR
78000 FH
SI:
16000 FC
OR
32000 FH
MRB
T:
12 YE
I:
6 YE
MRB CPCP
ST:
6 YE
SI:
6 YE
T:
24 YE
I:
6 YE
T:
12 YE
I:
6 YE
MRB CPCP
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
TPS
REFERENCES
574200-280-801
NTM 57-42-04
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.27
0.27
ALL
1
1
0.10
0.10
ALL
1
1
0.10
0.10
ALL
1
1
0.10
0.10
ALL
1
1
0.10
0.10
ALL
SOURCE:
MRB 574204-03-1
NO
574200-200-006
SOURCE:
MRB 574205-01-1
NO
574100-200-008
SOURCE:
MRB 574301-01-1
MRB CPCP
NO
574300-200-008
SOURCE:
MRB 574302-01-1
PREPARATION: BOLTS SUCCESSIVELY REMOVED; SLATS FULLY EXTENDED;
574304-01-1
500
600
SLAT 2 SKIN CONNECTIONS
DETAILED INSPECTION OF SLAT 2, SKIN CONNECTIONS IN
AREA OF LOWER GIRDER AT TRACK RIB STATIONS, LH/RH
NOTE: DET INSPECTION IS OF EXTERNAL STRUCTURE OF
SLAT 2.
PREPARATION: SLATS FULLY EXTENDED;
AF
DET
NO
574300-200-002
SOURCE:
MRB 574304-01-1
Sub 2 - Page 246 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
574304-02-2
ZONE
500
600
DESCRIPTION
SLAT 2 SKIN CONNECTIONS
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF SLAT 2,
SKIN CONNECTIONS IN AREA OF LOWER GIRDER AT TRACK RIB
STATIONS, LH/RH.
NOTE: SDET INSPECTION IS OF INTERNAL STRUCTURE OF
SLAT 2.
574304-03-1
500
600
PREPARATION: SLATS FULLY EXTENDED;
SLAT 2 SKIN CONNECTIONS
NDT
SDI
SPECIAL DETAILED INSPECTION (LFEC) OF SLAT 2, SKIN
CONNECTIONS IN AREA OF LOWER GIRDER AT TRACK RIB
STATIONS, LH/RH.
NOTE: SDET INSPECTION IS OF EXTERNAL STRUCTURE OF
SLAT 2.
574305-01-1
500
600
PREPARATION: SLATS FULLY EXTENDED;
SLAT 2 TRAILING EDGE
AF
DET
DETAILED INSPECTION OF SLAT 2, TRAILING EDGE, LOWER
FACE, LH/RH
574401-01-1
500
600
PREPARATION: SLATS FULLY EXTENDED;
SLAT 3 TRACK 7-8 ROLLER CONTACT AREA
AF
DET
DETAILED INSPECTION OF SLAT 3, TRACKS 7 AND 8 :
VISIBLE PART OF ROLLER CONTACT AREA WHEN SLAT IS
FULLY EXTENDED, LH/RH
PREPARATION: SLATS FULLY EXTENDED;
574402-01-1
500
600
SLAT 3 TRACK 7-8 ATTACHMENTS
DETAILED INSPECTION OF SLAT 3, TRACKS 7 AND 8
ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS,
BOLTS, LINKS AND SIDE PLATES, LH/RH
AF
DET
INTERVALS
SOURCE
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
ST:
39000 FC
OR
78000 FH
SI:
16000 FC
OR
32000 FH
MRB
T:
12 YE
I:
6 YE
MRB CPCP
ST:
6 YE
SI:
6 YE
T:
24 YE
I:
6 YE
T:
12 YE
I:
6 YE
MRB CPCP
TPS
NO
REFERENCES
574300-200-003
NTM 57-43-04
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.40
0.40
ALL
1
1
0.40
0.40
ALL
1
1
0.10
0.10
ALL
1
1
0.10
0.10
ALL
1
1
0.10
0.10
ALL
SOURCE:
MRB 574304-02-2
574300-280-801
NTM 57-43-04
SOURCE:
MRB 574304-03-1
NO
574300-200-001
SOURCE:
MRB 574305-01-1
NO
574100-200-009
SOURCE:
MRB 574401-01-1
MRB CPCP
NO
574400-200-010
SOURCE:
MRB 574402-01-1
PREPARATION: BOLTS SUCCESSIVELY REMOVED; SLATS FULLY EXTENDED;
Sub 2 - Page 247 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
574404-01-1
ZONE
500
600
DESCRIPTION
SLAT 3 SKIN CONNECTIONS
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF SLAT 3, SKIN
CONNECTIONS IN AREA OF LOWER GIRDER AT TRACK RIB
STATIONS, LH/RH
NOTE: DET INSPECTION IS OF EXTERNAL STRUCTURE OF
SLAT 3.
PREPARATION: SLATS FULLY EXTENDED;
574404-02-1
500
600
SLAT 3 SKIN CONNECTIONS
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF SLAT 3,
SKIN CONNECTIONS IN AREA OF LOWER GIRDER AT TRACK RIB
STATIONS, LH/RH.
NOTE: SDET INSPECTION IS OF INTERNAL STRUCTURE OF
SLAT 3.
574405-01-1
500
600
PREPARATION: SLATS FULLY EXTENDED;
SLAT 3 TRAILING EDGE
AF
DET
DETAILED INSPECTION OF SLAT 3, TRAILING EDGE, LOWER
FACE, LH/RH
574501-01-1
500
600
PREPARATION: SLATS FULLY EXTENDED;
SLAT 4 TRACK 9-10 ROLLER CONTACT AREA
AF
DET
DETAILED INSPECTION OF SLAT 4, TRACKS 9 AND 10 :
VISIBLE PART OF ROLLER CONTACT AREA WHEN SLAT IS
FULLY EXTENDED, LH/RH
PREPARATION: SLATS FULLY EXTENDED;
574502-01-1
500
600
SLAT 4 TRACK 9-10 ATTACHMENTS
DETAILED INSPECTION OF SLAT 4, TRACKS 9 AND 10
ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK LUGS,
BOLTS, LINKS AND SIDE PLATES, LH/RH
AF
DET
INTERVALS
SOURCE
ST:
12 YE
OR
39000 FC
OR
78000 FH
SI:
12 YE
OR
16000 FC
OR
32000 FH
T:
24 YE
I:
12 YE
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
T:
12 YE
I:
6 YE
MRB CPCP
ST:
6 YE
SI:
6 YE
T:
24 YE
I:
6 YE
T:
12 YE
I:
6 YE
MRB CPCP
TPS
NO
REFERENCES
574400-200-007
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.50
0.50
ALL
1
1
0.10
0.10
ALL
1
1
0.10
0.10
ALL
1
1
0.10
0.10
ALL
1
1
0.10
0.10
ALL
SOURCE:
MRB 574404-01-1
MRB CPCP
NO
574400-200-008
NTM 57-44-04
SOURCE:
MRB 574404-02-1
NO
574400-200-009
SOURCE:
MRB 574405-01-1
NO
574100-200-010
SOURCE:
MRB 574501-01-1
MRB CPCP
NO
574500-200-008
SOURCE:
MRB 574502-01-1
PREPARATION: BOLTS SUCCESSIVELY REMOVED; SLATS FULLY EXTENDED;
Sub 2 - Page 248 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
574504-01-1
ZONE
500
600
DESCRIPTION
SLAT 4 SKIN CONNECTIONS
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF SLAT 4, SKIN CONNECTIONS IN AREA OF LOWER
GIRDER AT TRACK RIB STATIONS, LH/RH
NOTE: DET INSPECTION IS OF EXTERNAL STRUCTURE OF SLAT 4.
PREPARATION: SLATS FULLY EXTENDED;
574504-02-1
500
600
SLAT 4 SKIN CONNECTIONS
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF SLAT 4,
SKIN CONNECTIONS IN AREA OF LOWER GIRDER AT TRACK RIB
STATIONS, LH/RH.
NOTE: SDET INSPECTION IS OF INTERNAL STRUCTURE OF
SLAT 4.
574505-01-1
500
600
PREPARATION: SLATS FULLY EXTENDED;
SLAT 4 TRAILING EDGE
AF
DET
DETAILED INSPECTION OF SLAT 4, TRAILING EDGE, LOWER
FACE, LH/RH
574601-01-1
500
600
PREPARATION: SLATS FULLY EXTENDED;
SLAT 5 TRACK 11-12 ROLLER CONTACT AREA
AF
DET
DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND 12 :
VISIBLE PART OF ROLLER CONTACT AREA WHEN SLAT IS
FULLY EXTENDED, LH/RH
PREPARATION: SLATS FULLY EXTENDED;
574602-01-1
500
600
SLAT 5 TRACK 11-12 ATTACHMENTS
DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND 12
ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK LUGS,
BOLTS, LINKS AND SIDE PLATES, LH/RH
AF
DET
INTERVALS
SOURCE
ST:
12 YE
OR
39000 FC
OR
78000 FH
SI:
12 YE
OR
16000 FC
OR
32000 FH
T:
24 YE
I:
12 YE
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
T:
12 YE
I:
6 YE
MRB CPCP
ST:
6 YE
SI:
6 YE
T:
24 YE
I:
6 YE
T:
12 YE
I:
6 YE
MRB CPCP
TPS
NO
REFERENCES
574500-200-005
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.50
0.50
ALL
1
1
0.10
0.10
ALL
1
1
0.10
0.10
ALL
1
1
0.10
0.10
ALL
1
1
0.10
0.10
ALL
SOURCE:
MRB 574504-01-1
MRB CPCP
NO
574500-200-006
NTM 57-45-04
SOURCE:
MRB 574504-02-1
NO
574500-200-007
SOURCE:
MRB 574505-01-1
NO
574100-200-011
SOURCE:
MRB 574601-01-1
MRB CPCP
NO
574600-200-008
SOURCE:
MRB 574602-01-1
PREPARATION: BOLTS SUCCESSIVELY REMOVED; SLATS FULLY EXTENDED;
Sub 2 - Page 249 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
574604-01-1
ZONE
500
600
DESCRIPTION
SLAT 5 SKIN CONNECTIONS
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF SLAT 5, SKIN CONNECTIONS IN
AREA OF LOWER GIRDER AT TRACK RIB STATIONS, LH/RH.
NOTE: DETAILED INSPECTION IS OF EXTERNAL STRUCTURE OF
SLAT 5.
PREPARATION: SLATS FULLY EXTENDED;
574604-02-1
500
600
SLAT 5 SKIN CONNECTIONS
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF SLAT 5,
SKIN CONNECTIONS IN AREA OF LOWER GIRDER AT TRACK RIB
STATIONS, LH/RH.
NOTE: SDET INSPECTION IS OF INTERNAL STRUCTURE OF
SLAT 5.
574605-01-1
500
600
PREPARATION: SLATS FULLY EXTENDED;
SLAT 5 TRAILING EDGE
AF
DET
DETAILED INSPECTION OF SLAT 5, TRAILING EDGE, LOWER
FACE LH/RH
575101-01-1
575101-02-1
531
532
533
631
632
633
531
532
533
631
632
633
PREPARATION: SLATS FULLY EXTENDED;
TRAILING EDGE FLAP ACTUATOR BRACKETS
AF
DET
DETAILED INSPECTION OF OUTER WING, TRAILING EDGE FLAP
ACTUATOR BRACKETS AT FLAP TRACKS 2,3 AND 4
ACCESS PANELS: 531CB, 532CB, 533CB, 631CB, 632CB, 633CB
TRAILING EDGE FLAP ACTUATOR BRACKETS
SPECIAL DETAILED INSPECTION (US) OF OUTER WING,
TRAILING EDGE FLAP ACTUATOR BRACKETS AT FLAP TRACKS
2,3 AND 4
NDT
SDI
INTERVALS
SOURCE
ST:
12 YE
OR
39000 FC
OR
78000 FH
SI:
12 YE
OR
16000 FC
OR
32000 FH
T:
24 YE
I:
12 YE
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
T:
12 YE
I:
6 YE
MRB CPCP
T:
12 YE
I:
12 YE
MRB CPCP
ST:
48000 FC
SI:
20000 FC
MRB
TPS
NO
REFERENCES
574600-200-005
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.10
0.10
ALL
1
1
0.50
0.50
ALL
1
1
0.15
0.15
ALL
1
1
1
1
1
1
1
1
1
1
1
1
0.30
0.30
0.30
0.30
0.30
0.30
0.75
0.75
0.75
0.75
0.75
0.75
ALL
SOURCE:
MRB 574604-01-1
MRB CPCP
NO
574600-200-006
NTM 57-46-04
SOURCE:
MRB 574604-02-1
NO
574600-200-007
SOURCE:
MRB 574605-01-1
575100-220-004
SOURCE:
MRB 575101-01-1
575100-220-005
NTM 57-51-01
SOURCE:
MRB 575101-02-1
0649 1488
1560 1743
1761 1851
1863 1876
1890
ACCESS PANELS: 531CB, 532CB, 533CB, 631CB, 632CB, 633CB
Sub 2 - Page 250 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
575101-02-3
575104-01-1
ZONE
531
532
533
631
632
633
500
600
DESCRIPTION
TRAILING EDGE FLAP ACTUATOR BRACKETS
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (US) OF OUTER WING,
TRAILING EDGE FLAP ACTUATOR BRACKETS AT FLAP TRACKS
2,3 AND 4
ACCESS PANELS: 531CB, 532CB, 533CB, 631CB, 632CB, 633CB
TRAILING EDGE SPOILER 1 HINGE FITTINGS
AF
DET
DETAILED INSPECTION OF OUTER WING, TRAILING EDGE,
SPOILER 1 ACTUATOR AND HINGE FITTINGS
PREPARATION: FLAPS EXTENDED; SPOILERS EXTENDED;
575106-01-1
575106-02-1
574
575
582
583
584
585
586
674
675
682
683
684
685
686
574
575
582
583
584
585
586
674
675
682
683
684
685
686
TRAILING EDGE SPOILERS HINGE PINS
AF
DET
DETAILED INSPECTION OF OUTER WING, TRAILING EDGE,
SPOILERS 1,2,3,4 AND 5 HINGE PINS
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 575106-02-1
INTERVALS
SOURCE
ST:
48000 FC
SI:
15000 FC
MRB
ST:
48000 FC
SI:
15000 FC
T:
12 YE
I:
12 YE
ST:
48000 FC
SI:
15000 FC
MRB CPCP
ST:
48000 FC
SI:
20000 FC
MRB
TPS
REFERENCES
575100-220-005
NTM 57-51-01
SOURCE:
MRB 575101-02-3
575100-220-006
MRB
575100-210-001
SOURCE:
MRB 575106-01-1
ACCESS PANELS: 573BB, 575BB, 575DB, 575EB, 575GB, 673BB, 675BB, 675DB,
675EB, 675GB
SPECIAL DETAILED INSPECTION (MPI) OF OUTER WING,
TRAILING EDGE, SPOILERS 1,2,3,4 AND 5 HINGE PINS
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 575106-01-1
PREPARATION: PINS REMOVED;
ACCESS PANELS: 573BB, 575BB, 575DB, 575EB, 575GB, 673BB, 675BB, 675DB,
675EB, 675GB
NDT
SDI
TASKM. APPLICABI
H.
LITY
1
1
1
1
1
1
0.75
0.75
0.75
0.75
0.75
0.75
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.30
0.30
ALL
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
0.03
0.03
0.03
0.03
0.03
0.03
0.03
0.03
0.03
0.03
0.03
0.03
0.03
0.03
0.75
0.75
0.75
0.75
0.75
0.75
0.75
0.75
0.75
0.75
0.75
0.75
0.75
0.75
ALL
SOURCE:
MRB 575104-01-1
PREPARATION: PINS REMOVED;
TRAILING EDGE SPOILERS HINGE PINS
MEN
575100-220-015
NTM 57-51-06
SOURCE:
MRB 575106-02-1
ALL
Sub 2 - Page 251 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
575106-03-1
575107-01-1
575107-02-1
575107-02-3
ZONE
574
575
582
583
584
585
586
674
675
682
683
684
685
686
575
583
584
585
586
675
683
684
685
686
575
583
584
585
586
675
683
684
685
686
575
583
584
585
586
675
683
684
685
686
DESCRIPTION
TRAILING EDGE SPOILERS HINGE PINS
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING TRAILING EDGE
SPOILERS 1,2,3,4 AND 5 HINGE PINS
INTERVALS
SOURCE
T:
12 YE
I:
12 YE
MRB CPCP
T:
12 YE
I:
6 YE
MRB CPCP
ST:
48000 FC
SI:
15000 FC
MRB
ST:
48000 FC
SI:
13600 FC
MRB
TPS
REFERENCES
575100-210-002
SOURCE:
MRB 575106-03-1
PREPARATION: PINS REMOVED;
ACCESS PANELS: 573BB, 575BB, 575DB, 575EB, 575GB, 673BB, 675BB, 675DB,
675EB, 675GB
TRAILING EDGE SPOILER 2-5 FITTINGS
AF
DET
DETAILED INSPECTION OF OUTER WING, TRAILING EDGE,
SPOILERS 2,3,4 AND 5 ACTUATOR AND HINGE FITTINGS
575100-220-009
SOURCE:
MRB 575107-01-1
PREPARATION: FLAPS EXTENDED; SPOILERS EXTENDED;
TRAILING EDGE SPOILER 2-5 FITTINGS
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,
TRAILING EDGE, SPOILERS 2,3,4 AND 5 ACTUATOR AND
HINGE FITTINGS
575100-220-010
NTM 57-51-07
SOURCE:
MRB 575107-02-1
PREPARATION: FLAPS EXTENDED; SPOILERS EXTENDED;
TRAILING EDGE SPOILER 2-5 FITTINGS
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING, TRAILING EDGE,
SPOILERS 2,3,4 AND 5 ACTUATOR AND HINGE FITTINGS
PREPARATION: FLAPS AND SPOILERS EXTENDED;
NDT
SDI
575100-220-010
NTM 57-51-07
SOURCE:
MRB 575107-02-3
MEN
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
TASKM. APPLICABI
H.
LITY
0.20
0.20
0.20
0.20
0.20
0.20
0.20
0.20
0.20
0.20
0.20
0.20
0.20
0.20
0.24
0.24
0.24
0.24
0.24
0.24
0.24
0.24
0.24
0.24
0.75
0.75
0.75
0.75
0.75
0.75
0.75
0.75
0.75
0.75
0.75
0.75
0.75
0.75
0.75
0.75
0.75
0.75
0.75
0.75
ALL
ALL
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1130 1200
1379 1578
1657 1767
Sub 2 - Page 252 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
575119-01-1
ZONE
575
590
675
690
DESCRIPTION
TRAILING EDGE AILERON HINGE FITTINGS
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, TRAILING EDGE,
AILERON HINGE FITTINGS 1 TO 5 AND "A" FRAMES
ACCESS PANELS: 575AT, 575JB, 575KB, 575LB, 575MB, 675AT, 675JB, 675KB,
675LB, 675MB
575120-01-1
575
590
675
690
TRAILING EDGE AILERON HINGE PINS
AF
DET
DETAILED INSPECTION OF OUTER WING, TRAILING EDGE,
AILERON HINGE PINS 1 TO 5
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 575120-02-1
INTERVALS
SOURCE
ST:
30500 FC
SI:
16500 FC
T:
12 YE
I:
12 YE
ST:
48000 FC
SI:
15000 FC
MRB CPCP
ST:
48000 FC
SI:
20000 FC
MRB
T:
12 YE
I:
7.5 YE
MRB CPCP
TPS
REFERENCES
575100-220-001
SOURCE:
MRB 575119-01-1
MRB
575100-220-002
SOURCE:
MRB 575120-01-1
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
0.13
0.13
0.13
0.13
ALL
1
1
1
1
0.30
0.30
0.30
0.30
ALL
1
1
1
1
0.80
0.80
0.80
0.80
ALL
1
1
1
1
0.30
0.30
0.30
0.30
ALL
PREPARATION: PINS REMOVED;
575120-02-1
575
590
675
690
ACCESS PANELS: 575AT, 575JB, 575KB, 575LB, 575MB, 675AT, 675JB, 675KB,
675LB, 675MB
TRAILING EDGE AILERON HINGE PINS
NDT
SDI
SPECIAL DETAILED INSPECTION (MPI) OF OUTER WING,
TRAILING EDGE, AILERON HINGE PINS 1 TO 5
575100-220-013
NTM 57-51-20
SOURCE:
MRB 575120-02-1
NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 575120-01-1
PREPARATION: PINS REMOVED;
575120-03-1
575
590
675
690
ACCESS PANELS: 575AT, 575JB, 575KB, 575LB, 575MB, 675AT, 675JB, 675KB,
675LB, 675MB
TRAILING EDGE AILERON HINGE PINS
DETAILED INSPECTION OF OUTER WING, TRAILING EDGE,
AILERON HINGE PINS 1 TO 5
AF
DET
575100-220-016
SOURCE:
MRB 575120-03-1
PREPARATION: PINS REMOVED;
ACCESS PANELS: 575AT, 575JB, 575KB, 575LB, 575MB, 675AT, 675JB, 675KB,
675LB, 675MB
Sub 2 - Page 253 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
575121-01-1
ZONE
575
590
675
690
DESCRIPTION
TRAILING EDGE AILERON ACTUATOR FITTING
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, TRAILING EDGE,
AILERON, INBOARD AND OUTBOARD ACTUATOR FITTINGS
ACCESS PANELS: 575KB, 575LB, 675KB, 675LB
575130-01-2
575
675
TRAILING EDGE SPOILER 2-4 FITTINGS/LEGS
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING, TRAILING EDGE,
SPOILERS 2, 3 AND 4 ACTUATOR AND HINGE FITTINGS AT VERTICAL LEGS
(APPLICABLE ONLY TO PART NUMBER D575-40139, 40140, 40141)
575140-01-1
147
148
PREPARATION: FLAPS AND SPOILERS EXTENDED;
FLAP TRACK 1
AF
DET
DETAILED INSPECTION OF FLAP TRACK 1, INCLUDING
ATTACHMENT BRACKETS TO FUSELAGE, STRUT, CARRIAGE AND
SWINGING LINK (PENDULUM), LH/RH
PREPARATION: FLAPS EXTENDED;
ACCESS PANELS: 191ET, 193AT, 734, 192ET, 194AT, 744
575142-01-1
147
148
INBOARD FLAP ACTUATOR DRIVE ARM
AF
DET
DETAILED INSPECTION OF INBOARD FLAP, INBOARD ACTUATOR
DRIVE ARM, DRIVE STRUT AND OUTER PART OF TRUNNION,
LH/RH
PREPARATION: FLAPS EXTENDED;
575150-01-2
571
671
ACCESS PANELS: 734, 744
OUTER WING MLG SUPPORT RIBS
DETAILED INSPECTION OF OUTER WING, MLG SUPPORT RIB 5,
OUTBOARD AND INBOARD FACES
AF
DET
INTERVALS
SOURCE
ST:
6 YE
OR
30000 FC
SI:
6 YE
OR
28000 FC
T:
24 YE
I:
6 YE
ST:
48000 FC
SI:
10800 FC
MRB CPCP
ST:
12 YE
OR
30000 FC
SI:
12 YE
OR
15000 FC
T:
24 YE
I:
12 YE
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
T:
12 YE
I:
6 YE
MRB CPCP
MRB
TPS
REFERENCES
575100-220-003
MEN
TASKM. APPLICABI
H.
LITY
0.10
0.10
0.10
0.10
ALL
SOURCE:
MRB 575121-01-1
1
1
1
1
575100-200-002
NTM 57-51-30
1
1
0.60
0.60
1130 1200
1379 1578
1657 1767
1
1
0.30
0.30
ALL
1
1
0.30
0.30
ALL
1
1
0.50
0.50
ALL
SOURCE:
MRB 575130-01-2
575100-200-003
SOURCE:
MRB 575140-01-1
MRB CPCP
575100-200-004
SOURCE:
MRB 575142-01-1
1+2 575100-200-005
SOURCE:
MRB 575150-01-2
ACCESS PANELS: 574AB, 674AB
Sub 2 - Page 254 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
575151-01-2
ZONE
573
574
673
674
DESCRIPTION
TRAILING EDGE FALSE REAR SPAR
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, TRAILING EDGE FALSE REAR SPAR,
FORWARD AND AFT FACES
ACCESS PANELS: 573AB, 573BB, 573CB, 574AB, 574BB, 673AB, 673BB, 673CB,
674AB, 674BB
575151-01-4
573
574
673
674
INNER REAR SPAR TRAILING EDGE
AF
DET
DETAILED INSPECTION OF OUTER WING, TRAILING EDGE FALSE REAR SPAR,
FORWARD AND AFT FACES
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
575151-01-2
575151-01-5
573
574
673
674
ACCESS PANELS: 573AB, 573BB, 573CB, 574AB, 574BB, 673AB, 673BB, 673CB,
674AB, 674BB
INNER REAR SPAR TRAILING EDGE
AF
DET
DETAILED INSPECTION OF OUTER WING, TRAILING EDGE,
FALSE REAR SPAR, FORWARD AND AFT FACES
ACCESS PANELS: 573AB, 573BB, 573CB, 574AB, 574BB, 673AB, 673BB, 673CB,
674AB, 674BB
575155-01-4
500
600
OUTER WING TRAILING EDGE TOP SKIN
AF
GVI
GENERAL VISUAL INSPECTION OF OUTER WING, TRAILING
EDGE, TOP SKIN UPPER SURFACE, AFT OF REAR SPAR
BETWEEN RIB 1 AND RIB 9
575158-01-1
500
600
OUTER WING BOTTOM SKIN LOWER SURFACE
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN
LOWER SURFACE, AFT OF REAR SPAR BETWEEN RIB 1 AND RIB
9, EXCLUDING AREAS COVERED BY FLAP TRACK 2 FAIRINGS
AND PYLON FAIRINGS
AF
GVI
INTERVALS
SOURCE
ST:
48000 FC
OR
96000 FH
SI:
15000 FC
OR
30000 FH
MRB
ST:
30000 FC
OR
46700 FH
SI:
7300 FC
OR
9500 FH
MRB
ST:
48000 FC
OR
60000 FH
SI:
15000 FC
OR
23300 FH
MRB
T:
55800 FC
OR
111600 FH
I:
10200 FC
OR
20400 FH
T:
24000 FC
OR
42000 FH
I:
5200 FC
OR
8800 FH
ALI
TPS
REFERENCES
575100-200-006
SOURCE:
MRB 575151-01-2
575100-200-006
SOURCE:
MRB 575151-01-4
575100-200-006
SOURCE:
MRB 575151-01-5
575100-210-802
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
0.38
0.38
0.38
0.38
1130 1200
1379 1578
1657 1767
1
1
1
1
0.38
0.38
0.38
0.38
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
1
1
0.38
0.38
0.38
0.38
2151 2163
1
1
0.20
0.20
1130 1200
1379 1578
1657 1767
1
1
0.10
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
ALI 575155-01-4
ALI
575100-210-003
SOURCE:
ALI 575158-01-1
Sub 2 - Page 255 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
575158-01-5
ZONE
500
600
DESCRIPTION
OUTER WING BOTTOM SKIN LOWER SURFACE
SKILL TASK
CODE CODE
AF
GVI
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN
LOWER SURFACE, AFT OF REAR SPAR BETWEEN RIB 1 AND RIB
9, EXCLUDING AREAS COVERED BY FLAP TRACK 2 FAIRINGS
AND PYLON FAIRINGS
575158-01-6
500
600
OUTER WING BOTTOM SKIN LOWER SURFACE
AF
GVI
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN
LOWER SURFACE, AFT OF REAR SPAR BETWEEN RIB 1 AND RIB
9, EXCLUDING AREAS COVERED BY FLAP TRACK 2 FAIRINGS
AND PYLON FAIRINGS
575159-01-1
500
600
OUTER WING BOTTOM SKIN/REAR SPAR
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER
SURFACE CURVED SKIN EDGE, AFT OF REAR SPAR JUST
INBOARD OF MLG SUPPORT RIB 5
575159-01-5
500
600
OUTER WING BOTTOM SKIN/REAR SPAR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER SURFACE
CURVED SKIN EDGE, AFT OF REAR SPAR JUST INBOARD OF MLG SUPPORT
RIB 5
AF
DET
INTERVALS
SOURCE
T:
25400 FC
OR
50800 FH
I:
13600 FC
OR
27200 FH
T:
25400 FC
OR
42900 FH
I:
4900 FC
OR
8300 FH
ST:
30000 FC
OR
60000 FH
SI:
9000 FC
OR
18000 FH
ALI
ST:
30000 FC
OR
48000 FH
SI:
7500 FC
OR
12000 FH
T:
41200 FC
OR
60000 FH
I:
7500 FC
OR
12000 FH
ALI
MRB
TPS
REFERENCES
575100-210-003
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.10
0.10
1130 1200
1379 1578
1657 1767
1
1
0.10
0.10
2151 2163
1
1
0.10
0.10
1130 1200
1379 1578
1657 1767
1
1
0.10
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
SOURCE:
ALI 575158-01-5
ALI
575100-210-003
SOURCE:
ALI 575158-01-6
MRB
575100-200-007
SOURCE:
MRB 575159-01-1
575100-200-007
SOURCE:
ALI 575159-01-5
MRB 575159-01-5
Sub 2 - Page 256 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
575160-01-1
ZONE
574
674
DESCRIPTION
TRAILING EDGE BOTTOM SKIN REAR SPAR
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OF OUTER
WING, TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR,
ABOVE MLG REINFORCING
PREPARATION: MLG SECONDARY HINGED FAIRING;
575160-01-5
574
674
ACCESS PANELS: 574AB, 674AB
TRAILING EDGE BOTTOM SKIN REAR SPAR
NDT
SDI
SPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OF OUTER WING, TRAILING
EDGE, BOTTOM SKIN, AFT OF REAR SPAR ABOVE MLG REINFORCING
PREPARATION: MLG SECONDARY HINGED FAIRING;
ACCESS PANELS: 574AB, 674AB
575160-01-7
574
674
TRAILING EDGE BOTTOM SKIN REAR SPAR
NDT
SDI
SPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OF OUTER
WING, TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR,
ABOVE MLG REINFORCING
PREPARATION: MLG SECONDARY HINGED
FAIRING;
575161-01-1
500
600
ACCESS PANELS: 574AB, 674AB
TRAILING EDGE BOTTOM SKIN REAR SPAR
GENERAL VISUAL INSPECTION OF OUTER WING, TRAILING
EDGE BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR FROM
RIB 9 TO RIB 12, INCLUDING JACKING FITTING HOLE AT
RIB 9 AND SIGHTING ROD HOLE AT RIB 10
AF
GVI
INTERVALS
SOURCE
T:
24000 FC
OR
38400 FH
I:
11800 FC
OR
18900 FH
ALI
ST:
33500 FC
OR
67000 FH
SI:
11800 FC
OR
23600 FH
T:
60000 FC
OR
120000 FH
I:
11800 FC
OR
23600 FH
T:
23100 FC
OR
37000 FH
I:
13400 FC
OR
21500 FH
ALI
MRB
T:
24000 FC
OR
42000 FH
I:
3800 FC
OR
6400 FH
ALI
TPS
REFERENCES
575100-200-008
NTM 57-51-60
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.80
0.80
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.80
0.80
1130 1200
1379 1578
1657 1767
1
1
0.80
0.80
2151 2163
1
1
0.10
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
ALI 575160-01-1
575100-200-008
NTM 57-51-60
SOURCE:
ALI 575160-01-5
MRB 575160-01-5
ALI
575100-200-008
NTM 57-51-60
SOURCE:
ALI 575160-01-7
575100-210-004
SOURCE:
ALI 575161-01-1
Sub 2 - Page 257 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
575161-01-5
ZONE
500
600
DESCRIPTION
TRAILING EDGE BOTTOM SKIN REAR SPAR
SKILL TASK
CODE CODE
AF
GVI
GENERAL VISUAL INSPECTION OF OUTER WING, TRAILING
EDGE BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR FROM
RIB 9 TO RIB 12, INCLUDING JACKING FITTING HOLE AT
RIB 9 AND SIGHTING ROD HOLE AT RIB 10
575163-01-2
574
674
OUTER WING BOTTOM SKIN UND PYLON FAIR
NDT
SDI
SPECIAL DETAILED INSPECTION (LFEC) OF OUTER WING,
BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR, UNDER
PYLON FAIRING
PREPARATION: PYLON FAIRINGS REMOVED;
575163-01-5
574
674
OUTER WING BOTTOM SKIN UNDER PYLON
FAIRING
SPECIAL DETAILED INSPECTION (LFEC) OF OUTER WING,
BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR, UNDER
PYLON FAIRING.
PREPARATION: PYLON FAIRINGS
REMOVED;
NDT
SDI
INTERVALS
T:
40400 FC
OR
60000 FH
I:
4500 FC
OR
7600 FH
ST:
30000 FC
OR
60000 FH
SI:
13200 FC
OR
26400 FH
T:
48000 FC
OR
96000 FH
I:
13200 FC
OR
26400 FH
ST:
30000 FC
OR
46500 FH
SI:
12100 FC
OR
18800 FH
T:
48000 FC
OR
60000 FH
I:
12100 FC
OR
18800 FH
SOURCE
ALI
TPS
REFERENCES
575100-210-004
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.10
0.10
2151 2163
1
1
0.75
0.75
1130 1200
1379 1578
1657 1767
1
1
0.75
0.75
2151 2163
SOURCE:
ALI 575161-01-5
ALI
MRB
575100-220-011
NTM 57-51-63
SOURCE:
ALI 575163-01-2
MRB 575163-01-2
ALI
MRB
575100-220-011
NTM 57-51-63
SOURCE:
ALI 575163-01-5
MRB 575163-01-5
Sub 2 - Page 258 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
575163-01-6
ZONE
574
674
DESCRIPTION
OUTER WING BOTTOM SKIN UNDER PYLON FAIRING
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (LFEC) OF OUTER WING, BOTTOM SKIN
LOWER SURFACE, AFT OF REAR SPAR UNDER PYLON FAIRING.
PREPARATION: FAIRINGS; PYLON; REMOVED;
575164-01-2
531
574
631
674
OUTER WING BOTTOM SKIN UND FLAP TRACK2
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,
BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR, AROUND
FLAP TRACK 2 FORWARD FITTINGS.
ACCESS PANELS: 531AB, 531BB, 631AB, 631BB
575165-01-3
531
574
631
674
OUTER WING BOTTOM SKIN UND FLAP 2 FAIR
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE, AFT OF REAR SPAR, UNDER FLAP TRACK 2 FAIRING
ACCESS PANELS: 531AB, 531BB, 631AB, 631BB
575165-01-5
531
574
631
674
OUTER WING BOTTOM SKIN UND FLAP 2 FAIR
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE, AFT OF REAR SPAR, UNDER FLAP TRACK 2 FAIRING
ACCESS PANELS: 531AB, 531BB, 631AB, 631BB
575166-01-2
574
674
OUTER WING FALSE REAR SPAR LWR FLANGE
DETAILED INSPECTION OF OUTER WING, FALSE REAR SPAR,
FORWARD FACE, LOWER FLANGE, BETWEEN RIB 7 AND RIB 9
ACCESS PANELS: 573BB, 573CB, 573DB, 573EB, 673BB, 673CB, 673DB, 673EB
AF
DET
INTERVALS
SOURCE
ST:
30000 FC
OR
46500 FH
SI:
10000 FC
OR
15500 FH
MRB
ST:
30000 FC
OR
52500 FH
SI:
11400 FC
OR
19000 FH
MRB
ST:
30000 FC
OR
52500 FH
SI:
12700 FC
OR
21100 FH
MRB
ST:
30000 FC
OR
52500 FH
SI:
11400 FC
OR
19000 FH
MRB
ST:
48000 FC
OR
96000 FH
SI:
7000 FC
OR
14000 FH
MRB
TPS
REFERENCES
575100-220-011
NTM 57-51-63
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.75
0.75
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
1
1
0.75
0.75
0.75
0.75
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
1
1
1
0.10
0.10
0.10
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
1
1
0.10
0.10
0.10
0.10
2151 2163
1
1
0.10
0.10
1130 1200
1379 1578
1657 1767
SOURCE:
MRB 575163-01-6
575100-220-012
NTM 57-51-64
SOURCE:
MRB 575164-01-2
575100-200-009
SOURCE:
MRB 575165-01-3
575100-200-009
SOURCE:
MRB 575165-01-5
575100-200-010
SOURCE:
MRB 575166-01-2
Sub 2 - Page 259 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
575166-01-4
ZONE
574
674
DESCRIPTION
OUTER WING FALSE REAR SPAR LWR FLANGE
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, FALSE REAR SPAR, FORWARD FACE,
LOWER FLANGE BETWEEN RIB 7 AND RIB 9
NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK
575166-01-2
INTERVALS
SOURCE
ST:
48000 FC
OR
60000 FH
SI:
7300 FC
OR
12300 FH
MRB
T:
6 YE
I:
6 YE
MRB CPCP
I:
12000 FC
OR
144 MO
ISB
MRB 6
LUR
ST:
12 YE
OR
32000 FC
SI:
12 YE
OR
13900 FC
T:
24 YE
I:
12 YE
MRB CPCP
TPS
REFERENCES
575100-200-010
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.10
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890 2151
2163
1
1
0.10
0.10
ALL
1
1
0.50
0.50
0649
1
1
0.30
0.30
ALL
SOURCE:
MRB 575166-01-4
ACCESS PANELS: 573BB, 573CB, 573DB, 573EB, 673BB, 673CB, 673DB, 673EB
575167-01-1
574
674
OUTER WING BOTTOM SKIN UPPER SURFACE
AF
DET
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN PANEL
NO. 3, UPPER SURFACE, BETWEEN REAR SPAR AND FALSE
REAR SPAR, AND BETWEEN GEAR SUPPORT RIB 5 AND RIB 8.
575200-01-1
500
600
ACCESS PANELS: 574AB, 574BB, 674AB, 674BB
INBOARD FLAP
AF
DET
DETAILED INSPECTION OF FLAP TRACK NO 1 DRIVE LEVER ARM FOR SIDE
PLAY
1+2 575100-200-011
SOURCE:
MRB 575167-01-1
575200-200-010
ISB 57-1108
SOURCE:
MRB 27.50.00/14
PREPARATION: FLAPS EXTENDED;
575203-01-1
581
681
ACCESS PANELS: 193AB, 193BB, 734, 194AB, 194BB, 744
INBOARD FLAP TRUNNION ATTACH BRACKET
DETAILED INSPECTION OF INBOARD FLAP, TRUNNION
ATTACHMENT BRACKET INCLUDING INBOARD TRUNNION, LH/RH
NOTE: THIS TASK HAS TO BE PERFORMED THE SAME TIME AS
TASK 575203-02-1.
PREPARATION: RUBBER SEALS; FLAPS EXTENDED;
AF
DET
NO
575200-200-007
SOURCE:
MRB 575203-01-1
Sub 2 - Page 260 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
575203-02-1
ZONE
581
681
DESCRIPTION
INBOARD FLAP TRUNNION ATTACH BRACKET
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF INBOARD
FLAP, TRUNNION ATTACHMENT BRACKET INCLUDING INBOARD
TRUNNION, LH/RH
NOTE: - INSPECTION IS THROUGH INSPECTION HOLES
- THIS TASK HAS TO BE PERFORMED THE SAME TIME
AS TASK 575203-01-1.
575205-01-1
531
581
631
681
PREPARATION: COVER TAPES FROM INSPECTION HOLES REMOVED; FLAPS
EXTENDED;
INBOARD FLAP DRIVE STRUT AND LEVER
AF
DET
DETAILED INSPECTION OF INBOARD FLAP, DRIVE STRUT FOR
FLAP AND DRIVE LEVER FOR FLAP TRACK FAIRING,
INCLUDING ATTACHMENT BRACKETS TO THE FLAP AND
SURROUNDING SKIN AT TRACK 2, LH/RH
PREPARATION: FLAPS EXTENDED;
575206-01-1
581
681
ACCESS PANELS: 531AT, 531CB, 631AT, 631CB
INBOARD FLAP INTERNAL BRACKETS
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF INBOARD
FLAP, INTERNAL BRACKETS AT TRACK 2, LH/RH
NOTE: INSPECTION IS THROUGH INSPECTION HOLES
PREPARATION: COVER TAPES FROM INSPECTION HOLES REMOVED; FLAPS
EXTENDED;
ACCESS PANELS: 531AT, 531CB, 631AT, 631CB
575207-01-1
531
581
631
681
INBOARD FLAP CARRIAGE ATTACH BRACKET
DETAILED INSPECTION OF INBOARD FLAP, FLAP TO CARRIAGE
ATTACHMENT BRACKET AT TRACK 2, INCLUDING SURROUNDING
SKIN, LH/RH
PREPARATION: FLAPS EXTENDED;
ACCESS PANELS: 531AT, 531CB, 631AT, 631CB
AF
DET
INTERVALS
SOURCE
ST:
12 YE
OR
32000 FC
SI:
12 YE
OR
13900 FC
T:
24 YE
I:
12 YE
ST:
42000 FC
SI:
15000 FC
T:
12 YE
I:
12 YE
MRB CPCP
ST:
12 YE
OR
32000 FC
SI:
12 YE
OR
15000 FC
T:
24 YE
I:
12 YE
ST:
12 YE
OR
32000 FC
SI:
12 YE
OR
16000 FC
T:
24 YE
I:
12 YE
MRB CPCP
TPS
NO
REFERENCES
575200-220-006
NTM 57-52-03
MEN
TASKM. APPLICABI
H.
LITY
1
1
1.00
1.00
ALL
0.50
0.50
0.50
0.50
ALL
SOURCE:
MRB 575205-01-1
1
1
1
1
575200-220-008
NTM 57-52-06
1
1
1.00
1.00
ALL
1
1
1
1
0.10
0.10
0.10
0.10
ALL
SOURCE:
MRB 575203-02-1
MRB CPCP
575200-200-008
NO
SOURCE:
MRB 575206-01-1
MRB CPCP
575200-200-009
SOURCE:
MRB 575207-01-1
Sub 2 - Page 261 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
575209-01-1
ZONE
477
487
581
681
DESCRIPTION
INBOARD FLAP ATTACH BRACKET OF FAIRING
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF INBOARD FLAP, ATTACHMENT
BRACKET OF PYLON AFT FAIRING, INCLUDING SURROUNDING
SKIN, LH/RH
PREPARATION: PYLON FAIRINGS REMOVED;
575210-01-1
581
681
INBOARD FLAP INTERNAL SUPPORT BRACKET
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF INBOARD
FLAP, INTERNAL SUPPORT BRACKET OF PYLON AFT FAIRING
ATTACHMENT, LH/RH
NOTE: INSPECTION IS THROUGH INSPECTION HOLES
PREPARATION: COVER TAPES FROM INSPECTION HOLES REMOVED; FLAPS
EXTENDED;
575211-01-1
581
681
INBOARD FLAP END RIB
AF
DET
DETAILED INSPECTION OF INBOARD FLAP, END RIB,
INCLUDING ROLLER AND INTERCONNECTION STRUT ATTACHMENT
BRACKET, LH/RH
575250-01-1
500
600
PREPARATION: RUBBER SEALS; FLAPS EXTENDED;
INBOARD FLAP TRACK 2 CARRIAGE
AF
DET
DETAILED INSPECTION OF OUTER WING, INBOARD FLAP TRACK
2 CARRIAGE FORGING
PREPARATION: FLAPS EXTENDED;
575250-02-1
500
600
INBOARD FLAP TRACK 2 CARRIAGE
SPECIAL DETAILED INSPECTION (U/S) OF OUTER WING,
INBOARD FLAP TRACK 2 CARRIAGE FORGING
NDT
SDI
INTERVALS
SOURCE
ST:
12 YE
OR
30000 FC
SI:
12 YE
OR
15100 FC
T:
24 YE
I:
12 YE
ST:
12 YE
OR
39000 FC
SI:
12 YE
OR
15300 FC
T:
24 YE
I:
12 YE
T:
12 YE
I:
12 YE
MRB CPCP
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
ST:
48000 FC
SI:
20000 FC
MRB CPCP
MRB CPCP
TPS
REFERENCES
575200-200-002
NO
MEN
TASKM. APPLICABI
H.
LITY
0.10
0.10
0.10
0.10
ALL
SOURCE:
MRB 575209-01-1
1
1
1
1
575200-200-003
NTM 57-52-10
1
1
1.00
1.00
ALL
1
1
0.45
0.45
ALL
1
1
0.10
0.10
ALL
1
1
0.80
0.80
ALL
SOURCE:
MRB 575210-01-1
MRB CPCP
575200-200-004
SOURCE:
MRB 575211-01-1
575200-200-005
SOURCE:
MRB 575250-01-1
MRB
575200-220-004
NTM 57-52-50
SOURCE:
MRB 575250-02-1
PREPARATION: FLAPS EXTENDED;
Sub 2 - Page 262 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
575251-01-1
ZONE
500
600
DESCRIPTION
INBOARD FLAP TRACK 2 ROLLERS
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING, INBOARD FLAP TRACK
2 CARRIAGE ROLLERS
575252-01-1
531
631
PREPARATION: FLAPS EXTENDED;
INBOARD FLAP TRACK 2 BOLT ASSEMBLY
NDT
SDI
SPECIAL DETAILED INSPECTION (MPI) OF OUTER WING,
INBOARD FLAP TRACK 2 FLAP PIVOT BOLT ASSEMBLY
575254-01-1
531
631
PREPARATION: INNER BOLT REMOVED; FLAPS EXTENDED;
INBOARD FLAP TRACK 2 DRIVE LEVER
AF
DET
DETAILED INSPECTION OF OUTER WING, INBOARD FLAP TRACK
2, DRIVE LEVER
PREPARATION: FLAPS EXTENDED; SPOILERS EXTENDED;
575254-02-1
531
631
INBOARD FLAP TRACK 2 DRIVE LEVER
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,
INBOARD FLAP TRACK 2, DRIVE LEVER
575303-01-1
587
687
PREPARATION: FLAPS EXTENDED; SPOILERS EXTENDED;
OUTBOARD FLAP TRACK 3 ATTACH AREAS
DETAILED INSPECTION OF OUTBOARD FLAP, FRONT SPAR
SPLICES AND ATTACHMENT AREAS AT TRACK 3, INTERNAL AND
EXTERNAL, LH/RH
AF
DET
INTERVALS
SOURCE
ST:
48000 FC
SI:
7500 FC
MRB
ST:
48000 FC
SI:
15000 FC
MRB
ST:
6 YE
SI:
6 YE
T:
24 YE
I:
6 YE
ST:
48000 FC
SI:
15500 FC
MRB CPCP
T:
6 YE
I:
6 YE
MRB CPCP
TPS
REFERENCES
575200-200-001
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.10
0.10
ALL
1
1
1.00
1.00
ALL
1
1
0.10
0.10
ALL
1
1
0.80
0.80
ALL
1
1
0.30
0.30
0649
SOURCE:
MRB 575251-01-1
575200-220-007
NTM 57-52-52
SOURCE:
MRB 575252-01-1
NO
575200-200-006
SOURCE:
MRB 575254-01-1
MRB
575200-220-005
NTM 57-52-54
SOURCE:
MRB 575254-02-1
NO
575300-200-004
SOURCE:
MRB 575303-01-1
NOTE: THIS TASK HAS TO BE PERFORMED THE SAME TIME AS
TASK 575303-02-1.
PREPARATION: LEADING EDGE PANEL 2; FLAPS EXTENDED;
ACCESS PANELS: 532AT, 532CB, 632AT, 632CB
Sub 2 - Page 263 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
575303-02-1
ZONE
587
687
DESCRIPTION
OUTBOARD FLAP TRACK 3 ATTACH AREAS
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
FLAP, FRONT SPAR SPLICES AND ATTACHMENT AREAS AT
TRACK 3, INTERNAL AND EXTERNAL, LH/RH
INTERVALS
SOURCE
T:
6 YE
I:
6 YE
MRB CPCP
T:
6 YE
I:
6 YE
MRB CPCP
T:
6 YE
I:
6 YE
MRB CPCP
TPS
NO
REFERENCES
575300-220-003
NTM 57-53-03
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.75
0.75
0649
1
1
0.75
0.75
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
1
1
0.30
0.30
0649 1130
1200 1379
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
SOURCE:
MRB 575303-02-1
NOTE: INSPECTION IS THROUGH INSPECTION HOLES
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS
TASK 575303-01-1.
PREPARATION: COVER TAPES FROM INSPECTION HOLES REMOVED; LEADING
EDGE PANEL 2 REMOVED; FLAPS EXTENDED;
575303-02-4
587
687
ACCESS PANELS: 532AT, 532CB, 632AT, 632CB
OUTBOARD FLAP TRACK 3 ATTACH AREAS
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
FLAP, FRONT SPAR SPLICES AND ATTACHMENT AREAS AT
TRACK 3, INTERNAL AND EXTERNAL, LH/RH
NO
575300-220-003
NTM 57-53-03
SOURCE:
MRB 575303-02-4
NOTE: INSPECTION IS THROUGH INSPECTION HOLES
PREPARATION: COVER TAPES FROM INSPECTION HOLES REMOVED; FLAPS
EXTENDED;
575305-01-1
587
687
ACCESS PANELS: 532AT, 532CB, 632AT, 632CB
OUTBOARD FLAP TRACK 4 ATTACH AREAS
DETAILED INSPECTION OF OUTBOARD FLAP, FRONT SPAR
SPLICES AND ATTACHMENT AREAS AT TRACK 4, INTERNAL AND
EXTERNAL, LH/RH
NOTE: THIS TASK HAS TO BE PERFORMED THE SAME TIME AS
TASK 575305-02-1.
AF
DET
NO
575300-200-006
SOURCE:
MRB 575305-01-1
PREPARATION: LEADING EDGE PANEL 5 REMOVED; FLAPS EXTENDED;
ACCESS PANELS: 533AT, 533CB, 633AT, 633CB
Sub 2 - Page 264 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
575305-02-1
ZONE
587
687
DESCRIPTION
OUTBOARD FLAP TRACK 4 ATTACH AREAS
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
FLAP, FRONT SPAR SPLICES AND ATTACHMENT AREAS AT
TRACK 4, INTERNAL AND EXTERNAL, LH/RH
INTERVALS
SOURCE
T:
6 YE
I:
6 YE
MRB CPCP
T:
12 YE
I:
12 YE
MRB CPCP
T:
12 YE
I:
12 YE
MRB CPCP
ST:
12 YE
OR
30000 FC
SI:
12 YE
OR
15000 FC
T:
24 YE
I:
12 YE
MRB CPCP
TPS
NO
REFERENCES
575300-220-009
NTM 57-53-05
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.75
0.75
0649 1130
1200 1379
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
1
1
0.30
0.30
ALL
1
1
0.75
0.75
ALL
1
1
1
1
0.30
0.30
0.30
0.30
0649
SOURCE:
MRB 575305-02-1
NOTE: INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575305-01-1.
PREPARATION: COVER TAPES FROM INSPECTION HOLES REMOVED; LEADING
EDGE PANEL 5 REMOVED; FLAPS EXTENDED;
575307-01-1
587
687
ACCESS PANELS: 533AT, 533CB, 633AT, 633CB
OUTBOARD FLAP INBOARD RIB
AF
DET
DETAILED INSPECTION OF OUTBOARD FLAP, INBOARD RIB,
FORWARD SECTION INCLUDING ROLLER, INTERNAL AND
EXTERNAL, LH/RH
NOTE: THIS TASK HAS TO BE PERFORMED THE SAME TIME AS
TASK 575307-02-1.
575307-02-1
587
687
PREPARATION: RUBBER SEALING REMOVED; FLAPS EXTENDED;
OUTBOARD FLAP INBOARD RIB
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
FLAP, INBOARD RIB, FORWARD SECTION INCLUDING ROLLER,
INTERNAL AND EXTERNAL, LH/RH
NO
575300-200-003
SOURCE:
MRB 575307-01-1
NO
575300-220-002
NTM 57-53-07
SOURCE:
MRB 575307-02-1
NOTE: INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575307-01-1.
575309-01-1
532
587
632
687
PREPARATION: COVER TAPES FROM INSPECTION HOLES REMOVED; RUBBER
SEALS; FLAPS EXTENDED;
OUTBOARD FLAP SUPPORT TRACK 3
DETAILED INSPECTION OF OUTBOARD FLAP SUPPORT AT TRACK
3, INCLUDING RIB 5, FITTING ASSEMBLY AND ATTACHMENT
STRUCTURE, INTERNAL AND EXTERNAL, LH/RH
NOTE: THIS TASK HAS TO BE PERFORMED THE SAME TIME AS
TASK 575309-02-1.
PREPARATION: LEADING EDGE PANEL 2; FLAPS EXTENDED;
ACCESS PANELS: 532AT, 532CB, 632AT, 632CB
AF
DET
NO
575300-200-005
SOURCE:
MRB 575309-01-1
Sub 2 - Page 265 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
575309-01-4
ZONE
532
587
632
687
DESCRIPTION
OUTBOARD FLAP SUPPORT TRACK 3
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTBOARD FLAP SUPPORT AT TRACK
3, INCLUDING RIB 5, FITTING ASSEMBLY AND ATTACHMENT
STRUCTURE, INTERNAL AND EXTERNAL, LH/RH
NOTE: THIS TASK HAS TO BE PERFORMED THE SAME TIME AS
TASK 575309-02-4.
INTERVALS
SOURCE
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
ST:
12 YE
OR
30000 FC
SI:
12 YE
OR
15000 FC
T:
24 YE
I:
12 YE
MRB CPCP
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
TPS
NO
REFERENCES
575300-200-005
SOURCE:
MRB 575309-01-4
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
0.30
0.30
0.30
0.30
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
1
1
1
1
0.75
0.75
0.75
0.75
0649
1
1
1
1
0.40
0.40
0.40
0.40
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
PREPARATION: LEADING EDGE PANEL 2 REMOVED; FLAPS EXTENDED;
575309-02-1
532
587
632
687
ACCESS PANELS: 532AT, 532CB, 632AT, 632CB
OUTBOARD FLAP SUPPORT TRACK 3
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
FLAP SUPPORT AT TRACK 3, INCLUDING RIB 5, FITTING
ASSEMBLY AND ATTACHMENT STRUCTURE, INTERNAL AND
EXTERNAL, LH/RH
NOTE: INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575309-01-1.
PREPARATION: COVER TAPES FROM INSPECTION HOLES REMOVED; LEADING
EDGE PANEL 2 REMOVED; FLAPS EXTENDED;
575309-02-4
532
587
632
687
ACCESS PANELS: 532AT, 532CB, 632AT, 632CB
OUTBOARD FLAP SUPPORT TRACK 3
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
FLAP SUPPORT AT TRACK 3, INCLUDING RIB 5, FITTING
ASSEMBLY AND ATTACHMENT STRUCTURE, INTERNAL AND
EXTERNAL, LH/RH
NOTE: INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575309-01-4.
NDT
SDI
NO
575300-220-004
NTM 57-53-09
SOURCE:
MRB 575309-02-1
NO
575300-220-004
NTM 57-53-09
SOURCE:
MRB 575309-02-4
PREPARATION: FLAPS EXTENDED; COVER TAPES FROM INSPECTION HOLES
REMOVED;
ACCESS PANELS: 532AT, 532CB, 632AT, 632CB
Sub 2 - Page 266 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
575311-01-1
ZONE
532
587
632
687
DESCRIPTION
OUTBOARD FLAP TRACK 3 DRIVE LINKAGE
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTBOARD FLAP, DRIVE LINKAGE
AND DRIVE FITTING AT TRACK 3, LH/RH
PREPARATION: FLAPS EXTENDED;
ACCESS PANELS: 532AT, 532CB, 632AT, 632CB
575312-01-1
587
687
OUTBOARD FLAP TRACK 3 INTERNAL SUPPORT
AF
DET
DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL
SUPPORT AT TRACK 3 INCLUDING RIB 6, FITTING AT FRONT
SPAR AND INTERNAL DOUBLER, LH/RH
NOTE: THIS TASK HAS TO BE PERFORMED THE SAME TIME AS
TASK 575312-02-1.
INTERVALS
SOURCE
ST:
12 YE
OR
32000 FC
SI:
12 YE
OR
15000 FC
T:
24 YE
I:
12 YE
ST:
34000 FC
SI:
15000 FC
T:
12 YE
I:
12 YE
MRB CPCP
ST:
34000 FC
SI:
15000 FC
T:
12 YE
I:
12 YE
MRB CPCP
TPS
REFERENCES
575300-200-007
SOURCE:
MRB 575311-01-1
MRB CPCP
NO
575300-200-008
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
0.30
0.30
0.30
0.30
ALL
1
1
0.30
0.30
0649
1
1
0.75
0.75
0649
SOURCE:
MRB 575312-01-1
PREPARATION: LEADING EDGE PANEL 2; FLAPS EXTENDED;
575312-02-1
587
687
ACCESS PANELS: 532AT, 532CB, 632AT, 632CB
OUTBOARD FLAP TRACK 3 INTERNAL SUPPORT
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
FLAP, INTERNAL SUPPORT AT TRACK 3, INCLUDING RIB 6,
FITTING AT FRONT SPAR AND INTERNAL DOUBLER, LH/RH
NOTE: INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575312-01-1.
NDT
SDI
NO
575300-220-005
NTM 57-53-12
SOURCE:
MRB 575312-02-1
PREPARATION: COVER TAPES FROM INSPECTION HOLES REMOVED; LEADING
EDGE PANEL 2 REMOVED; FLAPS EXTENDED;
ACCESS PANELS: 532AT, 532CB, 632AT, 632CB
Sub 2 - Page 267 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
575312-02-4
ZONE
587
687
DESCRIPTION
OUTBOARD FLAP TRACK 3 INTERNAL SUPPORT
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
FLAP, INTERNAL SUPPORT AT TRACK 3, INCLUDING RIB 6,
FITTING AT FRONT SPAR AND INTERNAL DOUBLER, LH/RH
INTERVALS
SOURCE
T:
12 YE
I:
12 YE
MRB CPCP
ST:
30000 FC
SI:
15000 FC
T:
12 YE
I:
12 YE
MRB CPCP
ST:
30000 FC
SI:
15000 FC
T:
12 YE
I:
12 YE
MRB CPCP
TPS
NO
REFERENCES
575300-220-005
NTM 57-53-12
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.75
0.75
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
1
1
1
1
0.10
0.10
0.10
0.10
0649 1130
1200 1379
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
1
1
1
1
0.10
0.10
0.10
0.10
2151 2163
SOURCE:
MRB 575312-02-4
NOTE: INSPECTION IS THROUGH INSPECTION HOLES.
PREPARATION: COVER TAPES FROM INSPECTION HOLES REMOVED; FLAPS
EXTENDED;
575313-01-1
533
587
633
687
ACCESS PANELS: 532AT, 532CB, 632AT, 632CB
OUTBOARD FLAP SUPPORT TRACK 4
AF
DET
DETAILED INSPECTION OF OUTBOARD FLAP, SUPPORT AT
TRACK 4, INCLUDING RIB 14, FITTING ASSEMBLY, PENDULUM
SUPPORT AND ATTACHMENT STRUCTURE, INTERNAL AND
EXTERNAL, LH/RH
NOTE: THIS TASK HAS TO BE PERFORMED THE SAME TIME AS
TASK 575313-02-1.
NO
575300-200-011
SOURCE:
MRB 575313-01-1
PREPARATION: LEADING EDGE PANEL 5 REMOVED; FLAPS EXTENDED;
575313-01-4
533
587
633
687
ACCESS PANELS: 533AT, 533CB, 633AT, 633CB
OUTBOARD FLAP SUPPORT TRACK 4
DETAILED INSPECTION OF OUTBOARD FLAP, SUPPORT AT
TRACK 4, INCLUDING RIB 14, FITTING ASSEMBLY, PENDULUM
SUPPORT AND ATTACHMENT STRUCTURE, INTERNAL AND
EXTERNAL, LH/RH
NOTE: THIS TASK HAS TO BE PERFORMED THE SAME TIME AS
TASK 575313-02-4.
AF
DET
NO
575300-200-011
SOURCE:
MRB 575313-01-4
PREPARATION: FLAPS EXTENDED;
ACCESS PANELS: 533AT, 533CB, 633AT, 633CB
Sub 2 - Page 268 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
575313-02-1
ZONE
533
587
633
687
DESCRIPTION
OUTBOARD FLAP SUPPORT TRACK 4
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
FLAP, SUPPORT AT TRACK 4, INCLUDING RIB 14, FITTING
ASSEMBLY, PENDULUM SUPPORT AND ATTACHMENT STRUCTURE,
INTERNAL AND EXTERNAL, LH/RH
NOTE: INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575313-01-1.
INTERVALS
SOURCE
ST:
30000 FC
SI:
15000 FC
T:
12 YE
I:
12 YE
MRB CPCP
ST:
30000 FC
SI:
15000 FC
T:
12 YE
I:
12 YE
MRB CPCP
ST:
12 YE
OR
32000 FC
SI:
12 YE
OR
15000 FC
T:
24 YE
I:
12 YE
MRB CPCP
TPS
NO
REFERENCES
575300-220-010
NTM 57-53-13
SOURCE:
MRB 575313-02-1
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
0.75
0.75
0.75
0.75
0649 1130
1200 1379
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
1
1
1
1
0.75
0.75
0.75
0.75
2151 2163
1
1
1
1
0.30
0.30
0.30
0.30
0649 1130
1200 1379
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
PREPARATION: COVER TAPES FROM INSPECTION HOLES REMOVED; LEADING
EDGE PANEL 5 REMOVED; FLAPS EXTENDED;
575313-02-4
533
587
633
687
ACCESS PANELS: 533AT, 533CB, 633AT, 633CB
OUTBOARD FLAP SUPPORT TRACK 4
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
FLAP, SUPPORT AT TRACK 4, INCLUDING RIB 14, FITTING
ASSEMBLY, PENDULUM SUPPORT AND ATTACHMENT STRUCTURE,
INTERNAL AND EXTERNAL, LH/RH
NOTE: INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575313-01-4.
NO
575300-220-010
NTM 57-53-13
SOURCE:
MRB 575313-02-4
PREPARATION: COVER TAPES FROM
INSPECTION HOLES
REMOVED;
FLAPS EXTENDED;
575315-01-1
533
587
633
687
ACCESS PANELS: 533AT, 533CB, 633AT, 633CB
OUTBOARD FLAP TRACK 4 DRIVE LINKAGE
DETAILED INSPECTION OF OUTBOARD FLAP, DRIVE LINKAGE
AND DRIVE FITTING AT TRACK 4, LH/RH
PREPARATION: LEADING EDGE PANEL 5 REMOVED; FLAPS EXTENDED;
ACCESS PANELS: 533AT, 533CB, 633AT, 633CB
AF
DET
575300-200-012
SOURCE:
MRB 575315-01-1
Sub 2 - Page 269 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
575315-01-4
ZONE
533
587
633
687
DESCRIPTION
OUTBOARD FLAP TRACK 4 DRIVE LINKAGE
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTBOARD FLAP, DRIVE LINKAGE
AND DRIVE FITTING AT TRACK 4, LH/RH
PREPARATION: FLAPS EXTENDED;
ACCESS PANELS: 533AT, 533CB, 633AT, 633CB
575316-01-1
587
687
OUTBOARD FLAP TRACK 4 INTERNAL SUPPORT
AF
DET
DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL
SUPPORT AT TRACK 4 INCLUDING RIB 15, FITTING AT
FRONT SPAR AND INTERNAL DOUBLER, LH/RH
NOTE: THIS TASK HAS TO BE PERFORMED THE SAME TIME AS
TASK 575316-02-1.
INTERVALS
SOURCE
ST:
12 YE
OR
32000 FC
SI:
12 YE
OR
15000 FC
T:
24 YE
I:
12 YE
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
TPS
REFERENCES
575300-200-012
SOURCE:
MRB 575315-01-4
MRB CPCP
NO
575300-200-013
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
0.30
0.30
0.30
0.30
2151 2163
1
1
0.30
0.30
0649 1130
1200 1379
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
1
1
0.30
0.30
2151 2163
SOURCE:
MRB 575316-01-1
PREPARATION: LEADING EDGE PANEL 5 REMOVED; FLAPS EXTENDED;
575316-01-4
587
687
ACCESS PANELS: 533AT, 533CB, 633AT, 633CB
OUTBOARD FLAP TRACK 4 INTERNAL SUPPORT
DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL
SUPPORT AT TRACK 4, INCLUDING RIB 15, FITTING AT
FRONT SPAR AND INTERNAL DOUBLER, LH/RH
NOTE: THIS TASK HAS TO BE PERFORMED THE SAME TIME AS
TASK 575316-02-4.
AF
DET
NO
575300-200-013
SOURCE:
MRB 575316-01-4
PREPARATION: FLAPS EXTENDED;
ACCESS PANELS: 533AT, 533CB, 633AT, 633CB
Sub 2 - Page 270 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
575316-02-1
ZONE
587
687
DESCRIPTION
OUTBOARD FLAP TRACK 4 INTERNAL SUPPORT
SKILL TASK
CODE CODE
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
FLAP, INTERNAL SUPPORT AT TRACK 4, INCLUDING RIB 15,
FITTING AT FRONT SPAR AND INTERNAL DOUBLER, LH/RH
NOTE: INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575316-01-1.
INTERVALS
SOURCE
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB CPCP
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
ST:
48000 FC
SI:
20000 FC
MRB CPCP
TPS
NO
REFERENCES
575300-220-012
NTM 57-53-16
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.75
0.75
0649 1130
1200 1379
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
1
1
0.75
0.75
2151 2163
1
1
1
1
0.10
0.10
0.10
0.10
ALL
1
1
1
1
1.00
1.00
1.00
1.00
ALL
SOURCE:
MRB 575316-02-1
PREPARATION: COVER TAPES FROM INSPECTION HOLES REMOVED; LEADING
EDGE PANEL 5 REMOVED; FLAPS EXTENDED;
575316-02-4
587
687
ACCESS PANELS: 533AT, 533CB, 633AT, 633CB
OUTBOARD FLAP TRACK 4 INTERNAL SUPPORT
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
FLAP, INTERNAL SUPPORT AT TRACK 4, INCLUDING RIB 15,
FITTING AT FRONT SPAR AND INTERNAL DOUBLER, LH/RH
NOTE: INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575316-01-4.
NO
575300-220-012
NTM 57-53-16
SOURCE:
MRB 575316-02-4
PREPARATION: COVER TAPES FROM
INSPECTION HOLES
REMOVED;
FLAPS EXTENDED;
575350-01-1
532
533
632
633
ACCESS PANELS: 533AT, 533CB, 633AT, 633CB
OUTBOARD FLAP TACK 3-4 CARRIAGE
AF
DET
DETAILED INSPECTION OF OUTER WING OUTBOARD FLAP TRACK
3 AND 4 CARRIAGE FORGINGS
PREPARATION: FLAPS EXTENDED;
575350-02-1
532
533
632
633
OUTBOARD FLAP TACK 3-4 CARRIAGE
SPECIAL DETAILED INSPECTION (US) OF OUTER WING
OUTBOARD FLAP TRACK 3 AND 4 CARRIAGE FORGINGS
NDT
SDI
575300-200-009
SOURCE:
MRB 575350-01-1
MRB
575300-220-006
NTM 57-53-50
SOURCE:
MRB 575350-02-1
PREPARATION: FLAPS EXTENDED;
Sub 2 - Page 271 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
575351-01-1
ZONE
500
600
DESCRIPTION
OUTBOARD FLAP TRACK 3-4 ROLLERS
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF OUTER WING OUTBOARD FLAP TRACK
3 AND 4 CARRIAGE ROLLERS
575352-01-1
575354-01-1
532
533
632
633
532
533
632
633
PREPARATION: FLAPS EXTENDED;
OUTBOARD FLAP TRACK 3-4 BOLT ASSEMBLY
NDT
SDI
SPECIAL DETAILED INSPECTION (MPI) OF OUTER WING
OUTBOARD FLAP TRACK 3 AND 4 FLAP PIVOT BOLT ASSEMBLY.
PREPARATION: INNER BOLT REMOVED; FLAPS EXTENDED;
OUTBOARD FLAP TRACK 3-4 DRIVE LEVERS
AF
DET
DETAILED INSPECTION OF OUTER WING OUTBOARD FLAP TRACK
3 AND 4 DRIVE LEVERS
PREPARATION: FLAPS EXTENDED; SPOILERS EXTENDED;
575354-02-1
575900-01-1
576103-01-1
532
533
632
633
500
600
575
675
OUTBOARD FLAP TRACK3-4 DRIVE LEVERS
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING
OUTBOARD FLAP TRACK 3 AND 4 DRIVE LEVERS
PREPARATION: FLAPS EXTENDED; SPOILERS EXTENDED;
MISCELLANEOUS (DRAINS) FOR
LEADING/TRAILING EDGE AND
LEADING/TRAILING EDGE DEVICES
CHECK OF DRAIN HOLES FOR CLOGGING
AILERON HINGE AND ACTUATOR FITTINGS
DETAILED INSPECTION OF AILERON, HINGE FITTINGS AND
ACTUATOR ATTACHMENT FITTINGS
ACCESS PANELS: 575AT, 575KB, 575LB, 575MB, 675AT, 675KB, 675LB, 675MB
AF
OPC
INTERVALS
SOURCE
ST:
48000 FC
SI:
7500 FC
MRB
ST:
48000 FC
SI:
15000 FC
MRB
ST:
6 YE
SI:
6 YE
T:
24 YE
I:
6 YE
ST:
48000 FC
SI:
20000 FC
MRB CPCP
I:
80 MO
MRB 9
TPS
REFERENCES
575300-200-001
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.10
0.10
ALL
1
1
1
1
1.00
1.00
1.00
1.00
ALL
1
1
1
1
0.15
0.15
0.15
0.15
ALL
1
1
1
1
1.00
1.00
1.00
1.00
ALL
1
1
0.50
0.50
ALL
1
1
0.10
0.10
ALL
SOURCE:
MRB 575351-01-1
575300-220-007
NTM 57-53-52
SOURCE:
MRB 575352-01-1
NO
575300-200-010
SOURCE:
MRB 575354-01-1
MRB
575300-220-008
NTM 57-53-54
SOURCE:
MRB 575354-02-1
575900-200-002
SOURCE:
MRB 57.59.00/01
AF
DET
ST:
30000 FC
SI:
15800 FC
T:
12 YE
OR
38700 FC
I:
12 YE
OR
15800 FC
ALI
MRB CPCP
576000-200-002
SOURCE:
ALI 576103-01-1
MRB 576103-01-1
Sub 2 - Page 272 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
576104-01-1
576106-01-1
ZONE
500
600
500
600
DESCRIPTION
AILERON SKIN ATTACH TO TRAILING EDGE
DETAILED INSPECTION OF AILERON, UPPER AND LOWER
EXTERNAL SKINS AT ATTACHMENT TO TRAILING EDGE,
INBOARD AND OUTBOARD EDGES, SPARS AND RIBS
AILERON UPPER AND LOWER SKINS
SKILL TASK
CODE CODE
AF
AF
DET
DET
DETAILED INSPECTION OF AILERON, UPPER AND LOWER
SKINS, EXTERNAL SURFACE
577001-01-1
500
600
SPOILER 1 FITTING
AF
DET
DETAILED INSPECTION OF SPOILER 1, CENTER HINGE
FITTING AND ACTUATOR BRACKET
NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS
TASK 577001-02-1
577001-01-6
500
600
PREPARATION: FLAPS EXTENDED; SPOILERS EXTENDED;
SPOILER 1 FITTING
AF
DET
DETAILED INSPECTION OF SPOILER 1, CENTER HINGE
FITTING AND ACTUATOR BRACKET
PREPARATION: FLAPS AND SPOILERS EXTENDED;
577001-02-1
500
600
SPOILER 1 FITTING
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC) OF SPOILER 1, ACTUATOR BRACKET.
INTERVALS
SOURCE
T:
12 YE
I:
12 YE
MRB
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
ST:
48000 FC
SI:
20000 FC
MRB
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
ST:
48000 FC
SI:
20000 FC
MRB CPCP
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB
TPS
REFERENCES
576000-200-003
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.50
0.50
ALL
1
1
0.50
0.50
ALL
1
1
0.10
0.10
ALL
1
1
0.10
0.10
ALL
1
1
1.00
1.00
ALL
1
1
0.10
0.10
ALL
SOURCE:
MRB 576104-01-1
576000-210-001
SOURCE:
MRB 576106-01-1
MRB
577100-200-001
SOURCE:
MRB 577001-01-1
577100-200-001
SOURCE:
MRB 577001-01-6
MRB
577100-220-001
NTM 57-70-01
SOURCE:
MRB 577001-02-1
NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 57700101-1
PREPARATION: PINS REMOVED; FLAPS EXTENDED; SPOILERS EXTENDED;
577002-01-1
500
600
SPOILER 1 SKINS OF CENTER FITTING
DETAILED INSPECTION OF SPOILER 1, UPPER AND LOWER
SKINS, IN REGION OF CENTER HINGE FITTING
PREPARATION: FLAPS EXTENDED; SPOILERS EXTENDED;
AF
DET
577100-200-002
SOURCE:
MRB 577002-01-1
Sub 2 - Page 273 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
577003-01-1
ZONE
500
600
DESCRIPTION
SPOILER 1 SKINS AT TRAILING EDGE
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF SPOILER 1, UPPER AND LOWER
SKINS, AT TRAILING EDGE AND INBOARD AND OUTBOARD
EDGES
PREPARATION: SPOILERS EXTENDED;
577006-01-1
500
600
SPOILER 2-5 CENTRE FITTING
AF
DET
DETAILED INSPECTION OF SPOILER 2,3,4 AND 5, CENTER
HINGE FITTINGS
577006-02-1
500
600
PREPARATION: FLAPS EXTENDED; SPOILERS EXTENDED;
SPOILER 2-5 CENTRE FITTING
NDT
SDI
SPECIAL DETAILED INSPECTION (HFEC AND US) OF SPOILER
2, 3, 4 AND 5, CENTER HINGE FITTINGS
577007-01-1
500
600
PREPARATION: PINS REMOVED; FLAPS EXTENDED; SPOILERS EXTENDED;
SPOILER 2-5 SKINS OF CENTER FITTING
AF
DET
DETAILED INSPECTION OF SPOILER 2,3,4 AND 5, UPPER AND
LOWER SKINS IN REGION OF CENTER HINGE FITTING
PREPARATION: FLAPS EXTENDED; SPOILERS EXTENDED;
577008-01-1
500
600
SPOILER 2-5 SKINS AT TRAILING EDGE
AF
DET
DETAILED INSPECTION OF SPOILER 2,3,4 AND 5, UPPER AND
LOWER SKINS AT TRAILING EDGE AND INBOARD AND OUTBOARD
EDGES
PREPARATION: FLAPS EXTENDED; SPOILERS EXTENDED;
577009-01-1
500
600
SPOILERS 1 TO 5 EXTERNAL SURFACE
DETAILED INSPECTION OF SPOILERS 1 TO 5, UPPER AND
LOWER SKINS, EXTERNAL SURFACE
PREPARATION: FLAPS EXTENDED; SPOILERS EXTENDED;
AF
DET
INTERVALS
SOURCE
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
T:
12 YE
I:
12 YE
MRB
ST:
48000 FC
SI:
20000 FC
MRB
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
ST:
12 YE
SI:
12 YE
T:
24 YE
I:
12 YE
MRB
TPS
REFERENCES
577100-200-003
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
ALL
1
1
0.10
0.10
ALL
1
1
2.00
2.00
ALL
1
1
0.10
0.10
ALL
1
1
0.80
0.80
ALL
1
1
0.40
0.40
ALL
SOURCE:
MRB 577003-01-1
MRB CPCP
577200-200-002
SOURCE:
MRB 577006-01-1
577200-200-004
NTM 57-70-06
SOURCE:
MRB 577006-02-1
577500-200-001
SOURCE:
MRB 577007-01-1
MRB
577200-200-003
SOURCE:
MRB 577008-01-1
MRB
577100-210-001
SOURCE:
MRB 577009-01-1
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SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
711000-C1-1
ZONE
430
440
DESCRIPTION
COWLINGS
SKILL TASK
CODE CODE
EN
GVI
GENERAL VISUAL INSPECTION OF AIR INTAKE COWL AFT
BULKHEAD
711000-C4-2
430
440
ACCESS PANELS: 437AL, 438AR, 447AL, 448AR
COWLINGS
EN
GVI
INTERVALS
SOURCE
I:
7500 FH
OR
50 MO
MRB 8
LUR
I:
24 MO
MRB 8
430
440
ACCESS PANELS: 437AL, 438AR, 447AL, 448AR
COWLINGS
430
440
ACCESS PANELS: 437AL, 438AR, 447AL, 448AR
COWLINGS
EN
FNC
430
440
ACCESS PANELS: 437AL, 438AR, 447AL, 448AR
COWLINGS
EN
GVI
EN
GVI
GENERAL VISUAL INSPECTION OF FAN COWL DOOR FIRE SEALS
711300-01-1
711300-C1-1
437
438
447
448
430
440
ACCESS PANELS: 437AL, 438AR, 447AL, 448AR
FAN COWL DOOR HINGE FITTINGS
AF
GVI
GENERAL VISUAL INSPECTION OF FAN COWL DOOR HINGE
FITTINGS
ACCESS PANELS: 437AL, 438AR, 447AL, 448AR
FAN COWLINGS
I:
24 MO
MRB 8
EN
FNC
I:
7500 FH
OR
24 MO
MRB 8
430
440
ACCESS PANELS: 437AL, 438AR, 447AL, 448AR
FAN COWLINGS
DETAILED INSPECTION OF THE KEEPER ASSY FAN COWL
LOCKING DEVICE
1
1
0.05
0.05
ALL
711311-200-804
1
1
0.45
0.45
ALL
711311-280-802
1
1
0.25
0.25
ALL
I:
7500 FH
OR
24 MO
MRB 8
T:
7500 FC
I:
7500 FC
ALI
I:
20 MO
MRB 8
711313-220-802
1
1
0.40
0.40
ALL
1
1
0.42
0.42
ALL
1
1
1
1
0.20
0.20
0.20
0.20
ALL
1
1
0.10
0.10
ALL
1
1
0.15
0.15
ALL
SOURCE:
MRB 71.10.00/06-C5
711311-200-802
SOURCE:
MRB 71.10.00/07-C5
711313-220-040
SOURCE:
ALI 711300-01-1
FUNCTIONAL CHECK OF FAN COWL LATCH TENSION
711300-C2-1
TASKM. APPLICABI
H.
LITY
SOURCE:
MRB 71.10.00/05-C5
GENERAL VISUAL INSPECTION OF FAN COWL LATCHES AND ADJACENT
STRUCTURE
711000-C7-1
711100-210-041
MEN
SOURCE:
MRB 71.10.00/04-C5
FUNCTIONAL CHECK OF PRESSURE RELIEF DOOR LATCH TENSION.
711000-C6-1
REFERENCES
SOURCE:
MRB 71.10.00/01-C5
GENERAL VISUAL INSPECTION OF FAN COWL DOORS
711000-C5-1
TPS
711300-800-042
SOURCE:
MRB 71.10.00/08-C5
EN
DET
I:
1500 FC
OR
24 MO
MRB 9
LUR
711313-220-041
AOT 71-A1024
SOURCE:
MRB 71.10.00/09-C5
ACCESS PANELS: 437AL, 438AR, 447AL, 448AR
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SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
712111-01-1
712111-02-1
ZONE
DESCRIPTION
435
436
445
446
451
461
FORWARD ENGINE MOUNT
435
436
445
446
451
461
FORWARD ENGINE MOUNT
SKILL TASK
CODE CODE
EN
DET
DETAILED INSPECTION OF FORWARD ENGINE MOUNT
INSTALLATION
ACCESS PANELS: 437AL, 438AR, 447AL, 448AR, 451AL, 452AR, 461AL, 462AR
EN
DET
DETAILED INSPECTION OF FORWARD ENGINE MOUNT
INSTALLATION
NOTE: ACCOMPLISHMENT OF THIS INSPECTION TO BE
PERFORMED WITH A MAXIMUM INTERVAL OF 12 YEARS
BETWEEN MOUNT DISASSEMBLY
INTERVALS
SOURCE
T:
7500 FC
OR
15000 FH
I:
7500 FC
OR
15000 FH
T:
12 YE
I:
12 YE
NOTE
ALI
T:
7500 FC
OR
15000 FH
I:
7500 FC
OR
15000 FH
T:
7500 FC
OR
15000 FH
I:
7500 FC
OR
15000 FH
T:
12 YE
I:
12 YE
NOTE
ALI
TPS
REFERENCES
712111-210-040
SOURCE:
ALI 712111-01-1
MRB CPCP
NO
712111-210-042
SOURCE:
MRB 712111-02-1
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
1
1
0.10
0.10
0.10
0.10
0.10
0.10
ALL
1
1
1
1
1
1
0.50
0.50
0.50
0.50
0.50
0.50
ALL
1
1
0.58
0.58
ALL
1
1
0.55
0.55
ALL
1
1
1
1
1
1
0.50
0.50
0.50
0.50
0.50
0.50
ALL
PREPARATION: ENGINE MOUNT DISASSEMBLED; ENGINE REMOVED;
ACCESS PANELS: 437AL, 438AR, 447AL, 448AR, 451AL, 452AR, 461AL, 462AR
712111-05-4
450
460
FORWARD ENGINE MOUNT
AF
SDI
SPECIAL DETAILED INSPECTION (TC) OF FORWARD ENGINE MOUNT PYLON
BOLTS
ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR
712112-01-1
450
460
FORWARD ENGINE MOUNT
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF FORWARD
ENGINE MOUNT LINK LUGS
ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR
712211-01-1
451
453
454
461
463
464
AFT ENGINE MOUNT
DETAILED INSPECTION OF AFT ENGINE MOUNT INSTALLATION
NOTE: ACCOMPLISHMENT OF THIS INSPECTION TO BE
PERFORMED WITH A MAXIMUM INTERVAL OF 12 YEARS
BETWEEN MOUNT DISASSEMBLY
EN
DET
712111-210-803
SOURCE:
ALI 712111-05-4
ALI
712112-200-803
SOURCE:
ALI 712112-01-1
MRB CPCP
NO
712211-210-040
SOURCE:
MRB 712211-01-1
PREPARATION: ENGINE MOUNT DISASSEMBLED; ENGINE REMOVED;
ACCESS PANELS: 451AL, 437AL, 438AR, 452AR, 461AL, 447AL, 448AR, 462AR
Sub 2 - Page 276 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
712211-03-1
712211-05-1
ZONE
DESCRIPTION
451
453
454
461
463
464
AFT ENGINE MOUNT
450
460
AFT ENGINE MOUNT
SKILL TASK
CODE CODE
EN
DET
DETAILED INSPECTION OF AFT ENGINE MOUNT INSTALLATION
ACCESS PANELS: 451AL, 437AL, 438AR, 452AR, 461AL, 447AL, 448AR, 462AR
AF
SDI
SPECIAL DETAILED INSPECTION (TC) OF AFT ENGINE MOUNT PYLON BOLTS
ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR
712212-01-1
450
460
AFT ENGINE MOUNT
NDT
SDI
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF AFT ENGINE MOUNT LINK
LUGS
ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR
712213-01-1
450
460
AFT ENGINE MOUNT
EN
DET
DETAILED INSPECTION OF AFT ENGINE MOUNT PINS
ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR
722000-C1-1
430
440
FAN SECTION
EN
DET
DETAILED INSPECTION OF ENGINE INLET, FAN BLADES, FAN
OUTLET AND ABRADABLE MATERIAL
722000-C2-1
430
440
ACCESS PANELS: 437AL, 438AR, 447AL, 448AR
FAN SECTION
DETAILED INSPECTION AND RELUBRICATION OF FAN BLADE
DOVETAILS, MIDSPAN SHROUDS, RETAINERS, SPACERS,
DAMPERS AND FAN DISC DOVETAIL SLOTS
EN
DET
INTERVALS
SOURCE
T:
7500 FC
OR
15000 FH
I:
7500 FC
OR
15000 FH
T:
7500 FC
OR
15000 FH
I:
7500 FC
OR
15000 FH
T:
7500 FC
OR
15000 FH
I:
7500 FC
OR
15000 FH
T:
7500 FC
OR
15000 FH
I:
7500 FC
OR
15000 FH
I:
1500 FC
OR
24 MO
ALI
I:
3000 FC
OR
48 MO
MRB 6
LUR
TPS
REFERENCES
712211-210-042
SOURCE:
ALI 712211-03-1
ALI
712211-210-803
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
1
1
0.10
0.10
0.10
0.10
0.10
0.10
ALL
1
1
0.50
0.50
ALL
0.63
0.63
TBD
TBD
ALL
1
1
0.80
0.80
ALL
1
1
0.30
0.30
ALL
1
1
3.00
3.00
ALL
SOURCE:
ALI 712211-05-1
ALI
712212-210-802
SOURCE:
ALI 712212-01-1
ALI
712211-210-802
SOURCE:
ALI 712213-01-1
MRB 6
LUR
722300-210-003
SOURCE:
MRB 72.20.00/01-C5
722100-210-004
SOURCE:
MRB 72.20.00/06-C5
PREPARATION: FAN BLADES REMOVED;
Sub 2 - Page 277 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
725000-C1-1
ZONE
450
460
DESCRIPTION
TURBINE SECTION
SKILL TASK
CODE CODE
EN
SDI
BORESCOPE INSPECTION OF HPT BLADES (FROM THE FRONT
AND THE REAR)
INTERVALS
SOURCE
I:
1600 FC
OR
72 MO
MRB 6
LUR
TPS
REFERENCES
725200-290-001
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.60
0.60
0649
SOURCE:
MRB 72.50.00/01-C5
ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR
730000-C2-1
731111-C1-1
210
435
445
ENGINE FUEL & CONTROL-GENERAL
EN
OPC
I:
1200 FH
SIL
732160-740-028
SIL 73-017
1
0.10
ALL
CORRECT FAULTS OF THE ENGINE SCHEDULED MAINTENANCE
REPORT (SMR).
HOSE - MAIN FUEL SUPPLY
EN
DET
T:
2000 FH
I:
1200 FH
NOTE
VSB
VSB RA32073-5
1
1
0.70
0.70
0649
ACCESS PANELS: 437AL, 438AR, 447AL, 448AR
FUNCTIONAL INTERFACES
EN
DET
I:
30000 FH
SIL
732900-710-042
SIL 73-022
1
0.20
ALL
CHECK FOR ERRONEOUS SIGNAL POSITIONS TO THE
ZONES CONTROLLER FROM THE BLEED AND WING/
NACELLE ANTI-ICE VALVES WITH ENGINES, APU
AND PACKS OPERATING
HOT EXHAUST
EN
GVI
I:
6000 FH
OR
60 MO
MRB 8
LUR
781111-210-043
1
1
0.10
0.10
ALL
I:
7500 FH
OR
50 MO
MRB 9
LUR
1
1
0.20
0.20
ALL
I:
24 MO
MRB 8
1
1
0.20
0.20
ALL
CARRY OUT LEAK CHECK OF ENGINE MAIN FUEL FEED HOSE
NOTE :
- IT IS RECOMMENDED TO REPLACE HOSES THAT ARE OLDER
THAN 6 YEARS SINCE MANUFACTURE
- REPLACEMENT BY TEFLON HOSE P/N FOR THIS TASK
AE707422-2 IS TERMINATING ACTION
732500-C1-1
781100-C2-1
210
450
460
GENERAL VISUAL INSPECTION OF INNER AND OUTER SEALS
783000-C2-1
450
460
ACCESS PANELS: 451AL, 452AR, 461AL, 462AR
THRUST REVERSER
EN
GVI
GENERAL VISUAL INSPECTION OF BLOCKER DOOR SEALS
(BLOCKER DOORS DEPLOYED)
783000-C4-1
450
460
PREPARATION: BLOCKER DOORS DEPLOYMENT;
THRUST REVERSER
GENERAL VISUAL INSPECTION OF THRUST REVERSER HALF
TENSION HOOK LATCH AND ADJACENT STRUCTURE (C DUCTS
OPEN)
EN
GVI
SOURCE:
MRB 78.11.00/02-C5
783241-210-042
SOURCE:
MRB 78.30.00/03-C5
783641-210-040
SOURCE:
MRB 78.30.00/04-C5
Sub 2 - Page 278 of 305
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SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
783000-C8-1
783001-01-1
ZONE
450
460
451
452
461
462
DESCRIPTION
THRUST REVERSER
GENERAL VISUAL INSPECTION OF INNER BARREL HEATSHIELD,
FIRE PROTECTIVE COATING AND FIRE SEALS (C DUCTS OPEN)
THRUST REV 12 O´CLOCK BEAM JUNCTION
SKILL TASK
CODE CODE
EN
AF
GVI
DET
DETAILED INSPECTION OF THRUST REVERSER 12 O´CLOCK
BEAM JUNCTION WITH THE FORWARD FRAME
PREPARATION: HEAT SHIELDS REMOVED; THRUST REVERSERS REMOVED;
ACCESS PANELS: 437AL, 451AL, 438AR, 452AR, 447AL, 461AL, 448AR, 462AR
783002-01-1
451
452
461
462
THRUST REVERSER FORWARD FRAME
AF
DET
DETAILED INSPECTION OF THRUST REVERSER FORWARD FRAME
TO 6 O´CLOCK BEAM JOINT
PREPARATION: CUT CORNERS REMOVED;
ACCESS PANELS: 437AL, 451AL, 438AR, 452AR, 447AL, 461AL, 448AR, 462AR
783003-01-1
451
452
461
462
THRUST REVERSER FORWARD FRAME
AF
DET
DETAILED INSPECTION OF THRUST REVERSER FORWARD FRAME
TO 3/9 O´CLOCK BEAM JOINT
PREPARATION: HEAT SHIELDS REMOVED; BRACKETS AND PIPES REMOVED;
ACCESS PANELS: 437AL, 451AL, 438AR, 452AR, 447AL, 461AL, 448AR, 462AR
783004-01-1
451
452
461
462
THRUST REVERSER FORWARD FRAME
SPECIAL DETAILED INSPECTION (HFEC) OF THRUST REVERSER
FORWARD FRAME AT ACTUATOR ATTACHMENT
NDT
SDI
INTERVALS
SOURCE
I:
7500 FH
OR
50 MO
T:
10 YE
OR
24000 FC
I:
10 YE
OR
12000 FC
MRB 8
LUR
T:
10 YE
OR
24000 FC
I:
10 YE
OR
12000 FC
ALI
MRB CPCP
T:
10 YE
OR
24000 FC
I:
10 YE
OR
12000 FC
ALI
MRB CPCP
T:
24000 FC
I:
12000 FC
ALI
ALI
MRB CPCP
TPS
REFERENCES
783211-220-040
SOURCE:
MRB 78.30.00/08-C5
1+2 783200-210-044
SOURCE:
ALI 783001-01-1
MRB 783001-01-1
1+2 783200-210-041
SOURCE:
ALI 783002-01-1
MRB 783002-01-1
1+2 783200-210-042
SOURCE:
ALI 783003-01-1
MRB 783003-01-1
783200-210-043
SOURCE:
ALI 783004-01-1
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
ALL
1
1
1
1
0.20
0.20
0.20
0.20
ALL
1
1
1
1
0.20
0.20
0.20
0.20
ALL
1
1
1
1
0.20
0.20
0.20
0.20
ALL
1
1
1
1
TBD
TBD
TBD
TBD
ALL
PREPARATION: ACTUATORS REMOVED;
ACCESS PANELS: 437AL, 451AL, 438AR, 452AR, 447AL, 461AL, 448AR, 462AR
Sub 2 - Page 279 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
783004-02-1
ZONE
451
452
461
462
DESCRIPTION
THRUST REVERSER FORWARD FRAME
SKILL TASK
CODE CODE
AF
DET
DETAILED INSPECTION OF THRUST REVERSER FORWARD FRAME
AT ACTUATOR ATTACHMENT
INTERVALS
SOURCE
T:
10 YE
I:
10 YE
MRB CPCP
I:
7500 FH
OR
24 MO
MRB 6
I:
5000 FC
OR
60 MO
MRB 8
LUR
I:
6000 FH
OR
40 MO
MRB 6
LUR
T:
7500 FC
I:
7500 FC
ALI
I:
600 FH
OR
6 MO
MRB 9
LUR
TPS
REFERENCES
1+2 783200-210-046
SOURCE:
MRB 783004-02-1
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
0.20
0.20
0.20
0.20
ALL
1
1
1
1
0.08
0.08
0.08
0.08
ALL
1
1
0.20
0.20
ALL
1
1
1
1
0.15
0.15
0.15
0.15
ALL
1
1
1
1
0.15
0.15
0.15
0.15
ALL
1
1
0.10
0.10
0649
PREPARATION: ACTUATORS REMOVED;
ACCESS PANELS: 437AL, 451AL, 438AR, 452AR, 447AL, 461AL, 448AR, 462AR
783100-C5-1
437
438
447
448
THRUST REVERSER CONTROL AND INDICATING
EN
DET
DETAILED INSPECTION OF ACTUATOR ROD END ATTACHMENTS
(BLOCKER DOORS DEPLOYED)
783141-210-042
SOURCE:
MRB 78.30.00/09-C5
MRB 78.31.00/06-C5
PREPARATION: BLOCKER DOORS DEPLOYMENT;
ACCESS PANELS: 437AL, 451AL, 452AR, 438AR, 447AL, 461AL, 462AR, 448AR
783100-C6-1
450
460
THRUST REVERSER CONTROL AND INDICATING
EN
OPC
OPERATIONAL CHECK OF ACTUATOR SECONDARY LOCK MECHANISM
783100-C7-1
437
438
447
448
ACCESS PANELS: 437AL, 438AR, 447AL, 448AR
THRUST REVERSER CONTROL AND INDICATING
EN
GVI
GENERAL VISUAL INSPECTION OF PRIMARY LATCH MECHANISM
(BLOCKER DOORS DEPLOYED)
783141-720-040
SOURCE:
MRB 78.31.00/03-C5
783100-210-041
SOURCE:
MRB 78.30.00/02-C5
MRB 78.31.00/04-C5
PREPARATION: BLOCKER DOORS DEPLOYMENT;
783200-01-1
451
452
461
462
ACCESS PANELS: 437AL, 438AR, 447AL, 448AR
"C" DUCT HINGE FITTING
AF
GVI
GENERAL VISUAL INSPECTION OF "C" DUCT HINGE FITTINGS
783200-210-045
SOURCE:
ALI 783200-01-1
PREPARATION: UPPER HINGE ACCESS FAIRING;
ACCESS PANELS: 437AL, 451AL, 438AR, 452AR, 447AL, 461AL, 448AR, 462AR
792000-C1-1
435
445
DISTRIBUTION
CHECK SUPPLY AND SCAVENGE FILTERS CLOGGING INDICATOR POSITION
EN
VCK
792110-210-001
SOURCE:
MRB 79.20.00/01-C5
ACCESS PANELS: 437AL, 447AL
Sub 2 - Page 280 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
792000-C2-1
ZONE
435
445
DESCRIPTION
DISTRIBUTION
SKILL TASK
CODE CODE
EN
DET
CHECK THE FOLLOWING MAGNETIC PLUG AND SCREENS :
- ACCESSORY GEARBOX SCAVENGE
- AFT SUMP SCAVENGE
792000-C3-1
435
445
ACCESS PANELS: 437AL, 447AL
DISTRIBUTION
EN
DIS
REMOVE AND DISCARD SCAVENGE FILTER
792000-C4-1
435
445
ACCESS PANELS: 437AL, 447AL
DISTRIBUTION
EN
DIS
REMOVE AND DISCARD SUPPLY FILTER
792000-C5-1
435
445
ACCESS PANELS: 437AL, 447AL
DISTRIBUTION
EN
DET
INTERVALS
SOURCE
I:
600 FH
OR
6 MO
MRB 6,9
LUR
I:
4000 FH
OR
36 MO
MRB 6
LUR
I:
4000 FH
OR
36 MO
MRB 9
LUR
I:
600 FH
CN
MRB 6,9
VSB
LUR
CHECK THE FORWARD SUMP SCAVENGE MAGNETIC PLUG AND
SCREEN
TPS
REFERENCES
792110-210-003
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.10
0.10
0649
1
1
0.30
0.30
0649
1
1
0.30
0.30
0649
1
1
0.10
0.10
0649
1
1
0.10
0.10
0649
1
1
0.30
0.30
ALL
1
1
0.20
0.20
ALL
1
1
0.30
0.30
ALL
SOURCE:
MRB 79.20.00/02-C5
792110-920-001
SOURCE:
MRB 79.20.00/03-C5
792110-920-002
SOURCE:
MRB 79.20.00/04-C5
792110-210-004
CN
1989-181(B)R3
VSB CFM56-5A
72-A118
ACCESS PANELS: 437AL, 447AL
792000-C6-1
435
445
DISTRIBUTION
EN
DET
I:
600 FH
CHECK THE TRANSFER GEARBOX SCAVENGE MAGNETIC PLUG
AND SCREEN.
801110-C1-1
436
446
STARTER
EN
DET
CHECK CHIP DETECTOR
801110-C2-1
436
446
ACCESS PANELS: 438AR, 448AR
STARTER
EN
SVC
REPLENISH OIL SYSTEM
801110-C3-1
436
446
ACCESS PANELS: 438AR, 448AR
STARTER
DRAIN AND REPLENISH OIL SYSTEM
EN
SVC
MRB 6,9
VSB
LUR
I:
600 FH
OR
6 MO
MRB 6,9
LUR
I:
600 FH
OR
6 MO
MRB 6,9
LUR
I:
1200 FH
OR
12 MO
MRB 6,9
LUR
SOURCE:
MRB 79.20.00/02-C5
792110-210-005
VSB CFM56-5A
72-0326
SOURCE:
MRB 79.20.00/02-C5
801110-210-001
SOURCE:
MRB 80.10.00/01-C5
121380-610-002
SOURCE:
MRB 80.10.00/02-C5
121380-610-001
SOURCE:
MRB 80.10.00/03-C5
ACCESS PANELS: 438AR, 448AR
Sub 2 - Page 281 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
ZL-100-02-1
ZONE
100
DESCRIPTION
LOWER HALF OF FUSELAGE
SKILL TASK
CODE CODE
AF
GVI
INTERVALS
I:
4 MO
SOURCE
110
RADOME
AF
GVI
I:
48 MO
121
122
ACCESS PANELS: 110AL
AVIONIC COMPARTMENT
121
122
ACCESS PANELS: 811
AVIONIC COMPARTMENT
TASKM. APPLICABI
H.
LITY
1
0.20
ALL
MRB
SOURCE:
MRB ZL-100-02-1
052110-200-001
1
0.10
ALL
1
1
0.10
0.10
ALL
1
1
0.30
0.30
ALL
1
0.20
ALL
1
1
1
0.20
0.20
0.20
1130 1200
1379 1578
1657 1767
2151 2163
1
1
1
0.20
0.20
0.20
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
MRB ZL-110-01-1
AF
GVI
I:
24 MO
MRB
GENERAL VISUAL INSPECTION OF AVIONIC COMPARTMENT (EWIS)
ZL-121-02-1
MEN
052100-200-002
GENERAL VISUAL INSPECTION OF RADOME (EWIS)
ZL-121-01-1
REFERENCES
MRB
GENERAL VISUAL INSPECTION OF LOWER HALF OF FUSELAGE
ZL-110-01-1
TPS
052120-200-001
SOURCE:
MRB ZL-121-01-1
AF
GVI
I:
6 YE
MRB
GENERAL VISUAL INSPECTION OF AVIONIC
COMPARTMENT (EWIS)
052120-200-007
SOURCE:
MRB ZL-121-02-1
PREPARATION: INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE
THE REQUIRED INSPECTION;
ZL-123-02-1
123
ACCESS PANELS: 121AF, 121AL, 121BF, 121CF, 811, 122BF
NOSE LANDING GEAR WELL
AF
GVI
I:
4 MO
MRB
GENERAL VISUAL INSPECTION OF NOSE GEAR WELL (EWIS)
ZL-125-01-1
125
126
129
ACCESS PANELS: 713, 714
LATERAL AVIONIC COMPARTMENT
052120-200-012
SOURCE:
MRB ZL-123-02-1
AF
GVI
GENERAL VISUAL INSPECTION OF LATERAL AVIONIC
COMPARTMENT (EWIS)
I:
24 MO
OR
7500 FH
MRB
I:
24 MO
MRB
052120-200-003
SOURCE:
MRB ZL-125-01-1
PREPARATION: 813 IF INSTALLED;
ZL-125-01-2
125
126
129
ACCESS PANELS: 125AL, 812, 822
LATERAL AVIONIC COMPARTMENT
GENERAL VISUAL INSPECTION OF LATERAL AVIONIC
COMPARTMENT (EWIS)
AF
GVI
052120-200-003
SOURCE:
MRB ZL-125-01-2
PREPARATION: 813 IF INSTALLED;
ACCESS PANELS: 125AL, 812, 822
Sub 2 - Page 282 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
ZL-125-02-1
ZONE
125
126
DESCRIPTION
LATERAL AVIONIC COMPARTMENT
SKILL TASK
CODE CODE
AF
GVI
GENERAL VISUAL INSPECTION OF LATERAL AVIONIC
COMPARTMENT (EWIS)
INTERVALS
SOURCE
I:
6 YE
OR
24000 FH
MRB
I:
24 MO
MRB
TPS
REFERENCES
052120-200-008
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
ALL
1
1
0.10
0.10
ALL
1
1
0.30
0.30
ALL
1
1
0.10
0.10
1
1
0.10
0.10
0649 1130
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
1200 1379
2151 2163
1
1
0.20
0.20
SOURCE:
MRB ZL-125-02-1
PREPARATION: INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE
THE REQUIRED INSPECTION; 813 IF INSTALLED;
ZL-127-01-1
127
128
ACCESS PANELS: 812, 831, 822, 824
REAR AVIONIC COMPARTMENT
AF
GVI
GENERAL VISUAL INSPECTION OF REAR AVIONIC
COMPARTMENT (EWIS)
ZL-127-02-2
127
128
ACCESS PANELS: 824
REAR AVIONIC COMPARTMENT
052120-200-005
SOURCE:
MRB ZL-127-01-1
AF
GVI
I:
6 YE
MRB
GENERAL VISUAL INSPECTION OF REAR AVIONIC
COMPARTMENT (EWIS)
052120-200-010
SOURCE:
MRB ZL-127-02-2
PREPARATION: INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE
THE REQUIRED INSPECTION;
ZL-131-01-1
131
132
ACCESS PANELS: 127BF, 127BG, 127CF, 127DF, 131AW, 131BW, 131CW, 131DW,
825, 128CF, 128EG, 132BW, 132EW, 824
FORWARD CARGO COMPARTMENT
AF
GVI
GENERAL VISUAL INSPECTION OF FORWARD CARGO
COMPARTMENT (AS FAR AS VISIBLE, IF ACT(S)
INSTALLED) (EWIS)
ZL-131-01-2
131
132
ACCESS PANELS: 825
FORWARD CARGO COMPARTMENT
AF
GVI
GENERAL VISUAL INSPECTION OF FORWARD CARGO COMPARTMENT(AS FAR
AS VISIBLE IF ACT(S) INSTALLED) (EWIS)
ZL-131-02-1
131
132
ACCESS PANELS: 825
FORWARD CARGO COMPARTMENT
GENERAL VISUAL INSPECTION OF FORWARD CARGO
COMPARTMENT (EWIS)
AF
GVI
I:
4 MO
OR
750 FH
OR
750 FC
MRB
I:
4 MO
OR
750 FH
OR
750 FC
I:
6 YE
OR
24000 FH
MRB
052130-200-001
SOURCE:
MRB ZL-131-01-1
052130-200-001
SOURCE:
MRB ZL-131-01-2
MRB
052130-200-004
SOURCE:
MRB ZL-131-02-1
1130 1200
1379 1578
1657 1767
2151 2163
ACCESS PANELS: 131AC, 131BC, 131FF, 131GF, 131GW, 131HW, 131JF, 131KF,
131MW, 132FF, 132GF, 132JF, 132MW, 825
Sub 2 - Page 283 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
ZL-131-02-3
ZONE
131
132
DESCRIPTION
FORWARD CARGO COMPARTMENT
SKILL TASK
CODE CODE
AF
GVI
GENERAL VISUAL INSPECTION OF FORWARD CARGO
COMPARTMENT (EWIS)
INTERVALS
SOURCE
I:
6 YE
OR
24000 FH
MRB
I:
12 YE
MRB
TPS
REFERENCES
052130-200-004
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.30
0.30
ALL
1
1
0.25
0.25
0649 1130
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
1
1
0.25
0.25
1200 1379
2151 2163
SOURCE:
MRB ZL-131-02-3
PREPARATION: ACT(S) REMOVED (IF INSTALLED);
ZL-131-03-1
131
132
ACCESS PANELS: 131DG, 131EG, 131GW, 131HW, 131NC, 131SW, 132DG, 132EG,
132SW, 825
FORWARD CARGO COMPARTMENT
AF
GVI
GENERAL VISUAL INSPECTION OF FORWARD CARGO
COMPARTMENT (EWIS)
052130-200-006
SOURCE:
MRB ZL-131-03-1
PREPARATION: ACT(S) REMOVED (IF INSTALLED); CEILING PANELS FROM FR 24
TO FR 34; INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE
REQUIRED INSPECTION; SIDEWALL PANELS FROM FR 24 TO FR 34;
ACCESS PANELS: 825
ZL-133-01-1
133
134
UNDERFLOOR BAY OF FWD CARGO COMPARTMENT
AF
GVI
GENERAL VISUAL INSPECTION OF UNDERFLOOR BAY OF FWD
CARGO COMPARTMENT (EWIS)
I:
6 YE
OR
24000 FH
MRB
I:
6 YE
OR
24000 FH
MRB
052130-200-002
SOURCE:
MRB ZL-133-01-1
PREPARATION: FLOOR PANELS FROM FR 24 TO FR 34;
ZL-133-01-6
133
134
ACCESS PANELS: 133AL, 825, 134AR
UNDERFLOOR BAY OF FWD CARGO COMPARTMENT
GENERAL VISUAL INSPECTION OF UNDERFLOOR BAY OF FWD CARGO
COMPARTMENT (EWIS)
AF
GVI
052130-200-002
SOURCE:
MRB ZL-133-01-6
PREPARATION: ACT(S) REMOVED (IF
INSTALLED);
FLOOR PANELS FROM FR 24 TO FR 34;
ACCESS PANELS: 133AL, 825, 134AR
Sub 2 - Page 284 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
ZL-137-01-1
ZONE
137
138
DESCRIPTION
BAY BEHIND FWD CARGO COMPARTMENT
SKILL TASK
CODE CODE
AF
GVI
GENERAL VISUAL INSPECTION OF BAY BEHIND FWD CARGO
COMPARTMENT (EWIS)
INTERVALS
SOURCE
I:
6 YE
OR
24000 FH
MRB
I:
12 YE
MRB
TPS
REFERENCES
052130-200-003
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
ALL
1
1
0.30
0.30
ALL
2
2
0.50
0.50
ALL
1
1
0.10
0.10
ALL
1
1
0.20
0.20
ALL
1
1
0.10
0.10
ALL
SOURCE:
MRB ZL-137-01-1
PREPARATION: ACT(S) NO.4 AND NO.6 REMOVED (IF INSTALLED); INSULATION
TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION;
ACCESS PANELS: 131NW, 131PW, 825, 132PW
ZL-141-01-1
141
142
CENTER WING BOX
AF
GVI
GENERAL VISUAL INSPECTION OF CENTER WING BOX (EWIS)
ZL-145-01-1
145
146
ACCESS PANELS: 147AZ, 734, 148AZ, 744
ZONE UNDER CABIN FLOOR
052140-200-001
SOURCE:
MRB ZL-141-01-1
AF
GVI
I:
6 YE
MRB
GENERAL VISUAL INSPECTION OF ZONE UNDER CABIN FLOOR
(EWIS)
052140-200-002
SOURCE:
MRB ZL-145-01-1
PREPARATION: FLOOR PANELS FROM FR 36 TO FR 46; INSULATION TO BE
DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION;
ZL-147-02-1
147
148
ACCESS PANELS: 832, 842
MLG-WELL AND HYDRAULIC COMPARTMENT
AF
GVI
I:
4 MO
MRB
GENERAL VISUAL INSPECTION OF MLG-WELL AND HYDRAULIC
COMPARTMENT (EWIS)
ZL-147-03-1
147
148
ACCESS PANELS: 734, 744
MLG-WELL AND HYDRAULIC COMPARTMENT
SOURCE:
MRB ZL-147-02-1
AF
GVI
GENERAL VISUAL INSPECTION OF MLG-WELL AND HYDRAULIC
COMPARTMENT (EWIS)
ZL-151-01-1
151
152
ACCESS PANELS: 147AB, 734, 147EB, 744
AFT CARGO COMPARTMENT
GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT
(AS FAR AS VISIBLE, IF ACT IS INSTALLED) (EWIS)
ACCESS PANELS: 826
052140-200-004
AF
GVI
I:
6 YE
OR
24000 FH
MRB
I:
4 MO
OR
750 FH
OR
750 FC
MRB
052140-200-005
SOURCE:
MRB ZL-147-03-1
052150-200-001
SOURCE:
MRB ZL-151-01-1
Sub 2 - Page 285 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
ZL-151-02-3
ZONE
151
152
DESCRIPTION
AFT CARGO COMPARTMENT
SKILL TASK
CODE CODE
AF
GVI
GENERAL VISUAL INSPECTION OF AFT CARGO
COMPARTMENT (EWIS)
INTERVALS
SOURCE
I:
6 YE
OR
24000 FH
MRB
I:
6 YE
OR
24000 FH
MRB
I:
12 YE
MRB
TPS
REFERENCES
052150-200-003
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.25
0.25
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.25
0.25
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.20
0.20
ALL
1
1
0.20
0.20
ALL
1
1
0.10
0.10
ALL
SOURCE:
MRB ZL-151-02-3
PREPARATION: ACT(S) REMOVED (IF INSTALLED);
ZL-151-02-5
151
152
ACCESS PANELS: 151AC, 151AW, 151BW, 151CW, 151DW, 151EW, 151GC,
151HW, 151JW, 152BW, 152CW, 152DW, 152FW, 152GW, 152HW, 152JW, 826
AFT CARGO COMPARTMENT
AF
GVI
GENERAL VISUAL INSPECTION OF AFT CARGO
COMPARTMENT (EWIS)
052150-200-003
SOURCE:
MRB ZL-151-02-5
PREPARATION: ACT(S) REMOVED (IF INSTALLED);
ZL-151-03-7
151
152
ACCESS PANELS: 151BW, 151EC, 151GC, 151TW, 151UW, 152BW, 152FW,
152GW, 152SW, 152TW, 826
AFT CARGO COMPARTMENT
AF
GVI
GENERAL VISUAL INSPECTION OF AFT CARGO
COMPARTMENT (EWIS)
052150-200-004
SOURCE:
MRB ZL-151-03-7
PREPARATION: CEILING PANELS FROM FR 46 TO FR 59; INSULATION TO BE
DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION;
SIDEWALL PANELS FROM FR 46 TO FR 59; ACT(S) REMOVED (IF INSTALLED);
ACCESS PANELS: 826
ZL-153-01-1
153
154
UNDERFLOOR BAY OF AFT CARGO COMPTMENT
AF
GVI
GENERAL VISUAL INSPECTION OF UNDERFLOOR BAY OF AFT
CARGO COMPARTMENT (EWIS)
I:
6 YE
OR
24000 FH
MRB
I:
4 MO
OR
750 FH
MRB
052150-200-002
SOURCE:
MRB ZL-153-01-1
PREPARATION: FLOOR PANELS FROM FR 46 TO FR 59; ACT(S) REMOVED (IF
INSTALLED);
ZL-161-01-1
161
162
ACCESS PANELS: 826
BULK CARGO COMPARTMENT
GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT
(AS FAR AS VISIBLE, IF ACT IS INSTALLED) (EWIS)
AF
GVI
052160-200-001
SOURCE:
MRB ZL-161-01-1
ACCESS PANELS: 826
Sub 2 - Page 286 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
ZL-161-02-1
ZONE
161
162
DESCRIPTION
BULK CARGO COMPARTMENT
SKILL TASK
CODE CODE
AF
GVI
GENERAL VISUAL INSPECTION OF BULK CARGO
COMPARTMENT (EWIS)
INTERVALS
SOURCE
I:
6 YE
OR
24000 FH
MRB
I:
12 YE
MRB
TPS
REFERENCES
052160-200-003
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
ALL
1
1
0.20
0.20
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.20
0.20
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.30
0.30
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.30
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890
SOURCE:
MRB ZL-161-02-1
PREPARATION: ACT(S) REMOVED (IF INSTALLED);
ACCESS PANELS: 161AC, 161AW, 161BW, 161CW, 162BW, 162CW, 162EW, 826
ZL-161-03-1
161
162
BULK CARGO COMPARTMENT
AF
GVI
GENERAL VISUAL INSPECTION OF BULK CARGO
COMPARTMENT (EWIS)
052160-200-004
SOURCE:
MRB ZL-161-03-1
PREPARATION: CEILING PANELS FROM FR 59 TO FR 65; INSULATION TO BE
DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION;
SIDEWALL PANELS FROM FR 59 TO FR 65; ACT(S) REMOVED (IF INSTALLED);
ACCESS PANELS: 826
ZL-161-03-2
161
162
BULK CARGO COMPARTMENT
AF
GVI
I:
12 YE
MRB
GENERAL VISUAL INSPECTION OF BULK CARGO
COMPARTMENT (EWIS)
052160-200-004
SOURCE:
MRB ZL-161-03-2
PREPARATION: CEILING PANELS FROM FR 59 TO FR 65; INSULATION TO BE
DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION;
SIDEWALL PANELS FROM FR 59 TO FR 65;
ZL-163-01-1
163
164
ACCESS PANELS: 826, 827
UNDERFLOOR BAY OF BULK CARGO COMPTMENT
AF
GVI
I:
6 YE
MRB
GENERAL VISUAL INSPECTION OF UNDERFLOOR BAY OF BULK
CARGO COMPARTMENT (EWIS)
052160-200-002
SOURCE:
MRB ZL-163-01-1
PREPARATION: FLOOR PANELS FROM FR 59 TO FR 65;
ZL-163-01-2
163
164
ACCESS PANELS: 826, 827
UNDERFLOOR BAY OF BULK CARGO COMPTMENT
GENERAL VISUAL INSPECTION OF UNDERFLOOR BAY OF BULK
CARGO COMPARTMENT (EWIS)
AF
GVI
I:
6 YE
MRB
052160-200-002
SOURCE:
MRB ZL-163-01-2
PREPARATION: FLOOR PANELS FROM FR 59 TO FR 65; ACT(S) REMOVED (IF
INSTALLED);
ACCESS PANELS: 826
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
ZL-171-01-1
ZONE
171
172
DESCRIPTION
AFT CABIN UNDERFLOOR COMPARTMENT
SKILL TASK
CODE CODE
AF
GVI
GENERAL VISUAL INSPECTION OF AFT CABIN UNDERFLOOR
COMPARTMENT (EWIS)
ZL-171-01-2
171
172
ACCESS PANELS: 161DW, 171AL, 162DW, 172AR, 826
AFT CABIN UNDERFLOOR COMPARTMENT
AF
GVI
GENERAL VISUAL INSPECTION OF AFT CABIN UNDERFLOOR
COMPARTMENT (EWIS)
ZL-171-02-1
171
172
ACCESS PANELS: 161DW, 171AL, 162DW, 172AR, 826
AFT CABIN UNDERFLOOR COMPARTMENT
AF
GVI
GENERAL VISUAL INSPECTION OF AFT CABIN UNDERFLOOR COMPARTMENT
(EWIS)
INTERVALS
SOURCE
I:
24 MO
OR
7500 FH
MRB
I:
24 MO
OR
7500 FH
MRB
I:
72 MO
OR
24000 FH
MRB
I:
24 MO
MRB
TPS
REFERENCES
052170-200-001
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.25
0.25
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.25
0.25
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.40
0.40
ALL
1
1
0.20
0.20
ALL
1
1
0.50
0.50
ALL
1
1
0.10
0.10
ALL
SOURCE:
MRB ZL-171-01-1
052170-200-001
SOURCE:
MRB ZL-171-01-2
052170-200-002
SOURCE:
MRB ZL-171-02-1
PREPARATION: ACT(S) REMOVED (IF INSTALLED);
INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED
INSPECTION;
ZL-191-01-1
191
192
ACCESS PANELS: 161DW, 171AL, 162DW, 172AR, 826
AIR CONDITIONING COMPARTMENT AND
FAIRINGS
AF
GVI
SOURCE:
MRB ZL-191-01-1
GENERAL VISUAL INSPECTION OF AIR CONDITIONING
COMPARTMENT AND FAIRINGS (EWIS)
ZL-191-02-1
191
192
ACCESS PANELS: 191BB, 191KB, 192KB
AIR CONDITIONING COMPARTMENT AND
FAIRINGS
AF
GVI
GENERAL VISUAL INSPECTION OF AIR CONDITIONING
COMPARTMENT AND FAIRINGS (EWIS)
ZL-193-01-1
193
194
ACCESS PANELS: 191AB, 191AT, 191BT, 191CT, 191DT, 191EB, 191ET, 191GB,
191HB, 191JB, 191KB, 191LB, 192AB, 192AT, 192BT, 192CT, 192DT, 192EB, 192ET,
192FB, 192KB, 192LB, 192MB
OFFWING ESCAPE SLIDE STOWAGE AREA
AF
GENERAL VISUAL INSPECTION OF OFFWING ESCAPE SLIDE
STOWAGE AREA (EWIS)
052190-200-001
GVI
I:
6 YE
OR
24000 FH
MRB
I:
6 YE
MRB
052190-200-009
SOURCE:
MRB ZL-191-02-1
052190-200-003
SOURCE:
MRB ZL-193-01-1
PREPARATION: ESCAPE SLIDE STOWAGE CONTAINER REMOVED;
Sub 2 - Page 288 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
ZL-195-01-1
ZONE
195
196
DESCRIPTION
HYDRAULIC COMPARTMENT AND FAIRINGS
SKILL TASK
CODE CODE
AF
GVI
INTERVALS
I:
24 MO
SOURCE
MRB
GENERAL VISUAL INSPECTION OF HYDRAULIC COMPARTMENT
AND FAIRINGS (EWIS)
ZL-197-01-1
197
198
ACCESS PANELS: 195BB, 196BB
REAR FAIRING
197
198
ACCESS PANELS: 197AB, 197BB, 197GB, 198BB, 198GB, 826GR
REAR FAIRING
AF
GVI
I:
6 YE
MRB
200
ACCESS PANELS: 197AB, 197GB, 197KB, 198GB, 198KB, 826DR
UPPER HALF OF FUSELAGE
AF
GVI
I:
6 YE
MRB
211
212
COCKPIT
AF
GVI
I:
24 MO
ZL-211-02-1
211
212
GENERAL VISUAL INSPECTION OF COCKPIT (EWIS)
052190-200-007
052190-200-007
MRB
052200-200-002
MRB
SOURCE:
MRB ZL-200-02-1
052210-200-001
AF
GVI
I:
48 MO
GENERAL VISUAL INSPECTION OF COCKPIT (EWIS)
ACCESS PANELS: 211AW, 211AZ, 211BW, 211EW, 211LW, 831, 212AW, 212AZ,
212BW, 212EW, 212JW
COCKPIT
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
ALL
1
1
0.30
0.30
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.30
0.30
1
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890
ALL
1
1
0.10
0.10
ALL
1
1
0.20
0.20
ALL
SOURCE:
MRB ZL-197-01-3
GENERAL VISUAL INSPECTION OF UPPER HALF OF FUSELAGE
ZL-211-01-1
052190-200-005
MEN
SOURCE:
MRB ZL-197-01-1
GENERAL VISUAL INSPECTION OF REAR FAIRING (EWIS)
ZL-200-02-1
REFERENCES
SOURCE:
MRB ZL-195-01-1
GENERAL VISUAL INSPECTION OF REAR FAIRING (EWIS)
ZL-197-01-3
TPS
SOURCE:
MRB ZL-211-01-1
AF
GVI
I:
12 YE
MRB
052210-200-002
SOURCE:
MRB ZL-211-02-1
PREPARATION: INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE
THE REQUIRED INSPECTION;
ACCESS PANELS: 211BC, 211FC, 211HC, 831, 212BC, 212FC, 212KW
Sub 2 - Page 289 of 305
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SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
ZL-221-02-1
ZONE
221
222
DESCRIPTION
FORWARD CABIN UTILITY AREA
SKILL TASK
CODE CODE
AF
GVI
INTERVALS
I:
12 YE
SOURCE
MRB
GENERAL VISUAL INSPECTION OF FWD CABIN UTILITY AREAS
INCLUDING FLOOR STRUCTURE (EWIS)
TPS
REFERENCES
052220-200-006
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
ALL
1
1
0.15
0.15
ALL
1
1
0.35
0.35
ALL
SOURCE:
MRB ZL-221-02-1
PREPARATION: DOOR FRAME LINING REMOVED; FLOOR PANELS FROM FR 12
TO FR 20; FURNISHINGS FROM FR 12 TO FR 20; GALLEYS; INSULATION TO BE
DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION; SEATS
REMOVED; TOILET REMOVAL/INSTALLATION ;
ACCESS PANELS: 831, 841
ZL-223-01-1
223
224
FWD CABIN UTILITY AREA OVERHEAD
COMPARTMENT
AF
GVI
I:
12 YE
MRB
052220-200-003
SOURCE:
MRB ZL-223-01-1
GENERAL VISUAL INSPECTION OF FWD CABIN UTILITY AREA
OVERHEAD COMPARTMENT (EWIS)
PREPARATION: CEILING PANELS FROM FR 12 TO FR 20; GALLEYS; INSULATION
TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION;
OVERHEAD STOWAGE COMPARTMENTS REMOVED; TOILET
REMOVAL/INSTALLATION ;
ZL-231-01-3
231
232
ACCESS PANELS: 831, 841
FORWARD PASSENGER COMPARTMENT
GENERAL VISUAL INSPECTION OF FWD PASSENGER
COMPARTMENT (EWIS)
(INCLUDING FLOOR STRUCTURE)
AF
GVI
I:
12 YE
MRB
052230-200-001
SOURCE:
MRB ZL-231-01-3
PREPARATION: FURNISHING REMOVED; GALLEYS; INSULATION TO BE
DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION; SEATS
REMOVED; SIDEWALL AND FLOOR PANELS FROM FR 20 TO FR 35 REMOVED;
TOILET REMOVAL/INSTALLATION ;
ACCESS PANELS: 831, 841
Sub 2 - Page 290 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
ZL-233-01-1
ZONE
233
234
DESCRIPTION
FWD PASSENGER OVERHEAD COMPARTMENT
SKILL TASK
CODE CODE
AF
GVI
INTERVALS
I:
12 YE
SOURCE
MRB
GENERAL VISUAL INSPECTION OF FWD PASSENGER OVERHEAD
COMPARTMENT (EWIS)
TPS
REFERENCES
052230-200-003
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.30
0.30
ALL
1
1
0.25
0.25
ALL
1
1
0.25
0.25
ALL
SOURCE:
MRB ZL-233-01-1
PREPARATION: CEILING PANELS FROM FR 20 TO FR 35; GALLEYS; INSULATION
TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION;
OVERHEAD STOWAGE COMPARTMENTS REMOVED; TOILET
REMOVAL/INSTALLATION ;
ACCESS PANELS: 831, 841
ZL-241-01-3
241
242
CENTER PASSENGER COMPARTMENT
AF
GVI
I:
12 YE
MRB
GENERAL VISUAL INSPECTION OF CENTER PASSENGER
COMPARTMENT (EWIS)
(INCLUDING FLOOR STRUCTURE)
052240-200-001
SOURCE:
MRB ZL-241-01-3
PREPARATION: GALLEYS; INSULATION TO BE DISPLACED AS REQUIRED TO
COMPLETE THE REQUIRED INSPECTION; FURNISHING, SIDEWALL (EXCEPT
EMERGENCY EXIT PANELS) AND FLOOR PANELS FROM FR 35 TO FR 47
REMOVED; TOILET REMOVAL/INSTALLATION ;
ACCESS PANELS: 832, 842
ZL-243-01-1
243
244
CENTER PASSENGER OVERHEAD COMPARTMENT
GENERAL VISUAL INSPECTION OF CENTER PASSENGER
OVERHEAD COMPARTMENT (EWIS)
AF
GVI
I:
12 YE
MRB
052240-200-003
SOURCE:
MRB ZL-243-01-1
PREPARATION: CEILING PANELS FROM FR 35 TO FR 47; GALLEYS; INSULATION
TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION;
OVERHEAD STOWAGE COMPARTMENTS REMOVED; TOILET
REMOVAL/INSTALLATION ;
ACCESS PANELS: 832, 842
Sub 2 - Page 291 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
ZL-251-01-3
ZONE
251
252
DESCRIPTION
AFT PASSENGER COMPARTMENT
SKILL TASK
CODE CODE
AF
GVI
INTERVALS
I:
12 YE
SOURCE
MRB
GENERAL VISUAL INSPECTION OF AFT PASSENGER
COMPARTMENT (EWIS)
(INCLUDING FLOOR STRUCTURE)
TPS
REFERENCES
052250-200-001
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.35
0.35
ALL
1
1
0.40
0.40
ALL
1488 1560
1743 1761
1851 1863
1876 1890
1488 1560
1743 1761
1851 1863
1876 1890
1488 1560
1743 1761
1851 1863
1876 1890
SOURCE:
MRB ZL-251-01-3
PREPARATION: GALLEYS; INSULATION TO BE DISPLACED AS REQUIRED TO
COMPLETE THE REQUIRED INSPECTION; FURNISHING, SIDEWALL AND FLOOR
PANELS FROM FR 47 TO FR 64 REMOVED; TOILET REMOVAL/INSTALLATION ;
ACCESS PANELS: 832, 842
ZL-253-01-1
253
254
AFT PASSENGER OVERHEAD COMPARTMENT
AF
GVI
I:
12 YE
MRB
GENERAL VISUAL INSPECTION OF AFT PASSENGER OVERHEAD
COMPARTMENT (EWIS)
052250-200-003
SOURCE:
MRB ZL-253-01-1
PREPARATION: CEILING PANELS FROM FR 47 TO FR 64; GALLEYS; INSULATION
TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION;
OVERHEAD STOWAGE COMPARTMENTS REMOVED; TOILET
REMOVAL/INSTALLATION ;
ACCESS PANELS: 832, 842
ZL-253-50-1-SDM
253
254
LIVETV RADOME INSTL AREA-FRAME C52 TO C56 & STR 5L TO 5R
AF
GVI
LIVETV RADOME INST AREA-FRAME C52 TO C56 & STR 5L TO 5R
AF
GVI
GENERAL VISUAL INSPECTION OF INTERNAL SUPPORT STRUCTURE FOR
LIVETV INSTALLATION.
LIVETV WADL ANTENNA INSTL AREA-FRAME C60 TO C61 & STR P1 TO P´1
AF
GVI
AF
GVI
EXTERNAL GENERAL VISUAL INSPECTION OF SKIN COVERED BY RADOME.
ZL-253-51-1-SDM
ZL-253-53-1-SDM
253
254
253
254
INTERNAL GENERAL VISUAL INSPECTION OF SKIN ADGACENT TO ANTENNA
SUPPORT DOUBLERS.
ZL-253-54-1-SDM
253
254
PREPARATION: LINING AND INSULATION REMOVED;
OVERHEAD STOWAGE COMPARTMENTS REMOVED;
LIVETV LNA INST AREA-FRAME C59 TO C60 & STR P´4 TO P´5
INTERNAL GENERAL VISUAL INSPECTION OF STRINGERS AT LNA SUPPORT
STRUCTURE FOR LIVETV INSTALLATION.
T:
5 YE
I:
5 YE
T:
9 YE
I:
8 YE
T:
9 YE
I:
8 YE
S-ICA
JIC A320-53-41-04
STC ST00788SE
ICA BERG-151-701
1
1
TBD
TBD
S-ICA
JIC A320-53-41-01
STC ST00788SE
ICA BERG-151-701
1
1
TBD
TBD
S-ICA
JIC A320-53-41-02
STC ST00788SE
ICA BERG-151-701
1
1
TBD
TBD
T:
9 YE
I:
8 YE
S-ICA
JIC A320-53-41-03
STC ST00788SE
ICA BERG-151-701
1
1
TBD
TBD
1488 1560
1743 1761
1851 1863
1876 1890
Sub 2 - Page 292 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
ZL-261-02-1
ZONE
261
262
DESCRIPTION
AFT CABIN UTILITY AREAS
SKILL TASK
CODE CODE
AF
GVI
INTERVALS
I:
12 YE
SOURCE
MRB
GENERAL VISUAL INSPECTION OF AFT CABIN UTILITY AREAS
INCLUDING FLOOR STRUCTURE (EWIS)
TPS
REFERENCES
052260-200-004
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.30
0.30
ALL
1
1
0.35
0.35
ALL
1
0.20
ALL
1
1
0.10
0.10
ALL
1
1
0.05
0.05
ALL
SOURCE:
MRB ZL-261-02-1
PREPARATION: FLOOR PANELS BETWEEN FR 64 TO 70; FURNISHINGS
BETWEEN FR 64 TO 70; GALLEYS; INSULATION TO BE DISPLACED AS
REQUIRED TO COMPLETE THE REQUIRED INSPECTION; SEATS REMOVED;
SIDEWALL/DOOR FRAME LINING REMOVED; TOILET REMOVAL/INSTALLATION ;
ACCESS PANELS: 832, 842
ZL-263-01-1
263
264
AFT CABIN OVERHEAD COMPARTMENT
AF
GVI
I:
12 YE
MRB
GENERAL VISUAL INSPECTION OF AFT CABIN OVERHEAD
COMPARTMENT (EWIS)
052260-200-003
SOURCE:
MRB ZL-263-01-1
PREPARATION: CEILING PANELS FROM FR 64 TO FR 70; GALLEYS; INSULATION
TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION;
OVERHEAD STOWAGE COMPARTMENTS REMOVED; TOILET
REMOVAL/INSTALLATION ;
ACCESS PANELS: 832, 842
ZL-300-02-1
ZL-311-01-1
300
311
312
STABILIZERS AND CONE/REAR FUSELAGE
GENERAL VISUAL INSPECTION OF STABILIZERS AND
CONE/REAR FUSELAGE
AFT FUSELAGE TAIL SECTION
AF
AF
GVI
GVI
I:
24 MO
OR
7500 FH
I:
24 MO
MRB
052300-200-002
MRB
SOURCE:
MRB ZL-300-02-1
052310-200-001
GENERAL VISUAL INSPECTION OF AFT FUSELAGE TAIL
SECTION (EWIS)
ZL-313-01-1
313
314
ACCESS PANELS: 312AR, 314AR
TAIL CONE APU AIR INTAKE AREA
GENERAL VISUAL INSPECTION OF TAIL CONE APU AIR INTAKE
AREA (EWIS)
SOURCE:
MRB ZL-311-01-1
AF
GVI
I:
24 MO
MRB
052310-200-002
SOURCE:
MRB ZL-313-01-1
ACCESS PANELS: 314AR
Sub 2 - Page 293 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
TASK
E
NUMBER
V
R ZL-315-01-1
ZONE
315
316
DESCRIPTION
TAIL CONE APU AND ACCESSORY COMPARTMENT
SKILL TASK
CODE CODE
AF
GVI
INTERVALS
I:
24 MO
SOURCE
MRB
GENERAL VISUAL INSPECTION OF TAIL CONE APU AND
ACCESSORY COMPARTMENT (EWIS)
D ZL-315-01-3
315
316
ACCESS PANELS: 315AL, 316AR
TAIL CONE APU AND ACCESSORY COMPARTMENT
317
ACCESS PANELS: 315AL, 316AR
TAIL CONE/APU EXHAUST AREA
AF
GVI
I:
24 MO
MRB
321
ACCESS PANELS: 317AL
DORSAL FIN
AF
GVI
I:
24 MO
MRB
322
ACCESS PANELS: 321AL
VERTICAL STABILIZER LEADING EDGE
AF
GVI
I:
12 YE
MRB
323
ACCESS PANELS: 322AL, 322BL, 322CL
VERTICAL STABILIZER SPAR BOX
1
1
0.10
0.10
ALL
052310-200-003
1
1
0.10
0.10
052310-200-004
1
0.10
ALL
052320-200-001
1
0.10
ALL
1
0.30
ALL
1
0.50
ALL
1
0.10
ALL
SOURCE:
MRB ZL-321-01-1
AF
GVI
I:
12 YE
MRB
GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER
LEADING EDGE (EWIS)
ZL-323-01-1
TASKM. APPLICABI
H.
LITY
SOURCE:
MRB ZL-317-01-1
GENERAL VISUAL INSPECTION OF DORSAL FIN (EWIS)
ZL-322-01-1
052310-200-003
MEN
SOURCE:
MRB ZL-315-01-3
GENERAL VISUAL INSPECTION OF TAIL CONE APU EXHAUST
AREA (EWIS)
ZL-321-01-1
REFERENCES
SOURCE:
MRB ZL-315-01-1
GENERAL VISUAL INSPECTION OF TAIL CONE APU AND ACCESSORY
COMPARTMENT (EWIS)
ZL-317-01-1
TPS
052320-200-002
SOURCE:
MRB ZL-322-01-1
AF
GVI
I:
12 YE
MRB
GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER SPAR
BOX (EWIS)
052320-200-003
SOURCE:
MRB ZL-323-01-1
PREPARATION: PEELABLE HOLE COVERS REMOVED;
ZL-324-01-1
324
ACCESS PANELS: 321AL, 322BL, 323AL, 323AR, 325AL, 325AR
VERTICAL STABILIZER TIP
GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER
TIP (EWIS)
AF
GVI
I:
12 YE
MRB
052320-200-004
SOURCE:
MRB ZL-324-01-1
ACCESS PANELS: 324AT
Sub 2 - Page 294 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
ZL-325-01-1
ZONE
325
DESCRIPTION
VERTICAL STABILIZER TRAILING EDGE
SKILL TASK
CODE CODE
AF
GVI
INTERVALS
I:
24 MO
SOURCE
MRB
GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER
TRAILING EDGE (EWIS)
ZL-325-02-1
325
ACCESS PANELS: 325BL, 325CL, 325DL, 325EL
VERTICAL STABILIZER TRAILING EDGE
ZL-326-01-1
326
AF
GVI
I:
6 YE
MRB
ZL-326-02-1
326
052320-200-005
MEN
TASKM. APPLICABI
H.
LITY
1
0.20
ALL
052320-200-007
1
0.40
ALL
1
0.40
ALL
1
0.60
ALL
1
1
0.30
0.30
ALL
1
1
0.10
0.10
ALL
SOURCE:
MRB ZL-325-02-1
AF
GVI
I:
6 YE
MRB
GENERAL VISUAL INSPECTION OF RUDDER (EWIS)
ACCESS PANELS: 325AL, 325AR, 325BL, 325BR, 325CL, 325CR, 325DL, 325DR,
325EL, 325ER, 326AT
RUDDER
REFERENCES
SOURCE:
MRB ZL-325-01-1
GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER
TRAILING EDGE (EWIS)
ACCESS PANELS: 325AL, 325AR, 325BL, 325BR, 325CL, 325CR, 325DL, 325DR,
325EL, 325ER
RUDDER
TPS
052320-200-006
SOURCE:
MRB ZL-326-01-1
AF
GVI
I:
12 YE
MRB
GENERAL VISUAL INSPECTION OF RUDDER (EWIS)
052320-200-008
SOURCE:
MRB ZL-326-02-1
PREPARATION: PEELABLE HOLE COVERS REMOVED;
ZL-331-01-1
331
341
ACCESS PANELS: 325AL, 325AR, 325BL, 325BR, 325CL, 325CR, 325DL, 325DR,
325EL, 325ER, 326AT
THS LEADING EDGE
AF
GVI
I:
6 YE
MRB
GENERAL VISUAL INSPECTION OF TRIMMABLE HORIZONTAL
STABILIZER LEADING EDGE (EWIS)
ZL-332-01-1
332
342
ACCESS PANELS: 331AB, 331BB, 331CB, 341AB, 341BB, 341CB
THS TIP
GENERAL VISUAL INSPECTION OF TRIMMABLE HORIZONTAL
STABILIZER TIP (EWIS)
052330-200-001
SOURCE:
MRB ZL-331-01-1
AF
GVI
I:
12 YE
MRB
052330-200-002
SOURCE:
MRB ZL-332-01-1
ACCESS PANELS: 332AB, 342AB
Sub 2 - Page 295 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
ZL-333-01-1
ZONE
333
343
DESCRIPTION
THS SPAR BOX
SKILL TASK
CODE CODE
AF
GVI
INTERVALS
I:
12 YE
SOURCE
MRB
GENERAL VISUAL INSPECTION OF TRIMMABLE HORIZONTAL
STABILIZER SPAR BOX (EWIS)
TPS
REFERENCES
052330-200-003
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
ALL
1
1
0.20
0.20
ALL
1
1
0.40
0.40
ALL
1
1
0.20
0.20
ALL
1
0.20
ALL
1
1
1
1
1
1
0.03
0.03
0.03
0.03
0.03
0.03
ALL
SOURCE:
MRB ZL-333-01-1
PREPARATION: PEELABLE HOLE COVERS REMOVED;
ZL-334-01-1
334
344
ACCESS PANELS: 312AR, 314AR, 331AB, 331BB, 331CB, 332AB, 333AB, 333AT,
334AB, 334BB, 334CB, 334DB, 334EB, 334FB, 334GB, 334HB, 341AB, 341BB,
341CB, 342AB, 343AB, 343AT, 344AB, 344BB, 344CB, 344DB, 344EB, 344FB,
344GB, 344HB
THS TRAILING EDGE
AF
GVI
I:
24 MO
MRB
GENERAL VISUAL INSPECTION OF TRIMMABLE HORIZONTAL
STABILIZER TRAILING EDGE (EWIS)
052330-200-004
SOURCE:
MRB ZL-334-01-1
ACCESS PANELS: 334BB, 334DB, 334FB, 334HB, 344BB, 344DB, 344FB, 344HB
ZL-334-02-1
334
344
THS TRAILING EDGE
AF
GVI
I:
6 YE
MRB
GENERAL VISUAL INSPECTION OF TRIMMABLE HORIZONTAL
STABILIZER TRAILING EDGE (EWIS)
ZL-335-01-1
335
345
SOURCE:
MRB ZL-334-02-1
ACCESS PANELS: 334AB, 334AT, 334BB, 334BT, 334CB, 334CT, 334DB, 334DT,
334EB, 334FB, 334GB, 334HB, 344AB, 344AT, 344BB, 344BT, 344CB, 344CT, 344DB,
344DT, 344EB, 344FB, 344GB, 344HB
ELEVATOR
AF
GVI
I:
6 YE
MRB
GENERAL VISUAL INSPECTION OF ELEVATOR (EWIS)
ZL-400-02-1
ZL-411-01-1
400
411
413
414
421
423
424
ACCESS PANELS: 334BB, 334DB, 334FB, 334HB, 335AB, 335BB, 335CB, 335DB,
344BB, 344DB, 344FB, 344HB, 345AB, 345BB, 345CB, 345DB
POWERPLANTS, NACELLES AND PYLONS
GENERAL VISUAL INSPECTION OF POWERPLANTS, NACELLES
AND PYLONS
UPPER FORWARD PYLON
GENERAL VISUAL INSPECTION OF UPPER FWD PYLON (EWIS)
ACCESS PANELS: 413AL, 413BL, 413CL, 413DL, 413EL, 414AR, 414AZ, 414BR,
414CR, 414FR, 423AL, 423AZ, 423BL, 423CL, 423DL, 423FL, 424AR, 424BR, 424CR,
424ER
052330-200-007
052330-200-005
SOURCE:
MRB ZL-335-01-1
EN
EN
GVI
GVI
I:
4 MO
I:
20 MO
MRB
052400-200-002
MRB
SOURCE:
MRB ZL-400-02-1
052410-200-001
SOURCE:
MRB ZL-411-01-1
Sub 2 - Page 296 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
ZL-415-01-1
ZONE
415
425
DESCRIPTION
LOWER PYLON
SKILL TASK
CODE CODE
EN
GVI
INTERVALS
I:
20 MO
SOURCE
MRB
GENERAL VISUAL INSPECTION OF LOWER PYLON (EWIS)
TPS
REFERENCES
052410-200-002
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.20
0.20
ALL
1
1
1
1
0.15
0.15
0.15
0.15
ALL
1
1
1
1
0.10
0.10
0.10
0.10
ALL
1
1
1
1
0.10
0.10
0.10
0.10
ALL
1
1
1
1
1
1
1
1
1
1
1
1
1
1
0.03
0.03
0.03
0.03
0.03
0.03
0.03
0.03
0.03
0.03
0.03
0.03
0.30
0.30
ALL
SOURCE:
MRB ZL-415-01-1
ACCESS PANELS: 415AL, 415AR, 415BL, 415BR, 425AL, 425AR, 425BL, 425BR
ZL-433-01-1
ZL-437-01-1
ZL-451-01-1
433
434
443
444
437
438
447
448
451
452
461
462
AIR INTAKE LIP
EN
GVI
GENERAL VISUAL INSPECTION OF AIR INTAKE LIP (EWIS)
ACCESS PANELS: 433AZ, 433BZ, 437AL, 434AR, 434BZ, 438AR, 443AZ, 443BZ,
447AL, 444AR, 444BZ, 448AR
FAN COWL
EN
GVI
I:
6 YE
OR
24000 FH
MRB
I:
16 MO
MRB
SOURCE:
MRB ZL-433-01-1
GENERAL VISUAL INSPECTION OF FAN COWL (EWIS)
ACCESS PANELS: 437AL, 438AR, 447AL, 448AR
THRUST REVERSER
052430-200-001
052430-200-003
SOURCE:
MRB ZL-437-01-1
EN
GVI
I:
16 MO
MRB
GENERAL VISUAL INSPECTION OF THRUST REVERSER (EWIS)
052450-200-001
SOURCE:
MRB ZL-451-01-1
PREPARATION: THRUST REVERSER PIVOTING DOOR OPENED;
ZL-471-01-1
ZL-500-02-1
471
472
473
475
476
477
481
482
483
485
486
487
500
600
ACCESS PANELS: 451AL, 452AR, 461AL, 462AR
PYLON LEADING EDGE AND LOWER FAIRING
EN
GVI
I:
24 MO
MRB
GENERAL VISUAL INSPECTION OF PYLON LEADING EDGE AND
LOWER FAIRING (EWIS)
052470-200-001
SIL 54-023
SOURCE:
MRB ZL-471-01-1
ACCESS PANELS: 471AL, 471BL, 471CL, 472AR, 472BR, 473AL, 473AR, 475AL,
475BL, 475CL, 476AR, 476BR, 476CR, 477AL, 481AL, 481BL, 482AR, 482BR, 482CR,
483AL, 483AR, 485AL, 485BL, 485CL, 486AR, 486BR, 486CR, 487AR
WING LOWER SURFACE
GENERAL VISUAL INSPECTION OF WING LOWER SURFACE
INCLUDING UPPER AND LOWER SURFACES OF SLATS AND
FLAPS (EWIS)
AF
GVI
I:
8 DY
MRB
052500-200-002
ALL
SOURCE:
MRB ZL-500-02-1
PREPARATION: FLAPS EXTENDED; SLATS FULLY EXTENDED;
Sub 2 - Page 297 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
ZL-500-03-1
ZONE
500
600
DESCRIPTION
WING UPPER SURFACE
SKILL TASK
CODE CODE
AF
GVI
INTERVALS
I:
48 MO
SOURCE
MRB
GENERAL VISUAL INSPECTION OF WING UPPER SURFACE
INCLUDING SLATS, FLAPS AND SPOILERS (EWIS)
ZL-521-01-1
521
621
PREPARATION: FLAPS EXTENDED; SPOILERS EXTENDED; SLATS FULLY
EXTENDED;
INBOARD FIXED LEADING EDGE STRUCTURE
TPS
REFERENCES
052500-200-003
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.30
0.30
ALL
1
1
0.20
0.20
ALL
1
1
0.20
0.20
ALL
1
1
0.10
0.10
ALL
1
1
0.30
0.30
ALL
SOURCE:
MRB ZL-500-03-1
AF
GVI
I:
24 MO
MRB
GENERAL VISUAL INSPECTION OF INBOARD FIXED LEADING
EDGE STRUCTURE (EWIS)
052520-200-001
SOURCE:
MRB ZL-521-01-1
PREPARATION: SLATS FULLY EXTENDED;
ZL-522-01-1
522
622
ACCESS PANELS: 521AB, 521AT, 521BT, 521CB, 521EB, 521GB, 521HB, 621AB,
621AT, 621BT, 621CB, 621EB, 621GB, 621HB
OUTBOARD FIXED LEADING EDGE STRUCTURE
AF
GVI
I:
24 MO
MRB
GENERAL VISUAL INSPECTION OF OUTBOARD FIXED LEADING
EDGE STRUCTURE (EWIS)
052520-200-002
SOURCE:
MRB ZL-522-01-1
PREPARATION: SLATS FULLY EXTENDED;
ACCESS PANELS: 522AB, 522AT, 522BT, 522CB, 522EB, 522FB, 522HB, 522JB,
522KB, 522LB, 522NB, 522QB, 522SB, 522UB, 622AB, 622AT, 622BT, 622CB, 622EB,
622FB, 622HB, 622JB, 622KB, 622LB, 622NB, 622QB, 622SB, 622UB
ZL-531-01-1
531
631
FLAP TRACK NO 2 AND FAIRING
AF
GVI
I:
24 MO
MRB
GENERAL VISUAL INSPECTION OF FLAP TRACK NO 2 AND
FAIRING (EWIS)
052530-200-001
SOURCE:
MRB ZL-531-01-1
PREPARATION: FLAPS EXTENDED;
ZL-531-02-1
531
631
ACCESS PANELS: 531AT, 631AT
FLAP TRACK NO 2 AND FAIRING
GENERAL VISUAL INSPECTION OF FLAP TRACK NO 2 AND
FAIRING (EWIS)
AF
GVI
I:
6 YE
MRB
052530-200-005
SOURCE:
MRB ZL-531-02-1
PREPARATION: FLAPS EXTENDED;
ACCESS PANELS: 531AB, 531AL, 531AR, 531AT, 531BB, 531CB, 531DB, 631AB,
631AL, 631AR, 631AT, 631BB, 631CB, 631DB
Sub 2 - Page 298 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
ZL-532-01-1
ZONE
532
632
DESCRIPTION
FLAP TRACK NO 3 AND FAIRING
SKILL TASK
CODE CODE
AF
GVI
INTERVALS
I:
24 MO
SOURCE
MRB
GENERAL VISUAL INSPECTION OF FLAP TRACK NO 3 AND
FAIRING (EWIS)
TPS
REFERENCES
052530-200-002
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.10
0.10
ALL
1
1
0.30
0.30
ALL
1
1
0.10
0.10
ALL
1
1
0.30
0.30
ALL
1
1
0.10
0.10
ALL
SOURCE:
MRB ZL-532-01-1
PREPARATION: FLAPS EXTENDED;
ZL-532-02-1
532
632
ACCESS PANELS: 532AT, 632AT
FLAP TRACK NO 3 AND FAIRING
AF
GVI
I:
6 YE
MRB
GENERAL VISUAL INSPECTION OF FLAP TRACK NO 3 AND
FAIRING (EWIS)
052530-200-006
SOURCE:
MRB ZL-532-02-1
PREPARATION: FLAPS EXTENDED;
ZL-533-01-1
533
633
ACCESS PANELS: 532AB, 532AL, 532AR, 532AT, 532BB, 532CB, 532DB, 632AB,
632AL, 632AR, 632AT, 632BB, 632CB, 632DB
FLAP TRACK NO 4 AND FAIRING
AF
GVI
I:
24 MO
MRB
GENERAL VISUAL INSPECTION OF FLAP TRACK NO 4 AND
FAIRING (EWIS)
052530-200-003
SOURCE:
MRB ZL-533-01-1
PREPARATION: FLAPS EXTENDED;
ZL-533-02-1
533
633
ACCESS PANELS: 533AT, 633AT
FLAP TRACK NO 4 AND FAIRING
AF
GVI
I:
6 YE
MRB
GENERAL VISUAL INSPECTION OF FLAP TRACK NO 4 AND
FAIRING (EWIS)
052530-200-007
SOURCE:
MRB ZL-533-02-1
PREPARATION: FLAPS EXTENDED;
ZL-534-01-2
534
634
ACCESS PANELS: 533AB, 533AL, 533AR, 533AT, 533BB, 533CB, 533DB, 633AB,
633AL, 633AR, 633AT, 633BB, 633CB, 633DB
WING TIP
GENERAL VISUAL INSPECTION OF WING TIP (EWIS)
AF
GVI
I:
72 MO
MRB
052530-200-004
SOURCE:
MRB ZL-534-01-2
ACCESS PANELS: 534AB, 534AL, 534BL, 634AB, 634AL, 634BL
Sub 2 - Page 299 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
ZL-540-01-1
ZONE
540
640
DESCRIPTION
WING FUEL TANK
SKILL TASK
CODE CODE
AF
GVI
GENERAL VISUAL INSPECTION OF WING FUEL TANK (EWIS)
INTERVALS
SOURCE
I:
6 YE
NOTE
MRB
I:
12 YE
MRB
TPS
REFERENCES
052540-200-005
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.40
0.40
ALL
1
1
1.50
1.50
ALL
1
1
0.30
0.30
ALL
1
1
0.10
0.10
ALL
1
1
0.20
0.20
ALL
SOURCE:
MRB ZL-540-01-1
NOTE: INTERVAL MAY BE ADJUSTED BY INDIVIDUAL
OPERATORS IN CONSIDERATION OF THEIR OWN
INSERVICE EXPERIENCE AND OPERATIONAL
ENVIRONMENT.
ZL-540-02-2
540
640
ACCESS PANELS: 540AB, 540AZ, 540BZ, 540JB, 540KB, 640AB, 640AZ, 640BZ,
640JB, 640KB
WING FUEL TANK
AF
GVI
GENERAL VISUAL INSPECTION OF WING FUEL TANK (EWIS)
052540-200-004
SOURCE:
MRB ZL-540-02-2
NOTE: ALTERNATIVE COMPLIANCE FOR THE DRY BAY AREA IS
SHOWN BY PERFORMING TASKS 572050-02-1, 572050-02-2,
572050-02-4, 572050-02-5 AND 572050-02-6 AT THE SAME
TIME. ACCESS PANELS 540/640CZ AND 540/640DZ NEED NOT
TO BE REMOVED IN THIS CASE
ZL-550-01-1
550
650
ACCESS PANELS: 521AZ, 521BZ, 540AB, 540AZ, 540BB, 540BZ, 540CB, 540CZ,
540DB, 540DZ, 540EB, 540FB, 540GB, 540HB, 540JB, 540KB, 540LB, 540MB, 540NB,
540PB, 540QB, 540RB, 621AZ, 621BZ, 640AB, 640AZ, 640BB, 640BZ, 640CB, 640CZ,
640DB, 640DZ, 640EB, 640FB, 640GB, 640HB, 640JB, 640KB, 640LB, 640MB, 640NB,
640PB, 640QB, 640RB
VENT SURGE TANK
AF
GVI
I:
12 YE
MRB
GENERAL VISUAL INSPECTION OF VENT SURGE TANK (EWIS)
052550-200-001
SOURCE:
MRB ZL-550-01-1
ACCESS PANELS: 550AB, 550BB, 550CB, 550DB, 650AB, 650BB, 650CB, 650DB
ZL-560-01-1
560
660
DRY BAY
AF
GVI
I:
12 YE
MRB
GENERAL VISUAL INSPECTION OF DRY BAY
(OUTBOARD) (EWIS)
ZL-571-02-1
571
671
ACCESS PANELS: 560AB, 660AB
MAIN LANDING GEAR BAY
GENERAL VISUAL INSPECTION OF MLG BAY (EWIS)
052560-200-001
SOURCE:
MRB ZL-560-01-1
AF
GVI
I:
48 MO
MRB
052570-200-006
SOURCE:
MRB ZL-571-02-1
Sub 2 - Page 300 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
ZL-572-01-1
ZONE
572
672
DESCRIPTION
SHROUD BOX
SKILL TASK
CODE CODE
AF
GVI
INTERVALS
I:
48 MO
SOURCE
MRB
GENERAL VISUAL INSPECTION OF SHROUD BOX (EWIS)
TPS
REFERENCES
052570-200-002
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.10
0.10
0649
1
1
0.10
0.10
1
1
0.10
0.10
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
ALL
1
1
0.10
0.10
ALL
1
1
0.30
0.30
ALL
1
1
0.10
0.10
ALL
SOURCE:
MRB ZL-572-01-1
PREPARATION: FLAPS EXTENDED;
ZL-572-01-2
572
672
ACCESS PANELS: 571AB, 572AB, 572BB, 671AB, 672AB, 672BB
SHROUD BOX
AF
GVI
I:
48 MO
MRB
GENERAL VISUAL INSPECTION OF SHROUD BOX (EWIS)
052570-200-002
SOURCE:
MRB ZL-572-01-2
PREPARATION: FLAPS EXTENDED;
ACCESS PANELS: 571AB, 671AB
ZL-573-01-1
573
673
INBOARD FIXED TRAILING EDGE STRUCTURE
AF
GVI
I:
24 MO
MRB
GENERAL VISUAL INSPECTION OF INBOARD FIXED TRAILING
EDGE STRUCTURE FROM SHROUD BOX TO RIB 9 (EWIS)
ZL-574-01-1
574
674
PREPARATION: FLAPS EXTENDED; SPOILERS EXTENDED;
FALSE SPAR BOX
052570-200-003
SOURCE:
MRB ZL-573-01-1
AF
GVI
I:
24 MO
MRB
GENERAL VISUAL INSPECTION OF FALSE SPAR BOX (EWIS)
052570-200-004
SOURCE:
MRB ZL-574-01-1
PREPARATION: PYLON FAIRINGS REMOVED;
ZL-575-01-1
575
675
ACCESS PANELS: 573AB, 573BB, 573CB, 573DB, 573EB, 574AB, 574BB, 673AB,
673BB, 673CB, 673DB, 673EB, 674AB, 674BB
OUTB FIXED TRAILING EDGE STRUCTURE
AF
GVI
I:
24 MO
MRB
GENERAL VISUAL INSPECTION OF OUTBOARD FIXED TRAILING
EDGE STRUCTURE FROM RIB 9 TO RIB 27 (EWIS)
052570-200-005
SOURCE:
MRB ZL-575-01-1
PREPARATION: FLAPS EXTENDED; SPOILERS EXTENDED;
ACCESS PANELS: 575AT, 575KB, 575LB, 575MB, 675AT, 675KB, 675LB, 675MB
ZL-590-01-1
590
690
AILERON
GENERAL VISUAL INSPECTION OF AILERON (EWIS)
AF
GVI
I:
48 MO
MRB
052590-200-001
SOURCE:
MRB ZL-590-01-1
ACCESS PANELS: 590AB, 590BB, 690AB, 690BB
Sub 2 - Page 301 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
ZL-711-01-1
ZL-731-01-1
ZL-732-01-1
ZL-733-01-1
ZL-734-01-1
ZONE
711
712
713
714
715
716
731
741
732
742
733
743
734
744
DESCRIPTION
NOSE GEAR AND NOSE GEAR DOORS
SKILL TASK
CODE CODE
AF
GVI
INTERVALS
I:
4 MO
SOURCE
MRB
GENERAL VISUAL INSPECTION OF NOSE GEAR AND NOSE GEAR
DOORS (EWIS)
ACCESS PANELS: 713, 714
LH/RH MAIN LANDING GEAR
GENERAL VISUAL INSPECTION OF LH/RH MAIN LANDING
GEAR (EWIS)
MAIN LANDING GEAR CYLINDER DOOR
GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR
CYLINDER DOOR (EWIS)
MAIN LANDING GEAR SECONDARY DOOR
GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR
SECONDARY DOOR (EWIS)
MAIN LANDING GEAR MAIN DOORS
811
ACCESS PANELS: 734, 744
FWD AVIONICS COMPARTMENT DOOR
AF
AF
AF
AF
GVI
GVI
GVI
GVI
I:
4 MO
811
ACCESS PANELS: 811
FWD AVIONICS COMPARTMENT DOOR
052710-200-001
I:
4 MO
I:
4 MO
I:
4 MO
MRB
052730-200-001
MRB
SOURCE:
MRB ZL-731-01-1
052730-200-002
MRB
SOURCE:
MRB ZL-732-01-1
052730-200-003
MRB
SOURCE:
MRB ZL-733-01-1
052730-200-004
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
1
1
1
1
0.10
0.10
0.10
0.10
0.10
0.10
0.10
0.10
ALL
1
1
0.10
0.10
ALL
1
1
0.10
0.10
ALL
1
1
0.10
0.10
ALL
1
0.10
ALL
1
0.40
ALL
1
1
0.10
0.10
ALL
ALL
SOURCE:
MRB ZL-734-01-1
AF
GVI
I:
24 MO
MRB
GENERAL VISUAL INSPECTION OF FWD AVIONICS COMPARTMENT
DOOR (EWIS)
(INCLUDING EXTERNAL SURFACE)
ZL-811-02-1
REFERENCES
SOURCE:
MRB ZL-711-01-1
GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR MAIN
DOORS (EWIS)
ZL-811-01-1
TPS
052810-200-001
SOURCE:
MRB ZL-811-01-1
AF
GVI
I:
12 YE
MRB
GENERAL VISUAL INSPECTION OF FWD AVIONICS COMPARTMENT
DOOR (EWIS)
052810-200-002
SOURCE:
MRB ZL-811-02-1
PREPARATION: DOOR PANELS REMOVED;
ZL-812-01-1
812
822
ACCESS PANELS: 811
LATERAL AVIONICS COMPARTMENT DOORS
GENERAL VISUAL INSPECTION OF LATERAL AVIONICS
COMPARTMENT DOORS (EWIS)
(INCLUDING EXTERNAL SURFACE)
AF
GVI
I:
24 MO
MRB
052810-200-003
SOURCE:
MRB ZL-812-01-1
ACCESS PANELS: 812, 822
Sub 2 - Page 302 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
ZL-812-02-1
ZONE
812
822
DESCRIPTION
LATERAL AVIONICS COMPARTMENT DOORS
SKILL TASK
CODE CODE
AF
GVI
INTERVALS
I:
12 YE
SOURCE
MRB
GENERAL VISUAL INSPECTION OF LATERAL AVIONICS
COMPARTMENT DOORS (EWIS)
ZL-824-01-1
824
ACCESS PANELS: 812, 822
REAR AVIONIC COMPARTMENT DOOR
824
ACCESS PANELS: 824
REAR AVIONIC COMPARTMENT DOOR
AF
GVI
I:
24 MO
MRB
825
ACCESS PANELS: 824
FORWARD CARGO COMPARTMENT DOOR
AF
GVI
I:
12 YE
MRB
825
ACCESS PANELS: 825
FWD CARGO COMPARTMENT DOOR
TASKM. APPLICABI
H.
LITY
1
1
0.40
0.40
ALL
052820-200-007
1
0.10
ALL
052820-200-008
1
0.40
ALL
1
0.10
ALL
1
0.80
ALL
1
0.10
1130 1200
1379 1578
1657 1767
2151 2163
SOURCE:
MRB ZL-824-02-1
AF
GVI
I:
4 MO
MRB
GENERAL VISUAL INSPECTION OF FWD CARGO COMPARTMENT
DOOR INCLUDING FUSELAGE DOOR SILL, DOOR SEAL AND LOCK
FITTINGS, EXTERNAL SURFACE (EWIS)
ZL-825-02-1
052810-200-004
MEN
SOURCE:
MRB ZL-824-01-1
GENERAL VISUAL INSPECTION OF REAR AVIONIC COMPARTMENT
DOOR (EWIS)
ZL-825-01-1
REFERENCES
SOURCE:
MRB ZL-812-02-1
GENERAL VISUAL INSPECTION OF REAR AVIONIC COMPARTMENT
DOOR (EWIS)
(INCLUDING EXTERNAL SURFACE)
ZL-824-02-1
TPS
052820-200-001
SOURCE:
MRB ZL-825-01-1
AF
GVI
I:
12 YE
MRB
GENERAL VISUAL INSPECTION OF FWD CARGO COMPARTMENT
DOOR (EWIS)
052820-200-004
SOURCE:
MRB ZL-825-02-1
PREPARATION: INSULATION REMOVED;
ZL-826-01-1
826
ACCESS PANELS: 825, 825AR
AFT CARGO COMPARTMENT DOOR
GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT
DOOR INCLUDING FUSELAGE DOOR SILL, DOOR SEAL AND LOCK
FITTINGS (EWIS)
AF
GVI
I:
4 MO
MRB
052820-200-002
SOURCE:
MRB ZL-826-01-1
ACCESS PANELS: 826
Sub 2 - Page 303 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
ZL-826-01-2
ZONE
826
DESCRIPTION
AFT CARGO COMPARTMENT DOOR
SKILL TASK
CODE CODE
AF
GVI
INTERVALS
I:
4 MO
SOURCE
MRB
GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT
DOOR INCLUDING FUSELAGE DOOR SILL, DOOR SEAL AND LOCK
FITTINGS (EWIS)
ZL-826-02-1
826
ACCESS PANELS: 826
AFT CARGO COMPARTMENT DOOR
TPS
REFERENCES
052820-200-002
MEN
TASKM. APPLICABI
H.
LITY
1
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.30
1130 1200
1379 1578
1657 1767
2151 2163
1
0.30
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.20
1130 1200
1379 1578
1657 1767
2151 2163
1
0.20
1130 1200
1379 1578
1657 1767
2151 2163
1
1
1
1
0.05
0.05
0.05
0.05
ALL
SOURCE:
MRB ZL-826-01-2
AF
GVI
I:
12 YE
MRB
GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT
DOOR (EWIS)
052820-200-005
SOURCE:
MRB ZL-826-02-1
PREPARATION: INSULATION REMOVED;
ZL-826-02-2
826
ACCESS PANELS: 826, 826AR
AFT CARGO COMPARTMENT DOOR
AF
GVI
I:
12 YE
MRB
GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT
DOOR (EWIS)
052820-200-005
SOURCE:
MRB ZL-826-02-2
PREPARATION: INSULATION REMOVED;
ZL-827-01-1
827
ACCESS PANELS: 826, 826AR, 826BR, 826CR
BULK CARGO COMPARTMENT DOOR
AF
GVI
I:
4 MO
MRB
GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT
DOOR INCLUDING DOOR STOPS ON FUSELAGE DOOR
FRAME (EWIS)
ZL-827-02-1
827
ACCESS PANELS: 827
BULK CARGO COMPARTMENT DOOR
052820-200-003
SOURCE:
MRB ZL-827-01-1
AF
GVI
I:
12 YE
MRB
GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT
DOOR (EWIS)
052820-200-006
SOURCE:
MRB ZL-827-02-1
PREPARATION: INSULATION REMOVED;
ZL-831-01-1
831
832
841
842
ACCESS PANELS: 827
FWD AND AFT PASSENGER/CREW DOOR
GENERAL VISUAL INSPECTION OF FWD AND AFT
PASSENGER/CREW DOORS INCLUDING DOOR STOPS ON FUSELAGE
DOOR FRAMES AND DOOR SEALS, EXTERNAL SURFACE (EWIS)
AF
GVI
I:
4 MO
MRB
052830-200-001
SOURCE:
MRB ZL-831-01-1
ACCESS PANELS: 831, 832, 841, 842
Sub 2 - Page 304 of 305
MP REF: SDM.A320.BDCA
SECTION: II
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
SCHEDULED MAINTENANCE PROGRAM
R
E
V
TASK
NUMBER
ZL-831-02-1
ZONE
831
832
841
842
DESCRIPTION
FWD AND AFT PASSENGER/CREW DOOR
SKILL TASK
CODE CODE
AF
GVI
INTERVALS
I:
12 YE
SOURCE
MRB
GENERAL VISUAL INSPECTION OF FWD AND AFT
PASSENGER/CREW DOORS (EWIS)
TPS
REFERENCES
052830-200-005
SOURCE:
MRB ZL-831-02-1
MEN
TASKM. APPLICABI
H.
LITY
1
1
1
1
0.20
0.20
0.20
0.20
ALL
1
1
1
1
0.05
0.05
0.05
0.05
1130 1200
1379 1578
1657 1767
2151 2163
1
1
1
1
0.15
0.15
0.15
0.15
1130 1200
1379 1578
1657 1767
2151 2163
1
1
0.10
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
1
0.10
0.10
0649 1488
1560 1743
1761 1851
1863 1876
1890
PREPARATION: INSULATION REMOVED;
ZL-833-01-1
ZL-833-02-1
833
834
843
844
833
834
843
844
ACCESS PANELS: 831, 831AZ, 831BZ, 831CZ, 831DZ, 831EZ, 831FZ, 831GZ, 832,
832AZ, 832BZ, 832CZ, 832DZ, 832EZ, 832FZ, 832GZ, 841, 841AZ, 841BZ, 841CZ,
841DZ, 841EZ, 841FZ, 841GZ, 842, 842AZ, 842BZ, 842CZ, 842DZ, 842EZ, 842FZ,
842GZ
FWD AND AFT EMERGENCY EXITS
AF
GVI
I:
48 MO
MRB
GENERAL VISUAL INSPECTION OF FWD AND AFT EMERGENCY
EXITS INCLUDING DOOR SURROUND ON FUSELAGE DOOR FRAMES
AND DOOR SEALS, EXTERNAL SURFACE (EWIS)
ACCESS PANELS: 833, 834, 843, 844
FWD AND AFT EMERGENCY EXITS
052830-200-003
SOURCE:
MRB ZL-833-01-1
AF
GVI
I:
6 YE
MRB
GENERAL VISUAL INSPECTION OF FWD AND AFT EMERGENCY EXITS (EWIS)
052830-200-007
SOURCE:
MRB ZL-833-02-1
PREPARATION: INSULATION REMOVED;
ACCESS PANELS: 833, 833AZ, 833BZ, 834, 834AZ, 834BZ, 843, 843AZ, 843BZ, 844,
844AZ, 844BZ
ZL-834-05-1
834
844
EMERGENCY EXITS
AF
GVI
I:
48 MO
MRB
GENERAL VISUAL INSPECTION OF EMERGENCY EXITS
INCLUDING DOOR SURROUND ON FUSELAGE AND DOOR SEALS,
EXTERNAL SURFACE (EWIS)
ZL-834-06-1
834
844
ACCESS PANELS: 834, 844
EMERGENCY EXITS
GENERAL VISUAL INSPECTION OF EMERGENCY EXITS (EWIS)
ACCESS PANELS: 834, 834AZ, 834BZ, 844, 844AZ, 844BZ
052830-200-013
SOURCE:
MRB ZL-834-05-1
AF
GVI
I:
6 YE
MRB
052830-200-014
SOURCE:
MRB ZL-834-06-1
Sub 2 - Page 305 of 305
SDM A319/A320 MAINTENANCE PROGRAM
TIME CONTROLLED ITEMS
III.
MP-REF: SDM.A320.BDCA
SECTION: III
REV: 03 DATE: 06-Oct-2014
TIME CONTROLLED ITEMS
Time controlled items section contains tasks that are controlled by Rotable Requirements and linked to exact serial number on the A/C. Either
component removal or with “on-wing” maintenance in particular cases may satisfy the requirement of the task.
Operator specific TCI selection could e.g. reflect components, which often (or likely) rotate between A/C due to unscheduled and scheduled
replacements.
NOTE: Time Controlled tasks introduced in the separate section only for the planning convenience. This division is demanded neither by any source
document nor by any certification authority.
Sub 1 - Page 1 of 1
MP REF: SDM.A320.BDCA
SECTION: III
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
TIME CONTROLLED ITEMS
R
E
V
TASK
NUMBER
212652-01-1
ZONE
127
DESCRIPTION
AVIONICS VENT SKIN AIR INLET VALVE (SAIV)
SKILL TASK
CODE CODE
ACCESS PANELS: 824
AVIONICS VENT SKIN AIR OUTLET VALVE (SAOV)
212653-02-1
126
210
MEN
TASKM. APPLICABI
H.
LITY
SIL
LUR
212652-000-802
SIL 21-159
1
1.32
ALL
AF
RST
I:
7500 FH
OR
24 MO
NOTE
MRB 6
LUR
212653-000-001
SIL 21-099
1
1.27
0649 1560
2151 2163
SOURCE:
MRB 21.26.00/23
AF
RST
SIL
LUR
212653-000-803
SIL 21-159
1
1.27
NOTE: MPD INTERVAL IS 18000 FH OR 120 MO. TRIAL INTERVAL REDUCTION TO
IMPROVE RELIABILITY. ORIGINAL MPD INTERVAL MAY BE APPLIED FOR THE
PLANNING PURPOSES
PRESSURE CONTROL AND MONITORING
AF
I:
7500 FH
OR
24 MO
NOTE
FNC
I:
24000 FH
OR
80 MO
CMR**
MRB 6,9
213100-720-001
2
0.83
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
ALL
I:
50000 FH
OR
210 MO
MRB 9
1
0.65
ALL
REMOVE SKIN AIR OUTLET VALVE FOR OVERHAUL
213100-05-1
REFERENCES
I:
7500 FH
OR
24 MO
NOTE
REMOVE SKIN AIR OUTLET VALVE FOR OVERHAUL
NOTE: MPD INTERVAL IS 12000 FH OR 80 MO. TRIAL INTERVAL REDUCTION TO
IMPROVE RELIABILITY. ORIGINAL MPD INTERVAL MAY BE APPLIED FOR THE
PLANNING PURPOSES
AVIONICS VENT SKIN AIR OUTLET VALVE (SAOV)
TPS
RST
NOTE: MPD INTERVAL IS 18000 FH OR 120 MO. TRIAL INTERVAL REDUCTION TO
IMPROVE RELIABILITY. ORIGINAL MPD INTERVAL MAY BE APPLIED FOR THE
PLANNING PURPOSES
126
SOURCE
AF
REMOVE SKIN AIR INLET VALVE FOR OVERHAUL
212653-01-1
INTERVALS
FUNCTIONAL CHECK OF POSITIVE/NEGATIVE DELTA "P"
PROTECTION OF THE SAFETY VALVES.
SOURCE:
CMR 213100-00001-1-C
CMR 213100-00001-2-C
CMR 213100-00001-3-C
MRB 21.31.00/06
NOTE:
- THE FUNCTIONAL CHECK MAY ALTERNATIVELY BE ACCOMPLISHED AS AN
OFF AIRCRAFT TASK.
- THE CHECK OF POSITION INDICATION OF SAFETY VALVES IS PART OF THIS
TASK AFTER THE FUNCTIONAL CHECK/RE-INSTALLION.
- REFER TO ALS PART 3 FOR THE CMR** REQUIREMENTS COVERED BY THIS
TASKS FOR DIFFERENT AIRCRAFT CONFIGURATIONS.
PREPARATION: ACCESS THROUGH REAR GALLEY WALL REQUIRED;
213100-08-1
260
ACCESS PANELS: 312AR
PRESSURE CONTROL AND MONITORING
REMOVE SAFETY VALVE FOR RESTORATION
AF
RST
213100-600-001
SOURCE:
MRB 21.31.00/07
PREPARATION: ACCESS THROUGH REAR GALLEY WALL REQUIRED;
Sub 2 - Page 1 of 13
MP REF: SDM.A320.BDCA
SECTION: III
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
TIME CONTROLLED ITEMS
R
E
V
TASK
NUMBER
215141-01-1
ZONE
130
DESCRIPTION
AIR COOLING AND TEMPERATURE CONTROL
SKILL TASK
CODE CODE
AF
FNC
REMOVE OZONE CONVERTER FOR FUNCTIONAL CHECK
215200-01-1
191
192
NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL
MAY BE USED.
AIR CONDITIONING PACK
AF
RST
REMOVE PRIMARY AND MAIN HEAT EXCHANGERS FOR CLEANING.
NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY
BE USED.
215200-02-1
191
192
ACCESS PANELS: 191KB, 192KB
AIR CONDITIONING PACK
AF
RST
REMOVE REHEATER FOR CLEANING.
215200-02-2
191
192
ACCESS PANELS: 191KB, 192KB
AIR CONDITIONING PACK
AF
RST
REMOVE REHEATER FOR CLEANING.
215200-04-1
191
192
ACCESS PANELS: 191KB, 192KB
AIR CONDITIONING PACK
AF
FNC
REMOVE CONDENSER FOR LEAK CHECK
215222-01-1
191
192
ACCESS PANELS: 191KB, 192KB
AIR CYCLE MACHINE
AF
DET
DETAILED INSPECTION OF INTERIOR AND EXTERIOR OF
PLENUM CHAMBER (10HM5 AND 11HM5) FOR SIGNS OF
DELAMINATION
NOTE: TO BE ACCOMPLISHED WITH TASK 215200-01-1
INTERVALS
SOURCE
I:
9000 FH
OR
60 MO
NOTE
MRB 9
LUR
I:
12000 FH
OR
80 MO
NOTE
MRB 9
LUR
I:
5500 FH
OR
48 MO
MRB 9
LUR
I:
12000 FH
OR
80 MO
TPS
REFERENCES
215141-920-001
MEN
TASKM. APPLICABI
H.
LITY
1
0.30
2
2
1.00
1.00
215200-100-002
SIL 21-067
2
2
0.42
0.42
0649
MRB 9
LUR
SOURCE:
MRB 21.50.00/18
215200-100-002
SIL 21-067
2
2
0.42
0.42
I:
18000 FH
OR
120 MO
MRB 9
LUR
SOURCE:
MRB 21.50.00/15
215200-790-001
SIL 21-067
2
2
1.00
1.00
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
ALL
I:
12000 FH
OR
80 MO
MRB 9
LUR
SOURCE:
MRB 21.50.00/16
215200-200-001
SIL 21-067
1
1
0.30
0.30
ALL
I:
6 YE
MRB 9
1
0.10
ALL
SOURCE:
MRB 21.50.00/10
215200-100-001
SIL 21-067
0649 1130
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890 2151
2163
ALL
SOURCE:
MRB 21.50.00/12
SOURCE:
MRB 21.50.00/19
PREPARATION: REMOVE HEAT EXCHANGER;
237135-01-1
312
ACCESS PANELS: 191KB, 192KB
COCKPIT VOICE RECORDER
DISCARD ULB BATTERY
RA
DIS
237135-920-001
SOURCE:
MRB 23.71.00/03
ACCESS PANELS: 312AR
Sub 2 - Page 2 of 13
MP REF: SDM.A320.BDCA
SECTION: III
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
TIME CONTROLLED ITEMS
R
E
V
TASK
NUMBER
242100-04-1
ZONE
438
448
DESCRIPTION
INTEGRATED DRIVE GENERATOR
SKILL TASK
CODE CODE
AF
OPC
INTERVALS
I:
NOTE
SOURCE
MRB 9
OPERATIONAL CHECK OF INTEGRATED DRIVE GENERATOR
(IDG) DISCONNECT AND RECONNECT FUNCTION.
242100-05-1
437
447
NOTE: TASK TO BE PERFORMED AT OPPORTUNITY OF
ENGINE CHANGE OR IDG CHANGE.
INTEGRATED DRIVE GENERATOR
243851-01-1
126
REFERENCES
242100-710-040
MEN
TASKM. APPLICABI
H.
LITY
2
2
0.20
0.20
ALL
1
1
0.20
0.20
ALL
1
0.15
ALL
1
0.15
ALL
2
2
2
2
0.30
0.30
0.30
0.30
ALL
SOURCE:
MRB 24.20.00/11
EN
RST
I:
NOTE
MRB 6
CLEAN INTEGRATED DRIVE GENERATOR (IDG) OIL
COOLER.
NOTE: TASK TO BE PERFORMED AT OPPORTUNITY OF
ENGINE SHOP VISIT.
DC GENERATION
TPS
731160-100-040
SOURCE:
MRB 24.20.00/12
EL
RST
I:
1 YE
MRB 6
243851-280-001
CMM 24-38-51
REMOVE BATTERY FOR OVERHAUL
SOURCE:
MRB 24.30.00/05
NOTE:
P/N 2758, VENDOR: SAFT
243851-02-1
126
ACCESS PANELS: 822
DC GENERATION
EL
RST
REMOVE BATTERY FOR CHECK IN WORKSHOP
VENDOR: SAFT P/N: 2758
I:
6 MO
NOTE
MRB 6
243851-280-802
CMM 24-38-51
SOURCE:
MRB 24.30.00/12
NOTE: PERIODICAL CHECK DURING THE A/C CHECK NEAREST TO 1,000
OPERATING HOURS REGULAR CHECK DURING THE A/C NEAREST TO 2,000
OPERATING HOURS OR AT MOST EVERY 6 MONTHS
256241-02-1
831
832
841
842
ACCESS PANELS: 822
DOOR ESCAPE SLIDE
REMOVE DOOR ESCAPE SLIDE/RAFT FOR HYDROSTATIC TEST OF INFLATION
RESERVOIR
AF
FNC
I:
3 YE
MRB 6,8
256200-750-001
SOURCE:
MRB 25.62.00/02`
NOTE:
TASK TO BE PERFORMED WITH 256241-03-1.
TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW DOORS /
EMERGENCY EXITS.
- AFTER 15 YEARS OF AGE, PERFORM CHECK/TEST INCL. HYDROSTATIC TEST
EVERY YEAR
- IF THE INFLATABLE, RESERVOIR, HOSE, AND APPLICABLE LIFE-LIMITED ITEMS
ARE REPLACED AT 15 YEARS, THEN THE STANDARD 3 YEAR MAINTENANCE
INTERVAL IS RE-INSTATED FOR THE NEXT 15 YEARS
Sub 2 - Page 3 of 13
MP REF: SDM.A320.BDCA
SECTION: III
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
TIME CONTROLLED ITEMS
R
E
V
TASK
NUMBER
256241-03-1
256241-04-1
ZONE
831
832
841
842
831
832
841
842
DESCRIPTION
DOOR ESCAPE SLIDE
SKILL TASK
CODE CODE
AF
RST
INTERVALS
I:
3 YE
SOURCE
MRB 8
REMOVE DOOR ESCAPE SLIDE/RAFT FOR RESTORATION
TPS
REFERENCES
256244-920-001
SOURCE:
MRB 25.62.00/03
NOTE:
- TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW DOORS /
EMERGENCY EXITS.
- AFTER 15 YEARS OF AGE, PERFORM RESTORATIONEVERY YEAR
- IF THE INFLATABLE, RESERVOIR, HOSE, AND APPLICABLELIFE-LIMITED ITEMS
ARE REPLACED AT 15 YEARS, THEN THE STANDARD 3 YEAR MAINTENANCE
INTERVAL IS RE-INSTATED FOR THE NEXT 15 YEARS
DOOR ESCAPE SLIDE
CA
OPC
OPERATIONAL CHECK OF FWD AND AFT PAX/CREW DOOR ESCAPE
SLIDES/RAFT DEPLOYMENT.
I:
3 YE
NOTE
MRB 8
I:
3 YE
MRB 6,8
256200-710-001
SOURCE:
MRB 25.62.00/04
MEN
TASKM. APPLICABI
H.
LITY
2
2
2
2
0.30
0.30
0.30
0.30
ALL
1
1
1
1
0.30
0.30
0.30
0.30
ALL
2
2
0.30
0.30
ALL
2
2
0.40
0.40
ALL
NOTE:
- TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW DOORS.
- ALTERNATE DOOR POSITION AT NEXT INTERVAL RECOMMENDED.
- AFTER 15 YEARS OF AGE, PERFORM RESTORATIONEVERY YEAR
- IF THE INFLATABLE, RESERVOIR, HOSE, AND APPLICABLELIFE-LIMITED ITEMS
ARE REPLACED AT 15 YEARS, THEN THE STANDARD 3 YEAR MAINTENANCE
INTERVAL IS RE-INSTATED FOR THE NEXT 15 YEARS
- THIS OPERATIONAL CHECK MUST BE PERFORMED, PEROPERATOR'S FLEET,
I.A.W THE FOLLOWING SAMPLING SCHEDULE: 1 FWD PASSENGER / CREW
DOOR, 1 AFT PASSENGER DOOR / CREW DOOR
- CHECKS MAY BE PERFORMED ON EITHER SIDE AND DO NOTALL HAVE TO BE
PERFORMED ON THE SAME AIRCRAFT
- INADVERTENT DEPLOYMENTS MAY NOT BE USED TO SATISFYTHE ABOVE
REQUIREMENT.A318/A319/A320/A321 FLEETS CAN BE COMBINED FOR COMMON
DOORS
256242-01-1
151
152
OFFWING ESCAPE SLIDE
AF
FNC
REMOVE OFFWING ESCAPE SLIDE GAS CYLINDER FOR HYDROSTATIC TEST
256200-750-002
SOURCE:
MRB 25.62.00/02
NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED EMERGENCY EXITS.
ACCESS PANELS: 151CW, 152CW
256242-02-1
191
192
OFFWING ESCAPE SLIDE
REMOVE OFFWING ESCAPE SLIDE FOR RESTORATION
AF
RST
I:
3 YE
MRB 8
256242-920-001
SOURCE:
MRB 25.62.00/03
NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED OR PASSENGER/CREW
DOORS / EMERGENCY EXITS.
ACCESS PANELS: 193AT, 194AT
Sub 2 - Page 4 of 13
MP REF: SDM.A320.BDCA
SECTION: III
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
TIME CONTROLLED ITEMS
R
E
V
TASK
NUMBER
256242-03-1
ZONE
830
840
DESCRIPTION
OFFWING ESCAPE SLIDE
SKILL TASK
CODE CODE
CA
OPC
OPERATIONAL CHECK OF OFF WING EMERGENCY EXIT ESCAPE SLIDE
DEPLOYMENT
256532-01-1
200
NOTE:
- TASK IS NOT APPLICABLE FOR DEACTIVATED EMERGENCY
EXITS.
- ALTERNATE DOOR POSITION AT NEXT INTERVAL RECOMMENDED
- AFTER 15 YEARS OF AGE, PERFORMRESTORATION EVERY YEAR
- IF THE INFLATABLE, RESERVOIR, HOSE,AND APPLICABLE LIFE-LIMITED ITEMS
ARE REPLACED AT 15 YEARS, THEN THE STANDARD 3 YEAR MAINTENANCE
INTERVAL IS RE-INSTATED FOR THE NEXT 15 YEARS
- THIS OPERATIONAL CHECK MUSTBEPERFORMED, PER OPERATOR´S FLEET,
I.A.W THE FOLLOWING SAMPLING SCHEDULE: 1 FWD PASSENGER / CREW
DOOR, 1 AFT PASSENGER DOOR / CREW DOOR
- CHECKS MAY BE PERFORMED ON EITHER SIDE AND DO NOT ALL HAVE TO BE
PERFORMED ON THE SAME AIRCRAFT
- INADVERTENT DEPLOYMENTS MAY NOT BE USED TO SATISFY THE ABOVE
REQUIREMENT. A318/A319/A320/A321 FLEETS CAN BE COMBINED FOR
COMMON DOORS
PORTABLE EMERGENCY BEACON TRANSMITTER
CA
FNC
INTERVALS
SOURCE
I:
3 YE
NOTE
MRB 8
I:
NOTE
MRB 9
256532-01-2-SDM
200
REFERENCES
256200-710-002
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.10
0.10
ALL
1
0.20
ALL
SOURCE:
MRB 25.62.00/04
REMOVE THE EMERGENCY LOCATOR TRANSMITTER FOR WORKSHOP TEST
(BATTERY CHECK & FUNCTIONAL CHECK)
NOTE:
5 YE: PN 1151324-1M273; 1151324-1M310
3 YE: PN 94N6097; S1823502-03
PORTABLE EMERGENCY BEACON TRANSMITTER
TPS
256500-720-001
SOURCE:
MRB 25.65.32/01
CA
FNC
I:
6 MO
S-ICA
JIC A320-25-65-01
1
0.20
1200 1379
2151 2163
CA
FNC
I:
5 YE
S-ICA
JIC A320-25-65-02
1
0.20
1200 1379
2151 2163
EL
OPC
I:
24 MO
MRB 8
256500-710-001
1
0.10
ALL
MRB 8
SOURCE:
MRB 25.65.35/01
256500-720-004
2
0.50
ALL
OPERATIONAL CHECK OF ELT USING BITE TEST
256532-02-2-SDM
200
PN 500-12Y
PORTABLE EMERGENCY BEACON TRANSMITTER
REPLACE BATTERY OF PORTABLE ELT
256535-01-1
200
PN 500-12Y
ELT (REAR FUSELAGE)
OPERATIONAL CHECK OF ELT SYSTEM BY MANUAL ACTIVATION
256535-02-1
200
ELT (REAR FUSELAGE)
REMOVE ELT FOR BATTERY REPLACEMENT AND OPERATIONAL CHECK OF
ACCELERATION SENSOR
EL
RST
I:
5 YE
SOURCE:
MRB 25.65.35/02
Sub 2 - Page 5 of 13
MP REF: SDM.A320.BDCA
SECTION: III
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
TIME CONTROLLED ITEMS
R
E
V
TASK
NUMBER
256652-01-1
ZONE
200
DESCRIPTION
LIFE VESTS
SKILL TASK
CODE CODE
CA
RST
INTERVALS
I:
NOTE
SOURCE
MRB 8
RESTORATION OF LIFE VESTS
261700-04-1
200
NOTE: CONTROLLED BY TASK 256000-01-1-SDM
LAVATORY SMOKE DETECTION
415
425
ENGINE FIRE EXTINGUISHER BOTTLES
EL
RST
CA
FNC
I:
12000 FH
OR
80 MO
I:
10 YE
MRB 9
LUR
MRB 6,9
HYDROSTATIC TEST OF BOTTLES INCLUDING CHECK SETTING
OF PRESSURE SWITCH
262142-01-1
415
425
ACCESS PANELS: 415BL, 415BR, 425BL, 425BR
ENGINE FIRE EXTINGUISHER BOTTLE CARTRIDGES
313
ACCESS PANELS: 415BL, 415BR, 425BL, 425BR
APU FIRE EXTINGUISHER BOTTLE
EL
DIS
I:
10 YE
MRB 9
313
ACCESS PANELS: 314AR
APU FIRE EXTIR BOTTLE CARTRIDGE
CA
FNC
I:
10 YE
MRB 6,8
132
ACCESS PANELS: 314AR
CARGO COMPARTMENT FIRE EXTINGUISHING
EL
DIS
I:
10 YE
MRB 8
132
ACCESS PANELS: 132SW, 825
CARGO COMPARTMENT FIRE EXTINGUISHING
AV
DIS
I:
10 YE
MRB 8
132
ACCESS PANELS: 132MW, 825
CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE
REMOVE CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE
FOR WEIGHT CHECK
ALL
261715-100-003
1
0.30
ALL
SOURCE:
MRB 26.17.00/04
262141-280-002
SIL 96-2
1
1
0.20
0.20
ALL
1
1
0.25
0.25
ALL
1
0.40
ALL
1
0.50
ALL
1
0.40
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.40
1130 1200
1379 1578
1657 1767
2151 2163
1
0.40
0649 1488
1560 1743
1761 1851
1863 1876
1890
262141-920-001
262241-280-002
262242-920-001
262341-920-001
SOURCE:
MRB 26.23.00/05
AV
DIS
I:
10 YE
MRB 8
REMOVE AND DISCARD CARGO COMPARTMENT FIRE
EXTINGUISHER BOTTLE CARTRIDGES
262341-01-1
0.40
SOURCE:
MRB 26.22.00/04
REMOVE AND DISCARD CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE
CARTRIDGES
262300-04-3
1
SOURCE:
MRB 26.22.00/03
DISCARD CARTRIDGE
262300-04-1
TASKM. APPLICABI
H.
LITY
SOURCE:
MRB 26.21.00/06
HYDROSTATIC TEST OF BOTTLE INCLUDING CHECK OF PRESSURE SWITCH
SETTING
262242-01-1
256652-920-001
MEN
SOURCE:
MRB 26.21.00/07
DISCARD CARTRIDGE
262241-01-1
REFERENCES
SOURCE:
MRB 25.66.52/01
REMOVE FOR CLEANING
262141-02-1
TPS
262341-920-001
SOURCE:
MRB 26.23.00/05
CA
FNC
I:
22500 FH
OR
72 MO
MRB 8
262341-280-001
SOURCE:
MRB 26.23.00/01
ACCESS PANELS: 132SW, 825
Sub 2 - Page 6 of 13
MP REF: SDM.A320.BDCA
SECTION: III
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
TIME CONTROLLED ITEMS
R
E
V
TASK
NUMBER
262341-01-2
ZONE
132
DESCRIPTION
CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE
SKILL TASK
CODE CODE
CA
FNC
REMOVE CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE
FOR WEIGHT CHECK
262341-02-1
132
ACCESS PANELS: 132MW, 825
CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE
CA
FNC
INTERVALS
SOURCE
I:
22500 FH
OR
72 MO
MRB 8
I:
10 YE
MRB 6,8
TPS
262341-280-001
132
ACCESS PANELS: 132SW, 825
CARGO COMPARTMENT FIRE EXTINGUISHER
BOTTLE
262341-280-002
200
ACCESS PANELS: 132MW, 825
PORTABLE FIRE EXTINGUISHER
CA
FNC
I:
10 YE
MRB 6,8
262341-280-002
200
PORTABLE FIRE EXTINGUISHER
CA
FNC
I:
10 YE
200
ACCESS PANELS: 831
PORTABLE FIRE EXTINGUISHER
200
ACCESS PANELS: 831
PORTABLE FIRE EXTINGUISHER
1130 1200
1379 1578
1657 1767
2151 2163
1
0.40
0649 1488
1560 1743
1761 1851
1863 1876
1890
1
0.40
1130 1200
1379 1578
1657 1767
2151 2163
262400-280-001
1
0.20
MRB 9
SOURCE:
MRB 26.24.00/02
262400-210-003
0649 1200
1379 2151
2163
CA
FNC
I:
1 YE
1
0.10
ALL
1
0.10
1
0.20
262500-200-003
1
0.20
1488 1560
1578 1743
1761 1851
1863 1876
1890
1130 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
ALL
SOURCE:
MRB 26.25.00/02
272641-280-001
1
0.20
ALL
SOURCE:
MRB 26.24.00/03
CA
FNC
I:
1 YE
MRB 9
262400-280-002
WEIGHT CHECK OF PROPELLANT CARTRIDGE
262441-05-1
0.40
MRB 9
WEIGHT CHECK OF PORTABLE FIRE EXTINGUISHER
262441-04-1
1
SOURCE:
MRB 26.23.00/06
HYDROSTATIC TEST OF BOTTLES
262441-03-1
TASKM. APPLICABI
H.
LITY
SOURCE:
MRB 26.23.00/06
REMOVE CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE FOR
HYDROSTATIC TEST AND CHECK OF PRESSURE SWITCH SETTING
262441-02-1
MEN
SOURCE:
MRB 26.23.00/01
REMOVE CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE FOR
HYDROSTATIC TEST AND CHECK OF PRESSURE SWITCH SETTING
262341-02-2
REFERENCES
SOURCE:
MRB 26.24.00/04
CA
DIS
I:
10 YE
MRB 9
T
262400-280-001
DISCARD PORTABLE FIRE EXTINGUISHER
SOURCE:
MRB 26.24.00/05
ACCESS PANELS: 831
262541-02-1
200
LAVATORY FIRE EXTINGUISHER BOTTLE
CA
FNC
I:
72 MO
MRB 9
REMOVE LAVATORY FIRE EXTINGUISHER BOTTLE FOR WEIGHT CHECK
272100-04-1
325
RUDDER MECHANICAL CONTROL
REMOVE YAW DAMPER SPRING ROD FOR WORKSHOP CHECK
AF
OPC
I:
24000 FH
OR
156 MO
MRB 9
LUR
SOURCE:
MRB 27.21.00/04
ACCESS PANELS: 325BL
Sub 2 - Page 7 of 13
MP REF: SDM.A320.BDCA
SECTION: III
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
TIME CONTROLLED ITEMS
R
E
V
TASK
NUMBER
275117-01-1
ZONE
212
DESCRIPTION
FLAP/SLAT COMMAND SENSOR UNIT
SKILL TASK
CODE CODE
AF
FNC
INTERVALS
I:
40 MO
SOURCE
540
640
MAIN FUEL PUMP SYSTEM
AF
FNC
I:
144 MO
275117-280-001
MRB 8
SOURCE:
MRB 27.50.00/07
MRB 27.50.01/07
MRB 27.80.00/05
282100-720-802
REMOVE AIR RELEASE VALVE FOR FUNCTIONAL CHECK OF FLOAT
292000-11-1
195
ACCESS PANELS: 540CB
640CB
AUXILIARY HYDRAULIC POWER
REFERENCES
MRB 8
REMOVE CSU FOR WORKSHOP CHECK OF FRICTION BRAKE
282100-10-1
TPS
MEN
TASKM. APPLICABI
H.
LITY
1
0.30
ALL
1
1
TBD
TBD
ALL
0
N/A
ALL
1
0.25
ALL
0
0
N/A
N/A
ALL
0
N/A
ALL
SOURCE:
MRB 28.21.00/10
AF
RST
REMOVE RAT AND ACTUATOR FOR OVERHAUL AND REPLACE WITH NEW OR
RECONDITIONED UNITS.
T:
20 YE
I:
20 YE
ASM
I:
6 YE
MRB 9
292200-960-001
SOURCE:
ASM 292200-00001-1-E
PREPARATION: RAT; RAT ACTUATOR;
313300-01-1
312
ACCESS PANELS: 147BB, 147CB, 195BB, 734
DFDR SYSTEM INTERCONNECTION
AV
DIS
DISCARD UNDERWATER LOCATOR BEACON BATTERY
321111-01-2
731
741
ACCESS PANELS: 312AR
MAIN LANDING GEAR
SOURCE:
MRB 31.33.00/02
AF
SDI
SPECIAL DETAILED INSPECTION (OVERHAUL) OF MAIN GEAR
(OFF AIRCRAFT)
I:
120 MO
OR
20000 FC
MRB CPCP
MRB 5,8
321111-920-001
APPENDIX 7
I:
120 MO
OR
20000 FC
MRB CPCP
MRB 5,8
SOURCE:
MRB 32.11.00/14
MRB 32.11.00/19
MRB 321105-03-1
MRB 321110-03-1
MRB 321111-02-1
MRB 321116-02-1
MRB 321128-03-1
MRB 321141-01-1
MRB 321169-01-1
322100-200-802
APPENDIX 7
PREPARATION: AIRCRAFT JACKING; MAIN LANDING GEAR REMOVAL;
ACCESS PANELS: 734, 744
322111-01-1
710
NOSE LANDING GEAR
SPECIAL DETAILED INSPECTION (OVERHAUL) OF NOSE GEAR (OFF AIRCRAFT)
PREPARATION: NLG REMOVED; AIRCRAFT JACKING;
ACCESS PANELS: 713, 714, 734
313355-920-001
AF
SDI
SOURCE:
MRB 32.21.00/05
MRB 32.50.00/02
MRB 322105-03-1
MRB 322110-03-1
Sub 2 - Page 8 of 13
MP REF: SDM.A320.BDCA
SECTION: III
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
TIME CONTROLLED ITEMS
R
E
V
TASK
NUMBER
323100-08-1
ZONE
711
DESCRIPTION
NORMAL EXTENSION AND RETRACTION
SKILL TASK
CODE CODE
AF
SDI
SPECIAL DETAILED INSPECTION (OVERHAUL) OF THE NOSE LANDING GEAR
ACTUATING CYLINDER AND GEAR ATTACHMENT PIN (OFF AIRCRAFT).
INTERVALS
I:
10 YE
OR
20000 FC
SOURCE
ISB
MRB CPCP
VSB
PREPARATION: ACTUATING CYLINDER - NLG;
731
741
NORMAL EXTENSION AND RETRACTION
REFERENCES
323122-920-001
ISB 32-1307
VSB 580-32-3160
APPENDIX 7
MEN
TASKM. APPLICABI
H.
LITY
0
N/A
ALL
0
0
N/A
N/A
ALL
SOURCE:
MRB 322152-01-1
MRB 322158-01-1
ACCESS PANELS: 713, 714
323100-09-1
TPS
AF
SDI
SPECIAL DETAILED INSPECTION (OVERHAUL) OF THE MAIN
LANDING GEAR RETRACTION ACTUATOR AND ATTACHMENT PINS
(OFF AIRCRAFT)
I:
10 YE
OR
20000 FC
MRB CPCP
323100-220-002
APPENDIX 7
SOURCE:
MRB 321147-01-1
MRB 321171-01-1
PREPARATION: RETRACTION ACTUATOR REMOVED.;
344200-02-1
150
ACCESS PANELS: 734, 744
RADIO ALTIMETER
RA
DIS
I:
144 MO
SIL
344211-920-001
SIL 34-097
1
11.42
ALL
AF
FNC
I:
3 YE
MRB 5
351141-750-002
1
0.20
ALL
RADIO ALTIMETER ANTENNAS AND COAXIAL CABLES
REPLACEMENT.
351141-01-1
125
ACCESS PANELS: 151AG, 151UF, 152AG, 152GW, 152HW, 152MF, 152NF
CREW OXYGEN CYLINDER
HYDROSTATIC TEST OF OXYGEN CYLINDER
351241-02-1
352142-01-1
210
ACCESS PANELS: 812
CREW OXYGEN MASK REGULATORS
200
REMOVE FOR FUNCTIONAL CHECK OF MASK REGULATOR
ASSEMBLY
OXYGEN GENERATORS
SOURCE:
MRB 35.10.00/05
AF
AF
FNC
DIS
I:
6 YE
I:
15 YE
MRB 9
351241-750-001
1
1.00
ALL
MRB 9
SOURCE:
MRB 35.10.00/04
352100-920-001
1
5.40
ALL
MRB 9
SOURCE:
MRB 35.20.00/03
353242-750-001
1
0.30
ALL
1
0.20
ALL
DISCARD OXYGEN GENERATORS
353000-02-1
353000-06-1
200
PORTABLE OXYGEN
200
REMOVE PORTABLE OXYGEN CYLINDER ASSEMBLY FOR HYDROSTATIC TEST
(INCLUDING FUNCTIONAL CHECK OF OXYGEN REGULATOR AND LP RELIEF
VALVE)
PROTECT. BREATHING EQPT (CKPT & CABIN)
DISCARD PROTECTIVE BREATHING EQUIPMENT
AF
FNC
I:
5 YE
SOURCE:
MRB 35.30.00/02
AF
DIS
I:
10 YE
MRB 8
353000-920-001
SOURCE:
MRB 35.30.00/05
Sub 2 - Page 9 of 13
MP REF: SDM.A320.BDCA
SECTION: III
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
TIME CONTROLLED ITEMS
R
TASK
E
NUMBER
V
R 492100-B5-1
ZONE
315
317
DESCRIPTION
POWER SECTION
SKILL TASK
CODE CODE
EN
DIS
INTERVALS
I:
NOTE
SOURCE
MRB 7
DISCARD LIFE LIMITED PARTS OF THE APU POWER
SECTION IN ACCORDANCE WITH OEM RECOMMENDATION
TPS
REFERENCES
492100-920-007
MEN
TASKM. APPLICABI
H.
LITY
0
0
N/A
N/A
ALL
0
0
N/A
N/A
ALL
0
0
N/A
N/A
ALL
0
0
N/A
N/A
ALL
1
1
3.00
3.00
0649
SOURCE:
MRB 49.21.00/05-13
NOTE: REFER TO APPROVED ENGINE MANUAL FOR INTERVAL.
PREPARATION: APU REMOVED;
722100-C1-1
430
440
ACCESS PANELS: 315AL, 316AR, 317AL
FAN AND BOOSTER ASSEMBLY
EN
DIS
I:
NOTE
MRB 5
DISCARD FAN DISC AND BOOSTER SPOOL
722100-920-001
SOURCE:
MRB 72.20.00/02-C5
NOTE: REFER TO APPROVED ENGINE MANUAL FOR INTERVAL.
722100-C2-1
430
440
PREPARATION: ENGINE REMOVED;
FAN AND BOOSTER ASSEMBLY
EN
DIS
I:
NOTE
MRB 5
DISCARD FAN SHAFT
722100-920-002
SOURCE:
MRB 72.20.00/03-C5
NOTE: REFER TO APPROVED ENGINE MANUAL FOR INTERVAL.
723000-C1-1
450
460
PREPARATION: ENGINE REMOVED;
HP COMPRESSOR SECTION
EN
DIS
I:
NOTE
MRB 5
DISCARD LIFE LIMITED HP COMPRESSOR ROTATING PARTS
723000-920-001
SOURCE:
MRB 72.30.00/01-C5
NOTE: REFER TO APPROVED ENGINE MANUAL FOR INTERVAL.
723200-C2-1
450
460
PREPARATION: ENGINE REMOVED;
HIGH PRESSURE COMPRESSOR FRONT STATOR
ASSEMBLY
BORESCOPE INSPECTION FOR HPC STATOR-TO-ROTOR
CONTACT
EN
SDI
T:
24000 FH
NOTE
I:
600 FH
NOTE
VSB
VSB CFM56-5
72-766
NOTE: - CFM RECOMMENDS THAT YOU DO THIS INSPECTION
WITHIN 600 FLIGHT HOURS AFTER 24,000 HOURS TIME SINCE
NEW (TSN) OR 24,000 FLIGHT HOURS SINCE THE HPC INNER
AND OUTER VARIABLE STATOR VANE (VSV) BUSHINGS AND
OUTER WASHERS HAVE BEEN REPLACED WITH NEW (NOT
USED-SERVICEABLE) PARTS.
- RE-INSPECTION INTERVALS DEPEND ON THE AMOUNT OF
SERVICEABLE DISTRESS FOUND. REFER TO CFM56-5
SB 72-766 FOR THRESHOLD AND INTERVAL
ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR
Sub 2 - Page 10 of 13
MP REF: SDM.A320.BDCA
SECTION: III
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
TIME CONTROLLED ITEMS
R
E
V
TASK
NUMBER
724000-C1-1
ZONE
450
460
DESCRIPTION
COMBUSTION SECTION
SKILL TASK
CODE CODE
EN
SDI
BORESCOPE INSPECTION OF COMBUSTION CHAMBER LINERS,
DOME AREAS, HPT NOZZLE VANES AND SHROUDS (AS FAR AS
VISIBLE THROUGH TWO OPPOSITE PORTS)
INTERVALS
SOURCE
I:
1600 FC
OR
72 MO
MRB 9
LUR
I:
NOTE
MRB 5
TPS
REFERENCES
724100-290-001
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.60
0.60
ALL
0
0
N/A
N/A
ALL
0
0
N/A
N/A
ALL
1
1
0.40
0.40
ALL
1
1
0.05
0.05
ALL
1
1
0.20
0.20
ALL
SOURCE:
MRB 72.40.00/01-C5
ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR
725000-C2-1
450
460
TURBINE SECTION
EN
DIS
DISCARD LIFE LIMITED PARTS OF HPT AND LPT
725000-920-001
SOURCE:
MRB 72.50.00/02-C5
NOTE: REFER TO APPROVED ENGINE MANUAL FOR INTERVAL.
725000-C6-1
450
460
PREPARATION: ENGINE REMOVED;
TURBINE SECTION
EN
DET
I:
NOTE
MRB 6,9
SURVEILLANCE INSPECTION OF TURBINE FRAME AFT ENGINE
MOUNT LUGS
712212-210-001
SOURCE:
MRB 72.50.00/06-C5
NOTE: TASK TO BE PERFORMED AT OPPORTUNITY OF
ENGINE SHOP VISIT.
730000-C4-1
435
445
PREPARATION: ENGINE REMOVED;
ENGINE FUEL AND CONTROL
EN
DIS
REMOVE, INSPECT AND REPLACE FUEL FILTER ELEMENT
NOTE: - REMOVE AND REPLACE FILTER ELEMENT AT 150 FH, 750 FH AND 1500
FH AFTER A/C DELIVERY THEREAFTER EVERY 4000 FH OR 36 MO.
I:
4000 FH
OR
36 MO
NOTE
MRB 6
SIL
LUR
I:
7500 FH
OR
50 MO
I:
7500 FH
OR
50 MO
MRB 9
LUR
731110-920-001
SIL 73-024
SOURCE:
MRB 73.00.00/05-C5
- REMOVE AND REPLACE FILTER ELEMENT AT 150 FH AND 750 FH AFTER
MAJOR TANK INTERVENTION THEREAFTER EVERY 4000 FH OR 36 MO.
752000-C1-1
434
444
ACCESS PANELS: 437AL, 438AR, 447AL, 448AR
COOLING
EN
OPC
CHECK ECU AIR COOLING PIPE INLET/OUTLET FOR BLOCKAGE
752000-C3-1
452
462
COOLING
GENERAL VISUAL INSPECTION OF PIPING OF LPT CASE AIR COOLING
EN
GVI
MRB 9
LUR
752449-210-041
SOURCE:
MRB 75.20.00/01-C5
725400-210-003
SOURCE:
MRB 75.20.00/03-C5
ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR
Sub 2 - Page 11 of 13
MP REF: SDM.A320.BDCA
SECTION: III
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
TIME CONTROLLED ITEMS
R
E
V
TASK
NUMBER
752110-01-1-SDM
ZONE
400
DESCRIPTION
HIGH PRESSURE TURBINE CLEARANCE CONTROL VALVE (HPTCCV)
SKILL TASK
CODE CODE
INTERVALS
SOURCE
753100-01-1-SDM-LH
430
450
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
EN
RST
I:
NOTE
SPECI
752110-000-002
752110-400-002
752110-000-001
752110-400-001
2
5.00
ALL
EN
LUB
I:
1 YE
SPECI
JIC A320-75-31-00
CFM56-5B SB 75-0043
1
1
6
6
EN
LUB
I:
1 YE
SPECI
JIC A320-75-31-00
CFM56-5B SB 75-0043
1
1
6
6
EN
RST
I:
10000 FH
SPECI
752110-000-002
753120-400-002
753120-000-001
753120-400-001
2
4.00
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
ALL
EN
DET
I:
3000 FH
MRB 6
781112-210-041
AOL CFM 56-003
SB RA320 78-65
1
1
0.42
0.42
0649
1
1
0.30
0.30
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
REMOVE FOR RESTORATION HPTCCV AND REPLACE WITH THE OVERHAULED
OR NEW ONE
NOTE: EFFECTIVE ONLY FOR THE FOLLOWING PARTNUMBERS
PN 329695-3/-4 AND PN 326635-2/-3/-4 EVERY 10000 FH
PN 329695-5 OR PN 324685-4/-5 EVERY 15000 FH
VBV SYSTEM LUBRICATION
TPS
LUBRICATE VBV SYSTEM OF THE ENGINE
PREPARATION: OPEN ENGINE COWLS
753100-01-1-SDM-RH
440
460
VBV SYSTEM LUBRICATION
LUBRICATE VBV SYSTEM OF THE ENGINE
PREPARATION: OPEN ENGINE COWLS
R 753120-01-1-SDM
400
BLEED VALVE STOP MECHANISM
REMOVE FOR RESTORATION BLEED VALVE STOP MECHANISM AND REPLACE
WITH THE OVERHAULED OR NEW ONE
781112-C1-1
450
460
NOTE: PN 3282970-4
CENTERBODY
DETAILED INSPECTION OF THE EXHAUST CENTERBODY IN ACCORDANCE
WITH ROHR AOL CFM56-003.
792000-C4-2
435
445
DISTRIBUTION
REMOVE AND DISCARD SUPPLY FILTER
ACCESS PANELS: 437AL, 447AL
EN
DIS
I:
4000 FH
OR
36 MO
MRB 9
LUR
SOURCE:
MRB 78.11.00/04-C5
792110-920-002
SOURCE:
MRB 79.20.00/06-C5
Sub 2 - Page 12 of 13
MP REF: SDM.A320.BDCA
SECTION: III
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
TIME CONTROLLED ITEMS
R
E
V
TASK
NUMBER
792000-C7-1
ZONE
435
445
DESCRIPTION
DISTRIBUTION
SKILL TASK
CODE CODE
EN
DET
CHECK OF FWD SUMP, AFT SUMP, AGB, AND TGB SCAVENGE
SCREENS
INTERVALS
SOURCE
I:
3000 FH
OR
20 MO
MRB 6
LUR
I:
600 FH
OR
6 MO
MRB 6
LUR
I:
3000 FH
OR
20 MO
MRB 9
LUR
I:
400 DY
MRB
TPS
REFERENCES
790000-281-003
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.40
0.40
1
1
0.60
0.60
1
1
0.45
0.45
1
1
1
1
0.10
0.10
0.10
0.10
1
1
1
1
0.10
0.10
0.10
0.10
SOURCE:
MRB 79.20.00/05-C5
ACCESS PANELS: 437AL, 447AL
792000-C8-1
435
445
DISTRIBUTION
EN
DET
CHECK MASTER MAGNETIC CHIP DETECTOR FOR PARTICLES
SOURCE:
MRB 72.20.00/05-C5
MRB 79.20.00/07-C5
ACCESS PANELS: 437AL, 447AL
792000-C9-1
435
445
DISTRIBUTION
EN
OPC
OPERATIONAL CHECK OF THE MASTER CHIP DETECTOR REMOTE INDICATION
ZL-435-01-1
ZL-453-01-1
435
436
445
446
453
454
463
464
FAN AND ACCESSORY GEAR BOX
EN
GVI
GENERAL VISUAL INSPECTION OF HOT SECTION (EWIS)
790000-200-001
SOURCE:
MRB 79.20.00/08-C5
GENERAL VISUAL INSPECTION OF FAN AND ACCESSORY GEAR
BOX (EWIS)
ACCESS PANELS: 437AL, 438AR, 447AL, 448AR
HOT SECTION
790000-281-002
052430-200-002
SOURCE:
MRB ZL-435-01-1
EN
GVI
I:
16 MO
MRB
052450-200-002
SOURCE:
MRB ZL-453-01-1
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
ALL
ALL
ACCESS PANELS: 451AL, 452AR, 461AL, 462AR
Sub 2 - Page 13 of 13
SDM A319/A320 MAINTENANCE PROGRAM
MOD CONTROLLED ITEMS
MP-REF: SDM.A320.BDCA
SECTION: IV
REV: 03 DATE: 06-Oct-2014
IV. MOD CONTROLLED ITEMS
This section is for maintenance program tasks that are controlled by MODs due to complex interval/threshold parameters. For the aircraft last done
and due status refer to the corresponding MOD document status.
Sub 1 - Page 1 of 1
MP REF: SDM.A320.BDCA
SECTION: IV
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
MOD CONTROLLED ITEMS
R
E
V
TASK
NUMBER
254000-03-1
ZONE
200
DESCRIPTION
LAVATORIES
SKILL TASK
CODE CODE
127
128
127
128
AVIONICS COMPARTMENT
334
344
ELEVATOR AND HYDRAULIC ACTUATION
MEN
TASKM. APPLICABI
H.
LITY
EASA AD
FAA AD
ISB
254000-220-001
EASA AD
2010-0148
FAA AD
2006-09-11
ISB 25-1365
1
2.00
0649 1130
1379 1578
1657
NDT
SDI
T:
20000 FC
I:
500 FC
EASA AD
ISB
257100-290-001
EASA AD
2012-0134
ISB 25A1555
1
1
1.75
1.75
1379 1488
1657 1743
1767 2151
2163
NDT
SDI
T:
20000 FC
I:
500 FC
EASA AD
ISB
257100-290-002
EASA AD
2012-0134
ISB 25A1555
1
1
1.75
1.75
1379 1488
1657 1743
1767 2151
2163
NDT
SDI
I:
5000 FC
NOTE
EASA AD
FAA AD
ISB
EASA AD
2010-0046
FAA AD
2011-19-04
ISB 27A1186
1
1
3.00
3.00
ALL
AF
DET
I:
12000 FH
OR
40 MO
MRB 6,8
274451-220-002
1
0.15
ALL
BORESCOPE INSPECTION OF THE 80VU RACK LOWER CENTRAL FITTINGS AND
VISUAL INSPECTION OF THE UPPER FITTINGS AND CENTRAL SHELVE FITTINGS
273400-07-1
REFERENCES
T:
2400 FH
OR
15 MO
I:
15 MO
NOTE
BORESCOPE INSPECTION OF THE 80VU RACK LOWER LATERAL FITTINGS AND
VISUAL INSPECTION OF THE UPPER FITTINGS AND CENTRAL SHELVE FITTINGS
257100-02-1
TPS
DET
NOTE:- REFER TO ISB 25-1365 FIGURE 1 SHEET 1 FLOW
CHART FOR FURTHER DETAILS
257100-01-1
SOURCE
AF
DETAILED INSPECTION OF LAVATORY WALL
- TASK NOT APPLICABLE IF COMPOSITE REPAIR I.A.W.
CMM ACCOMPLISHED REFER TO ISB 25-1365 FIGURE 1
SHEET 1 FLOW CHART FOR FURTHER DETAILS.
AVIONICS COMPARTMENT
INTERVALS
SPECIAL DETAILED INSPECTION OF ELEVATOR SERVOCONTROL
ROD EYE-ENDS
NOTE:
-REFER TO EASA AD 2010-0046/FAA AD 2011-19-04 AND
ISB 27A1186 FOR IMPLEMENTATION PERIODS AND TIME
UNTIL FIRST REPEAT ON SERVICE AIRCRAFT
274451-05-1
310
ACCESS PANELS: 334DB, 344DB
THS ACTUATOR
DETAILED INSPECTION OF UPPER AND LOWER THS ACTUATOR ATTACHMENT
(PRIMARY AND SECONDARY)
SOURCE:
MRB 27.40.00/10
NOTE: ENSURE THAT INSPECTIONS ACCORDING 274451-10-1 AND 274451-11-1
ARE CARRIED OUT PRIOR TO TASK 274451-05-1 (AND PRIOR TO ANY
CLEANING), WHEN PLANNED AT THE SAME TIME
ACCESS PANELS: 312AR
Sub 2 - Page 1 of 5
MP REF: SDM.A320.BDCA
SECTION: IV
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
MOD CONTROLLED ITEMS
R
E
V
TASK
NUMBER
274451-10-1
ZONE
310
DESCRIPTION
THS ACTUATOR
SKILL TASK
CODE CODE
INTERVALS
SOURCE
ACCESS PANELS: 312AR
THS ACTUATOR
EASA AD
FAA AD
ISB
274451-220-003
EASA AD
2008-0150
FAA AD
2007-06-02
ISB 27-1164
1
3.50
ALL
AF
DET
T:
22 YE
NOTE
I:
24 MO
NOTE
ISB
OIT
274451-220-802
EASA AD 2012-0175
ISB 27-1214
OIT 999.0021/12
1
2.00
ALL
AF
OPC
T:
800 FC
I:
8 DY
AOT
EASA AD
FAA AD
ISB
AOT 32A1390
EASA AD 2011-0288
FAA AD 2011-13-11
ISB 32-1390
1
1
0.05
0.05
NDT
SDI
ISB
ISB 53-1258
1
15.00
NDT
SDI
T:
24000 FC
OR
48000 FH
I:
7500 FC
OR
15000 FH
T:
NOTE
I:
NOTE
EASA AD
FAA AD
ISB
533100-210-044
EASA AD
2011-0134
FAA AD
2004-13-06
ISB 53-1060
1
2.00
1130 1200
1379 1578
1657 1767
1851 1876
1890 2151
2163
0649 1130
1200 1379
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890 2163
0649 1130
1200 1379
1488
NOTE:
- TO BE ACCOMPLISHED BEFORE ACCUMULATING 22 YEARS, BUT NOT
BEFORE 20 YEARS SINCE THSA FIRST FLIGHT. SEE EASA AD 2012-0175 FOR
DETAILS OF COMPLIANCE.
- TASK INTERVAL IS RELATED TO EQUIPMENT LEVEL (THSA MONTH BASED)
AND NOT TO A/C LEVEL.
730
740
ACCESS PANELS: 312AR
NORMAL EXTENSION AND RETRACTION
OPERATIONAL CHECK OF THE MLG DOOR ACTUATOR
531258-01-1
240
SIDE BOX BEAM FLANGE
SPECIAL DETAILED INSPECTION (ROTO) OF THE SIDE
BOX BEAM FLANGE AT LH/RH IN S15 FR43 AREA
ACCESS PANELS: 241LF, 241MF, 242LF, 242MF
533142-01-1
190
RIVETED AREA OF KEEL BEAM SIDE PANEL
SPECIAL DETAILED INSPECTION (HFEC) OF RIVETED AREA
OF KEEL BEAM SIDE PANEL AT ATTACHMENT TO CENTER WING
BOX, LH/RH
TASKM. APPLICABI
H.
LITY
I:
20 MO
DETAILED INSPECTION OF THSA BALL SCREW SHAFT LOWER SPLINES
323105-02-1
MEN
DET
NOTE: PERFORM INSPECTION PRIOR TO TASK 274451-05-1 (IF PLANNED AT
THE SAME TIME) AND PRIOR TO ANY CLEANING.
INTERVAL STARTING POINT IS THE AIRCRAFT FIRST FLIGHT AND NOT
DELIVERY FLIGHT.
310
REFERENCES
AF
DETAILED INSPECTION OF THSA LOWER ATTACHMENTS FOR SECONDARY
LOAD PATH LOADING
274451-12-1
TPS
NOTE: FOR THRESHOLD AND INTERVAL, REFER TO SB 53-1060
REV 02.
ACCESS PANELS: 191KB, 192KB, 195BB, 196BB, 734, 744
Sub 2 - Page 2 of 5
MP REF: SDM.A320.BDCA
SECTION: IV
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
MOD CONTROLLED ITEMS
R
E
V
TASK
NUMBER
533154-03-1
ZONE
147
148
DESCRIPTION
MLG DOORS FITTINGS
SKILL TASK
CODE CODE
INTERVALS
SOURCE
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
NDT
SDI
T:
NOTE
I:
NOTE
EASA AD
FAA AD
ISB
533100-220-001
EASA AD
2012-0118
FAA AD
2009-20-05
ISB 53-1195
1
1
3.00
3.00
ALL
NDT
SDI
T:
NOTE
I:
NOTE
EASA AD
FAA AD
ISB
533100-220-001
EASA AD
2012-0118
FAA AD
2009-20-05
ISB 53-1196
1
1
2.50
2.50
ALL
NDT
SDI
T:
NOTE
I:
NOTE
CN
ISB
CN
2004-189(B)R1
ISB 53A1135
REV.3
ISB 53-1140
REV.2
ISB 53-1148
ISB 53-1149
ISB 53-1158
ISB 53-1160
1
1
2.00
2.00
0649 1130
1200 1379
1488
AF
DET
T:
NOTE
I:
500 FC
EASA AD
ISB
EASA AD
2012-0032
ISB 57A1166
1
1
1.25
1.25
0649 1130
1200 1379
1488 1560
1578 1657
1743 1761
1767
AF
DET
T:
NOTE
I:
500 FC
EASA AD
ISB
EASA AD
2012-0032
ISB 57-1168
1
1
1.25
1.25
1851 1863
1876 1890
2163
SPECIAL DETAILED INSPECTION (US AND HFEC) OF ACTUATOR FITTINGS FOR
MLG DOORS AT KEEL BEAM LH/RH (FOR TWIN WHEEL A/C OR FOR BOGIE A/C)
NOTE: FOR THRESHOLD AND INTERVAL, REFER TO AD 2012-0118
PREPARATION: ACTUATOR REMOVED;
533154-04-1
147
148
MLG DOORS FITTINGS
SPECIAL DETAILED INSPECTION (HFEC) OF THE KEEL BEAM MLG DOOR FWD
HINGE FITTING (FOR TWIN WHEEL A/C), OR OF THE KEEL BEAM MLG DOOR
CENTER-HINGE-FITTING (FOR BOGIE A/C), LH/RH
NOTE:
-FOR THRESHOLD AND INTERVAL, REFER TO AD 2012-0118.
533176-01-1
147
148
PREPARATION: ACTUATOR REMOVED;
MLG DOOR FITTINGS
SPECIAL DETAILED INSPECTION OF MLG DOOR ACTUATOR FITTING
ATTACHMENT AREA AT KEEL BEAM
NOTE: FOR DETAILS OF PLANNING AND ACCOMPLISHMENT OF TASK REFER
TO AD AND RELATED ISB´S
PREPARATION: NOTE;
575171-01-3
730
740
ACCESS PANELS: 734, 744
MAIN LANDING GEAR SUPPORT RIB 5 LUGS
DETAILED INSPECTION OF MAIN LANDING GEAR SUPPORT
RIB 5 LUGS.
NOTE: FOR THRESHOLD REFER TO ISB 57A1166.
575171-01-4
730
740
ACCESS PANELS: 734, 744
MAIN LANDING GEAR SUPPORT RIB 5 LUGS
DETAILED INSPECTION OF MAIN LANDING GEAR SUPPORT
RIB 5 LUGS.
NOTE: FOR THRESHOLD REFER TO ISB 57-1168.
ACCESS PANELS: 734, 744
Sub 2 - Page 3 of 5
MP REF: SDM.A320.BDCA
SECTION: IV
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
MOD CONTROLLED ITEMS
R
E
V
TASK
NUMBER
723100-C2-1
ZONE
450
460
DESCRIPTION
HPC ROTOR ASSEMBLY
SKILL TASK
CODE CODE
INTERVALS
SOURCE
TPS
REFERENCES
MEN
TASKM. APPLICABI
H.
LITY
EN
SDI
T:
NOTE
I:
NOTE
VSB
VSB CFM56-5B
72-0727
1
1
1.00
1.00
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151
EN
SDI
T:
24000 FH
NOTE
I:
600 FH
NOTE
VSB
VSB CFM56-5B
72-553
1
1
3.00
3.00
1200 1379
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890 2151
2163
EN
BSI
T:
10000 FH
I:
2000 FH
VSB
VSB 72-0246
CFM 56-5B
1
1
0.60
0.60
BORESCOPE INSPECTION OF HP COMPRESSOR STAGES 1, 3
AND 8
NOTE: REFER TO VSB 72-0727 FOR THRESHOLD AND INTERVAL
ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR
723200-C1-1
450
460
HIGH PRESSURE COMPRESSOR FRONT STATOR
ASSEMBLY
BORESCOPE INSPECTION FOR HPC STATOR-TO-ROTOR
CONTACT
NOTE: - CFM RECOMMENDS THAT YOU DO THIS INSPECTION
WITHIN 600 FLIGHT HOURS AFTER 24,000 HOURS TSN
(TIME SINCE NEW) OR 24,000 FLIGHT HOURS SINCE THE
HPC INNER AND OUTER VSV BUSHINGS AND OUTER WASHERS
HAVE BEEN REPLACED WITH NEW (NOT USED-SERVICEABLE)
PARTS.
- RE-INSPECTION INTERVALS DEPEND ON THE AMOUNT OF
SERVICEABLE DISTRESS FOUND. REFER TO CFM56-5B
SB 72-553 FOR THRESHOLD AND INTERVAL
ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR
D 724000-C3-1
450
460
COMBUSTION SECTION
BORESCOPE INSPECTION OF COMBUSTION CHAMBER OUTER COWL
ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR
Sub 2 - Page 4 of 5
MP REF: SDM.A320.BDCA
SECTION: IV
REV: 03 DATE:06-OCT-2014
SDM A319/A320 MAINTENANCE PROGRAM
MOD CONTROLLED ITEMS
R
E
V
TASK
NUMBER
725000-C1-3
ZONE
450
460
DESCRIPTION
TURBINE SECTION
SKILL TASK
CODE CODE
EN
SDI
BORESCOPE INSPECTION OF HPT BLADES (FROM THE FRONT
AND THE REAR)
INTERVALS
I:
1600 FC
OR
72 MO
NOTE
SOURCE
MRB 6
VSB
LUR
NOTE: - TASK INTERVAL ACCORDING TO CFM 56-5B
SB 72-240 FOR ENGINES WITH BLADES
P/N 1795M60P01
- TASK INTERVAL 1000 CY ACCORDING TO
CFM 56-5B SB 72-098 FOR ENGINES WITH
BLADES P/N 2002M52P03 / P04 / P05
- TASK INTERVAL IS 1600 FC OR 72 MO FOR ENGINES
WITH BLADES NOT MENTIONED IN PREVIOUS
NOTES
TPS
REFERENCES
725200-290-001
VSB 72-0098
CFM 56-5B
VSB 72-0240
CFM 56-5B
MEN
TASKM. APPLICABI
H.
LITY
1
1
0.60
0.60
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
SOURCE:
MRB 72.50.00/01-C5
ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR
725100-C1-1
725600-C3-1
450
460
450
460
HPT NOZZLE ASSEMBLY
EN
BSI
I:
NOTE
VSB
725100-290-003
VSB CFM 72-170
1
1
1.00
1.00
0649
BORESCOPE INSPECTION OF HIGH PRESSURE TURBINE
NOZZLE
NOTE :
- INITIAL AND SUBSEQUENT INSPECTIONS
AS PER SB (CFM56-5) 72-170
TURBINE FRAME ASSEMBLY
EN
SDI
T:
NOTE
I:
NOTE
EASA AD
FAA AD
VSB
1
1
TBD
TBD
EN
DET
I:
400 FH
AOL
VSB
EASA AD
2007-0221
EASA AD
2009-0110
FAA AD
2009-18-01
VSB CFM 56-5B
72-0620
781112-210-041
AOL CFM 56-003
VSB RA32078-65
1
1
0.42
0.42
1130 1200
1379 1488
1560 1578
1657 1743
1761 1767
1851 1863
1876 1890
2151 2163
0649 1130
1200 1379
1488 1560
1578 1657
1743 1761
1767 1851
1863 1876
1890
EDDY CURRENT INSPECTION OF THE 3 MOUNT STRUTS ( 1, 3
AND 14) OF TANGENTIAL STRUTS OF TURBINE REAR FRAME
NOTE: REFER TO VSB FOR THRESHOLD, INTERVAL AND
APPLICABLE PART NUMBERS.
781112-C1-2
450
460
CENTERBODY
DETAILED INSPECTION OF THE EXHAUST CENTERBODY IN ACCORDANCE
WITH ROHR AOL CFM56-003.
NOTE: CENTERBODY WITH P/N 238-0451-505, 238-0451-515, 238-0451-519 AND
238-0451-521 CAN BE INSPECTED EVERY 3000FH IF A REINFORCEMENT
DOUBLER HAS BEEN INSTALLED (POST VSB RA32078-65).
Sub 2 - Page 5 of 5
SDM A319/A320 MAINTENANCE PROGRAM
INDIVIDUAL STRUCTURAL INSPECTIONS
V.
MP-REF: SDM.A320.BDCA
SECTION: V
REV: 03 DATE: 06-Oct-2014
INDIVIDUAL STRUCTURAL INSPECTIONS
Section is dedicated to the individual structural inspections driven by Repairs and Damages. All the requirements given in this section are recorded
and monitored in the AMOS system.
All of these damages are recorded in the Structural Damage chart as well with the same item number as in this OMP.
A.
STRUCTURAL INSPECTIONS LAYOUT
1. MSN
Applicable MSN of the aircraft for the inspection to be performed on.
2. ITEM
Unique for the MSN structural damage chart item number.
3. REASON
Workorder reference and damage that caused individual structural inspection.
4. FURTHER ACTION
Description of the further action to be performed when the AC reaches limit WO.
5. PERIODIC INSPECTION
There can be either OMP taskcard number (in case inspection is covered by scheduled MP task and satisfies damage inspection requirements) or
special dedicated AD-HOC JIC with the unique number. AD-HOC JICs are handled same as common SRT.
Page 1 of 2
SDM A319/A320 MAINTENANCE PROGRAM
INDIVIDUAL STRUCTURAL INSPECTIONS
MP-REF: SDM.A320.BDCA
SECTION: V
REV: 03 DATE: 06-Oct-2014
6. LIMIT
Workorder unique number and it’s limitation in FH/FC/Calendar Date. Document contains all neseccary information to perform corrective action, links
to the documents related to the damage and repair.
By the limit given in Workorder corrective action should be performed and either new limit should be set or final repair performed.
B.
INSPECTIONS MAINTNENANCE PROGRAM
Refer to the next page.
Page 2 of 2
SDM A319/A320 MAINTENANCE PROGRAM
INDIVIDUAL STRUCTURAL INSPECTIONS
MSN
ITEM
0649
2
0649
2
0649
REASON
FURTHER ACTION
SKIN DENT BETWEEN STGR22-23 LH, FR21-22
MP REF: SDM.A320.BDCA
SECTION: V
REV: 03 DATE:06-OCT-2014
PERIODIC INSPECTION
LIMIT
IIR 53-11-11-1-001-00 First Inspection after Repair
Embodiment 60000FC (WO:500454255)
FWD CARGO DOOR SKIN ABOVE VENT LAP DENTS IIR 52-30-00-1-001-00 FIRST INSPECTION AFTER
(2EA)
REPAIR EMBODIMENT 60000FC (WO:500465021)
N/A
3
RH Fuselage Lower Shell Skin Dent
N/A
WO: 500471292
TAC: 72559
0649
4
WO: 500430015
Nick Bellow RH FWD Entry Door Aft Corner
IIR 53-11-11-1-001-00 FIRST INSPECTION FROM
TIME OF DENT OCCURRENCE 60000FC
(WO:500471292)
IIR 53-11-11-1-002-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 60000FC (WO:500471291)
N/A
WO: 500471291
TAC: 72559
0649
5
Stone Hit Between Fr 24A-24 Stgr 42-43 LH
IIR 53-21-11-1-003-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 60000FC (WO:500471184)
N/A
WO: 500471184
TAC: 75150
0649
26
WO: 500016648
Dent Between Fr. 7 & 8 RH Side Of Fuselage
N/A
WO: 500066450
TAC: 67474
0649
28
WO: 500016640
LH Side Fuselage below str 23 & FR 9-10 Dent Repair
IIR 53-11-11-1-001-00 FIRST INSPECTION FROM
TIME OF DENT OCCURRENCE 60000FC
(WO:500066450)
IIR 53-11-11-2-003-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 60000FC (WO:500066484)
N/A
WO: 500066484
TAC: 73997
0649
77
RDAS REQUIREMENTS FIRST INSPECTION AFTER
REPAIR EMBODIMENT 78935FC (WO:500470961)
N/A
WO: 500470961
TAC: 92932
1130
1
WO: 500729690
LH Side Fuselage FR69-70; STGR 19-20 Scratch &
Dent
LH Side Of Fuselage At 23 FR Floor Line
N/A
1130
2
1130
4
1130
6
1130
7
1130
8
Upper Fuselage Above R-2 Door Cut-out, AFT Corner
have Deep Rub Marks
Upper Fuselage Above L-2 Door Cut-out, AFT Corner
have Deep Rub Marks
Upper Fuselage Above R-2 Door Cut-out, Fwd Corner
have Deep Rub Marks
Upper Fuselage Above L-2 Door Cut-out, Fwd Corner
have Deep Rub Marks
Scratch In Fuselage Skin Lower Half FR 1 - 2; Y-130
1130
16
Impact Fuselage skin FWD LH Fuselage Door
IIR 53-11-11-1-001-00 First Inspection From time of
dent occurrence: 60000FC (WO:500674852)
IIR 53-41-11-1-003-00 FIRST INSPECTION FROM
AIRCRAFT DELIVERY 60000FC (WO:500030185)
IIR 53-41-11-1-002-00 FIRST INSPECTION FROM
AIRCRAFT DELIVERY 60000FC (WO:500030160)
IIR 53-41-11-1-003-00 FIRST INSPECTION FROM
AIRCRAFT DELIVERY 60000FC (WO:500030186)
IIR 53-41-11-1-002-00 FIRST INSPECTION FROM
AIRCRAFT DELIVERY 60000FC (WO:500030183)
IIR 53-11-11-1-002-00 From time of rework
accomplishment 60000FC (WO:500030187)
RDAS requirement: First Inspection from Time of Repair
Embodiment 60000FC (WO:500060139)
WO: 500674852
TAC: 67660
WO: 500030185
TAC: 60000
WO: 500030160
TAC: 60000
WO: 500030186
TAC: 60000
WO: 500030183
TAC: 60000
WO: 500030187
TAC: 71502
WO: 500060139
TAC: 63215
N/A
N/A
N/A
N/A
N/A
N/A
N/A
WO: 500454255
TAC: 74598
WO: 500465021
TAC: 75730
Sub 2 - Page 1 of 16
SDM A319/A320 MAINTENANCE PROGRAM
INDIVIDUAL STRUCTURAL INSPECTIONS
MSN
ITEM
REASON
FURTHER ACTION
MP REF: SDM.A320.BDCA
SECTION: V
REV: 03 DATE:06-OCT-2014
PERIODIC INSPECTION
1130
17
Fuselage skin AFT Rear Cargo Door Gouge
IIR 53-41-11-1-006-00 First Inspection from AC Delivery N/A
60000FC/75000FH (WO:500460883)
1130
19
LH Elevator Top Skin Dent with Delamination
IIR 55-21-11-2-002-00 First Inspection after Component N/A
Delivery 48000FC/60000FH (WO:500462994)
1130
20
R/H Fuselage Static Port Area Puncture
1130
28
Scratch on Fuselage Skin FR 8-9 150mm above the
STGR37RH
RAS Requirements: First Instpection from Time of
N/A
Repair Embodiment 60000FC (WO:500022794)
IIR 53-11-11-1-002-00 – 60000FC FIRST INSPECTION N/A
AFTER REPAIR EMBODIMENT (WO:500471463)
1130
36
Fuselage skin FR 9-10 STGR 20-21 LH Dent
1130
37
Fuselage skin FR10-11 STGR 30-31 LH Dent
1130
38
Doubler FR16-17 Above STGR29 Fuselage Skin RH
1130
41
1130
44
1130
45
1130
IIR 53-11-11-1-001-00 FIRST INSPECTION FROM
TIME OF DENT OCCURRENCE 60000FC
(WO:500471469)
IIR 53-11-11-1-001-00 FIRST INSPECTION FROM
TIME OF DENT OCCURRENCE 60000FC
(WO:500471470)
RDAS REQUIREMENTS FIRST INSPECTION AFTER
REPAIR EMBODIMENT 67000FC (WO:500062779)
LIMIT
WO: 500460883
TAH: 75000
TAC: 60000
WO: 500462994
TAH: 60000
TAC: 48000
WO: 500022794
TAC: 71090
WO: 500471463
TAC: 70295
N/A
WO: 500471469
TAC: 70399
N/A
WO: 500471470
TAC: 71024
N/A
WO: 500062779
TAC: 73954
FUSELAGE SKIN FWD SIDE SHELL 2 DENTS FR. 13- IIR 53-11-11-1-001-00 FIRST INSPECTION FROM
14 RH ABOVE FLOR LINE
TIME OF DENT OCCURRENCE 60000FC
(WO:500062912)
SKIN DENT BETWEEN STGR22-23 LH, FR21-22
IIR 53-11-11-1-001-00 First Inspection after Repair
Embodiment 60000FC (WO:500454255)
SKIN DENT BETWEEN STGR24-25 LH, FR23-24
IIR 53-11-11-1-001-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 60000FC (WO:500454256)
N/A
WO: 500062912
TAC: 68958
N/A
WO: 500454255
TAC: 74598
WO: 500454256
TAC: 74598
46
SKIN DENT BETWEEN STGR24-25 LH, FR22-23
IIR 53-11-11-1-001-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 60000 FC (WO:500454259)
N/A
WO: 500454259
TAC: 74598
1130
47
SKIN DENT BETWEEN STGR24-25 LH, FR20-21
IIR 53-11-11-1-001-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 60000 FC (WO:500454261)
N/A
WO: 500454261
TAC: 74598
1130
48
LH FWD Door Skin Scratch
IIR 52-10-00-1-002-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 60000FC (WO:500016692)
N/A
WO: 500016692
TAC: 77073
N/A
Sub 2 - Page 2 of 16
SDM A319/A320 MAINTENANCE PROGRAM
INDIVIDUAL STRUCTURAL INSPECTIONS
MSN
ITEM
REASON
FURTHER ACTION
MP REF: SDM.A320.BDCA
SECTION: V
REV: 03 DATE:06-OCT-2014
PERIODIC INSPECTION
LIMIT
1130
55
LH FWD Door Skin Dent
IIR 52-10-00-1-001-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 60000FC (WO:500016689)
N/A
WO: 500016689
TAC: 76801
1130
57
DENT IN FR 11-12 STGR 23-24 L/H FUSELAGE
N/A
WO: 500465925
TAC: 67615
1130
81
WO: 500909016
BLENDED. FR 68-69, STGR 18-19 LH FUSELAGE
N/A
1130
82
WO: 500909016
SCRATCHES. FR 66-67, STGR 23-24 LH FUSELAGE
1130
83
IIR 53-11-11-1-001-00 FIRST INSPECTION FROM
TIME OF DENT OCCURRENCE 60000FC
(WO:500465925)
IIR 53-41-11-1-002-00 FIRST INSPECTION FROM
AIRCRAFT DELIVERY 60000FC/120000FH
(WO:500465831)
IIR 53-41-11-1-002-00 FIRST INSPECTION FROM
AIRCRAFT DELIVERY 60000FC/120000FH
(WO:500465851)
IIR 52-33-00-1-001-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 140000FC (WO:500465956)
N/A
1488
1
1488
15
WO: 500909016
GOUGE. HANDLE BULK CARGO DOOR. RH
FUSELAGE
WO: 500479406
IIR 53-11-11-1-003-00 FIRST INSPECTION AFTER
WEAR ON DOOR 1R SURROUNDING PANEL UPPER REPAIR EMBODIMENT 60000FC (WO:500465959)
AFT CORNER
Doubler at fuselage skin FR. 11-12 STGR.22-23 LH
IIR 53-11-11-2-003-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 60000FC (WO:500468959)
WO: 500465831
TAH: 120000
TAC: 60000
WO: 500465851
TAH: 120000
TAC: 60000
WO: 500465956
TAC: 149052
1488
16
Lower AFT Edge Door 2RH Skin
1488
17
Blended Area Capt & F/O Statics Ports RH Side
1488
18
RH Side FR 13-14 Below Floor Level
1488
23
1488
42
1488
54
N/A
N/A
WO: 500465959
TAC: 67615
N/A
WO: 500468959
TAC: 69861
IIR 52-10-00-1-001-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 60000FC (WO:500468998)
N/A
WO: 500468998
TAC: 69861
RDAS REQUIREMENTS: FIRST INSPECTION AFTER
REPAIR EMBODIMENT 100000FC (WO:500469076)
N/A
WO: 500469076
TAC: 109861
N/A
WO: 500469541
TAC: 70143
N/A
WO: 500464995
TAC: 67529
WO: 500465008
TAH: 62634
TAC: 42151
WO: 500465023
TAH: 130064
TAC: 70798
IIR 53-11-11-1-001-00 FIRST INSPECTION FROM
TIME OF DENT OCCURRENCE 60000FC
(WO:500469541)
WO: 500723252
IIR 52-10-00-2-010-00 First Inspection After Repair
L1 Door FWD Bottom Corner Repair
Embodiment 60000FC (WO:500464995)
WO: 500098920
RDAS REQUIREMENTS: LIFE LIMITATION
Corrosion on integrated floor structure FR 59 RH
32900FC/41100FH from Time of Repair Embodiment
(WO:500465008)
WO: 500110669
IIR 53-41-11-1-007-00 First Inspection after Repair
DENT ON BLUE COLOR LINE BETWEEN FR63-FR64 Embodiment 60000FC/105000FH (WO:500465023)
LH (LAST PASSENGER WINDOW)
N/A
N/A
Sub 2 - Page 3 of 16
SDM A319/A320 MAINTENANCE PROGRAM
INDIVIDUAL STRUCTURAL INSPECTIONS
MSN
ITEM
1488
81
1488
89
1560
REASON
FURTHER ACTION
MP REF: SDM.A320.BDCA
SECTION: V
REV: 03 DATE:06-OCT-2014
PERIODIC INSPECTION
LIMIT
WO: 500723202
DENT ON BLUE COLOR LINE BETWEEN FR63-FR64
LH (LAST PASSENGER WINDOW)
WO: 500795727
L/H ENTRY DOOR LOWER EDGE PANEL DAMAGE
IIR 53-41-11-1-007-00 First Inspection after Repair
Embodiment 60000FC/105000FH (WO:500465023)
N/A
IIR 52-10-00-2-010-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 60000FC (WO:500059122)
N/A
4
Stone Hit Behaind Fr 23 RH 155mm from CL
IIR 53-11-11-1-002-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 60000FC (WO:500059117)
N/A
WO: 500059117
TAC: 72447
1560
12
20
RDAS Requirements: First Inspection from Time of
Repair Embodiment 60000FC/120000FH
(WO:500463625)
IIR 52-10-00-1-001-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 60000FC (WO:500465248)
N/A
1560
WO: 500463625
TAH: 151747
TAC: 73505
WO: 500465248
TAC: 75629
1560
27
RDAS REQUIREMENTS (JIC:11877 controlled)
11877
1560
32
RDAS REQUIREMENTS (JIC:11878 controlled)
11878
1560
63
WO: 500044596
THREE SCUFFING OF LOWER GIRDER PART OF
TOP SKIN R/H #3 SLAT
WO: 500055175
DENT ON FWD R/H PASSENGER/CREW DOOR
PANEL EDGE
WO: 500097084
Corrosion, Top Skin Panel 2, T/E Overhang, Multi-Site,
WO: 500357784
Corrosion, Top Skin Panel 2, Lower Surface, T/E
Corrosion, Top Skin Panel 2, Lower Surface, T/E
Overhang, Multi-Site, LH
1560
67
1578
4
1578
5
1578
RDAS REQUIREMENTS: FIRST INSPECTION AFTER
REPAIR EMBODIMENT 72900FC/101900FH
(WO:500469844)
DENT FUSELAGE FR9-10 RH LOWER PART OF THE IIR 53-11-11-2-003-00 FIRST INSPECTION AFTER
SKIN PANEL
REPAIR EMBODIMENT 60000FC (WO:500470984)
N/A
N/A
N/A
TWO DENTS ON THE LH SIDE OF FUSELAGE,
STR23L FR23
WO: 500062903
Trapped Water Indication LH Elevator Upper Skin
IIR 53-11-11-1-001-00 First Inspection from Time of
N/A
Dent Occurrence 60000FC (WO:500455233)
IIR 55-21-11-2-002-00 First Inspection After Component N/A
Delivery 48000FC/60000FH (WO:500460229)
16
LH AFT passenger door skin panel scratch (Blue line)
N/A
1578
18
Passenger compt. window frame lower part and
adjacent skin panel FR 63-64 LH
IIR 52-10-00-1-002-00 First Inspection After Repair
Embodiment 60000FC (WO:500455242)
IIR 53-00-29-1-001-00 JIC:11794 Controlled
1578
20
Blended Area On FR67 STGR23-25 LH Fuselage
IIR 53-41-11-1-002-00 FIRST INSPECTION FROM
AIRCRAFT DELIVERY 60000FC/120000FH
(WO:500465855)
N/A
11794
WO: 500465023
TAH: 130064
TAC: 70798
WO: 500059122
TAC: 72181
WO: 500469638
DATE: 2932167
WO: 500469835
DATE: 2932167
WO: 500469844
TAH: 134055
TAC: 85887
WO: 500470984
TAC: 76494
WO: 500455233
TAC: 68074
WO: 500460229
TAH: 60000
TAC: 48000
WO: 500455242
TAC: 72300
WO: 500081897
DATE: 2932167
WO: 500465855
TAH: 120000
TAC: 60000
Sub 2 - Page 4 of 16
SDM A319/A320 MAINTENANCE PROGRAM
INDIVIDUAL STRUCTURAL INSPECTIONS
MSN
ITEM
1578
25
1578
36
1578
REASON
FURTHER ACTION
MP REF: SDM.A320.BDCA
SECTION: V
REV: 03 DATE:06-OCT-2014
PERIODIC INSPECTION
LIMIT
WO: 500062903
Reworked Sckratch On FR68-69 STGR18-20 LH
Fuselage
WO: 500042128
Reworked Sckratch On Door #2 (Rear) LH Outer Skin
IIR 53-41-11-1-002-00 FIRST INSPECTION FROM
AIRCRAFT DELIVERY 60000FC/120000FH
(WO:500465864)
IIR 52-10-00-1-002-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 60000FC (WO:500465985)
N/A
37
WO: 500057280
Blended Area On FR65-66 STGR24-25 LH Fuselage
N/A
1578
46
Blended Area On FR67-68 STGR 25-26 LH Fuselage
1578
47
Blended Area On FR68 STGR 26-28 LH Fuselage
1578
48
Blended Area On FR68-69 STGR 24-25 LH Fuselage
1578
49
Blended Area On FR68 STGR 21-22 LH Fuselage
1578
50
Reworked Sckratch On FR16-17 STGR34-35 RH
Fuselage
IIR 53-41-11-1-002-00 FIRST INSPECTION FROM
AIRCRAFT DELIVERY 60000FC/120000FH
(WO:500465867)
IIR 53-41-11-1-002-00 FIRST INSPECTION FROM
AIRCRAFT DELIVERY 60000FC/120000FH
(WO:500465870)
IIR 53-41-11-1-002-00 FIRST INSPECTION FROM
AIRCRAFT DELIVERY 60000FC/120000FH
(WO:500465876)
IIR 53-41-11-1-002-00 FIRST INSPECTION FROM
AIRCRAFT DELIVERY 60000FC/120000FH
(WO:500465886)
IIR 53-41-11-1-002-00 FIRST INSPECTION FROM
AIRCRAFT DELIVERY 60000FC/120000FH
(WO:500465900)
IIR 53-11-11-1-002-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 60000FC (WO:500465990)
1578
63
L/H FWD Fuselage FR3-4 Under center line
N/A
WO: 500466065
TAC: 71354
1578
64
FR10 200mm ABOVE FLIGHT CMPT AFT FIXED
WINDOW CUT OUT L/H FUSELAGE
N/A
WO: 500467230
TAC: 103637
1657
1
FR 21, STR 19 L/H Fuselage Dent
IIR 53-11-11-1-001-00 FIRST INSPECTION FROM
TIME OF DENT OCCURRENCE 60000FC
(WO:500466065)
RDAS Ref: 70561317/003/2012 ISSUE: A – 90000 FC
FIRST INSPECTION AFTER REPAIR EMBODIMENT
WO:500467230
IIR 53-11-11-2-003-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 60000FC (WO:500719703)
N/A
WO: 500719703
TAC: 73637
1657
2
LH AFT Passenger Door Skin Panel Dents 2ea
IIR 52-10-00-1-001-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 60000FC (WO:500465787)
N/A
WO: 500465787
TAC: 72025
1657
4
LH AFT Passenger Door Skin Panel Dent
IIR 52-10-00-2-012-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 60000FC (WO:500466343)
N/A
WO: 500466343
TAC: 72025
N/A
N/A
N/A
N/A
N/A
N/A
WO: 500465864
TAH: 120000
TAC: 60000
WO: 500465985
TAC: 67615
WO: 500465867
TAH: 120000
TAC: 60000
WO: 500465870
TAH: 120000
TAC: 60000
WO: 500465876
TAH: 120000
TAC: 60000
WO: 500465886
TAH: 120000
TAC: 60000
WO: 500465900
TAH: 120000
TAC: 60000
WO: 500465990
TAC: 70330
Sub 2 - Page 5 of 16
SDM A319/A320 MAINTENANCE PROGRAM
INDIVIDUAL STRUCTURAL INSPECTIONS
MSN
ITEM
REASON
FURTHER ACTION
MP REF: SDM.A320.BDCA
SECTION: V
REV: 03 DATE:06-OCT-2014
PERIODIC INSPECTION
LIMIT
1657
5
R/H Wing Top Skin Panel 2 overhang RIB 14
RDAS REQUIREMENTS (JIC:11869 controlled)
11869
1657
6
L/H Wing Top Skin Panel 2 overhang RIB 14
RDAS REQUIREMENTS (JIC:11865 controlled)
11865
1657
7
AFT Cargo Compartment Door Scratches around CL
IIR 52-30-00-1-002-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 60000FC (WO:500057836)
N/A
1657
8
Rudder shell LH near rudder tip-Vacuum loss indication RDAS REQUIREMENTS (JIC:3146 controlled)
at 2 inspection holes
3146
WO: 500704733
DATE: 2932167
1657
9
FWD Avionic Compartment Door Around Handle
Chafting Mark
11860
WO: 500466670
DATE: 2932167
1657
11
11862
WO: 500466722
DATE: 2932167
1657
20
WO: 500748409
RH Rear Avionic Compartment Door Around Handle
Chafting Mark
LH Lateral Avionic Compartment Door Around Handle
Chafting Mark
11861
WO: 500466704
DATE: 2932167
1657
31
LH Fuselage Skin 20-21Fr, 20 Str Scratch
N/A
1657
50
L/H Fuselage Between Frames 60 & 61 STGR 26L &
27L
IIR 52-41-00-1-001-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 40000FC (JIC:11860
controlled)
IIR 52-41-00-1-001-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 40000FC (JIC:11862
controlled)
IIR 52-41-00-1-001-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 40000FC (JIC:11861
controlled)
IIR 53-11-11-1-002-00 First Inspection After Repair
Embodiment 60000FC (WO:500455229)
IIR 53-41-11-1-007-00 First Inspection After Repair
Embodiment 60000FC/105000FH (WO:500465191)
1657
51
L/H Fuselage FR 65 STGR 24L FWD Of L2 Door
N/A
1657
52
R/H Fuselage FWD Of R1 Door Dent
1657
64
SCRATCHES AREA BELOW FWD LOWER CORNER
OF FWD ENTRY DOOR.
IIR 53-41-11-1-002-00 First Inspection from A/C
Delivery 60000FC (WO:500465203)
IIR 53-11-11-1-001-00 First Inspection From Time of
Dent Occurrence 60000FC(WO:500465306)
IIR 53-11-11-1-002-00. First Inspection from Time of
Rework Accomplishment 60000FC (WO:500465597)
WO: 500455229
TAC: 72001
WO: 500465191
TAH: 118339
TAC: 65668
WO: 500465203
TAC: 60000
WO: 500465306
TAC: 65652
WO: 500465597
TAC: 71400
1657
67
RH FWD Passenger Door Frame FWD Upper Corner is IIR 53-11-11-1-003-00 First Inspection after Repair
chafled
Embodiment 60000FC (WO:500465629)
N/A
WO: 500465629
TAC: 72533
1657
68
DENT L/H FUSELAGE FR 24 STRG 24
N/A
WO: 500471014
TAC: 60494
1657
69
R/H wing-top skin panel 2 upper surfaceof the rear spar RDAS REQUIREMENTS (JIC:11864 controlled)
RIB 10; 11; 12
11864
WO: 500467639
DATE: 2932167
RDAS REQUIREMENTS FIRST INSPECTION AFTER
REPAIR EMBODIMENT 44000FC (WO:500471014)
N/A
N/A
N/A
WO: 500468726
DATE: 2932167
WO: 500467692
DATE: 2932167
WO: 500057836
TAC: 72679
Sub 2 - Page 6 of 16
SDM A319/A320 MAINTENANCE PROGRAM
INDIVIDUAL STRUCTURAL INSPECTIONS
MSN
ITEM
REASON
FURTHER ACTION
MP REF: SDM.A320.BDCA
SECTION: V
REV: 03 DATE:06-OCT-2014
PERIODIC INSPECTION
R/H wing-top skin panel 2 upper surfaceof the rear spar RDAS Ref:RAS/BAE/1014661/2010 issue C – 60000FC
RIB 19; 20
or 107700FH FIRST INSPECTION AFTER REPAIR
EMBODIMENT WO:500467610
WO: 500014685
RDAS Ref:70568458/004/2012 issue A – 62100FC or
CORROSION TOP SKIN LOWER SURFACE T/E
111400FH FIRST INSPECTION AFTER REPAIR
OVERHANG RIB 16 R/H WING
EMBODIMENT WO^500467741
WO: 500014685
RDAS REQUIREMENTS (JIC:11866 controlled)
R/H WING REAR SPAR TOP FLANGE BETWEEN RIB
15-17 AT THE ATTACHMENT TO THE REPAIR PLATE
WO: 500036479
Contact Airbus required before reaching Repair Life
EXTERNAL DOUBLER WITH TWO DENTS ON ITS
Limit. Expected Apr.2021 (WO:500457760).
DENT. Iberworld x-ref 2.
IIR 53-11-11-1-001-00, FIRST INSPECTION FROM
TIME OF DENT OCCURRENCE 60000FC
(WO:500460663)
Dents on LH Fuselage skin at FR 21-24 (3EA)
IIR 53-11-11-1-001-00 First Inspection From Time of
Dent Occurrence 60000FC (WO:500455241)
Crack on Lower Skin of RH THS External Structure at
RDAS Requirements: First Inspection from Component
Rib 11
First Flight 48000FC/60000FH (WO:500453296)
N/A
EXTERNAL PATCH, DENT REPAIR. Iberworld x-ref 21. IIR 53-11-11-2-003-00 FIRST INSPECTION DUE TAC:
58,287 (tracked with WO 500404918).
BLENDING. Iberworld x-ref 22.
IIR 53-41-11-1-002-00 FIRST INSPECTION DUE AT
60,000 TAC / 120,000 TAH (WO:500460789)
N/A
90
BLENDING ON FUSELAGE SKIN. Iberworld x-ref 27.
IIR 53-41-11-1-002-00 FIRST INSPECTION AT 60`000
CSN / 120,000 TAH (WO:500460797)
N/A
1657
91
EXTERNAL PATCH, DOOR 2R. Iberworld x-ref 26.
N/A
1657
92
DENT. Iberworld x-ref 1.
1657
93
BULK CARGO DOOR DOUBLER. Iberworld x-ref 7.
1657
94
DRESS OUT OF TWO DENTS WITH REWORK OF
SCRATCHES. Iberworld x-ref 10.
IIR 52-10-00-2-010-00 INSPECT FIRST INSPECTION
AFTER REPAIR EMBODIMENT 60000FC
(WO:500457971)
IIR 53-11-11-1-001-00, FIRST INSPECTION FROM
TIME OF DENT OCCURRENCE 60000FC
(WO:500460654)
IIR 52-33-00-2-002-00, First inspection after repair
embodiment 60000FC (WO:500457957)
The repair is acceptable up to 1.25 DSG (60,000 FC)
with inspection threshold 37,000 FC from repair
embodiment. Due at: 40,772 FC (tracked with WO
500`403`952)
1657
70
1657
79
1657
80
1657
84
1657
85
1657
86
1657
87
1657
88
1657
89
1657
N/A
11866
N/A
N/A
N/A
N/A
N/A
LIMIT
WO: 500467610
TAH: 135231
TAC: 72025
WO: 500467741
TAH: 146154
TAC: 76382
WO: 500467754
DATE: 2932167
WO: 500457760
TAC: 27341
WO: 500460663
TAC: 62798
WO: 500455241
TAC: 75814
WO: 500453296
TAH: 60000
TAC: 48000
WO: 500404918
TAC: 58287
WO: 500460789
TAH: 120000
TAC: 60000
WO: 500460797
TAH: 120000
TAC: 60000
WO: 500457971
TAC: 71335
N/A
WO: 500460654
TAC: 62798
N/A
WO: 500457957
TAC: 65018
WO: 500403952
TAC: 40722
N/A
Sub 2 - Page 7 of 16
SDM A319/A320 MAINTENANCE PROGRAM
INDIVIDUAL STRUCTURAL INSPECTIONS
MSN
ITEM
REASON
1657
95
SMOOTH DENT. Iberworld x-ref 9.
1657
96
Liquid ingress on the RH elevator upper and lower
honeycomb filler.
1657
97
CORROSION ON STGR 41
1657
1657
1657
FURTHER ACTION
111 DENT. Iberworld x-ref 52.
1657
112 EXTERNAL REPAIR PLATE, SEVERAL REWORKED
AREAS, OVERSIZED BOLTS. Iberworld x-ref 53.
1743
1
1743
2
1743
11
1743
19
1743
25
1743
69
PERIODIC INSPECTION
IIR 53-11-11-1-001-00 FIRST INSPECTION FROM
N/A
TIME OF DENT OCCURRENCE 60,000FC
(WO:500460664)
IIR 55-21-11-2-002-00 First Inspection After Component N/A
Delivery 48000FC/60000FH (WO:500460245)
IIR 53-21-13-2-003-00 First Inspection After Repair
Embodiment 60000 FC (WO:500456478)
98 CORROSION, MLG SIDE STAY FITTINGS OUTB LUG Repair Life Limit (WO:500409255)
BORES, BOTH WINGS.
100 SCRATCH. Iberworld x-ref 40.
IIR 53-21-11-1-002-00 First Inspection from A/C first
flight 60000FC (WO:500460802)
110 DENT, DOOR 2L. Iberworld x-ref 51.
IIR 52-10-00-1-001-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 60000FC (WO:500461019)
1657
MP REF: SDM.A320.BDCA
SECTION: V
REV: 03 DATE:06-OCT-2014
N/A
N/A
N/A
N/A
IIR 53-11-11-1-001-00 FIRST INSPECTION AT 71`392 N/A
CSN, (WO:500460665)
Post Repair Inspection Programm for 6 locations.
8548
Repair Life Limit: 72`122 TAH / 36`592 TAC CONTACT
AIRBUS BEFORE THE LIFE LIMIT IS REACHED
(WO:500401846)
IIR 52-33-00-1-001-00 FIRST INSPECTION AFTER
N/A
REPAIR EMBODIMENT 140000FC (WO:500457969).
WO: 500014741
REWORK OF DOOR SKIN EDGE IN HANDLE
CUTOUT AREA. Iberworld x-ref 58.
WO: 500356801
RDAS REQUIREMENTS TH: 88900FC.
EXTERNAL DOUBLER, BUTTJOINT AREA. Iberworld x- (WO:500457821)
WO: 500356650
IIR 55-21-11-2-002-00 FIRST INSPECTION DUE AT
COMPOSITE REPAIR AT THE TRAILING EDGE,
48,000 FC / 60,000 FH after component delivery
THERMOGRAPHY DETECTION OF TRAPPED
(WO:500460868)
WO: 500015000
IIR 53-11-11-1-001-00 FIRST INSPECTION FROM
DENT. Iberworld x-ref 66.
TIME OF DENT OCCURRENCE 60000FC
(WO:500460668)
WO: 500047022
IIR 53-11-11-1-001-00 FIRST INSPECTION FROM
DENT. Iberworld x-ref 67.
TIME OF DENT OCCURRENCE 60000FC
(WO:500460669)
DENT. Iberworld x-ref 68.
IIR 53-21-11-1-001-00 FIRST INSPECTION FROM
TIME OF DENT OCCURRENCE 60000FC
(WO:500461020)
N/A
N/A
N/A
LIMIT
WO: 500460664
TAC: 62798
WO: 500460245
TAH: 60000
TAC: 48000
WO: 500456478
TAC: 76047
WO: 500409255
TAC: 21469
WO: 500460802
TAC: 60000
WO: 500461019
TAC: 71392
WO: 500460665
TAC: 71392
WO: 500401846
TAH: 72122
TAC: 36592
WO: 500457969
TAC: 151392
WO: 500457821
TAC: 100524
WO: 500460868
TAH: 60000
TAC: 48000
WO: 500460668
TAC: 71969
N/A
WO: 500460669
TAC: 71969
N/A
WO: 500461020
TAC: 71969
Sub 2 - Page 8 of 16
SDM A319/A320 MAINTENANCE PROGRAM
INDIVIDUAL STRUCTURAL INSPECTIONS
MSN
ITEM
REASON
1743
70
DOOR 2R - SKIN BLEND OUT. Iberworld x-ref 98.
1743
73
R/H Wing Top Skin Panel 2 overhang RIB 14
1743
77
R/H Wing Top Skin Panel 2 overhang RIB 14
1743
78
PERMANENT REPAIR. DOUBLER FR 69-70 LH
1761
8
SCRATCH REWORKED FUSELAGE FRAME 65-66
STGR 24-25LH
1761
13
BLEND OUT FR 69-70 & STGR 42-43 LH
1761
22
BLENDED AREA FR 12 & STGR 25-26 RH
1761
24
1761
FURTHER ACTION
MP REF: SDM.A320.BDCA
SECTION: V
REV: 03 DATE:06-OCT-2014
PERIODIC INSPECTION
LIMIT
IIR 52-10-00-1-002-00 FIRST INSPECTION
(WO:500457981)
RDAS Ref: RAS/BAE/1014745/2010 ISSUE D –
118300FC or 212300FH FIRST INSPECTION FROM
FIRST FLIGHT WO:500468700
RDAS Ref: RAS/BAE/1014745/2010 ISSUE D –
38025FC or 74131FH FIRST INSPECTION AFTER
REPAIR EMBODIMENT WO:500468713
IIR 53-00-11-2-003-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 60000FC (WO:500463781)
N/A
IIR 53-41-11-1-002-00 FIRST INSPECTION FROM
AIRCRAFT DELIVERY 60000FC/120000FH
(WO:500460280)
IIR 53-41-11-1-005-00 FIRST INSPECTION FROM
AIRCRAFT DELIVERY 60000FC/120000FH
(WO:500460178)
IIR 53-11-11-1-002-00 First Inspection From Time of
Rework Accomplishment 60000FC (WO: 500459724)
N/A
WO: 500081897
BLENDED AREA FR 10-11 & STGR 26-27 RH
IIR 53-11-11-1-002-00 First Inspection From Time of
Rework Accomplishment 60000FC (WO:500459782)
N/A
WO: 500459782
TAC: 67945
26
WO: 500022819
SCRATCHED AREA FR 17; STGR 27-28 RH
IIR 53-11-11-1-002-00 First Inspection From Time of
Rework Accomplishment 60000FC (WO:500459843)
N/A
WO: 500459843
TAC: 67945
1761
55
BLENDED AREA FR 10-11 & STGR 24-25 RH
IIR 53-11-11-1-002-00 First Inspection From Time of
Rework Accomplishment 60000FC (WO:500459781)
N/A
WO: 500459781
TAC: 67945
1761
56
WO: 500426401
BLENDED AREA FR 15-16 & STGR 23-24 RH
IIR 53-11-11-1-002-00 First Inspection From Time of
Rework Accomplishment 60000FC (WO:500459783)
N/A
WO: 500459783
TAC: 67945
1761
66
RDAS REQUIREMENTS (JIC:11880 controlled)
11880
1761
67
WO: 500442881
Corrosion, Top Skin Panel 2, Lower Surface, RH, Rib
WO: 500444286
Corrosion, Top Skin Panel 2, T/E Overhang, Multi-Site,
LH
RDAS LIFE LIMIT FROM TIME OF REPAIR
EMBODIMENT 22600FC/40500FH (WO:500486064)
N/A
WO: 500469855
DATE: 2932167
WO: 500486064
TAH: 72655
TAC: 35587
N/A
N/A
N/A
N/A
N/A
WO: 500457981
TAC: 71969
WO: 500468700
TAH: 212300
TAC: 118300
WO: 500468713
TAH: 74131
TAC: 38025
WO: 500463781
TAC: 67945
WO: 500460280
TAH: 120000
TAC: 60000
WO: 500460178
TAH: 120000
TAC: 60000
WO: 500459724
TAC: 67945
Sub 2 - Page 9 of 16
SDM A319/A320 MAINTENANCE PROGRAM
INDIVIDUAL STRUCTURAL INSPECTIONS
MSN
ITEM
REASON
1767
1
Water Ingress on the RH Elevator Upper & Lower
honeycomb Filler
1767
4
Water Ingress on the LH Elevator Upper & Lower
honeycomb Filler
1767
8
CORROSION AREAS ON RH WING TOP SKIN
(UPPER AND LOWER SURFACES)
1767
9
1767
12
1767
29
Corrosion on the upper surface of the upper skin of the
center wing box LH
WO: 500730779
SCRATCH ON HANDLE HOUSING BULK CARGO
DOOR
CORROSION AREAS ON RH WING TOP SKIN
(UPPER AND LOWER SURFACES)
1767
30
DENT ON FUSELAGE SKIN FR 21-23 LH
1767
31
DENT ON FUSELAGE SKIN FR 21-23 LH
1767
32
DENT ON FUSELAGE SKIN FR 21-23 LH
1767
33
FWD RH PAX/CREW DOOR SCRATCH
1767
34
1767
1767
FURTHER ACTION
MP REF: SDM.A320.BDCA
SECTION: V
REV: 03 DATE:06-OCT-2014
PERIODIC INSPECTION
LIMIT
IIR 55-21-11-2-002-00 FIRST INSPECTION AFTER
COMPONENT DELIVERY 48000FC/60000FH
(WO:500470771)
IIR 55-21-11-2-002-00 FIRST INSPECTION AFTER
COMPONENT DELIVERY 48000FC/60000FH
(WO:500470747)
RDAS RAS/BAE/104455/2007 Issue B
REQUIREMENTS: First Inspection After Repair
Embodiment 54300FC (WO:500462362)
RDAS Requirements: TH 6Y from time of repair
embodiment Interval: 6Y (JIC:13540)
IIR 52-33-00-1-001-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT - 40000FC (WO:500460357)
N/A
RDAS RAS/BAE/104455/2007 Issue B
REQUIREMENTS: First Inspection After Repair
Embodiment 74200FC (WO:500462329)
IIR 53-11-11-1-001-00 FIRST INSPECTION FROM
TIME OF DENT OCCURRENCE 60000FC
(WO:500459862)
IIR 53-11-11-1-001-00 FIRST INSPECTION FROM
TIME OF DENT OCCURRENCE 60000FC
(WO:500459868)
IIR 53-11-11-1-001-00 FIRST INSPECTION FROM
TIME OF DENT OCCURRENCE 60000FC
(WO:500459873)
IIR 52-10-00-1-002-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 60000FC (WO:500736309)
N/A
WO: 500462329
TAC: 80767
N/A
WO: 500459862
TAC: 69884
N/A
WO: 500459868
TAC: 69884
N/A
WO: 500459873
TAC: 69884
N/A
WO: 500736309
TAC: 82021
Corrosion on angle at bottom centerline BTW FR21 and IIR 53-00-13-2-001-00 FIRST INSPECTION AFTER
FR23
REPAIR EMBODIMENT - 60000FC (WO:500893826)
N/A
WO: 500893826
TAC: 77095
35
Undocumentated Repair BTW FR21 and FR23 Bottom
Part
IIR 53-00-11-2-017-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT - 60000FC (WO:500893831)
N/A
WO: 500893831
TAC: 77095
36
R2 Door Sill Beam Repair.
IRR 53-41-14-2-001-00, First inspection after repair
embodiment 92731 FC / 208644 FH, tracked with WO
500`752`500.
N/A
WO: 500752500
TAH: 249799
TAC: 110554
N/A
N/A
13540
N/A
WO: 500470771
TAH: 60000
TAC: 48000
WO: 500470747
TAH: 60000
TAC: 48000
WO: 500462362
TAC: 60867
WO: 500717715
DATE: 2932167
WO: 500460357
TAC: 46567
Sub 2 - Page 10 of 16
SDM A319/A320 MAINTENANCE PROGRAM
INDIVIDUAL STRUCTURAL INSPECTIONS
MSN
ITEM
REASON
1767
37
Dents on external surface of skin at FR 73 - 74 LH
1767
48
1767
63
1767
64
WO: 500568784
RH Elevator Upper Surface Water ingress areas
detected. 4 Areas
WO: 500033105
LH Elevator Upper and Lower Surfaces Water ingress
areas detected. 10 Areas
WO: 500033104
Water Ingress on Elevator RH Upper Skin 13 Areas
1767
65
1767
66
Center tank upper panel corrosion in the area of FR42
FURTHER ACTION
IIR 53-51-11-1-001-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT - 60000FC/75000FH
(WO:500893834)
IIR 55-21-11-2-002-00 FIRST INSPECTION AFTER
COMPONENT DELIVERY - 48000FC/60000FH
(WO:500893850)
IIR 55-21-11-2-002-00 FIRST INSPECTION AFTER
COMPONENT DELIVERY - 48000FC/60000FH
(WO:500893852)
RDAS Requirements: First Inspection at 37500 FC /
80000 FH from Component First Flight (WO:
500784925)
Periodical inspection 6Y interval (JIC:14029 Controlled)
MP REF: SDM.A320.BDCA
SECTION: V
REV: 03 DATE:06-OCT-2014
PERIODIC INSPECTION
N/A
N/A
N/A
N/A
14029
LIMIT
WO: 500893834
TAH: 115429
TAC: 77095
WO: 500893850
TAH: 60000
TAC: 48000
WO: 500893852
TAH: 60000
TAC: 48000
WO: 500784925
TAH: 74491
TAC: 33845
WO: 500784922
DATE: 17609
WO: 500801669
TAH: 185988
TAC: 91284
WO: 500460222
TAH: 120000
TAC: 60000
WO: 500460228
TAH: 120000
TAC: 60000
WO: 500460231
TAH: 120000
TAC: 60000
WO: 500460345
TAH: 120000
TAC: 60000
WO: 500460314
TAC: 70952
DENT ON FUSELAGE SKIN FR 69-70 STGR 22-23 LH IIR 53-41-11-1-007-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT - 81400FC/162800FH
(WO:500801669)
72 REWORKED (TWO AREAS) BETWEEN FR 66-67 AND IIR 53-41-11-1-002-00 FIRST INSPECTION FROM
STRG 23-24
AIRCRAFT FIRST FLIGHT 60000FC/120000FH
(WO:500460222)
73 REWORKED (TWO AREAS) BETWEEN FR 66-67 AND IIR 53-41-11-1-002-00 FIRST INSPECTION FROM
STRG 24-25
AIRCRAFT FIRST FLIGHT 60000FC/120000FH
(WO:500460228)
75 WO: 500057466
IIR 53-41-11-1-002-00 FIRST INSPECTION FROM
REWORKED (TWO AREAS) BETWEEN FR 67-68 AND AIRCRAFT FIRST FLIGHT 60000FC/120000FH
STRG 24-25
(WO:500460231)
81 WO: 500033247
IIR 53-41-11-1-002-00 FIRST INSPECTION FROM
REWORKED AREA BETWEEN 68-69 AND STRG. 22- AIRCRAFT FIRST FLIGHT 60000FC/120000FH
23 RH
(WO:500460345)
100 Dent on LH FWD Entry Door Rear lower corner
IIR 52-10-00-1-001-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT - 60000FC (WO:500460314)
N/A
1767
101 Dent on LH FWD Entry Door FWD lower corner
N/A
WO: 500460321
TAC: 70952
1767
102 DENT ON L/H FUSELAGE SKIN FR.62-63 STRG.25-26 IIR 53-41-11-1-007-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT – 60000FC/105000FH
(WO:500460823)
N/A
WO: 500460823
TAH: 133840
TAC: 71581
1767
1767
1767
1767
1767
IIR 52-10-00-1-001-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT - 60000FC (WO:500460321)
N/A
N/A
N/A
N/A
N/A
Sub 2 - Page 11 of 16
SDM A319/A320 MAINTENANCE PROGRAM
INDIVIDUAL STRUCTURAL INSPECTIONS
MSN
1767
ITEM
REASON
FURTHER ACTION
PERIODIC INSPECTION
LIMIT
RDAS REQUIREMENTS. FIRST INSPECTION AFTER
REPAIR EMBODIMENT - 60000FC/107700FH
(WO:500461244)
111 Corrosion on RH wing top skin TE overhang RIB 15-19 RDAS REQUIREMENTS. TH: 20000FC/35800FH,
INTERVAL: 9000FC/12000FH (JIC:11839 controlled)
N/A
1767
113 Corrosion on RH wing top skin under the repair plate
top skin RIB 15-17
RDAS REQUIREMENTS. TH: 49100FC/68600FH,
INTERVAL: 13800FC/24800FH (JIC:11833 controlled)
11833
WO: 500463331
DATE: 2932167
1767
114 Corrosion on RH wing rear spar top flange RIB 15-17
RDAS REQUIREMENTS. TH: 28900FC/47400FH,
INTERVAL: 15000FC/24400FH (JIC:11834 controlled)
11834
WO: 500463448
DATE: 2932167
1767
115 Corrosion on RH wing top skin TE overhang and rear
spar attachments RIB 14-15
RDAS REQUIREMENTS. LL 12200FC/42300FH
(WO:500461251)
N/A
1767
116 Corrosion on RH wing top skin under the repair plate
RIB 13-14
RDAS REQUIREMENTS. LL: 26000FC/37100FH
(WO:500461255)
N/A
1767
120 Corrosion on RH wing rear spar top flange RIB 13-14
RDAS REQUIREMENTS. TH: 23200FC/38100FH
INTERVAL: 15000FC/25200FH (JIC:11835 controlled)
11835
WO: 500461251
TAH: 71409
TAC: 23879
WO: 500461255
TAH: 66209
TAC: 37679
WO: 500463551
DATE: 2932167
1767
110 Corrosion on RH wing top skin trailing edge overhang,
RIB 19-20
MP REF: SDM.A320.BDCA
SECTION: V
REV: 03 DATE:06-OCT-2014
11839
WO: 500461244
TAH: 136809
TAC: 71679
WO: 500463746
DATE: 2932167
1851
6
Corrosion on RH wing top skin TE overhang and false
rear spar attachments RIB 7-9; RIB 11-12
RDAS REQUIREMENTS. TH: 9000FC/12000FH,
INTERVAL: 9000FC/12000FH (JIC:11837 controlled)
11837
WO: 500463703
DATE: 2932167
1851
10
Corrosion on RH wing top skin under the repair plate
RIB 9-11
RDAS REQUIREMENTS. LL: 16300FC/29300FH
(WO:500461386)
N/A
1851
19
WO: 500053374
Corrosion on RH wing rear spar top flange RIB 9-11
RDAS REQUIREMENTS. TH: 38300FC/62800FH,
INTERVAL: 9100FC/14900FH (JIC:11836 controlled)
11836
WO: 500461386
TAH: 58409
TAC: 27979
WO: 500463555
DATE: 2932167
1851
20
RDAS REQUIREMENTS. TH: 20000FC/35000FH
INTERVAL: 9000FC/12000FH (JIC:11831 controlled)
11831
WO: 500462375
DATE: 2932167
1863
8
21
RDAS REQUIREMENTS. FIRST INSPECTION AFTER
REPAIR EMBODIMENT - 122700FC/192300FH
(WO:500461435)
RDAS REQUIREMENTS. LL: 26000FC/46600FH
(WO:500461453)
N/A
1863
WO: 500053374
Corrosion on LH wing top skin false rear spar trailing
edge RIB 7-9 & RIB 13-18
WO: 500009136
Corrosion on LH wing, False rear spar, top flange RIB 7
to RIB 9
WO: 500053172
Corrosion on LH wing top skin under the repair plate
RIB 13-16
WO: 500461435
TAH: 221409
TAC: 134379
WO: 500461453
TAH: 75709
TAC: 37679
N/A
Sub 2 - Page 12 of 16
SDM A319/A320 MAINTENANCE PROGRAM
INDIVIDUAL STRUCTURAL INSPECTIONS
MSN
ITEM
REASON
1863
22
1863
68
1863
84
1876
8
1876
12
UPR side Inserts #29 and #18 missed + 2 Composite
Repairs on Upper Skin.
1876
15
Internal corrosion FR30-34 STGR40-43R
1876
21
1876
29
1876
52
1876
53
1876
54
1876
57
WO: 500019020
Corrosion on LH Wing Top Skin lower Surface
Overhang Panel near RIB 22
WO: 500094865
1R DOOR SKIN DENT AND BLENDOUT.
BULK CARGO DOOR SKIN HANDLE CUTOUT
REWORK.
RIGHT AVIONIC DOOR 822, REWORK ON SKIN
HANDLE CUTOUT.
LEFT AVIONIC DOOR 812, REWORK ON SKIN
HANDLE CUTOUT.
FUSELAGE SKIN DENT WITH REWORK.
1876
70
FUSELAGE SKIN EXTERNAL DOUBLER.
1876
71
FUSELAGE SKIN DENT DRESS-OUT.
1876
75
FUSELAGE SKIN DENT.
1876
76
FUSELAGE SKIN EXTERNAL DOUBLER.
FURTHER ACTION
MP REF: SDM.A320.BDCA
SECTION: V
REV: 03 DATE:06-OCT-2014
PERIODIC INSPECTION
LIMIT
WO: 500053169
Corrosion on LH wing rear spar top flange at the
oversized fasteners RIB 13-16
WO: 500884930
LH FWD ENTRY DOOR SCRATCHES (2EA)
RDAS REQUIREMENTS. TH: 29400FC/48200FH,
INTERVAL: 15000FC/24400FH (JIC:11832 controlled)
11832
WO: 500462877
DATE: 2932167
IIR 52-10-00-1-002-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT – 60000FC (WO:500460799)
N/A
WO: 500460799
TAC: 73509
WO: 500873377
Corrosion on LH Wing Top Skin lower Surface
Overhang Panel near RIB 7A
Corrosion on LH Wing Top Skin lower Surface
Overhang Panel near RIB 18, 19.
IIR 57-21-11-1-005-00 FIRST INSPECTION AFTER
AIRCRAFT FIRST FLIGHT - 60000FC/107700FH
(WO:500801691)
IIR 57-21-11-1-006-00 FIRST INSPECTION AFTER
AIRCRAFT FIRST FLIGHT - 60000FC/107700FH
(WO:500894344)
IIR 55-21-11-2-002-00 at 60000 FH / 48000 FC from
component delivery, controlled by WO 500898763.
N/A
RDAS Requirements: First Inspection from Time of
Repair Embodiment - 43700FC, controlled by WO
500899390.
IIR 57-21-11-1-006-00 FIRST INSPECTION AFTER
AIRCRAFT FIRST FLIGHT - 60000FC/107700FH
(WO:500894346)
Inspection Threshold: 72991 CSN, controlled by WO
500881399.
IIR 52-33-00-1-001-00 at 143208 CSN, controlled by
WO 500881398.
IIR 52-41-00-1-001-00 at 51540 FC, controlled by WO
500888436.
IIR 52-41-00-1-001-00 at 51540 FC, controlled by WO
500888444.
Inspection Threshold at 95492 TAC, controlled by WO
500888503.
Inspection Threshold: 113458 TAC, tracked by WO
500893829.
Inspection Threshold at 98891 TAC, controlled by WO
500893825.
IIR 53-21-11-1-001-00 at 61367 TAC, controlled by WO
500893840.
IIR 53-00-11-2-017-00 at 63208 TAC, tracked by WO
500893956.
N/A
WO: 500801691
TAH: 107700
TAC: 60000
WO: 500894344
TAH: 107700
TAC: 60000
WO: 500898763
TAH: 46822
TAC: 29505
WO: 500899390
TAC: 60666
N/A
N/A
N/A
N/A
N/A
N/A
N/A
N/A
N/A
N/A
N/A
N/A
WO: 500894346
TAH: 107700
TAC: 60000
WO: 500881399
TAC: 72991
WO: 500881398
TAC: 143208
WO: 500888436
TAC: 51540
WO: 500888444
TAC: 51540
WO: 500888503
TAC: 95492
WO: 500893829
TAC: 113458
WO: 500893825
TAC: 98891
WO: 500893840
TAC: 61367
WO: 500893956
TAC: 63208
Sub 2 - Page 13 of 16
SDM A319/A320 MAINTENANCE PROGRAM
INDIVIDUAL STRUCTURAL INSPECTIONS
MSN
ITEM
1890
7
1890
9
1890
12
1890
74
1890
REASON
FURTHER ACTION
FUSELAGE SKIN DENT.
MP REF: SDM.A320.BDCA
SECTION: V
REV: 03 DATE:06-OCT-2014
PERIODIC INSPECTION
IIR 53-11-11-1-001-00 at 67470 TAC, controlled by WO
500893994.
WO: 500019240
IIR 53-11-11-1-001-00 at 66873 TAC, controlled by WO
FUSELAGE SKIN DENT.
500894017.
WO: 500067679
IIR 53-11-11-2-009-00 at 72991 TAC, controlled by WO
FUSELAGE SKIN FLUSH REPAIR.
500894098.
CHAFING REWORKS AT UPPER CORNERS OF FWD IIR 53-11-11-1-003-00 at 72991 TAC / 157601 FH,
LH PAX DOOR SURROUNDING PANEL.
controlled by WO 500894132.
N/A
75
CHAFING REWORKS AT UPPER CORNERS OF FWD IIR 53-11-11-1-003-00 at 72991 TAC / 157601 FH,
RH PAX DOOR SURROUNDING PANEL.
controlled by WO 500894136.
N/A
1890
80
FUSELAGE SKIN EXTERNAL DOUBLER.
N/A
1890
81
REWORK ON FUSELAGE SKIN.
1890
82
WING Corrosion on Top Skin LWR Surface of LH TE
Panel #2
1890
86
FUSELAGE SKIN DENT.
1890
87
1890
88
IIR 57-21-11-1-005-00; JIC:14145 CONTROLLED
14145
1890
89
WING Corrosion on Top Skin LWR Surface of RH TE
Panel #2
WING Corrosion on Top Skin LWR Surface of RH TE
Panel #2
FUSELAGE SKIN DENT.
IIR 53-21-11-2-007-00 at 72991 TAC, controlled by WO
500894154.
IIR 53-21-11-1-003-00 at 72991 FC, controlled by WO
500894291.
IIR 57-21-11-1-004-00; FIRST INSPECTION AFTER
AIRCRAFT FIRST FLIGHT - 60000FC/107700FH;
WO:500894299
IIR 53-41-11-1-008-00 at 72991 TAC, controlled by WO
500894296.
IIR 57-21-11-1-007-00; JIC:14144 CONTROLLED
N/A
1890
90
FUSELAGE SKIN REWORK.
1890
91
FUSELAGE SKIN DENT WITH REWORK.
1890
94
FUSELAGE SKIN BULGE.
2151
1
R/H THS SPAR BOX LOWER SKIN BLENDOUTS
WITH SURFACE REPAIRS.
IIR 53-11-11-1-001-00 at 66873 TAC, controlled by WO
500894352.
IIR 53-11-11-1-002-00 at 72992 TAC, controlled by WO
500894528.
Inspection Threshold at 112992 TAC, controlled by WO
500894530.
Inspection Threshold at 72992 TAC, controlled by WO
500894532.
Inspection Threshold at 48000 FC / 60000 FH,
controlled by WO 500895011.
2151
2
DENT ON R/H SLAT #3 NOSE PART OF TOP SKIN.
IIR 57-40-00-1-001-00 at 120000 TAH / 60000 TAC,
controlled by WO 500897007.
N/A
N/A
N/A
N/A
N/A
N/A
N/A
14144
N/A
N/A
N/A
N/A
LIMIT
WO: 500893994
TAC: 67470
WO: 500894017
TAC: 66873
WO: 500894098
TAC: 72991
WO: 500894132
TAH: 157601
TAC: 72991
WO: 500894136
TAH: 157601
TAC: 72991
WO: 500894154
TAC: 72991
WO: 500894291
TAC: 72991
WO: 500894299
TAH: 107700
TAC: 60000
WO: 500894296
TAC: 72991
WO: 500894300
DATE: 2932167
WO: 500894332
DATE: 2932167
WO: 500894352
TAC: 66873
WO: 500894528
TAC: 72992
WO: 500894530
TAC: 112992
WO: 500894532
TAC: 72992
WO: 500895011
TAH: 60000
TAC: 48000
WO: 500897007
TAH: 120000
TAC: 60000
Sub 2 - Page 14 of 16
SDM A319/A320 MAINTENANCE PROGRAM
INDIVIDUAL STRUCTURAL INSPECTIONS
MSN
ITEM
REASON
FURTHER ACTION
MP REF: SDM.A320.BDCA
SECTION: V
REV: 03 DATE:06-OCT-2014
PERIODIC INSPECTION
LIMIT
2151
6
TWO REWORKS ON R/H WING SLAT #3 NOSE PART IIR 57-40-00-1-002-00 at 120000 TAH / 60000 TAC,
OF TOP SKIN.
controlled by WO 500896978.
N/A
2151
7
REWORK ON L/H WING SLAT #3 NOSE PART OF
TOP SKIN.
IIR 57-40-00-1-002-00 at 120000 TAH / 60000 TAC,
controlled by WO 500897029.
N/A
2151
9
10
2151
11
2151
12
2151
15
LH Elevator legacy repairs
2151
18
RH Wing fuel tank acc. door cutouts bottom skin
sarface fretting corrosion.
2151
19
PUNCTURE ON FUSELAGE SKIN UNDER BELLY
FAIRING LOCATED BETWEEN FR28 AND FR29.
RDAS Requirements: Periodical Inspection TH:6Y;
Interval:6Y (JIC:14255)
RDAS Requirements: Periodical Inspection TH6Y;
Interval:6Y (JIC:JIC:14255)
RDAS Requirements: Periodical Inspection
TH:41500FC; Interval:38700FC (JIC:14256)
IIR 57-21-11-1-002-00 (SSI 57.21.39) FIRST
INSPECTION AFTER AIRCRAFT FIRST FLIGHT:
60000FC/97500FH (WO:500914063)
IIR 55-21-11-2-002-00 FIRST INSPECTION AFTER
COMPONENT DELIVERY - 48000FC/60000FH
(WO:500914158)
IIR 57-21-11-1-002-00 (SSI 57.21.39) FIRST
INSPECTION AFTER AIRCRAFT FIRST FLIGHT:
60000FC/97500FH (WO:500914076)
IIR 53-00-11-2-004-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT - 60000FC (WO:500914087)
14255
2151
RUDDER SHELL HOIST POINT #3 LH WATER
INGRESS
RUDDER SHELL HOIST POINT #3 RH WATER
INGRESS
Crack on Fastener Hole #3 of Upper Flange of LH Side
Box Beam
LH Wing fuel tank acc. door cutouts bottom skin sarface
fretting corrosion.
2151
22
Corrosion on AFT Passenger Door Sill Beam of
Fuselage Floor Structure
N/A
2151
23
CHAFING ON FUSELAGE SKIN, AFT
PASSENGER/CREW LH DOOR UPPER CUTOUTS
RDAS Requirements: IIR 53-41-14-2-001-00 FIRST
INSPECTION AFTER REPAIR EMBODIMENT 92731FC/208644FH (WO:500914099)
IIR 53-41-11-1-002-00 FIRST INSPECTION FROM
AIRCRAFT DELIVERY - 60000FC (WO:500914148)
2151
24
CHAFING ON FUSELAGE SKIN, AFT
PASSENGER/CREW RH DOOR UPPER CUTOUTS
IIR 53-41-11-1-003-00 FIRST INSPECTION FROM
AIRCRAFT DELIVERY - 60000FC (WO:500914150)
N/A
WO: 500914150
TAC: 60000
2151
25
14254
2151
26
Corrosion on Upper Surface Upper Skin of Center Wing RDAS Requirements: Periodical Inspection TH:3Y;
Box
Interval:3Y (JIC:14254)
Internal corrosion between FR 30-34 (6 places)
IIR 53-21-11-1-003-00 FIRST INSPECTION AFTER
AIRCRAFT FIRST FLIGHT - 60000FC
(WO:500913835)
WO: 500913277
DATE: 2932167
WO: 500913835
TAC: 60000
14255
14256
N/A
N/A
N/A
N/A
N/A
N/A
WO: 500896978
TAH: 120000
TAC: 60000
WO: 500897029
TAH: 120000
TAC: 60000
WO: 500913848
DATE: 2932167
WO: 500913848
DATE: 2932167
WO: 500913898
DATE: 2932167
WO: 500914063
TAH: 97500
TAC: 60000
WO: 500914158
TAH: 69224
TAC: 32786
WO: 500914076
TAH: 97500
TAC: 60000
WO: 500914087
TAC: 77857
WO: 500914099
TAH: 249159
TAC: 110588
WO: 500914148
TAC: 60000
Sub 2 - Page 15 of 16
SDM A319/A320 MAINTENANCE PROGRAM
INDIVIDUAL STRUCTURAL INSPECTIONS
MSN
ITEM
REASON
FURTHER ACTION
MP REF: SDM.A320.BDCA
SECTION: V
REV: 03 DATE:06-OCT-2014
PERIODIC INSPECTION
LIMIT
2151
27
Corrosion on Fuselage skin R/H of FWD Cargo
Compartment
IRR 53-21-11-1-003-00 FIRST INSPECTION AFTER
REPAIR EMBODIMENT 60000FC (WO:500899857)
N/A
WO: 500899857
TAC: 77027
2151
31
L/H AFT PAX DOOR SEAL BEAM CORROSION
REWORKS.
Inspection Threshold at 246245 TAH / 105722 TAC,
controlled by WO 500897115.
N/A
2151
34
R/H AFT PAX DOOR SEAL BEAM CORROSION
REWORKS.
Inspection Threshold at 246245 TAH / 105722 TAC,
controlled by WO 500897123.
N/A
2151
35
36
Inspection Threshold at 55291 TAC, controlled by WO
500897155.
IIR 55-26-00-1-002-00 at 60000 TAC / 120000 TAH,
controlled by WO 500897167.
N/A
2151
BULK CARGO DOOR FRAME STOP FITTINGS WEAR.
L/H ELEVATOR ATTACH FITTING LOCKING LUG
WEAR.
2151
41
R/H ELEVATOR ATTACH FITTING LOCKING LUG
WEAR.
IIR 55-26-00-1-002-00 at 60000 TAC / 120000 TAH,
controlled by WO 500897171.
N/A
2151
52
Liquid ingress on the LH elevator top and bottom skin
panels
N/A
2151
53
Liquid ingress on the rudder side panel
IIR 55-21-11-2-002-00 FIRST INSPECTION AFTER
COMPONENT DELIVERY - 48000FC/60000FH
(WO:500904334)
IIR 55-41-13-1-002-00 FIRST INSPECTION AFTER
COMPONENT DELIVERY 48000FC WO:500899900
WO: 500897115
TAH: 246245
TAC: 105722
WO: 500897123
TAH: 246245
TAC: 105722
WO: 500897155
TAC: 55291
WO: 500897167
TAH: 120000
TAC: 60000
WO: 500897171
TAH: 120000
TAC: 60000
WO: 500904334
TAH: 60000
TAC: 48000
WO: 500899900
TAC: 48000
2151
54
Liquid ingress on the rudder side panel
IIR 55-41-13-1-002-00 FIRST INSPECTION AFTER
COMPONENT DELIVERY 48000FC WO:500899900
N/A
WO: 500899900
TAC: 48000
2151
62
Liquid ingress on the RH elevator top and bottom skin
panels
N/A
2151
63
AFT PAX/CREW DOOR REAR LOWER CORNER ON
DOOR SKIN EDGE 130MM FROM BOTTOM
IIR 55-21-11-2-002-00 FIRST INSPECTION AFTER
COMPONENT DELIVERY - 48000FC/60000FH
(WO:500904336)
IRR 52-10-00-1-002-00 INSPECTION AFTER 60000
FH REQUIRED WO: 500908515
WO: 500904336
TAH: 60000
TAC: 48000
WO: 500908515
TAH: 60000
2151
64
BURN MARK ON THE FUSELAGE SKIN
N/A
2151
65
BURN MARK ON THE SEVERAL HEAD RIVETS
2151
66
BURN MARK ON THE SEVERAL HEAD RIVETS
IRR 53-11-11-2-002-00 60000FC AFTER REPAIR
EMBODIMENT LIMWO: 500912082
IRR 53-11-11-2-002-00 48000FC AFTER REPAIR
EMBODIMENT LIMWO: 500912087; JIC Controlled
IRR 53-21-11-2-002-00 48000FC AFTER REPAIR
EMBODIMENT LIMWO: 500912135
N/A
N/A
N/A
14242
14243
WO: 500912082
TAC: 76594
WO: 500912087
TAC: 76594
WO: 500912135
TAC: 76594
Sub 2 - Page 16 of 16
SDM A319/A320 MAINTENANCE PROGRAM
APPENDIX I. EASA REQUIREMENTS REFERENCES
MP-REF: SDM.A320.BDCA
SECTION: VI
REV: 03 DATE: 06-Oct-2014
APPENDIX I. EASA REQUIREMENTS REFERENCES
This section provides the cross reference between the EASA requirements and the contents of this Operator Maintenance Program.
Appendix 1A to AMC M.A. 302 (EASA document ED Decision N°2003/19/RM 28/11/2003 amended by EASA document ED Decision 2007/001/R
13/03/2007)
Section
Requirements
Means of Compliance
1
General Requirements
N/A
1.1
Maintenance program basic information
N/A
1.1.1
The type/model and registration number of the aeroplane, engines and, where Section I:
applicable, auxiliary power units and propellers.
I. Introduction. C. Fleet Effectivity and Utilization
1.1.2
The name and address of the operator.
1.1.3
The operator’s reference identification of the program document; the date of All pages
issue and issue number.
1.1.4
A statement signed by the operator to the effect that the specified aeroplanes Section I:
will be maintained to the program and that the program will be reviewed and Operator's Certification Statement
updated as required by paragraph 5.
1.1.5
Contents/list of effective pages and their revision status of the document.
Section I:
List of Effective Pages And Recording Procedure
1.1.6
Check periods which reflect the anticipated utilization of the aeroplane. Such
utilization should be stated and include a tolerance of not more than 25%.
Where utilization cannot be anticipated, calendar time limits should also be
included.
Section I:
I. Introduction. C. Fleet Effectivity, Utilization and
Limit of Validity
I. Introduction. D. Intervals and Checks
1.1.7
Procedures for the escalation of established check periods, where applicable Section I:
Cover Page
Page 1 of 6
SDM A319/A320 MAINTENANCE PROGRAM
APPENDIX I. EASA REQUIREMENTS REFERENCES
Section
MP-REF: SDM.A320.BDCA
SECTION: VI
REV: 03 DATE: 06-Oct-2014
Requirements
Means of Compliance
and acceptable to the National Authority.
I. Introduction. D.4. Escalation of established
periods
1.1.8
Provision to record date and reference to approved amendments incorporated Section I:
in the program.
Records and Revision Highlights
1.1.9
Details of pre-flight maintenance tasks that are accomplished by maintenance Section I:
staff.
I. Introduction. D.2.a). Preflight Check
1.1.10
The tasks and the periods (intervals/frequencies) at which each part of the Sections II and III
aircraft, engines, APU’s, propellers, components, accessories, equipment,
instruments, electrical and radio apparatus, together with the associated
systems and installations should be inspected. This should be include the type
and degree of inspection required.
1.1.11
The periods at which items as appropriate, should be checked, cleaned, Sections II and III
lubricated, replenished, adjusted and tested.
1.1.12
If applicable details of ageing aircraft system requirements together with any Section I:
specified sampling programs.
I. Introduction. E.2. Structural Inspection
Program
1.1.13
If applicable details of specific structural maintenance programmes where Section I:
issued by the type certificate holder including but not limited to:
I. Introduction. E.2. Structural Inspection
 Maintenance of structural integrity by damage tolerance and Program
supplemental structural inspection programmes (SSID)
 Structural maintenance programmes resulting from SB review performed
by the TC holder
 Corrosion prevention and control
 Repair assessment
Page 2 of 6
SDM A319/A320 MAINTENANCE PROGRAM
APPENDIX I. EASA REQUIREMENTS REFERENCES
Section
Requirements

MP-REF: SDM.A320.BDCA
SECTION: VI
REV: 03 DATE: 06-Oct-2014
Means of Compliance
Widespread fatigue damage
1.1.14
If applicable, details of Critical Design Configuration Control Limitations together N/A
with appropriate procedure.
Refer to owner or an M.A. subpart G approved
organization's Aircraft Maintenance Manual
1.1.15
If applicable a statement of the limit of validity in terms of total flight Section I. C. Fleet effectivity, utilization and limit
cycles/calendar date/flight hours for structural programme in 1.1.13.
of validity
1.1.16
The periods at which overhauls and/or replacements by new or overhauled Section III
parts should be made
1.1.17
A cross-reference to other documents approved by the Authority which contain
the details of maintenance tasks related to mandatory life limitations,
Certification Maintenance Requirements (CMR’s) and Airworthiness Directives
(AD’s).
To prevent inadvertent variations to such tasks or intervals these items should
not be included in the main portion of the maintenance program document, or
any planning control system, without specific identification of their mandatory
status.
Section I,
I. Introduction, E. Incorporated Maintenance
Programs, 5. Additional Programs
All mandatory tasks have identification mark in
the Source Column of the MP.
1.1.18
Details of, or cross-reference to, any required Reliability Program or statistical Section I:
methods of continuous Surveillance.
I. Introduction, E. Incorporated Maintenance
Programs, 5. Additional Programs, e) Reliability
Program
1.1.19
A statement that practices and procedures to satisfy the Program should be to Section I:
the standards specified in the Type Certificate Holder’s Maintenance OPERATOR’S CERTIFICATION STATEMENT:
Instructions. In the case of approved practices and procedures that differ, the
statement should refer to this Manual.
Page 3 of 6
SDM A319/A320 MAINTENANCE PROGRAM
APPENDIX I. EASA REQUIREMENTS REFERENCES
MP-REF: SDM.A320.BDCA
SECTION: VI
REV: 03 DATE: 06-Oct-2014
Section
Requirements
Means of Compliance
1.1.20
Each maintenance task quoted should be defined in a definition section of the Section II and III:
Program.
2
Program basis
2.1
An owner or an M.A. subpart G approved organization's aircraft Maintenance Section I:
programs should normally be based upon the Maintenance Review Board I. Introduction, B. Maintenance Program
Report, where available, and the Type Certificate holder’s Maintenance Documents
Planning Document or Chapter 5 of the Maintenance Manual, (i.e. the
Manufacturer’s recommended Maintenance Program). The structure and format
of these maintenance recommendations may be re-written by the owner or an
M.A. subpart G approved organization to better suit his operation and control of
the particular maintenance program.
2.2
For a newly type-certificated aeroplane, where no previously approved N/A
Maintenance Program exists, it will be necessary for the owner or an M.A.
subpart G approved organization to comprehensively appraise the
manufacturer’s recommendations (and the MRB Report where applicable),
together with other airworthiness information, in order to produce a realistic
Program for approval.
2.3
For existing aeroplane types it is permissible for the operator to make Section Airworthiness Authorities Approval
comparisons with maintenance programs previously approved. It should not be
assumed that a Program approved for another operator will automatically be
approved for the operator. Evaluation is to be made of aircraft/fleet utilization,
landing rate, equipment fit and, in particular, the experience of the owner or an
M.A. subpart G approved organization when assessing an existing programme.
Where the Authority is not satisfied that the proposed maintenance program can
be used as is, the Authority should request appropriate changes such as
N/A
Page 4 of 6
SDM A319/A320 MAINTENANCE PROGRAM
APPENDIX I. EASA REQUIREMENTS REFERENCES
Section
Requirements
MP-REF: SDM.A320.BDCA
SECTION: VI
REV: 03 DATE: 06-Oct-2014
Means of Compliance
additional maintenance tasks or de-escalation of check frequencies as
necessary.
2.4
If CDCCL have been identified for the aircraft type by the TC/STC holder, Section I, F. 1. General Standard, g) CDCCL
maintenance instructions should be developed. CDCCL's are characterized by
features in an aircraft installation or component that should be retained during Refer to owner or an M.A. subpart G approved
modification, change, repair, or scheduled maintenance for the operational life organization's Aircraft Maintenance Manual
of the aircraft or applicable component or part.
3
Amendments
3.1
Amendments (revisions) to the approved Program should be raised by the Section I: RECORDS AND REVISION
owner or an M.A. subpart G approved organization, to reflect changes in the HIGHLIGHTS
type certificate holder’s recommendations, modifications, service experience, or B. Procedure of revisions
as required by the Authority.
4
Permitted variations to maintenance periods
4.1
The owner or an M.A. subpart G approved organization may only vary the Section I. Introduction, D. Intervals and checks.
periods prescribed by the Programme with the approval of the Authority or 5. Variations to maintenance periods
through a procedure developed in the maintenance programme and approved
by the competent authority.
5
Periodic review of maintenance program contents
5.1
The owner or an M.A. subpart G approved organization's approved Section RECORDS AND REVISION
Maintenance Programmes should be subject to periodic review to ensure that HIGHLIGHTS
they reflect current Type Certificate holder’s recommendations, revisions to the B. Procedure of revisions
Maintenance Review Board Report if applicable, mandatory requirements and
maintenance needs of the aircraft.
5.2
The owner or an M.A. subpart G approved organization should review the Section RECORDS AND REVISION
N/A
N/A
N/A
Page 5 of 6
SDM A319/A320 MAINTENANCE PROGRAM
APPENDIX I. EASA REQUIREMENTS REFERENCES
Section
Requirements
MP-REF: SDM.A320.BDCA
SECTION: VI
REV: 03 DATE: 06-Oct-2014
Means of Compliance
detailed requirements at least annually for continued validity in the light of HIGHLIGHTS
operating experience.
B. Procedure of revisions
Page 6 of 6
MP-REF: SDM.A320.BDCA
SECTION: VII
REV: 03 DATE: 06-Oct-2014
SDM A319/A320 MAINTENANCE PROGRAM
APPENDIX II. BDCA AW 287 REFERENCES
APPENDIX II. BDCA AW 287 REFERENCES
Here’s filled form in order to reflect maintenance program compliance with OTAR 39 Maintenance Programme Compliance Checklist Form AW 287:
#
Reference
Requirement
MP Reference
Compliance Notes
1
39.51 (a)
Except where provided in paragraph 39.51(b), the owner or, where it is Section I "Operator's Operator and CAMO is
leased, the lessee of an aircraft registered in the Territory shall appoint a Certification
the same company
person acceptable to the Governor and known as the Technical Statement"
Coordinator who will ensure that appropriate arrangements for continued
airworthiness management required by this OTAR Part are in place.
2
39.51 (b)
Each holder of an air operator’s
certificate shall appoint a post holder under the requirements of OTAR Part
119 within its organisation who will be
responsible for the continued
airworthiness management of the operator’s aircraft as required by this
OTAR Part.
3
39.51 (c)
The appointed post-holder for
Section I "Operator's Operator and CAMO is
continued airworthiness of Territory registered aircraft operating under a Certification
the same company
foreign air operator’s certificate and the provisions of an ICAO Article 83bis Statement"
agreement shall establish and maintain arrangements for the continued
airworthiness management of the Territory registered aircraft as required
by Subpart F of this OTAR Part.
4
39.61 (a)
Aircraft granted a certificate of
Section
airworthiness to the equirements of OTAR Part 21 Subpart E shall be "Authorities
maintained in accordance with a maintenance programme approved by the Approval"
Governor.
N/A
Operator is not OTAR
119 certified, refer to
39.51 (c).
I.
Page 1 of 10
MP-REF: SDM.A320.BDCA
SECTION: VII
REV: 03 DATE: 06-Oct-2014
SDM A319/A320 MAINTENANCE PROGRAM
APPENDIX II. BDCA AW 287 REFERENCES
#
5
Reference
39.61 (b)
Requirement
The maintenance programme and any amendments shall require approval
by the Governor for each aircraft, and shall include details of the
maintenance of the aircraft, engines, propellers, rotors,
appliances and emergency equipment items.
MP Reference
Compliance Notes
Section I.
- CONTENTS
- RECORDS AND
REVISION
HIGHLIGHTS
Section I. I.C
6
39.61 (c)
The maintenance programme shall reference the required inspection Section
I.
I.B
standards, practices and procedures that shall be at least equivalent to the Maintenance
Type Certificate holder’s scheduled maintenance requirements.
Program Documents
7
39.61 (d)
Any schedule of inspections/tests required by any approved programme Section
amendment shall be introduced in a controlled manner to ensure the RECORDS
continued airworthiness of the aircraft.
REVISION
HIGHLIGHTS
I.
AND
Page 2 of 10
SDM A319/A320 MAINTENANCE PROGRAM
APPENDIX II. BDCA AW 287 REFERENCES
#
8
Reference
39.61 (e)
Requirement
Consideration shall be given to human performance within the
maintenance programme including the format of the maintenance
programme document, maintenance task breakdown and combined
maintenance tasking, particularly safety critical tasks which shall be
identified in the maintenance programme.
MP Reference
MP-REF: SDM.A320.BDCA
SECTION: VII
REV: 03 DATE: 06-Oct-2014
Compliance Notes
Sections II and III AMO planning will take
Maintenance
in account HF critical
program with the list factors while packaging
of tasks.
maintenance events.
Source
column
identifies ALI, FAL,
AD/CN
for
the
Safety
Critical
Tasks.
AMP
have
all
necessary references
to
the
critical
inspections.
MCM/CAME
All tasks have AMM Reference:
or JIC references.
SDM.CAME 2.8
and
SDM MOE P.2.23
9
39.61 (f)
See also
item #25
The maintenance programme shall readily identify any certification Section
I.
I.H.8 All tasks have their
inspection tasks and other significant continued airworthiness inspection Source Column
source reference. This
tasks that are the subject of specific control and mandated by the
section shows task
applicable State of Type Certification, as referred to in OTAR Part 21.19(a)
source data including
such as but not limited to:
special requirements
(1)Supplemental Structural
Inspection Document;
(2)Fuel Tank Safety Inspections;
(3)Ageing Aircraft;
(4)Widespread FatigueDamage;
(5)Electrical Wiring Interconnection
Systems (EWIS).
Page 3 of 10
SDM A319/A320 MAINTENANCE PROGRAM
APPENDIX II. BDCA AW 287 REFERENCES
#
Reference
Requirement
MP Reference
MP-REF: SDM.A320.BDCA
SECTION: VII
REV: 03 DATE: 06-Oct-2014
Compliance Notes
10
39.61 (g)
Each maintenance programme approval holder shall make any revisions to Section I "Operator's
the maintenance programme as required by the Governor and any Certification
applicable mandatory amendments promulgated by the Type Certificate Statement"
holder or its NAA to satisfy the continuing airworthiness requirements of the
aircraft.
11
39.61 (h)
(1) an explanation of the programme, including the continuity of inspection Section I. I.A
responsibility, procedures for making any required reports and
Section I. I.B
technical reference material; and
12
39.61 (h)
(2) instructions and procedures for the implementation of inspection tasks Section I.
for the particular aircraft type, taking account of the aircraft modification I.E.5.p)
status and any repairs that have associated instructions for continued I.E.5.q)
airworthiness; and
Modification inspection
requirements
implemented into AMP
13
39.61 (h)
(3) an inspection schedule for performing the inspections required by the Section II
programme expressed in terms of the total time in service, cycles, calendar Section III
time, number of system operations, or any combination of these; and
Maintenance
tasks
program
14
39.61 (h)
(4) for a progressive inspection
Section II
programme, an inspection schedule that provides for the complete Section III
inspection of the aircraft within each 12 month period or is consistent with:
(i) the manufacturer’s
recommendations;
(ii) the operator’s service experience;
(iii) the type of operation in which the aircraft is engaged;
(iv) the utilisation of the aircraft in terms of hours and cycles or a
combination there of.
Maintenance
tasks
program
Page 4 of 10
SDM A319/A320 MAINTENANCE PROGRAM
APPENDIX II. BDCA AW 287 REFERENCES
#
15
Reference
39.61 (h)
16
Requirement
(5) instructions taking account of
detailed technical justification, for altering and gaining approval for a
change of inspection intervals or a maintenance process because of
service experience; and
MP Reference
MP-REF: SDM.A320.BDCA
SECTION: VII
REV: 03 DATE: 06-Oct-2014
Compliance Notes
Section I
I. D. 4 Escalation of
established periods
(6) instructions for varying an
Section I I.D.5
inspection interval under exceptional circumstances taking account of Variations
to
overriding mandatory requirements and maintenance programme maintenance periods
inspection requirements
referred to in paragraphs 39.61(e) and (f); and
17
39.61 (h)
(7) sample inspection forms, reports and instructions for their use; and
MCM/CAME
Reference:
SDM CAME 5.1
18
39.61 (h)
(8) procedures for maintenance trend analysis if the programme utilizes Section I:
condition monitored maintenance or information derived from health and I.E.5.e)
usage monitoring systems; and
I.E.5.f)
MCM/CAME
Reference:
1.10
Reliability
Program
19
39.61 (h)
(9) inspection requirements required for approved special operations; and
20
39.61 (h)
(10) instructions for continued
Task interval 24MO
airworthiness including verification of data acquisition of any installed flight
recorder systems required by the applicable State of Type
313300-01-1-SDM
Certification; and
21
39.61 (h)
(11) a list of definitions and acronyms used
Section I:
I.E.5.g)
Section I. I.F
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SDM A319/A320 MAINTENANCE PROGRAM
APPENDIX II. BDCA AW 287 REFERENCES
#
Reference
Requirement
MP Reference
22
39.63 (b)
(b) The application for approval of the maintenance programme shall Cover Page,
contain, or references shall be made to, the following information:
Section
I.
(1) the name and address of the
AIRWORTHINESS
owner or lessee or the holder of
AUTHORITIES
an air operator’s certificate; and
APPROVAL
23
39.63 (b)
(4) technical justification relating
to the anticipated utilisation of
the aircraft, inspection intervals
and procedures for inspection
task management; and
24
39.63 (b)
(5) a copy of the maintenance
programme either in hard copy or electronic format in a manner
acceptable to the Governor; and
25
39.63 (b)
See also
item #9
(6) copies of any other supporting documents, such as condition monitored Section I. I.B
maintenance activities, structural integrity programmes, engine off-wing
maintenance programes, fuel tank safety inspection programmes; and
26
39.63 (b)
(7) the aircraft designation, serial number and registration mark for each Section I. I.C
aircraft that is subject to the programme; and
27
39.63 (b)
(8) any further particulars relating to the programme and applicant as may
be required by the Governor.
Section I. I.C
MP-REF: SDM.A320.BDCA
SECTION: VII
REV: 03 DATE: 06-Oct-2014
Compliance Notes
Task
intervals
in
maintenance program
Se mail attachment
N/A
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28
Reference
39.65
Requirement
MP Reference
(a) Where the anufacturer of aircraft, engines and propellers prescribe Section I:
condition monitoring, reliability programmes or health and usage monitoring I.E.5.e)
systems these shall form part of the maintenance programme approved by I.E.5.f)
the Governor under
paragraph 39.63. (b) Appropriate procedures acceptable to the Governor
shall be established for any applicable condition monitoring or reliability or
health and usage monitoring systems referred to in paragraph 39.65(a). (c)
Where data gathering is required, the following shall form the basis of an
acceptable programme:
(1) aircraft utilisation; and
(2) pilot reports; and
(3) aircraft mechanical delays and cancellations;
(4) unscheduled engine shutdowns; and
(5) unscheduled engine removals;
(6) unscheduled component
removals; and
(7) confirmed component failures;
(8) occurrences.
MP-REF: SDM.A320.BDCA
SECTION: VII
REV: 03 DATE: 06-Oct-2014
Compliance Notes
MCM/CAME
Reference:
1.10
Reliability
Program
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29
Reference
39.81
Requirement
(a) Aircraft are to be weighed at intervals not exceeding 5 years; or (1)
where the aircraft is part of a fleet weighing programme specified by the
type certificate holder and accepted by the Governor, at intervals specified
by that programme; and (2) whenever alterations affecting mass and
balance of the aircraft are made that exceed the limits for computed mass
and balance changes advised by the aircraft type certificate holder.
MP Reference
MP-REF: SDM.A320.BDCA
SECTION: VII
REV: 03 DATE: 06-Oct-2014
Compliance Notes
(a) MP task 00000101-1-SDM interval 4
Years
(1) N/A
(2) MCM/CAME
Reference:
1.12
Aeroplane
weighing
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Reference
30
OTAC 39-6
(Issue 2,
13 March
2012)
Requirement
15 Permitted variations to Maintenance periods
15.1 Periods prescribed by the Maintenance Programme may only be
varied with theapproval of BDCA .15.2 It is the responsibility of the
Technical Coordinator (TC) or contracted approvedContinued
Airworthiness Management organisation to ensure that arrangements
areeffectively established to maintain the aircraft in accordance with the
approved Maintenance Programme. 15.3 Unless specifically prohibited by
an Airworthiness Directive or a manufacturer’s requirement, inspection
periods may be varied in accordance with the ‘Inspection Planning
Tolerance – Extensions’ (shown in Table 1 below) Table 1
PERIOD
Items controlled by flying hours
5,000 flying hours or less
More than 5,000 flying hours
Items controlled by calendar time
One year or less
More than 1year but less than 3
yearsthan 3 years
More
MP Reference
MP-REF: SDM.A320.BDCA
SECTION: VII
REV: 03 DATE: 06-Oct-2014
Compliance Notes
Section I I.D.5
Variations
to
maintenance periods
MAXIMUM VARIATION
10%
500 flying hours
The lesser of 10% or one month
2 months
3 Months
Items controlled by cycles or landings
500 cycles/landings or less
More than 500 cycles/landings
The lesser of 10% or 25 cycles/landings
The lesser of 10% or 500 cycles/landings
15.4 For items that are controlled by more than one limit i.e. flying hours
and calendar time, the more restrictive limit will apply.15.5 The extension
periods in Table 1 above should be supported by appropriate technical
justification. This should be established from a detailed review of the
aircraft records, maintenance and operational history. It should also
establish inspection requirements that cannot be subject to variation as per
Table 1. 15.6 The period to the next required inspection shall be deemed to
begin at the point prior to when the task/interval was extended. No
extension may be taken towards the next required inspection.
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SECTION: VII
REV: 03 DATE: 06-Oct-2014
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