MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 Produced by Operator’s Engineering Department Approved by IAA SDM A319/A320 MAINTENANCE PROGRAM COVER PAGE MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 THIS PAGE INTENTIONALLY LEFT BLANK Page 2 of 116 SDM A319/A320 MAINTENANCE PROGRAM OPERATOR’S CERTIFICATION STATEMENT MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 THIS PAGE INTENTIONALLY LEFT BLANK Page 4 of 116 SDM A319/A320 MAINTENANCE PROGRAM LIST OF CONCORDANCE MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 THIS PAGE INTENTIONALLY LEFT BLANK Page 6 of 116 SDM A319/A320 MAINTENANCE PROGRAM AIRWORTHINESS AUTHORITIES APPROVAL MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 THIS PAGE INTENTIONALLY LEFT BLANK Page 8 of 116 SDM A319/A320 MAINTENANCE PROGRAM AIRWORTHINESS AUTHORITIES APPROVAL MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 THIS PAGE IS RESERVED FOR IAA MAINTENANCE PROGRAM APPROVAL CERTIFICATE THIS SHEET HAS TO BE CHANGED AS SOON AS MAINTENANCE PROGRAM APPROVAL CERTIFICATE RECEIVED Page 9 of 116 SDM A319/A320 MAINTENANCE PROGRAM AIRWORTHINESS AUTHORITIES APPROVAL MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 THIS PAGE IS RESERVED FOR IAA MAINTENANCE PROGRAM APPROVAL CERTIFICATE THIS SHEET HAS TO BE CHANGED AS SOON AS MAINTENANCE PROGRAM APPROVAL CERTIFICATE RECEIVED Page 10 of 116 SDM A319/A320 MAINTENANCE PROGRAM CONTENTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 CONTENTS COVER PAGE ..................................................................................................................................................................................................................... 1 OPERATOR’S CERTIFICATION STATEMENT .................................................................................................................................................................. 3 LIST OF CONCORDANCE .................................................................................................................................................................................................. 5 AIRWORTHINESS AUTHORITIES APPROVAL ................................................................................................................................................................. 7 CONTENTS ....................................................................................................................................................................................................................... 11 LIST OF EFFECTIVE PAGES AND RECORDING PROCEDURE .................................................................................................................................... 13 RECORDS AND REVISION HIGHLIGHTS ....................................................................................................................................................................... 19 A. DISTRIBUTION LIST .............................................................................................................................................................................................. 19 B. PROCEDURE OF REVISIONS............................................................................................................................................................................... 20 C. PROCEDURE OF TEMPORARY REVISIONS ....................................................................................................................................................... 22 D. REVISION HIGHLIGHTS ........................................................................................................................................................................................ 23 I. INTRODUCTION ........................................................................................................................................................................................................ 51 A. MAINTENANCE PROGRAM DESCRIPTION ........................................................................................................................................................ 51 B. MAINTENANCE PROGRAM DOCUMENTS ......................................................................................................................................................... 51 C. FLEET EFFECTIVITY, UTILIZATION AND LIMIT OF VALIDITY (LOV) ................................................................................................................ 53 D. INTERVALS AND CHECKS ................................................................................................................................................................................... 56 E. INCORPORATED MAINTENANCE PROGRAMS ................................................................................................................................................. 64 F. STANDARDS, DEFINITIONS AND ABBREVATIONS ........................................................................................................................................... 88 G. ZONAL DIAGRAMS ............................................................................................................................................................................................. 101 Page 11 of 116 SDM A319/A320 MAINTENANCE PROGRAM CONTENTS H. MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 MAINTENANCE PROGRAM LAYOUT ................................................................................................................................................................ 108 II. SCHEDULED MAINTENANCE PROGRAM ............................................................................................................................................................. 1 III. TIME CONTROLLED ITEMS .................................................................................................................................................................................... 1 IV. MOD CONTROLLED ITEMS .................................................................................................................................................................................... 1 V. INDIVIDUAL STRUCTURAL INSPECTIONS ........................................................................................................................................................... 1 A. STRUCTURAL INSPECTIONS LAYOUT ................................................................................................................................................................. 1 B. INSPECTIONS MAINTNENANCE PROGRAM ........................................................................................................................................................ 2 APPENDIX I. EASA REQUIREMENTS REFERENCES ..................................................................................................................................................... 1 Page 12 of 116 SDM A319/A320 MAINTENANCE PROGRAM LIST OF EFFECTIVE PAGES AND RECORDING PROCEDURE MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 LIST OF EFFECTIVE PAGES AND RECORDING PROCEDURE 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. Page 13 of 116 MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-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 I 1 29-Dec-2014 I 27 29-Dec-2014 I 53 29-Dec-2014 I 79 29-Dec-2014 I 105 29-Dec-2014 I 2 29-Dec-2014 I 28 29-Dec-2014 I 54 29-Dec-2014 I 80 29-Dec-2014 I 106 29-Dec-2014 I 3 29-Dec-2014 I 29 29-Dec-2014 I 55 29-Dec-2014 I 81 29-Dec-2014 I 107 29-Dec-2014 I 4 29-Dec-2014 I 30 29-Dec-2014 I 56 29-Dec-2014 I 82 29-Dec-2014 I 108 29-Dec-2014 I 5 29-Dec-2014 I 31 29-Dec-2014 I 57 29-Dec-2014 I 83 29-Dec-2014 I 109 29-Dec-2014 I 6 29-Dec-2014 I 32 29-Dec-2014 I 58 29-Dec-2014 I 84 29-Dec-2014 I 110 29-Dec-2014 I 7 29-Dec-2014 I 33 29-Dec-2014 I 59 29-Dec-2014 I 85 29-Dec-2014 I 111 29-Dec-2014 I 8 29-Dec-2014 I 34 29-Dec-2014 I 60 29-Dec-2014 I 86 29-Dec-2014 I 112 29-Dec-2014 I 9 29-Dec-2014 I 35 29-Dec-2014 I 61 29-Dec-2014 I 87 29-Dec-2014 I 113 29-Dec-2014 I 10 29-Dec-2014 I 36 29-Dec-2014 I 62 29-Dec-2014 I 88 29-Dec-2014 I 114 29-Dec-2014 I 11 29-Dec-2014 I 37 29-Dec-2014 I 63 29-Dec-2014 I 89 29-Dec-2014 I 115 29-Dec-2014 I 12 29-Dec-2014 I 38 29-Dec-2014 I 64 29-Dec-2014 I 90 29-Dec-2014 I 116 29-Dec-2014 I 13 29-Dec-2014 I 39 29-Dec-2014 I 65 29-Dec-2014 I 91 29-Dec-2014 II-1 1 29-Dec-2014 I 14 29-Dec-2014 I 40 29-Dec-2014 I 66 29-Dec-2014 I 92 29-Dec-2014 II-2 1 29-Dec-2014 I 15 29-Dec-2014 I 41 29-Dec-2014 I 67 29-Dec-2014 I 93 29-Dec-2014 II-2 2 29-Dec-2014 I 16 29-Dec-2014 I 42 29-Dec-2014 I 68 29-Dec-2014 I 94 29-Dec-2014 II-2 3 29-Dec-2014 I 17 29-Dec-2014 I 43 29-Dec-2014 I 69 29-Dec-2014 I 95 29-Dec-2014 II-2 4 29-Dec-2014 I 18 29-Dec-2014 I 44 29-Dec-2014 I 70 29-Dec-2014 I 96 29-Dec-2014 II-2 5 29-Dec-2014 I 19 29-Dec-2014 I 45 29-Dec-2014 I 71 29-Dec-2014 I 97 29-Dec-2014 II-2 6 29-Dec-2014 I 20 29-Dec-2014 I 46 29-Dec-2014 I 72 29-Dec-2014 I 98 29-Dec-2014 II-2 7 29-Dec-2014 I 21 29-Dec-2014 I 47 29-Dec-2014 I 73 29-Dec-2014 I 99 29-Dec-2014 II-2 8 29-Dec-2014 I 22 29-Dec-2014 I 48 29-Dec-2014 I 74 29-Dec-2014 I 100 29-Dec-2014 II-2 9 29-Dec-2014 I 23 29-Dec-2014 I 49 29-Dec-2014 I 75 29-Dec-2014 I 101 29-Dec-2014 II-2 10 29-Dec-2014 I 24 29-Dec-2014 I 50 29-Dec-2014 I 76 29-Dec-2014 I 102 29-Dec-2014 II-2 11 29-Dec-2014 I 25 29-Dec-2014 I 51 29-Dec-2014 I 77 29-Dec-2014 I 103 29-Dec-2014 II-2 12 29-Dec-2014 I 26 29-Dec-2014 I 52 29-Dec-2014 I 78 29-Dec-2014 I 104 29-Dec-2014 II-2 13 29-Dec-2014 Page 14 of 116 MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-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 II-2 14 29-Dec-2014 II-2 40 29-Dec-2014 II-2 66 29-Dec-2014 II-2 92 29-Dec-2014 II-2 118 29-Dec-2014 II-2 15 29-Dec-2014 II-2 41 29-Dec-2014 II-2 67 29-Dec-2014 II-2 93 29-Dec-2014 II-2 119 29-Dec-2014 II-2 16 29-Dec-2014 II-2 42 29-Dec-2014 II-2 68 29-Dec-2014 II-2 94 29-Dec-2014 II-2 120 29-Dec-2014 II-2 17 29-Dec-2014 II-2 43 29-Dec-2014 II-2 69 29-Dec-2014 II-2 95 29-Dec-2014 II-2 121 29-Dec-2014 II-2 18 29-Dec-2014 II-2 44 29-Dec-2014 II-2 70 29-Dec-2014 II-2 96 29-Dec-2014 II-2 122 29-Dec-2014 II-2 19 29-Dec-2014 II-2 45 29-Dec-2014 II-2 71 29-Dec-2014 II-2 97 29-Dec-2014 II-2 123 29-Dec-2014 II-2 20 29-Dec-2014 II-2 46 29-Dec-2014 II-2 72 29-Dec-2014 II-2 98 29-Dec-2014 II-2 124 29-Dec-2014 II-2 21 29-Dec-2014 II-2 47 29-Dec-2014 II-2 73 29-Dec-2014 II-2 99 29-Dec-2014 II-2 125 29-Dec-2014 II-2 22 29-Dec-2014 II-2 48 29-Dec-2014 II-2 74 29-Dec-2014 II-2 100 29-Dec-2014 II-2 126 29-Dec-2014 II-2 23 29-Dec-2014 II-2 49 29-Dec-2014 II-2 75 29-Dec-2014 II-2 101 29-Dec-2014 II-2 127 29-Dec-2014 II-2 24 29-Dec-2014 II-2 50 29-Dec-2014 II-2 76 29-Dec-2014 II-2 102 29-Dec-2014 II-2 128 29-Dec-2014 II-2 25 29-Dec-2014 II-2 51 29-Dec-2014 II-2 77 29-Dec-2014 II-2 103 29-Dec-2014 II-2 129 29-Dec-2014 II-2 26 29-Dec-2014 II-2 52 29-Dec-2014 II-2 78 29-Dec-2014 II-2 104 29-Dec-2014 II-2 130 29-Dec-2014 II-2 27 29-Dec-2014 II-2 53 29-Dec-2014 II-2 79 29-Dec-2014 II-2 105 29-Dec-2014 II-2 131 29-Dec-2014 II-2 28 29-Dec-2014 II-2 54 29-Dec-2014 II-2 80 29-Dec-2014 II-2 106 29-Dec-2014 II-2 132 29-Dec-2014 II-2 29 29-Dec-2014 II-2 55 29-Dec-2014 II-2 81 29-Dec-2014 II-2 107 29-Dec-2014 II-2 133 29-Dec-2014 II-2 30 29-Dec-2014 II-2 56 29-Dec-2014 II-2 82 29-Dec-2014 II-2 108 29-Dec-2014 II-2 134 29-Dec-2014 II-2 31 29-Dec-2014 II-2 57 29-Dec-2014 II-2 83 29-Dec-2014 II-2 109 29-Dec-2014 II-2 135 29-Dec-2014 II-2 32 29-Dec-2014 II-2 58 29-Dec-2014 II-2 84 29-Dec-2014 II-2 110 29-Dec-2014 II-2 136 29-Dec-2014 II-2 33 29-Dec-2014 II-2 59 29-Dec-2014 II-2 85 29-Dec-2014 II-2 111 29-Dec-2014 II-2 137 29-Dec-2014 II-2 34 29-Dec-2014 II-2 60 29-Dec-2014 II-2 86 29-Dec-2014 II-2 112 29-Dec-2014 II-2 138 29-Dec-2014 II-2 35 29-Dec-2014 II-2 61 29-Dec-2014 II-2 87 29-Dec-2014 II-2 113 29-Dec-2014 II-2 139 29-Dec-2014 II-2 36 29-Dec-2014 II-2 62 29-Dec-2014 II-2 88 29-Dec-2014 II-2 114 29-Dec-2014 II-2 140 29-Dec-2014 II-2 37 29-Dec-2014 II-2 63 29-Dec-2014 II-2 89 29-Dec-2014 II-2 115 29-Dec-2014 II-2 141 29-Dec-2014 II-2 38 29-Dec-2014 II-2 64 29-Dec-2014 II-2 90 29-Dec-2014 II-2 116 29-Dec-2014 II-2 142 29-Dec-2014 II-2 39 29-Dec-2014 II-2 65 29-Dec-2014 II-2 91 29-Dec-2014 II-2 117 29-Dec-2014 II-2 143 29-Dec-2014 Page 15 of 116 MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-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 II-2 144 29-Dec-2014 II-2 170 29-Dec-2014 II-2 196 29-Dec-2014 II-2 222 29-Dec-2014 II-2 248 29-Dec-2014 II-2 145 29-Dec-2014 II-2 171 29-Dec-2014 II-2 197 29-Dec-2014 II-2 223 29-Dec-2014 II-2 249 29-Dec-2014 II-2 146 29-Dec-2014 II-2 172 29-Dec-2014 II-2 198 29-Dec-2014 II-2 224 29-Dec-2014 II-2 250 29-Dec-2014 II-2 147 29-Dec-2014 II-2 173 29-Dec-2014 II-2 199 29-Dec-2014 II-2 225 29-Dec-2014 II-2 251 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II-2 209 29-Dec-2014 II-2 235 29-Dec-2014 II-2 261 29-Dec-2014 II-2 158 29-Dec-2014 II-2 184 29-Dec-2014 II-2 210 29-Dec-2014 II-2 236 29-Dec-2014 II-2 262 29-Dec-2014 II-2 159 29-Dec-2014 II-2 185 29-Dec-2014 II-2 211 29-Dec-2014 II-2 237 29-Dec-2014 II-2 263 29-Dec-2014 II-2 160 29-Dec-2014 II-2 186 29-Dec-2014 II-2 212 29-Dec-2014 II-2 238 29-Dec-2014 II-2 264 29-Dec-2014 II-2 161 29-Dec-2014 II-2 187 29-Dec-2014 II-2 213 29-Dec-2014 II-2 239 29-Dec-2014 II-2 265 29-Dec-2014 II-2 162 29-Dec-2014 II-2 188 29-Dec-2014 II-2 214 29-Dec-2014 II-2 240 29-Dec-2014 II-2 266 29-Dec-2014 II-2 163 29-Dec-2014 II-2 189 29-Dec-2014 II-2 215 29-Dec-2014 II-2 241 29-Dec-2014 II-2 267 29-Dec-2014 II-2 164 29-Dec-2014 II-2 190 29-Dec-2014 II-2 216 29-Dec-2014 II-2 242 29-Dec-2014 II-2 268 29-Dec-2014 II-2 165 29-Dec-2014 II-2 191 29-Dec-2014 II-2 217 29-Dec-2014 II-2 243 29-Dec-2014 II-2 269 29-Dec-2014 II-2 166 29-Dec-2014 II-2 192 29-Dec-2014 II-2 218 29-Dec-2014 II-2 244 29-Dec-2014 II-2 270 29-Dec-2014 II-2 167 29-Dec-2014 II-2 193 29-Dec-2014 II-2 219 29-Dec-2014 II-2 245 29-Dec-2014 II-2 271 29-Dec-2014 II-2 168 29-Dec-2014 II-2 194 29-Dec-2014 II-2 220 29-Dec-2014 II-2 246 29-Dec-2014 II-2 272 29-Dec-2014 II-2 169 29-Dec-2014 II-2 195 29-Dec-2014 II-2 221 29-Dec-2014 II-2 247 29-Dec-2014 II-2 273 29-Dec-2014 Page 16 of 116 MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-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 II-2 274 29-Dec-2014 II-2 293 29-Dec-2014 III-2 11 29-Dec-2014 V-2 3 29-Dec-2014 II-2 275 29-Dec-2014 II-2 294 29-Dec-2014 III-2 12 29-Dec-2014 V-2 4 29-Dec-2014 II-2 276 29-Dec-2014 II-2 295 29-Dec-2014 III-2 13 29-Dec-2014 V-2 5 29-Dec-2014 II-2 277 29-Dec-2014 II-2 296 29-Dec-2014 III-2 14 29-Dec-2014 V-2 6 29-Dec-2014 II-2 278 29-Dec-2014 II-2 297 29-Dec-2014 III-2 15 29-Dec-2014 V-2 7 29-Dec-2014 II-2 279 29-Dec-2014 II-2 298 29-Dec-2014 III-2 16 29-Dec-2014 V-2 8 29-Dec-2014 II-2 280 29-Dec-2014 II-2 299 29-Dec-2014 III-2 17 29-Dec-2014 V-2 9 29-Dec-2014 II-2 281 29-Dec-2014 II-2 300 29-Dec-2014 III-2 18 29-Dec-2014 VI 1 29-Dec-2014 II-2 282 29-Dec-2014 III-1 1 29-Dec-2014 III-2 19 29-Dec-2014 VI 2 29-Dec-2014 II-2 283 29-Dec-2014 III-2 1 29-Dec-2014 III-2 20 29-Dec-2014 VI 3 29-Dec-2014 II-2 284 29-Dec-2014 III-2 2 29-Dec-2014 IV-1 1 29-Dec-2014 VI 4 29-Dec-2014 II-2 285 29-Dec-2014 III-2 3 29-Dec-2014 IV-2 1 29-Dec-2014 VI 5 29-Dec-2014 II-2 286 29-Dec-2014 III-2 4 29-Dec-2014 IV-2 2 29-Dec-2014 VI 6 29-Dec-2014 II-2 287 29-Dec-2014 III-2 5 29-Dec-2014 IV-2 3 29-Dec-2014 II-2 288 29-Dec-2014 III-2 6 29-Dec-2014 IV-2 4 29-Dec-2014 II-2 289 29-Dec-2014 III-2 7 29-Dec-2014 V-1 1 29-Dec-2014 II-2 290 29-Dec-2014 III-2 8 29-Dec-2014 V-1 2 29-Dec-2014 II-2 291 29-Dec-2014 III-2 9 29-Dec-2014 V-2 1 29-Dec-2014 II-2 292 29-Dec-2014 III-2 10 29-Dec-2014 V-2 2 29-Dec-2014 Page 17 of 116 SDM A319/A320 MAINTENANCE PROGRAM LIST OF EFFECTIVE PAGES AND RECORDING PROCEDURE MP-REF: SDM.A320.IRISH SECTION: II REV: 07 DATE: 29-Dec-2014 THIS PAGE INTENTIONALLY LEFT BLANK Page 18 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-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 Irish Aviation Authorities 3 PDF version “Rossiya airlines” OJSC internal server SDM Engineering Department Page 19 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS B. MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-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 20 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-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 18-Jan-2008 IRISH approved. EI-DXY; EI-DZR added in TR001/08 from 05-May-2008 01 SDM.A320.MS 15-Jul-2008 IRISH approved. EI-DXY, EI-DZR 02 SDM.A320.MS 25-Feb-2009 IRISH approved. EI-DXY, EI-DZR 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.IRISH 01-Dec-2012 MPD Rev 36. The first maintenance program developed special for IRISH fleet 01 SDM.A320.IRISH 01-Aug-2012 MPD Rev 38 implemented 02 SDM.A320.IRISH 02-Nov-2012 MPD 38. Publishing system together with layout was changed. Incorporation new aircrafts MSN 2497 and MSN 2930 to the maintenance program 03 SDM.A320.IRISH 20-Nov-2012 MPD 38. Incorporation of new aircraft MSN 2964 to the maintenance program and minor changes 04 SDM.A320.IRISH 26-Dec-2012 MPD 38. Incorporation of new aircrafts MSN 2465 and 3044 to the maintenance program and minor changes 05 SDM.A320.IRISH 04-Feb-2013 MPD 38. Incorporation of new aircrafts MSN 2879 and 2913 to the maintenance program. Aircraft applicabilities review and reliability control board changes 06 SDM.A320.IRISH 01-Jun-2014 MPD 39 Incorporated and applicability review 07 SDM.A320.IRISH 29-Dec-2014 MPD 39. Removal of aircrafts MSN 0427 and 0525. Aircraft applicability’s review and minor changes Page 21 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS C. MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 22 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS D. MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 REVISION HIGHLIGHTS The following tables represent tasks changes highlights. 1. NEW TASKS Task Number Change 272400-05-1 NEW TASK ADDED DUE TO GREASE 04-037 IS USED 274000-07-1 NEW TASK ADDED DUE TO GREASE 04-037 IS USED 251000-01-1-SDM NEW TASKS AS PART OF CABIN CONDITION IMPROVEMENT PROGRAM 252340-01-1-SDM NEW TASKS AS PART OF CABIN CONDITION IMPROVEMENT PROGRAM 252341-01-1-SDM NEW TASKS AS PART OF CABIN CONDITION IMPROVEMENT PROGRAM 252343-01-1-SDM NEW TASKS AS PART OF CABIN CONDITION IMPROVEMENT PROGRAM 252400-01-1-SDM NEW TASKS AS PART OF CABIN CONDITION IMPROVEMENT PROGRAM 252600-01-1-SDM NEW TASKS AS PART OF CABIN CONDITION IMPROVEMENT PROGRAM 252841-01-1-SDM NEW TASKS AS PART OF CABIN CONDITION IMPROVEMENT PROGRAM 253100-01-1-SDM NEW TASKS AS PART OF CABIN CONDITION IMPROVEMENT PROGRAM 253300-01-1-SDM NEW TASKS AS PART OF CABIN CONDITION IMPROVEMENT PROGRAM 252100-01-1-SDM NEW TASKS AS PART OF CABIN CONDITION IMPROVEMENT PROGRAM 252100-02-1-SDM NEW TASKS AS PART OF CABIN CONDITION IMPROVEMENT PROGRAM 252100-03-1-SDM NEW TASKS AS PART OF CABIN CONDITION IMPROVEMENT PROGRAM 252100-04-1-SDM NEW TASKS AS PART OF CABIN CONDITION IMPROVEMENT PROGRAM 252142-01-1-SDM NEW TASKS AS PART OF CABIN CONDITION IMPROVEMENT PROGRAM 353000-07-1-SDM NEW TASK ADDED AS A RESULT OF RELIABILITY MEETING 03.07.2014 TCHG.35300007 Page 23 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 2. DELETED TASKS Task Number Change 200001-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 200231-03-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 200241-04-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 200251-03-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 200261-03-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 212643-06-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 212653-01-1 TASK DELETED DUE TO N/A MSN0427 AND MSN0525. PN VFT300B00 INSTALLED 215000-03-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 215000-04-2 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 215200-02-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 216000-03-1 TASK DELETED DUE TO COVERED BY TASK 216000-03-2 SAME PROCEDURE AND SAME INTERVAL 237300-02-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 237300-08-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 237300-09-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 240000-03-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 242400-01-3 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 242600-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 242800-01-3 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 256600-02-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS Page 24 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS Task Number Change 262300-05-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 262300-06-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 262300-07-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 262300-08-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 262300-09-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 271400-02-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 272400-03-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 274000-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 275100-06-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 275100-07-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 275449-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 275449-02-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 275449-04-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 275449-05-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 281100-04-2 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 292000-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 292000-02-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 292000-06-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 292000-12-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 292251-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 321100-03-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 321156-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Page 25 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS Task Number Change 323105-03-1 DELETED DUE TO AD2014-0221 WHICH CANCELS THE REQUIREMENT 323112-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 324500-03-2 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 335100-02-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 335100-04-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 361100-05-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 361100-07-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 361143-02-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 361251-01-2 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 383200-02-1 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 494251-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 494251-02-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Page 26 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS Task Number Change 494251-03-1 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 499000-A1-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 499100-02-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 499141-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 521104-02-2 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 521304-02-2 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 522100-02-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 522100-07-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 523106-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 523116-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 523130-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 523131-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 525111-07-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 528101-02-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 531119-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 531124-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 531129-02-2 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 531135-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 531157-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 531162-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Page 27 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS Task Number Change 531166-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 531170-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 531170-02-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 531189-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 531190-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 531260-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 532120-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 532140-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 532140-02-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 532145-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 532155-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 532170-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 532180-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 533140-01-8 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 533142-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 533174-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 533176-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 534121-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 535119-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 552007-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 552007-01-3 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 571173-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Page 28 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS Task Number Change 571192-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 572110-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 572140-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 572161-01-10 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 574145-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 575200-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 575221-02-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 575303-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 575303-02-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 575309-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 575309-02-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 575312-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 575312-02-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 723200-C2-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 725000-C1-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 725100-C1-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 731111-C1-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 781112-C1-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 781112-C3-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 783100-C1-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 792000-C1-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 792000-C2-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Page 29 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS Task Number Change 792000-C3-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 792000-C4-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 792000-C5-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 792000-C6-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS ZL-151-02-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS ZL-315-01-3 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS ZL-572-01-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 3. REVISED APPLICABILITIES Task Number Change 212100-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 212600-06-1 IN APPLICABILITY 0525 REMOVED DUE TO A/C REMOVED FROM OMP 212643-07-1 IN APPLICABILITY 0427 REMOVED DUE TO A/C REMOVED FROM OMP 212643-09-1 IN APPLICABILITY 0427 REMOVED DUE TO A/C REMOVED FROM OMP 212643-10-1 IN APPLICABILITY 0427 REMOVED DUE TO A/C REMOVED FROM OMP 212652-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 215000-03-2 IN APPLICABILITY 0427 REMOVED DUE TO A/C REMOVED FROM OMP 215141-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 215200-08-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 216000-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 237300-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP Page 30 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Task Number Change 237600-01-1-SDM IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 237600-02-1-SDM IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 237600-03-1-SDM IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 242100-03-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 244100-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 253000-02-1 IN APPLICABILITY 0427 REMOVED DUE TO A/C REMOVED FROM OMP 254000-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 254000-03-1 IN APPLICABILITY 0525 REMOVED DUE TO A/C REMOVED FROM OMP 254000-04-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 256600-01-1 IN APPLICABILITY 0427 REMOVED DUE TO A/C REMOVED FROM OMP 257100-01-1 IN APPLICABILITY 1753, 2964, 2465 REMOVED DUE TO SB 25-1557 EMBODIED 257100-02-1 IN APPLICABILITY 1753, 2465 REMOVED DUE TO SB 53-1215 EMBODIED 261600-04-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 262300-02-3 IN APPLICABILITY 0525 REMOVED DUE TO A/C REMOVED FROM OMP 262300-03-3 IN APPLICABILITY 0525 REMOVED DUE TO A/C REMOVED FROM OMP 262300-04-3 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 262341-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 262341-02-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 262441-02-1 IN APPLICABILITY "2930 2964 3044 2879 2913" REMOVED AND "ALL" ADDED 262441-04-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 262441-05-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 262541-04-1 IN APPLICABILITY 0525 REMOVED DUE TO A/C REMOVED FROM OMP Page 31 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Task Number Change 271400-02-2 IN APPLICABILITY 0525 REMOVED DUE TO A/C REMOVED FROM OMP 281800-10-1 IN APPLICABILITY MSN 2930, 2964, 3044, 2879, 2465, 1753, 2913 ADDED DUE TO SB 28-1188 EMBODIED 282541-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 316000-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 316000-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 316322-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 316322-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 323000-17-1 IN APPLICABILITY 1753, 2465 ADDED DUE TO SB 32-1346 EMBODIED 323100-07-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 323105-02-1 IN APPLICABILITY MSN 0427, 0525, 2497, 2930, 2964 REMOVED DUE TO SB 32-1407 EMB 323300-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 324200-03-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 324300-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 324311-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 324314-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 324500-04-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 336000-01-1-SDM IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 336000-02-1-SDM IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 336000-03-1-SDM IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 336000-04-1-SDM IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 336000-05-1-SDM IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP Page 32 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Task Number Change 341300-10-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 342100-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 342100-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 344800-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 361143-01-1 IN APPLICABILITY 0427 REMOVED DUE TO A/C REMOVED FROM OMP 361200-02-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 361251-01-1 IN APPLICABILITY 0525 REMOVED DUE TO A/C REMOVED FROM OMP 381000-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 381000-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 384142-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 491200-A1-1 IN APPLICABILITY 0525 REMOVED DUE TO A/C REMOVED FROM OMP 491200-A2-1 IN APPLICABILITY 0525 REMOVED DUE TO A/C REMOVED FROM OMP 491300-A1-1 IN APPLICABILITY 0525 REMOVED DUE TO A/C REMOVED FROM OMP 491600-A1-1 IN APPLICABILITY 0525 REMOVED DUE TO A/C REMOVED FROM OMP 493400-A1-1 IN APPLICABILITY 0525 REMOVED DUE TO A/C REMOVED FROM OMP 494000-A1-1 IN APPLICABILITY 0525 REMOVED DUE TO A/C REMOVED FROM OMP 494251-A2-1 IN APPLICABILITY 0525 REMOVED DUE TO A/C REMOVED FROM OMP 498000-A4-1 IN APPLICABILITY 0525 REMOVED DUE TO A/C REMOVED FROM OMP 499000-A2-1 IN APPLICABILITY 0525 REMOVED DUE TO A/C REMOVED FROM OMP 522100-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 522100-08-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 522102-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP Page 33 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Task Number Change 522103-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 523111-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 523113-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 523115-01-3 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 523118-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 523119-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 523119-02-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 523300-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 523301-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 523303-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 523305-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 525111-06-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 531103-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 531105-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 531105-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 531108-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 531130-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 531277-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 531900-01-1 IN APPLICABILITY 0427 REMOVED DUE TO A/C REMOVED FROM OMP 531900-02-1 IN APPLICABILITY 0427 REMOVED DUE TO A/C REMOVED FROM OMP 532164-01-5 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 532165-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP Page 34 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Task Number Change 532186-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 533101-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 533103-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 533105-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 533110-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 533128-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 533129-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 533130-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 533131-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 533133-01-5 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 533138-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 533138-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 533139-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 533143-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 533151-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 533152-01-7 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 533180-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 533181-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 533182-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 533185-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534103-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534106-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP Page 35 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Task Number Change 534108-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534111-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534112-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534118-01-4 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534124-01-3 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534125-01-3 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534126-01-3 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534127-01-3 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534128-01-6 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534129-01-3 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534130-01-3 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534131-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534132-01-4 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534137-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534139-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534140-01-8 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534141-01-5 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534142-01-9 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534143-01-1 IN APPLICABILITY 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534143-01-3 IN APPLICABILITY 0427 REMOVED DUE TO A/C REMOVED FROM OMP 534146-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534147-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP Page 36 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Task Number Change 534148-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534150-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534152-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534153-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534154-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534155-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534156-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534156-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534157-01-4 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534159-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534160-01-3 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534160-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534163-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534164-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534167-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534169-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534171-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534172-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 534195-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 535113-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 535117-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 535162-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP Page 37 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Task Number Change 535900-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 545101-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 545102-01-10 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 545107-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 545114-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 545115-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 545115-02-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 545117-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 545120-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 545123-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 545126-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 545131-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 545134-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 545156-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 545161-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 545162-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 545162-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 545172-01-1 IN APPLICABILITY MSN 2465, 2930 DELETED DUE TO SB 54-1019 EMBODIED 545172-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 552006-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 552007-01-2 IN APPLICABILITY 0525 REMOVED DUE TO A/C REMOVED FROM OMP 552007-01-4 IN APPLICABILITY 0525 REMOVED DUE TO A/C REMOVED FROM OMP Page 38 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Task Number Change 553006-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 571106-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 571109-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 571120-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 571134-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 571135-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 571136-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 571170-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 571175-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 571181-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 571182-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 571183-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 571185-01-8 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 571189-01-8 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572004-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572007-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572008-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572009-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572010-01-4 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572011-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572012-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572014-01-3 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP Page 39 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Task Number Change 572019-01-4 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572020-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572024-01-4 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572026-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572027-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572028-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572029-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572032-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572033-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572036-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572037-02-4 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572038-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572040-03-4 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572041-02-4 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572042-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572044-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572047-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572050-01-4 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572050-02-4 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572052-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572053-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572054-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP Page 40 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Task Number Change 572101-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572106-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572108-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572109-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572111-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572112-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572114-01-4 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572115-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572116-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572120-01-3 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572123-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572124-01-3 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572126-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572127-01-1 IN APPLICABILITY MSN 2930, 2964 REMOVED DUE TO TERMINATING PART(OPTION 2) OF ISB 57-1155 PERFORMED 572127-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572129-01-4 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572130-01-7 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572134-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572137-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572139-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572140-01-2 IN APPLICABILITY 0427 REMOVED DUE TO A/C REMOVED FROM OMP Page 41 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Task Number Change 572140-02-4 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572142-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572143-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572144-01-5 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572148-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572149-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572150-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572151-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572153-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572155-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572157-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572158-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572160-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572161-01-11 IN APPLICABILITY 0427 REMOVED DUE TO A/C REMOVED FROM OMP 572164-02-6 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572601-01-3 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572601-02-3 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572604-01-4 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 572654-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 573101-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 574101-01-3 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 574102-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP Page 42 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Task Number Change 574106-01-3 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 574202-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 574302-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 574402-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 574502-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 574602-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 575101-02-3 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 575107-02-3 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 575130-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 575151-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 575155-01-4 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 575158-01-5 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 575159-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 575160-01-5 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 575163-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 575166-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 575171-01-3 IN APPLICABILITY 0525 REMOVED DUE TO A/C REMOVED FROM OMP 575305-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 575305-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 575313-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 575313-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 575315-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP Page 43 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Task Number Change 575316-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 575316-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 724000-C4-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO SB 72-0576 EMBODIED ZL-125-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP ZL-131-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP ZL-161-03-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP ZL-163-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP ZL-171-01-2 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP ZL-197-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP ZL-315-01-2 IN APPLICABILITY 0525 REMOVED DUE TO A/C REMOVED FROM OMP ZL-826-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP ZL-826-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP ZL-827-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP ZL-827-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP ZL-833-01-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP ZL-833-02-1 IN APPLICABILITY 0427, 0525 REMOVED DUE TO A/C REMOVED FROM OMP 4. REVISED INTERVALS Task Number Change 212653-02-1 INTERVAL CHANGED FROM "7500 FH OR 24 MO NOTE" TO "18000 FH OR 120 MO" TO RETURN TO MPD REQUIREMENTS 336000-02-1-SDM 100% INTERVAL CHANGED FROM: "6000 FH and 18 MO", TO: "7500 FH and 24 MO" Page 44 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Task Number Change 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" 336000-05-1-SDM 100% INTERVAL CHANGED FROM: "12000 FH and 36 MO", TO: "10 YE" 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 212653-02-1 IN DESCRIPTION REMOVED "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" 227100-01-1-SDM IN REFERENCES "JIC A320-22-70-00" ADDED 237135-01-1 IN DESCRIPTION "NOTE: CVR P/N 93A100-80, VENDOR: FAIRCHILD CVR P/N AP71232101, VENDOR: TEAM VENDOR DUKANE ULB: P/N ELP-362D, VENDOR BENTHOS CVR P/N 980-6022001, VENDOR: HONEYWELL ULB: P/N DK120, VENDOR DUKANE" ADDED 237135-02-1 IN DESCRIPTION: "NOTE: MSN 0427: CVR P/N 93A100-80, VENDOR: FAIRCHILD MSN 0525: CVR P/N AP71232101, VENDOR: TEAM ULB: P/N ELP-362D, VENDOR BENTHOS (MSN 0525)MSN 1654, 1679, 1753, 2465, 2497, 2879, 2913, 2930, 2964, 3044: CVR P/N 980-6022-001, VENDOR: HONEYWELL ULB: P/N DK120, VENDOR DUKANE " REMOVED AND "NOTE: CVR P/N 980-6022-001 VENDOR: HONEYWELL INTERNATIONAL INC ULB: P/N DK120, VENDOR DUKANE" ADDED 237135-02-1 IN REFERENCES "CMM 23-70-03" ADDED 254000-01-1 IN SOURCE LUR ADDED. 256241-02-1 IN DESCRIPTION "MSN 0427: ESCAPE SLIDES P/N D30664-309, 30665-309, D30664-309, D30665-309, VENDOR: AIR CRUISERS MSN 0525: ESCAPE SLIDES P/N D31516-121, D31517121, VENDOR: AIR CRUISERS MSN 1679, 1654, 1753: ESCAPE SLIDES P/N D31516-113 & Page 45 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS Task Number MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Change D31517-113 MSN 2465, 2497, 2879, 2913 : ESCAPE SLIDES PN D31516-417, D31517-417, VENDOR : AIR CRUISERS COMPANY MSN 2930, 2964, 3044 : ESCAPE SLIDES PN D30664-309, D30665-309, VENDOR : AIR CRUISERS COMPANY" REMOVED AND " ESCAPE SLIDES PN D31516-113, D31517-113, D31516-417, D31517-417, PN D30664-309, D30665-309, VENDOR : AIR CRUISERS COMPANY" 256242-01-1 IN DESCRIPTION " MSN 0427, 0525: OFFWING SLIDES P/N D31865-209, D31865-210 MSN 1679, 1654, 1753, 2465, 2497, 2879, 2913, 2930, 2964, 3044: OFFSWING SLIDE P/N D31865-111 & D31865-112 VENDOR : AIR CRUISERS" REMOVED AND " OFFWING SLIDES P/N D31865-209, D31865-210, D31865-111, D31865-112 VENDOR : AIR CRUISERS" ADDED 256242-02-1 IN DESCRIPTION "MSN 0427, 0525: OFFWING SLIDES P/N D31865-209, D31865-210 MSN 1679, 1654, 1753, 2465, 2497, 2879, 2913, 2930: P/N D31865-111 AND D31865-112 VENDOR: AIR CRUISERS" REMOVED AND "P/N D31865-111 AND D31865-112 VENDOR: AIR CRUISERS" ADDED 256532-01-1 IN DESCRIPTION "NOTE: MSN 0427, 0525, 1679, 1654, 1753, 2930: P/N 1151324-1MXXX, VENDOR: HONEYWELL MSN 0427: P/N 607690-5, VENDOR: HONEYWELL" REMOVED AND "NOTE: P/N 1151324-1MXXX, 607690-5, VENDOR: HONEYWELL" ADDED 256551-01-1 IN DESCRIPTION "NOTE:MSN 0427, 0525, 1654, 1679, 2465, 2497, 2879, 2913, 2930, 2964, 3044:P/N A12SA, VENDOR: FEDERAL SIGNAL" REMOVED AND "NOTE: P/N 965-0976-003-206206, VENDOR: HONEYWELL ;P/N 965-0676-020, VENDOR: SUNDSTRAND" REMOVED 256535-02-1 IN DESCRIPTION MSN 1654, 1679 P/N 01N65900: VENDOR: ELTA MSN 2497 P/N S1819502-02 VENDOR: THALES AVIONICS MSN 2930 P/N 1152682-1 VENDOR: HONEYWELL ASCA INC MSN 0427, 0525, 2879, 2913: PN S1821502-02 VENDOR: THALES AVIONICS" REMOVED AND " P/N 01N65900: VENDOR: ELTA P/N S1819502-02 VENDOR: THALES AVIONICS P/N 1152682-1 VENDOR: HONEYWELL ASCA INC P/N S1821502-02 VENDOR: THALES AVIONICS" ADDED 256652-01-1 IN DESCRIPTION "MSN 0525: P/N S-51950-6300-119101, VENDOR: SWITLIK MSN 0427: P/N 63600-101, VENDOR: AIR CRUISERS MSN 1679, 1654, 1753 P/N 63600-101 & 63600-501, VENDOR: AIR CRUISERS MSN 2465, 2497 PN : 63600-501 (CREW) VENDOR : AIR CRUISERS MSN 2930, 2964, 3044 PN: P0640-101W (INFANT) VENDOR : EASTERN AERO MARINE PN: P0723E105PW (PASSENGER) VENDOR : EASTERN AERO MARINE PN : P0723E105PWC Page 46 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS Task Number MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Change (CREW) VENDOR : EASTERN AERO MARINE MSN 2879, 2913 PN S10002-1300 (INFANT), S41150-7400 (CREW), S51150-6300 (PASSENGER) VENDOR : SWITLIK PARACHUTE, INC." REMOVED AND "PN: 63600-101 & 63600-501, VENDOR: AIR CRUISERS PN: 63600-501 (CREW) VENDOR : AIR CRUISERS PN: P0640-101W (INFANT) VENDOR : EASTERN AERO MARINE PN: P0723E105PW (PASSENGER) VENDOR : EASTERN AERO MARINE PN : P0723E105PWC (CREW) VENDOR : EASTERN AERO MARINE PN S10002-1300 (INFANT), S41150-7400 (CREW), S51150-6300 (PASSENGER) VENDOR : SWITLIK PARACHUTE, INC. " ADDED 262141-02-1 IN DESCRIPTION "MSN 0427, 0525, 2497: BOTTLE P/N 472088-1, VENDOR: KIDDE INC MSN 1679, 1654, 1753, 2879, 2913, 2930, 2964, 3044: BOTTLE P/N 34100005-1, VENDOR: PACIFIC" REMOVED AND "BOTTLE P/N 472088-1, VENDOR: KIDDE INC BOTTLE P/N 34100005-1, VENDOR: PACIFIC " ADDED. 262142-01-1 IN DESCRIPTION "MSN 0427, 0525, 2465, 2497: BOTTLE P/N 472088-1, VENDOR: KIDDE INC CARTRIDGE; P/N 446158, VENDOR: KIDDE MSN 1679, 1654, 1753, 2879, 2913, 2930, 2964, 3044: BOTTLE P/N 34100005-1, VENDOR: PACIFIC CARTRIDGE P/N 30903886, VENDOR: PACIFIC" REMOVED AND " BOTTLE P/N 472088-1, VENDOR: KIDDE INC CARTRIDGE; P/N 446158, VENDOR: KIDDE BOTTLE P/N 34100005-1, VENDOR: PACIFIC CARTRIDGE P/N 30903886, VENDOR: PACIFIC " ADDED 262241-01-1 IN DESCRIPTION "MSN 0427: BOTTLE P/N 33600005-1, VENDOR: PACIFIC SCIENTIFIC MSN 0525, 1679, 1654, 1753, 2465, 2497, 2879, 2913, 2930, 2964, 3044: BOTTLE P/N 33600005-3, VENDOR: PACIFIC SCIENTIFIC" REMOVED AND "BOTTLE P/N 33600005-3, VENDOR: PACIFIC SCIENTIFIC" ADDED 262242-01-1 IN DESCRIPTION "MSN 0427: BOTTLE P/N 33600005-1, VENDOR: PACIFIC SCIENTIFIC ARTRIDGE P/N 30903827, VENDOR: PACIFIC MSN 0525, 1679, 1654, 1753, 2465, 2497, 2879, 2913, 2930, 2964, 3044: BOTTLE P/N 33600005-3, VENDOR: PACIFIC CARTRIDGE P/N 30903827, VENDOR: PACIFIC" REMOVED AND " BOTTLE P/N 33600005-3, VENDOR: PACIFIC CARTRIDGE P/N 30903827, VENDOR: PACIFIC" ADDED 262441-02-1 DESCRIPTION "MSN 0525: P/N 466040, 466090, VENDOR: KIDDE P/N 74-20, 74-00, 74-21, 76-00, VENDOR: TOTAL WALTER FEURSCHUTZ GMBH MOBILER BRANDSCHUTZ P/N H1-10-AIR, VENDOR: GENERAL INCENDIE P/N BA51015, VENDOR: FIRE FIGHTING ENTERPRISE MSN Page 47 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS Task Number MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Change 0427: P/N 9821657 P/N 898052, VENDOR: KIDDE P/N H1-10-AIR, VENDOR: GENERAL INCENDIE MSN 1654 1679 1753: P/N 74-20, VENDOR: TOTAL WALTER FEURSCHUTZ GMBH MOBILER BRANDSCHUTZ P/N H1-10AIR, VENDOR: GENERAL INCENDIE MSN 2465, 2497 PN : 1708337B4 VENDOR: MAIP PN 892480 VENDOR : KIDDE BELLEVILLE PN 74-20 VENDOR : TOTAL WALTHER MSN 2930, 2964, 3044 PN 74-20 VENDOR : TOTAL FEUERSCHUTZ MSN 2879 2913 P/N 898052, 892480 VENDOR: KIDDE AEROSPACE " REMOVED 262541-02-1 IN DESCRIPTION "NOTE: MSN 0427: P/N A825100-3, VENDOR: KIDDE MSN 0525,1654 1679 1753: P/N BA21758, VENDOR: FIRE FIGHTING ENTERPRISE MSN 2465, 2497, 2879, 2913, 2930, 2964, 3044: PN BA24320A1 VENDOR: FIRE FIGHTING ENTERPRISES LTD" REMOVED AND "NOTE: PN A825100-3, VENDOR: KIDDE PN BA21758, VENDOR: FIRE FIGHTING ENTERPRISE PN BA24320A1 VENDOR: FIRE FIGHTING ENTERPRISES LTD" ADDED 313300-01-1-SDM IN DESCRIPTION "EU OPS 1" REMOVED AND "COMMISSION REGULATION (EU) No 965/2012" ADDED 325101-01-1-SDM TASK REFERENCE CHANGED FROM "A320-32-51-01" TO "A320-32-51-02" 336000-01-1-SDM TASK TITLE CHANGED FROM: "GENERAL VISUAL INSPECTION AND SERVICING", TO: "SYSTEM CHARGING" 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 IN REFERENCE(S): "STC ST02292AT" ADDED AND "STC 10042956" REMOVED 336000-01-1-SDM TASK CODE CHANGED FROM: "GVI", TO: "SVC" 336000-02-1-SDM IN REFERENCE(S): "STC ST02292AT" ADDED AND "STC 10042956" REMOVED 336000-02-1-SDM IN TASK TITLE: "6000 FH OR 18MO " DELETED 336000-03-1-SDM IN REFERENCE(S): "STC ST02292AT" ADDED AND "STC 10042956" REMOVED 336000-03-1-SDM IN TASK TITLE: "6000 FH OR 18MO " DELETED 336000-04-1-SDM IN REFERENCE(S): "STC ST02292AT" ADDED AND "STC 10042956" REMOVED Page 48 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Task Number Change 336000-04-1-SDM TASK TITLE CHANGED FROM: "12000 FH OR 36 MO INSPECTION AND FUNCTIONAL CHECK", TO: "GENERAL VISUAL INSPECTION". 336000-04-1-SDM TASK CODE CHANGED FROM: "FNC", TO: "GVI" 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" 336000-05-1-SDM IN TASK TITLE: "10 YEAR " DELETED 336000-05-1-SDM IN REFERENCE(S): "STC ST02292AT" ADDED AND "STC 10042956" REMOVED 342200-01-1 IN DESCRIPTION "NOTE: THIS NOTE FOR SDM BASE ONLY: AMTOSS REF 342200-710-001-A01 IS NOT REQUIRED TO BE PERFORMED. ONLY -A" ADDED 344800-01-1 IN DESCRIPTION "MSN 0427, 0525:P/N 965-0676-020, VENDOR: SUNDSTRAND MSN 1679, 1654, 1753: P/N 965-0976-003-206-206, VENDOR: HONEYWELL" REMOVED AND "NOTE: P/N 9650976-003-206-206, VENDOR: HONEYWELL ;P/N 965-0676-020, VENDOR: SUNDSTRAND" ADDED 351141-01-1 IN DESCRIPTION "NOTE: MSN 0427, 1679, 1654, 1753, 2879, 2913: P/N 89794077, VENDOR: AVOX SYSTEM MSN 0525: P/N 89794050, VENDOR: AVOX SYSTEM MSN 2497, 2930: PN 891511-14 VENDOR INTERTECHNIQUE SA" REMOVED AND "NOTE: PN 891511-14 VENDOR INTERTECHNIQUE SA" ADDED. 353000-02-1 IN DESCRIPTION "NOTE: MSN 0427, 2879, 2913: P/N 5500-C1A-BF23A, VENDOR: SCOTT AVIATION MSN 0525: P/N 9800-2D1A-F23AM, VENDOR : SCOTT AVIATION P/N 9700-C1ABF23A, VENDOR : SCOTT AVIATION MSN 1679, 1654, 1753, 2497, 2930: P/N 9700C1ABF23A, VENDOR: SCOTT AVIATION" AND "NOTE: P/N 5500-C1A-BF23A, VENDOR: SCOTT AVIATION P/N 9800-2D1A-F23AM, VENDOR : SCOTT AVIATION P/N 9700-C1A-BF23A, VENDOR : SCOTT AVIATION P/N 9700C1ABF23A, VENDOR: SCOTT AVIATION" 353000-06-1 IN DESCRIPTION "NOTE: MSN 0427: P/N 802300-14, VENDOR: SCOTT AVIATION MSN 0525: P/N E28180, VENDOR: SCOTT AVIATION MSN 1679 1654: P/N 119003-01 & 119003, VENDOR: B/E AEROSPACE MSN 1753: P/N 119003, VENDOR: B/E AEROSPACE MSN 2494 P/N : MR10049N VENDOR : ESSEX PB & R CORP MSN 2879, 2913, 2930, 2964, 3044 P/N : 119003-11 VENDOR : B/E AEROSPACE INTERIOR SYSTEMS GROUP" REMOVED AND " NOTE: P/N Page 49 of 116 SDM A319/A320 MAINTENANCE PROGRAM RECORDS AND REVISION HIGHLIGHTS Task Number MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Change 119003-01 & 119003, VENDOR: B/E AEROSPACE P/N : MR10049N VENDOR : ESSEX PB & R CORP P/N : 119003-11 VENDOR : B/E AEROSPACE INTERIOR SYSTEMS GROUP" ADDED 531259-01-1 IN SOURCE: "EASA AD" ADDED 724000-C4-1 TASK DELETED DUE TO NO APPLICABLE AIRCRAFTS 753120-01-1-SDM IN DESCRIPTION " ONLY PN 3282970-4 AND PN 3282970-4" REMOVED AND " PN 3282970-4" ADDED 753120-01-1-SDM IN REFERENCES "752110-000-002" DELETED AND "753120-000-002 " ADDED ZL-253-50-1-SDM IN REFERENCES "JIC A320-53-41-00" ADDED ZL-253-51-1-SDM IN REFERENCES "JIC A320-53-41-01" ADDED ZL-253-53-1-SDM IN REFERENCES "JIC A320-53-41-02" ADDED ZL-253-54-1-SDM IN REFERENCES "JIC A320-53-41-03" ADDED 6. MOVED TASK Task Number Change 261600-05-1 TASK MOVED FROM SYSTEM TO TCI SECTION Page 50 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION I. MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-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 1 – Safe Life Airworthiness Limitation Items documents, Revision 02 from 13 May 2011 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 STC EASA.IM.A.S.00199 ICA232010006 REV E from 07-Feb-2011. Airworks CDSS installation Page 51 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Engine Shop Manuals (ESM) for CFM56–5B engine APU Honeywell 131-9(A) Engine Manual APU APIC APS 3200 Engine Shop Manual Inspection Service Bulletins (ISB) Vendor Service Bulletins (VSB) Service Information Letter (SIL) Alert Operators Transmission (AOT) Airworthiness Directives (AD) Page 52 of 116 MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-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 EI-ETN EI-ETO EI-ETP EI-EYL EI-EYM EI-EZC EI-EZD EI-EYR EI-EYS EI-FAJ Type/TCDS A319-111 EASA A.064 A319-111 EASA A.064 A319-111 EASA A.064 A319-111 EASA A.064 A319-111 EASA A.064 A319-112 EASA A.064 A319-112 EASA A.064 A320-214 EASA A.064 A320-214 EASA A.064 A320-214 EASA A.064 MSN IPC eff DOM Engine Type APU WV GROUP LOV 1654 301 08.01.2002 CFM56-5B5/P 131–9(A) 001 19-1A 60 000 FH or 48 000 FC 1679 302 05.02.2002 CFM56-5B5/P 131–9(A) 001 19-1A 60 000 FH or 48 000 FC 1753 303 28.05.2002 CFM56-5B5/P 131–9(A) 001 19-1A 60 000 FH or 48 000 FC 2465 109 27.04.2005 CFM56-5B5/P 131-9(A) 001 19-1A 60 000 FH or 48 000 FC 2497 110 02.06.2005 CFM56-5B5/P 131–9(A) 001 19-1A 60 000 FH or 48 000 FC 2879 401 11.09.2006 CFM56-5B6/P 131–9(A) 001 19-1A 60 000 FH or 48 000 FC 2913 402 16.10.2006 CFM56-5B6/P 131–9(A) 001 19-1A 60 000 FH or 48 000 FC 2930 501 29.09.2006 CFM56-5B4/P APS 3200 010 N/A 60 000 FH or 48 000 FC 2964 502 28.11.2006 CFM56-5B4/P APS 3200 010 N/A 60 000 FH or 48 000 FC 3044 503 06.02.2007 CFM56-5B4/P APS 3200 010 N/A 60 000 FH or 48 000 FC 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.” Page 53 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 programme. 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. Page 54 of 116 MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION Fleet limit of validity status As of 24.12.2014 50000 45000 40000 35000 FC 30000 25000 EI-ETP EI-ETN 20000 EI-EYL EI-EYM EI-EZD 15000 EI-EZC EI-ETO EI-EYS EI-FAJ EI-EYR 10000 5000 0 0 10000 20000 30000 40000 50000 60000 70000 FH Page 55 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION D. MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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. Page 56 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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) 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. Page 57 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 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. Page 58 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 reasons 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. Page 59 of 116 MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION 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: Aircraft identification, by registration marks. Justification of the need for such a variation. Proposed extension in the appropriate figure (flight hours, cycles, etc.) Current inspection status of the aircraft. List of aircraft deferred defects which are affected by the variation. 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. Page 60 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 is possible Page 61 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 recommend 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 reivisons 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. Page 62 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Delay in accomplishment may lead to higher repair costs but not to a loss of continued airworthiness. Note that if a safety concern exists, 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 out-ofservice 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 Sefvice 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. Page 63 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION E. MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 56-5B (including engine and accessories, engine mounts, cowlings and thrust reversers) the Auxiliary Power Units APU “Hamilton Sundstrand (APIC) APS 3200“ and “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 56-5B Engine Manual Chapter 5.” “Hamilton Sundstrand (APIC) APS 3200 APU Component Maintenance Manual“ “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. Page 64 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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: Page 65 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 dependant, 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 Page 66 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 nonsampling 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 a 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. Page 67 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 a 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. Page 68 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 Page 69 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 one-time 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 Page 70 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 prevents 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. Page 71 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION 1. 2. 3. 4. 5. 6. 7. 8. 9. MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 bulging 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. Page 72 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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. Page 73 of 116 MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION 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 minimise 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 A319-112 19–1A 001 A320-214 N/A 010 h) Structure Program Reporting System Operators shall report any findings to the manufacturer via the inspection reporting system on AirbusWorld/Maintenance and Engineering/Prepare Maintenance/Optimize maintenance management/Optimize maintenance program/Report my check records. The following rules apply to the reporting: Page 74 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION 1. 2. MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 Page 75 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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'. Page 76 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION 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 MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 Page 77 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 Page 78 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 The following item could be considered to be covered by the ZIP if access to the electrical power centre, 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 Page 79 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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: Page 80 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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. Page 81 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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, 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. Provide justification for items with potential for interval increase. Page 82 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 Provide engine indicating system fault detection Page 83 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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. Page 84 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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. Page 85 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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. Page 86 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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. Page 87 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION F. MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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. Page 88 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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. Page 89 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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. Page 90 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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) Page 91 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 Page 92 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 Page 93 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 Page 94 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 Page 95 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION 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 MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Page 96 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION 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 MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 Page 97 of 116 MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION 4. ATA CHAPTERS 12 Servicing 32 Landing Gear 56 Windows 20 Standard Practices - Airframe 33 Lights 57 Wings 21 Air Conditioning 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 and Control 25 Equipment & Furnishings 46 Information systems 74 Ignition 26 Fire Protection 49 Airborne Auxiliary Power 75 Air 27 Flight Controls 51 Standard practices and Structures 76 Engine Controls 28 Fuel 52 Doors 77 Engine Indicating 29 Hydraulic Power 53 Fuselage 78 Exhaust 30 Ice and Rain Protection 54 Nacelles/Pylons 79 Oil 31 Indicating/Recording System 55 Stabilizers 80 Starting Page 98 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 5. TASK CODES AND MAINTENANCE OPERATIONS TASK CODE DEFINITION BSI Borecsope 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. RST Restoration. Term covering all actions (on/off the aircraft) necessary to return the item to a specific standard. Page 99 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION TASK CODE MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 DEFINITION 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 Non destructive 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. Page 100 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION G. MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 ZONAL DIAGRAMS The main aircraft zones are defined in the following pages. Refer to AMM: 06-20-00 for the details MAJOR ZONES, A320 MAJOR ZONES A/C A319 Page 101 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 MAJOR SUB-ZONES A/C A320, Fuselage and Vertical Stabilizer MAJOR SUB-ZONES FUSELAGE AND VERTICAL STABILIZER, A/C: A319 Page 102 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MAJOR SUB-ZONES – WING AND NCALLE (LEFT AND RIGHT) A/C A320 MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 MAJOR SUB-ZONES, WING AND NACELLE (LEFT AND RIGHT), A/C A320 Page 103 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 ZONES - FUSELAGE AND VERTICAL STABILIZER, A/C A320 ZONES - FUSELAGE AND VERTICAL STABILIZER, A/C A319 Page 104 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 ZONES – DOORS, A/C A320 ZONES - DOORS A/C A319 Page 105 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION ZONES – WING AND HORIZONTAL STABILIZER (LEFT AND RIGHT SIDES), A/C: A320 MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 ZONES – WING AND HORIZONTAL STABILIZER (LEFT AND RIGHT SIDES), A/C: A319 Page 106 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 ZONES – LANDING GEAR, A/C: ALL ZONES – NACELLES – LEFT AND RIGHT SIDES, A/C: ALL Page 107 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION H. MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 MAINTENANCE PROGRAM LAYOUT The tasks are listed per increasing ATA chapter. Page 108 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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. Page 109 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 Page 110 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION Skill Code Definition MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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: Page 111 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 “ 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. Page 112 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 Page 113 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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). Page 114 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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 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 Page 115 of 116 SDM A319/A320 MAINTENANCE PROGRAM INTRODUCTION MP-REF: SDM.A320.IRISH SECTION: I REV: 07 DATE: 29-Dec-2014 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. Page 116 of 116 SDM A319/A320 MAINTENANCE PROGRAM SCHEDULED MAINTENANCE PROGRAM II. MP-REF: SDM.A320.IRISH SECTION: II REV: 07 DATE: 29-Dec-2014 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. Sub 1 - Page 1 of 1 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 000001-01-1-SDM ZONE 100 DESCRIPTION AIRCRAFT WEIGHING SKILL TASK CODE CODE REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 571 671 HIRF/LIGHTNING PROTECTION-WING FNC I: 4 YE SPECI EL FNC I: 36 MO MRB 081000-200-001 EU PART CAT (EU) NO 965/2012 JIC A320-08-00 249200-210-022 MRB SOURCE: L/HIRF 20-00-01-1 249200-210-023 CHECK BONDING MEASUREMENT OF CLAMPS WITH A LOOP TESTER FROM FUSELAGE TO RIB 9 200001-02-1 511 520 611 620 HIRF/LIGHTNING PROTECTION-WING REFERENCES AF WEIGHING OF THE AIRCRAFT D 200001-01-1 TPS EL FNC I: 72 MO 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 MEN TASKM. H. APPL 4 TBD ALL 1 1 0.50 0.50 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 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 Sub 2 - Page 1 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 200003-03-1 ZONE 324 DESCRIPTION HIRF/LIGHTNING PROTECTION-VERTICAL FIN SKILL TASK CODE CODE EL GVI REV: 07 DATE: 29-Dec-2014 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. H. APPL 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 Sub 2 - Page 2 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 200125-03-1 ZONE 125 126 DESCRIPTION LATERAL AVIONIC COMPARTMENT SKILL TASK CODE CODE EL GVI REV: 07 DATE: 29-Dec-2014 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. H. APPL 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 SOURCE: MRB 20.0.127/02 AF 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 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 AF 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 Sub 2 - Page 3 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 200127-07-1 ZONE 127 128 DESCRIPTION REAR AVIONIC COMPARTMENT SKILL TASK CODE CODE EL DET REV: 07 DATE: 29-Dec-2014 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. H. APPL 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 1 1 0.25 0.25 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 AF RST I: 72 MO MRB CLEANING OF EWIS INSTALLED IN THE BAY BEHIND FWD CARGO COMPARTMENT (ONLY IF CONTAMINATED) (EWIS) 249200-100-029 SOURCE: MRB 20.0.137/01 PREPARATION: ACT(S) NO.4 AND NO.6 REMOVED (IF INSTALLED); 200141-01-1 141 142 ACCESS PANELS: 131NW, 131PW, 132PW, 825 WING CENTRE BOX GENERAL VISUAL INSPECTION OF EXPOSED EWIS INSTALLED IN THE WING CENTRE BOX (EWIS) AF GVI I: 144 MO MRB 249200-210-026 SOURCE: MRB 20.0.141/01 ACCESS PANELS: 147AZ, 734, 148AZ, 744 Sub 2 - Page 4 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 200145-01-1 ZONE 145 146 DESCRIPTION ZONE UNDER CABIN FLOOR SKILL TASK CODE CODE AF RST REV: 07 DATE: 29-Dec-2014 INTERVALS I: 72 MO SOURCE MRB CLEANING OF EWIS INSTALLED IN THE ZONE UNDER CABIN FLOOR (ONLY IF CONTAMINATED) (EWIS) TPS REFERENCES 249200-100-015 MEN TASKM. H. APPL 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 1 1 0.20 0.20 ALL 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 AF RST I: 72 MO MRB CLEANING OF EWIS INSTALLED IN THE BULK CARGO COMPARTMENT (ONLY IF CONTAMINATED) (EWIS) 249200-100-030 SOURCE: MRB 20.0.161/01 PREPARATION: SIDEWALL PANELS FROM FR 59 TO FR 65; ACT(S) REMOVED (IF INSTALLED); 200171-01-1 171 172 ACCESS PANELS: 826 AFT CABIN UNDERFLOOR COMPARTMENT CLEANING OF EWIS INSTALLED IN THE AFT CABIN UNDERFLOOR COMPARTMENT (ONLY IF CONTAMINATED)(EWIS) EL RST I: 144 MO MRB 249200-100-001 SOURCE: MRB 20.0.171/01 PREPARATION: ACT NO.5 REMOVED (IF INSTALLED); CABIN FLOOR PANELS FROM FR 65 TO FR 70; ACCESS PANELS: 161DW, 171AL, 162DW, 172AR, 826 Sub 2 - Page 5 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 200191-01-1 ZONE 191 192 DESCRIPTION AIR CONDITIONING COMPARTMENT AND FAIRINGS SKILL TASK CODE CODE AF RST REV: 07 DATE: 29-Dec-2014 INTERVALS I: 72 MO SOURCE MRB 200211-01-1 211 212 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 REFERENCES 249200-100-027 MEN TASKM. H. APPL 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 1 1 0.25 0.25 ALL SOURCE: MRB 20.0.191/01 CLEANING OF EWIS INSTALLED IN THE AIR CONDITIONING COMPARTMENT AND FAIRINGS (ONLY IF CONTAMINATED) (EWIS) 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 TPS 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 AF GVI I: 144 MO MRB GENERAL VISUAL INSPECTION OF EWIS OF 49VU AND THE 120VU (EWIS) 249200-210-035 SOURCE: MRB 20.0.211/03 PREPARATION: 120VU; 49VU; 200221-01-1 221 222 ACCESS PANELS: 831, 841 FORWARD CABIN UTILITY AREA CLEANING OF EWIS INSTALLED IN THE FORWARD CABIN UTILITY AREA (ONLY IF CONTAMINATED) (EWIS) AF RST I: 144 MO MRB 249200-100-007 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; ACCESS PANELS: 831, 841 Sub 2 - Page 6 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 200223-01-1 ZONE 223 224 DESCRIPTION FORWARD CABIN OVERHEAD COMPARTMENT SKILL TASK CODE CODE AF RST REV: 07 DATE: 29-Dec-2014 INTERVALS I: 144 MO SOURCE MRB CLEANING OF EWIS INSTALLED IN THE FORWARD CABIN OVERHEAD COMPARTMENT (ONLY IF CONTAMINATED) (EWIS) TPS REFERENCES 249200-100-010 MEN TASKM. H. APPL 1 1 0.20 0.20 ALL 1 1 0.25 0.25 ALL 1 1 0.25 0.25 ALL 1 1 0.25 0.25 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 AF RST I: 144 MO MRB CLEANING OF EWIS INSTALLED IN THE FORWARD PASSENGER COMPARTMENT (ONLY IF CONTAMINATED) (EWIS) 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 ; D 200231-03-1 231 232 ACCESS PANELS: 831, 841 FORWARD PASSENGER COMPARTMENT 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 AF GVI I: 72 MO MRB 249200-210-036 SOURCE: MRB 20.0.231/03 PREPARATION: SEAT COVERS REMOVED IF NECESSARY; ACCESS PANELS: 831, 841 Sub 2 - Page 7 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 200233-01-1 ZONE 233 234 DESCRIPTION FORWARD PASSENGER COMPARTMENT OVERHEAD COMPARTMENT SKILL TASK CODE CODE AF RST REV: 07 DATE: 29-Dec-2014 INTERVALS I: 144 MO SOURCE MRB TPS REFERENCES 249200-100-005 MEN TASKM. H. APPL 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 20.0.233/01 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 EL RST I: 144 MO MRB CLEANING OF EWIS INSTALLED IN THE CENTER PASSENGER COMPARTMENT (ONLY IF CONTAMINATED) (EWIS) 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 ; 200241-03-1 241 242 ACCESS PANELS: 832, 842 CENTER PASSENGER COMPARTMENT GENERAL VISUAL INSPECTION OF G ROUTES INSTALLED AT FR 47 (EWIS) EL GVI I: 144 MO MRB 249200-210-031 SOURCE: MRB 20.0.241/03 PREPARATION: GALLEYS AND TOILETS REMOVED; LINING AT FR 47, RH ONLY; ACCESS PANELS: 832, 842 Sub 2 - Page 8 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 200241-04-1 ZONE 241 242 DESCRIPTION CENTER PASSENGER COMPARTMENT SKILL TASK CODE CODE EL GVI REV: 07 DATE: 29-Dec-2014 INTERVALS I: 72 MO SOURCE 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 TPS REFERENCES 249200-210-037 MEN TASKM. H. APPL 1 1 0.25 0.25 1 1 0.20 0.20 ALL 1 1 0.15 0.15 ALL 1 1 0.25 0.25 ALL 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 EL GVI I: 144 MO MRB GENERAL VISUAL INSPECTION OF G AND P ROUTES INSTALLED IN THE CENTER PASSENGER OVERHEAD COMPARTMENT (EWIS) 249200-210-041 SOURCE: MRB 20.0.243/03 PREPARATION: CEILING PANELS REMOVED; OVERHEAD STOWAGE BINS FROM FR 35 TO FR 47; 200251-02-1 251 252 ACCESS PANELS: 832, 842 AFT PASSENGER COMPARTMENT CLEANING OF EWIS INSTALLED IN THE AFT PASSENGER COMPARTMENT (ONLY IF CONTAMINATED) (EWIS) EL RST I: 144 MO MRB 249200-100-019 SOURCE: MRB 20.0.251/02 PREPARATION: GALLEYS AND TOILETS REMOVED; SIDEWALL PANELS FROM FR 47 TO FR 64 REMOVED; ACCESS PANELS: 832, 842 Sub 2 - Page 9 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 200251-03-1 ZONE 251 252 DESCRIPTION AFT PASSENGER COMPARTMENT SKILL TASK CODE CODE EL GVI REV: 07 DATE: 29-Dec-2014 INTERVALS I: 72 MO SOURCE 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 TPS REFERENCES 249200-210-039 MEN TASKM. H. APPL 1 1 0.25 0.25 1 1 0.20 0.20 ALL 1 1 0.15 0.15 ALL 1 1 0.25 0.25 ALL 1 1 0.33 0.33 ALL 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 EL GVI I: 144 MO MRB GENERAL VISUAL INSPECTION OF G AND P ROUTES INSTALLED IN THE AFT PASSENGER OVERHEAD COMPARTMENT (EWIS) 249200-210-042 SOURCE: MRB 20.0.253/02 PREPARATION: CEILING PANELS REMOVED; OVERHEAD STOWAGE BINS FROM FR 47 TO FR 64 REMOVED; 200261-01-1 261 262 ACCESS PANELS: 832, 842 AFT CABIN UTILITY AREA EL RST I: 144 MO MRB CLEANING OF EWIS INSTALLED IN THE AFT CABIN UTILITY AREA (ONLY IF CONTAMINATED) (EWIS) 249200-100-022 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 GENERAL VISUAL INSPECTION OF P ROUTES INSTALLED IN THE AFT CABIN UTILITY AREA (EWIS) EL GVI I: 144 MO MRB 249200-210-044 SOURCE: MRB 20.0.261/02 PREPARATION: GALLEYS AND TOILETS REMOVED; LINING AT FR 67; ACCESS PANELS: 832, 842 Sub 2 - Page 10 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 200261-03-1 ZONE 261 262 DESCRIPTION AFT CABIN UTILITY AREA SKILL TASK CODE CODE EL GVI REV: 07 DATE: 29-Dec-2014 INTERVALS I: 72 MO SOURCE 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 TPS REFERENCES 249200-210-040 MEN TASKM. H. APPL 1 1 0.25 0.25 1 1 0.20 0.20 ALL 1 1 0.15 0.15 ALL 1 1 0.20 0.20 ALL 1 1 0.10 0.10 ALL 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 EL RST I: 144 MO MRB CLEANING OF EWIS INSTALLED IN THE AFT CABIN OVERHEAD COMPARTMENT (ONLY IF CONTAMINATED) (EWIS) 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; 200263-02-1 263 264 ACCESS PANELS: 832, 842 AFT CABIN OVERHEAD COMPARTMENT EL GVI I: 144 MO MRB GENERAL VISUAL INSPECTION OF G AND P ROUTES INSTALLED IN THE AFT CABIN OVERHEAD COMPARTMENT (EWIS) 249200-210-043 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 GENERAL VISUAL INSPECTION OF G AND P ROUTES INSTALLED IN THE TAIL CONE AND APU ACCESSORY COMPARTMENT (EWIS) EL GVI I: 24 MO MRB 249200-210-025 SOURCE: MRB 20.0.315/01 ACCESS PANELS: 315AL, 316AR Sub 2 - Page 11 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 200413-01-1 200435-01-1 200453-01-1 200540-02-1 ZONE 413 414 423 424 435 436 445 446 453 454 463 464 540 640 DESCRIPTION UPPER FORWARD PYLON SKILL TASK CODE CODE EL DET REV: 07 DATE: 29-Dec-2014 INTERVALS I: 24 MO SOURCE MRB DETAILED INSPECTION OF EWIS INSTALLED IN THE UPPER FORWARD PYLON (EWIS) 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 DET I: 24 MO MRB EL DET I: 24 MO MRB 200550-01-1 550 650 249200-220-003 249200-220-004 SOURCE: MRB 20.0.453/01 EL GVI I: 144 MO MRB GENERAL VISUAL INSPECTION OF EXPOSED EWIS WITHIN THE WING FUEL TANK (EWIS) 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 VENT SURGE TANK 249200-220-001 SOURCE: MRB 20.0.435/01 DETAILED INSPECTION OF EWIS INSTALLED IN THE HOT SECTION (EWIS) ACCESS PANELS: 451AL, 452AR, 461AL, 462AR WING FUEL TANK REFERENCES SOURCE: MRB 20.0.413/01 DETAILED INSPECTION OF EWIS IN THE FAN AND ACCESSORY GEAR BOX (EWIS) ACCESS PANELS: 437AL, 438AR, 447AL, 448AR HOT SECTION TPS 249200-210-801 MEN TASKM. H. APPL 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 1 1 0.30 0.30 ALL 1 1 0.25 0.25 ALL 1 1 0.15 0.15 ALL SOURCE: MRB 20.0.540/02 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) GENERAL VISUAL INSPECTION OF EXPOSED EWIS WITHIN THE DRY BAY (OUTBOARD) (EWIS) AF GVI I: 144 MO MRB 249200-210-803 SOURCE: MRB 20.0.560/01 ACCESS PANELS: 560AB, 660AB Sub 2 - Page 12 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 200571-01-1 ZONE 571 671 DESCRIPTION MLG BAY SKILL TASK CODE CODE AF GVI REV: 07 DATE: 29-Dec-2014 INTERVALS I: 144 MO SOURCE MRB GENERAL VISUAL INSPECTION OF P ROUTE PUMP FEEDER (EWIS) 202800-01-1 R 212100-01-1 300 500 600 700 800 131 PREPARATION: PUMP WIRING FAIRINGS; ELECTRICAL BONDING 131 212141-01-1 ACCESS PANELS: 131MW, 131PW, 825 AIR DISTRIBUTION AND RECIRCULATION 200 ACCESS PANELS: 131SW, 825 AIR DISTRIBUTION AND RECIRCULATION 130 GENERAL VISUAL INSPECTION OF RISER DUCTS IN THE PASSENGER COMPARTMENT RECIRCULATION FILTER 210 220 230 240 250 260 ACCESS PANELS: 131PW, 132PW LAVATORY AND GALLEY VENTILATION GENERAL VISUAL INSPECTION OF LAVATORY AND GALLEY VENTILATION DUCTING IN ZONES 210 THROUGH 260 APPL 1 1 0.25 0.25 ALL I: 24 MO SIL 249200-210-024 SIL 20-020 1 1 1 1 1 0.20 0.20 0.20 0.20 0.20 ALL AF RST I: 24000 FH OR 160 MO MRB 9 LUR 212149-100-001 1 0.20 2930 2964 3044 I: 24000 FH OR 160 MO MRB 9 LUR 1 0.20 1654 1679 1753 2465 2497 2879 2913 I: 12 YE MRB 9 212000-210-001 1 0.50 ALL SOURCE: MRB 21.21.00/04 212141-920-002 1 0.05 ALL 1 1 1 1 1 1 0.25 0.25 0.25 0.25 0.25 0.25 ALL 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 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 AIR DISTRIBUTION AND RECIRCULATION TASKM. H. DET AF RST AF AF GVI DIS DISCARD FILTER ELEMENTS OF RECIRCULATION SYSTEM 212300-01-1 249200-210-804 MEN EL CLEAN COCKPIT AIR SUPPLY DUCTING GRID 212100-02-1 REFERENCES SOURCE: MRB 20.0.571/01 CLEAN COCKPIT AIR SUPPLY DUCTING GRID 212100-01-2 TPS AF GVI 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 212000-210-002 SOURCE: MRB 21.23.00/02 Sub 2 - Page 13 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 212300-02-1 ZONE 200 DESCRIPTION LAVATORY AND GALLEY VENTILATION SKILL TASK CODE CODE AF DIS DISCARD LAVATORY AIR EXTRACTION FILTER ELEMENT 212600-01-1 210 NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED. AVIONICS EQUIPMENT VENTILATION AF OPERATIONAL CHECK OF SYSTEM VIA MCDU 212600-02-1 212600-03-1 212600-04-1 212600-05-1 210 AVIONICS EQUIPMENT VENTILATION 210 OPERATIONAL CHECK OF OVERRIDE FUNCTION (BLOWER AND EXTRACT) AVIONICS EQUIPMENT VENTILATION 210 OPERATIONAL CHECK OF SMOKE CONFIGURATION CONTROL CIRCUIT AVIONICS EQUIPMENT VENTILATION 120 OPERATIONAL CHECK OF DITCHING CONFIGURATION CONTROL CIRCUIT AVIONICS EQUIPMENT VENTILATION AF AF AF AF DETAILED INSPECTION OF SKIN HEAT EXCHANGER DRAIN HOSE CONNECTION AREA R 212600-06-1 212600-07-1 120 ACCESS PANELS: 812, 822 AVIONICS EQUIPMENT VENTILATION 128 DETAILED INSPECTION OF DEMISTER DRAIN HOSE CONNECTION AREA AVIONICS EQUIPMENT VENTILATION AF REV: 07 DATE: 29-Dec-2014 INTERVALS I: 1000 FH OR 12 MO NOTE MRB 7 LUR MRB 9 LUR OPC I: 24 MO MRB 9 OPC I: 7500 FH OR 50 MO OPC I: 15000 FH OR 100 MO DET I: 24000 FH OR 160 MO MRB 8 LUR DET MRB 9 LUR I: 24000 FH OR 160 MO I: 24000 FH OR 160 MO DET AF OPC I: 24 MO TPS REFERENCES 212300-600-001 MEN TASKM. H. MRB 9 LUR MRB 9 LUR APPL 1 0.20 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 212600-710-001 1 0.10 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 21.26.00/04 212600-710-004 1 0.10 ALL SOURCE: MRB 21.26.00/05 212642-200-003 1 0.40 ALL 1 0.20 2930 2964 3044 1 0.08 ALL 1 0.10 ALL SOURCE: MRB 21.23.00/03 OPC I: 750 FH OR 6 MO AF DETAILED INSPECTION OF ELBOW DRAIN HOSE CONNECTION AREA DOWNSTREAM OF BLOWER FAN SOURCE SOURCE: MRB 21.26.00/06 212642-210-001 SIL LUR SOURCE: MRB 21.26.00/08 212642-210-002 SIL 21-074 MRB 9 212656-280-002 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 SOURCE: MRB 21.26.00/16 Sub 2 - Page 14 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 212600-09-1 ZONE 120 DESCRIPTION AVIONICS EQUIPMENT VENTILATION SKILL TASK CODE CODE 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 AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE I: 40 MO NOTE MRB 9 I: 3600 FH OR 24 MO MRB 6 LUR I: 6 YE MRB 9 120 ACCESS PANELS: 824 AVIONICS VENTILATION DEMISTER REFERENCES 122113-100-002 MEN TASKM. H. APPL 1 0.30 ALL 1 0.10 2930 2964 3044 1 0.10 ALL 1 0.16 1 0.16 SOURCE: MRB 21.26.00/19 212643-600-016 SOURCE: MRB 21.26.00/21 DETAILED INSPECTION OF CHECK VALVE FLAPPERS FOR CONDITION AND OPERATION D 212643-06-1 TPS 212641-210-001 SOURCE: MRB 21.26.00/07 AF DET CHECK DEMISTER FILTER ELEMENT AND FILTER CARTRIDGE CLOGGING INDICATORS (POP OUT INDICATOR NOT VISIBLE) (LE BOZEC) I: 600 FH OR 6 MO NOTE MRB 6 LUR I: 1200 FH NOTE MRB 6 212643-200-001 SIL 21-100 SOURCE: MRB 21.26.00/11 NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED. R 212643-07-1 120 ACCESS PANELS: 824 AVIONICS VENTILATION DUST SEPARATOR DISCARD FILTER CARTRIDGE (PALL) 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 AF DIS 212643-920-001 SIL 21-078 SOURCE: MRB 21.26.00/13 1654 1679 1753 2465 2497 2879 2913 NOTE: MPD INTERVAL IS 3000 FH OR NOTE. TRIAL INTERVAL REDUCTION TO IMPROVE RELIABILITY. ORIGINAL MPD INTERVAL MAY BE APPLIED FOR THE PLANNING PURPOSES Sub 2 - Page 15 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 212643-09-1 ZONE 120 DESCRIPTION AVIONICS VENT. WATER/MOISTURE SEP. SKILL TASK CODE CODE EL OPERATIONAL CHECK OF NRV FOR FREE MOVEMENT AND CONFIRM THE BOWL IS CLEAN R 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 213100-01-1 210 AF OPERATIONAL CHECK OF SYSTEM VIA MCDU 213100-02-1 213100-03-1 213100-04-1 215000-02-1 210 PRESSURE CONTROL AND MONITORING 210 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 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 AF AF AF AF DETAILED INSPECTION OF PACK AIR CHECK VALVES FLAPPERS FOR CONDITION AND OPERATION D 215000-03-1 190 ACCESS PANELS: 131PW, 132PW, 191BB, 192FB PACK RAM AIR INLET DETAILED INSPECTION OF ACTUATOR MECHANISM AND INLET FLAP FOR EXCESSIVE PLAY AND CHECK GAP BETWEEN INLET NOSE AND DIFFUSER RAMP AF INTERVALS SOURCE OPC I: 1500 FH OR 12 MO MRB 9 LUR DET I: 3000 FH OR 24 MO MRB 9 LUR OPC I: 9000 FH OR 60 MO FNC I: 9000 FH OR 60 MO MRB 9 LUR OPC I: 22500 FH OR 150 MO OPC I: 22500 FH OR 150 MO DET I: 24000 FH OR 120 MO MRB 9 LUR DET ISB MRB 9 LUR INSPECTION OF THE SIPHON ASSEMBLY (STRAINER) FOR CLEANLINESS NOTE: THIS TASK IS CANCELLED AFTER REPLACEMENT OF PAL FILTER BY LE BOZEC FILTER PER MOD 32877 (SB 21-1139). PRESSURE CONTROL AND MONITORING REV: 07 DATE: 29-Dec-2014 I: 1800 FH OR 24 MO TPS REFERENCES 212643-710-001 SIL 21-078 MEN TASKM. H. APPL 1 0.16 1654 1679 1753 1 0.16 1654 1679 1753 213100-710-002 1 0.10 ALL SOURCE: MRB 21.31.00/02 213100-710-003 1 0.10 ALL 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 SOURCE: MRB 21.26.00/14 212643-100-001 SIL 21-100 SOURCE: MRB 21.26.00/15 MRB 6,9 LUR SOURCE: MRB 21.31.00/03 MRB 9 LUR MRB 9 SOURCE: MRB 21.31.00/05 215243-210-001 SOURCE: MRB 21.50.00/06 216151-200-001 ISB 21-1062 SOURCE: MRB 21.50.00/13 Sub 2 - Page 16 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 215000-03-2 ZONE 190 DESCRIPTION PACK RAM AIR INLET SKILL TASK CODE CODE AF DET DETAILED INSPECTION OF ACTUATOR MECHANISM AND INLET FLAP FOR EXCESSIVE PLAY AND CHECK GAP BETWEEN INLET NOSE AND DIFFUSER RAMP D 215000-04-2 215200-07-1 190 191 192 PACK RAM AIR OUTLET DETAILED INSPECTION OF RAM AIR OUTLET FLAP AND CHECK FOR EXCESSIVE BACKLASH OF OUTLET FLAP AIR COOLING AND TEMPERATURE CONTROL AF AF DET DIS DISCARD COMBO SEALS AND PERISEALS ON HOT AIR INLET DUCTING, PACK DUCTING AND TRIM AIR DUCTING. REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 TPS REFERENCES 216151-200-001 MEN TASKM. H. 1 1.00 1 1.00 1 1 2.50 2.50 1654 1679 1753 1 1 2.50 2.50 1654 1679 1753 2465 2497 2930 2964 2879 2913 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 APPL 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 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 R 215200-08-1 191 192 AIR COOLING AND TEMPERATURE CONTROL AF DIS DISCARD O-RING SEALS ON HOT AIR INLET DUCTING, PACK DUCTING AND TRIM AIR DUCTING. SOURCE: MRB 21.50.00/17 NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT 215242-01-1 215500-01-1 191 192 210 ACCESS PANELS: 191KB, 192KB INJECTOR - WATER AF GENERAL VISUAL INSPECTION OF WATER INJECTOR NOZZLES FOR EROSION. EMERGENCY RAM AIR INLET AF OPERATIONAL CHECK OF EMERGENCY RAM AIR INLET SYSTEM 215500-02-1 210 EMERGENCY RAM AIR INLET OPERATIONAL CHECK OF EMERGENCY RAM AIR INLET AND FLOW CONTROL VALVE CLOSING IN DITCHING CONFIGURATION AF GVI I: 24000 FH OR 160 MO OPC I: 15000 FH OR 100 MO OPC I: 15000 FH OR 100 MO 215200-920-002 SIL 21-039 SIL 36-047 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 MRB 9 LUR SOURCE: MRB 21.50.00/04 215500-710-002 SIL 21-060 SOURCE: MRB 21.50.00/11 Sub 2 - Page 17 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 215541-01-1 ZONE 137 DESCRIPTION EMERGENCY RAM AIR INLET CHECK VALVE SKILL TASK CODE CODE 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 R 216000-02-1 D 216000-03-1 210 ACCESS PANELS: 231CC, 251CC AIR COOLING AND TEMPERATURE CONTROL 130 OPERATIONAL CHECK OF ZONE CONTROLLER (BACK UP SWITCHING) VIA CFDS/MCDU TEMPERATURE CONTROL AF REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE I: 24000 FH OR 160 MO MRB 9 LUR I: 7500 FH OR 50 MO MRB 9 LUR TPS REFERENCES 215541-210-001 MEN TASKM. H. APPL 1 0.50 ALL 2 0.20 ALL 1 0.10 1654 1679 1753 1 1.50 SOURCE: MRB 21.50.00/07 216317-210-001 SOURCE: MRB 21.50.00/02 MRB 9 LUR AF OPC I: 9000 FH OR 60 MO RST I: 12000 FH OR 80 MO NOTE SIL LUR SOURCE: MRB 21.50.00/03 216300-920-001 SIL 21-134 AF DIS I: 12000 FH OR 80 MO NOTE SIL LUR 216300-920-001 SIL 21-134 1 1.50 ALL AF DET I: 9000 FH OR 60 MO MRB 9 LUR 216342-210-001 1 0.20 ALL REMOVE AND RESTORE TRIM AIR PRESSURE REGULATING VALVE (TAPRV) FILTER 216300-710-002 NOTE: ACCORDING TO SIL 21-134, TASK IS APPLICABLE TO AIRCRAFT FITTED WITH TAPRV P/N 746A0000-06 ONLY. INTERVAL MAY BE ADJUSTED IN ACCORDANCE WITH OPERATORS EXPERIENCE 216000-03-2 130 ACCESS PANELS: 131NW, 131PW 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. NOTE: INTERVAL MAY BE ADJUSTED IN ACCORDANCE WITH OPERATORS EXPERIENCE 216242-01-1 191 ACCESS PANELS: 131NW, 131PW AIR COOLING AND TEMPERATURE CONTROL DETAILED INSPECTION OF TRIM AIR CHECK VALVES FLAPPERS FOR CONDITION AND OPERATION SOURCE: MRB 21.50.00/05 PREPARATION: CHECK VALVE; ACCESS PANELS: 191BB, 192FB Sub 2 - Page 18 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 221000-01-1 223000-01-1 226000-01-1 ZONE DESCRIPTION 210 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) SKILL TASK CODE CODE AV AV AV OPERATIONAL CHECK OF AUTOMATIC CHANGEOVER (AFS TEST) 226000-02-1 210 FLIGHT AUGMENTATION (FAC) AV OPERATIONAL CHECK OF FAC 2 FUNCTIONS 226000-03-1 210 FLIGHT AUGMENTATION (FAC) AV OPERATIONAL CHECK OF "RETURN TO LOWSPEED" FUNCTION R 227100-01-1-SDM 210 FLIGHT MANAGEMENT SYSTEM (FMS) AV LOAD NAVIGATION DATA BASE AND UPDATE IDLE/PERF VALUE 231300-01-1 210 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 OPERATIONAL CHECK OF RADIO NAVIGATION SELECTION IN STANDBY MODE USING RMP 1 AND 2 233300-01-1 200 PASSENGER ENTERTAINMENT (MUSIC AND VIDEO) RA OPERATIONAL CHECK OF IFES POWER SHUTDOWN FUNCTION BY USING THE VCC MASTER POWER OR VCC MAIN POWER SWITCH IN VIDEO CONTROL CENTER. 235100-01-1 210 ACCESS PANELS: 831, 841 AUDIO MANAGEMENT OPERATIONAL CHECK OF CAPT. AND F/O AUDIO CONTROL PANELS SWITCHING TO THIRD AUDIO CONTROL PANEL RA REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE OPC I: 15000 FH OR 100 MO OPC I: 22500 FH OR 150 MO OPC I: 750 FH OR 6 MO OPC I: 7500 FH OR 50 MO OPC I: 7500 FH OR 50 MO SVC I: 28 DY NOTE MRB 9 LUR OPC I: 7500 FH OR 50 MO MRB 9 LUR OPC I: 15000 FH OR 100 MO MRB 9 LUR OPC I: 15000 FH OR 100 MO MRB 9 LUR MRB 9 LUR MRB 9 LUR MRB 9 LUR MRB 9 LUR SPECI TPS REFERENCES MEN TASKM. H. APPL 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 SOURCE: MRB 22.60.00/03 227000-610-008 JIC A320-22-83-00 JIC A320-22-70-00 1 1.00 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 233600-710-007 1 0.17 2930 2964 3044 1 0.10 ALL SOURCE: MRB 23.33.00/01 235100-710-003 SOURCE: MRB 23.50.00/01 Sub 2 - Page 19 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 OPERATIONAL CHECK OF CVR AND CVR-CHANNEL RECORDING 237100-02-1 R 237135-02-1 210 COCKPIT VOICE RECORDER 312 OPERATIONAL CHECK OF CVR RECORDING LOGIC INCLUDING TIME DELAY RELAY COCKPIT VOICE RECORDER RA AV FNC REV: 07 DATE: 29-Dec-2014 INTERVALS I: 20 MO OPC I: 7500 FH OR 50 MO OPC I: 15000 FH OR 100 MO OPC I: 2 YE SOURCE MRB 9 MRB 9 LUR MRB 9 LUR MRB 9 OPERATIONAL CHECK OF ULB NOTE: CVR P/N 980-6022-001 VENDOR: HONEYWELL INTERNATIONAL INC ULB: P/N DK120, VENDOR DUKANE R 237300-01-1 D 237300-02-1 210 ACCESS PANELS: 312AR CABIN INTERCOMMUNICATION DATA SYSTEM 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 200 CABIN INTERCOMMUNICATION DATA SYSTEM RA RA RA OPERATIONAL CHECK OF LOUDSPEAKERS VIA MCDU 237300-04-1 200 ACCESS PANELS: 831, 841 CABIN INTERCOMMUNICATION DATA SYSTEM OPERATIONAL CHECK OF DECODER/ENCODER UNITS ESSENTIAL POWER SUPPLY, AND DECODER/ENCODER UNITS-A CUT OFF FUNCTION REFERENCES 236100-200-001 MEN TASKM. H. APPL 1 1 1 0.60 0.60 0.60 ALL 1 0.40 ALL 1 0.50 ALL 1 0.15 ALL 1 0.30 1654 1679 1753 2930 237300-710-015 1 0.30 SOURCE: MRB 23.73.00/02 237300-710-036 1 0.20 ALL 1 0.20 2465 2497 2964 3044 2879 2913 SOURCE: MRB 23.60.00/01 237100-710-001 SOURCE: MRB 23.71.00/01 237100-710-002 SOURCE: MRB 23.71.00/02 237100-720-001 CMM 23-70-01 CMM 23-70-03 CMM 23-70-10 CMM 23-70-44 SOURCE: MRB 23.71.00/04 OPERATIONAL CHECK OF POWER TRANSFER FUNCTION 237300-03-1 TPS RA OPC I: 22500 FH OR 150 MO MRB 9 LUR OPC I: 22500 FH OR 150 MO OPC I: 7500 FH OR 50 MO MRB 9 LUR OPC I: 22500 FH OR 150 MO MRB 9 LUR 237300-710-002 SOURCE: MRB 23.73.00/01 MRB 9 LUR SOURCE: MRB 23.73.00/03 237300-710-038 SOURCE: MRB 23.73.00/04 ACCESS PANELS: 831, 841 Sub 2 - Page 20 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 237300-08-1 ZONE 200 DESCRIPTION CABIN INTERCOMMUNICATION DATA SYSTEM SKILL TASK CODE CODE RA OPERATIONAL CHECK OF BATTERY BUS POWERED PA D 237300-09-1 200 ACCESS PANELS: 831, 841 CABIN INTERCOMMUNICATION DATA SYSTEM RA OPERATIONAL CHECK OF CABIN BULB SIGNS VIA MCDU D 240000-03-1 240000-04-1 311 312 521 621 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE OPC I: 15000 FH OR 100 MO MRB 9 LUR OPC I: 1500 FH OR 10 MO DET I: 24 MO MRB 9 LUR TPS REFERENCES 237300-710-042 MEN TASKM. H. 1 0.10 237300-710-802 1 0.10 SOURCE: MRB 23.73.00/09 249219-210-001 ISB 24-1060 1 1 0.50 0.50 APPL SOURCE: MRB 23.73.00/08 ELECTRICAL POWER EL ISB DETAILED INSPECTION OF WIRING BETWEEN FR76 AND FR77 ELECTRICAL POWER EL TPS I: 24 MO SIL 2 249200-210-003 SIL 24-067 1 1 0.50 0.50 ALL 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 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 240000-05-1 522 622 ACCESS PANELS: 471CL, 521GB, 482CR, 621GB ELECTRICAL POWER 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 240000-06-1 571 574 671 674 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 Sub 2 - Page 21 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 240000-07-1 ZONE 575 675 DESCRIPTION ELECTRICAL POWER SKILL TASK CODE CODE REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE TPS REFERENCES MEN TASKM. H. APPL EL TPS I: 24 MO SIL 2 249200-210-006 SIL 24-067 1 1 0.50 0.50 ALL EL TPS I: 24 MO SIL 2 249200-210-013 SIL 24-067 1 1 0.25 0.25 ALL EL TPS I: 6 YE SIL 2 249200-210-005 SIL 24-067 1 1 0.75 0.75 ALL 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 APPLY TEMPORARY PROTECTION TO END FITTINGS OF ELECTRICAL CONDUITS IN WING OUTBOARD TRAILING EDGE 240000-08-1 531 631 ACCESS PANELS: 575BB, 575CB, 575DB, 575EB, 575FB, 575GB, 575HB, 575KB, 575LB, 575MB, 675BB, 675CB, 675DB, 675EB, 675FB, 675GB, 675HB, 675KB, 675LB, 675MB ELECTRICAL POWER 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 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 240000-10-1 560 660 ACCESS PANELS: 534AB, 634AB ELECTRICAL POWER 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 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 Sub 2 - Page 22 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 240000-12-1 ZONE 311 312 DESCRIPTION ELECTRICAL POWER SKILL TASK CODE CODE REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE TPS REFERENCES MEN TASKM. H. APPL 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 EL TPS I: 24 MO SIL 2 249200-210-011 SIL 24-067 1 1 0.40 0.40 ALL EL OPC T: 24 MO I: 36 MO SIL 240000-200-004 SIL 20-017 1 1 0.05 0.05 ALL EL OPC I: 750 FH OR 6 MO MRB 9 LUR 244100-740-002 1 0.10 2465 2497 2930 2964 3044 2879 2913 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 240000-16-1 321 322 324 334 344 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 ELECTRICAL POWER 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 SOURCE: MRB 24.20.00/19 Sub 2 - Page 23 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 242000-21-1 ZONE 438 448 DESCRIPTION AC GENERATION SKILL TASK CODE CODE EN DIS - REMOVE AND DISCARD SCAVENGE AND CHARGE FILTER ELEMENTS, - DRAIN AND REPLENISH OIL SYSTEM REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE I: 800 FH OR 6 MO NOTE CMP MRB 6 LUR I: 2400 FH OR 24 MO MRB 6 LUR I: 150 FH OR 1 MO NOTE MRB 6 LUR I: 800 FH OR 6 MO NOTE CMP MRB 6 LUR TPS REFERENCES 242100-920-040 SIL SUN 236 MEN TASKM. H. APPL 1 1 0.40 0.40 2465 2497 2930 2964 3044 2879 2913 1 1 0.30 0.30 ALL 1 1 0.02 0.02 ALL 1 1 0.40 0.40 1654 1679 1753 1 0.10 ALL 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 EN FNC CHECK TORQUE OF QUICK-ATTACH-DETACH (QAD) TENSION BOLT 242100-02-1 438 448 ACCESS PANELS: 438AR, 448AR INTEGRATED DRIVE GENERATOR EN DET -CHECK OIL LEVEL OF INTEGRATED DRIVE GENERATOR (GREEN RANGE) AND REPLENISH IF NECESSARY -CHECK FILTER DIFFERENTIAL PRESSURE INDICATOR ( POP OUT NOT PROTRUDING ) 242100-210-043 SOURCE: MRB 24.20.00/07 242100-210-046 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. R 242100-03-1 438 448 ACCESS PANELS: 438AR, 448AR INTEGRATED DRIVE GENERATOR EN - REMOVE AND DISCARD SCAVENGE FILTER ELEMENT - DRAIN AND REPLENISH OIL SYSTEM DIS 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 OPERATIONAL CHECK OF TRANSFER INHIBITION EL OPC I: 7500 FH OR 50 MO 242100-920-040 SIL SUN 236 MRB 9 LUR 242200-710-002 SOURCE: MRB 24.20.00/08 Sub 2 - Page 24 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 242400-01-2 ZONE 210 DESCRIPTION AC EMERGENCY GENERATION SKILL TASK CODE CODE EL OPERATIONAL CHECK OF EMERGENCY GENERATING SYSTEM D 242400-01-3 210 AC EMERGENCY GENERATION EL OPERATIONAL CHECK OF EMERGENCY GENERATING SYSTEM 242400-02-1 210 AC GENERATION EL OPERATIONAL CHECK OF EMERGENCY GCU VIA CFDS 242500-01-1 210 AC GENERATION EL OPERATIONAL CHECK OF AC ESS GENERATION SWITCHING D 242600-01-1 242600-02-1 210 AC GENERATION 210 OPERATIONAL CHECK OF MANUAL AND AUTOMATIC GALLEY SHEDDING AC GENERATION EL EL OPERATIONAL CHECK OF MANUAL AND AUTOMATIC GALLEY AND BUS SHEDDING 242800-01-2 210 STATIC INVERTER EL OPERATIONAL CHECK OF STATIC INVERTER D 242800-01-3 210 STATIC INVERTER OPERATIONAL CHECK OF STATIC INVERTER EL REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE OPC I: 120 FH OR 1 MO CMR* MRB 8 LUR OPC I: 90 FH OR 1 MO CMR* MRB 8 LUR OPC I: 15000 FH OR 100 MO OPC I: 7500 FH OR 50 MO OPC I: 8000 FH OR 60 MO OPC I: 15000 FH OR 100 MO MRB 9 LUR OPC I: 750 FH OR 6 MO CMR** MRB 8 LUR OPC I: 90 FH OR 1 MO CMR* MRB 8 LUR MRB 9 LUR MRB 8 LUR MRB 8 LUR TPS REFERENCES MEN TASKM. H. APPL 242400-710-001 1 0.02 SOURCE: CMR 242000-00002-1-C MRB 24.20.00/15 MRB 24.30.00/08 MRB 24.50.00/06 242400-710-001 1 0.02 SOURCE: CMR 242000-00002-2-C MRB 24.20.00/16 MRB 24.30.00/09 MRB 24.50.00/07 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 SOURCE: MRB 24.20.00/13 242600-710-002 1 0.10 242800-710-001 1 0.10 SOURCE: CMR 242000-00001-2-C MRB 24.20.00/17 MRB 24.30.00/10 MRB 24.50.00/08 242800-710-001 1 0.10 SOURCE: MRB 24.20.00/14 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 SOURCE: CMR 242000-00001-1-C MRB 24.20.00/18 MRB 24.30.00/11 MRB 24.50.00/09 Sub 2 - Page 25 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 243200-01-1 ZONE 210 DESCRIPTION DC GENERATION SKILL TASK CODE CODE EL OPERATIONAL CHECK OF DC GENERATION SWITCHING 243400-01-1 210 DC GENERATION EL OPERATIONAL CHECK OF "DC EMERG. CONFIG" CAUTION 243800-01-1 R 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 OPERATIONAL CHECK OF GPCU VIA CFDS 245100-01-1 210 AC/DC ELECTRICAL LOAD DISTRIBUTION EL OPERATIONAL CHECK OF GENERATOR LINE CONTACTOR OPENING 245100-02-1 210 AC/DC ELECTRICAL LOAD DISTRIBUTION EL OPERATIONAL CHECK OF COMMERCIAL ELECTRIC LOAD SHEDDING 251100-01-1 251100-02-1 210 COCKPIT SEATS 210 DETAILED INSPECTION OF SEAT STRUCTURE AND SEAT ATTACHMENT OF ALL FLIGHT DECK SEATS COCKPIT SEATS AF AF 252100-02-1 252200-01-1 200 PASSENGER COMPARTMENT SEATS 200 DETAILED INSPECTION OF SEAT TO FLOOR ATTACHMENT AND GENERAL VISUAL INSPECTION OF SEAT STRUCTURE PASSENGER COMPARTMENT SEATS 200 DETAILED INSPECTION OF SEAT BELT ATTACHMENT, SEAT BELT AND LOCK. CHECK OF LOCK CABIN ATTENDANT SEATS DETAILED INSPECTION OF SEAT ATTACHMENT AND GENERAL VISUAL INSPECTION OF SEAT STRUCTURE AF AF AF INTERVALS SOURCE OPC I: 6000 FH OR 48 MO OPC I: 7500 FH OR 50 MO OPC I: 750 FH OR 6 MO OPC I: 750 FH OR 6 MO OPC I: 15000 FH OR 100 MO OPC I: 15000 FH OR 100 MO MRB 9 LUR DET MRB 9 LUR FNC CHECK OF ADJUSTMENT OF SEAT CONTROL CABLES 252100-01-1 REV: 07 DATE: 29-Dec-2014 DET DET DET I: 24000 FH OR 160 MO I: 7500 FH OR 50 MO I: 15000 FH OR 100 MO I: 15000 FH OR 100 MO I: 15000 FH OR 100 MO MRB 9 LUR MRB 9 LUR MRB 9 LUR MRB 8 LUR MRB 9 LUR TPS REFERENCES MEN TASKM. H. 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 1654 1679 1753 SOURCE: MRB 24.20.00/03 242200-710-001 1 0.30 ALL SOURCE: MRB 24.50.00/04 245100-710-001 1 0.10 251100-200-001 1 0.30 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 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 252100-210-002 1 1.60 ALL SOURCE: MRB 25.21.00/02 252200-210-001 1 0.30 ALL SOURCE: MRB 24.50.00/05 MRB 6,9 LUR MRB 9 LUR MRB 9 LUR MRB 9 LUR APPL SOURCE: MRB 25.22.00/01 Sub 2 - Page 26 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 252200-02-1 252331-01-1 253000-01-1 ZONE DESCRIPTION SKILL TASK CODE CODE 200 CABIN ATTENDANT SEATS AF DET 200 DETAILED INSPECTION OF SEAT BELT ATTACHMENT, SEAT BELT AND LOCK. CHECK OF LOCK PANELS - LOWER SIDEWALL AF DET 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 BUFFET AND GALLEY CA DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE I: 15000 FH OR 100 MO I: 24 MO MRB 9 LUR I: 6 YE MRB 9 SIL DETAILED INSPECTION OF ATTACHMENT POINTS R 253000-02-1 200 BUFFET AND GALLEY AF DIS REMOVE AND DISCARD FILTER ELEMENT 253400-01-1 200 NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED. GALLEY COOLING AF RST CLEAN "CHILLED AIR IN" AND "CHILLED AIR OUT" GRILLES/FILTERS IN GALLEY CABINET 253400-02-1 200 NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED. GALLEY COOLING CLEAN AIR CHILLER CONDENSER AIR FILTER NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED. AF RST I: 5500 FH OR 40 MO NOTE MRB 7 LUR I: 1500 FH OR 12 MO NOTE MRB 9 LUR I: 1500 FH OR 12 MO OR VR/NT MRB 9 LUR TPS REFERENCES 252200-210-002 MEN TASKM. H. APPL 1 0.25 ALL 1 0.30 ALL 253000-210-001 1 0.30 ALL SOURCE: MRB 25.30.00/01 253000-920-001 1 0.20 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1 0.20 2879 2913 1 0.20 2879 2913 SOURCE: MRB 25.22.00/02 252344-210-001 SIL 25-085 SOURCE: MRB 25.30.00/04 253400-100-001 SOURCE: MRB 25.34.00/01 253400-100-002 SOURCE: MRB 25.34.00/02 Sub 2 - Page 27 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 254000-01-1 ZONE 200 DESCRIPTION LAVATORIES SKILL TASK CODE CODE CA DET REV: 07 DATE: 29-Dec-2014 INTERVALS I: 1000 FH DETAILED INSPECTION OF WASTE COMPARTMENT INCLUDING WASTE FLAP AND OPERATIONAL CHECK OF WASTE FLAP R 254000-02-1 200 NOTE: INTERVAL IS 1000 FH FOR OPERATOR FLYING UNDER FAA REGULATIONS AS PER FAA AD 74-08-09. LAVATORIES SOURCE FAA AD MRB 9 LUR 200 LAVATORIES CA DET I: 5 YE 200 LAVATORIES 200 LAVATORIES 255000-16-1 256000-01-1-SDM 130 150 160 130 150 160 200 CARGO COMPARTMENTS CA DET 0.20 ALL 1654 MRB 9 SOURCE: MRB 25.40.00/02 254000-210-002 I: 80 MO 1 0.30 1679 1753 2465 2497 2930 2964 3044 2879 2913 1654 1679 1753 SOURCE: MRB 25.40.00/03 CA DET CA DET AF VCK I: 6000 FH MRB 9 254000-210-004 1 1.50 MRB 9 SOURCE: MRB 25.40.00/04 254000-210-004 I: 7500 FH 1 1.50 MRB 8 SOURCE: MRB 25.40.00/05 255000-200-002 I: 8 DY 1 1 1 0.20 0.20 0.20 1 1 1 0.20 0.20 0.20 ALL 1 TBD ALL SOURCE: MRB 25.50.00/01 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. LIFE VESTS 1 0.30 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 CARGO COMPARTMENTS APPL 1 DETAILED INSPECTION OF LAVATORY FLOOR PAN 255000-01-1 TASKM. H. 254000-210-002 DETAILED INSPECTION OF LAVATORY FLOOR PAN 254000-04-2 254000-210-001 FAA AD 74-08-09 MEN MRB 9 DETAILED INSPECTION OF ATTACHMENT POINTS R 254000-04-1 REFERENCES SOURCE: MRB 25.40.00/01 DETAILED INSPECTION OF ATTACHMENT POINTS 254000-02-2 TPS CA VCK I: 750 FH OR 6 MO MRB 9 LUR I: 6 MO SPECI 255000-200-025 SOURCE: MRB 25.50.00/04 JIC A320-25-60-01 2465 2497 2930 2964 3044 2879 2913 ALL CHECK LIFE VESTS AVAILABLE AND SERVICE LIFE NOT EXPIRED NOTE: REPLACE LIFE VEST OR OPEN DEFERRED ITEM IF LIFE VEST EXPIRES IN LESS THAN 7 MO Sub 2 - Page 28 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 256000-01-5-SDM ZONE 260 DESCRIPTION FIRST AID KIT SKILL TASK CODE CODE REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE TPS REFERENCES MEN TASKM. H. APPL 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 1 1 1 1 0.10 0.10 0.10 0.10 ALL 256300-710-001 2 0.20 ALL MRB 9 SOURCE: MRB 23.73.00/05 256551-710-002 1 0.10 ALL MRB 8 SOURCE: MRB 25.65.51/02 256641-210-001 1 0.10 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 SOURCE: MRB 25.61.41/01 AF VCK CHECK DOOR AND OFFWING ESCAPE SLIDE/RAFT INFLATION RESERVOIR PRESSURE. I: 750 FH OR 6 MO MRB 8 LUR I: 1110 FC OR 400 DY NOTE MRB 9 SIL 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 256241-05-1 256300-01-1 221 222 261 262 200 DOOR ESCAPE SLIDE AF CLEAN DOOR GIRT BAR FITTING STOP LEVERS NOTE: INTERVAL TO BE ADJUSTED ACCORDING TO DOOR USAGE EVACUATION SIGNALLING EQUIPMENT CA OPERATIONAL CHECK OF EVAC FUNCTION 256551-02-1 200 RST MEGAPHONE CA OPC I: 22500 FH OR 150 MO OPC I: 24 MO SOURCE: MRB 52.10.00/07 MRB 9 LUR OPERATIONAL CHECK OF MEGAPHONE D 256600-02-1 200 SUPPLEMENTAL LIFE RAFT CHECK PRESSURE AT LIFE RAFT PRESSURE GAUGE (IF CONFIGURATION INCLUDES VISIBLE GAUGE) AF VCK I: 4 MO 531100-210-034 SIL 53-054 SOURCE: MRB 25.66.41/02 Sub 2 - Page 29 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 261200-01-1 ZONE 210 DESCRIPTION ENGINE FIRE AND OVERHEAT DETECTION SKILL TASK CODE CODE EL REV: 07 DATE: 29-Dec-2014 INTERVALS OPC I: 750 FH SOURCE MRB 8 OPERATIONAL CHECK OF LOOP/SQUIB 261300-01-1 210 APU FIRE AND OVERHEAT DETECTION EL OPERATIONAL CHECK OF LOOP/SQUIB 261500-03-1 128 AVIONICS COMPARTMENT SMOKE DETECTION AF 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. 261600-03-1 210 ACCESS PANELS: 824 CARGO COMPARTMENT SMOKE DETECTION EL OPERATIONAL CHECK OF CARGO COMPARTMENT SMOKE DETECTION BY PTT R 261600-04-1 261700-03-1 262100-02-1 262100-03-1 210 CARGO COMPARTMENT SMOKE DETECTION 210 OPERATIONAL CHECK OF CARGO COMPARTMENT SMOKE DETECTION BY CFDS TO CONFIRM ISOLATION VALVES LATCHING CIRCUIT INTEGRITY. LAVATORY SMOKE DETECTION 210 OPERATIONAL CHECK OF LAVATORY SMOKE DETECTION BY CFDS TO CONFIRM WARNINGS CAN BE DISPLAYED ENGINE FIRE EXTINGUISHING 415 425 OPERATIONAL CHECK OF BOTTLE LOW PRESSURE INDICATING CIRCUIT ENGINE FIRE EXTINGUISHING CHECK FIRING CIRCUIT CONTINUITY EL EL EL EL OPC I: 750 FH OR 6 MO MRB 8 LUR RST MRB 9 LUR I: 11000 FH OR 73 MO NOTE TPS REFERENCES MEN TASKM. H. APPL 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 261600-710-001 1 0.10 ALL SOURCE: MRB 26.16.00/01 MRB 26.23.00/02 261600-710-003 1 0.10 SOURCE: MRB 21.28.00/06 MRB 26.16.00/02 261700-710-001 1654 1679 1753 2465 2497 2879 2913 1 0.10 ALL SOURCE: MRB 26.17.00/01 262100-710-002 1 0.20 ALL 2 2 0.20 0.20 ALL SOURCE: MRB 26.15.00/03 OPC I: 750 FH OR 6 MO MRB 8 LUR OPC I: 750 FH OR 6 MO MRB 8 LUR OPC I: 800 FH OR 6 MO OPC I: 7500 FH OR 50 MO OPC I: 15000 FH OR 100 MO MRB 9 LUR MRB 9 LUR MRB 9 LUR SOURCE: MRB 26.21.00/02 262100-720-001 SOURCE: MRB 26.21.00/03 ACCESS PANELS: 415BR, 425BR Sub 2 - Page 30 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 262100-04-1 ZONE 415 425 DESCRIPTION ENGINE FIRE EXTINGUISHING SKILL TASK CODE CODE 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 EL OPERATIONAL CHECK OF FIRE CONTROL PUSH BUTTON SWITCH SUB FUNCTIONS RELATED TO ENGINE SHUTDOWN AND ISOLATION 262142-01-1-SDM 262200-02-1 415 425 ACCESS PANELS: 413DL, 423DL ENGINE FIRE EXTINGUISHER BOTTLE CARTRIDGE 210 CHECK ENGINE EXTINGUISHER SQUIBS FOR EXPERATION DATE APU FIRE EXTINGUISHING CA EL 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 CHECK FIRING CIRCUIT CONTINUITY 262200-04-1 313 ACCESS PANELS: 314AR APU FIRE EXTINGUISHING AF DETAILED INSPECTION OF DISTRIBUTION PIPING 262200-05-1 210 ACCESS PANELS: 314AR APU FIRE EXTINGUISHING OPERATIONAL CHECK OF LOW PRESSURE INDICATING CIRCUIT EL REV: 07 DATE: 29-Dec-2014 INTERVALS I: 8000 FH OR 72 MO SOURCE MRB 8 LUR REFERENCES 262100-720-003 MEN TASKM. H. APPL 2 2 1.00 1.00 ALL 1 0.50 ALL 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 SOURCE: MRB 26.21.00/04 OPC I: 15000 FH OR 100 MO MRB 8 LUR VCK SPECI I: 24 MO TPS 262100-710-004 SOURCE: MRB 26.21.00/08 MRB 36.00.00/06 OPC I: 3000 FH OR 20 MO MRB 8 LUR OPC I: 15000 FH OR 100 MO MRB 8 LUR DET I: 15000 FH OR 100 MO MRB 8 LUR OPC I: 15000 FH OR 100 MO MRB 8 LUR 262141-920-001 SOURCE: MRB 26.22.00/07 262200-210-001 SOURCE: MRB 26.22.00/05 262200-710-003 SOURCE: MRB 26.22.00/06 ACCESS PANELS: 314AR Sub 2 - Page 31 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 262200-06-1 ZONE 210 DESCRIPTION APU FIRE EXTINGUISHING SKILL TASK CODE CODE EL 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 CA REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 132 CARGO COMPARTMENT FIRE EXTINGUISHING EL CHECK FIRING CIRCUIT CONTINUITY R 262300-02-3 132 ACCESS PANELS: 132SW, 825 CARGO COMPARTMENT FIRE EXTINGUISHING EL CHECK FIRING CIRCUIT CONTINUITY 262300-02-4 162 ACCESS PANELS: 132MW, 825 CARGO COMPARTMENT FIRE EXTINGUISHING EL CHECK FIRING CIRCUIT CONTINUITY 262300-03-1 132 ACCESS PANELS: 162AW, 826 CARGO COMPARTMENT FIRE EXTINGUISHING CA 132 ACCESS PANELS: 132SW, 825 CARGO COMPARTMENT FIRE EXTINGUISHING CA 162 ACCESS PANELS: 132MW, 825 CARGO COMPARTMENT FIRE EXTINGUISHING CA 132 ACCESS PANELS: 162AW, 826 CARGO FIRE EXTINGUISHER BOTTLE - CARTRIDGE CA APPL 1 0.30 ALL VCK 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 26.22.00/04 262300-720-001 2 0.20 1654 1679 1753 2465 SOURCE: CMR 262300-00001-1-C MRB 26.23.00/03 262300-720-001 2 0.20 2930 2964 3044 SOURCE: CMR 262300-00001-1-C MRB 26.23.00/03 262300-720-001 2 0.20 2497 2879 2913 SOURCE: CMR 262300-00001-1-C MRB 26.23.00/03 262300-200-001 2 1.00 1654 1679 1753 2465 262300-200-001 2 1.00 2930 2964 3044 SOURCE: CMR 262300-00002-1-C MRB 26.23.00/04 262300-200-001 2 1.00 2497 2879 2913 SOURCE: CMR 262300-00002-1-C MRB 26.23.00/04 JIC A320-26-23-00 1 0.10 ALL I: 24 MO OPC I: 12000 FH OR 80 MO CMR** MRB 8 LUR OPC I: 12000 FH OR 80 MO CMR** MRB 8 LUR OPC I: 12000 FH OR 80 MO CMR** MRB 8 LUR FNC I: 18000 FH OR 120 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 I: 24 MO SPECI FNC FNC CHECK FIRE EXTINGUISHING LINES FOR LEAKAGE AND OBSTRUCTION 262300-04-1-SDM TASKM. H. 262200-710-004 CHECK FIRE EXTINGUISHING LINES FOR LEAKAGE AND OBSTRUCTION 262300-03-4 MEN MRB 8 CHECK FIRE EXTINGUISHING LINES FOR LEAKAGE AND OBSTRUCTION R 262300-03-3 REFERENCES OPC I: 24000 FH OR 80 MO CHECK APU EXTINGUISHER SQUIBS FOR EXPERATION DATE 262300-02-1 TPS VCK SOURCE: CMR 262300-00002-1-C MRB 26.23.00/04 CHECK CARGO FIRE EXTINGUISHER SQUIB FOR EXPERATION DATE Sub 2 - Page 32 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 262300-05-1 ZONE 132 210 DESCRIPTION CARGO COMPARTMENT FIRE EXTINGUISHING SKILL TASK CODE CODE EL FNC PERFORM FUNCTIONAL CHECK OF TIME DELAY FOR ILLUMINATION OF "DISCH AGENT 2" REMINDER LIGHT D 262300-06-1 132 210 ACCESS PANELS: 132MW, 825 CARGO COMPARTMENT FIRE EXTINGUISHING EL CHECK FIRING CIRCUIT CONTINUITY AND PERFORM OPERATIONAL CHECK OF PRIORITY SWITCHING D 262300-07-1 132 ACCESS PANELS: 132MW, 825 CARGO COMPARTMENT FIRE EXTINGUISHING AF 132 ACCESS PANELS: 132MW, 825 CARGO COMPARTMENT FIRE EXTINGUISHING AF 132 ACCESS PANELS: 132MW, 825 CARGO COMPARTMENT FIRE EXTINGUISHING AF I: 72 MO OR 16500 FH SOURCE MRB 9 TPS REFERENCES 262300-710-004 APPL 1 1 0.60 0.60 2 1.00 2 2.00 1 0.50 262400-210-002 1 0.10 ALL SOURCE: MRB 26.24.00/01 262500-200-002 1 0.10 ALL SOURCE: MRB 26.23.00/13 FNC I: 14000 FH OR 100 MO CMR** MRB 8 LUR 262300-200-003 I: 14000 FH OR 100 MO MRB 8 LUR 262300-200-002 I: 15 MO MRB 8 DIS TASKM. H. 1.10 1.10 262300-710-003 DET MEN 1 1 CMR** MRB 8 LUR -REMOVE HALON FILTER, CHECK VALVE AND DIAPHRAGM -INSPECT HALON FILTER -DO A DETAILED INSPECTION OF CHECK VALVE -DO A DETAILED INSPECTION OF DIAPHRAGM -REINSTALL HALON FILTER, CHECK VALVE AND DIAPHRAGM D 262300-09-1 INTERVALS OPC I: 6000 FH OR 72 MO FUNCTIONAL CHECK OF PRESSURE REDUCER IN FLOW METERING DEVICE INCLUDING CHECK OF FIRE EXTINGUISHING LINES FOR LEAKAGE AND OBSTRUCTION D 262300-08-1 REV: 07 DATE: 29-Dec-2014 SOURCE: CMR 262300-00001-1-C MRB 26.23.00/07 SOURCE: CMR 262300-00002-1-C MRB 26.23.00/04 MRB 26.23.00/08 SOURCE: MRB 26.23.00/09 MRB 26.23.00/10 MRB 26.23.00/11 262314-920-001 CMM 26-20-53 DISCARD WATER ADSORBING FILTER SOURCE: MRB 26.23.00/12 NOTE: MSN 0427, 0525: P/N QA06753, VENDOR: PALL FILTRATION 262441-01-1 200 ACCESS PANELS: 132MW, 825 PORTABLE FIRE EXTINGUISHER CA VCK CHECK PRESSURE GAUGE READING 262541-01-1 200 LAVATORY FIRE EXTINGUISHER GENERAL VISUAL INSPECTION OF LAVATORY FIRE EXTINGUISHER FOR SIGNS OF LEAKAGE/DISCHARGE CA GVI I: 750 FH OR 6 MO I: 48 MO MRB 9 LUR MRB 9 SOURCE: MRB 26.25.00/01 Sub 2 - Page 33 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 262541-04-1 ZONE 200 DESCRIPTION LAVATORY FIRE EXTINGUISHING SKILL TASK CODE CODE AF VCK REV: 07 DATE: 29-Dec-2014 INTERVALS I: 4 MO SOURCE MRB 9 VISUAL CHECK OF FIRE EXTINGUISHER BOTTLE PRESSURE READING 271400-01-1 210 AILERON AND HYDRAULIC ACTUATION 575 675 AILERON AND HYDRAULIC ACTUATION REFERENCES 262500-200-005 MEN TASKM. H. EL AF 0.10 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1 0.10 ALL 2 2 1.00 1.00 2 2 1.00 1.00 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1 1 0.20 0.20 ALL OPC I: 4000 FH OR 36 MO CMR** MRB 8 LUR FNC I: 5500 FH OR 48 MO MRB 9 LUR I: 18000 FH OR 120 MO MRB 9 LUR OPC I: 15000 FH OR 100 MO CMR** MRB 8 LUR 271400-220-002 OPC I: 1500 FH OR 12 MO DET I: 72 MO OR 24000 FH MRB 9 LUR 272200-710-001 1 0.10 ALL SOURCE: MRB 27.21.00/01 272100-210-002 1 0.30 ALL CHECK AILERON SERVO CONTROL AND HINGE BEARINGS FOR EXCESSIVE PLAY AND CONDITION 279600-710-007 APPL 1 SOURCE: MRB 26.25.00/04 OPERATIONAL CHECK OF DAMPING MEASUREMENT BY BITE D 271400-02-1 TPS SOURCE: CMR 271400-00001-1-C MRB 27.14.00/01 271400-220-001 SOURCE: MRB 27.14.00/03 ACCESS PANELS: 575KB, 575MB, 590AB, 590BB, 675KB, 675MB, 690AB, 690BB R 271400-02-2 575 675 AILERON AND HYDRAULIC ACTUATION AF CHECK AILERON SERVO CONTROL AND HINGE BEARINGS FOR EXCESSIVE PLAY AND CONDITION FNC 271400-220-001 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 CHECK FLUID RESERVE PISTON POSITION WITH HYDRAULIC RESERVOIR DEPRESSURIZED 272100-01-1 210 ACCESS PANELS: 575KB, 675KB RUDDER MECHANICAL CONTROL AF OPERATIONAL CHECK OF RESET FUNCTION 272100-02-1 100 RUDDER MECHANICAL CONTROL DETAILED INSPECTION OF RUDDER MECHANICAL CONTROL CABLES -INCLUDING ZONE 311- AF MRB 6 SOURCE: CMR 271400-00002-1-C MRB 27.14.00/02 SOURCE: MRB 27.21.00/03 ACCESS PANELS: 131AC, 131BC, 131CC, 131PW, 151AC, 151BC, 151CC, 151DC, 161AC, 161BC, 162DW, 241FF, 241KF, 312AR, 812, 824, 825, 826 Sub 2 - Page 34 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 272100-03-1 ZONE 145 DESCRIPTION RUDDER MECHANICAL CONTROL SKILL TASK CODE CODE AF FNC 210 ACCESS PANELS: 131BC, 811, 825 RUDDER MECHANICAL CONTROL AF OPERATIONAL CHECK OF CENTERING SPRING ROD 272100-07-1 325 ACCESS PANELS: 325CL, 325CR RUDDER MECHANICAL CONTROL AF INTERVALS SOURCE I: 72 MO OR 24000 FH MRB 6 OPC I: 18000 FH OR 72 MO MRB 8 DET I: 18000 FH OR 72 MO MRB 6,8 I: 20 MO MRB 6 I: 24000 FH OR 80 MO MRB 8 I: 24000 FH OR 80 MO MRB 9 CHECK TENSION OF RUDDER MECHANICAL CONTROL CABLES USING TENSIOMETER 272100-05-1 REV: 07 DATE: 29-Dec-2014 DETAILED INSPECTION OF MECHANICAL CONTROL LINKAGE IN FIN TPS REFERENCES 272100-220-001 MEN TASKM. H. APPL 1 0.10 ALL 2 0.40 ALL 1 0.10 ALL 272143-600-001 1 0.10 ALL SOURCE: MRB 27.21.00/09 272149-200-001 2 1.50 ALL 1 0.67 ALL 1 0.33 ALL 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 AF LUB LUBRICATION OF RUDDER PEDAL ADJUSTMENT MECHANISM 272100-10-1 320 RUDDER MECHANICAL CONTROL AF FNC FUNCTIONAL CHECK OF RUDDER SERVOCONTROL ACTUATING SPRING RODS SOURCE: MRB 27.21.00/10 ACCESS PANELS: 325BL, 325BR, 325CL, 325CR, 325DL, 325DR, 325EL, 325ER 272100-11-1 325 RUDDER MECHANICAL CONTROL AF 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 CHECK TENSION REGULATOR POINTER IS WITHIN THE LIMITS AF DET OPC I: 40 MO 272100-220-004 SOURCE: MRB 27.21.00/11 MRB 9 272100-220-002 SOURCE: MRB 27.21.00/02 ACCESS PANELS: 811 Sub 2 - Page 35 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 272400-01-1 ZONE 210 DESCRIPTION RUDDER HYDRAULIC ACTUATION SKILL TASK CODE CODE AF OPERATIONAL CHECK OF RUDDER SERVOCONTROLS WITH INDIVIDUAL HYDRAULIC SYSTEMS 272400-02-1 325 RUDDER HYDRAULIC ACTUATION AF 325 ACCESS PANELS: 325BL, 325CL, 325DL, 325EL RUDDER HYDRAULIC ACTUATION AF INTERVALS SOURCE OPC I: 750 FH OR 6 MO MRB 8 LUR FNC I: 18000 FH OR 120 MO MRB 9 LUR I: 5500 FH OR 15 MO MRB 9 I: 5500 FH OR 15 MO MRB 9 I: 5500 FH OR 20 MO MRB 9 OPC I: 4000 FH OR 36 MO CMR** MRB 8 LUR CHECK RUDDER SERVOCONTROL AND HINGE BEARINGS FOR EXCESSIVE PLAY AND CONDITION D 272400-03-1 REV: 07 DATE: 29-Dec-2014 LUB LUBRICATION OF RUDDER HINGE BEARING NO 6 WITH GREASE MAT. NO. 04-004 TPS REFERENCES MEN TASKM. H. APPL 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 1 0.10 1 0.10 ALL 1 0.10 ALL SOURCE: MRB 27.24.00/02 122255-640-001 SOURCE: MRB 27.24.00/03 NOTE: ALTERNATIVELY TASK 272400-05-1 CAN BE APPLIED. D 272400-03-1 325 ACCESS PANELS: 325DL, 325DR RUDDER HYDRAULIC ACTUATION AF LUB LUBRICATION OF RUDDER HINGE BEARING NO 6 WITH GREASE MAT. NO. 04-004 122255-640-001 SOURCE: MRB 27.24.00/03 NOTE: ALTERNATIVELY TASK 272400-05-1 CAN BE APPLIED. N 272400-05-1 325 ACCESS PANELS: 325DL, 325DR RUDDER HYDRAULIC ACTUATION AF LUBRICATION OF RUDDER HINGE BEARING NO 6 WITH GREASE MAT. NO. 04-037 LUB 122255-640-002 SOURCE: MRB 27.24.00/03 NOTE: THIS IS AN ALTERNATIVE TASK TO 272400-03-1. 273400-01-1 210 ACCESS PANELS: 325DL 325DR ELEVATOR AND HYDRAULIC ACTUATION OPERATIONAL CHECK OF DAMPING MEASUREMENT BY BITE EL 279600-710-008 SOURCE: CMR 273400-00001-1-C MRB 27.34.00/01 Sub 2 - Page 36 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 273400-02-1 ZONE 334 344 DESCRIPTION ELEVATOR AND HYDRAULIC ACTUATION SKILL TASK CODE CODE AF FNC CHECK ELEVATOR SERVO CONTROL AND HINGE BEARINGS FOR EXCESSIVE PLAY AND CONDITION REV: 07 DATE: 29-Dec-2014 INTERVALS I: 20 MO OR 12000 FH SOURCE EASA AD FAA AD MRB 9 ACCESS PANELS: 334BB, 334DB, 334FB, 334HB, 344BB, 344DB, 344FB, 344HB 273400-03-1 334 344 ELEVATOR AND HYDRAULIC ACTUATION AF CHECK FLUID RESERVE PISTON POSITION WITH HYDRAULIC RESERVOIR DEPRESSURIZED. 273400-04-2 334 344 ACCESS PANELS: 334DB, 344DB ELEVATOR AND HYDRAULIC ACTUATION AF OPC I: 15000 FH OR 100 MO CMR** MRB 8 LUR VCK MRB 8 LUR CHECK OF THE DIFFERENTIAL PRESSURE INDICATOR AND POSITION OF FLUID RESERVE PISTON OF ELEVATOR SERVO CONTROLS 273400-06-1 334 344 ACCESS PANELS: 334DB, 344DB ELEVATOR AND HYDRAULIC ACTUATION I: 24000 FH OR 160 MO TPS REFERENCES 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 MEN TASKM. H. APPL 2 2 1.00 1.00 ALL 1 1 0.20 0.20 ALL 1 1 0.20 0.20 ALL ALL SOURCE: CMR 273400-00002-1-C MRB 27.34.00/02 273400-220-002 SOURCE: MRB 27.34.00/04 AF CHK I: 80 MO SIL 273400-200-003 SIL 27-152 1 1 4.00 4.00 AF LUB I: 5500 FH OR 15 MO MRB 9 122253-640-001 1 0.10 I: 5500 FH OR 15 MO MRB 9 1 0.10 CHECK OF ELEVATOR NEUTRAL POSITION AND SERVO CONTROLS INSTALLATION D 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. D 274000-01-1 310 ACCESS PANELS: 314AR TRIMMABLE HORIZONTAL STABILIZER LUBRICATE THS BEARINGS AND ATTACHMENT FITTINGS WITH GREASE MAT. NO. 04-004 AF LUB 122253-640-001 SOURCE: MRB 27.40.00/04 NOTE: ALTERNATIVE TASK 274000-07-1 CAN BE APPLIED. ACCESS PANELS: 314AR Sub 2 - Page 37 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 274000-02-1 ZONE 210 DESCRIPTION TRIMMABLE HORIZONTAL STABILIZER (THS) SKILL TASK CODE CODE AF REV: 07 DATE: 29-Dec-2014 INTERVALS OPC I: 750 FH SOURCE CMR** MRB 8 OPERATIONAL CHECK OF THS ACTUATOR WITH INDIVIDUAL HYDRAULIC SYSTEMS 274000-03-1 210 TRIMMABLE HORIZONTAL STABILIZER (THS) AF OPERATIONAL CHECK OF THS ACTUATOR JAMMING PROTECTION DEVICE 274000-04-1 N 274000-07-1 210 ACCESS PANELS: 312AR TRIMMABLE HORIZONTAL STABILIZER 210 OPERATIONAL CHECK OF THS ACTUATOR WITH ELECTRICAL MOTOR NO 3 TRIMMABLE HORIZONTAL STABILIZER AF AF LUBRICATE THS BEARINGS AND ATTACHMENT FITTINGS WITH GREASE MAT. NO. 04-037 OPC I: 4000 FH OR 80 MO CMR** MRB 8 LUR OPC I: 15000 FH OR 100 MO OPC I: 5500 FH OR 20 MO MRB 9 LUR DET I: 72 MO OR 24000 FH MRB 6 I: 72 MO OR 24000 FH MRB 6 I: 30 MO OR 11000 FH MRB 6 I: 40 MO MRB 6 MRB 9 LUR TPS REFERENCES MEN TASKM. H. APPL 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 ALL 1 1 0.40 0.40 ALL 1 0.20 ALL 1 1 0.10 0.10 ALL 1 0.05 ALL 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 DETAILED INSPECTION OF THS MECHANICAL CONTROL 274100-02-1 145 PREPARATION: CEILING PANELS REMOVED; FLOOR PANELS REMOVED; THS MECHANICAL CONTROL AF FNC CHECK THS MECHANICAL CONTROL CABLES FOR CORRECT TENSION 274100-03-1 120 310 ACCESS PANELS: 241FF THS MECHANICAL CONTROL 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 CHECK POINTER ON TENSION COMPENSATOR SCALE WITHIN LIMITS AF FNC 274100-210-001 SOURCE: MRB 27.40.00/12 274100-220-002 SOURCE: MRB 27.40.00/13 122227-640-007 SOURCE: MRB 27.40.00/20 274100-220-001 SOURCE: MRB 27.40.00/07 ACCESS PANELS: 312AR Sub 2 - Page 38 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 274400-01-1 ZONE 310 DESCRIPTION THS HYDRAULIC ACTUATION SKILL TASK CODE CODE AF FNC 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 AF OPERATIONAL CHECK OF THS ACTUATOR NO-BACK DEVICE 274451-01-1 310 ACCESS PANELS: 312AR THS ACTUATOR AF 274451-02-1 310 AF I: 24000 FH OR 160 MO OPC I: 18000 FH OR 120 MO MRB 9 LUR LUB 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 I: 12000 FH OR 80 MO MRB 6,9 LUR FNC SVC CHECK OIL LEVEL OF THS ACTUATOR GEARBOX 274451-03-1 310 ACCESS PANELS: 312AR THS ACTUATOR AF DET CHECK INDICATOR OF THS ACTUATOR NO-BACK WEAR DETECTION DEVICE 274451-04-1 310 ACCESS PANELS: 312AR THS ACTUATOR DETAILED INSPECTION OF THS ACTUATOR BALL SCREW NUT BODY AND SCREW AND CLAW STOPS AF SOURCE MRB 9 LUR LUBRICATE THS ACTUATOR BALL SCREW NUT ACCESS PANELS: 312AR THS ACTUATOR INTERVALS I: 24000 FH OR 160 MO FUNCTIONAL CHECK OF THS ACTUATOR PRESSURE OFF BRAKE (APPLY TORQUE TO MANUAL CRANKING INPUT) 274400-02-1 REV: 07 DATE: 29-Dec-2014 DET TPS REFERENCES 274454-720-001 MEN TASKM. H. APPL 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 1 0.15 ALL 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 274451-220-001 SOURCE: MRB 27.40.00/09 ACCESS PANELS: 312AR Sub 2 - Page 39 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 274451-05-1 ZONE 310 DESCRIPTION THS ACTUATOR SKILL TASK CODE CODE AF DET DETAILED INSPECTION OF UPPER AND LOWER THS ACTUATOR ATTACHMENT (PRIMARY AND SECONDARY) REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE TPS REFERENCES I: 12000 FH OR 40 MO MRB 6,8 274451-220-002 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 I: 20 MO EASA AD FAA AD ISB MEN TASKM. H. APPL 1 0.15 ALL 1 0.05 ALL 1 0.40 ALL 1 0.10 ALL 1 0.50 ALL 1 3.50 ALL 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 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 274451-10-1 310 ACCESS PANELS: 312AR THS ACTUATOR DETAILED INSPECTION OF THSA LOWER ATTACHMENTS FOR SECONDARY LOAD PATH LOADING 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. AF DET 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 274451-220-003 EASA AD 2008-0150 FAA AD 2007-06-02 ISB 27-1164 ACCESS PANELS: 312AR Sub 2 - Page 40 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 274451-11-1 ZONE 310 DESCRIPTION THS ACTUATOR SKILL TASK CODE CODE REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 310 ACCESS PANELS: 312AR FLAPS 274451-220-004 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 2 0.30 ALL 1 0.10 ALL 1 1 0.40 0.40 ALL AF OPERATIONAL CHECK OF WTB/POB SOURCE: EASA AD OPC I: 7500 FH OR 50 MO CMR** MRB 6,8 LUR 275100-710-001 OPC I: 8000 FH OR 72 MO MRB 8 LUR 275100-710-002 DET CMR** MRB 6,8 LUR NOTE : FLAP SURFACES MOVE AUTOMATICALLY 275100-02-1 210 ACCESS PANELS: 575DB, 575EB, 575FB, 675DB, 675EB, 675FB FLAPS AF OPERATIONAL CHECK OF FLAP INTERCONNECTING STRUT AND FLAP DISCONNECT PROXIMITY SENSORS 275100-03-1 575 675 FLAPS CHECK OF FLAPS TRANSMISSION SHAFTING INTEGRITY, INCLUDING INSPECTION OF SEAL WITNESS DRAINS. 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 APPL EASA AD FAA AD ISB 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. 210 TASKM. H. I: 10 MO DETAILED INSPECTION OF THSA BALL SCREW SHAFT LOWER SPLINES 275100-01-2 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. 274451-12-1 REFERENCES AF DETAILED INSPECTION OF THSA UPPER ATTACHMENTS FOR SECONDARY LOAD PATH LOADING ACCESS PANELS: 312AR THS ACTUATOR TPS AF I: 7500 FH OR 50 MO SOURCE: CMR 275000-00001-1-C MRB 27.50.00/04 MRB 27.50.01/04 SOURCE: MRB 27.50.00/05 MRB 27.50.01/05 275400-210-002 SOURCE: CMR 275000-00001-1-C MRB 27.50.00/04 MRB 27.50.01/04 Sub 2 - Page 41 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 275100-06-1 D 275100-07-1 ZONE 575 675 581 681 DESCRIPTION SKILL TASK CODE CODE REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE TPS REFERENCES MEN TASKM. H. APPL FLAPS AF CHK I: 600 FH SIL 275400-210-005 SIL 27-121 1 1 0.20 0.20 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. FLAPS AF DET I: 5500 FC NOTE SIL 275400-220-006 SIL 27-133 1 1 0.25 0.25 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 1 1 0.40 0.40 ALL VISUAL INSPECTION OF THE INNER FLAP DRIVE TRUNNION CLAMP-TYPE STEEL RUBBING PADS FOR WEAR NOTE: TASK MAY BE ACCOMPLISHED TOGETHER WITH 575221-02-1 IF INTERVAL NOT EXCEEDED. PREPARATION: FLAPS EXTENDED; ACCESS PANELS: 193AB, 193BB, 734, 194AB, 194BB, 744 275144-01-1 580 680 FLAP INTERCONNECTING STRUT DETAILED INSPECTION OF INTERCONNECTING STRUT AND ATTACHMENTS 275400-01-1 570 670 PREPARATION: FLAPS EXTENDED; SLATS FULLY EXTENDED; FLAP TRANSMISSION ASSY AF DET DETAILED INSPECTION OF TRANSMISSION ASSY SOURCE: MRB 27.50.00/06 MRB 27.50.01/06 SOURCE: MRB 27.50.00/08 MRB 27.50.01/08 PREPARATION: FLAPS EXTENDED; SLATS FULLY EXTENDED; 275446-01-1 530 630 ACCESS PANELS: 734 FLAP TRACKS LUBRICATE ALL CARRIAGE ROLLERS ON ALL FLAP TRACKS PREPARATION: FLAPS EXTENDED; SLATS FULLY EXTENDED; AF LUB 275400-200-001 122227-640-004 SOURCE: MRB 27.50.00/02 MRB 27.50.01/02 Sub 2 - Page 42 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 275446-02-1 ZONE 530 630 DESCRIPTION FLAP TRACKS SKILL TASK CODE CODE AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS I: 22000 FH SOURCE MRB 6,9 DETAILED INSPECTION OF TRACKS, ROLLERS AND SPHERICAL BEARINGS (AS FAR AS VISIBLE). D 275449-01-1 575 675 PREPARATION: FLAPS EXTENDED; SLATS FULLY EXTENDED; ACTUATOR ASSEMBLY TPS REFERENCES 275446-200-001 MEN TASKM. H. 1 1 0.30 0.30 APPL ALL SOURCE: MRB 27.50.00/09 AF CHK I: 2400 FH ISB 275400-220-002 ISB 27-1067 ISB 27-1076 1 1 0.50 0.50 AF CHK I: 40 MO ISB 275400-220-001 ISB 27-1067 ISB 27-1076 2 2 1.00 1.00 AF DET I: 2400 FH ISB 275400-210-006 ISB 27-1067 ISB 27-1076 1 1 0.50 0.50 AF LUB I: 72 MO OR 18000 FC OR 24000 FH MRB 6 SIL 122227-640-008 SIL 27-126 1 1 4.00 4.00 I: 72 MO OR 24000 FH MRB 6 1 1 4.00 4.00 CHECK FLAP ROTARY ACTUATOR ASSEMBLY AT TRACK 2 FOR EVIDENCE OF WATER INGRESS. PREPARATION: FLAPS EXTENDED; D 275449-02-1 575 675 ACCESS PANELS: 573AB, 673AB ACTUATOR ASSEMBLY CHECK FLAP ROTARY ACTUATOR ASSEMBLIES AT TRACKS 1, 3 AND 4 FOR EVIDENCE OF WATER INGRESS. PREPARATION: FLAPS EXTENDED; ACCESS PANELS: 575BB, 575CB, 575FB, 575GB, 675BB, 675CB, 675FB, 675GB D 275449-04-1 575 675 ACTUATOR ASSEMBLY DETAILED INSPECTION OF THE INPUT SHAFT OF THE OFFSET GEARBOX AT TRACK N0.1 FOR EVIDENCE OF LATERAL PLAY D 275449-05-1 575 675 PREPARATION: FLAPS EXTENDED; ACTUATOR ASSEMBLY 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 DRAIN AND REFILL FLAP ACTUATOR ASSEMBLIES WITH SEMI-FLUID AF SVC SOURCE: MRB 27.50.00/15 MRB 27.50.01/13 121327-612-005 SOURCE: MRB 27.50.00/13 MRB 27.50.01/12 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 Sub 2 - Page 43 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 275451-01-1 ZONE 147 DESCRIPTION FLAP POWER CONTROL UNIT SKILL TASK CODE CODE AF SVC REV: 07 DATE: 29-Dec-2014 INTERVALS I: 24 MO SOURCE MRB 6 REPLENISH PCU GEARBOX TO CONFIRM FLUID LEVEL 276400-01-1 575 675 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 AF OPERATIONAL CHECK OF WTB/POB 278100-04-1 520 620 SLATS AF 278400-01-1 278451-01-1 147 190 520 620 147 AF REPLENISH PCU GEARBOX TO CONFIRM FLUID LEVEL AF I: 18000 FH OR 120 MO MRB 9 LUR I: 7500 FH OR 48 MO CMR** MRB 6,8 I: 24000 FH OR 80 MO MRB 6 I: 24 MO MRB 6 SVC 121327-612-002 MEN TASKM. H. APPL 1 0.10 ALL 1 1 0.25 0.25 ALL 2 2 1.40 1.40 ALL 1 1 0.10 0.10 ALL 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 SOURCE: MRB 27.50.00/03 MRB 27.50.01/03 122227-640-005 276400-200-001 SOURCE: MRB 27.64.00/03 DET DET REFERENCES SOURCE: MRB 27.64.00/02 CMR** MRB 6,8 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 MRB 9 LUR OPC I: 7500 FH OR 48 MO CHECK OF SLATS TRANSMISSION SHAFTING INTEGRITY, INCLUDING INSPECTION OF SEAL WITNESS DRAINS 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 I: 2000 FH OR 15 MO TPS 278100-710-001 SOURCE: CMR 278000-00001-1-C MRB 27.80.00/04 278400-210-002 SOURCE: CMR 278000-00001-1-C MRB 27.80.00/04 278400-200-001 SOURCE: MRB 27.80.00/03 ACCESS PANELS: 734 Sub 2 - Page 44 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 278468-01-1 ZONE 520 620 DESCRIPTION SLAT TRACKS SKILL TASK CODE CODE AF LUB LUBRICATE ALL TRACK ROLLERS AND PINIONS 278468-02-1 520 620 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 AF DET DETAILED INSPECTION OF SLAT TRACKS, ROLLER BEARINGS, PINION BEARINGS AND CURVED RACK GEARS - AS VISIBLE. REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE I: 20 MO OR 4500 FC MRB 6,9 I: 6 YE OR 22000 FH MRB CPCP MRB 6,9 279000-05-1 281100-01-2 210 190 500 600 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 TANKS AV AF DRAIN WATER CONTENT REFERENCES 122227-640-006 278400-210-001 TASKM. H. APPL 1 1 0.50 0.50 ALL 1 1 1.00 1.00 ALL 2 0.40 ALL 1 1 1 0.10 0.10 0.10 ALL 1 0.05 ALL 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 OPC I: 400 FH OR 80 DY CMR* MRB 8 LUR 279600-710-018 SVC MRB 9 123228-281-001 I: 36 HR NOTE MEN SOURCE: MRB 27.80.00/02 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) TPS SOURCE: CMR 279000-00001-1-C MRB 27.90.00/02 MRB 27.90.00/05 SOURCE: MRB 28.11.00/01 NOTE: DEPENDING ON OPERATING ENVIRONMENTAND OPERATORS EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED. 281100-02-1 196 ACCESS PANELS: 195BB, 196BB TANKS CHECK LEAK MONITOR FOR EVIDENCE OF FUEL LEAKAGE AND CORRECT CLOSURE OF THE VALVE AF OPC I: 750 FH OR 6 MO MRB 9 LUR 281100-200-002 SOURCE: MRB 28.11.00/02 MRB 28.13.00/02 MRB 28.21.00/01 MRB 28.25.00/01 Sub 2 - Page 45 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 281100-04-2 281142-01-1 ZONE 190 500 600 540 640 DESCRIPTION TANKS SKILL TASK CODE CODE INTERVALS AF SVC AF OPC I: 160 MO SAMPLE FUEL FOR MICROBIOLOGICAL CONTAMINATION ANALYSIS NOTE : INTERVAL DEPENDING ON EACH INDIVIDUAL OPERATOR´S ENVIRONMENT MPD INTERVAL IS: NOTE TANK FLAP VALVES REV: 07 DATE: 29-Dec-2014 I: 24 MO NOTE SOURCE TPS REFERENCES MEN TASKM. H. APPL SIL 123228-281-003 SIL 28-079 1 1 1 0.10 0.10 0.10 MRB 9 281100-200-001 2 2 0.10 0.10 ALL 1 1 0.10 0.10 ALL 1 1 0.02 0.02 ALL CHECK FOR FULL AND FREE MOVEMENT OF CLACK VALVES 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 1 1 0.10 0.10 ALL 1 1 1.00 1.00 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 AF OPERATIONAL CHECK OF INDIVIDUAL TRANSFER VALVES TO ENSURE VALVE SHAFT ROTATES VALVE TO OPEN POSITION 281600-01-1 281800-01-1 471 481 137 138 FUEL RECIRCULATION COOLING OPERATIONAL CHECK OF PYLON CHECK VALVE TO ENSURE VALVE NOT FAILED OPEN IGNITION PREVENTION FUNCTIONAL CHECK OF TANK VAPOUR SEAL AND VENT DRAIN SYSTEM (SFAR88) PREPARATION: FOR PRE 21003 - 241AF OR 131NW,FOR POST 21003 - 131NW, 132PW(REMOVE POTABLE WATER TANK); AF AF OPC I: 7500 FH OR 50 MO CMR** MRB 8 LUR OPC I: 7500 FH MRB 8 FNC I: 24000 FH OR 72 MO FAL MRB 8 SOURCE: CMR 281500-00001-1-C MRB 28.15.00/02 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 Sub 2 - Page 46 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 281800-02-1 ZONE 191 192 DESCRIPTION IGNITION PREVENTION SKILL TASK CODE CODE AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS I: 72 MO SOURCE 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 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. H. APPL 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 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 AF GVI I: 72 MO MRB 9 GENERAL VISUAL INSPECTION OF CENTER TANK FWD CARGO BAY ISOLATION MATS (SFAR88) 281800-06-1 145 146 ACCESS PANELS: 131NW, 131PW, 132PW IGNITION PREVENTION GENERAL VISUAL INSPECTION OF WIRING HARNESSES ABOVE CENTER TANK (SFAR88) 281852-210-001 SOURCE: MRB 28.18.00/05 AF GVI I: 144 MO MRB 9 281842-210-001 SOURCE: MRB 28.18.00/06 PREPARATION: FLOOR PANELS FROM FR 36 TO FR 46; Sub 2 - Page 47 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 281800-07-1 281800-08-1 ZONE 520 570 620 670 540 640 DESCRIPTION IGNITION PREVENTION SKILL TASK CODE CODE AF GVI REV: 07 DATE: 29-Dec-2014 INTERVALS I: 144 MO SOURCE MRB 9 GENERAL VISUAL INSPECTION OF WING LEADING EDGE AND TRAILING EDGE ELECTRICAL WIRING AND CONNECTIONS (SFAR88) 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 IGNITION PREVENTION 282100-01-1 282100-02-1 282100-03-1 282100-04-1 140 540 640 PREPARATION: FUEL PUMP FAIRINGS; IGNITION PREVENTION AF GVI I: 144 MO MRB 9 210 140 OPERATIONAL CHECK OF WING TANK PUMP PRESSURE SENSE LINE CHECK VALVES MAIN FUEL PUMP SYSTEM 210 OPERATIONAL CHECK OF CENTER TANK PUMP CANISTER CHECK VALVES MAIN FUEL PUMP SYSTEM 210 OPERATIONAL CHECK OF AIR RELEASE VALVES TO ENSURE ADEQUATE FUEL FLOW UNDER SUCTION FEED CONDITIONS MAIN FUEL PUMP SYSTEM OPERATIONAL CHECK TO ENSURE THAT BOTH CENTER TANK PUMPS FEED FOR 2 MINUTES AFTER ENGINE START 281841-210-001 MEN TASKM. H. APPL 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 282100-710-002 1 0.10 ALL SOURCE: MRB 28.21.00/04 282100-710-003 2 0.10 ALL SOURCE: MRB 28.21.00/05 282100-710-008 1 0.10 ALL SOURCE: MRB 28.21.00/08 282100-710-005 2 1.00 ALL 281843-210-001 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 MAIN FUEL PUMP SYSTEM REFERENCES SOURCE: MRB 28.18.00/07 GENERAL VISUAL INSPECTION OF WING FUEL PUMP ELECTRICAL CONNECTIONS AND UNDERWING ELECTRICAL SUPPLY CABLE (SFAR88) 281800-09-1 TPS 281851-210-001 SOURCE: MRB 28.18.00/09 AF AF AF AF OPC I: 24000 FH OPC I: 15000 FH OR 100 MO OPC I: 15000 FH OR 100 MO OPC I: 6500 FH MRB 9 MRB 8 LUR MRB 8 LUR CMR** MRB 8 SOURCE: CMR 282100-00001-1-C MRB 28.21.00/03 Sub 2 - Page 48 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 282100-05-1 ZONE 410 420 520 620 DESCRIPTION FUEL PUMP SYSTEM SKILL TASK CODE CODE 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 REV: 07 DATE: 29-Dec-2014 INTERVALS I: 7500 FH OR 50 MO SOURCE MRB 9 LUR TPS REFERENCES 282100-790-002 MEN TASKM. H. APPL 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 1 0.10 1654 1679 2465 2497 2930 2964 3044 2879 2913 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 CHECK SUCTION VALVES FOR FULL AND FREE MOVEMENT 282100-07-1 470 480 MAIN FUEL PUMP SYSTEM AF 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 AF 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 AF OPERATIONAL CHECK OF LP SHUT OFF VALVES AND THEIR CONTROLS TO ENSURE NO FLOW WHEN SELECTED CLOSED WITH BOOSTER PUMP ON 282541-01-1 622 NOTE: TASK MAY BE PERFORMED AT OPPORTUNITY OF ENGINE REMOVAL PROVIDED INTERVAL NOT EXCEEDED COUPLING REFUEL/DEFUEL DETAILED INSPECTION OF COUPLING REFUEL/DEFUEL. ACCESS PANELS: 622HB AF OPC I: 24000 FH OR 160 MO DIS I: 80 MO OR 24000 FH OR 18000 FC OPC I: 750 FH MRB 9 LUR SIL MRB 9 OPC I: 7500 FH OR 50 MO MRB 8 LUR OPC I: 15000 FH OR 100 MO NOTE MRB 8 LUR DET MRB 6 I: 5000 FC 282100-280-001 SOURCE: MRB 28.23.00/01 282400-790-003 SOURCE: MRB 28.24.00/01 MRB 28.24.00/02 282541-200-001 SOURCE: MRB 28.25.00/02 Sub 2 - Page 49 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 282541-01-2 ZONE 522 622 DESCRIPTION COUPLING REFUEL/DEFUEL SKILL TASK CODE CODE AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS I: 5000 FC SOURCE MRB 6 DETAILED INSPECTION OF COUPLING REFUEL/DEFUEL. 282900-02-1 210 ACCESS PANELS: 522HB, 622HB APU LOW PRESSURE FUEL SHUT OFF 435 445 ACCESS PANELS: 315AL HYDRAULIC POWER AF AF OPC I: 24000 FH OR 160 MO MRB 9 LUR VCK I: 1000 FH OR 12 MO MRB 9 LUR I: 1000 FH OR 12 MO MRB 9 LUR I: 24 MO SIL 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 AF VCK 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 290000-07-1 100 ACCESS PANELS: 195BB, 196BB, 197CB, 197FB, 734 HYDRAULIC SYSTEM SEALS REFERENCES 282541-200-001 MEN TASKM. H. APPL 1 1 0.10 0.10 1753 1 0.20 ALL 1 1 0.02 0.02 ALL 1 0.06 ALL 1 0.33 ALL SOURCE: MRB 28.25.00/02 OPERATIONAL CHECK OF APU LP FUEL VALVE FOR EVIDENCE OF INTERNAL LEAKAGE WITH LEFT WING TANK PUMP ON 290000-02-1 TPS AF VCK 282900-710-002 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 291000-200-025 SIL 29-064 VISUAL CHECK OF HIGH AND LOW PRESSURE MANIFOLDS AND GROUND SERVICE PANELS AND MANIFOLDS FOR SIGNS OF EXTERNAL LEAKAGE. 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. Sub 2 - Page 50 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 291000-01-1 ZONE 100 DESCRIPTION MAIN HYDRAULIC POWER SKILL TASK CODE CODE AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS I: 8 DY SOURCE MRB 6 LUR CHECK FLUID LEVEL ON RESERVOIR INDICATORS 291000-02-1 100 ACCESS PANELS: 196BB, 197FB, 744 MAIN HYDRAULIC POWER 210 ACCESS PANELS: 196BB, 197FB, 744 MAIN HYDRAULIC POWER AF DET I: 750 FH OR 6 MO MRB 6 LUR AF I: 22000 FH OR 144 MO I: 2250 FH OR 24 MO MRB 6 LUR I: 7500 FH OR 50 MO FNC I: 36000 FH OR 144 MO OPC I: 10000 FH OR 72 MO MRB 6 LUR FNC MRB 8 LUR 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 FUNCTIONAL CHECK OF PTU YELLOW TO GREEN 291000-08-1 291000-09-1 210 MAIN HYDRAULIC POWER 210 FUNCTIONAL CHECK OF PRIORITY VALVES IN GREEN, BLUE AND YELLOW SYSTEM MAIN HYDRAULIC POWER AF AF 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 FUNCTIONAL CHECK OF HYDRAULIC FIRE SHUT OFF VALVES REFERENCES 291000-200-001 MEN TASKM. H. APPL 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 SOURCE: MRB 29.10.00/19 291000-710-001 1 0.10 ALL 2 2 0.20 0.20 ALL SOURCE: MRB 29.10.00/01 CHECK RESERVOIR AIR PRESSURE ON RESERVOIR GAUGE 291000-04-1 TPS AF FNC I: 16000 FH OR 144 MO 291000-200-002 SOURCE: MRB 29.10.00/02 MRB 9 LUR SOURCE: MRB 29.10.00/13 MRB 6,8 MRB 8 LUR 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 ACCESS PANELS: 574AB, 674AB Sub 2 - Page 51 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 291000-14-1 ZONE 100 DESCRIPTION MAIN HYDRAULIC POWER SKILL TASK CODE CODE 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 ENVIRONMENTAND OPERATORS EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED. 291000-18-1 148 ACCESS PANELS: 734, 744 MAIN HYDRAULIC POWER 291000-19-1 210 AF EL OPERATIONAL CHECK OF PTU INHIBITION LOGIC 291000-20-1 210 ACCESS PANELS: 196BB, 734, 744 MAIN/AUXILIARY POWER INTERVALS SOURCE I: 600 FH OR 6 MO MRB 9 LUR I: 7500 FH OR 24 MO NOTE MRB 9 SIL 291900-01-1 291900-02-1 210 BLUE MAIN HYDRAULIC POWER 210 FUNCTIONAL CHECK OF BLUE ELECTRICAL PUMP PRESSURE BY READING ECAM INDICATION GROUND INTERNAL LEAK TEST SYSTEM 210 FUNCTIONAL CHECK TO MONITOR INTERNAL LEAK RATE OF YELLOW AND GREEN HYDRAULIC SYSTEMS GROUND INTERNAL LEAK TEST SYSTEM FUNCTIONAL CHECK TO MONITOR INTERNAL LEAK RATE OF BLUE HYDRAULIC SYSTEM REFERENCES 291000-200-008 SIL 29-092 MEN TASKM. H. APPL 1 0.10 ALL 1 0.30 ALL 1 0.30 ALL 1 0.75 2930 2964 3044 2879 2913 291000-710-004 1 0.25 ALL SOURCE: MRB 29.10.00/36 291200-710-001 1 0.05 ALL SOURCE: MRB 29.10.00/10 291000-220-001 2 0.40 ALL SOURCE: MRB 29.10.00/18 291000-220-002 2 0.30 ALL SOURCE: MRB 29.10.00/22 SVC I: 1500 FH OR 12 MO MRB 9 LUR 123229-281-001 JIC A320-29-10-00 SIL 29-081 OPC I: 7500 FH OR 50 MO MRB 9 LUR AF OPC I: 24 MO MRB 9 AF AF AF FNC FNC FNC I: 7500 FH OR 50 MO I: 24000 FH OR 144 MO I: 7500 FH OR 50 MO 291700-680-001 SOURCE: MRB 29.10.00/32 292300-710-006 SOURCE: MRB 29.10.00/35 OPERATIONAL CHECK OF EDP DEPESSURIZATION 291200-01-1 TPS SOURCE: MRB 29.10.00/23 DRAIN RECOVERY TANK ACCESS PANELS: 734, 744 MAIN/AUXILIARY POWER REV: 07 DATE: 29-Dec-2014 MRB 6 LUR MRB 6,9 CMR* MRB 8 LUR SOURCE: CMR 291000-00003-1-C MRB 29.10.00/05 MRB 29.10.00/12 Sub 2 - Page 52 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 292000-01-1 ZONE 190 DESCRIPTION AUXILIARY HYDRAULIC POWER SKILL TASK CODE CODE AF FNC 210 ACCESS PANELS: 195BB, 196BB, 197EB, 197FB AUXILIARY HYDRAULIC POWER AF OPERATIONAL CHECK OF RAM AIR TURBINE (RAT) AUTOMATIC DEPLOYMENT 292000-04-1 190 ACCESS PANELS: 197EB AUXILIARY HYDRAULIC POWER AF 292000-05-1 210 AF OPERATIONAL CHECK OF RAM AIR TURBINE (RAT) AUTOMATIC DEPLOYMENT 292000-07-1 190 ACCESS PANELS: 197EB AUXILIARY HYDRAULIC POWER AF SOURCE CMR* MRB 8 OPC I: 3600 FH OR 18 MO CMR* MRB 8 FNC I: 3600 FH OR 18 MO CMR* MRB 8 OPC I: 3600 FH OR 18 MO CMR* MRB 8 FNC MRB 8 OPERATIONAL CHECK OF RAT MANUAL DEPLOYMENT AND FUNCTIONAL CHECK OF RAT USING GROUND TEST UNIT, FOLLOWED BY CHECK OF FILTER INDICATOR ACCESS PANELS: 195BB, 197EB AUXILIARY HYDRAULIC POWER INTERVALS I: 1500 FH OR 8 MO OPERATIONAL CHECK OF RAT MANUAL DEPLOYMENT AND FUNCTIONAL CHECK OF RAT USING GROUND TEST UNIT, FOLLOWED BY CHECK OF FILTER INDICATOR D 292000-02-1 REV: 07 DATE: 29-Dec-2014 I: 72 MO 195 ACCESS PANELS: 197EB RAM AIR TURBINE REFERENCES 292200-720-001 MEN TASKM. H. 2 1.40 2 0.10 292200-720-003 2 1.00 SOURCE: CMR 291000-00001-2-C CMR 291000-00001-3-C MRB 24.50.00/10 MRB 29.10.00/29 292200-710-006 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 2 0.10 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 2 0.10 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1 0.30 1 0.30 292200-710-001 SOURCE: CMR 291000-00002-1-C MRB 29.10.00/08 SOURCE: CMR 291000-00002-1-C MRB 29.10.00/08 292200-280-002 SOURCE: MRB 29.10.00/27 AF DET I: 16 MO APPL SOURCE: CMR 291000-00001-1-C MRB 24.50.00/03 MRB 29.10.00/07 FUNCTIONAL CHECK OF ANTI-ICING DEVICE MAGNETS D 292251-01-1 TPS MRB 8 DETAILED INSPECTION OF RAT ASSEMBLY AND DOORS IN DEPLOYED POSITION 292251-210-001 SOURCE: MRB 29.10.00/33 PREPARATION: RAM AIR TURBINE EXTENSION; 292251-02-1 195 ACCESS PANELS: 195BB, 197EB RAM AIR TURBINE DETAILED INSPECTION OF RAT ASSEMBLY AND DOORS IN DEPLOYED POSITION AF DET I: 20 MO MRB 8 292251-200-003 SOURCE: MRB 29.10.00/09 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 PREPARATION: RAM AIR TURBINE EXTENSION; ACCESS PANELS: 195BB, 197EB Sub 2 - Page 53 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 293100-01-1 ZONE 190 DESCRIPTION HYDRAULIC FLUID QUANTITY INDICATING SKILL TASK CODE CODE AF FNC REV: 07 DATE: 29-Dec-2014 INTERVALS I: 24000 FH SOURCE MRB 9 FUNCTIONAL CHECK OF RESERVOIR LOW LEVEL WARNING 293400-01-1 301151-01-2 210 522 622 ACCESS PANELS: 197CB, 197EB, 198CB RESERVOIR PRESSURIZATION INDICATING OPERATIONAL CHECK OF RESERVOIR LOW AIR PRESSURE WARNING WING ANTI-ICE CONTROL VALVE 210 ACCESS PANELS: 522AB, 622AB ENGINE AIR INTAKE ICE PROTECTION AF AF OPC I: 7500 FH OR 50 MO DIS I: 22000 FH MRB 9 LUR MRB 6 302149-01-1 438 448 DETAILED INSPECTION OF INLET COWL ANTI-ICE SUPPLY DUCTS AND ASSOCIATED HARDWARE IN THE CORE COMPARTMENT 293100-710-001 MEN TASKM. H. APPL 1 0.30 ALL 293400-710-001 1 0.10 ALL SOURCE: MRB 29.30.00/04 301151-960-001 1 1 0.50 0.50 ALL 1 0.30 ALL 1 1 0.20 0.20 ALL SOURCE: MRB 30.11.00/03 AF OPC I: 48 MO MRB 9 OPERATIONAL CHECK OF ENGINE ANTI-ICE SYSTEM FAULT WARNING ACCESS PANELS: 438AR, 448AR ENGINE AIR INTAKE ANTI-ICE DUCT REFERENCES SOURCE: MRB 29.30.00/05 REPLACE WING ANTI-ICING FILTER 302100-01-1 TPS 302100-710-001 SOURCE: MRB 30.21.00/02 AF DET I: 6000 FH OR 40 MO MRB 6 LUR 302149-200-001 SOURCE: MRB 30.21.00/01 ACCESS PANELS: 438AR, 452AR, 448AR, 462AR Sub 2 - Page 54 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 313000-01-1 ZONE 210 DESCRIPTION CFDS AND DATA RECORDING SYSTEM SKILL TASK CODE CODE AV READ CENTRALIZED FAULT DISPLAY SYSTEM (CFDS) FOR CLASS 3 FAULTS R 313300-01-1-SDM 120 SOLID STATE FLIGHT DATA RECORDER (SSFDR) AV REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE OPC I: 750 FH OR 6 MO MRB 9 LUR SVC SPECI I: 24 MO TPS REFERENCES MEN TASKM. H. APPL 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 Sub 2 - Page 55 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 313300-03-1 ZONE 312 DESCRIPTION DFDR SYSTEM INTERCONNECTION SKILL TASK CODE CODE AV OPERATIONAL CHECK OF ULB REV: 07 DATE: 29-Dec-2014 INTERVALS OPC 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 R 316000-01-1 R 316000-02-1 210 210 210 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) 210 OPERATIONAL CHECK OF DMC3 POWER SUPPLY TRANSFER WHEN BUSBAR 101XP IS LOST ELECTRONIC INSTRUMENT SYSTEM 210 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 ELECTRONIC INSTRUMENT SYSTEM PERFORM ELECTRONIC INSTRUMENT SYSTEM (EIS) INPUT TEST REFERENCES 313300-710-015 CMM 31-31-36 CMM 31-30-40 MEN TASKM. H. APPL 1 0.15 ALL 313300-710-006 1 0.10 ALL SOURCE: MRB 31.33.00/05 316000-740-005 1 0.20 2465 2497 2930 2964 3044 2879 2913 1 0.40 2465 2497 2930 2964 3044 2879 2913 1 0.20 2465 2497 2930 2964 3044 2879 2913 1 0.30 1654 1679 1753 1 0.15 1654 1679 1753 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 EL OPC I: 7500 FH OR 50 MO MRB 9 LUR OPC I: 7500 FH OR 50 MO MRB 9 LUR OPC I: 7500 FH OR 50 MO MRB 9 LUR OPC I: 6000 FH OR 48 MO MRB 9 LUR OPC I: 7500 FH OR 50 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 316000-740-002 SOURCE: MRB 31.60.00/02 Sub 2 - Page 56 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 316322-01-1 R 316322-02-1 ZONE DESCRIPTION SKILL TASK CODE CODE 321000-01-1 INTERVALS SOURCE 321100-15-1 MEN TASKM. H. APPL EL SIL LUR 316322-400-002 JIC A320-31-63-00 SIL 31-025 1 0.25 1654 1679 1753 210 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 DISPLAY UNIT CHK I: 2400 FH OR 24 MO NOTE AF FNC SIL LUR 316322-200-001 SIL 31-030 1 0.25 1654 1679 1753 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 TBD ALL 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 SOURCE: MRB 32.11.00/02 MRB 32.11.00/18 MRB 32.30.00/03 122232-640-001 1 1 0.20 0.20 ALL 711 731 741 731 741 ACCESS PANELS: 734, 744 D 321100-03-1 REFERENCES DISPLAY UNIT LUBRICATION OF MAIN LANDING GEAR AND DOORS 321000-01-2-SDM TPS 210 FUNCTIONAL CHECK OF DISPLAY UNITS BRIGHTNESS NOTE : INTERVAL MAY BE ADJUSTED IN ACCORDANCE WITH OPERATOR EXPERIENCE 320000-01-1-SDM REV: 07 DATE: 29-Dec-2014 731 741 731 741 731 741 MLG LUBRICATION AF LUB I: 8 DY SPECI MLG LOWER BEARING 3 POINTS LUBRICATION MAIN LANDING GEAR AF SVC SIL 321143-600-001 SB 32-1158 SIL 32-078 1 1 0.70 0.70 APPLY TEMPORARY PROTECTION TO THE END FITTINGS OF THE MAIN LANDING GEAR ELECTRICAL HARNESS CONDUITS. MAIN GEAR I: 24 MO OR 7500 FH AF SDI I: 20000 FC OR 120 MO MRB 5,8 321100-220-006 0 0 N/A N/A ALL SPECIAL DETAILED INSPECTION OF BUSHINGS AND BEARINGS IN MLG AIRFRAME ATTACHMENT FITTINGS SOURCE: MRB 32.11.00/15 PREPARATION: AIRCRAFT JACKING; MAIN LANDING GEAR REMOVAL; 321101-01-3-SDM 731 741 321111-03-1 731 741 ACCESS PANELS: 734, 744 MLG SLIDING TUBE (CHROME EXTERNAL FASE) AF DET 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 LANDING GEAR AF FNC I: 1500 FC OR 18 MO MRB 6,9 LUR 321111-200-001 1 1 0.10 0.10 ALL CHECK OF MLG TORQUE LINK DAMPER FLUID LEVEL SOURCE: MRB 32.11.00/13 Sub 2 - Page 57 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 321113-03-1 ZONE 731 741 DESCRIPTION MAIN LANDING GEAR SHOCK ABSORBER SKILL TASK CODE CODE AF FNC CHECK OF MLG SHOCK ABSORBER FLUID LEVEL 321113-04-1 731 741 PREPARATION: AIRCRAFT JACKING; MAIN LANDING GEAR SHOCK ABSORBER AF FNC CHECK OF MLG SHOCK ABSORBER CHARGE PRESSURE 321127-01-1 731 741 MAIN LANDING GEAR TORQUE LINK AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 710 NOSE LANDING GEAR AND DOORS AF LUB LUBRICATION OF NOSE LANDING GEAR AND DOORS REFERENCES I: 10000 FC OR 80 MO MRB 6 121232-611-004 I: 5000 FC OR 24 MO I: 10000 FC MRB 6 121432-614-003 MRB 6 SOURCE: MRB 32.11.00/03 321127-200-001 I: 4 MO OR 500 FC TASKM. H. APPL 1.00 1.00 ALL 1 1 0.40 0.40 ALL 1 1 0.20 0.20 ALL MRB 5,8 SOURCE: MRB 32.11.00/05 122232-640-002 2 0.50 ALL 1 0.20 ALL 0 N/A ALL 1 0.40 ALL 1 0.60 ALL 1 1.50 1654 1679 1753 2465 SOURCE: MRB 32.11.00/04 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 I: 5000 FC OR 24 MO MRB 6 I: 5000 FC ISB MRB 6 ACCESS PANELS: 713, 714 SPECIAL DETAILED INSPECTION OF BUSHINGS AND BEARINGS IN NLG AIRFRAME ATTACHMENT FITTINGS. MEN 2 2 CHECK OF MLG TORQUE LINKS FOR EXCESSIVE PLAY 322000-01-1 TPS SOURCE: MRB 32.21.00/07 PREPARATION: NLG REMOVED; AIRCRAFT JACKING; 322113-01-1 711 ACCESS PANELS: 713, 714 NOSE LANDING GEAR SHOCK ABSORBER 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 121232-610-002 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 INSPECTION FOR BARREL WEAR SOURCE: MRB 32.21.00/02 AF GVI I: 4500 FC OR 20 MO ISB JIC A320-32-21-00 ISB 32-1323 Sub 2 - Page 58 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 323000-01-1 323000-16-1 R 323000-17-1 ZONE 711 731 741 711 731 741 210 DESCRIPTION NORMAL EXTENSION AND RETRACTION VISUAL CHECK OF NLG AND MLG DOWNLOCK SPRINGS AND ATTACHMENTS. NORMAL EXTENSION AND RETRACTION SKILL TASK CODE CODE AF AF 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 323100-02-1 323100-03-1 711 731 741 210 711 731 741 210 NORMAL EXTENSION AND RETRACTION AF 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) NORMAL EXTENSION AND RETRACTION EL AF DETAILED INSPECTION OF GEAR UPLOCK AND DOOR UPLOCK UNITS AND ROLLERS. ACCESS PANELS: 713, 714, 734, 744 NORMAL EXTENSION AND RETRACTION AF OPERATIONAL CHECK OF RETRACTION INHIBITION BAULK 323100-04-1 210 GVI NORMAL EXTENSION AND RETRACTION OPERATIONAL CHECK TO ENSURE SAFETY VALVE CLOSES AT 260 KTS AF REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE TPS REFERENCES 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 SOURCE: MRB 32.30.00/16 MRB 32.30.00/18 MRB 6 LUR MRB 9 LUR DET MRB 5,8 OPC I: 18000 FC OR 144 MO OPC I: 15000 FH OR 72 MO SOURCE: MRB 32.30.00/17 323100-210-002 SOURCE: MRB 32.30.00/19 OPC I: 750 FH OR 6 MO I: 3500 FC OR 24 MO 323100-720-008 326900-740-001 MEN TASKM. H. APPL 1 1 1 0.02 0.02 0.02 ALL 1 1 1 0.50 0.50 0.50 ALL 1 0.18 1753 2465 2930 2964 3044 1 1 1 0.80 0.80 0.80 ALL 1 0.10 ALL 1 1 1 0.60 0.60 0.60 ALL SOURCE: MRB 32.30.00/02 323100-200-001 SOURCE: MRB 32.30.00/07 MRB 9 323100-710-001 2 0.10 ALL MRB 8 SOURCE: MRB 32.30.00/11 323100-710-005 2 0.40 ALL SOURCE: MRB 32.30.00/12 PREPARATION: APU RUNNING; Sub 2 - Page 59 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 323100-05-1 ZONE 120 DESCRIPTION NORMAL EXTENSION AND RETRACTION SKILL TASK CODE CODE AF DET DETAILED INSPECTION OF NOSE GEAR DOOR OPERATING MECHANISM 210 ACCESS PANELS: 713, 714 NORMAL EXTENSION AND RETRACTION R 323100-07-1 210 BITE CHECK USING MCDU TO ENSURE "GEAR NOT DOWN FOR LANDING" WARNINGS OPERATIVE NORMAL EXTENSION AND RETRACTION EL D 323105-03-1 210 OPERATIONAL CHECK TO ENSURE SAFETY VALVE CLOSURE NORMAL EXTENSION AND RETRACTION 323100-06-1 AF 711 SELECTOR VALVE - LG R 323300-01-1 100 200 DETAILED INSPECTION OF FREE-FALL MECHANISM INCLUDING CABLES I: 5000 FC OR 24 MO SOURCE MRB 5 TPS REFERENCES 323000-200-001 MEN TASKM. H. APPL 1 0.30 ALL 1 0.10 ALL 2 0.10 1654 1679 SOURCE: MRB 32.30.00/06 MRB 9 LUR AF VCK T: 800 FC I: 8 DY AOT EASA AD JIC A320-32-31-05 AOT 32A1390 EASA AD 2011-0069 1 0.75 AF VCK T: REFER TO ISB / AD I: 20000 FC OR 89 MO EASA AD ISB JIC A320-32-31-00 EASA AD 2007-0065 ISB 32-1290 1 0.50 AF DET I: 72 MO MRB 8 323300-200-002 1 1 0.50 0.50 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 OPC I: 7500 FH OR 50 MO OPC I: 15000 FH CHECK CFDS (PFR) FOR SLOW DOOR OPENING/CLOSING MESSAGES D 323112-01-1 REV: 07 DATE: 29-Dec-2014 ISB 326100-710-001 SOURCE: MRB 32.30.00/05 323100-710-008 ISB 32-1225 2930 2964 3044 SOURCE: MRB 32.30.00/09 ACCESS PANELS: 131AC, 131BC, 131CC, 132PW, 241EF, 241FF, 241KF, 241LF, 241MF, 242FF, 242KF, 242LF, 242MF, 713, 714, 734, 744, 822, 824, 825, 211FF, 211JF Sub 2 - Page 60 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 323300-01-2 ZONE 100 200 DESCRIPTION LANDING GEAR FREE FALL EXTENSION SKILL TASK CODE CODE AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS I: 72 MO SOURCE MRB 8 DETAILED INSPECTION OF FREE-FALL MECHANISM INCLUDING CABLES 323300-03-1 700 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 AF FNC I: 15000 FC OR 80 MO MRB 8 ACCESS PANELS: 713, 714 LANDING GEAR FREE FALL EXTENSION AF FNC I: 72 MO MRB 8 CHECK OF FREE-FALL MECHANISM CABLE TENSION 323300-05-1 210 ACCESS PANELS: 131AC, 241EF, 242FF, 242LF, 713, 714, 734, 744, 822, 825 LANDING GEAR FREE FALL EXTENSION 324000-17-1 210 730 744 190 ACCESS PANELS: 713714734, 744 WHEELS AND BRAKES AF OPC I: 24 MO AF FNC AF FNC FUNCTIONAL CHECK OF BRAKE ACCUMULATOR SYSTEM. 324100-01-1 700 WHEELS MRB 8 AF FNC I: 5000 FC OR 48 MO MRB 8 731 741 LANDING GEAR WHEELS AND BRAKES DETAILED INSPECTION OF THE NORMAL BRAKE MANIFOLD 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 4 0.60 ALL 1 0.05 ALL 4 0.40 ALL 2 2 2 1.50 1.50 1.50 ALL 1 0.50 ALL 324100-210-003 1 0.10 ALL SOURCE: MRB 32.40.00/01 JIC A320-32-42-00 ISB 32-1282 1 1 3.00 3.00 2465 2497 323300-720-003 323300-200-001 323300-710-001 I: 5000 FC OR 7500 FH OR 50 MO I: 3 DY MRB 9 LUR AF DET T: 7500 FC I: 2000 FC 324200-720-004 SOURCE: MRB 32.40.00/14 324400-720-002 SOURCE: MRB 32.40.00/17 MRB 6,9 CHECK TIRE PRESSURE R 324200-03-1 APPL SOURCE: MRB 32.30.00/08 FUNCTIONAL CHECK OF THE AUTOMATIC REACTIVATION OF THE NORMAL BRAKING MODE (PARKING BRAKE APPLIED) PREPARATION: HYDRAULIC GROUND POWER; WHEELS AND BRAKES TASKM. H. SOURCE: MRB 32.30.00/15 OPERATIONAL CHECK OF FREE-FALL MECHANICAL CONTROL 324000-14-1 323300-200-002 MEN SOURCE: MRB 32.11.00/17 MRB 32.21.00/08 MRB 32.30.00/13 PREPARATION: AIRCRAFT JACKING; 100 REFERENCES SOURCE: MRB 32.30.00/09 FUNCTIONAL CHECK OF FREE-FALL SYSTEM 323300-04-1 TPS ISB PREPARATION: MLG FIXED LEG FAIRING; Sub 2 - Page 61 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 324227-01-1 ZONE 731 741 DESCRIPTION MAIN LANDING GEAR BRAKES SKILL TASK CODE CODE AF FNC FUNCTIONAL CHECK OF BRAKE HEAT PACK FOR WEAR BY USE OF THE WEAR INDICATOR (PARKING BRAKE APPLIED) R 324300-01-1 210 NOTE : DEPENDING ON OPERATORS EXPERIENCE, A HIGHER INITIAL INTERVAL MAY BE USED. ALTERNATE BRAKING SYSTEM AF OPERATIONAL CHECK OF ALTERNATE BRAKING SYSTEM 324300-01-3 210 NOTE: TASK MAY BE ACCOMPLISHED AT BRAKE CHANGE. ALTERNATE BRAKING SYSTEM AF OPERATIONAL CHECK OF ALTERNATE BRAKING SYSTEM 324300-02-1 210 NOTE: TASK MAY BE ACCOMPLISHED AT BRAKE CHANGE. ALTERNATE BRAKING SYSTEM AF REV: 07 DATE: 29-Dec-2014 INTERVALS I: 36 HR NOTE SOURCE MRB 6 122 LOW PRESSURE BRAKE RESERVOIR AF OPC I: 6000 FH OR 40 MO CMR* MRB 9 LUR OPC I: 7500 FH OR 50 MO MRB 9 LUR OPC I: 10000 FC MRB 9 FNC CHECK FLUID LEVEL OF LOW PRESSURE BRAKE RESERVOIR R 324314-01-1 148 ACCESS PANELS: 811 ALTERNATE BRAKE DIST. - DUAL VALVE AF RST 148 ACCESS PANELS: 148FB, 734, 744 BRAKE ACCUMULATOR 148 ACCESS PANELS: 744 PARKING/ULTIMATE EMERGENCY BRAKING SYSTEM OPERATIONAL CHECK OF THE PARKING BRAKE SYSTEM TASKM. H. APPL 1 1 0.02 0.02 ALL 324300-710-802 1 0.20 1654 1679 1753 SOURCE: CMR 324000-00001-1-C MRB 32.40.00/08 324300-710-802 1 0.20 2465 2497 2930 2964 3044 2879 2913 324200-710-003 1 0.10 ALL SOURCE: MRB 32.40.00/09 324311-210-001 I: 1500 FC OR 18 MO MRB 6 LUR 1 0.02 1654 1679 1753 I: 13 MO MRB 6 1 0.20 1654 1679 1753 1 0.02 ALL 1 0.20 ALL SOURCE: MRB 32.40.00/06 324314-200-002 SOURCE: MRB 32.40.00/12 AF FUNCTIONAL CHECK OF PARKING/EMERGENCY BRAKE ACCUMULATOR BY READING THE CHARGE PRESSURE ON THE ACCUMULATOR GAUGE 324500-01-1 324227-210-003 MEN SOURCE: MRB 32.40.00/08 DRAIN ACCUMULATED WATER FROM THE BRAKE DUAL DISTRIBUTION VALVE (BDDV) 324411-01-1 REFERENCES SOURCE: MRB 32.40.00/02 OPERATIONAL CHECK OF ANTISKID INHIBITION R 324311-01-1 TPS AF FNC I: 750 FH OR 4 MO OPC I: 2000 FC OR 24 MO CMP MRB 6,9 324411-200-001 SOURCE: CMP 32-2-0000-001 MRB 32.40.00/05 MRB 9 LUR 324500-710-001 SIL 32-091 SOURCE: MRB 32.40.00/13 Sub 2 - Page 62 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 324500-03-2 R 324500-04-1 R 325101-01-1-SDM 331400-01-1 ZONE 190 DESCRIPTION PARKING/ULTIMATE EMERGENCY BRAKING SYSTEM SKILL TASK CODE CODE AF 190 FUNCTIONAL CHECK OF BRAKE ACCUMULATOR SYSTEM PARKING/ULTIMATE EMERGENCY BRAKING SYSTEM AF FNC 711 INSPECTION OF THE ACCUMULATOR OF THE ALTERNATE BRAKING SYSTEM FOR PRESSURE DECREASE. NLG UPPER ELECTRICAL HARNESS CONNECTORS AF DET 210 DETAILED INSPECTION OF NLG UPPER ELECTRICAL HARNESS CONNECTORS FOR SIGNS OF CORROSION AND DETERIORATION ANNUNCIATOR LIGHT TEST AND DIMMING EL OPERATIONAL CHECK OF LIGHTS TEST SYSTEM 335100-01-1 FNC 210 CABIN EMERGENCY LIGHTING EL REV: 07 DATE: 29-Dec-2014 INTERVALS I: 60000 FH I: 7500 FH OR 5000 FC I: 4 MO SOURCE CMR* ISB 220 CABIN EMERGENCY LIGHTING EL OPERATIONAL CHECK OF EMERGENCY ESCAPE PATH MARKING LIGHTS 335100-03-1 220 CABIN EMERGENCY LIGHTING EL REFERENCES 324400-720-002 SOURCE: CMR 324000-00002-1-C JIC A320-32-45-00 ISB 32-1279 MEN TASKM. H. APPL 1 0.50 1 2.00 1654 1679 1753 SPECI JIC A320-32-51-02 1 0.3 ALL OPC I: 750 FH OR 6 MO MRB 9 LUR 331400-710-001 1 0.10 ALL OPC I: 8 DY MRB 8 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 SOURCE: MRB 33.51.00/01 335100-710-002 1 0.05 1 0.10 1 0.30 1 0.05 OPERATIONAL CHECK OF EMERGENCY LIGHTS D 335100-02-1 TPS OPC I: 750 FH OR 6 MO MRB 9 LUR OPC I: 400 DY MRB 9 SOURCE: MRB 33.51.00/02 335100-710-003 SIL 33-033 ALL CHECK BATTERY CAPACITY D 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 335100-05-1 200 NOTE: P/N 5822-21 VENDOR: LOCTITE LUMINESCENT SYSTEM CABIN EMERGENCY LIGHTING CHECK MANUAL OPERATION FROM BOTH CONTROL PANELS AND CHECK ALL CABIN LIGHTS AND SIGNS ILLUMINATED BY BATTERIES SOURCE: MRB 33.51.00/03 335139-920-001 CMM 33-51-02 SOURCE: MRB 33.51.00/04 EL OPC I: 15000 FH OR 100 MO MRB 9 LUR 335100-710-004 ALL SOURCE: MRB 33.51.00/05 Sub 2 - Page 63 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 335100-06-1 341300-01-1 341300-02-1 ZONE DESCRIPTION 220 CABIN EMERGENCY LIGHTING 210 CHECK OF DOOR SWITCH POWER SUPPLIED BY EMERGENCY LIGHTS SYSTEM AND CHECK DOOR SWITCH OPERATION TO ACTIVATE THE EXTERIOR LIGHTS AIR DATA 210 OPERATIONAL CHECK OF OVERSPEED WARNING VMO/MMO USING CFDS. AIR DATA SKILL TASK CODE CODE EL 341300-04-1 210 AIR DATA 210 OPERATIONAL CHECK OF OVERSPEED WARNINGS VFE/VLE USING CFDS. AIR DATA RA RA RA RA OPERATIONAL CHECK OF ALTITUDE COMPARISON WARNING 341300-05-1 341300-07-1 210 AIR DATA 120 OPERATIONAL CHECK OF THE 5-MINUTE TIME DELAY OF ADIRU 2 AND 3 POWER DISCONNECTION IN EMERGENCY CONFIGURATION AIR DATA OPC I: 24000 FH R 341300-10-1 120 120 AIR DATA CLEANING OF 1 OUT OF 3 PITOT PROBES. MRB 9 AV AV MRB 9 LUR RST I: 6000 FH OR 20 MO NOTE MRB 6 SIL TPS REFERENCES 335100-720-001 MEN TASKM. H. APPL 1 0.70 ALL 341300-710-002 1 0.20 ALL SOURCE: MRB 34.13.00/01 341300-710-001 MRB 9 LUR 1 0.10 ALL SOURCE: MRB 34.13.00/02 341300-710-007 MRB 9 LUR 1 0.20 ALL SOURCE: MRB 34.13.00/01 341300-710-003 MRB 9 LUR 1 0.10 ALL SOURCE: MRB 34.13.00/04 341000-710-009 MRB 9 LUR 1 0.20 ALL 1 0.20 ALL SOURCE: MRB 34.14.00/03 341000-170-001 SIL 34-084 SOURCE: MRB 34.13.00/06 EL FNC T: 5200 FH I: 2000 FH ISB 303100-710-007 ISB 34-1415 1 2.25 2465 2497 2930 2964 3044 2879 2913 AV RST I: 750 FH OR 4 MO SIL 341000-170-004 SIL 34-084 1 0.58 ALL FUNCTIONAL TEST OF THE HEATING OF THE THREE AOA SENSORS 341300-11-1 SOURCE OPC I: 15000 FH OR 100 MO OPC I: 15000 FH OR 100 MO OPC I: 15000 FH OR 100 MO OPC I: 7500 FH OR 50 MO OPC I: 12000 FH OR 80 MO 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 INTERVALS SOURCE: MRB 33.51.00/06 OPERATIONAL CHECK OF AIR DATA SWITCHING FUNCTION 341300-03-1 REV: 07 DATE: 29-Dec-2014 NOTE: TASK TO BE PERFORMED ALTERNATELY ON PITOT 1, 2 AND 3. Sub 2 - Page 64 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 341400-01-1 ZONE 210 DESCRIPTION ATTITUDE, HEADING AND POSITION SKILL TASK CODE CODE RA OPERATIONAL CHECK OF ATT/HDG SWITCHING FUNCTION 341400-02-1 342000-03-1 R 342100-01-1 210 210 120 ATTITUDE, HEADING AND POSITION OPERATIONAL CHECK OF ATTITUDE AND HEADING COMPARISON WARNING STANDBY NAVIGATION SYSTEMS (INCLUDING ISIS) OPERATIONAL CHECK OF ISIS DC HOT BUS SUPPLY STANDBY ALTITUDE AND AIRSPEED RA AV RA LOW RANGE LEAK TEST OF STANDBY PNEUMATIC CIRCUITS R 342100-02-1 120 ACCESS PANELS: 811 STANDBY ALTITUDE AND AIRSPEED RA ACCESS PANELS: 811, 812 STANDBY COMPASS RA OPERATIONAL CHECK OF THE STANDBY COMPASS INCLUDING LIGHT TEST AND VISUAL CHECK SOURCE TPS REFERENCES MRB 9 LUR MRB 6 LUR SOURCE: MRB 34.20.00/03 342100-790-001 SIL 34-084 SVC I: 6000 FH OR 20 MO NOTE MRB 6 SIL SOURCE: MRB 34.21.00/01 341000-170-003 SIL 34-084 OPC I: 6000 FH OR 48 MO MRB 9 LUR SVC MRB 6 SIL NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED. 210 INTERVALS OPC I: 7500 FH OR 50 MO OPC I: 7500 FH OR 50 MO OPC I: 7500 FH OR 50 MO FNC I: 12000 FH OR 80 MO DRAINING AND FLUSHING OF STANDBY PNEUMATIC CIRCUITS R 342200-01-1 REV: 07 DATE: 29-Dec-2014 MRB 9 LUR MRB 9 LUR MEN TASKM. H. APPL 341400-710-003 1 0.10 ALL SOURCE: MRB 34.14.00/01 341400-710-004 1 0.20 ALL SOURCE: MRB 34.14.00/02 342225-710-001 1 0.30 2 0.20 2465 2497 2930 2964 3044 2879 2913 1654 1679 1753 1 0.75 1654 1679 1753 1 0.10 ALL 1 0.75 2465 2497 2930 2964 3044 2879 2913 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 342200-02-1 120 STANDBY ALTITUDE AND HEADING 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. RA I: 6000 FH OR 20 MO NOTE 342225-170-001 SIL 34-084 SOURCE: MRB 34.20.00/02 ACCESS PANELS: 811, 812 Sub 2 - Page 65 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 342200-05-1 ZONE 120 DESCRIPTION STANDBY DATA - INTEGRATED STANDBY INSTRUMENT SYSTEM (ISIS) SKILL TASK CODE CODE RA FNC LOW RANGE LEAK TEST OF STANDBY PNEUMATIC CIRCUITS 344200-01-1 152 ACCESS PANELS: 811 RADIO ALTIMETER RA DET OPERATIONAL CHECK AND DETAILED INSPECTION FOR CONTAMINATION OF RADIO ALTIMETER FAN REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE I: 12000 FH OR 80 MO MRB 6 LUR I: 4000 FH OR 48 MO NOTE MRB 9 LUR I: 6 MO SIL MRB 9 LUR TPS REFERENCES 342225-790-001 SIL 34-084 MEN TASKM. H. APPL 1 0.42 2465 2497 2930 2964 3044 2879 2913 1 0.20 ALL 344211-615-001 SIL 34-099 1 0.40 ALL 344800-710-001 CMM 34-45-30 CMM 34-45-36 1 0.20 1654 1679 1753 2465 2497 2930 2964 3044 1 0.20 2879 2913 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 SOURCE: MRB 34.20.00/01 344200-750-001 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 R 344800-01-1 210 RADIO ALTIMETER ANTENNAS EXTERNAL SURFACE CLEANING GROUND PROXIMITY WARNING SYSTEM RA OPC I: 7500 FH OR 50 MO OPERATIONAL CHECK OF GROUND SELF TEST SYSTEM 344800-03-1 210 NOTE: P/N 965-0676-020, VENDOR: SUNDSTRAND; P/N 965-0976-003-206-206, VENDOR: HONEYWELL TERRAIN AWARENESS WARNING SYSTEM RA BITE TEST OF THE T2CAS 345200-02-1 210 ATC SYSTEM RA FUNCTIONAL CHECK OF ATC ANTENNAS 351000-01-1 210 CREW OXYGEN SYSTEM AF OPC I: 7500 FH OR 50 MO OR NR FNC I: 15000 FH OR 100 MO OPC I: 24 MO MRB 9 LUR SOURCE: MRB 34.48.00/01 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 34.48.00/01 344300-740-004 SOURCE: MRB 35.10.00/08 Sub 2 - Page 66 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 OPERATIONAL CHECK OF MANUAL MASK RELEASE 352000-02-1 200 PASSENGER OXYGEN (CHEMICAL) 352143-01-1-SDM 200 FUNCTIONAL CHECK OF AUTOMATIC MASK RELEASE, DETAILED INSPECTION OF MASKS AND VISUAL CHECK OF CHEMICAL OXYGEN GENERATORS CABIN OXYGEN MASKS 353000-01-1 200 CLEAN CABIN OXYGEN MASKS PORTABLE OXYGEN CYLINDERS AF AF AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS I: 24 MO OPC I: 24 MO SOURCE 200 PORTABLE OXYGEN AF 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 1 0.20 ALL 1 1 0.10 0.10 ALL I: 72 MO OR 24000 FH CMR** MRB 9 I: 24 MO SPECI I: 4 MO MRB 9 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 450 460 ENGINE BLEED AIR SUPPLY SYSTEM FUNCTIONAL CHECK OF OVERPRESSURE VALVE. AF FNC I: 5 YE OR 22000 FH 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 MRB 9 SOURCE: MRB 35.30.00/04 353000-220-001 MRB 9 SOURCE: MRB 35.30.00/06 361153-720-001 DETAILED INSPECTION OF PORTABLE OXYGEN MASK 361100-01-1 APPL 0.25 FNC VCK TASKM. H. 1 CHECK PRESSURE ON CYLINDER PRESSURE GAUGES 353000-04-1 MEN 351241-200-001 CMR** MRB 8 LUR VCK REFERENCES MRB 9 OPC I: 8500 FH OR 80 MO RST TPS SOURCE: MRB 36.00.00/05 ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR Sub 2 - Page 67 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 361100-05-1 ZONE 191 192 DESCRIPTION ENGINE BLEED AIR SUPPLY SYSTEM SKILL TASK CODE CODE AF DIS REMOVE AND REPLACE COMBO SEALS ON PACK INLET INCL. ON SLEEVES DOWNSTREAM AND UPSTREAM OF FLOW CONTROL VALVE REV: 07 DATE: 29-Dec-2014 INTERVALS I: 12000 FH OR 48 MO NOTE SOURCE MRB 6 SIL TPS REFERENCES 361241-920-001 SIL 21-039 SIL 36-047 MEN TASKM. H. 4 4 4.00 4.00 APPL 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 D 361100-07-1 361100-08-1 410 420 190 520 620 450 460 ENGINE BLEED AIR SUPPLY SYSTEM AF CHK I: 40 MO SIL 361100-790-002 SIL 36-047 2 2 0.10 0.10 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 AF DET I: 1800 FC OR 24 MO VSB LUR 361149-200-004 VSB RA32036-13 1 1 0.10 0.10 EN DET I: 5500 FH OR 36 MO MRB 6 LUR 361141-200-001 1 1 0.25 0.25 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 ACCESS PANELS: 191BT, 192BT, 521AB, 521AT, 621AB, 621AT ENGINE BLEED AIR SUPPLY SYSTEM DETAILLED INSPECTION OF HIGH PRESSURE BLEED AIR DUCT BEND RADIUS. 361141-03-1 453 463 IP BLEED CHECK VALVE REMOVE AND CHECK INTERMEDIATE PRESSURE BLEED CHECK VALVE FOR CONDITION ALL 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 ALL SOURCE: MRB 36.00.00/02 ACCESS PANELS: 437AL, 451AL, 447AL, 461AL Sub 2 - Page 68 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 361143-01-1 ZONE 413 423 DESCRIPTION THERMOSTAT - FAN AIR VALVE CONTROL SKILL TASK CODE CODE AF RST REMOVE THE THERMOSTAT-FILTER OF THE FAN AIR VALVE-CONTROL FOR CLEANING. REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE I: 6000 FH OR 40 MO MRB 6 SIL LUR I: 6000 FH OR 40 MO MRB 6 LUR I: 22000 FH OR 144 MO MRB 6 SIL LUR TPS REFERENCES 361143-100-001 SIL 36-055 MEN TASKM. H. APPL 1 1 0.50 0.50 1 1 0.50 0.50 1 1 0.50 0.50 ALL 1 0.10 ALL SOURCE: MRB 36.00.00/17 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 NOTE: - DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESS OR A MORE FREQUENT INITIAL INTERVAL MAY BE USED ACCESS PANELS: 413DL, 423DL D 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 EN PERFORM LEAK CHECK ON BLEED AIR DUCTING IN WING AREA BETWEEN BLEED AIR PRECOOLER, WING ANTI ICE VALVE AND WING/FUSELAGE CONNECTION NOTE: - TASK MAY BE COMBINED WITH TASKS 361200-02-1(A319) OR 361200-02-2(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 361200-01-1 210 ACCESS PANELS: 521AB, 521CB, 521EB, 621AB, 621CB, 621EB AIR BLEED AIR SUPPLY & CROSSBLEED SYST OPERATIONAL CHECK OF CROSSBLEED VALVE IN MANUAL MODE AF FNC OPC I: 50 MO 361148-790-001 SIL 36-047 SOURCE: MRB 36.00.00/10 MRB 9 361200-710-002 SOURCE: MRB 36.00.00/03 Sub 2 - Page 69 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 361200-02-1 R 361200-02-2 ZONE 150 160 190 310 147 148 151 161 198 312 314 315 DESCRIPTION APU BLEED AIR SUPPLY & CROSSBLEED SYST SKILL TASK CODE CODE 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 361200-790-002 SIL 36-047 MEN TASKM. H. APPL 1 1 1 1 0.50 0.50 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 0.50 0.50 0.50 0.50 0.50 0.50 0.50 0.50 2930 2964 3044 SOURCE: MRB 36.00.00/15 1 1 1 1 1 1 1 1 361200-790-003 SIL 36-047 1 1 0.50 0.50 ALL 1 0.50 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 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 R 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 Sub 2 - Page 70 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 361251-01-2 ZONE 192 DESCRIPTION APU BLEED CHECK VALVE SKILL TASK CODE CODE AF DET REMOVE AND CHECK AUXILIARY POWER UNIT BLEED CHECK VALVE FOR CONDITION 381000-01-1 171 ACCESS PANELS: 197BB POTABLE WATER SYSTEM CA RST STERILIZATION OF POTABLE WATER SYSTEM AND DISCARD OF WATER FILTER ELEMENTS, IF INSTALLED REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE I: 11000 FH OR 73 MO MRB 6,9 LUR 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 361251-200-001 SIL 36-038 MEN TASKM. H. APPL 1 0.50 2 3.00 1654 1679 1753 2465 2497 2879 2913 2 3.00 2930 2964 3044 1 0.75 2930 2964 3044 2 0.50 ALL 1 0.50 ALL SOURCE: MRB 36.00.00/13 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. R 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. R 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 ENVIRONMENTAND 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 Sub 2 - Page 71 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 383100-06-1 ZONE 200 DESCRIPTION VACUUM TOILET SYSTEM SKILL TASK CODE CODE AF RST CLEANING OF VACUUM WASTE LINES WITH CHEMICAL CLEANING AGENT AND CRUSHED ICE 383100-07-1 200 NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED. VACUUM TOILET SYSTEM 383200-01-1 200 D 383200-02-1 200 171 AIR FILTER 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 MRB 7 SIL LUR REFERENCES 383100-100-018 SIL 38-020 MEN TASKM. H. APPL 1 0.30 ALL SOURCE: MRB 38.31.01/05 SIL LUR 383100-100-004 SIL 38-020 2 10.00 ALL UT RST I: 1500 FH OR 24 MO NOTE MRB 7 LUR 383200-100-002 SIL 38-029 1 0.10 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 I: 6500 FH OR 48 MO I: 24000 FH OR 72 MO SIL LUR 1 0.30 1 0.10 1654 1679 1753 2465 2497 2879 2913 I: 24000 FH OR 72 MO NOTE MRB 6,9 1 0.10 2930 2964 3044 UT RST CA DIS DISCARD SYSTEM FILTER ELEMENT NOTE : DEPENDING ON EACH INDIVIDUAL OPERATOR´S ENVIRONMENT A MORE FREQUENT INTERVAL MAY BE USED R 384142-01-2 I: 150 FH OR 2 MO NOTE TPS I: 6000 FH OR 48 MO NOTE REMOVE FOR CLEANING THE SINK DRAIN AIR STOP VALVE. 384142-01-1 SOURCE RST 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. SINK DRAIN AIR STOP VALVE INTERVALS AF CORRECTIVE VACUUM WASTE LINE CLEANING. NOTE:INTERVAL MAY BE ADJUSTED ACCORDING TO OPERATOR EXPERIENCE. WASTE WATER DRAIN REV: 07 DATE: 29-Dec-2014 CA DIS 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 Sub 2 - Page 72 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 REV: 07 DATE: 29-Dec-2014 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 R 491200-A1-1 315 REFERENCES 384200-210-001 MEN TASKM. H. APPL 1 0.05 1753 1 0.10 1753 1 0.30 1 1 0.55 0.55 1 0.30 2930 2964 3044 1 1 0.55 0.55 2930 2964 3044 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. ACCESS PANELS: 315AL, 316AR APU MOUNTS 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 491200-210-004 SOURCE: MRB 49.12.00/02-32 NOTE : TASK MAY BE ACCOMPLISHED AT OPPORTUNITY OF APU CHANGE R 491200-A2-1 315 316 ACCESS PANELS: 315AL, 316AR APU MOUNTS GENERAL VISUAL INSPECTION OF APU SUSPENSION SYSTEM FOR CONDITION AND SECURITY. AF GVI 491200-210-005 SOURCE: MRB 49.12.00/01-32 ACCESS PANELS: 315AL, 316AR Sub 2 - Page 73 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 491200-B1-1 ZONE 315 DESCRIPTION APU MOUNTS SKILL TASK CODE CODE EN DET DETAILED INSPECTION OF APU SUSPENSION RODS, VIBRATION ISOLATOR STRUCTURE INCLUDING BRACKETS AND VISIBLE PART OF STRUCTURE ATTACHMENT FITTINGS REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE I: 80 MO NOTE MRB 9 I: 20 MO MRB 9 TPS REFERENCES 491200-210-007 MEN TASKM. H. APPL 1 0.30 1654 1679 1753 2465 2497 2879 2913 1 1 0.55 0.55 1654 1679 1753 2465 2497 2879 2913 1 1.42 1 1.42 2930 2964 3044 1 1.42 1654 1679 1753 2465 2497 2879 2913 SOURCE: MRB 49.12.00/02-13 NOTE : TASK MAY BE ACCOMPLISHED AT OPPORTUNITY OF APU CHANGE 491200-B2-1 315 316 ACCESS PANELS: 315AL, 316AR APU MOUNTS AF GVI GENERAL VISUAL INSPECTION OF APU SUSPENSION SYSTEM FOR CONDITION AND SECURITY. D 491300-01-1 310 ACCESS PANELS: 315AL, 316AR FIRE SEALS SOURCE: MRB 49.12.00/01-13 EN GVI I: 20 MO 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-A1-1 310 ACCESS PANELS: 315AL, 316AR FIRE SEALS 491300-B1-1 310 GENERAL VISUAL INSPECTION OF ALL APU COMPARTMENT FIRE WALLS AND SEALS: - COMPARTMENT DOORS - FWD AND AFT FIRE WALLS - SIDE FIRE WALLS - UPPER FIRE WALL 491300-200-001 SOURCE: MRB 49.13.00/01-36 EN GVI I: 20 MO 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 ACCESS PANELS: 315AL, 316AR FIRE SEALS 491200-210-804 491300-200-002 SOURCE: MRB 49.13.00/01-32 EN GVI I: 20 MO MRB 8 491300-200-003 SOURCE: MRB 49.13.00/01-13 ACCESS PANELS: 315AL, 316AR Sub 2 - Page 74 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 491600-01-1 ZONE 310 DESCRIPTION AIR INTAKE SYSTEM SKILL TASK CODE CODE AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS I: 40 MO SOURCE MRB 9 DETAILED INSPECTION OF APU AIR INTAKE, DIFFUSER ELBOW, SEALS AND FELT METAL D 491600-03-1 310 ACCESS PANELS: 314AR, 315AL, 316AR AIR INTAKE SYSTEM 310 ACCESS PANELS: 315AL, 316AR APU AIR INTAKE SYSTEM 310 ACCESS PANELS: 315AL, 316AR AIR INTAKE SYSTEM 313 315 ACCESS PANELS: 314AR, 315AL, 316AR AIR INTAKE SYSTEM 310 ACCESS PANELS: 314AR, 316AR, 315AL ENGINE 315 ACCESS PANELS: 315AL, 316AR ENGINE FUEL AND CONTROL 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 491600-210-002 1 0.30 2930 2964 3044 1 1 0.15 0.15 1654 1679 1753 2465 2497 2879 2913 1 0.10 1 0.15 1 0.02 SOURCE: MRB 49.16.00/03-32 EN DET I: 40 MO MRB 9 310 ACCESS PANELS: 315AL, 316AR FUEL DISTRIBUTION VISUAL CHECK OF FUEL FILTER DIFFERENTIAL PRESSURE INDICATOR. 491600-200-002 SOURCE: MRB 49.16.00/01-13 EN DET EN DIS DISCARD FUEL INLET FILTER ELEMENT D 493100-01-1 0.30 EASA AD ISB DETAILED INSPECTION OF MAGNETIC CHIP DETECTOR 493000-B1-1 1 APPL I: 2400 FH DETAILED INSPECTION OF APU AIR INTAKE, DIFFUSER ELBOW, SEALS AND FELT METAL D 492000-01-1 TASKM. H. RST DETAILED INSPECTION OF APU AIR INTAKE, DIFFUSER ELBOW, SEALS AND FELT METAL 491600-B1-1 491600-210-001 MEN AF GENERAL VISUAL INSPECTION OF APU AIR INLET PLENUM AND APU AIR INTAKE. R 491600-A1-1 REFERENCES SOURCE: MRB 49.16.00/02-36 CLEANING OF APU AIR INTAKE D 491600-04-1 TPS EN VCK 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 499142-200-001 SOURCE: MRB 49.20.00/01-36 493241-920-001 SOURCE: MRB 49.30.00/02-13 493211-210-001 1654 1679 1753 2465 2497 2879 2913 SOURCE: MRB 49.31.00/01-36 ACCESS PANELS: 315AL Sub 2 - Page 75 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 493400-01-1 ZONE 210 DESCRIPTION APU FUEL LOW PRESSURE WARNING SKILL TASK CODE CODE EN REV: 07 DATE: 29-Dec-2014 INTERVALS OPC I: 24 MO SOURCE 210 APU FUEL LOW PRESSURE WARNING EN OPC I: 24 MO 210 APU FUEL LOW PRESSURE WARNING EN OPC I: 24 MO 316 ACCESS PANELS: 315AL, 316AR IGNITION AND STARTING EN DIS 315 ACCESS PANELS: 315AL, 316AR IGNITION AND STARTING EN DET DETAILED INSPECTION OF IGNITER PLUG 494000-B3-2 315 ACCESS PANELS: 315AL, 316AR IGNITION AND STARTING MRB 9 SOURCE: MRB 49.34.00/01-36 493100-710-002 1 0.10 2930 2964 3044 MRB 9 SOURCE: MRB 49.34.00/01-32 493100-710-003 1 0.10 1654 1679 1753 2465 2497 2879 2913 1 0.05 2930 2964 3044 1 0.20 1654 1679 1753 2465 2497 2879 2913 1654 1679 1753 2879 2913 D 494141-01-1 316 ACCESS PANELS: 315AL IGNITER PLUG 315 ACCESS PANELS: 315AL, 316AR STARTER MOTOR MRB 9 LUR I: 6000 FH OR 40 MO MRB 7 LUR SOURCE: MRB 49.40.00/02-32 315 ACCESS PANELS: 315AL, 316AR STARTER MOTOR MONITORING TEST OF APU STARTER MOTOR ACCESS PANELS: 315AL, 316AR 494141-220-001 SOURCE: MRB 49.40.00/02-13 I: 750 FH OR 6 MO SIL LUR 494251-200-008 SIL 49-043 1 0.10 EN DET I: 6000 FH OR 40 MO MRB 7 LUR 494141-220-002 1 0.20 SOURCE: MRB 49.40.00/03-36 EN OPC I: 600 FH EASA AD ISB 494251-700-001 EASA AD 2006-0153 ISB 49-1068 1 0.50 AF OPC I: 600 FH EASA AD ISB 494251-700-003 EASA AD 2006-0153 ISB 49-1068 VSB 2000866-49-2356 1 0.40 TEST OF CLUTCH OF APU STARTER MOTOR D 494251-03-1 494141-920-001 VCK DETAILED INSPECTION OF IGNITER PLUG D 494251-02-1 I: 2250 FH OR 24 MO EN CHECK WEAR INDICATOR OF STARTER MOTOR BRUSH APPL 0.10 SOURCE: MRB 49.34.00/01-13 REMOVE AND DISCARD IGNITER PLUGS 494000-B2-1 TASKM. H. 1 OPERATIONAL CHECK OF APU FUEL LOW PRESSURE CIRCUIT R 494000-A1-1 MEN 493100-710-001 OPERATIONAL CHECK OF APU FUEL LOW PRESSURE CIRCUIT 493400-B1-1 REFERENCES MRB 9 OPERATIONAL CHECK OF APU FUEL LOW PRESSURE CIRCUIT R 493400-A1-1 TPS Sub 2 - Page 76 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 494251-A2-1 ZONE 315 DESCRIPTION STARTER MOTOR SKILL TASK CODE CODE 315 ACCESS PANELS: 315AL LOAD COMPRESSOR SURGE/REVERSE FLOW PROTECTION 498000-B1-1 310 ACCESS PANELS: 315AL, 316AR EXHAUST 310 VISUAL CHECK OF APU COMPARTMENT EXHAUST MUFFLER INSULATION COVERS AND BELLOWS EXHAUST SOURCE 310 ACCESS PANELS: 315AL, 316AR EXHAUST SYSTEM 310 ACCESS PANELS: 315AL, 316AR OIL SYSTEM 310 ACCESS PANELS: 315AL, 316AR OIL SYSTEM 310 ACCESS PANELS: 315AL, 316AR STORAGE AND DISTRIBUTION CHECK APU COMPARTMENT AND AIR INTAKE DUCT FOR OIL CONTAMINATION APPL 1 0.05 AF RST I: 2250 FH OR 24 MO MRB 7 LUR 495152-600-001 1 0.30 I: 24 MO MRB 9 498100-200-016 1 0.10 2930 2964 3044 MRB 9 SOURCE: MRB 49.80.00/04-32 498100-200-017 1 0.10 1654 1679 1753 2465 2497 2879 2913 1 0.10 1 0.20 EN EN VCK VCK I: 24 MO EN DET I: 24 MO 2930 2964 3044 SOURCE: MRB 49.51.20/02-36 SOURCE: MRB 49.80.00/01-13 MRB 9 498100-200-015 SOURCE: MRB 49.80.00/04-36 EN DIS I: 3000 FH OR 24 MO MRB 9 LUR 499141-920-001 SOURCE: MRB 49.90.00/02-32 EN VCK I: 7500 FH OR 50 MO SIL LUR 490000-790-007 SIL 49-032 1 0.60 EN VCK I: 7500 FH OR 50 MO AOT SIL LUR 490000-790-001 AOT 49-03 SIL 49-032 1 0.60 CHECK APU COMPARTMENT AND AIR INTAKE DUCT FOR OIL CONTAMINATION D 499100-02-1 TASKM. H. 494251-200-006 SIL 49-043 DISCARD PRESSURE OIL FILTER ELEMENT R 499000-A2-1 MEN SIL LUR VISUAL CHECK OF APU COMPARTMENT EXHAUST MUFFLER INSULATION COVERS AND BELLOWS D 499000-A1-1 REFERENCES I: 750 FH OR 6 MO VISUAL CHECK OF APU COMPARTMENT EXHAUST MUFFLER INSULATION COVERS AND BELLOWS D 498100-04-1 TPS VCK CLEAN SURGE VALVE FILTER R 498000-A4-1 INTERVALS EN CHECK WEAR INDICATOR OF STARTER MOTOR BRUSH D 495100-01-1 REV: 07 DATE: 29-Dec-2014 2930 2964 3044 ACCESS PANELS: 314AR, 315AL, 316AR Sub 2 - Page 77 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 499100-B2-1 ZONE 315 DESCRIPTION STORAGE AND DISTRIBUTION SKILL TASK CODE CODE REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE TPS REFERENCES MEN TASKM. H. APPL AF DIS I: 3000 FH OR 24 MO NOTE SIL LUR 499141-200-002 SIL 49-051 1 0.20 1654 1679 1753 2465 2497 2879 2913 EN VCK I: 7500 FH OR 50 MO SIL LUR 490000-790-008 SIL 49-032 1 0.60 1654 1679 1753 2465 2497 2879 2913 EN DIS I: 1500 FH OR 12 MO MRB 9 LUR 499145-200-002 1 0.20 I: 8 DY MRB 8 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 1 1 1 1 0.05 0.05 0.05 0.05 ALL REMOVE AND DISCARD OIL FILTER ELEMENTS (8069KM) AND (8076KM). NOTE: DEPENDING ON OPERATING ENVIROMENT AND OPERATORS EXPERIENCE A HIGHER INITIAL INTERVAL MAY BE USED 499100-B4-1 310 ACCESS PANELS: 315AL, 316AR STORAGE AND DISTRIBUTION CHECK APU COMPARTMENT AND AIR INTAKE DUCT FOR OIL CONTAMINATION D 499141-01-1 310 ACCESS PANELS: 314AR, 315AL, 316AR OIL FILTER DISCARD LUBE AND ALTERNATOR SCAVENGE FILTER ELEMENTS 521000-01-1 521000-02-1 521000-03-1 831 832 841 842 831 832 841 842 831 832 841 842 ACCESS PANELS: 315AL, 316AR PASSENGER/CREW DOOR AF FNC SOURCE: MRB 49.91.00/02-36 CHECK EMERGENCY CYLINDER/ACCUMULATOR PRESSURE NOTE : TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW DOORS PASSENGER/CREW DOOR SOURCE: MRB 52.10.00/01 AF FNC FUNCTIONAL CHECK OF DOOR SUSPENSION ACCESS PANELS: 831, 831FZ, 831GZ, 832, 832FZ, 832GZ, 841, 841FZ, 841GZ, 842, 842FZ, 842GZ PASSENGER/CREW DOOR DETAILED INSPECTION OF DOOR SEALS 521000-210-004 AF DET I: 15000 FH OR 10000 FC OR 80 MO I: 48 MO MRB 6,9 521000-720-001 SOURCE: MRB 52.10.00/02 MRB 6 521000-220-006 SOURCE: MRB 52.10.00/06 NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW DOORS ACCESS PANELS: 831, 832, 841, 842 Sub 2 - Page 78 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 521000-04-1 ZONE 831 832 841 842 DESCRIPTION PASSENGER/CREW DOOR SKILL TASK CODE CODE AF DET REV: 07 DATE: 29-Dec-2014 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 OPC I: 15000 FH OR 10000 FC OR 80 MO MRB 6,9 FNC MRB 6,9 DETAILED INSPECTION OF PASSENGER/CREW DOOR FOR INTEGRITY AND GOOD ADJUSTMENT OF MECHANISMS (INCLUDING GIRT BAR) TPS REFERENCES 521000-200-002 SOURCE: MRB 52.10.00/02 MEN TASKM. H. APPL 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 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 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 FUNCTIONAL CHECK OF ESCAPE SLIDE RELEASE MECHANISM NOTE : ONLY FWD DOORS FOR POST 37807 (IF AFT DOORS FULLY DEACTIVATED). PASSENGER/CREW DOOR AF CHECK OF DOOR STOPS ADJUSTMENT ACCESS PANELS: 831, 832, 841, 842 521000-08-1 831 832 841 842 FNC PASSENGER/CREW DOOR AF OPERATIONAL CHECK OF INTERLOCK MECHANISM TO ENSURE THAT EMERGENCY ESCAPE HANDLE STAYS IN DISARMED POSITION WHEN DOOR IS UP AND OUTSIDE OF FRAME 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 MRB 6,9 521000-710-002 SOURCE: MRB 52.10.00/02 NOTE : ONLY FWD DOORS FOR POST 37807 (IF AFT DOORS FULLY DEACTIVATED). 521000-09-1 831 832 841 842 ACCESS PANELS: 831, 832, 841, 842 PASSENGER/CREW DOOR FUNCTIONAL CHECK OF MECHANICAL LOCKING INDICATION ACCESS PANELS: 831, 832, 841, 842 AF I: 15000 FH OR 10000 FC OR 80 MO 521000-720-004 SOURCE: MRB 52.10.00/02 Sub 2 - Page 79 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 521000-10-1 ZONE 831 832 841 842 DESCRIPTION PASSENGER/CREW DOOR SKILL TASK CODE CODE AF 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 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 AF 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). 521000-14-1 521121-01-1 831 832 841 842 831 832 841 842 ACCESS PANELS: 831, 832, 841, 842 PASSENGER/CREW DOOR AF REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE OPC I: 15000 FH OR 10000 FC OR 80 MO MRB 6,9 OPC I: 15000 FH OR 10000 FC OR 80 MO MRB 6,9 OPC I: 15000 FH OR 10000 FC OR 80 MO MRB 6,9 LUB MRB 9 SIL I: 20 MO TPS REFERENCES 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 122252-640-016 SIL 53-076 LUBRICATION OF HINGE ARM SUPPORT FITTING BEARINGS NOTE : TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW DOORS PASSENGER / CREW DOOR LUBRICATION OF EXTERIOR CONTROL HANDLE AND TELESCOPIC ARM SOURCE: MRB 52.10.00/05 AF LUB I: 20 MO MRB 6 122252-640-006 SOURCE: MRB 52.10.00/03 MEN TASKM. H. APPL 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 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 NOTE : TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW DOORS Sub 2 - Page 80 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 521121-02-1 ZONE 831 832 841 842 DESCRIPTION PASSENGER / CREW DOOR SKILL TASK CODE CODE AF LUB REV: 07 DATE: 29-Dec-2014 INTERVALS I: 36 MO SOURCE MRB 6 LUBRICATION OF SAFETY PIN GUIDE FITTING AND DOOR ARMING/DISARMING MECHANISM TPS REFERENCES 122252-640-014 AOT 52A1103 SOURCE: MRB 52.10.00/04 MEN TASKM. H. APPL 1 1 1 1 0.10 0.10 0.10 0.10 ALL 2 2 2 2 2 2 0.20 0.20 0.20 0.20 0.20 0.20 2930 2964 3044 2 2 2 2 0.20 0.20 0.20 0.20 1654 1679 1753 2465 2497 2879 2913 1 1 1 1 1 1 0.20 0.20 0.20 0.20 0.20 0.20 1 1 1 1 0.20 0.20 0.20 0.20 NOTE : TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW DOORS R 522100-01-1 522100-01-2 151 152 833 834 843 844 151 152 834 844 ACCESS PANELS: 831BZ, 831CZ, 831DZ, 832BZ, 832CZ, 832DZ, 841BZ, 841CZ, 841DZ, 842BZ, 842CZ, 842DZ PASSENGER COMPARTMENT EMERGENCY EXIT AF OPERATIONAL CHECK OF UNLOCKING AND OPENING FROM INSIDE IN ARMED MODE. OPC I: 9000 FH OR 60 MO MRB 8 LUR OPC I: 9000 FH OR 5 YE MRB 8 LUR FNC I: 12000 FH OR 80 MO MRB 8 LUR I: 12000 FH OR 80 MO MRB 8 LUR 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 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 D 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 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 1654 1679 1753 2465 2497 2879 2913 NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED EMERGENCY EXITS ACCESS PANELS: 151CW, 152CW, 826, 834BZ, 844BZ Sub 2 - Page 81 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 522100-02-5 D 522100-07-1 522100-07-2 ZONE 151 152 833 834 843 844 151 152 833 834 843 844 151 152 834 844 DESCRIPTION PASSENGER COMPARTMENT EMERGENCY EXIT SKILL TASK CODE CODE AF FUNCTIONAL CHECK OF MANUAL AND AUTOMATIC SLIDE RELEASE SIGNAL. FNC REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE I: 15000 FH OR 100 MO MRB 8 LUR OPC I: 12000 FH OR 80 MO MRB 8 LUR OPC I: 12000 FH OR 80 MO MRB 8 LUR OPC 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 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 OPERATIONAL CHECK OF UNLOCKING AND OPENING FROM OUTSIDE IN ARMED MODE 522100-710-004 SOURCE: MRB 52.21.00/02 MEN TASKM. H. APPL 1 1 1 1 1 1 0.20 0.20 0.20 0.20 0.20 0.20 2930 2964 3044 2 2 2 2 2 2 0.20 0.20 0.20 0.20 0.20 0.20 2 2 2 2 0.20 0.20 0.20 0.20 1654 1679 1753 2465 2497 2879 2913 2 2 2 2 2 2 0.20 0.20 0.20 0.20 0.20 0.20 2930 2964 3044 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 522100-710-004 SOURCE: MRB 52.21.00/04 ACCESS PANELS: 151CW, 152CW, 826, 833BZ, 834BZ, 843BZ, 844BZ Sub 2 - Page 82 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 522100-08-1 ZONE 151 152 833 834 843 844 DESCRIPTION PASSENGER COMPARTMENT EMERGENCY EXIT SKILL TASK CODE CODE AF - 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. REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE OPC I: 15000 FH OR 100 MO MRB 9 LUR OPC I: 15000 FH OR 100 MO MRB 9 LUR LUB 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 TPS REFERENCES 522100-710-005 SOURCE: MRB 52.21.00/03 MEN TASKM. H. APPL 2 2 2 2 2 2 0.20 0.20 0.20 0.20 0.20 0.20 2930 2964 3044 2 2 2 2 0.20 0.20 0.20 0.20 1654 1679 1753 2465 2497 2879 2913 1 1 0.20 0.20 ALL 1 1 0.10 0.10 ALL 2 0.20 ALL 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 - 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 523000-01-1 825 826 ACCESS PANELS: 151CW, 152CW, 826, 834BZ, 844BZ CARGO COMPARTMENT DOOR, FWD AND AFT AF 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 FUNCTIONAL CHECK OF FORWARD CARGO COMPARTMENT DOOR, COMPRISING FUNCTIONAL CHECKS OF: - LOCKING MECHANISM - INTERLOCK MECHANISM - DRIFT PIN MECHANISM - SAFETY MECHANISM AF FNC 122252-640-002 SOURCE: MRB 52.31.00/01 122252-640-009 SOURCE: MRB 52.31.00/01 523100-720-001 SOURCE: MRB 52.31.00/02 ACCESS PANELS: 825, 825AR Sub 2 - Page 83 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 523200-01-1 ZONE 826 DESCRIPTION AFT CARGO COMPARTMENT DOOR SKILL TASK CODE CODE AF FNC FUNCTIONAL CHECK OF AFT CARGO COMPARTMENT DOOR, COMPRISING FUNCTIONAL CHECKS OF: - LOCKING MECHANISM - INTERLOCK MECHANISM - DRIFT PIN MECHANISM - SAFETY MECHANISM R 523300-01-1 827 ACCESS PANELS: 826, 826AR BULK CARGO COMPARTMENT DOOR AF LUB LUBRICATION OF BULK CARGO COMPARTMENT DOOR HANDLE AND HINGE ARM BEARINGS 524100-01-1 524100-02-1 525111-01-1 525111-02-1 525111-04-1 525111-05-1 811 812 822 824 811 812 822 824 NOTE: INTERVAL MAY NEED TO BE MORE FREQUENT WHEN OPERATING IN HOSTILE ENVIRONMENTS ACCESS DOORS AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE I: 18000 FC OR 72 MO MRB 6,9 I: 18 MO OR 4500 FC MRB 6,9 I: 48 MO MRB 9 ACCESS PANELS: 811, 812, 822, 824 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. 523200-720-001 AF LUB AF AF AF AF DET I: 20 MO NOTE I: 15000 FH OR 100 MO OPC I: 15000 FH OR 48 MO OPC I: 15000 FH OR 48 MO OPC I: 15000 FH OR 48 MO MEN TASKM. H. APPL 0.20 ALL 1 0.10 2930 2964 3044 1 1 1 1 0.05 0.05 0.05 0.05 ALL 0.05 0.05 0.05 0.05 ALL SOURCE: MRB 52.41.00/02 1 1 1 1 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 52.31.00/02 122252-640-007 SOURCE: MRB 52.33.00/01 524100-210-001 SOURCE: MRB 52.41.00/01 LUBRICATION OF EXTERIOR AVIONIC COMPARTMENT DOOR HANDLE NOTE: INTERVAL MAY NEED TO BE MORE FREQUENT WHEN OPERATING IN HOSTILE ENVIRONMENTS 220 REFERENCES 2 DETAILED INSPECTION OF DOOR SEALS ACCESS PANELS: 811, 812, 822, 824 ACCESS DOORS TPS MRB 9 MRB 6,9 LUR 122252-640-008 SOURCE: MRB 52.51.11/02 Sub 2 - Page 84 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 525111-06-1 D 525111-07-1 ZONE DESCRIPTION SKILL TASK CODE CODE INTERVALS 220 COCKPIT DOOR AF FNC 220 FUNCTIONAL CHECK OF THE CORRECT ADJUSTMENT OF THE COCKPIT DOOR, ELECTRICAL RELEASE STRIKES AND LATCH MECHANISM COCKPIT DOOR AF OPC I: 12000 FH OR 80 MO OPC I: 72 MO OPERATIONAL CHECK OF DEADBOLT 525111-08-1 REV: 07 DATE: 29-Dec-2014 220 COCKPIT DOOR AF I: 20 MO SOURCE 210 DOOR WARNING EL 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 REFERENCES MEN TASKM. H. APPL SIL 525100-720-003 SIL 52-061 1 3.00 MRB 9 LUR 525100-710-008 1 0.05 MRB 9 SOURCE: MRB 52.51.11/04 525100-710-010 1 0.13 ALL OPC I: 7500 FH OR 40 MO MRB 9 SOURCE: MRB 52.51.11/05 527100-710-001 1 0.05 ALL LUB 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 1 0.10 ALL OPERATIONAL CHECK OF MANUAL RELEASE OF PIP-PINS 527100-01-1 TPS I: 18 MO 1654 1679 1753 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 EL OPERATIONAL CHECK OF EMERGENCY ESCAPE SLIDE RELEASE WARNING 527300-02-1 122 NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW DOORS / EMERGENCY EXITS EMERGENCY ESCAPE SLIDE RELEASE AND OVERPRESSURE WARNING SYSTEMS OPERATIONAL CHECK OF RESIDUAL CABIN PRESSURE WARNING AND FUNCTIONAL CHECK OF DIFFERENTIAL PRESSURE SWITCH AF OPC I: 7500 FH OR 40 MO MRB 9 FNC MRB 9 I: 18000 FC OR 80 MO SOURCE: MRB 52.73.00/01 527300-720-003 SOURCE: MRB 52.73.00/02 NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW DOORS ACCESS PANELS: 811 Sub 2 - Page 85 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 530000-01-1 R 531900-01-1 ZONE DESCRIPTION 100 FUSELAGE DRAINAGE 220 REMOVE AND DETAILED INSPECTION OF PISTON TYPE DRAIN VALVES IN LOWER FUSELAGE SHELL FUSELAGE DRAINAGE SKILL TASK CODE CODE AF AF DET DET REV: 07 DATE: 29-Dec-2014 INTERVALS I: 6 YE I: 4 MO SOURCE 120 FUSELAGE DRAINAGE REFERENCES MEN TASKM. H. 530000-210-001 1 0.40 ALL MRB 9 SOURCE: MRB 53.19.00/03 531900-210-001 1 0.10 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 2 0.60 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1 1 1 0.20 0.20 0.20 ALL 1 0.10 ALL SOURCE: MRB 53.19.00/06 AF OPC I: 24 MO MRB 9 OPERATIONAL CHECK OF THE COCKPIT DRAINAGE PIPE 531900-710-001 SOURCE: MRB 53.19.00/07 ACCESS PANELS: 824, 825 531900-03-1 533900-01-1 535900-01-1 R 535900-02-1 545000-01-1 120 130 150 FUSELAGE DRAINAGE 140 OPERATIONAL CHECK OF PISTON TYPE DRAIN VALVES IN LOWER FUSELAGE SHELL FROM OUTSIDE FUSELAGE DRAINAGE 310 OPERATIONAL CHECK OF RUBBER FLAP DRAIN VALVE HOLES IN PRESSURE FLOOR FROM MLG BAY FUSELAGE DRAINAGE 827 OPERATIONAL CHECK OF SINGLE DRAIN PIPE AFT OF FR 70 FROM OUTSIDE FUSELAGE DRAINAGE 410 420 OPERATIONAL CHECK OF RUBBER FLAP DRAIN VALVE AT BULK CARGO COMPARTMENT DOOR FROM OUTSIDE PYLONS AF AF AF AF AF OPC I: 24 MO OR 5000 FC OPC I: 24 MO OPC I: 8 MO OPC I: 24 MO GVI I: 24 MO APPL MRB 9 INSPECTION OF THE COCKPIT GRID COLLECTOR ASSY R 531900-02-1 TPS MRB 9 531900-710-003 MRB 9 SOURCE: MRB 53.19.00/08 533900-210-001 MRB 9 SOURCE: MRB 53.19.00/01 535900-210-001 1 0.05 ALL MRB 9 SOURCE: MRB 53.19.00/02 535900-210-002 1 0.10 2930 2964 3044 MRB 8 SOURCE: MRB 53.19.00/05 545000-200-001 1 1 0.10 0.10 ALL 2 2 0.10 0.10 ALL GENERAL VISUAL INSPECTION OF COMPARTMENT A AND F PYLON DRAIN SYSTEM 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 FLOW CHECK OF INDIVIDUAL DRAIN LINES OF PYLON SYSTEM AF FNC I: 72 MO MRB 8 545000-200-002 SOURCE: MRB 54.50.00/02 ACCESS PANELS: 413AL, 471AL, 471BL, 423AL, 482AR, 482BR Sub 2 - Page 86 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 545000-03-1 ZONE 410 420 DESCRIPTION PYLON DRAINAGE SKILL TASK CODE CODE REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE TPS REFERENCES MEN TASKM. H. APPL 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 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. 552600-01-1 335 345 PREPARATION: LOWER AFT PYLON FAIRING REMOVED; ELEVATOR ATTACH FITTINGS SOURCE: MRB 54.50.00/03 AF CHK I: 12 YE SIL 552600-200-002 SIL 55-035 1 1 2.50 2.50 ALL AF CHK T: 6 YE I: 6 YE SIL 554600-200-802 SIL 55-038 1 6.42 ALL 561000-200-003 JIC A320-56-10-00 SIL 56-017 561000-200-005 SIL 56-017 1 0.30 ALL 1 0.30 ALL 1 0.10 ALL 1 0.20 ALL 1 1 0.40 0.40 ALL CHECK OF ELEVATOR ATTACHMENT FITTINGS FOR WEAR, LH/RH PREPARATION: ELEVATOR REMOVED; ACCESS PANELS: 334BB, 334DB, 334FB, 334HB, 344BB, 344DB, 344FB, 344HB 553600-01-1 325 RUDDER ATTACH FITTINGS CHECK OF RUDDER ATTACHMENT FITTINGS FOR WEAR ACCESS PANELS: 325BL, 325BR, 325CL, 325CR, 325DL, 325DR, 325EL, 325ER 561000-01-1 210 COCKPIT WINDOWS AF DET I: 4 MO SIL 561000-02-1 210 DETAILED INSPECTION OF ALL COCKPIT WINDOWS FROM INSIDE COCKPIT WINDOWS AF DET I: 20 MO SIL 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 MRB 6,8 SOURCE: MRB 56.12.00/02 122256-600-001 MRB 9 SOURCE: MRB 56.12.00/01 572900-210-002 561200-01-1 DETAILED INSPECTION OF WINDOW SEALS 561200-02-1 210 SLIDING WINDOWS AF LUB I: 20 MO LUBRICATION OF COCKPIT SLIDING WINDOW TRACKS 572900-01-1 500 600 MISCELLANEOUS (DRAINS) FOR OUTER WING CHECK OF DRAIN HOLES AND HOSES FOR CLOGGING AF OPC I: 80 MO SOURCE: MRB 57.29.00/01 Sub 2 - Page 87 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 573900-01-1 ZONE 530 630 DESCRIPTION MISCELLANEOUS (DRAINS) FOR WING TIP SKILL TASK CODE CODE AF REV: 07 DATE: 29-Dec-2014 INTERVALS OPC I: 80 MO SOURCE MRB 9 CHECK OF DRAIN HOLES FOR CLOGGING D 575200-01-1 500 600 INBOARD FLAP AF DET DETAILED INSPECTION OF FLAP TRACK NO 1 DRIVE LEVER ARM FOR SIDE PLAY I: 12000 FC OR 144 MO ISB MRB 6 LUR TPS REFERENCES 573900-200-002 SOURCE: MRB 57.39.00/01 575200-200-010 ISB 57-1108 MEN TASKM. H. APPL 1 1 0.10 0.10 ALL 1 1 0.50 0.50 1 1 0.50 0.50 ALL 1 1 0.05 0.05 ALL 1 1 0.45 0.45 ALL 1 1 0.25 0.25 ALL 1 1 0.40 0.40 ALL 1 1 0.42 0.42 ALL SOURCE: MRB 27.50.00/14 PREPARATION: FLAPS EXTENDED; 575900-01-1 711000-C1-1 500 600 430 440 ACCESS PANELS: 193AB, 193BB, 734, 194AB, 194BB, 744 MISCELLANEOUS (DRAINS) FOR LEADING/TRAILING EDGE AND LEADING/TRAILING EDGE DEVICES CHECK OF DRAIN HOLES FOR CLOGGING COWLINGS AF OPC I: 80 MO 430 440 ACCESS PANELS: 437AL, 438AR, 447AL, 448AR COWLINGS EN GVI EN GVI I: 7500 FH OR 50 MO MRB 8 LUR I: 24 MO MRB 8 711000-C5-1 430 440 430 440 ACCESS PANELS: 437AL, 438AR, 447AL, 448AR COWLINGS EN FNC I: 24 MO MRB 8 430 440 ACCESS PANELS: 437AL, 438AR, 447AL, 448AR COWLINGS GENERAL VISUAL INSPECTION OF FAN COWL DOOR FIRE SEALS 711311-280-802 SOURCE: MRB 71.10.00/05-C5 EN GVI GENERAL VISUAL INSPECTION OF FAN COWL LATCHES AND ADJACENT STRUCTURE 711000-C7-1 711311-200-804 SOURCE: MRB 71.10.00/04-C5 FUNCTIONAL CHECK OF PRESSURE RELIEF DOOR LATCH TENSION. 711000-C6-1 711100-210-041 SOURCE: MRB 71.10.00/01-C5 GENERAL VISUAL INSPECTION OF FAN COWL DOORS ACCESS PANELS: 437AL, 438AR, 447AL, 448AR COWLINGS 575900-200-002 SOURCE: MRB 57.59.00/01 GENERAL VISUAL INSPECTION OF AIR INTAKE COWL AFT BULKHEAD 711000-C4-2 MRB 9 EN GVI I: 7500 FH OR 24 MO MRB 8 I: 7500 FH OR 24 MO MRB 8 711313-220-802 SOURCE: MRB 71.10.00/06-C5 711311-200-802 SOURCE: MRB 71.10.00/07-C5 ACCESS PANELS: 437AL, 438AR, 447AL, 448AR Sub 2 - Page 88 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 711300-C1-1 ZONE 430 440 DESCRIPTION FAN COWLINGS SKILL TASK CODE CODE EN FNC REV: 07 DATE: 29-Dec-2014 INTERVALS I: 20 MO SOURCE MRB 8 FUNCTIONAL CHECK OF FAN COWL LATCH TENSION 711300-C2-1 430 440 ACCESS PANELS: 437AL, 438AR, 447AL, 448AR FAN COWLINGS 430 440 ACCESS PANELS: 437AL, 438AR, 447AL, 448AR FAN SECTION EN DET 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 EN DET DETAILED INSPECTION AND RELUBRICATION OF FAN BLADE DOVETAILS, MIDSPAN SHROUDS, RETAINERS, SPACERS, DAMPERS AND FAN DISC DOVETAIL SLOTS D 724000-C4-1 450 460 PREPARATION: FAN BLADES REMOVED; COMBUSTION SECTION REFERENCES 711300-800-042 MEN TASKM. H. APPL 1 1 0.10 0.10 ALL 1 1 0.15 0.15 ALL 1 1 0.30 0.30 ALL 1 1 3.00 3.00 ALL SOURCE: MRB 71.10.00/08-C5 DETAILED INSPECTION OF THE KEEPER ASSY FAN COWL LOCKING DEVICE 722000-C1-1 TPS I: 1500 FC OR 24 MO MRB 9 LUR I: 1500 FC OR 24 MO MRB 6 LUR I: 3000 FC OR 48 MO MRB 6 LUR 711313-220-041 AOT 71-A1024 SOURCE: MRB 71.10.00/09-C5 722300-210-003 SOURCE: MRB 72.20.00/01-C5 722100-210-004 SOURCE: MRB 72.20.00/06-C5 EN BSI T: 12000 FH I: 2000 FH VSB VSB 72-0536 CFM 56-5A 1 1 0.60 0.60 EN SDI I: 1600 FC OR 72 MO MRB 6 LUR 725200-290-001 1 1 0.60 0.60 1 0.10 BORESCOPE INSPECTION OF COMBUSTION CHAMBER OUTER COWL ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR D 725000-C1-1 450 460 TURBINE SECTION BORESCOPE INSPECTION OF HPT BLADES (FROM THE FRONT AND THE REAR) SOURCE: MRB 72.50.00/01-C5 ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR 730000-C2-1 210 ENGINE FUEL & CONTROL-GENERAL EN OPC I: 1200 FH SIL 732160-740-028 SIL 73-017 ALL CORRECT FAULTS OF THE ENGINE SCHEDULED MAINTENANCE REPORT (SMR). Sub 2 - Page 89 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 731111-C1-1 ZONE 435 445 DESCRIPTION HOSE - MAIN FUEL SUPPLY SKILL TASK CODE CODE 781100-C2-1 450 460 783000-C2-1 450 460 450 460 783000-C8-1 450 460 450 460 REFERENCES MEN TASKM. H. APPL VSB VSB RA32073-5 1 1 0.70 0.70 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 SOURCE: MRB 78.11.00/02-C5 ACCESS PANELS: 451AL, 452AR, 461AL, 462AR CENTERBODY EN DET I: 6000 FH SB SB RA320 78-74 1 1 0.50 0.50 DETAILED INSPECTION OF THE EXHAUST NOZZLE, RADIUS OF THE 238-0404-5 BULKHEAD OUTER NOTE : TASK IS NOT APPLICABLE WITH SB RA32078-77 EMBODIED. THRUST REVERSER EN GVI I: 7500 FH OR 50 MO MRB 9 LUR 783241-210-042 1 1 0.20 0.20 ALL I: 24 MO MRB 8 1 1 0.20 0.20 ALL 1 1 0.20 0.20 ALL GENERAL VISUAL INSPECTION OF BLOCKER DOOR SEALS (BLOCKER DOORS DEPLOYED) 783000-C4-1 TPS T: 2000 FH I: 1200 FH NOTE GENERAL VISUAL INSPECTION OF INNER AND OUTER SEALS D 781112-C3-1 SOURCE DET 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 210 INTERVALS EN CARRY OUT LEAK CHECK OF ENGINE MAIN FUEL FEED HOSE 732500-C1-1 REV: 07 DATE: 29-Dec-2014 PREPARATION: BLOCKER DOORS DEPLOYMENT; THRUST REVERSER GENERAL VISUAL INSPECTION OF THRUST REVERSER HALF TENSION HOOK LATCH AND ADJACENT STRUCTURE (C DUCTS OPEN) THRUST REVERSER GENERAL VISUAL INSPECTION OF INNER BARREL HEATSHIELD, FIRE PROTECTIVE COATING AND FIRE SEALS (C DUCTS OPEN) EN GVI SOURCE: MRB 78.30.00/03-C5 783641-210-040 SOURCE: MRB 78.30.00/04-C5 EN GVI I: 7500 FH OR 50 MO MRB 8 LUR 783211-220-040 SOURCE: MRB 78.30.00/08-C5 Sub 2 - Page 90 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 783100-C1-1 ZONE 452 462 DESCRIPTION THRUST REVERSER CONTROL AND INDICATING SKILL TASK CODE CODE EN VCK 437 438 447 448 ACCESS PANELS: 438AR, 448AR THRUST REVERSER CONTROL AND INDICATING EN INTERVALS SOURCE I: 1500 FH OR 12 MO MRB 9 LUR I: 7500 FH OR 24 MO MRB 6 OPC I: 5000 FC OR 60 MO MRB 8 LUR GVI I: 6000 FH OR 40 MO MRB 6 LUR I: 600 FH OR 6 MO MRB 9 LUR I: 600 FH OR 6 MO MRB 6,9 LUR I: 4000 FH OR 36 MO MRB 6 LUR CHECK HYDRAULIC CONTROL UNIT FILTER POP-OUT INDICATOR POSITION 783100-C5-1 REV: 07 DATE: 29-Dec-2014 DET DETAILED INSPECTION OF ACTUATOR ROD END ATTACHMENTS (BLOCKER DOORS DEPLOYED) TPS REFERENCES 783151-210-041 MEN TASKM. H. APPL 1 1 0.10 0.10 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 0.10 0.10 1 1 0.10 0.10 1 1 0.30 0.30 SOURCE: MRB 78.31.00/02-C5 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 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 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; D 792000-C1-1 435 445 ACCESS PANELS: 437AL, 438AR, 447AL, 448AR DISTRIBUTION EN VCK CHECK SUPPLY AND SCAVENGE FILTERS CLOGGING INDICATOR POSITION D 792000-C2-1 435 445 ACCESS PANELS: 437AL, 447AL DISTRIBUTION EN DET CHECK THE FOLLOWING MAGNETIC PLUG AND SCREENS : - ACCESSORY GEARBOX SCAVENGE - AFT SUMP SCAVENGE D 792000-C3-1 435 445 ACCESS PANELS: 437AL, 447AL DISTRIBUTION REMOVE AND DISCARD SCAVENGE FILTER EN DIS 792110-210-001 SOURCE: MRB 79.20.00/01-C5 792110-210-003 SOURCE: MRB 79.20.00/02-C5 792110-920-001 SOURCE: MRB 79.20.00/03-C5 ACCESS PANELS: 437AL, 447AL Sub 2 - Page 91 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 792000-C4-1 ZONE 435 445 DESCRIPTION DISTRIBUTION SKILL TASK CODE CODE EN DIS REMOVE AND DISCARD SUPPLY FILTER D 792000-C5-1 435 445 ACCESS PANELS: 437AL, 447AL DISTRIBUTION EN DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE I: 4000 FH OR 36 MO MRB 9 LUR I: 600 FH CN MRB 6,9 VSB CHECK THE FORWARD SUMP SCAVENGE MAGNETIC PLUG AND SCREEN TPS REFERENCES MEN 792110-920-002 TASKM. H. APPL 1 1 0.30 0.30 1 1 0.10 0.10 1 1 0.10 0.10 1 1 0.30 0.30 ALL 1 1 0.20 0.20 ALL 1 1 0.30 0.30 ALL 1 0.20 2465 2497 1 0.40 2465 2497 1 1.00 2465 2497 SOURCE: MRB 79.20.00/04-C5 792110-210-004 CN 1989-181(B)R3 VSB CFM56-5A 72-A118 ACCESS PANELS: 437AL, 447AL D 792000-C6-1 435 445 DISTRIBUTION EN DET I: 600 FH MRB 6,9 VSB 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 EN SVC DRAIN AND REPLENISH OIL SYSTEM 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 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 R 237600-01-1-SDM 200 ACCESS PANELS: 438AR, 448AR GLOBAL AIRWORKS CDSS SYSTEM - CLEANING AF FNC I: 6 MO S-ICA R 237600-02-1-SDM 210 CLEAN CDSS VIDEO CAMERA HOUSING VIEWING WINDOW GLOBAL AIRWORKS CDSS SYSTEM – ADJUSTMENT/TEST AF OPC I: 12 MO S-ICA R 237600-03-1-SDM 210 CDSS SYSTEM OPERATION TEST OF MONITOR 1 AND MONITOR 2 GLOBAL AIRWORKS CDSS VISUAL/INSTALLATION 24MO INSPECTION AF FNC I: 24 MO S-ICA VISUAL AND INSTALLATION INSPECTION CDSS MONITORS, CAMERA, SYSTEM CONTROL UNIT, ON-OFF SWITCH, CIRCUIT BREAKER, CABINREADY SWITCH. SOURCE: MRB 79.20.00/02-C5 792110-210-005 VSB CFM56-5A 72-0326 JIC A320-23-76-00 STC EASA.IM.A.S.00199 ICA ICA232010006 JIC A320-23-76-01 STC EASA.IM.A.S.00199 ICA ICA232010006 JIC A320-23-76-02 STC EASA.IM.A.S.00199 ICA ICA232010006 Sub 2 - Page 92 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 256551-01-1 R 281800-10-1 ZONE 200 122 DESCRIPTION MEGAPHONE BATTERIES SKILL TASK CODE CODE CA INTERVALS TPS IGNITION PREVENTION SOURCE: MRB 25.65.51/01 281800-710-801 I: 24 MO MRB 9 MRB 8 OPERATIONAL CHECK OF CENTRE TANK FUEL PUMP GFI (SFAR88) 303100-01-1 120 PROBE ICE PROTECTION EL FNC I: 24 MO SOURCE: MRB 28.18.00/10 303100-720-001 SIL 34-084 MRB 9 FUNCTIONAL CHECK OF THE INSULATION RESISTANCE OF THE PITOT PROBE HEATER 321101-01-2 731 741 MAIN GEAR 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. 321103-01-1 321146-01-1 731 741 731 741 REFERENCES DISCARD MEGAPHONE BATTERIES OPC I: 1 YE SOURCE 256551-920-001 JIC A320-25-65-51 CMM 25-65-04 AF DIS REV: 07 DATE: 29-Dec-2014 PREPARATION: AIRCRAFT JACKED, SLIDING TUBE FULLY EXTENDED.; MAIN GEAR 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 PARTS DETAILED INSPECTION OF MAIN LANDING GEAR, RETRACTION ACTUATOR - EXTERNAL SURFACE, EXCEPT WHERE COVERED BY DRESSINGS & BUSH FLANGES. AF AF DET DET T: 6 YE I: 6 YE MRB CPCP T: 6 YE I: 6 YE MRB CPCP T: 6 YE I: 6 YE MRB CPCP NO SOURCE: MRB 30.31.00/02 321100-200-008 MEN TASKM. H. APPL 1 0.20 ALL 1 0.12 1 0.25 1679 1753 2465 2930 2964 3044 2879 2913 ALL 1 1 0.40 0.40 ALL 1 1 0.40 0.40 ALL 1 1 0.60 0.60 ALL SOURCE: MRB 321101-01-2 321100-200-009 SOURCE: MRB 321103-01-1 321100-200-018 SOURCE: MRB 321146-01-1 Sub 2 - Page 93 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 321156-01-1 321156-01-2 322141-01-1 ZONE 731 741 731 741 711 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 PARTS SKILL TASK CODE CODE AF AF AF DET DET DET 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 322143-01-1 711 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 DETAILED INSPECTION OF NOSE LANDING GEAR, FORESTAY UPPER PANEL, LOWER LINK AND UNIVERSAL JOINT EXTERNAL SURFACES, EXCEPT WHERE COVERED BY DRESSINGS AND BUSH FLANGES. AF AF DET DET REV: 07 DATE: 29-Dec-2014 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 T: 6 YE I: 6 YE MRB CPCP TPS REFERENCES 321100-200-019 MEN TASKM. H. APPL 1 1 0.67 0.67 1 1 0.67 0.67 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1 0.18 ALL 1 0.13 ALL 1 0.20 ALL SOURCE: MRB 321156-01-1 321100-200-019 SOURCE: MRB 321156-01-2 322100-200-018 SOURCE: MRB 322141-01-1 322100-200-013 SOURCE: MRB 322142-01-1 322100-200-014 SOURCE: MRB 322143-01-1 Sub 2 - Page 94 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 322144-01-1 322145-01-1 322151-01-1 335100-01-1-SDM R 336000-01-1-SDM ZONE DESCRIPTION SKILL TASK CODE CODE 711 NOSE LANDING GEAR PARTS AF 711 DETAILED INSPECTION OF NOSE LANDING GEAR, LOCK LINK UPPER AND LOCK LINK LOWER - EXTERNAL SURFACES, EXCEPT WHERE COVERED BY DRESSINGS AND BUSH FLANGES. 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 200 DETAILED INSPECTION OF NOSE LANDING GEAR, ACTUATING CYLINDER - EXTERNAL SURFACES, EXCEPT WHERE COVERED BY DRESSINGS AND BUSH FLANGES. LHT EMERGENCY ESCAPE PATH. CABIN EMERGENCY LIGHTING AF 200 VISUAL INSPECTION OF PHOTOLUMINESCENT FLOOR PATH MARKING FOR CRACKS AND PROPER INSTALLATION SAFTGLO. DAILY SYSTEM CHARGING INTERVALS SOURCE R 336000-03-1-SDM REFERENCES MRB CPCP T: 6 YE I: 6 YE MRB CPCP T: 6 YE I: 6 YE MRB CPCP GVI I: 3 MO S-ICA JIC A320-33-51-00 STC 10014013 ICA A320-EB33-0300 AF SVC I: DY S-ICA AF DET DET MEN 322100-200-012 TASKM. H. APPL 1 0.20 ALL 1 0.73 ALL 1 0.33 ALL 1 0.20 1654 1679 1753 JIC A320-33-60-00 STC ST02292AT ICA L67-10 1 TBD 2465 2497 SOURCE: MRB 322144-01-1 322100-200-009 SOURCE: MRB 322145-01-1 322100-200-015 SOURCE: MRB 322151-01-1 PERFORM INITIAL DAILY CHARGE PER APPROVED PROCEDURES BY ACTIVATING CABIN LIGHTING R 336000-02-1-SDM TPS T: 6 YE I: 6 YE AF DET REV: 07 DATE: 29-Dec-2014 200 SAFTGLO. INSPECTION AND SERVICING-CLEANING AF SVC S-ICA JIC A320-33-60-01 STC ST02292AT ICA L67-10 1 TBD 2465 2497 200 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 SAFTGLO. FUNCTIONAL CHECK AF I: 7500 FH OR 24 MO FNC I: 7500 FH OR 24 MO S-ICA JIC A320-33-60-02 STC ST02292AT ICA L67-10 1 TBD 2465 2497 INSPECTION INTERIOR LIGHTING: OVERALL CEILING LIGHTING, INOPERATIVE CEILING LAMPS AT LIFE RAFT AREA, MISSING ELECTRICALLY ILLUMINATED EXIT MARKER Sub 2 - Page 95 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 336000-04-1-SDM ZONE 200 DESCRIPTION SAFTGLO. GENERAL VISUAL INSPECTION SKILL TASK CODE CODE REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 200 120 315 TASKM. H. APPL I: 90 DY S-ICA JIC A320-33-60-03 STC ST02292AT ICA L67-10 1 TBD 2465 2497 AF FNC I: 10 YE S-ICA JIC A320-33-60-04 STC ST02292AT ICA L67-10 1 TBD 2465 2497 RA RST I: 72 MO OR 30000 FH NOTE SIL 344100-100-801 SIL 34-102 1 0.42 1654 1679 1753 2465 2497 NOTE: DEPENDING ON OPERATING ENVIRONMENT AND THE OPERATOR'S EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED. STARTER MOTOR EN VCK I: 600 FH EASA AD ISB 1 0.10 DET T: 12 YE I: 12 YE MRB CPCP 1 1 0.23 0.23 ALL T: 14800 FC I: 14800 FC T: 12 YE I: 6 YE ALI 1 1 0.15 0.15 ALL 1 1 0.50 0.50 ALL SAFTGLO. INSPECTION AND FUNCTIONAL CHECK. WEATHER RADAR SYSTEM REMOVE WEATHER RADAR TRANSCEIVER MOUNTING TRAY FILTER FOR CLEANING D 494251-01-1 MEN GVI INSPECTION AND FUNCTIONAL CHECK TEST COUPON (FWD RH CABIN) 344100-02-1 REFERENCES AF GVI OF FLOOR MOUNTED COMPONENTS AND INTERIOR LIGHTING R 336000-05-1-SDM TPS CHECK WEAR INDICATOR OF STARTER MOTOR BRUSH 521101-01-1 831 841 ACCESS PANELS: 315AL FWD PAX/CREW DOOR STOP ASSEMBLIES AF DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ON FORWARD PASSENGER/CREW DOOR, LH/RH 521103-01-1 521104-01-1 831 841 831 841 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 DETAILED INSPECTION OF FORWARD PASSENGER/CREW DOOR, INTERNAL STRUCTURE, LH/RH AF AF GVI DET 521100-200-001 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; ACCESS PANELS: 831, 841 Sub 2 - Page 96 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 521104-02-2 ZONE 831 841 DESCRIPTION FWD PAX/CREW DOOR INTERNAL STRUCTURE SKILL TASK CODE CODE NDT SDI SPECIAL DETAILED INSPECTION (LFEC) OF FORWARD PASSENGER/CREW DOOR, INTERNAL STRUCTURE, LH/RH. NOTE: TASK 521104-02-2 NEED TO BE PERFORMED AT SAME TIME AS TASK 521104-01-1 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 12 YE I: 6 YE MRB CPCP T: 12 YE I: 12 YE MRB CPCP T: 14800 FC I: 14800 FC T: 12 YE I: 6 YE ALI T: 12 YE I: 6 YE MRB CPCP T: 12 YE OR 39300 FC I: 6 YE OR 11400 FC ALI MRB CPCP TPS REFERENCES 521100-250-001 NTM 52-11-04 MEN TASKM. H. APPL 1 1 1.00 1.00 1 1 0.23 0.23 ALL 1 1 0.15 0.15 ALL 1 1 0.50 0.50 ALL 1 1 1.00 1.00 1 1 1 1 1.00 1.00 1.00 1.00 SOURCE: MRB 521104-02-2 PREPARATION: LINING REMOVED; INSULATION REMOVED; 521301-01-1 832 842 ACCESS PANELS: 831, 841 AFT PAX/CREW DOOR STOP ASSEMBLIES AF DET DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ON AFT PASSENGER/CREW DOOR, LH/RH 521303-01-1 521304-01-1 832 842 832 842 ACCESS PANELS: 832, 842 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 AF AF GVI DET DETAILED INSPECTION OF AFT PASSENGER/CREW DOOR, INTERNAL STRUCTURE, LH/RH 521300-200-001 SOURCE: MRB 521301-01-1 MRB CPCP 521300-210-002 SOURCE: ALI 521303-01-1 1+2 521300-200-002 SOURCE: MRB 521304-01-1 PREPARATION: LINING REMOVED; INSULATION REMOVED; D 521304-02-2 832 842 ACCESS PANELS: 832, 842 AFT PAX/CREW DOOR INTERNAL STRUCTURE NDT SDI SPECIAL DETAILED INSPECTION (LFEC) OF AFT PASSENGER/CREW DOOR, INTERNAL STRUCTURE, LH/RH. NOTE: TASK 521304-02-2 NEED TO BE PERFORMED AT SAME TIME AS TASK 521304-01-1 R 522102-01-1 833 834 843 844 ACCESS PANELS: 832, 842 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 521300-250-001 NTM 52-13-04 SOURCE: MRB 521304-02-2 1 522100-200-001 SOURCE: ALI 522102-01-1 MRB 522102-01-1 2930 2964 3044 Sub 2 - Page 97 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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; R 522103-01-1 833 834 843 844 ACCESS PANELS: 834, 844 EMERGENCY EXITS STRUCTURE REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 12 YE OR 39300 FC I: 6 YE OR 11400 FC T: 24000 FC I: 4500 FC ALI MRB CPCP ISB TPS 1 REFERENCES 522100-200-001 MEN TASKM. H. APPL 1 1 1.00 1.00 1654 1679 1753 2465 2497 2879 2913 522100-200-003 ISB 52-1145 1 1 1 1 2.00 2.00 2.00 2.00 2930 2964 3044 SOURCE: ALI 522102-01-2 MRB 522102-01-2 NDT SDI NDT SDI T: 24000 FC I: 4500 FC ISB 522100-200-003 ISB 52-1145 1 1 2.00 2.00 2465 2497 2879 2913 AF GVI T: 12500 FC OR 25000 FH I: 12500 FC OR 25000 FH T: 12 YE I: 6 YE ALI 523111-200-011 1 0.10 ALL 1 1.50 ALL T: 5300 FC I: 5300 FC MRB 1 0.33 ALL SPECIAL DETAILED INSPECTION OF OVERWING EMERGENCY EXIT FRAME. PREPARATION: LINING REMOVED; INSULATION REMOVED; 522103-01-2 834 844 ACCESS PANELS: 833, 834, 843, 844 EMERGENCY EXITS STRUCTURE SPECIAL DETAILED INSPECTION OF OVERWING EMERGENCY EXIT FRAME. PREPARATION: LINING REMOVED; INSULATION REMOVED; 523101-01-1 825 ACCESS PANELS: 834, 844 FWD CARGO COMPARTMENT DOOR SKIN GENERAL VISUAL INSPECTION OF FORWARD CARGO COMPARTMENT DOOR SKIN, EXTERNAL SURFACE 523103-01-1 825 FWD CARGO DOOR INTERNAL STRUCTURE AF DET DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT DOOR, INTERNAL STRUCTURE SOURCE: ALI 523101-01-1 MRB CPCP 1 523111-200-001 SOURCE: MRB 523103-01-1 PREPARATION: LINING REMOVED; INSULATION REMOVED; 523105-01-3 825 ACCESS PANELS: 825 FWD CARGO COMPARTMENT DOOR ACTUATOR GENERAL VISUAL INSPECTION OF FORWARD CARGO COMPARTMENT DOOR, ACTUATOR ATTACH FITTINGS AF GVI 523111-200-022 SOURCE: MRB 523105-01-3 ACCESS PANELS: 825 Sub 2 - Page 98 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 523106-01-1 ZONE 825 DESCRIPTION FWD CARGO DOOR UNDER HINGE FITTINGS SKILL TASK CODE CODE NDT SDI SPECIAL DETAILED INSPECTION (ROTO) OF FORWARD CARGO COMPARTMENT DOOR SKIN, UNDERNEATH HINGE FITTINGS AT SELECTED BOLT HOLES PREPARATION: BOLTS REMOVED; LINING REMOVED; INSULATION REMOVED; ACCESS PANELS: 825 523108-01-1 825 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 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 AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS ST: 12 YE SI: 12 YE T: 24 YE OR 40000 FC OR 80000 FH I: 12 YE OR 23400 FC OR 46900 FH 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 SOURCE TPS ALI MRB CPCP REFERENCES 523111-200-006 NTM 52-31-06 MEN TASKM. H. APPL 1 0.50 1 0.30 ALL 1 0.50 ALL SOURCE: ALI 523106-01-1 MRB 523106-01-1 ALI MRB CPCP 1 523111-200-004 SOURCE: ALI 523108-01-1 MRB 523108-01-1 MRB CPCP 1 523111-200-005 SOURCE: MRB 523109-01-1 Sub 2 - Page 99 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 523109-02-1 ZONE 825 DESCRIPTION FWD CARGO DOOR LOCKING HOOKS SKILL TASK CODE CODE AF GVI 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 R 523111-01-1 826 AFT CARGO DOOR SKIN AF GVI GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT DOOR SKIN, EXTERNAL SURFACE R 523113-01-1 826 AFT CARGO DOOR INTERNAL STRUCTURE AF DET DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR, INTERNAL STRUCTURE REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 10300 FC OR 20700 FH I: 10300 FC OR 20700 FH 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 ST: 12 YE SI: 12 YE T: 24 YE OR 40000 FC OR 80000 FH I: 12 YE OR 23400 FC OR 46900 FH ALI MRB CPCP TPS REFERENCES 523111-200-013 MEN TASKM. H. APPL 1 0.30 ALL 1 0.10 2930 2964 3044 1 1.50 2930 2964 3044 1 0.10 2930 2964 3044 1 0.50 SOURCE: ALI 523109-02-1 ALI 523211-200-011 SOURCE: ALI 523111-01-1 MRB CPCP 1 523211-200-001 SOURCE: MRB 523113-01-1 PREPARATION: LINING REMOVED; INSULATION REMOVED; R 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 D 523116-01-1 826 ACCESS PANELS: 826 AFT CARGO DOOR UNDER HINGE FITTINGS SPECIAL DETAILED INSPECTION (ROTO) OF AFT CARGO COMPARTMENT DOOR SKIN UNDERNEATH HINGE FITTINGS AT SELECTED BOLT HOLES PREPARATION: BOLTS REMOVED; LINING REMOVED; INSULATION REMOVED; ACCESS PANELS: 826 NDT SDI 523211-200-022 SOURCE: MRB 523115-01-3 523211-200-003 NTM 52-31-16 SOURCE: ALI 523116-01-1 MRB 523116-01-1 Sub 2 - Page 100 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 523118-01-2 ZONE 826 DESCRIPTION AFT CARGO DOOR FITTINGS EXTERNAL AREA SKILL TASK CODE CODE 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 R 523119-01-2 826 AFT CARGO DOOR LOCKING HOOKS 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 R 523119-02-2 826 AFT CARGO DOOR LOCKING HOOKS 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 D 523130-01-1 825 826 FWD / AFT CARGO DOOR HANDLE DETAILED INSPECTION OF BEARING HOUSING OF THE FORWARD / AFT CARGO DOOR LOCKING HANDLE AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS 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 T: 4500 FC I: 4500 FC SOURCE ALI MRB CPCP TPS 1 REFERENCES 523211-200-005 MEN TASKM. H. APPL 1 0.30 2930 2964 3044 1 0.50 2930 2964 3044 1 0.30 2930 2964 3044 1 1 0.40 0.40 SOURCE: ALI 523118-01-2 MRB 523118-01-2 MRB CPCP 1 523211-200-006 SOURCE: MRB 523119-01-2 ALI 523211-200-012 SOURCE: ALI 523119-02-2 ISB 523000-220-001 ISB 52-1127 ACCESS PANELS: 825, 825AR, 826, 826AR Sub 2 - Page 101 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 523131-01-1 ZONE 825 826 DESCRIPTION FWD / AFT CARGO DOOR FRAME SKILL TASK CODE CODE REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE TPS REFERENCES MEN TASKM. H. APPL NDT SDI T: NOTE I: 15000 FC ISB ISB 52-1032 1 1 7.50 7.50 AF GVI T: 4500 FC I: 4500 FC T: 12 YE I: 6 YE ALI 523211-200-013 1 0.30 MRB CPCP SOURCE: ALI 523211-01-1 523211-200-007 1 0.30 T: 5300 FC I: 5300 FC MRB 1 0.30 1654 1679 1753 2465 2497 2879 2913 ST: 30000 FC SI: 15000 FC T: 35200 FC I: 15000 FC ALI MRB 1 0.30 1654 1679 1753 2465 2497 2879 2913 SPECIAL DETAILED INSPECTION OF FWD AND AFT CARGO COMPARTMENT DOOR FRAME FORK ENDS AND OUTER SKIN NOTE: FOR THRESHOLD AND INTERVAL REFER TO SB 52-1032. PREPARATION: CARGO COMP DOOR LININGS; INSULATION REMOVED; 523211-01-1 523213-01-1 826 ACCESS PANELS: 825, 826 AFT CARGO DOOR SKIN EXTERNAL 826 GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT DOOR SKIN, EXTERNAL SURFACE AFT CARGO DOOR INTERNAL STRUCTURE AF DET DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR, INTERNAL STRUCTURE 1 SOURCE: MRB 523213-01-1 1654 1679 1753 2465 2497 2879 2913 1654 1679 1753 2465 2497 2879 2913 PREPARATION: LINING REMOVED; INSULATION REMOVED; 523215-01-1 826 ACCESS PANELS: 826 AFT CARGO DOOR ACTUATOR ATTACH FITTINGS AF GVI GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT DOOR ACTUATOR ATTACH FITTINGS 523217-01-1 826 ACCESS PANELS: 826 AFT CARGO DOOR FITTINGS INTERNAL AREA DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR, HINGE FITTINGS ATTACHMENT AREA, INTERNAL PREPARATION: LINING REMOVED; INSULATION REMOVED; ACCESS PANELS: 826 AF DET 523211-200-014 SOURCE: MRB 523215-01-1 523211-200-010 SOURCE: ALI 523217-01-1 MRB 523217-01-1 Sub 2 - Page 102 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 523218-01-1 ZONE 826 DESCRIPTION AFT CARGO DOOR FITTINGS EXTERNAL AREA SKILL TASK CODE CODE 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) R 523301-01-1 R 523303-01-1 827 ACCESS PANELS: 826 BULK CARGO DOOR SKIN EXTERNAL 827 GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT DOOR SKIN, EXTERNAL SURFACE BULK CARGO DOOR INTERNAL DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR, INTERNAL STRUCTURE AF AF GVI DET REV: 07 DATE: 29-Dec-2014 INTERVALS 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 T: 7500 FC I: 7500 FC T: 12 YE I: 6 YE SOURCE ALI MRB CPCP TPS 1 REFERENCES 523211-200-008 MEN TASKM. H. 1 0.30 1654 1679 1753 2465 2497 2879 2913 1 0.50 1654 1679 1753 2465 2497 2879 2913 1 0.30 1654 1679 1753 2465 2497 2879 2913 SOURCE: ALI 523218-01-1 MRB 523218-01-1 MRB CPCP 1 523211-200-009 SOURCE: MRB 523219-01-1 ALI 523211-200-015 APPL SOURCE: ALI 523219-02-1 ALI 523311-200-004 1 0.10 2930 2964 3044 MRB CPCP SOURCE: ALI 523301-01-1 523311-200-003 1 0.20 2930 2964 3044 1 SOURCE: MRB 523303-01-1 PREPARATION: LINING REMOVED; INSULATION REMOVED; ACCESS PANELS: 827 Sub 2 - Page 103 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 523305-01-1 ZONE 827 DESCRIPTION BULK CARGO DOOR FITTINGS AREA SKILL TASK CODE CODE AF DET DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR STOP FITTINGS AND ATTACHMENT AREA, EXTERNAL AND INTERNAL REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 12 YE I: 12 YE MRB CPCP 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 T: 6 YE I: 6 YE MRB CPCP TPS 1 REFERENCES 523311-200-002 MEN TASKM. H. APPL 1 0.75 2930 2964 3044 1 0.30 ALL 1 0.20 ALL 1 0.20 ALL 1 0.20 ALL 1 1 0.15 0.15 ALL SOURCE: MRB 523305-01-1 PREPARATION: LINING REMOVED; INSULATION REMOVED; 524111-01-1 811 ACCESS PANELS: 827 FWD AVIONIC DOOR INTERNAL STRUCTURE AF DET DETAILED INSPECTION OF FORWARD AVIONICS COMPARTMENT ACCESS DOOR, INTERNAL STRUCTURE, INCLUDING HINGE ARMS 1 524111-200-001 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; 528101-01-1 734 744 ACCESS PANELS: 812 MLG DOOR FWD AND AFT FITTING DETAILED INSPECTION OF MLG DOOR, FORWARD AND AFT FITTINGS, LH/RH AF DET 1 528100-200-001 SOURCE: MRB 528101-01-1 ACCESS PANELS: 734, 744 Sub 2 - Page 104 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 528101-02-1 ZONE 734 744 DESCRIPTION MLG DOOR FWD FITTING SKILL TASK CODE CODE 734 744 ACCESS PANELS: 734, 744 MAIN GEAR DOORS INTERVALS SOURCE TPS REFERENCES MEN TASKM. H. APPL NDT SDI T: 9000 FC I: 800 FC CN ISB 528100-200-004 NTM 52-81-14 CN 2003-434(B) ISB 52-1096 1 1 1.50 1.50 NDT SDI T: 18800 FC I: 3600 FC MRB 528100-280-801 NTM 52-81-06 1 1 1.00 1.00 ALL T: 49100 FC I: 2800 FC ALI 1 1 0.15 0.15 ALL T: 6 YE I: 6 YE MRB CPCP 1 1 0.15 0.15 ALL T: 6 YE I: 6 YE MRB CPCP 1 1 0.15 0.15 ALL T: 26000 FC I: 7500 FC MRB 1 1 0.17 0.17 ALL SPECIAL DETAILED INSPECTION (EC) OF MLG DOOR, FORWARD FITTING, IN KINK AND NERVE AREA, LH/RH 528106-01-1 REV: 07 DATE: 29-Dec-2014 SPECIAL DETAILED INSPECTION (HFEC & US) OF MLG DOOR ACTUATOR LUGS, LH/RH 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 AF DET DETAILED INSPECTION OF NLG, MAIN DOOR HINGES, LH/RH 528221-01-1 715 716 ACCESS PANELS: 713, 714 NLG SECONDARY DOOR HINGES AF DET DETAILED INSPECTION OF NLG, SECONDARY DOOR HINGES, LH/RH 528223-01-1 715 716 ACCESS PANELS: 715, 716 NOSE GEAR DOORS DETAILED INSPECTION OF NLG AFT DOOR AFT FITTINGS, LH/RH AF DET 1 528200-200-001 SOURCE: MRB 528211-01-1 1 528200-200-002 SOURCE: MRB 528221-01-1 528200-220-801 SOURCE: MRB 528223-01-1 ACCESS PANELS: 715, 716 Sub 2 - Page 105 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 531101-01-1 ZONE 220 DESCRIPTION FWD PAX/CREW DOOR SKILL TASK CODE CODE AF DET DETAILED INSPECTION OF FWD PASSENGER/CREW DOOR CUTOUT, INTERCOSTALS FITTINGS N°7 BETWEEN FR15-16 AND FR20-21, LH/RH REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 NOTE I: 16800 FC NOTE ALI MRB CPCP ST: 48000 FC OR 96000 FH SI: 8000 FC OR 16000 FH MRB TPS REFERENCES 531100-220-802 MEN TASKM. H. APPL 1 0.40 ALL 1 0.30 ALL 1 1 0.93 0.93 2930 2964 3044 1 0.20 ALL 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 R 531103-01-1 221 222 MAIN STRUCTURE NDT SDI 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. PREPARATION: INSULATION REMOVED; LINING REMOVED; STOP FITTING BOLT REMOVED; CEILING PANELS REMOVED; GALLEY & TOILET IF INSTALLED; 531104-01-1 220 ACCESS PANELS: 831, 841 DOOR FRAME FWD LOWER CORNER 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 AF DET 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 531100-210-002 SOURCE: MRB 531104-01-1 PREPARATION: FWD CORNER SCUFF PLATE REMOVED; Sub 2 - Page 106 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 531104-02-1 ZONE 220 DESCRIPTION DOOR FRAME EXTERNAL SURFACE SKILL TASK CODE CODE 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 R 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; R 531105-02-1 211 212 MAIN STRUCTURE NDT SDI 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. REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 ST: 30000 FC SI: 20000 FC MRB TPS REFERENCES 531100-210-028 NTM 53-11-04 MEN TASKM. H. APPL 1 0.50 ALL 1 1 0.30 0.30 2930 2964 3044 1 1 0.50 0.50 2930 2964 3044 1 0.20 ALL 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 PREPARATION: SLIDING WINDOW OPENED; 531107-01-1 110 FWD PRESSURE BULKHEAD 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 AF DET 531100-210-003 SOURCE: MRB 531107-01-1 PREPARATION: UPPER PROTECTIVE SHIELD; ACCESS PANELS: 110AL Sub 2 - Page 107 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 531108-01-1 ZONE 123 DESCRIPTION MAIN STRUCTURE SKILL TASK CODE CODE 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 531112-01-1 100 AVIONICS DOORS SURROUND 100 GENERAL VISUAL INSPECTION OF AVIONICS COMPARTMENT DOORS, SURROUND CORNERS, EXTERNAL SURFACE (4 DOORS) FUSELAGE LOWER PANEL EXTERNAL SURFACE DETAILED INSPECTION OF FUSELAGE LOWER PANEL AT NLG BAY AFT CORNERS, EXTERNAL SURFACE, LH/RH AF AF GVI DET REV: 07 DATE: 29-Dec-2014 INTERVALS 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 T: 16300 FC OR 32600 FH I: 16300 FC OR 32600 FH SOURCE ALI MRB TPS REFERENCES 531100-220-804 NTM 53-11-08 MEN TASKM. H. APPL 1 0.37 2930 2964 3044 1 1 0.13 0.13 ALL 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 1 0.20 ALL ALI SOURCE: ALI 531111-01-1 531100-210-005 1 0.30 ALL SOURCE: ALI 531112-01-1 Sub 2 - Page 108 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 531113-01-1 531114-01-1 531117-01-1 531118-01-1 ZONE DESCRIPTION 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 SKILL TASK CODE CODE 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 D 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 AF DET DETAILED INSPECTION OF UPPER SKIN OF LOWER LONGITUDINAL LAP JOINT, BETWEEN FR 9 AND FR 20, EXTERNAL SURFACE, LH/RH 531120-01-1 200 UPPER LAP JOINT EXTERNAL SURFACE 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 AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE TPS REFERENCES MEN TASKM. H. APPL T: 41400 FC I: 7400 FC T: 5700 FC I: 5700 FC ALI 531100-210-818 1 0.25 ALL ALI SOURCE: ALI 531113-01-1 531100-210-006 1 0.50 ALL T: 14500 FC I: 14500 FC ALI 1 0.10 ALL T: 100 DY NOTE I: 4300 FC ALI 1 0.25 ALL ST: 30000 FC SI: 12600 FC T: 41000 FC I: 12600 FC ST: 30000 FC SI: 11700 FC T: 35300 FC I: 11700 FC ST: 30000 FC SI: 18500 FC ALI MRB 1 0.60 1 0.60 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1 0.30 ALL 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 MRB 531100-210-008 SOURCE: MRB 531120-01-1 Sub 2 - Page 109 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 531121-01-1 531123-01-1 ZONE DESCRIPTION 100 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 DET DET DETAILED INSPECTION OF OUTER SKIN OF LATERAL LONGITUDINAL LAP JOINT, BETWEEN FR 1 AND FR 24, LH/RH D 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 ST: 30000 FC SI: 9900 FC T: 42400 FC I: 9900 FC ALI MRB TPS REFERENCES 531100-210-009 MEN TASKM. H. APPL 1 0.30 ALL 1 1.00 ALL 1 1 0.15 0.15 1 1 0.15 0.15 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1 1 0.17 0.17 ALL 1 1 0.28 0.28 ALL 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 AF DET DETAILED INSPECTION OF CENTRAL/LATERAL WINDOW FRAME AROUND FASTENER HOLE, UPPER AREA, LH/RH 531127-01-1 211 212 PREPARATION: SLIDING WINDOW OPENED; MAIN STRUCTURE SPECIAL DETAILED INSPECTION (HFEC) OF LATERAL SPLICING, FR11, LH/RH PREPARATION: INSULATION REMOVED; LINING REMOVED; NDT SDI 531100-220-805 SOURCE: MRB 531125-02-1 531100-220-807 NTM 53-11-27 SOURCE: ALI 531127-01-1 MRB 531127-01-1 Sub 2 - Page 110 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 531129-02-2 ZONE 211 212 DESCRIPTION WINDSHIELD CTR POST LWR ATTACHMENT SKILL TASK CODE CODE 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 T: 26700 FC I: 2700 FC ALI TPS REFERENCES 531100-220-001 NTM 53-11-29 MEN TASKM. H. APPL 1 1 0.50 0.50 1 1 0.50 0.50 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1 1 0.15 0.15 2930 2964 3044 1 1 0.20 0.20 ALL 1 1 0.20 0.20 ALL 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; R 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 AF DET DETAILED INSPECTION OF WINDSHIELD CENTER POST, UPPER ATTACHMENT AREA, INTERNAL SIDE 531133-01-1 211 212 ACCESS PANELS: 211LC, 211MC, 211MW, 212LC WINDSHIELD SIDE POST LWR ATTACHMENT 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 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 531100-210-014 SOURCE: ALI 531133-01-1 PREPARATION: SLIDING WINDOW OPENED; ACCESS PANELS: 211NW, 211PW, 212NW, 212PW Sub 2 - Page 111 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 531133-02-1 ZONE 211 212 DESCRIPTION WINDSHIELD SIDE POST LWR ATTACHMENT SKILL TASK CODE CODE NDT SDI SPECIAL DETAILED INSPECTION (HFEC) OF WINDSHIELD SIDE POST AT FR 4, LOWER ATTACHMENT, INTERNAL SIDE, LH/RH REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 T: 12 YE I: 12 YE MRB CPCP TPS REFERENCES 531100-210-029 NTM 53-11-33 MEN TASKM. H. APPL 1 1 0.50 0.50 ALL 1 1 0.50 0.50 1 1 0.50 0.50 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1 0.20 ALL 1 1 0.40 0.40 ALL SOURCE: ALI 531133-02-1 NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531133-01-1 PREPARATION: SLIDING WINDOW OPENED; D 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 531151-01-1 200 221 222 SIDE WINDOW STRUCTURE DETAILED INSPECTION OF SIDE WINDOW STRUCTURE, UPPER JUNCTION, BETWEEN FORWARD AND REAR FR, EXTERNAL SURFACE, LH/RH DOOR STOP FITTINGS DETAILED INSPECTION OF DOOR STOP FITTINGS ON FR 16 AND FR 20, LH/RH AF AF DET DET 531100-210-015 SOURCE: MRB 531141-01-1 531100-210-017 SOURCE: MRB 531151-01-1 PREPARATION: LINING REMOVED; ACCESS PANELS: 831, 841 Sub 2 - Page 112 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 531153-02-1 ZONE 221 222 DESCRIPTION DOOR STOPS AT FR 16 SKILL TASK CODE CODE 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. REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 T: 6 YE I: 6 YE MRB CPCP TPS REFERENCES 531100-210-025 NTM 53-11-53 MEN TASKM. H. APPL 1 1 1.00 1.00 ALL 1 1 1.00 1.00 ALL 1 1 0.75 0.75 1 1 0.75 0.75 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1 0.20 ALL 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 D 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 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 531157-01-2 PREPARATION: FLOOR PANELS REMOVED; LADDER; 531161-01-1 123 ACCESS PANELS: 824 NLG BAY ALL PANELS GENERAL VISUAL INSPECTION OF NLG BAY, ALL PANELS, LH/RH AF GVI 1 531100-210-803 SOURCE: MRB 531161-01-1 ACCESS PANELS: 713, 714 Sub 2 - Page 113 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 531162-01-1 ZONE 127 128 DESCRIPTION NLG BAY SKILL TASK CODE CODE 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 AF DET 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 T: 6 YE I: 6 YE MRB CPCP TPS REFERENCES 531100-210-018 MEN TASKM. H. APPL 1 1 0.45 0.45 1 1 0.45 0.45 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1 1 0.80 0.80 ALL 1 1 0.50 0.50 ALL 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; 531164-01-1 125 126 ACCESS PANELS: 831, 841 FUSELAGE FR 15-21 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. AF DET 1 531100-210-801 SOURCE: MRB 531164-01-1 PREPARATION: INSULATION REMOVED; ACCESS PANELS: 812, 824 Sub 2 - Page 114 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 531166-01-1 ZONE 221 222 DESCRIPTION FUSELAGE FR 16-20 SKILL TASK CODE CODE 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. REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 ST: 30000 FC SI: 5700 FC T: 36700 FC I: 5700 FC ALI MRB TPS REFERENCES 1+2 531100-220-006 MEN TASKM. H. APPL 1 1 0.80 0.80 1 1 0.80 0.80 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1 0.20 ALL 1 1 1.50 1.50 ALL 1 0.30 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 AF GVI 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 1 531100-210-036 SOURCE: MRB 531167-01-1 1 531100-210-804 SOURCE: MRB 531169-01-1 PREPARATION: INSULATION REMOVED; D 531170-01-1 200 ACCESS PANELS: 812, 822 COCKPIT WINDSHIELD LOWER FRONT FTG 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. AF DET 531100-210-038 SOURCE: ALI 531170-01-1 MRB 531170-01-1 PREPARATION: LOWER RETAINERS; Sub 2 - Page 115 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 531170-01-2 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 531170-02-2 D 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. REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE ST: 30000 FC SI: 5500 FC T: 36700 FC I: 5500 FC ALI MRB 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. H. 1 0.30 1 1.00 1 1.00 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1 1 0.20 0.20 ALL 1 0.50 ALL SOURCE: ALI 531170-01-2 MRB 531170-01-2 531100-210-039 NTM 53-11-70 APPL 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 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 116 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 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 117 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 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 118 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 531189-01-1 531189-01-2 D 531190-01-1 531190-01-2 531191-01-1 ZONE 211 212 221 222 231 232 211 212 221 222 231 232 221 222 231 232 221 222 231 232 121 122 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 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 PREPARATION: CABIN FLOOR PANELS; 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 REV: 07 DATE: 29-Dec-2014 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 1+2 531100-210-805 SOURCE: MRB 531190-01-1 1+2 531100-210-805 SOURCE: MRB 531190-01-2 1 531100-220-002 MEN TASKM. H. APPL 1 1 1 1 1 1 0.25 0.25 0.25 0.25 0.25 0.25 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 1 1 1 1 1.20 1.20 1.20 1.20 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1 1 1.50 1.50 ALL 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 SOURCE: MRB 531191-01-1 PREPARATION: FORWARD AVIONICS BAY FLOOR PANELS REMOVED; INSULATION DISPLACED; WIRING BUNDLES DISPLACED; ACCESS PANELS: 811 Sub 2 - Page 119 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 12 YE I: 12 YE MRB CPCP T: 12 YE I: 12 YE MRB CPCP T: 38200 FC OR 76400 FH I: 5000 FC OR 10000 FH T: 30000 FC OR 60000 FH I: 5000 FC OR 10000 FH ISB ISB EASA AD TPS 1 REFERENCES 531100-210-806 MEN TASKM. H. APPL 1 1 1 1 1.00 1.00 1.00 1.00 ALL 1 1 0.30 0.30 ALL ISB 53-1257 1 1 12.00 12.00 ALL JIC A320-54-12-00 EASA AD 2013-0122 ISB 53-1259 1 2.00 ALL SOURCE: MRB 531192-01-1 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; 531257-01-1 150 160 ACCESS PANELS: 824 TACK HOLES AT FR50-FR63 NDT SDI SPECIAL DETAILED INSPECTION (HFEC) OF TACK HOLES AT FR50-FR63 BETWEEN P33-P39 (LH ONLY) IN CARGO FLOOR AREA. R 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 PANEL DETAILED INSPECTION OF OF TI-ANGLE CONNECTION BETWEEN BELLY FAIRING AND KEEL BEAM SIDE PANEL FR41-FR42, RH/LH. ACCESS PANELS: 147BZ 148AZ AF DET SOURCE: EASA AD Sub 2 - Page 120 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 531260-01-1 ZONE 240 250 DESCRIPTION SPLICE PLATE OF FR47 BUTT JOINT CROSSING AREA SKILL TASK CODE CODE NDT SDI AF DET NDT SDI NDT SDI AF GVI 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. R 531277-01-1 240 EMERGENCY EXIT DOOR HATCHES IN SECTION 15 SPECIAL DETAILED INSPECTION OF THE EMERGENCY EXIT DOOR HATCHES (LH/RH) IN SECTION 15. 532102-01-1 231 232 FLOOR STRUCTURE FR 24-35 GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE, EXCLUDING AREAS BELOW GALLEYS AND TOILETS (IF INSTALLED), BETWEEN FR 24 AND FR 35 REV: 07 DATE: 29-Dec-2014 INTERVALS 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 T: 48000 FC OR 96000 FH I: 6000 FC OR 12000 FH T: 12 YE I: 12 YE SOURCE TPS REFERENCES MEN TASKM. H. APPL ISB ISB 53-1260 1 1 21.00 21.00 ISB ISB 53-1269 1 1.00 ALL ISB ISB 53-1269 1 1.00 ALL ISB ISB 53-1277 1 5.00 2930 2964 3044 532100-210-001 2 2 1.50 1.50 ALL MRB CPCP 1 SOURCE: MRB 532102-01-1 PREPARATION: CABIN FLOOR PANELS; Sub 2 - Page 121 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 532104-01-1 ZONE 131 132 DESCRIPTION FLOOR STRUCTURE SKILL TASK CODE CODE NDT SDI 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; D 532120-01-1 231 232 ACCESS PANELS: 825 FRAME WEBS AF DET DETAILED INSPECTION OF FRAME WEBS AT STRINGER 18 LH/RH FOR FR 25, 26, 27, 28, 32, 33, 34 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 43400 FC OR 86900 FH I: 35600 FC OR 71200 FH ALI WFD ST: 30000 FC SI: 9500 FC MRB ST: 30000 FC SI: 9200 FC MRB ST: 30000 FC SI: 9500 FC MRB ST: 30000 FC OR 60000 FH SI: 10400 FC OR 20800 FH MRB TPS REFERENCES 532100-220-802 NTM 53-21-04 MEN TASKM. H. APPL 1 1 0.08 0.08 ALL 1 1 0.30 0.30 1 1 0.30 0.30 2930 2964 3044 1 1 0.25 0.25 1654 1679 1753 2465 2497 2879 2913 1 1 0.20 0.20 ALL SOURCE: ALI 532104-01-1 532100-200-001 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; 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 122 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 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 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 D 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 123 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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; D 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; D 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 REV: 07 DATE: 29-Dec-2014 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. H. 1 1 0.50 0.50 1 1 0.50 0.50 1 1 0.50 0.50 1 1 0.50 0.50 1 1 0.50 0.50 SOURCE: MRB 532140-01-2 532100-200-017 NTM 53-21-40 APPL 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 SOURCE: MRB 532140-02-1 532100-200-017 NTM 53-21-40 SOURCE: MRB 532140-02-2 532100-200-009 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 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 AF DET 532100-200-009 SOURCE: MRB 532145-01-2 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 PREPARATION: CARGO FLOOR PANELS REMOVED; ACCESS PANELS: 825 Sub 2 - Page 124 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 1 0.90 1 0.90 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1 1.10 ALL 1 2.57 1654 1679 1753 2465 2497 2879 2913 1 3.52 2930 2964 3044 1 0.40 2930 2964 3044 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. R 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. R 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 125 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 REV: 07 DATE: 29-Dec-2014 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. H. 1 0.40 1654 1679 1753 2465 2497 2879 2913 1 1 0.50 0.50 ALL 1 1 0.32 0.32 ALL SOURCE: ALI 532165-01-2 532100-200-023 APPL 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 126 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 9300 FC OR 6 YE I: 9300 FC OR 6 YE ALI MRB CPCP T: 9100 FC OR 6 YE I: 9100 FC OR 6 YE ALI MRB CPCP T: 12 YE I: 6 YE MRB CPCP T: 5 YE I: 5 YE MRB CPCP TPS 1 REFERENCES 532100-210-006 MEN TASKM. H. APPL 1 0.30 1 0.30 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1 1 0.80 0.80 ALL 1 1 1 1 0.10 0.10 0.10 0.10 SOURCE: ALI 532170-01-1 MRB 532170-01-4 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; D 532180-01-1 133 134 137 138 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 532180-01-1 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; ACCESS PANELS: 825 Sub 2 - Page 127 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 532180-01-2 ZONE 133 134 137 138 DESCRIPTION FUSELAGE FR 24-35 SKILL TASK CODE CODE AF DET DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE INCLUDING FORWARD FACE OF PRESSURE BULKHEAD, FROM STRINGER 38 LH/RH TO BOTTOM CENTERLINE REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 6 YE I: 6 YE MRB CPCP 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 ALI WFD TPS REFERENCES 1+2 532100-200-013 SOURCE: MRB 532180-01-2 MEN TASKM. H. APPL 1 1 1 1 0.10 0.10 0.10 0.10 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1 3.42 2930 2964 3044 1 3.42 1654 1679 1753 2465 2497 2879 2913 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); R 532186-01-1 200 ACCESS PANELS: 825 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 532186-01-2 200 CIRCUMFERENTIAL JOINT AT FR 35 SPECIAL DETAILED INSPECTION (LFEC) OF CIRCUMFERENTIAL JOINT AT FR 35, BETWEEN STRINGER 10 LH AND STRINGER 10 RH, EXTERNAL SIDE. NDT SDI 532100-200-024 NTM 53-21-86 SOURCE: ALI 532186-01-1 ALI MRB 532100-200-024 NTM 53-21-86 SOURCE: ALI 532186-01-2 MRB 532186-01-2 Sub 2 - Page 128 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 532188-01-1 ZONE 200 DESCRIPTION CIRCUMFERENTIAL JOINT AT FR 35 SKILL TASK CODE CODE 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 AF AF GVI GVI GENERAL VISUAL INSPECTION OF FORWARD CARGO DOOR ACTUATOR ATTACH BRACKETS, BETWEEN CABIN FLOOR BEAMS, FROM FR 25 TO FR 27 532196-01-1 132 ACCESS PANELS: 131AC, 825 FWD CARGO DOOR ECCENTRIC BOLTS 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 R 533101-01-1 147 148 AFT PRESSURE BULKHEAD FWD FACE DETAILED INSPECTION OF PRESSURE BULKHEAD AT FR 46, FORWARD FACE ACCESS PANELS: 734, 744 AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE ST: 30000 FC OR 60000 FH SI: 20000 FC OR 42000 FH MRB T: 48000 FC I: 8100 FC ALI T: 16700 FC I: 16700 FC MRB 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 TPS REFERENCES 532100-200-026 MEN TASKM. H. 1 0.30 1654 1679 1753 2465 2497 2879 2913 1 0.10 ALL 1 0.10 ALL 1 1.00 ALL 1 1 0.50 0.50 2930 2964 3044 SOURCE: MRB 532188-01-1 532100-210-007 APPL SOURCE: ALI 532190-01-1 532100-210-008 SOURCE: MRB 532195-01-1 NO 532100-200-005 SOURCE: MRB 532196-01-1 MRB 533100-210-002 SOURCE: MRB 533101-01-1 Sub 2 - Page 129 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 533101-01-3 ZONE 147 148 DESCRIPTION AFT PRESSURE BULKHEAD FWD FACE SKILL TASK CODE CODE 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. R 533103-01-1 151 152 ACCESS PANELS: 734, 744 AFT PRESSURE BULKHEAD AFT FACE AF DET DETAILED INSPECTION OF PRESSURE BULKHEAD AT FR 46, AFT FACE, INCLUDING VERTICAL BEAMS, ABOVE CARGO FLOOR LEVEL REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE ST: 30000 FC OR 60000 FH SI: 18800 FC OR 37600 FH MRB T: 12 YE I: 12 YE MRB CPCP 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 MRB CPCP TPS REFERENCES 533100-210-002 MEN TASKM. H. 1 1 1.00 1.00 1654 1679 1753 2465 2497 2879 2913 1 1 0.50 0.50 2930 2964 3044 1 1 1.00 1.00 1654 1679 1753 2465 2497 2879 2913 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 SOURCE: MRB 533101-01-3 1 533100-210-008 APPL SOURCE: MRB 533103-01-1 PREPARATION: INSULATION REMOVED; ACT(S) REMOVED (IF INSTALLED); 533103-01-5 151 152 ACCESS PANELS: 151AW, 151BW, 152BW AFT PRESSURE BULKHEAD AFT FACE 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; 533105-01-1 147 148 ACCESS PANELS: 151AW, 151BW, 152BW MLG BAY SIDE PANELS 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 AF DET 1 533100-210-008 SOURCE: MRB 533103-01-5 ALI MRB CPCP 533100-210-003 SOURCE: ALI 533105-01-1 MRB 533105-01-1 Sub 2 - Page 130 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 533105-01-2 ZONE 147 148 DESCRIPTION MLG BAY SIDE PANELS SKILL TASK CODE CODE 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 AF DET DETAILED INSPECTION OF MLG BAY FUSELAGE SIDE PANELS, OUTBOARD FACE, BETWEEN FR 42 AND FR 47, FROM STRINGER 26 TO STRINGER 36, LH/RH 533109-01-1 145 146 ACCESS PANELS: 191ET, 193AT, 734, 192ET, 194AT, 744 PRESSURE DECK MEMBRANES UPR SURFACE 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 R 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 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. NDT SDI REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE ST: 12 YE SI: 6 YE T: 24 YE I: 6 YE ST: 48000 FC SI: 20000 FC MRB CPCP 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 TPS REFERENCES 533100-210-003 MEN TASKM. H. APPL 1 1 0.50 0.50 2930 2964 3044 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 1 1 0.75 0.75 1654 1679 1753 2465 2497 2879 2913 1 1 1.00 1.00 2930 2964 3044 1 1 1.00 1.00 1654 1679 1753 2465 2497 2879 2913 SOURCE: MRB 533105-01-2 MRB 533100-210-004 SOURCE: MRB 533107-01-1 533100-210-005 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 PREPARATION: CABIN FLOOR PANELS REMOVED; Sub 2 - Page 131 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 533111-01-1 ZONE 147 148 DESCRIPTION PRESSURE DECK MEMBRANES LWR SURFACE SKILL TASK CODE CODE 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 533122-01-3 R 533128-01-2 200 CIRCUMFERENTIAL SPLICE AT FR 35 200 DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREA AT FR 35 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 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 DETAILED INSPECTION OF EMERGENCY EXIT SKIN CUTOUTS, UPPER AND LOWER CORNERS, LH/RH ACCESS PANELS: 834, 844 AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 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 ALI TPS REFERENCES 533100-210-006 MEN TASKM. H. APPL 1 1 0.75 0.75 ALL 1 0.50 1654 1679 1753 2465 2497 2879 2913 1 0.50 1654 1679 1753 2465 2497 2879 2913 1 1.00 2930 2964 3044 1 0.50 1654 1679 1753 2465 2497 2879 2913 SOURCE: ALI 533111-01-1 MRB 533111-01-1 MRB 533100-210-018 SOURCE: MRB 533121-01-1 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 Sub 2 - Page 132 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 533129-01-1 ZONE 241 242 DESCRIPTION EMERGENCY EXIT CUTOUTS SKILL TASK CODE CODE AF DET 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 12 YE I: 6 YE MRB CPCP 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 MRB CPCP TPS 1 REFERENCES 533100-210-009 MEN TASKM. H. APPL 1 1 0.25 0.25 2930 2964 3044 1 1 0.25 0.25 1654 1679 1753 2465 2497 2879 2913 1 0.10 2930 2964 3044 SOURCE: MRB 533129-01-1 PREPARATION: CABIN AIR OUTLET ASSEMBLY; LINING REMOVED; RISER DUCT; INSULATION REMOVED; 533129-01-2 241 242 ACCESS PANELS: 833, 834, 843, 844 EMERGENCY EXIT CUTOUTS 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 1 533100-210-009 SOURCE: MRB 533129-01-2 PREPARATION: CABIN AIR OUTLET ASSEMBLY; LINING REMOVED; RISER DUCT; INSULATION REMOVED; R 533130-01-1 200 ACCESS PANELS: 834, 844 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 PREPARATION: COVER OF ANTI-COLLISION LIGHT AND ANTI-COLLISION LIGHT REMOVED; AF DET 533100-210-010 SOURCE: MRB 533130-01-1 Sub 2 - Page 133 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 533130-01-2 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 NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 533130-01-1. PREPARATION: COVER OF ANTI-COLLISION LIGHT AND ANTI-COLLISION LIGHT REMOVED; R 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. R 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 AF GVI REV: 07 DATE: 29-Dec-2014 INTERVALS ST: 12 YE SI: 12 YE T: 24 YE OR 30500 FC I: 12 YE OR 17000 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. H. 1 0.10 1654 1679 1753 2465 2497 2879 2913 1 0.30 2930 2964 3044 1 0.30 1654 1679 1753 2465 2497 2879 2913 1 2.65 1654 1679 1753 2465 2497 2879 2913 1 8.40 2930 2964 3044 SOURCE: ALI 533130-01-2 MRB 533130-01-2 MRB CPCP 533100-210-011 APPL 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 NOTE: INSPECT FROM FR 35 TO FR 47. Sub 2 - Page 134 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 R 533138-01-1 241 242 ACCESS PANELS: 734, 744 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 533138-02-1 PREPARATION: LINING REMOVED; INSULATION REMOVED; AF DET REV: 07 DATE: 29-Dec-2014 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 ALI MRB TPS REFERENCES 533100-210-038 MEN TASKM. H. 1 8.40 1654 1679 1753 2465 2497 2879 2913 1 1 0.50 0.50 ALL 1 1 0.10 0.10 ALL 1 1 0.25 0.25 2930 2964 3044 SOURCE: MRB 533133-01-7 1 533100-210-031 APPL 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 Sub 2 - Page 135 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 533138-01-2 ZONE 241 242 DESCRIPTION LONGITUDINAL LAP JOINT AT FR 42 SKILL TASK CODE CODE 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 533138-02-2 R 533138-02-1 241 242 PREPARATION: LINING AND INSULATION REMOVED; 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 533138-01-1 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 R 533139-01-1 241 242 PREPARATION: LINING AND INSULATION REMOVED; FRAME FLANGES AT FR 38, 39, 40 AND 41 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 AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE ST: 30000 FC SI: 10000 FC T: 40000 FC I: 10000 FC ALI MRB 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 TPS REFERENCES 533100-210-027 MEN TASKM. H. 1 1 0.25 0.25 1654 1679 1753 2465 2497 2879 2913 1 1 0.60 0.60 2930 2964 3044 1 1 0.60 0.60 1654 1679 1753 2465 2497 2879 2913 1 1 0.30 0.30 2930 2964 3044 SOURCE: ALI 533138-01-2 MRB 533138-01-2 533100-220-004 NTM 53-31-38 APPL 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 PREPARATION: LINING REMOVED; INSULATION REMOVED; Sub 2 - Page 136 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 533139-01-2 ZONE 241 242 DESCRIPTION FRAME FLANGES AT FR 40 AND 41 SKILL TASK CODE CODE AF DET 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 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 D 533140-01-8 200 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 SDI REV: 07 DATE: 29-Dec-2014 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: 40300 FC OR 80700 FH I: 14800 FC OR 29700 FH ALI MRB TPS REFERENCES 533100-210-028 MEN TASKM. H. 1 1 0.30 0.30 1654 1679 1753 2465 2497 2879 2913 1 1.00 2930 2964 3044 1 1.00 1654 1679 1753 2465 2497 2879 2913 1 1.00 SOURCE: ALI 533139-01-2 533100-220-006 NTM 53-31-40 APPL SOURCE: MRB 533140-01-2 533100-220-006 NTM 53-31-40 SOURCE: ALI 533140-01-4 MRB 533140-01-4 ALI WFD 533100-220-006 NTM 53-31-40 SOURCE: ALI 533140-01-8 Sub 2 - Page 137 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 R 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; R 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 1 0.40 ALL 1 1 0.20 0.20 1654 1679 1753 2465 2497 2879 2913 1 1 0.30 0.30 1654 1679 1753 2465 2497 2879 2913 1 1 1 1 1 1 0.30 0.30 0.30 0.30 0.30 0.30 2930 2964 3044 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 138 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 533151-01-3 533152-01-4 ZONE 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 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. REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 I: 6 YE MRB CPCP T: 6 YE I: 6 YE MRB CPCP TPS 1 REFERENCES 533100-210-007 SOURCE: MRB 533151-01-3 ALI MRB CPCP 1 533100-210-012 MEN TASKM. H. APPL 1 1 1 1 1 1 0.30 0.30 0.30 0.30 0.30 0.30 1654 1679 1753 2465 2497 2879 2913 1 1 0.75 0.75 1654 1679 1753 2465 2497 2879 2913 1 1 0.75 0.75 2930 2964 3044 1 1 0.15 0.15 ALL SOURCE: ALI 533152-01-4 MRB 533152-01-4 PREPARATION: AIR DUCT; RECIRCULATION FILTER REMOVED; INSULATION REMOVED; R 533152-01-7 137 138 ACCESS PANELS: 131NW, 131PW, 132PW PRESSURE BULKHEAD AT FR 35 FWD FACE AF DET DETAILED INSPECTION OF PRESSURE BULKHEAD FORWARD FACE 1 533100-210-012 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 GENERAL VISUAL INSPECTION OF PRESSURE BULKHEAD AFT FACE AND LOWER SKIN OF RESSURE DECK LOWER SURFACE AF GVI 1 533100-210-032 SOURCE: MRB 533153-02-1 NOTE: INSPECTION AT FR 35 AND LOWER SKIN OF PRESSURE DECK LOWER SURFACE, BETWEEN FR 35 AND FR 36. ACCESS PANELS: 191BB, 191EB, 192EB, 192FB Sub 2 - Page 139 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 533154-01-1 ZONE 147 148 DESCRIPTION MLG DOORS FITTINGS SKILL TASK CODE CODE 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 NDT SDI SPECIAL DETAILED INSPECTION (HFEC) OF KEELBEAM BOX ELLIPTICAL CUTOUT AT FR 46, LH/RH ACCESS PANELS: 734, 744 D 533174-01-1 240 CENTER FUSELAGE-FR 37 THRU FR 41- NDT SDI NDT SDI SPECIAL DETAILED INSPECTION OF THE FRAMES AND THE FRAME FEET, FROM FR 37 TO FR 41, ADJACENT TO STGR 23. NOTE : REFER TO ISB A320-53-1141 R 533180-01-1 145 146 PREPARATION: REFER TO ISB 53-1141; 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 T: NOTE I: 3500 FC ALI MRB CN ISB T: 48100 FC OR 96200 FH I: 6100 FC OR 12200 FH ALI WFD TPS 1 REFERENCES 533100-210-014 MEN TASKM. H. APPL 1 1 0.20 0.20 ALL 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 533100-220-009 CN 1998-509-123(B) ISB 53-1141 1 0.60 533100-220-803 NTM 53-31-80 1 1 1.60 1.60 SOURCE: MRB 533154-01-1 533100-220-007 NTM 53-31-55 SOURCE: ALI 533155-03-1 MRB 533155-03-1 2930 2964 3044 SOURCE: ALI 533180-01-1 PREPARATION: CABIN FLOOR PANELS REMOVED; INSULATION REMOVED; Sub 2 - Page 140 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 533181-01-1 ZONE 147 148 DESCRIPTION LONGITUDINAL BEAMS FLANGES AT ATTACHMENT AREA TO PRESSURE DECK MEMBRANE BETWEEN FR 42 AND FR 46 SKILL TASK CODE CODE NDT 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 48500 FC OR 97000 FH I: 17200 FC OR 34400 FH ALI WFD T: 48000 FC OR 96000 FH I: 20000 FC OR 40000 FH MRB T: 48000 FC OR 96000 FH I: 31200 FC OR 62500 FH ALI TPS REFERENCES MEN 533100-220-802 NTM 53-31-81 TASKM. H. APPL 1 1 1.40 1.40 2930 2964 3044 1 1 0.75 0.75 2930 2964 3044 1.20 1.20 2930 2964 3044 SOURCE: ALI 533181-01-1 PREPARATION: CABIN FLOOR PANELS REMOVED; INSULATION REMOVED; R 533182-01-1 145 146 ACCESS PANELS: 734, 744 CENTER FUSELAGE NDT DET 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) R 533185-01-2 137 138 PREPARATION: CABIN FLOOR PANELS REMOVED; INSULATION REMOVED; PRESSURE DECK MEMBRANE UPPER SURFACE TO CENTER WING BOX, UNDER TITANIUM ANGLE CONNECTION AND CORNER BRACKETS AT FR 36 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 (IF INSTALLED); NDT SDI 533100-210-802 SOURCE: MRB 533182-01-1 533100-220-804 NTM 53-31-85 1 1 SOURCE: ALI 533185-01-2 ACCESS PANELS: 131NW, 131PW, 132PW, 825 Sub 2 - Page 141 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 533186-01-1 ZONE 137 138 DESCRIPTION FR 35 FORWARD FACE TO PRESSURE BULKHEAD ATTACHMENTS SKILL TASK CODE CODE NDT SDI SPECIAL DETAILED INSPECTION (HFEC) OF FR 35 FORWARD FACE TO PRESSURE 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) NOTE: PRESSURE BULKHEAD FR 35. 533189-01-1 191 192 ACCESS PANELS: 191BB, 191EB, 192EB, 192FB ANGLE FITTING ATTACHMENT AT FR 36 AT STRINGER STR 30 NDT SDI SPECIAL DETAILED INSPECTION (LFEC) OF ANGLE FITTING FORWARD ATTACHMENT, AT FRAME 36 AT STRINGER 30, LH/RH PREPARATION: AIR CONDITIONING DUCTS REMOVED; 533500-01-1-SDM R 534103-01-1 147 148 191 192 193 194 195 196 197 198 200 ACCESS PANELS: 191BT, 192BT FAIRINGS AF DET AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE TPS REFERENCES T: 40000 FC OR 80000 FH I: 15000 FC OR 30000 FH ALI 533100-220-805 NTM 53-31-86 T: 30300 FC I: 8400 FC ALI T: 26900 FC OR 53800 FH I: 21500 FC OR 43000 FH I: 750 FH ALI SPECI 533500-200-002 ST: 48000 FC OR 96000 FH SI: 17300 FC OR 34600 FH MRB 534100-210-016 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 TASKM. H. APPL 1 1 2.92 2.92 ALL 1 1 0.30 0.30 ALL 1 1 0.55 0.55 ALL 1 1 1 1 1 1 1 1 1 1 1 TBD TBD TBD TBD TBD TBD TBD TBD TBD TBD 0.50 ALL SOURCE: ALI 533186-01-1 533100-220-806 SOURCE: ALI 533188-01-1 533100-220-807 NTM 53-31-89 SOURCE: ALI 533189-01-1 INSPECTION OF THE WING TO FUSELAGE FAIRINGS AND BELLY FAIRING ACCESS PANELS FOR MISSING FASTENERS WINDOW FORGINGS FR 47-65 MEN 2930 2964 3044 SOURCE: MRB 534103-01-1 Sub 2 - Page 142 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 534103-01-3 R 534106-01-1 ZONE DESCRIPTION 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 SKILL TASK CODE CODE AF AF DET DET 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; 534106-01-5 252 ACCESS PANELS: 252HW, 252LW, 252PW FRAME SPLICES FR 53-56 AF DET DETAILED INSPECTION OF FRAME SPLICES AND ADJACENT AREA LOCATED ABOVE STRINGER 18 RH REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE ST: 33600 FC SI: 20000 FC MRB T: 51300 FC OR 102700 FH I: 12900 FC OR 25800 FH ALI ST: 48000 FC SI: 13600 FC MRB ST: 48000 FC SI: 20000 FC MRB TPS REFERENCES 534100-210-016 MEN TASKM. H. 1 0.50 1654 1679 1753 2465 2497 2879 2913 1 0.30 2930 2964 3044 1 0.30 1654 1679 1753 2465 2497 2879 2913 1 0.30 1654 1679 1753 2465 2497 2879 2913 SOURCE: MRB 534103-01-3 534100-210-011 APPL SOURCE: ALI 534106-01-1 534100-210-011 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 SPECIAL DETAILED INSPECTION (US) OF FRAME SPLICES AND ADJACENT AREA LOCATED ABOVE STRINGER 18 NDT SDI 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; ACCESS PANELS: 252HW, 252LW, 252PW Sub 2 - Page 143 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 534107-01-1 ZONE 153 154 DESCRIPTION FUSELAGE INTERNAL STRUCTURE FR 46-65 SKILL TASK CODE CODE 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. REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 6 YE I: 6 YE MRB CPCP T: 3000 FC I: 3000 FC ALI T: 3000 FC I: 3000 FC ALI ST: 48000 FC SI: 20000 FC MRB ST: 48000 FC SI: 20000 FC MRB TPS REFERENCES 1+2 534100-210-014 MEN TASKM. H. APPL 1 1 2.00 2.00 ALL 1 0.50 2930 2964 3044 1 0.50 1654 1679 1753 2465 2497 2879 2913 1 1 0.30 0.30 1654 1679 1753 2465 2497 2879 2913 1 1 0.30 0.30 1654 1679 1753 2465 2497 2879 2913 SOURCE: MRB 534107-01-1 NOTE: CREDIT CAN BE TAKEN FROM PREVIUS ACCOMPLISHMENT OF TASK 534107-01-4. R 534108-01-2 534108-01-4 534109-01-1 100 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 47/51-70 263 264 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 UPPER SEGMENT OF FR 70 AF AF AF GVI GVI 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 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 AF DET 534100-210-810 SOURCE: ALI 534108-01-2 534100-210-810 SOURCE: ALI 534108-01-4 534100-210-036 SOURCE: MRB 534109-01-1 534100-210-018 SOURCE: MRB 534110-01-1 ACCESS PANELS: 323AL, 323AR Sub 2 - Page 144 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 534111-01-1 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. 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 AF DET 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; R 534112-01-1 200 VHF3 ANTENNA SKIN CUTOUT DETAILED INSPECTION OF SKIN AROUND VHF 3 ANTENNA CUTOUT, BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE NOTE: INSPECTION BETWEEN FR 52 AND FR 53. PREPARATION: ANTENNA REMOVED; AF DET REV: 07 DATE: 29-Dec-2014 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 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 ALI MRB CPCP TPS REFERENCES 534100-210-002 MEN TASKM. H. APPL 1 0.30 2930 2964 3044 1 0.30 1654 1679 1753 2465 2497 2879 2913 1 0.30 2930 2964 3044 SOURCE: MRB 534111-01-1 534100-210-002 SOURCE: ALI 534111-01-3 MRB 534111-01-3 MRB CPCP 534100-210-019 SOURCE: MRB 534112-01-1 Sub 2 - Page 145 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 534112-01-3 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 56 AND FR 57. 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 R 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 D 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 REV: 07 DATE: 29-Dec-2014 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. H. 1 0.30 1654 1679 1753 2465 2497 2879 2913 1 0.50 1654 1679 1753 2465 2497 2879 2913 0 N/A 2930 2964 3044 0 N/A 1654 1679 1753 2465 2497 2879 2913 1 0.70 SOURCE: ALI 534112-01-3 MRB 534112-01-3 ALI MRB 534100-210-020 SOURCE: ALI 534113-01-1 MRB 534113-01-1 MRB 534100-210-823 APPL 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 146 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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; REV: 07 DATE: 29-Dec-2014 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 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 T: 32100 FC OR 60000 FH I: 3000 FC OR 6000 FH ALI WFD TPS REFERENCES 534100-220-010 NTM 53-41-21 MEN TASKM. H. 1 0.70 1654 1679 1753 2465 2497 2879 2913 1 1 1 1 0.33 0.33 0.33 0.33 1654 1679 1753 2465 2497 2879 2913 1 1 0.67 0.67 1654 1679 1753 2465 2497 2879 2913 1 1 0.67 0.67 2930 2964 3044 1 1.14 1654 1679 1753 2465 2497 2879 2913 SOURCE: ALI 534121-01-4 MRB 534121-01-4 MRB 534100-220-802 NTM 53-41-23 SOURCE: MRB 534123-01-2 APPL 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; R 534124-01-3 263 264 ACCESS PANELS: 832, 842 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; 534125-01-2 100 ACCESS PANELS: 832, 842 REAR FUSELAGE 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 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 534100-220-809 NTM 53-41-25 SOURCE: ALI 534125-01-2 Sub 2 - Page 147 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 534125-01-3 ZONE 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 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 R 534126-01-3 100 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 534127-01-2 263 264 REAR FUSELAGE 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; NDT SDI REV: 07 DATE: 29-Dec-2014 INTERVALS 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 T: 27700 FC OR 55400 FH I: 5700 FC OR 11400 FH SOURCE ALI WFD MRB TPS REFERENCES 534100-220-809 NTM 53-41-25 MEN TASKM. H. APPL 1 1.14 2930 2964 3044 1 1.30 1654 1679 1753 2465 2497 2879 2913 1 1.30 2930 2964 3044 1 1 0.20 0.20 1654 1679 1753 2465 2497 2879 2913 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 ALI 534100-220-811 NTM 53-41-27 SOURCE: ALI 534127-01-2 ACCESS PANELS: 832, 842 Sub 2 - Page 148 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 534127-01-3 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; 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 ST: 30000 FC OR 60000 FH SI: 8300 FC OR 16600 FH T: 40200 FC OR 60000 FH I: 8300 FC OR 16600 FH ALI MRB TPS REFERENCES 534100-220-811 NTM 53-41-27 MEN TASKM. H. APPL 1 1 0.20 0.20 2930 2964 3044 1 0.30 1654 1679 1753 2465 2497 2879 2913 1 0.30 2930 2964 3044 1 1 0.47 0.47 1654 1679 1753 2465 2497 2879 2913 SOURCE: ALI 534127-01-3 534100-210-806 SOURCE: MRB 534128-01-4 ACCESS PANELS: 321AL R 534128-01-6 200 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 534128-01-1 534100-210-806 SOURCE: MRB 534128-01-6 ACCESS PANELS: 321AL 534129-01-2 261 262 REAR FUSELAGE 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 NDT SDI 534100-220-812 NTM 53-41-29 SOURCE: ALI 534129-01-2 MRB 534129-01-2 Sub 2 - Page 149 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 534129-01-3 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 66 WEB, LH/RH PREPARATION: BOLTS REMOVED; LINING REMOVED; ACCESS PANELS: 832, 842 534130-01-2 261 262 REAR FUSELAGE 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; R 534130-01-3 261 262 ACCESS PANELS: 832, 842 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; ACCESS PANELS: 832, 842 NDT SDI REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 ALI MRB ST: 30000 FC OR 60000 FH SI: 9700 FC OR 19400 FH T: 40900 FC OR 81800 FH I: 9700 FC OR 19400 FH ALI MRB TPS REFERENCES 534100-220-812 NTM 53-41-29 MEN TASKM. H. APPL 1 1 0.47 0.47 2930 2964 3044 1 1 0.47 0.47 1654 1679 1753 2465 2497 2879 2913 1 1 0.47 0.47 2930 2964 3044 SOURCE: ALI 534129-01-3 MRB 534129-01-3 ALI 534100-220-813 NTM 53-41-30 SOURCE: ALI 534130-01-2 534100-220-813 NTM 53-41-30 SOURCE: ALI 534130-01-3 MRB 534130-01-3 Sub 2 - Page 150 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 534131-01-1 ZONE 100 200 DESCRIPTION FUSELAGE SKIN BETWEEN FR 65 AND 70 SKILL TASK CODE CODE 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 R 534132-01-4 260 NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534131-01-1. AFT PAX/CREW DOOR CUTOUT UPR CORNER 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 534132-01-1. 534132-01-6 260 ACCESS PANELS: 832, 842 AFT PAX/CREW DOOR CUTOUT UPR CORNER 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 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; AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 T: 16300 FC OR 32600 FH I: 10300 FC OR 20600 FH ALI 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 TPS REFERENCES 534100-210-814 MEN TASKM. H. APPL 1 1 0.50 0.50 2930 2964 3044 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 1 0.15 2930 2964 3044 1 0.15 1654 1679 1753 2465 2497 2879 2913 1 1 0.25 0.25 1654 1679 1753 2465 2497 2879 2913 SOURCE: ALI 534131-01-1 ALI 534100-210-814 SOURCE: ALI 534131-01-3 534100-210-010 SOURCE: ALI 534132-01-4 534100-210-010 SOURCE: ALI 534132-01-6 534100-210-021 SOURCE: MRB 534133-01-6 ACCESS PANELS: 832, 842 Sub 2 - Page 151 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 534133-02-2 ZONE 170 260 DESCRIPTION REAR FUSELAGE SKILL TASK CODE CODE 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. REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE ST: 48000 FC OR 60000 FH SI: 39600 FC OR 60000 FH MRB T: 12 YE I: 12 YE MRB CPCP T: 6 YE I: 6 YE MRB CPCP T: 12 YE I: 12 YE MRB CPCP TPS REFERENCES 534100-220-008 NTM 53-41-33 MEN TASKM. H. APPL 1 1 0.60 0.60 1654 1679 1753 2465 2497 2879 2913 1 1 0.25 0.25 ALL 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 SOURCE: MRB 534133-02-2 PREPARATION: LINING AND INSULATION REMOVED; CORNER SCUFF PLATES REMOVED; 534134-01-1 261 262 ACCESS PANELS: 832, 842 DOOR STOP FITTINGS FR 66 AND 68 AF DET DETAILED INSPECTION OF DOOR STOP FITTINGS ON FR 66 AND FR 68, LH/RH 534100-210-029 SOURCE: MRB 534134-01-1 PREPARATION: LINING REMOVED; 534135-01-4 261 262 263 264 ACCESS PANELS: 832, 842 AFT PAX/CREW DOOR CUTOUT 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 1 534100-210-003 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 DETAILED INSPECTION OF AFT PASSENGER/CREW DOOR CUTOUT, UNDERNEATH THE SCUFF PLATE, LH/RH AF DET SOURCE: MRB 534136-01-1 PREPARATION: SCUFF PLATE; ACCESS PANELS: 832, 842 Sub 2 - Page 152 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 534137-01-1 ZONE 100 DESCRIPTION WASTE SERVICE PANEL CUTOUT 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 534137-01-3 100 REAR FUSELAGE NDT SDI SPECIAL DETAILED INSPECTION (LFEC) OF INTERNAL DOUBLER, FORWARD AND AFT OF WASTE SERVICE PANEL CUTOUT, BETWEEN STRINGER 35 AND STRINGER 39, RH R 534139-01-1 100 WATER SERVICE PANEL CUTOUT AFT DOUBLER SPECIAL DETAILED INSPECTION (LFEC) OF INTERNAL DOUBLER, FORWARD AND AFT OF WATER SERVICE PANEL CUTOUT, BETWEEN STRINGER 38 AND STRINGER 42, LH NDT SDI REV: 07 DATE: 29-Dec-2014 INTERVALS ST: 30000 FC OR 60000 FH SI: 24900 FC OR 49800 FH T: 57700 FC OR 115400 FH I: 24900 FC OR 49800 FH 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 SOURCE ALI MRB TPS REFERENCES 534100-220-009 NTM 53-41-37 MEN TASKM. H. APPL 1 0.25 2930 2964 3044 1 0.25 1654 1679 1753 2465 2497 2879 2913 1 0.25 2930 2964 3044 SOURCE: ALI 534137-01-1 MRB 534137-01-1 ALI MRB 534100-220-009 NTM 53-41-37 SOURCE: ALI 534137-01-3 MRB 534137-01-3 MRB 534100-220-007 NTM 53-41-39 SOURCE: MRB 534139-01-1 Sub 2 - Page 153 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 534139-01-2 ZONE 100 DESCRIPTION REAR FUSELAGE SKILL TASK CODE CODE 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 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 R 534140-01-8 100 NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534140-01-3. FUSELAGE SKIN AROUND OUTFLOW VALVE CUTOUT 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 R 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 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 AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 T: 35600 FC OR 71200 FH I: 3200 FC OR 6400 FH ALI 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 TPS REFERENCES 534100-220-007 NTM 53-41-39 MEN TASKM. H. 1 0.25 1654 1679 1753 2465 2497 2879 2913 1 0.15 1654 1679 1753 2465 2497 2879 2913 1 0.15 2930 2964 3044 1 0.15 2930 2964 3044 1 0.15 1654 1679 1753 2465 2497 2879 2913 SOURCE: MRB 534139-01-2 534100-210-815 SOURCE: ALI 534140-01-6 ALI 534100-210-815 APPL SOURCE: ALI 534140-01-8 534100-210-816 SOURCE: ALI 534141-01-5 534100-210-816 SOURCE: ALI 534141-01-8 NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534141-01-4. Sub 2 - Page 154 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 534142-01-8 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 R 534142-01-9 100 NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534142-01-4. FUSELAGE SKIN AROUND WASTE SERVICE PANEL CUTOUT 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. R 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 33000 FC OR 60000 FH I: 12900 FC OR 25800 FH ALI 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 ALI MRB TPS REFERENCES 534100-210-817 MEN TASKM. H. 1 0.15 1654 1679 1753 2465 2497 2879 2913 1 0.15 2930 2964 3044 1 1 0.20 0.20 1654 1679 1753 2465 2497 SOURCE: ALI 534142-01-8 534100-210-817 APPL 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 155 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 1 1 0.20 0.20 2930 2964 3044 2879 2913 1 1 0.50 0.50 ALL 1 1 1 1 0.50 0.50 0.50 0.50 2930 2964 3044 1 1 1 1 0.50 0.50 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 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; R 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 156 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 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. REV: 07 DATE: 29-Dec-2014 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. H. APPL 1 1 1 1 1.50 1.50 1.50 1.50 2930 2964 3044 SOURCE: MRB 534147-01-2 1 1 1 1 1.50 1.50 1.50 1.50 1654 1679 1753 2465 2497 2879 2913 534100-210-802 1 4.00 2930 2964 3044 1 4.00 1654 1679 1753 2465 2497 2879 2913 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 R 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 157 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 1 0.50 2930 2964 3044 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 1 0.60 2930 2964 3044 1 0.60 1654 1679 1753 2465 2497 2879 2913 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; R 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 158 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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; R 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; R 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); REV: 07 DATE: 29-Dec-2014 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. H. 1 0.40 1654 1679 1753 2465 2497 2879 2913 1 0.40 2930 2964 3044 1 0.25 2930 2964 3044 1 0.27 2930 2964 3044 SOURCE: MRB 534153-01-1 1 534100-210-006 APPL SOURCE: MRB 534153-01-2 534100-220-815 NTM 53-41-54 SOURCE: ALI 534154-01-1 ACCESS PANELS: 252NW, 826 R 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 159 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 R 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 REV: 07 DATE: 29-Dec-2014 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. H. 1 0.27 1654 1679 1753 2465 2497 2879 2913 1 0.90 2930 2964 3044 1 0.90 1654 1679 1753 2465 2497 2879 2913 SOURCE: MRB 534155-01-4 MRB 534100-210-012 APPL 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 160 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 1 0.35 2930 2964 3044 1 0.35 1654 1679 1753 2465 2497 2879 2913 1 0.15 2930 2964 3044 1 0.15 1654 1679 1753 2465 2497 2879 2913 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; R 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 161 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 1 1 1 0.20 0.20 0.20 2930 2964 3044 1 1 1 0.20 0.20 0.20 1654 1679 1753 2465 2497 2879 2913 1 0.15 2930 2964 3044 1 0.15 1654 1679 1753 2465 2497 2879 2913 1 0.50 2930 2964 3044 NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 534159-01-1 R 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. R 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 162 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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. R 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 REV: 07 DATE: 29-Dec-2014 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. H. 1 0.50 1654 1679 1753 2465 2497 2879 2913 1 0.10 2930 2964 3044 1 0.10 1654 1679 1753 2465 2497 2879 2913 1 0.50 2930 2964 3044 SOURCE: ALI 534160-02-2 MRB 534100-210-819 APPL 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; R 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 163 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 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. REV: 07 DATE: 29-Dec-2014 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. H. APPL 1 0.10 2930 2964 3044 1 1 0.10 0.10 2930 2964 3044 1 0.20 2930 2964 3044 1 0.10 2930 2964 3044 SOURCE: MRB 534167-02-1 PREPARATION: INSULATION REMOVED; R 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; R 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. R 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 164 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 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. REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 5 YE I: 5 YE MRB CPCP ST: 35000 FC SI: 20000 FC MRB TPS REFERENCES 1+2 534100-210-835 MEN TASKM. H. APPL 1 1 0.33 0.33 1654 1679 1753 2465 2497 2930 2964 2879 2913 1 0.30 2465 2497 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; 534197-01-1 200 ACCESS PANELS: 832, 842 INTERNAL SKIN AROUND CUT OUT AF DET DETAILED INSPECTION OF INTERNAL SKIN AROUND LIVE-TV ANTENNA ATTACHMENT FITTINGS AND WIRE CUT OUT BETWEEN P4 L/H AND P4 R/H 534100-210-838 SOURCE: MRB 534197-01-1 NOTE: INSPECTION FROM FRAME 52 TO FRAME 56. 534199-01-1-SDM 253 254 PREPARATION: LINING AND INSULATION REMOVED; 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 2465 2497 AF DET T: 24000 FC I: 11000 FC S-ICA STC ST00788SE ICA BERG-151-701 1 1 TBD TBD 2465 2497 AF DET T: 24000 FC I: 15000 FC S-ICA STC ST00788SE ICA BERG-151-701 1 1 TBD TBD 2465 2497 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. 534199-03-1-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 AT THE CENTER POINT DOUBLER. PREPARATION: LINING AND INSULATION REMOVED; OVERHEAD STOWAGE COMPARTMENTS REMOVED; Sub 2 - Page 165 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 534199-04-1-SDM ZONE 253 254 DESCRIPTION LIVETV RADOME INSTL AREA-FRAME C52 TO C56 & STR 5L TO 5R SKILL TASK CODE CODE 534199-05-1-SDM 253 254 534199-06-1-SDM 253 254 SOURCE TPS REFERENCES MEN TASKM. H. APPL DET T: 24000 FC I: 7000 FC S-ICA STC ST00788SE ICA BERG-151-701 1 1 TBD TBD 2465 2497 AF DET T: 24000 FC I: 15000 FC S-ICA STC ST00788SE ICA BERG-151-701 1 1 TBD TBD 2465 2497 AF DET T: 24000 FC I: 7000 FC S-ICA STC ST00788SE ICA BERG-151-701 1 1 TBD TBD 2465 2497 AF DET T: 24000 FC I: 24000 FC NOTE S-ICA STC ST00788SE ICA BERG-151-701 1 1 TBD TBD 2497 AF DET T: 24000 FC I: 24000 FC NOTE S-ICA STC ST00788SE ICA BERG-151-701 1 1 TBD TBD 2465 2497 NDT SDI T: 24000 FC I: 5000 FC NOTE SPECI STC ST00788SE ICA BERG-151-701 NTM 51-10-11 PART 6 JIC A320-53-41-00 1 1 TBD TBD 2465 DETAILED VISUAL INSPECTION OF INTERNAL SUPPORT STRUCTURE FOR LIVETV INSTALLATION. PREPARATION: LINING AND INSULATION REMOVED; OVERHEAD STOWAGE COMPARTMENTS REMOVED; LIVETV RADOME INST AREA-FRAME C52 TO C56 & STR 5L TO 5R INTERVALS AF EXTERNAL DETAILED VISUAL INSPECTION OF SKIN COVERED BY RADOME. PREPARATION: COVER OF ANTENNA AND ANTENNA REMOVED; BLANKING PLATE REMOVED; LIVETV RADOME INST AREA-FRAME C52 TO C56 & STR 5L TO 5R REV: 07 DATE: 29-Dec-2014 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 534199-09-1-SDM 253 254 NOTE: INTERVAL : 24000 FC (BASED ON AVERAGE FLIGHT LENGTH OF 1 HOUR) LIVETV LNA INSTALLATION - STRINGERS P4 AND P5 BETWEEN FRAME C59 AND C60 INTERNAL DETAILED VISUAL INSPECTION (DET) OF THE STRINGER SECTION FOR FAILED EDGE LIGAMENT 534199-10-1-SDM 253 254 NOTE: INTERVAL : 24000 FC (BASED ON AVERAGE FLIGHT LENGTH OF 1 HOUR) LIVETV WADL ANTENNA INSTL REPAIR DOUBLER EXTERNAL LOW FREQUENCY EDDY CURRENT INSPECTION OF FRAME C60 TO C61 & STR P’1 TO P1 NOTE: INTERVAL : 5000 FC (BASED ON AVERAGE FLIGHT LENGTH OF 1 HOUR) Sub 2 - Page 166 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 1 1 0.60 0.60 ALL 1 0.15 ALL 1 1 0.30 0.30 1654 1679 1753 2465 2497 2879 2913 1 1 0.75 0.75 1654 1679 1753 2465 2497 2879 2913 1 1 0.20 0.20 2930 2964 3044 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 R 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 167 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 R 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 CONE/REAR FUSELAGE 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. D 535119-01-1 311 312 PREPARATION: 312AR 314AR; 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 REV: 07 DATE: 29-Dec-2014 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. H. 1 1 0.20 0.20 1654 1679 1753 2465 2497 2879 2913 1 1 0.90 0.90 ALL 1 1 0.90 0.90 2930 2964 3044 1 1 0.90 0.90 1654 1679 1753 2465 2497 2879 2913 1 1 0.40 0.40 1 1 0.60 0.60 SOURCE: MRB 535113-01-5 1 535100-210-005 APPL SOURCE: MRB 535115-01-1 1 535100-210-007 SOURCE: MRB 535117-01-1 1 535100-210-007 SOURCE: MRB 535117-01-5 535100-210-017 SOURCE: ALI 535119-01-1 MRB CPCP 1 535100-210-002 ALL SOURCE: MRB 535121-01-1 ACCESS PANELS: 162DW Sub 2 - Page 168 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 R 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 545101-01-1 415 425 ACCESS PANELS: 323AL, 323AR 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 REV: 07 DATE: 29-Dec-2014 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 ST: 30000 FC OR 60000 FH SI: 8600 FC OR 17200 FH MRB TPS 1 REFERENCES 535100-210-008 MEN TASKM. H. APPL 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 2930 2964 3044 1 1.20 1654 1679 1753 2465 2497 2879 2913 1 1 0.75 0.75 1654 1679 1753 2465 2497 2879 2913 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 545100-200-001 NTM 54-51-01 SOURCE: MRB 545101-01-1 Sub 2 - Page 169 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 545101-01-2 ZONE 415 425 DESCRIPTION PYLON FWD MOUNT FITTING SKILL TASK CODE CODE 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 R 545102-01-10 415 425 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE ST: 30000 FC OR 60000 FH SI: 17400 FC OR 34800 FH MRB 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 545100-200-001 NTM 54-51-01 MEN TASKM. H. APPL 1 1 0.75 0.75 2930 2964 3044 1 1 0.75 0.75 2930 2964 3044 1 1 0.75 0.75 1654 1679 1753 2465 2497 2879 2913 1 1 0.20 0.20 ALL 1 1 0.50 0.50 ALL SOURCE: MRB 545101-01-2 545100-200-002 NTM 54-51-02 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 170 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 1 1 0.75 0.75 ALL 1 1 0.50 0.50 ALL 1 1 0.30 0.30 2930 2964 3044 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 R 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 171 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 R 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 REV: 07 DATE: 29-Dec-2014 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. H. 1 1 0.30 0.30 1654 1679 1753 2465 2497 2879 2913 1 1 0.40 0.40 1654 1679 1753 2465 2497 2879 2913 1 1 0.40 0.40 2930 2964 3044 SOURCE: MRB 545107-01-5 MRB 545100-200-006 SOURCE: MRB 545114-01-1 545100-200-006 APPL SOURCE: ALI 545114-01-2 MRB 545114-01-2 Sub 2 - Page 172 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 R 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 REV: 07 DATE: 29-Dec-2014 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. H. 1 1 0.40 0.40 1654 1679 1753 2465 2497 2879 2913 1 1 0.40 0.40 2930 2964 3044 1 1 0.60 0.60 1654 1679 1753 2465 2497 2879 2913 SOURCE: MRB 545115-01-1 545100-200-008 APPL 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 173 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 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; R 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 REV: 07 DATE: 29-Dec-2014 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: 12 YE SI: 12 YE T: 24 YE I: 12 YE MRB CPCP TPS REFERENCES 545100-200-007 NTM 54-51-15 MEN TASKM. H. APPL 1 1 0.60 0.60 2930 2964 3044 1 1 0.30 0.30 ALL 1 1 0.70 0.70 1654 1679 1753 2465 2497 1 1 0.70 0.70 2930 2964 3044 2879 2913 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; 545117-01-2 415 425 ACCESS PANELS: 415BL, 415BR, 471AL, 471BL, 472AR, 472BR, 425BL, 425BR, 481AL, 481BL, 482AR, 482BR PYLON SPIGOT DETAILED INSPECTION OF PYLON SPIGOT RECEPTACLE UPPER SURFACE, INCLUDING FITTING BORE, AND UPPER SPAR SURROUNDING SURFACE PREPARATION: BALL JOINT REMOVED; AF DET NO 545100-200-010 SOURCE: MRB 545117-01-2 ACCESS PANELS: 415BL, 415BR, 471AL, 471BL, 472AR, 472BR, 425BL, 425BR, 481AL, 481BL, 482AR, 482BR Sub 2 - Page 174 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 545120-01-1 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 R 545120-01-2 415 425 PYLON/WING ATTACH FITTINGS LUGS RIB 10 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 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE ST: 30000 FC OR 60000 FH SI: 11000 FC OR 22000 FH MRB 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 TPS REFERENCES 545100-200-011 MEN TASKM. H. 1 1 0.20 0.20 1654 1679 1753 2465 2497 2879 2913 1 1 0.20 0.20 2930 2964 3044 1 1 0.60 0.60 1654 1679 1753 2465 2497 2879 2913 SOURCE: MRB 545120-01-1 545100-200-011 APPL SOURCE: ALI 545120-01-2 MRB 545120-01-2 MRB 545100-220-001 NTM 54-51-23 SOURCE: MRB 545123-01-1 Sub 2 - Page 175 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 545123-01-2 ZONE 415 425 DESCRIPTION PYLON/WING AFT ATTACHMENT SHACKLES AT RIB 10 SKILL TASK CODE CODE 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 545124-01-1 415 425 PYLON/WING AFT ATTACH FITTING SLEEVES 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 R 545126-01-2 410 420 PYLON LATERAL PANELS FASTENERS AREAS 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 AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE ST: 30000 FC OR 60000 FH SI: 13200 FC OR 26400 FH T: 48000 FC OR 80000 FH I: 13200 FC OR 26400 FH ST: 12 YE SI: 12 YE T: 24 YE I: 12 YE ST: 30000 FC OR 60000 FH SI: 6000 FC OR 12000 FH ALI MRB ST: 30000 FC OR 60000 FH SI: 9500 FC OR 19000 FH MRB TPS REFERENCES 545100-220-001 NTM 54-51-23 MEN TASKM. H. APPL 1 1 0.60 0.60 2930 2964 3044 1 1 0.20 0.20 ALL 1 1 0.20 0.20 1654 1679 1753 2465 2497 2879 2913 1 1 0.20 0.20 2930 2964 3044 SOURCE: ALI 545123-01-2 MRB 545123-01-2 MRB CPCP NO 545100-200-014 SOURCE: MRB 545124-01-1 MRB 545100-200-015 SOURCE: MRB 545126-01-1 545100-200-015 SOURCE: MRB 545126-01-2 Sub 2 - Page 176 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 545130-01-1 ZONE 415 425 DESCRIPTION PYLON LATERAL PANELS EDGE OF CUTOUTS SKILL TASK CODE CODE 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 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 R 545131-01-2 410 420 PYLON LATERAL PANELS CUTOUT CORNERS 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 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 AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 20000 FC I: 20000 FC ALI ST: 30000 FC OR 60000 FH SI: 5000 FC OR 10000 FH MRB 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 TPS REFERENCES 545100-200-016 MEN TASKM. H. APPL 1 1 0.20 0.20 ALL 1 1 0.20 0.20 1654 1679 1753 2465 2497 2879 2913 1 1 0.20 0.20 2930 2964 3044 1 1 0.50 0.50 ALL 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 SOURCE: ALI 545130-01-1 545100-200-017 SOURCE: MRB 545131-01-1 545100-200-017 SOURCE: MRB 545131-01-2 545100-200-018 SOURCE: MRB 545133-01-1 545100-200-019 SOURCE: MRB 545134-01-1 Sub 2 - Page 177 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 545134-01-2 ZONE 415 425 DESCRIPTION PYLON UPR SPAR RIB 4 AND 10 SKILL TASK CODE CODE 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 R 545156-01-1 415 425 PYLON UPPER SPARS UPPER SURFACE AF DET DETAILED INSPECTION OF PYLON, UPPER SPARS, UPPER SURFACE, FROM FORWARD OF RIB 1 TO RIB 10 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE ST: 30000 FC OR 60000 FH SI: 9900 FC OR 19800 FH MRB T: 10 YE I: 10 YE MRB CPCP T: 12 YE I: 12 YE MRB CPCP T: 10 YE I: 10 YE MRB CPCP T: 12 YE I: 12 YE MRB CPCP TPS REFERENCES 545100-200-019 MEN TASKM. H. APPL 1 1 0.50 0.50 2930 2964 3044 1 1 0.35 0.35 1654 1679 1753 2465 2497 1 1 0.35 0.35 2930 2964 3044 2879 2913 1 1 0.50 0.50 1654 1679 1753 2465 2497 1 1 0.50 0.50 2930 2964 3044 2879 2913 SOURCE: MRB 545134-01-2 NO 545100-200-021 SOURCE: MRB 545156-01-1 PREPARATION: PRE-COOLER; 545156-01-3 415 425 ACCESS PANELS: 413CL, 413DL, 413EL, 414CR, 414FR, 471AL, 471BL, 471CL, 472AR, 472BR, 423CL, 423DL, 423FL, 424CR, 424ER, 481AL, 481BL, 482AR, 482BR, 482CR PYLON UPPER SPARS UPPER SURFACE AF DET DETAILED INSPECTION OF PYLON, UPPER SPARS, UPPER SURFACE, FROM FORWARD OF RIB 1 TO RIB 10 NO 545100-200-021 SOURCE: MRB 545156-01-3 PREPARATION: PRECOOLER REMOVED; R 545161-01-1 415 425 ACCESS PANELS: 413CL, 413DL, 413EL, 414CR, 414FR, 471AL, 471BL, 471CL, 472AR, 472BR, 423CL, 423DL, 423FL, 424CR, 424ER, 481AL, 481BL, 482AR, 482BR, 482CR PYLON UPPER SPAR LOWER SURFACE AF DET DETAILED INSPECTION OF PYLON, UPPER SPAR, LOWER SURFACE, FORWARD OF RIB 1 NO 545100-200-022 SOURCE: MRB 545161-01-1 ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR 545161-01-2 415 425 PYLON UPPER SPAR LOWER SURFACE DETAILED INSPECTION OF PYLON, UPPER SPAR, LOWER SURFACE, FORWARD OF RIB 1 AF DET NO 545100-200-022 SOURCE: MRB 545161-01-2 ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR Sub 2 - Page 178 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 545162-01-1 ZONE 415 425 DESCRIPTION PYLON UPPER SPAR LOWER SURFACE SKILL TASK CODE CODE AF DET DETAILED INSPECTION OF PYLON, UPPER SPAR, LOWER SURFACE, 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 545162-01-2 415 425 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 545162-02-2 ACCESS PANELS: 415AL, 415AR, 415BL, 415BR, 425AL, 425AR, 425BL, 425BR R 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. REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 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 MRB CPCP ST: 12 YE SI: 12 YE T: 24 YE I: 12 YE MRB CPCP TPS NO REFERENCES 545100-200-023 MEN TASKM. H. 1 1 0.60 0.60 1654 1679 1753 2465 2497 1 1 0.60 0.60 2930 2964 3044 2879 2913 1 1 0.75 0.75 1654 1679 1753 2465 2497 1 1 0.75 0.75 2930 2964 3044 2879 2913 1 1 0.10 0.10 ALL SOURCE: MRB 545162-01-1 NO 545100-200-023 SOURCE: MRB 545162-01-2 NO 545100-200-024 NTM 54-51-62 APPL SOURCE: MRB 545162-02-1 ACCESS PANELS: 415AL, 415AR, 415BL, 415BR, 425AL, 425AR, 425BL, 425BR 545162-02-2 415 425 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 545162-01-2. NO 545100-200-024 NTM 54-51-62 SOURCE: MRB 545162-02-2 ACCESS PANELS: 415AL, 415AR, 415BL, 415BR, 425AL, 425AR, 425BL, 425BR 545170-01-1 415 425 PYLON PYRAMID MATING FACE DETAILED INSPECTION OF PYLON, PYRAMID MATING FACE WITH THE ENGINE FORWARD MOUNT FITTING PREPARATION: ENGINE REMOVED; AF DET NO 545100-200-025 SOURCE: MRB 545170-01-1 Sub 2 - Page 179 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 545171-01-1 ZONE 415 425 DESCRIPTION PYLON ENGINE AFT ATTACHMENT BEAM SKILL TASK CODE CODE AF DET DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENT BEAM MATING FACE WITH THE ENGINE AFT MOUNT FITTING PREPARATION: ENGINE REMOVED; R 545172-01-1 551001-01-1 475 476 485 486 333 343 PYLON FWD CORNER FITTINGS AF DET AF DET DETAILED INSPECTION OF AFT PYLON SECONDARY STRUCTURE, FORWARD CORNER FITTINGS ACCESS PANELS: 475AL, 476AR, 485AL, 486AR 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE ST: 12 YE SI: 12 YE T: 24 YE I: 12 YE T: 6 YE I: 6 YE MRB CPCP ISB OIT T: 6 YE I: 6 YE MRB ST: 32000 FC SI: 24000 FC MRB T: 6 YE I: 6 YE MRB T: 12 YE I: 12 YE MRB TPS NO REFERENCES 545100-200-026 MEN TASKM. H. APPL 1 1 0.15 0.15 ALL 545400-220-002 ISB 54-1022 OIT 999.0037/11 1 1 1 1 1.00 1.00 1.00 1.00 1654 1679 1753 2497 2964 3044 2879 2913 551634-200-001 1 1 0.20 0.20 ALL 1 1 0.30 0.30 ALL 1 1 0.25 0.25 ALL 1 1 0.15 0.15 ALL SOURCE: MRB 545171-01-1 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 180 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 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 181 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 10 YE I: 10 YE MRB CPCP T: 12 YE I: 12 YE MRB CPCP T: 6 YE NOTE I: 6 YE ALI T: 12 YE NOTE I: 6 YE ALI TPS REFERENCES 552000-200-005 MEN TASKM. H. APPL 1 1 0.30 0.30 1654 1679 1753 1 1 0.30 0.30 2465 2497 2930 2964 3044 2879 2913 2 2 3.00 3.00 2 2 3.00 3.00 SOURCE: MRB 552006-01-1 NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 552005-01-1 IN CASE THIS INSPECTION WAS PERFORMED PRIOR JUNE 2004. 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 552000-200-005 SOURCE: MRB 552006-01-2 NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 552005-01-1 IN CASE THIS INSPECTION WAS PERFORMED PRIOR JUNE 2004. PREPARATION: ELEVATOR TIP; ACCESS PANELS: 332AB, 342AB D 552007-01-1 335 345 ELEVATOR TOP AND BOTTOM SKIN PANELS NDT SDI SPECIAL DETAILED INSPECTION (THERMOGRAPHIC) OF ELEVATOR TOP AND BOTTOM SKIN PANELS, LH/RH. SOURCE: ALI 552007-01-1 NOTE: THRESHOLD IS 6 YEARS SINCE THE DATE OF THE FIRST FLIGHT AFTER ACCOMPLISHMENT OF SB A320-55-1024, MANDATED BY CN-2001-062(B). R 552007-01-2 335 345 NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 552007-01-3. 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. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 552007-01-4. NDT SDI 552000-200-006 NTM 55-20-07 SIL 55-037 552000-200-006 NTM 55-20-07 SIL 55-037 1654 1679 1753 2465 2497 SOURCE: ALI 552007-01-2 Sub 2 - Page 182 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 552007-01-3 ZONE 335 345 DESCRIPTION ELEVATOR TOP AND BOTTOM SKIN PANELS SKILL TASK CODE CODE NDT SDI SPECIAL DETAILED INSPECTION (THERMOGRAPHIC) OF ELEVATOR TOP AND BOTTOM SKIN PANELS, LH/RH. REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 6 YE NOTE I: 6 YE ALI T: 12 YE NOTE I: 6 YE ALI T: 12 YE I: 12 YE MRB T: 6 YE I: 6 YE MRB TPS REFERENCES 552000-200-006 NTM 55-20-07 SIL 55-037 MEN TASKM. H. APPL 2 2 3.00 3.00 2 2 3.00 3.00 1654 1679 1753 2465 2497 0.75 0.75 0.75 0.75 ALL SOURCE: MRB 553003-01-1 1 1 1 1 553600-210-001 1 0.30 ALL SOURCE: ALI 552007-01-3 NOTE: -THRESHOLD IS 6 YEARS SINCE THE DATE OF THE FIRST FLIGHT AFTER ACOMPLILSHMENT OF SB A320-55-1024, MANDATED BY CN-2001-062(B). -THIS TASK IS AN ALTERNATIVE TO TASK 552007-01-1. R 552007-01-4 335 345 PREPARATION: ELEVATOR REMOVED; ELEVATOR TOP AND BOTTOM SKIN PANELS NDT SDI SPECIAL DETAILED INSPECTION (THERMOGRAPHIC) OF ELEVATOR TOP AND BOTTOM SKIN PANELS, LH/RH. 552000-200-006 NTM 55-20-07 SIL 55-037 SOURCE: ALI 552007-01-4 NOTE: -THRESHOLD IS 12 YEARS SINCE THE DATE OF THE FIRST FLIGHT. -THIS TASK IS AN ALTERNATIVE TO TASK 552007-01-2. 553003-01-1 321 322 323 324 PREPARATION: ELEVATOR REMOVED; VERT STABILIZER CENTER BOX AF DET DETAILED INSPECTION OF VERTICAL STABILIZER, CENTER BOX, INTERNAL STRUCTURE AS FAR AS VISIBLE, FRONT SPAR FORWARD FACE AND UPPER CLOSING RIB, UPPER SURFACE 553000-200-001 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 DETAILED INSPECTION OF VERTICAL STABILIZER, ATTACH FITTINGS, INCLUDING LOAD INTRODUCTION AREA AT SKIN PANELS AF DET SOURCE: MRB 553004-01-1 ACCESS PANELS: 323AL, 323AR Sub 2 - Page 183 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 553005-01-1 ZONE 325 DESCRIPTION RUDDER HINGE ARMS AND ACTUATOR SKILL TASK CODE CODE AF DET DETAILED INSPECTION OF RUDDER HINGE ARM 1,2,3,4 AND 5 AND FIN ACTUATOR FITTINGS (ACTUATOR 1, 2 AND 3) R 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 AF DET DETAILED INSPECTION OF RUDDER HINGE ARM 6 AND 7 554003-01-1 554004-01-1 300 ACCESS PANELS: 324AT, 325DL, 325EL, 326CT 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 NDT AF SDI DET DETAILED INSPECTION OF RUDDER SIDE PANELS, INTERNAL SURFACES NOTE: ALTERNATIVE ACCESS: 325AR 325BR 325CR 325DR 325ER 326AT REV: 07 DATE: 29-Dec-2014 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 T: 12 YE I: 12 YE MRB T: 6 YE I: 6 YE MRB CPCP TPS 1 REFERENCES 553000-210-001 MEN TASKM. H. APPL 1 0.20 ALL 1 0.15 1654 1679 1 0.15 1753 2465 2497 2930 2964 3044 2879 2913 1 1.00 ALL 1 0.50 ALL 1 0.20 ALL SOURCE: MRB 553005-01-1 1 553000-210-002 SOURCE: MRB 553006-01-1 1 553000-210-002 SOURCE: MRB 553006-01-2 554000-210-001 NTM 55-40-03 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 DETAILED INSPECTION OF RUDDER ATTACH FITTING 1,2,3,4 AND 5 AND RUDDER ACTUATOR ATTACH FITTINGS (ACTUATOR 1, 2 AND 3) AF DET 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. ACCESS PANELS: 325BL, 325CL Sub 2 - Page 184 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 554006-01-1 ZONE 326 DESCRIPTION RUDDER ATTACH FITTING 6 AND 7 SKILL TASK CODE CODE AF DET DETAILED INSPECTION OF RUDDER ATTACH FITTING 6 AND 7 554008-01-1 300 ACCESS PANELS: 324AT, 325DL, 325EL RUDDER SIDE PANELS 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. 562101-01-1 221 222 231 232 241 242 251 252 261 262 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. WINDOW PANES DETAILED INSPECTION OF CABIN WINDOW PANES, INCLUDING WINDOW PANES IN DOORS ACCESS PANELS: 831 AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 6 YE I: 6 YE MRB CPCP T: 6 YE I: 6 YE MRB T: 6 YE I: 6 YE MRB T: 6 YE I: 6 YE MRB TPS 1 REFERENCES 554000-210-005 MEN TASKM. H. APPL 1 0.15 ALL 1 2.50 ALL 1 4.66 ALL 2 2 2 2 2 2 2 2 2 2 0.60 0.60 0.60 0.60 0.60 0.60 0.60 0.60 0.60 0.60 ALL SOURCE: MRB 554006-01-1 554000-220-001 NTM 55-40-08 SOURCE: MRB 554008-01-1 554000-210-006 NTM 55-40-09 SOURCE: MRB 554009-01-1 NO 562113-200-001 SOURCE: MRB 562101-01-1 Sub 2 - Page 185 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 571101-02-1 ZONE 147 148 DESCRIPTION MAIN STRUCTURE SKILL TASK CODE CODE NDT SDI SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING BOX, REAR SPAR, SYSTEM HOLES NEAR MAN HOLES ACCESS PANELS: 734, 744 R 571106-01-2 141 142 CENTER WING BOX LWR SKIN 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 DETAILED INSPECTION OF CENTER WING BOX, REAR SPAR, AROUND ACCESS DOOR CUTOUTS AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 ST: 30000 FC OR 60000 FH SI: 10600 FC OR 29100 FH MRB T: 12 YE I: 12 YE MRB CPCP TPS REFERENCES 571000-220-802 NTM 57-11-01 MEN TASKM. H. APPL 1 1 0.27 0.27 ALL 1 1 3.10 3.10 2930 2964 3044 1 1 3.10 3.10 1654 1679 1753 2465 2497 2879 2913 1 1 0.19 0.19 ALL SOURCE: ALI 571101-02-1 MRB 571101-02-1 MRB 571000-220-002 NTM 57-11-06 SOURCE: MRB 571106-01-2 571000-220-002 NTM 57-11-06 SOURCE: MRB 571106-01-7 NO 571000-200-004 SOURCE: MRB 571109-01-1 ACCESS PANELS: 147AZ, 734, 148AZ, 744 Sub 2 - Page 186 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 571109-02-1 ZONE 147 148 DESCRIPTION CENTER WING BOX REAR SPAR SKILL TASK CODE CODE 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 NDT SDI SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING BOX, REAR SPAR, AROUND ACCESS DOOR CUTOUTS. ACCESS PANELS: 147AZ, 734, 148AZ, 744 571120-01-1 137 138 CENTER WING SPANWISE AF DET DETAILED INSPECTION OF CENTER WING SPANWISE FORMED ANGLE, ALONG LOWER EDGE OF FRONT SPAR, FORWARD FACE PREPARATION: LINING REMOVED; INSULATION REMOVED; ACCESS PANELS: 825 R 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; 571122-01-1 147 148 ACCESS PANELS: 825 CENTER WING BOX REAR SPAR DETAILED INSPECTION OF CENTER WING BOX, REAR SPAR AFT FACE AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 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 T: 6 YE I: 6 YE MRB CPCP TPS REFERENCES 571000-220-001 NTM 57-11-09 MEN TASKM. H. APPL 1 1 0.60 0.60 2930 2964 3044 1 1 0.60 0.60 1654 1679 1753 2465 2497 2879 2913 1 1 0.13 0.13 1654 1679 1753 2465 2497 2879 2913 1 1 0.13 0.13 2930 2964 3044 1 1 0.75 0.75 ALL SOURCE: MRB 571109-02-1 571000-220-001 NTM 57-11-09 SOURCE: MRB 571109-02-2 571000-200-006 SOURCE: MRB 571120-01-1 571000-200-006 SOURCE: MRB 571120-01-2 1+2 571000-200-012 SOURCE: MRB 571122-01-1 ACCESS PANELS: 734, 744 Sub 2 - Page 187 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 571134-01-1 571134-01-4 ZONE 191 192 195 196 191 192 195 196 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 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 R 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 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 32800 FC OR 65600 FH I: 7200 FC OR 14500 FH ST: 42000 FC OR 60000 FH SI: 11600 FC OR 32000 FH ALI 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 TPS REFERENCES 571000-200-013 SOURCE: ALI 571134-01-1 MRB 571000-200-013 SOURCE: MRB 571134-01-4 571000-200-014 MEN TASKM. H. APPL 1 1 1 1 0.25 0.25 0.25 0.25 2930 2964 3044 1 1 1 1 0.25 0.25 0.25 0.25 1654 1679 1753 2465 2497 2879 2913 1 1 0.50 0.50 2930 2964 3044 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 SOURCE: ALI 571135-01-1 MRB 571000-200-014 SOURCE: MRB 571135-01-4 Sub 2 - Page 188 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 1 1 1.00 1.00 2930 2964 3044 1 1 1.00 1.00 1654 1679 1753 2465 2497 2879 2913 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 189 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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. REV: 07 DATE: 29-Dec-2014 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. H. APPL 1 1 0.40 0.40 ALL 1 1 0.75 0.75 ALL 1 1 0.60 0.60 1654 1679 1753 2465 2497 2879 2913 1 1 0.60 0.60 2930 2964 3044 1 1 14.00 14.00 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 R 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 D 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 190 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 571175-01-1 ZONE 191 192 DESCRIPTION CENTER WING BOX - EXTERNAL SKILL TASK CODE CODE REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE ACCESS PANELS: 147CB, 191LB, 148DB, 192LB CENTER WING BOX TRIFORM FITTING ACCESS PANELS: 147AZ, 734, 148AZ, 744 CENTER WING BOX TRIFORM FITTING NTM 57-11-75 EASA AD 2007-0067 FAA AD 2008-02-15 ISB 57-1130 1 1 6.00 6.00 1654 1679 1753 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 2930 2964 3044 ST: 30000 FC OR 60000 FH SI: 14400 FC OR 39600 FH MRB 1 1 1.00 1.00 1654 1679 1753 2465 2497 2879 2913 T: 29600 FC OR 59300 FH I: 14800 FC OR 29700 FH ALI WFD 1 1 1.00 1.00 2930 2964 3044 ST: 30000 FC OR 60000 FH SI: 14400 FC OR 39600 FH MRB 1 1 1.00 1.00 1654 1679 1753 2465 2497 2879 2913 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; R 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; APPL EASA AD FAA AD ISB PREPARATION: SEALANT REMOVED; 141 142 TASKM. H. 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 R 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 191 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 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; R 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; 571189-01-3 141 142 ACCESS PANELS: 540AB, 540AZ, 540BZ, 640AB, 640AZ, 640BZ 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 REV: 07 DATE: 29-Dec-2014 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. H. 1 1 1 1 1.00 1.00 1.00 1.00 2930 2964 3044 1 1 1 1 1.00 1.00 1.00 1.00 1654 1679 1753 2465 2497 2879 2913 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 1 1 0.50 0.50 2930 2964 3044 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 SOURCE: ALI 571185-01-1 571000-200-026 NTM 57-11-85 APPL SOURCE: MRB 571185-01-8 571000-200-017 SOURCE: ALI 571189-01-3 Sub 2 - Page 192 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 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. REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE ST: 30000 FC OR 60000 FH SI: 26000 FC OR 52000 FH MRB T: 21400 FC OR 42800 FH I: 10900 FC OR 21800 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. H. APPL 1 1 0.60 0.60 2930 2964 3044 1 1 0.50 0.50 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 D 571192-01-1 141 142 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 571192-01-1 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 193 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 R 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 REV: 07 DATE: 29-Dec-2014 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. H. 1 1 0.20 0.20 1654 1679 1753 2465 2497 2879 2913 1 1 1.00 1.00 2930 2964 3044 SOURCE: MRB 572002-01-1 ALI MRB 572000-200-004 APPL SOURCE: ALI 572004-01-1 MRB 572004-01-1 Sub 2 - Page 194 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 R 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 DETAILED INSPECTION OF OUTER WING, REAR SPAR, AFT FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING REAR SPAR ANGLE AF DET REV: 07 DATE: 29-Dec-2014 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. H. 1 1 1,00 1.00 1654 1679 1753 2465 2497 2879 2913 1 1 0.50 0.50 2930 2964 3044 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 SOURCE: ALI 572004-01-4 MRB 572004-01-4 ALI MRB CPCP 1+2 572000-200-005 APPL 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 195 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 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 R 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 1 1 0.50 0.50 2930 2964 3044 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 1 1 0.62 0.62 2930 2964 3044 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 196 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 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 REV: 07 DATE: 29-Dec-2014 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 MEN 1 1 TASKM. H. 0.20 0.20 APPL 2930 2964 3044 SOURCE: ALI 572010-01-4 MRB 572010-01-4 Sub 2 - Page 197 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 572010-01-5 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 R 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 REV: 07 DATE: 29-Dec-2014 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 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. H. 1 1 0.20 0.20 1654 1679 1753 2465 2497 2879 2913 1 1 1.00 1.00 2930 2964 3044 1 1 1.00 1.00 1654 1679 1753 2465 2497 2879 2913 SOURCE: ALI 572010-01-5 MRB 572010-01-5 ALI 572000-200-008 APPL SOURCE: ALI 572011-01-2 ALI 572000-200-008 SOURCE: ALI 572011-01-5 Sub 2 - Page 198 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 572012-01-1 ZONE 500 600 DESCRIPTION OUTER WING TOP SKIN UPR SURFACE SKILL TASK CODE CODE 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 R 572014-01-3 500 600 OUTER WING TOP SKIN AF GVI 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 572019-01-1 540 640 OUTER WING TOP SKIN STGR CROWN FTG 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 AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 MRB T: 48300 FC OR 96600 FH I: 15000 FC OR 30000 FH ST: 48000 FC OR 60000 FH SI: 20000 FC OR 27900 FH ALI TPS REFERENCES 572000-220-001 MEN TASKM. H. APPL 1 1 0.50 0.50 2930 2964 3044 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 1 1 1.25 1.25 2930 2964 3044 1 1 0.34 0.34 1654 1679 1753 2465 2497 2879 2913 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 MRB 572000-200-009 SOURCE: MRB 572019-01-1 Sub 2 - Page 199 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 572019-01-4 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 R 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 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 TPS REFERENCES 572000-200-009 MEN TASKM. H. APPL 1 1 0.34 0.34 2930 2964 3044 2 2 3.00 3.00 2930 2964 3044 2 2 3.00 3.00 1654 1679 1753 2465 2497 2879 2913 1 1 1 1 0.15 0.15 0.15 0.15 ALL 1 1 1.00 1.00 1654 1679 1753 2465 2497 2879 2913 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 AF DET 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 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 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 AF DET 572000-200-010 SOURCE: ALI 572020-01-3 572000-200-011 SOURCE: MRB 572022-01-1 MRB 572000-200-013 SOURCE: MRB 572024-01-1 Sub 2 - Page 200 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 572024-01-4 ZONE 540 640 DESCRIPTION OUTER WING RIBS OUTBOARD FACE SKILL TASK CODE CODE 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 R 572026-01-1 540 640 OUTER WING BOLTED PANEL 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 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE ST: 30000 FC OR 60000 FH SI: 19300 FC OR 38600 FH MRB 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 TPS REFERENCES 572000-200-013 MEN TASKM. H. APPL 1 1 1.00 1.00 2930 2964 3044 1 1 0.50 0.50 2930 2964 3044 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 1 1 0.70 0.70 1654 1679 1753 2465 2497 2879 2913 SOURCE: MRB 572024-01-4 572000-200-014 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 Sub 2 - Page 201 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 572027-01-2 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 ACCESS PANELS: 540AB, 540BB, 640AB, 640BB R 572028-01-1 540 640 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 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 R 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 572029-01-6 500 600 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE ST: 30000 FC OR 60000 FH SI: 16000 FC OR 32000 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: 14000 FC OR 20000 FH MRB TPS REFERENCES 572000-200-015 MEN TASKM. H. APPL 1 1 0.70 0.70 2930 2964 3044 1 1 0.50 0.50 2930 2964 3044 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 1 1 0.10 0.10 2930 2964 3044 1 1 0.10 0.10 1654 1679 1753 2465 2497 2879 2913 SOURCE: MRB 572027-01-2 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 572029-01-6 Sub 2 - Page 202 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 572031-01-1 ZONE 411 421 500 600 DESCRIPTION OUTER WING BOTTOM SKIN LWR SURFACE SKILL TASK CODE CODE 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; R 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 572000-200-019 SOURCE: MRB 572031-01-1 572000-200-020 MEN TASKM. H. APPL 1 1 1 1 0.20 0.20 0.20 0.20 1654 1679 1753 2465 2497 2879 2913 1 1 0.20 0.20 2930 2964 3044 1 1 0.20 0.20 1654 1679 1753 2465 2497 2879 2913 SOURCE: ALI 572032-01-1 MRB 572032-01-1 ALI 572000-200-020 SOURCE: ALI 572032-01-3 Sub 2 - Page 203 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 572033-01-1 ZONE 540 640 DESCRIPTION OUTER WING BOTTOM SKIN LDG PLATE SKILL TASK CODE CODE 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 572034-01-1 500 600 OUTER WING BOTTOM SKIN LDG PLATE GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACE MLG REINFORCING PLATE AF GVI REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 MRB T: 31700 FC OR 51400 FH I: 10100 FC OR 16300 FH ALI TPS REFERENCES 572000-200-021 NTM 57-20-33 MEN TASKM. H. APPL 1 1 0.50 0.50 2930 2964 3044 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 1 1 0.20 0.20 1654 1679 1753 2465 2497 2879 2913 SOURCE: ALI 572033-01-1 MRB 572033-01-1 MRB 572000-200-021 NTM 57-20-33 SOURCE: MRB 572033-01-3 572000-210-003 SOURCE: ALI 572034-01-1 Sub 2 - Page 204 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 572036-01-2 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 572036-01-5 531 631 OUTER WING BOTTOM SKIN FLAP TRACK 2 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 R 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 REV: 07 DATE: 29-Dec-2014 INTERVALS ST: 33800 FC OR 67600 FH SI: 10700 FC OR 21400 FH T: 60000 FC OR 120000 FH I: 10700 FC OR 21400 FH 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: 32800 FC OR 65600 FH SI: 5300 FC OR 10600 FH SOURCE ALI MRB TPS REFERENCES 572000-200-022 MEN TASKM. H. APPL 1 1 0.10 0.10 2930 2964 3044 1 1 0.10 0.10 1654 1679 1753 2465 2497 2879 2913 1 1 0.50 0.50 2930 2964 3044 SOURCE: ALI 572036-01-2 MRB 572036-01-2 ALI MRB 572000-200-022 SOURCE: ALI 572036-01-5 MRB 572036-01-5 MRB 572000-220-804 SOURCE: MRB 572037-02-4 Sub 2 - Page 205 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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; R 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 67 AF DET REV: 07 DATE: 29-Dec-2014 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. H. 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 1 1 0.35 0.35 2930 2964 3044 1 1 0.35 0.35 1654 1679 1753 2465 2497 2879 2913 1 1 1 1 0.10 0.10 ALL SOURCE: MRB 572037-02-5 572000-200-023 APPL 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 206 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 R 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 R 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 REV: 07 DATE: 29-Dec-2014 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 T: 31200 FC OR 62400 FH I: 4900 FC OR 9800 FH ALI MRB TPS REFERENCES 572000-200-032 NTM 57-20-40 MEN TASKM. H. 1 1 1.00 1.00 1654 1679 1753 2465 2497 2879 2913 1 1 1.00 1.00 2930 2964 3044 1 1 0.70 0.70 2930 2964 3044 SOURCE: MRB 572040-03-2 572000-200-032 NTM 57-20-40 APPL SOURCE: ALI 572040-03-4 MRB 572040-03-4 ALI 572000-220-802 SOURCE: ALI 572041-02-4 Sub 2 - Page 207 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 572041-02-7 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. R 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 AF GVI 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 R 572044-01-2 500 600 PREPARATION: PYLON FAIRINGS REMOVED; OUTER WING BOTTOM SKIN LOWER SURFACE 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 AF GVI REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 ALI MRB T: 38000 FC OR 76000 FH I: 5800 FC OR 11600 FH ALI TPS REFERENCES 572000-220-802 MEN TASKM. H. 1 1 0.70 0.70 1654 1679 1753 2465 2497 2879 2913 1 1 0.15 0.15 2930 2964 3044 1 1 0.15 0.15 1654 1679 1753 2465 2497 2879 2913 1 1 0.10 0.10 2930 2964 3044 SOURCE: ALI 572041-02-7 MRB 572041-02-7 ALI 572000-210-005 APPL SOURCE: ALI 572042-01-2 ALI 572000-210-005 SOURCE: ALI 572042-01-7 572000-210-004 SOURCE: ALI 572044-01-2 Sub 2 - Page 208 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 572044-01-3 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 R 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; 572047-01-4 471 481 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; 572049-01-4 500 600 OUTER WING BOTTOM SKIN DRAIN HOLES 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. AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 26300 FC OR 42800 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: 15000 FC OR 22400 FH MRB T: 6 YE I: 6 YE MRB CPCP TPS REFERENCES 572000-210-004 MEN TASKM. H. 1 1 0.10 0.10 1654 1679 1753 2465 2497 2879 2913 1 1 0.30 0.30 2930 2964 3044 1 1 0.30 0.30 1654 1679 1753 2465 2497 2879 2913 1 1 0.10 0.10 ALL SOURCE: ALI 572044-01-3 MRB 572000-200-024 NTM 57-20-47 APPL SOURCE: MRB 572047-01-1 572000-200-024 NTM 57-20-47 SOURCE: MRB 572047-01-4 574100-200-003 SOURCE: MRB 572049-01-4 Sub 2 - Page 209 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 572050-01-1 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 572050-02-1. - 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. REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 T: 25000 FC OR 44800 FH I: 10600 FC OR 20500 FH ALI TPS REFERENCES 572000-200-034 MEN TASKM. H. APPL 1 1 0.60 0.60 1654 1679 1753 2465 2497 2879 2913 1 1 0.60 0.60 2930 2964 3044 1 1 1.00 1.00 1654 1679 1753 2465 2497 2879 2913 SOURCE: ALI 572050-01-1 ACCESS PANELS: 540AB, 540BB, 540CZ, 540DZ, 640AB, 640BB, 640CZ, 640DZ R 572050-01-4 540 640 OUTER WING, DRY BAY AREA AF DET DETAILED INSPECTION OF OUTER WING, DRY BAY AREA NOTE: - THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-4. - 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. 572000-200-034 SOURCE: ALI 572050-01-4 ACCESS PANELS: 540AB, 540BB, 540CZ, 540DZ, 640AB, 640BB, 640CZ, 640DZ 572050-02-1 521 621 OUTER WING, DRY BAY AREA SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER WING, DRY BAY AREA NOTE: - THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-1. - 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. NDT SDI 572000-220-011 NTM 57-20-50 SOURCE: ALI 572050-02-1 ACCESS PANELS: 521AZ, 521BZ, 521EB, 621AZ, 621BZ, 621EB Sub 2 - Page 210 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 572050-02-4 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 572050-01-4. - 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. REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 29800 FC OR 59600 FH I: 15000 FC OR 30000 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. H. APPL 1 1 1.00 1.00 2930 2964 3044 1 1 0.10 0.10 2930 2964 3044 1 1 0.10 0.10 1654 1679 1753 2465 2497 2879 2913 SOURCE: ALI 572050-02-4 ACCESS PANELS: 521AZ, 521BZ, 521EB, 621AZ, 621BZ, 621EB R 572052-01-1 540 640 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 NO 572000-200-025 SOURCE: MRB 572052-01-1 MRB CPCP NO 572000-200-025 SOURCE: MRB 572052-01-8 Sub 2 - Page 211 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 572053-01-2 ZONE 540 640 DESCRIPTION OUTER WING BOTTOM SKIN STRINGERS SKILL TASK CODE CODE 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 REV: 07 DATE: 29-Dec-2014 INTERVALS 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 ALI MRB TPS REFERENCES 572000-200-026 MEN TASKM. H. APPL 1 1 0.50 0.50 2930 2964 3044 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 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 212 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 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 AND ADJACENT HOLES 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 1 1 0.10 0.10 2930 2964 3044 1 1 0.10 0.10 1654 1679 1753 2465 2497 2879 2913 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 213 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 REV: 07 DATE: 29-Dec-2014 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. H. 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 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 APPL SOURCE: MRB 572063-01-1 Sub 2 - Page 214 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 1 1 0.75 0.75 2930 2964 3044 1 1 0.75 0.75 1654 1679 1753 2465 2497 2879 2913 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 215 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 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 R 572108-01-2 540 640 OUTER WING FRT SPAR AFT FACE RIB 8-22 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 AF DET REV: 07 DATE: 29-Dec-2014 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: 30000 FC OR 60000 FH SI: 15000 FC OR 30000 FH T: 35700 FC OR 71400 FH I: 15000 FC OR 30000 FH SOURCE MRB CPCP TPS REFERENCES 572100-200-007 MEN TASKM. H. APPL 1 1 0.30 0.30 2930 2964 3044 1 1 0.30 0.30 1654 1679 1753 2465 2497 2879 2913 1 1 0.50 0.50 2930 2964 3044 SOURCE: MRB 572106-01-1 MRB CPCP 572100-200-007 SOURCE: MRB 572106-01-5 ALI MRB 572100-200-008 SOURCE: ALI 572108-01-2 MRB 572108-01-2 Sub 2 - Page 216 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 572108-01-4 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 R 572109-01-1 550 560 650 660 OUTER WING FRT SPAR AFT FACE RIB 22-27 AF DET 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 572109-01-4 550 560 650 660 MAIN STRUCTURE 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 D 572110-01-1 540 640 INSPECTION OF THE REAR SPAR. SPECIAL DETAILED INSPECTION OF (US) OF THE INNER REAR SPAR AND THE SUPPORT AREA OF THE MAIN LANDING GEAR. NOTE: REFER TO CN 2001-249(B) FOR THRESHOLD REQUIREMENTS. NDT SDI REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 31000 FC OR 51200 FH I: 8800 FC OR 14500 FH ALI ST: 39000 FC OR 78000 FH SI: 20000 FC OR 40000 FH MRB ST: 48000 FC OR 60000 FH SI: 20000 FC OR 27900 FH MRB T: NOTE I: 3600 FC OR 6700 FH CN ISB TPS REFERENCES 572100-200-008 MEN TASKM. H. 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 1 1 1 1 0.20 0.20 0.20 0.20 2930 2964 3044 1 1 1 1 0.20 0.20 0.20 0.20 1654 1679 1753 2465 2497 2879 2913 2 2 4.00 4.00 SOURCE: ALI 572108-01-4 572100-200-009 SOURCE: MRB 572109-01-1 572100-200-009 SOURCE: MRB 572109-01-4 JIC A320-57-21-00 NTM 57-21-10 CN 2001-249(B) FAA AD 2004-19-11 ISB 57-1088 APPL PREPARATION: AIRCRAFT DEFUELED; FLAPS EXTENDED; ACCESS PANELS: 540AB, 640AB Sub 2 - Page 217 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 572111-01-1 ZONE 574 575 674 675 DESCRIPTION OUTER WING REAR SPAR AFT FACE RIB 8-11 SKILL TASK CODE CODE 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 R 572112-01-1 575 675 OUTER WING REAR SPAR AFT FACE RIB11-27 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 AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS 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 21000 FC OR 42000 FH I: 6 YE OR 15000 FC OR 30000 FH SOURCE MRB CPCP TPS REFERENCES 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 572100-200-003 MEN TASKM. H. APPL 1 1 1 1 0.10 0.10 0.10 0.10 2930 2964 3044 1 1 1 1 0.10 0.10 0.10 0.10 1654 1679 1753 2465 2497 2879 2913 1 1 0.75 0.75 2930 2964 3044 SOURCE: ALI 572112-01-1 MRB 572112-01-1 Sub 2 - Page 218 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 572112-01-2 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, 575JB, 575KB, 575LB, 575MB, 675BB, 675CB, 675DB, 675EB, 675FB, 675GB, 675HB, 675JB, 675KB, 675LB, 675MB 572114-01-3 540 640 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 R 572114-01-4 540 640 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 572115-01-1 540 550 560 640 650 660 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 REV: 07 DATE: 29-Dec-2014 INTERVALS T: 12 YE OR 22800 FC OR 40300 FH I: 6 YE OR 12500 FC OR 22100 FH T: 30100 FC OR 49400 FH I: 9400 FC OR 15300 FH T: 30100 FC OR 60200 FH I: 10100 FC OR 20200 FH ST: 30000 FC OR 48900 FH SI: 15500 FC OR 25200 FH SOURCE ALI MRB CPCP TPS REFERENCES 572100-200-003 MEN TASKM. H. 1 1 0.75 0.75 1654 1679 1753 2465 2497 2879 2913 1 1 0.30 0.30 1654 1679 1753 2465 2497 2879 2913 1 1 0.30 0.30 2930 2964 3044 1 1 1 1 1 1 0.11 0.11 0.11 0.11 0.11 0.11 1654 1679 1753 2465 2497 2879 2913 SOURCE: ALI 572112-01-2 MRB 572112-01-2 ALI 572100-200-010 SOURCE: ALI 572114-01-3 ALI 572100-200-010 APPL SOURCE: ALI 572114-01-4 MRB 572100-200-011 SOURCE: MRB 572115-01-1 Sub 2 - Page 219 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 572115-01-2 ZONE 540 550 560 640 650 660 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 R 572116-02-1 500 600 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 572116-02-2 500 600 MAIN STRUCTURE DETAILED INSPECTION OF OUTER WING, TOP SKIN, UPPER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR BETWEEN RIB 8 AND RIB 22 AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS ST: 30000 FC OR 60000 FH SI: 15000 FC OR 30000 FH T: 43200 FC OR 86400 FH I: 15000 FC OR 30000 FH 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 SOURCE ALI MRB TPS REFERENCES 572100-200-011 SOURCE: ALI 572115-01-2 MRB 572115-01-2 ALI MRB 572100-220-801 MEN TASKM. H. APPL 1 1 1 1 1 1 0.11 0.11 0.11 0.11 0.11 0.11 2930 2964 3044 1 1 0.60 0.60 2930 2964 3044 1 1 0.60 0.60 1654 1679 1753 2465 2497 2879 2913 SOURCE: ALI 572116-02-1 MRB 572116-02-1 MRB 572100-220-801 SOURCE: MRB 572116-02-2 Sub 2 - Page 220 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 572120-01-3 ZONE 500 600 DESCRIPTION OUTER WING TOP SKIN SKILL TASK CODE CODE AF GVI 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 572122-01-1 500 600 OUTER WING TOP SKIN RIB 19-20 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 R 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 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 AF AF DET DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 51700 FC OR 103400 FH I: 15000 FC OR 30000 FH ST: 48000 FC OR 60000 FH SI: 20000 FC OR 32100 FH ALI 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 ALI MRB TPS REFERENCES 572100-210-804 MEN TASKM. H. APPL 1 1 0.40 0.40 2930 2964 3044 1 1 0.10 0.10 1654 1679 1753 2465 2497 2879 2913 1 1 0.10 0.10 ALL 2 2 2.00 2.00 2930 2964 3044 SOURCE: ALI 572120-01-3 MRB 572100-200-001 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 Sub 2 - Page 221 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 572123-01-3 ZONE 540 640 DESCRIPTION OUTER WING TOP SKIN STGR RIB 8-13 SKILL TASK CODE CODE AF 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 NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 572123-01-1 R 572124-01-3 540 550 560 640 650 660 ACCESS PANELS: 540CB, 540DB, 540EB, 540FB, 540GB, 640CB, 640DB, 640EB, 640FB, 640GB OUTER WING TOP SKIN STGR RIB 13-27 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE ST: 30000 FC OR 52500 FH SI: 20000 FC OR 29000 FH MRB 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 ALI MRB TPS REFERENCES 572100-200-012 MEN TASKM. H. 2 2 2.00 2.00 1654 1679 1753 2465 2497 2879 2913 1 1 1 1 1 1 0.67 0.67 0.67 0.67 0.67 0.67 2930 2964 3044 1 1 1 1 1 1 0.67 0.67 0.67 0.67 0.67 0.67 1654 1679 1753 2465 2497 2879 2913 SOURCE: MRB 572123-01-3 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 APPL Sub 2 - Page 222 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 572125-01-1 ZONE 575 675 DESCRIPTION TOP SKIN PANEL 2 OVERHANG BETWEEN RIB 22 AND RIB 27 SKILL TASK CODE CODE R 572126-01-1 540 550 560 640 650 660 540 550 560 640 650 660 575 675 SPECIAL DETAILED INSPECTION OF OUTER WING, TOP SKIN PANEL 2 OVERHANG BETWEEN RIB 4 AND RIB 22 MEN TASKM. H. APPL 572100-270-001 ISB 57-1154 2 2 3.00 3.00 ALL AF DET ST: 30000 FC OR 60000 FH SI: 20000 FC OR 40000 FH MRB 572100-200-014 1 1 1 1 1 1 0.53 0.53 0.53 0.53 0.53 0.53 2930 2964 3044 ST: 30000 FC OR 52500 FH SI: 20000 FC OR 31900 FH MRB SOURCE: MRB 572126-01-3 1 1 1 1 1 1 0.53 0.53 0.53 0.53 0.53 0.53 1654 1679 1753 2465 2497 2879 2913 T: NOTE I: 40 MO ISB 572100-270-002 ISB 57-1155 2 2 8.00 8.00 1654 1679 1753 2465 2497 3044 2879 2913 AF DET DETAILED INSPECTION OF OUTER WING, RIB 9 TO RIB 27, AT SKIN ATTACHMENTS, INCLUDING CLEATS, SPAR ATTACHMENTS AND IN REGION OF STRINGER CUTOUTS TOP SKIN PANEL 2 OVERHANG BETWEEN RIB 4 AND RIB 22 REFERENCES ISB 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 R 572127-01-1 TPS T: NOTE I: 40 MO DETAILED INSPECTION OF OUTER WING, RIB 9 TO RIB 27, AT SKIN ATTACHMENTS, INCLUDING CLEATS, SPAR ATTACHMENTS AND IN REGION OF STRINGER CUTOUTS OUTER WING RIB9-27 AT SKIN ATTACHMENTS SOURCE SDI 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 INTERVALS NDT SPECIAL DETAILED INSPECTION OF OUTER WING, TOP SKIN PANEL 2 OVERHANG BETWEEN RIB 22 AND RIB 27 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 REV: 07 DATE: 29-Dec-2014 NDT SDI SOURCE: MRB 572126-01-1 572100-200-014 NOTE : - FOR THRESHOLD REFER TO ISB 57-1155. - REFER TO ISB 57-1155 FOR ALTERNATIVE TASK TERMINATING THIS INSPECTION. Sub 2 - Page 223 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 572129-01-1 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 R 572129-01-4 500 600 OUTER WING BOTTOM SKIN ATTACH RIB 8-15 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 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 REV: 07 DATE: 29-Dec-2014 INTERVALS 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 ST: 31000 FC OR 53900 FH SI: 16200 FC OR 28100 FH SOURCE ALI TPS REFERENCES 572100-200-015 MEN TASKM. H. 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 1 1 0.50 0.50 2930 2964 3044 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 SOURCE: ALI 572129-01-1 ALI MRB 572100-200-015 APPL SOURCE: ALI 572129-01-4 MRB 572129-01-4 MRB 572100-200-016 SOURCE: MRB 572130-01-2 Sub 2 - Page 224 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 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 R 572134-01-2 540 640 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 REV: 07 DATE: 29-Dec-2014 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 60000 FH SI: 8800 FC OR 17600 FH T: 53500 FC OR 107000 FH I: 8800 FC OR 17600 FH ALI MRB TPS REFERENCES 572100-200-016 MEN TASKM. H. APPL 1 1 0.50 0.50 2930 2964 3044 1 1 0.20 0.20 1654 1679 1753 2465 2497 2879 2913 1 1 0.20 0.20 2930 2964 3044 SOURCE: ALI 572130-01-7 MRB 572130-01-7 MRB 572100-200-017 SOURCE: MRB 572131-01-1 572100-200-018 SOURCE: ALI 572134-01-2 MRB 572134-01-2 Sub 2 - Page 225 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 572134-01-4 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 R 572137-01-2 500 600 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) 572137-01-4 500 600 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) 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 32000 FC OR 60000 FH I: 10600 FC OR 24200 FH ALI 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: 12 YE I: 6 YE ALI MRB TPS REFERENCES 572100-200-018 MEN TASKM. H. 1 1 0.20 0.20 1654 1679 1753 2465 2497 2879 2913 1 1 0.12 0.12 2930 2964 3044 1 1 0.12 0.12 1654 1679 1753 2465 2497 2879 2913 1 1 1 1 0.13 0.13 0.13 0.13 ALL SOURCE: ALI 572134-01-4 572100-200-019 APPL SOURCE: ALI 572137-01-2 MRB 572137-01-2 ALI 572100-200-019 SOURCE: ALI 572137-01-4 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 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 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 D 572140-01-1 R 572140-01-2 500 540 600 640 500 540 550 560 600 640 650 660 500 540 550 560 600 640 650 660 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 CUTOUTS AF DET DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER SURFACES, AROUND ACCESS DOOR CUTOUTS IN ALL BAYS, BETWEEN RIB 13 AND RIB 27 REV: 07 DATE: 29-Dec-2014 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 T: 10 YE I: 7.5 YE MRB CPCP 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 572100-200-021 SOURCE: MRB 572140-01-1 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 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 572100-200-021 SOURCE: MRB 572140-01-2 MEN TASKM. H. APPL 1 1 1 1 0.30 0.30 0.30 0.30 2930 2964 3044 1 1 1 1 0.30 0.30 0.30 0.30 1654 1679 1753 2465 2497 2879 2913 1 1 1 1 1 1 1 1 0.10 0.10 0.10 0.10 0.10 0.10 0.10 0.10 1 1 1 1 1 1 1 1 0.10 0.10 0.10 0.10 0.10 0.10 0.10 0.10 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 Sub 2 - Page 227 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 572140-02-4 R 572142-01-2 ZONE 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 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 R 572143-01-2 532 533 632 633 OUTER WING BOTTOM SKIN RIB/STGR ATTACH 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 AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS T: 42900 FC OR 85800 FH I: 3300 FC OR 6600 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 ST: 30000 FC OR 60000 FH SI: 10900 FC OR 21800 FH T: 53500 FC OR 107000 FH I: 10900 FC OR 21800 FH SOURCE ALI TPS REFERENCES 572100-210-001 SOURCE: ALI 572140-02-4 ALI 572100-210-002 MEN TASKM. H. APPL 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 0.12 0.12 2930 2964 3044 1 1 0.12 0.12 1654 1679 1753 2465 2497 2879 2913 1 1 1 1 0.10 0.10 0.10 0.10 2930 2964 3044 2930 2964 3044 SOURCE: ALI 572142-01-2 ALI 572100-210-002 SOURCE: ALI 572142-01-3 ALI MRB 572100-200-022 SOURCE: ALI 572143-01-2 MRB 572143-01-2 Sub 2 - Page 228 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 572143-01-5 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 NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 572143-01-2 R 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. R 572148-01-2 500 600 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 8 AND RIB 18, EXCLUDING AREAS COVERED BY PYLON FAIRING AND BY FLAP TRACK 3 FAIRING 572148-01-3 500 600 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 8 AND RIB 18, EXCLUDING AREAS COVERED BY PYLON FAIRING AND BY FLAP TRACK 3 FAIRING R 572149-01-2 500 600 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 18 AND RIB 21, ADJACENT TO FRONT SPAR AND REAR SPAR, EXCLUDING AREA COVERED BY FLAP TRACK 4 FAIRING AF GVI REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 31700 FC OR 54000 FH I: 9400 FC OR 16000 FH ALI T: 50800 FC OR 101600 FH I: 6700 FC OR 13400 FH T: 48300 FC OR 96600 FH I: 6000 FC OR 12000 FH T: 24000 FC OR 40400 FH I: 3800 FC OR 6100 FH T: 56500 FC OR 113000 FH I: 6000 FC OR 12000 FH ALI TPS REFERENCES 572100-200-022 SOURCE: ALI 572143-01-5 572100-210-803 MEN TASKM. H. APPL 1 1 1 1 0.10 0.10 0.10 0.10 1654 1679 1753 2465 2497 2879 2913 1 1 0.32 0.32 2930 2964 3044 1 1 0.15 0.15 2930 2964 3044 1 1 0.15 0.15 1654 1679 1753 2465 2497 2879 2913 1 1 0.10 0.10 2930 2964 3044 SOURCE: ALI 572144-01-5 ALI 572100-210-003 SOURCE: ALI 572148-01-2 ALI 572100-210-003 SOURCE: ALI 572148-01-3 ALI 572100-210-004 SOURCE: ALI 572149-01-2 Sub 2 - Page 229 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 572149-01-3 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 18 AND RIB 21, ADJACENT TO FRONT SPAR AND REAR SPAR, EXCLUDING AREA COVERED BY FLAP TRACK 4 FAIRING R 572150-01-2 532 632 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 572150-01-3 532 632 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 REV: 07 DATE: 29-Dec-2014 INTERVALS T: 25800 FC OR 42000 FH I: 5100 FC OR 8300 FH 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 SOURCE ALI TPS REFERENCES 572100-210-004 MEN TASKM. H. 1 1 0.10 0.10 1654 1679 1753 2465 2497 2879 2913 1 1 0.10 0.10 2930 2964 3044 1 1 0.10 0.10 1654 1679 1753 2465 2497 2879 2913 SOURCE: ALI 572149-01-3 ALI MRB 572100-200-023 APPL SOURCE: ALI 572150-01-2 MRB 572150-01-2 ALI 572100-200-023 SOURCE: ALI 572150-01-3 Sub 2 - Page 230 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 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 REV: 07 DATE: 29-Dec-2014 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 T: 6 YE I: 6 YE MRB CPCP ST: 34500 FC OR 69000 FH SI: 10500 FC OR 21000 FH MRB TPS REFERENCES 572100-200-024 MEN TASKM. H. APPL 1 1 0.10 0.10 2930 2964 3044 1 1 0.10 0.10 1654 1679 1753 2465 2497 2879 2913 1 1 0.12 0.12 ALL 1 1 0.12 0.12 2930 2964 3044 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 572153-01-1 R 572153-01-2 500 600 500 600 OUTER WING BOTTOM SKIN DRAIN HOLES AF 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 OUTER WING BOTTOM SKIN DRAIN HOLES AF 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 DET DET 572100-200-025 SOURCE: MRB 572153-01-1 572100-200-025 SOURCE: MRB 572153-01-2 Sub 2 - Page 231 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 572153-01-3 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 R 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 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 NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 572155-01-1 R 572157-01-1 500 600 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 OUTER WING BOTTOM SKIN RUNOUT 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. NDT SDI REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 ST: 34000 FC OR 68000 FH SI: 20000 FC OR 40000 FH MRB TPS REFERENCES 572100-200-025 MEN TASKM. H. 1 1 0.12 0.12 1654 1679 1753 2465 2497 2879 2913 1 1 1.00 1.00 2930 2964 3044 1 1 1.00 1.00 1654 1679 1753 2465 2497 2879 2913 1 1 0.50 0.50 2930 2964 3044 SOURCE: MRB 572153-01-3 572100-200-026 APPL SOURCE: ALI 572155-01-1 MRB 572155-01-1 ALI 572100-200-026 SOURCE: ALI 572155-01-7 572100-200-027 NTM 57-21-57 SOURCE: MRB 572157-01-1 ACCESS PANELS: 540PB, 540QB, 540RB, 640PB, 640QB, 640RB Sub 2 - Page 232 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 572157-01-5 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 NOTE: CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF TASK 572157-01-1 R 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 & 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 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 & 13 R 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 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 AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 ST: 34000 FC OR 68000 FH SI: 15500 FC OR 31000 FH MRB TPS REFERENCES 572100-200-027 NTM 57-21-57 MEN TASKM. H. 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 1 1 1.00 1.00 2930 2964 3044 1 1 1.00 1.00 1654 1679 1753 2465 2497 2879 2913 1 1 1 1 1 1 0.67 0.67 0.67 0.67 0.67 0.67 2930 2964 3044 SOURCE: MRB 572157-01-5 572100-200-028 APPL SOURCE: ALI 572158-01-2 MRB 572158-01-2 ALI 572100-200-028 SOURCE: ALI 572158-01-5 572100-200-029 SOURCE: MRB 572160-01-2 Sub 2 - Page 233 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 572160-01-5 ZONE 540 550 560 640 650 660 DESCRIPTION OUTER WING BOTTOM SKIN STGR RIB 18-27 SKILL TASK CODE CODE 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 34000 FC OR 58700 FH I: 15500 FC OR 26800 FH ALI T: 10 YE I: 10 YE MRB CPCP T: 12 YE I: 12 YE MRB CPCP ST: 48000 FC OR 60000 FH SI: 11800 FC OR 20200 FH T: 12 YE I: 12 YE T: 6 YE I: 6 YE MRB CPCP TPS REFERENCES 572100-200-029 SOURCE: ALI 572160-01-5 MEN TASKM. H. APPL 1 1 1 1 1 1 0.67 0.67 0.67 0.67 0.67 0.67 1654 1679 1753 2465 2497 2879 2913 1 1 1 1 1 1 0.10 0.10 0.10 0.10 0.10 0.10 1 1 1 1 1 1 0.10 0.10 0.10 0.10 0.10 0.10 2930 2964 3044 1 1 1 1 1 1 0.10 0.10 0.10 0.10 0.10 0.10 1654 1679 1753 2465 2497 2879 2913 1 1 0.17 0.17 ALL ACCESS PANELS: 540NB, 540PB, 540QB, 540RB, 550AB, 550BB, 550CB, 550DB, 560AB, 640NB, 640PB, 640QB, 640RB, 650AB, 650BB, 650CB, 650DB, 660AB D 572161-01-10 R 572161-01-11 572161-01-5 572164-01-1 540 550 560 640 650 660 MAIN STRUCTURE 540 550 560 640 650 660 MAIN STRUCTURE 540 550 560 640 650 660 OUTER WING BOTTOM SKIN ACCESS DOORS 500 600 OUTER WING BOTTOM SKIN FUEL DRAIN AF DET DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, ACCESS DOORS BETWEEN RIB 13 AND RIB 27 NO 572100-200-030 SOURCE: MRB 572161-01-10 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 DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, ACCESS DOORS BETWEEN RIB 13 AND RIB 27 NO 572100-200-030 SOURCE: MRB 572161-01-11 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 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. AF DET NO 572100-200-030 SOURCE: MRB 572161-01-5 MRB CPCP 574100-200-005 SOURCE: MRB 572164-01-1 Sub 2 - Page 234 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 572164-02-6 ZONE 500 600 DESCRIPTION OUTER WING BOTTOM SKIN FUEL DRAIN SKILL TASK CODE CODE AF 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 48000 FC OR 96000 FH I: 8300 FC OR 16600 FH ST: 48000 FC SI: 7500 FC ALI ST: 48000 FC SI: 4500 FC MRB ST: 48000 FC SI: 15000 FC MRB TPS REFERENCES 572100-210-802 MEN TASKM. H. APPL 1 1 0.10 0.10 2930 2964 3044 1 1 1 1 1 1 0.10 0.10 0.10 0.10 0.10 0.10 1654 1679 1753 2465 2497 2879 2913 1 1 1 1 1 1 0.10 0.10 0.10 0.10 0.10 0.10 2930 2964 3044 1 1 1 1 1 1 0.20 0.20 0.20 0.20 0.20 0.20 1654 1679 1753 2465 2497 2879 2913 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 R 572601-01-3 531 532 533 631 632 633 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 572601-02-3 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 572601-02-1 531 532 533 631 632 633 FLAP TRACK BEAMS UPR FLANGE RADII 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 NDT SDI 572600-220-003 NTM 57-26-01 SOURCE: MRB 572601-02-1 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 235 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 572601-02-3 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 572601-01-3 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE ST: 48000 FC SI: 9300 FC MRB ST: 48000 FC SI: 7500 FC MRB ST: 48000 FC SI: 4300 FC MRB T: 6 YE I: 6 YE MRB CPCP ST: 48000 FC SI: 7100 FC MRB TPS REFERENCES 572600-220-003 NTM 57-26-01 SOURCE: MRB 572601-02-3 MEN TASKM. H. APPL 1 1 1 1 1 1 0.20 0.20 0.20 0.20 0.20 0.20 2930 2964 3044 1 1 1 1 1 1 0.10 0.10 0.10 0.10 0.10 0.10 1654 1679 1753 2465 2497 2879 2913 1 1 1 1 1 1 0.10 0.10 0.10 0.10 0.10 0.10 2930 2964 3044 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 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 R 572604-01-4 531 532 533 631 632 633 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 572604-01-4 PREPARATION: FLAPS EXTENDED; ACCESS PANELS: 531AB, 531BB, 531CB, 532AB, 532BB, 532CB, 533AB, 533BB, 533CB, 631AB, 631BB, 631CB, 632AB, 632BB, 632CB, 633AB, 633BB, 633CB 572607-01-1 572607-02-1 531 532 533 631 632 633 531 532 533 631 632 633 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. ACCESS PANELS: 531AB, 531BB, 532AB, 532BB, 533AB, 533BB, 631AB, 631BB, 632AB, 632BB, 633AB, 633BB FLAP TRACK BEAMS FWD SPIGOT ATTACH DETAILED INSPECTION OF OUTER WING, FLAP TRACK BEAMS 2,3,4 FORWARD SPIGOT PINS, BOLTS AND FITTINGS NOTE: REFER TO AMM FOR GAP CHECK AF DET NO 572600-200-006 SOURCE: MRB 572607-01-1 572600-220-004 SOURCE: MRB 572607-02-1 ACCESS PANELS: 531AB, 531BB, 532AB, 532BB, 533AB, 533BB, 631AB, 631BB, 632AB, 632BB, 633AB, 633BB Sub 2 - Page 236 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 572610-01-1 ZONE 531 532 533 631 632 633 DESCRIPTION FLAP TRACK BEAMS AFT SPIGOT SKILL TASK CODE CODE AF DET DETAILED INSPECTION OF OUTER WING, FLAP TRACK BEAMS 2,3,4 AFT SPIGOT NOTE: REFER TO AMM FOR TORQUE CHECK REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 ST: 48000 FC SI: 20000 FC T: 12 YE I: 12 YE MRB CPCP TPS REFERENCES 572600-220-005 SOURCE: MRB 572610-01-1 MEN TASKM. H. APPL 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 1 1 1 1 1 1 0.10 0.10 0.10 0.10 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 ACCESS PANELS: 531CB, 532CB, 533CB, 631CB, 632CB, 633CB OUTER WING REAR SPAR SIDESTAY FITTING AF DET OUTER WING REAR SPAR JACK FITTING AF DET DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT FACE RETRACTION JACK FITTING 572653-01-1 531 532 533 631 632 633 572600-200-010 SOURCE: MRB 572610-02-1 PREPARATION: FLAPS EXTENDED; DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT FACE SIDESTAY FITTING 572651-01-1 NO PREPARATION: RETRACTION ANCHORAGE ACTUATOR REMOVED; BEARING ASSEMBLY REMOVED; FLAP TRACK 2 AFT ATTACH FITTINGS 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 AF DET 572600-200-008 SOURCE: MRB 572650-01-1 MRB CPCP 572600-200-007 SOURCE: MRB 572651-01-1 NO 572600-200-001 SOURCE: MRB 572653-01-1 Sub 2 - Page 237 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 572654-01-1 ZONE 521 621 DESCRIPTION OUTER WING PYLON FWD ATTACH FITTING SKILL TASK CODE CODE 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 AF DET DETAILED INSPECTION OF OUTER WING, AFT PYLON ATTACHMENT FITTING LUG PREPARATION: PYLON FAIRINGS REMOVED; 572658-01-1 531 532 533 631 632 633 OUTER WING BOTTOM SKIN TRACK BEAM FTG 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 AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 ST: 12 YE SI: 12 YE T: 24 YE I: 12 YE MRB CPCP TPS REFERENCES 572600-220-001 NTM 57-26-54 MEN TASKM. H. APPL 1 1 0.50 0.50 2930 2964 3044 1 1 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 1 1 0.10 0.10 ALL 1 1 0.10 0.10 ALL 1 1 1 1 1 1 0.10 0.10 0.10 0.10 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 MRB CPCP 572600-200-009 SOURCE: MRB 572658-01-1 Sub 2 - Page 238 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 573101-01-1 ZONE 534 634 DESCRIPTION WING TIP BOTTOM SKIN LWR SURFACE JOINT SKILL TASK CODE CODE 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 574101-01-1 521 522 621 622 FIXED LE ROLLER PIN HOLES 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 AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS 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 ST: 30000 FC OR 52500 FH SI: 23000 FC OR 32000 FH T: 12 YE I: 6 YE SOURCE ALI MRB TPS REFERENCES 573000-200-001 MEN TASKM. H. APPL 1 1 0.20 0.20 2930 2964 3044 1 1 0.20 0.20 1654 1679 1753 2465 2497 2879 2913 1 1 1 1 0.73 0.73 0.73 0.73 1654 1679 1753 2465 2497 2879 2913 SOURCE: ALI 573101-01-1 MRB 573101-01-1 ALI 573000-200-001 SOURCE: ALI 573101-01-4 MRB CPCP 574100-200-012 SOURCE: MRB 574101-01-1 Sub 2 - Page 239 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 574101-01-3 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 R 574102-01-1 522 622 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; REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 ALI MRB CPCP ST: 48000 FC OR 60000 FH SI: 25500 FC OR 31400 FH MRB TPS REFERENCES 574100-200-012 SOURCE: ALI 574101-01-3 MRB 574101-01-3 MRB 574100-200-013 NTM 57-41-02 MEN TASKM. H. APPL 1 1 1 1 0.73 0.73 0.73 0.73 2930 2964 3044 1 1 0.80 0.80 2930 2964 3044 1 1 0.80 0.80 1654 1679 1753 2465 2497 2879 2913 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 574102-01-4 522 622 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 574100-200-013 NTM 57-41-02 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 Sub 2 - Page 240 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 574106-01-1 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 R 574106-01-3 521 522 621 622 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 REV: 07 DATE: 29-Dec-2014 INTERVALS ST: 12 YE OR 30000 FC OR 52500 FH SI: 6 YE OR 21000 FC OR 29600 FH T: 24 YE I: 6 YE 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 SI: 6 YE T: 24 YE I: 6 YE SOURCE MRB CPCP TPS REFERENCES 574100-200-014 SOURCE: MRB 574106-01-1 MRB CPCP 574100-200-014 SOURCE: MRB 574106-01-3 MRB CPCP 574100-200-015 SOURCE: MRB 574112-01-1 MEN TASKM. H. APPL 1 1 1 1 0.10 0.10 0.10 0.10 1654 1679 1753 2465 2497 2879 2913 1 1 1 1 0.10 0.10 0.10 0.10 2930 2964 3044 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 241 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 D 574145-01-1 521 621 LEADING EDGE ACCESS PANEL LANDING AND ADJACENT AREA AF DET AF DET 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 574201-01-1 500 600 SLAT 1, TRACKS 1-4 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; REV: 07 DATE: 29-Dec-2014 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: 750 FH OR 750 FC OR 4 MO I: 15000 FH OR 10000 FC OR 48 MO ST: 6 YE SI: 6 YE T: 24 YE I: 6 YE ALI MRB TPS REFERENCES 574100-200-016 ALL 1 1 1 1 0.50 0.50 0.50 0.50 1654 1679 1753 2465 2497 2879 2913 JIC A320-57-41-00 ISB 57-1122 1 1 0.25 0.25 574100-200-002 1 1 0.20 0.20 574100-200-017 NTM 57-41-14 NO APPL 0.25 0.25 0.25 0.25 SOURCE: ALI 574114-01-1 MRB 574114-01-1 MRB CPCP TASKM. H. 1 1 1 1 SOURCE: MRB 574113-01-1 ISB MEN ALL SOURCE: MRB 574201-01-1 Sub 2 - Page 242 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 574202-01-1 ZONE 500 600 DESCRIPTION SLAT 1 TRACKS 1-4 ATTACHMENTS SKILL TASK CODE CODE 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 12 YE I: 6 YE MRB CPCP 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 574200-200-001 MEN TASKM. H. APPL 1 1 0.20 0.20 1654 1679 1753 1 1 0.20 0.20 2465 2497 2930 2964 3044 2879 2913 1 1 0.20 0.20 ALL 1 1 0.40 0.40 ALL SOURCE: MRB 574202-01-1 PREPARATION: BOLTS SUCCESSIVELY REMOVED; SLATS FULLY EXTENDED; 574202-01-2 500 600 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 574204-01-1 500 600 PREPARATION: SLATS FULLY EXTENDED; 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 574200-200-001 SOURCE: MRB 574202-01-2 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 243 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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; R 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 REV: 07 DATE: 29-Dec-2014 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 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. H. APPL 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 1654 1679 1753 1 1 0.10 0.10 2465 2497 2930 2964 3044 2879 2913 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; 574302-01-2 500 600 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 574304-01-1 500 600 PREPARATION: SLATS FULLY EXTENDED; 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 574300-200-008 SOURCE: MRB 574302-01-2 NO 574300-200-002 SOURCE: MRB 574304-01-1 Sub 2 - Page 244 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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; R 574402-01-1 500 600 SLAT 3 TRACK 7-8 ATTACHMENTS AF DET DETAILED INSPECTION OF SLAT 3, TRACKS 7 AND 8 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, BOLTS, LINKS AND SIDE PLATES, LH/RH REV: 07 DATE: 29-Dec-2014 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 T: 12 YE I: 6 YE MRB CPCP TPS NO REFERENCES 574300-200-003 NTM 57-43-04 MEN TASKM. H. APPL 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 1654 1679 1753 1 1 0.10 0.10 2465 2497 2930 2964 3044 2879 2913 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; 574402-01-2 500 600 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 NO 574400-200-010 SOURCE: MRB 574402-01-2 PREPARATION: SLATS FULLY EXTENDED; Sub 2 - Page 245 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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; R 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 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 1654 1679 1753 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 246 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 574502-01-2 ZONE 500 600 DESCRIPTION SLAT 4 TRACK 9-10 ATTACHMENTS SKILL TASK CODE CODE AF DET DETAILED INSPECTION OF SLAT 4, TRACKS 9 AND 10 ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK LUGS, BOLTS, LINKS AND SIDE PLATES, LH/RH 574504-01-1 500 600 PREPARATION: SLATS FULLY EXTENDED; SLAT 4 SKIN CONNECTIONS 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 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; AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 T: 12 YE I: 6 YE MRB CPCP ST: 6 YE SI: 6 YE T: 24 YE I: 6 YE MRB CPCP TPS NO REFERENCES 574500-200-008 MEN TASKM. H. 1 1 0.10 0.10 2465 2497 2930 2964 3044 2879 2913 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 SOURCE: MRB 574502-01-2 NO 574500-200-005 APPL 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 Sub 2 - Page 247 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 574602-01-1 ZONE 500 600 DESCRIPTION SLAT 5 TRACK 11-12 ATTACHMENTS SKILL TASK CODE CODE AF DET DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND 12 ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK LUGS, BOLTS, LINKS AND SIDE PLATES, LH/RH REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 12 YE I: 6 YE MRB CPCP 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 T: 12 YE I: 6 YE MRB CPCP TPS NO REFERENCES 574600-200-008 MEN TASKM. H. APPL 1 1 0.10 0.10 1654 1679 1753 1 1 0.10 0.10 2465 2497 2930 2964 3044 2879 2913 1 1 0.10 0.10 ALL 1 1 0.50 0.50 ALL 1 1 0.15 0.15 ALL SOURCE: MRB 574602-01-1 PREPARATION: BOLTS SUCCESSIVELY REMOVED; SLATS FULLY EXTENDED; 574602-01-2 500 600 SLAT 5 TRACK 11-12 ATTACHMENTS AF DET DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND 12 ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK LUGS, BOLTS, LINKS AND SIDE PLATES, LH/RH 574604-01-1 500 600 PREPARATION: SLATS FULLY EXTENDED; SLAT 5 SKIN CONNECTIONS 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 DETAILED INSPECTION OF SLAT 5, TRAILING EDGE, LOWER FACE LH/RH AF DET NO 574600-200-008 SOURCE: MRB 574602-01-2 NO 574600-200-005 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 PREPARATION: SLATS FULLY EXTENDED; Sub 2 - Page 248 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 575101-01-1 575101-02-1 R 575101-02-3 575104-01-1 ZONE 531 532 533 631 632 633 531 532 533 631 632 633 531 532 533 631 632 633 500 600 DESCRIPTION TRAILING EDGE FLAP ACTUATOR BRACKETS SKILL TASK CODE CODE 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 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 FLAP ACTUATOR BRACKETS 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; 575106-01-1 574 575 582 583 584 585 586 674 675 682 683 684 685 686 TRAILING EDGE SPOILERS HINGE PINS 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 PREPARATION: PINS REMOVED; ACCESS PANELS: 573BB, 575BB, 575DB, 575EB, 575GB, 673BB, 675BB, 675DB, 675EB, 675GB AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 12 YE I: 12 YE MRB CPCP ST: 48000 FC SI: 20000 FC MRB 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 TPS REFERENCES 575100-220-004 SOURCE: MRB 575101-01-1 575100-220-005 NTM 57-51-01 SOURCE: MRB 575101-02-1 575100-220-005 NTM 57-51-01 SOURCE: MRB 575101-02-3 575100-220-006 MEN TASKM. H. APPL 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 1 1 1 1 1 1 0.75 0.75 0.75 0.75 0.75 0.75 2930 2964 3044 1 1 0.30 0.30 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 0.03 0.03 ALL 1654 1679 1753 2465 2497 2879 2913 SOURCE: MRB 575104-01-1 MRB 575100-210-001 SOURCE: MRB 575106-01-1 Sub 2 - Page 249 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 575106-02-1 575106-03-1 575107-01-1 ZONE 574 575 582 583 584 585 586 674 675 682 683 684 685 686 574 575 582 583 584 585 586 674 675 682 683 684 685 686 575 583 584 585 586 675 683 684 685 686 DESCRIPTION TRAILING EDGE SPOILERS HINGE PINS SKILL TASK CODE CODE NDT SDI 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE ST: 48000 FC SI: 20000 FC MRB T: 12 YE I: 12 YE MRB CPCP T: 12 YE I: 6 YE MRB CPCP TPS REFERENCES 575100-220-015 NTM 57-51-06 SOURCE: MRB 575106-02-1 PREPARATION: PINS REMOVED; ACCESS PANELS: 573BB, 575BB, 575DB, 575EB, 575GB, 673BB, 675BB, 675DB, 675EB, 675GB TRAILING EDGE SPOILERS HINGE PINS AF DET DETAILED INSPECTION OF OUTER WING TRAILING EDGE SPOILERS 1,2,3,4 AND 5 HINGE PINS 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 DETAILED INSPECTION OF OUTER WING, TRAILING EDGE, SPOILERS 2,3,4 AND 5 ACTUATOR AND HINGE FITTINGS PREPARATION: FLAPS EXTENDED; SPOILERS EXTENDED; AF DET 575100-220-009 SOURCE: MRB 575107-01-1 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 TASKM. H. 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 0.20 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 APPL ALL ALL ALL Sub 2 - Page 250 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 575107-02-1 R 575107-02-3 575119-01-1 ZONE 575 583 584 585 586 675 683 684 685 686 575 583 584 585 586 675 683 684 685 686 575 590 675 690 DESCRIPTION TRAILING EDGE SPOILER 2-5 FITTINGS SKILL TASK CODE CODE NDT SDI SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING, TRAILING EDGE, SPOILERS 2,3,4 AND 5 ACTUATOR AND HINGE FITTINGS 575 590 675 690 INTERVALS SOURCE ST: 48000 FC SI: 15000 FC MRB ST: 48000 FC SI: 13600 FC MRB ST: 30500 FC SI: 16500 FC T: 12 YE I: 12 YE ST: 48000 FC SI: 15000 FC MRB CPCP TPS REFERENCES 575100-220-010 NTM 57-51-07 SOURCE: MRB 575107-02-1 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 575107-02-3 PREPARATION: FLAPS AND SPOILERS EXTENDED; TRAILING EDGE AILERON HINGE FITTINGS 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 REV: 07 DATE: 29-Dec-2014 TRAILING EDGE AILERON HINGE PINS DETAILED INSPECTION OF OUTER WING, TRAILING EDGE, AILERON HINGE PINS 1 TO 5 NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 575120-02-1 AF DET 575100-220-001 SOURCE: MRB 575119-01-1 MRB 575100-220-002 SOURCE: MRB 575120-01-1 MEN TASKM. H. APPL 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 0.75 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 0.13 0.13 0.13 0.13 1654 1679 1753 2465 2497 2879 2913 1 1 1 1 0.30 0.30 0.30 0.30 ALL 2930 2964 3044 ALL PREPARATION: PINS REMOVED; ACCESS PANELS: 575AT, 575JB, 575KB, 575LB, 575MB, 675AT, 675JB, 675KB, 675LB, 675MB Sub 2 - Page 251 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 575120-02-1 ZONE 575 590 675 690 DESCRIPTION TRAILING EDGE AILERON HINGE PINS SKILL TASK CODE CODE NDT SDI SPECIAL DETAILED INSPECTION (MPI) OF OUTER WING, TRAILING EDGE, AILERON HINGE PINS 1 TO 5 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE ST: 48000 FC SI: 20000 FC MRB T: 12 YE I: 7.5 YE MRB CPCP 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 TPS REFERENCES 575100-220-013 NTM 57-51-20 MEN TASKM. H. APPL 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 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 2930 2964 3044 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 AF DET DETAILED INSPECTION OF OUTER WING, TRAILING EDGE, AILERON HINGE PINS 1 TO 5 575100-220-016 SOURCE: MRB 575120-03-1 PREPARATION: PINS REMOVED; 575121-01-1 575 590 675 690 ACCESS PANELS: 575AT, 575JB, 575KB, 575LB, 575MB, 675AT, 675JB, 675KB, 675LB, 675MB TRAILING EDGE AILERON ACTUATOR FITTING AF DET DETAILED INSPECTION OF OUTER WING, TRAILING EDGE, AILERON, INBOARD AND OUTBOARD ACTUATOR FITTINGS ACCESS PANELS: 575KB, 575LB, 675KB, 675LB R 575130-01-2 575 675 TRAILING EDGE SPOILER2-4 FITTINGS/LEGS 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) NDT SDI MRB 575100-220-003 SOURCE: MRB 575130-01-2 PREPARATION: FLAPS AND SPOILERS EXTENDED; Sub 2 - Page 252 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 575140-01-1 ZONE 147 148 DESCRIPTION FLAP TRACK 1 SKILL TASK CODE CODE 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 AF DET DETAILED INSPECTION OF OUTER WING, MLG SUPPORT RIB 5, OUTBOARD AND INBOARD FACES R 575151-01-2 573 574 673 674 ACCESS PANELS: 574AB, 674AB TRAILING EDGE FALSE REAR SPAR 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 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 AF DET REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 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 TPS REFERENCES 575100-200-003 MEN TASKM. H. APPL 1 1 0.30 0.30 ALL 1 1 0.30 0.30 ALL 1 1 0.50 0.50 ALL 1 1 1 1 0.38 0.38 0.38 0.38 2930 2964 3044 1 1 1 1 0.38 0.38 0.38 0.38 1654 1679 1753 2465 2497 2879 2913 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 575100-200-006 SOURCE: MRB 575151-01-2 575100-200-006 SOURCE: MRB 575151-01-4 ACCESS PANELS: 573AB, 573BB, 573CB, 574AB, 574BB, 673AB, 673BB, 673CB, 674AB, 674BB Sub 2 - Page 253 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 575155-01-4 ZONE 500 600 DESCRIPTION OUTER WING TRAILING EDGE TOP SKIN SKILL TASK CODE CODE 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 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 R 575158-01-5 500 600 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 R 575159-01-1 500 600 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 REV: 07 DATE: 29-Dec-2014 INTERVALS T: 55800 FC OR 111600 FH I: 10200 FC OR 20400 FH T: 24000 FC OR 42000 FH I: 5200 FC OR 8800 FH T: 25400 FC OR 50800 FH I: 13600 FC OR 27200 FH ST: 30000 FC OR 60000 FH SI: 9000 FC OR 18000 FH SOURCE ALI TPS REFERENCES 575100-210-802 MEN TASKM. H. APPL 1 1 0.20 0.20 2930 2964 3044 1 1 0.10 0.10 1654 1679 1753 2465 2497 2879 2913 1 1 0.10 0.10 2930 2964 3044 1 1 0.10 0.10 2930 2964 3044 SOURCE: ALI 575155-01-4 ALI 575100-210-003 SOURCE: ALI 575158-01-1 ALI 575100-210-003 SOURCE: ALI 575158-01-5 MRB 575100-200-007 SOURCE: MRB 575159-01-1 Sub 2 - Page 254 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 575159-01-5 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 CURVED SKIN EDGE, AFT OF REAR SPAR JUST INBOARD OF MLG SUPPORT RIB 5 575160-01-1 574 674 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; R 575160-01-5 574 674 ACCESS PANELS: 574AB, 674AB TRAILING EDGE BOTTOM SKIN REAR SPAR 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 NDT SDI REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE ST: 30000 FC OR 48000 FH SI: 7500 FC OR 12000 FH T: 41200 FC OR 60000 FH I: 7500 FC OR 12000 FH T: 24000 FC OR 38400 FH I: 11800 FC OR 18900 FH ALI MRB ST: 33500 FC OR 67000 FH SI: 11800 FC OR 23600 FH T: 60000 FC OR 120000 FH I: 11800 FC OR 23600 FH ALI MRB TPS REFERENCES 575100-200-007 MEN TASKM. H. 1 1 0.10 0.10 1654 1679 1753 2465 2497 2879 2913 1 1 0.80 0.80 1654 1679 1753 2465 2497 2879 2913 1 1 0.80 0.80 2930 2964 3044 SOURCE: ALI 575159-01-5 MRB 575159-01-5 ALI 575100-200-008 NTM 57-51-60 SOURCE: ALI 575160-01-1 575100-200-008 NTM 57-51-60 APPL SOURCE: ALI 575160-01-5 MRB 575160-01-5 Sub 2 - Page 255 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 575161-01-1 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 R 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; 575163-01-6 574 674 OUTER WING BOTTOM SKIN UNDER PYLON FAIRING 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 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 NDT SDI REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 24000 FC OR 42000 FH I: 3800 FC OR 6400 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: 10000 FC OR 15500 FH ALI ST: 30000 FC OR 52500 FH SI: 11400 FC OR 19000 FH MRB TPS REFERENCES 575100-210-004 MEN TASKM. H. 1 1 0.10 0.10 1654 1679 1753 2465 2497 2879 2913 1 1 0.75 0.75 2930 2964 3044 1 1 0.75 0.75 1654 1679 1753 2465 2497 2879 2913 1 1 1 1 0.75 0.75 0.75 0.75 1654 1679 1753 2465 2497 2879 2913 SOURCE: ALI 575161-01-1 ALI MRB 575100-220-011 NTM 57-51-63 APPL SOURCE: ALI 575163-01-2 MRB 575163-01-2 MRB 575100-220-011 NTM 57-51-63 SOURCE: MRB 575163-01-6 575100-220-012 NTM 57-51-64 SOURCE: MRB 575164-01-2 Sub 2 - Page 256 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 575165-01-3 ZONE 531 574 631 674 DESCRIPTION OUTER WING BOTTOM SKIN UND FLAP 2 FAIR SKILL TASK CODE CODE 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 R 575166-01-2 574 674 OUTER WING FALSE REAR SPAR LWR FLANGE AF DET 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 575166-01-4 574 674 OUTER WING FALSE REAR SPAR LWR FLANGE 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE ST: 30000 FC OR 52500 FH SI: 12700 FC OR 21100 FH MRB ST: 48000 FC OR 96000 FH SI: 7000 FC OR 14000 FH MRB ST: 48000 FC OR 60000 FH SI: 7300 FC OR 12300 FH MRB T: 6 YE I: 6 YE MRB CPCP ST: 12 YE OR 32000 FC SI: 12 YE OR 13900 FC T: 24 YE I: 12 YE MRB CPCP TPS REFERENCES 575100-200-009 SOURCE: MRB 575165-01-3 575100-200-010 MEN TASKM. H. APPL 1 1 1 1 0.10 0.10 0.10 0.10 1654 1679 1753 2465 2497 2879 2913 1 1 0.10 0.10 2930 2964 3044 1 1 0.10 0.10 1654 1679 1753 2465 2497 2879 2913 1 1 0.10 0.10 ALL 1 1 0.30 0.30 ALL SOURCE: MRB 575166-01-2 575100-200-010 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. 575203-01-1 581 681 ACCESS PANELS: 574AB, 574BB, 674AB, 674BB 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 1+2 575100-200-011 SOURCE: MRB 575167-01-1 NO 575200-200-007 SOURCE: MRB 575203-01-1 Sub 2 - Page 257 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 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 258 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 D 575221-02-1 581 681 PREPARATION: RUBBER SEALS; FLAPS EXTENDED; FLAPS REV: 07 DATE: 29-Dec-2014 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 MRB CPCP ACCESS PANELS: 193AB, 193BB, 195AB, 195BB, 734, 194AB, 194BB, 744 INBOARD FLAP TRACK 2 CARRIAGE DETAILED INSPECTION OF OUTER WING, INBOARD FLAP TRACK 2 CARRIAGE FORGING PREPARATION: FLAPS EXTENDED; 575200-200-002 NO MEN TASKM. H. APPL 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 SOURCE: MRB 575210-01-1 MRB CPCP 575200-200-004 SOURCE: MRB 575211-01-1 DET I: 4000 FH EASA AD FAA AD ISB 575200-210-010 EASA AD 2010-0209 FAA AD 2008-05-12 ISB 57-1133 1 1 0.50 0.50 AF DET ST: 12 YE SI: 12 YE T: 24 YE I: 12 YE MRB CPCP 575200-200-005 1 1 0.10 0.10 PREPARATION: FLAPS EXTENDED; 500 600 REFERENCES AF DETAILED INSPECTION OF INBOARD FLAP TRUNNION AND SLIDING PANEL 575250-01-1 TPS ALL SOURCE: MRB 575250-01-1 Sub 2 - Page 259 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 575250-02-1 ZONE 500 600 DESCRIPTION INBOARD FLAP TRACK 2 CARRIAGE SKILL TASK CODE CODE NDT SDI SPECIAL DETAILED INSPECTION (U/S) OF OUTER WING, INBOARD FLAP TRACK 2 CARRIAGE FORGING 575251-01-1 500 600 PREPARATION: FLAPS EXTENDED; INBOARD FLAP TRACK 2 ROLLERS 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 D 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE ST: 48000 FC SI: 20000 FC MRB 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 575200-220-004 NTM 57-52-50 MEN TASKM. H. APPL 1 1 0.80 0.80 ALL 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 SOURCE: MRB 575250-02-1 575200-200-001 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 260 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V D 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 1 1 0.75 0.75 1 1 0.75 0.75 1654 1679 1753 1 1 0.30 0.30 1654 1679 1753 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; R 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 261 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 1 1 0.75 0.75 1654 1679 1753 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 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. D 575309-01-1 532 587 632 687 PREPARATION: COVER TAPES FROM INSPECTION HOLES REMOVED; RUBBER SEALS; FLAPS EXTENDED; OUTBOARD FLAP SUPPORT TRACK 3 AF 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 DET NO 575300-200-005 SOURCE: MRB 575309-01-1 Sub 2 - Page 262 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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. REV: 07 DATE: 29-Dec-2014 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. H. 1 1 1 1 0.30 0.30 0.30 0.30 1 1 1 1 0.75 0.75 0.75 0.75 1 1 1 1 0.40 0.40 0.40 0.40 APPL 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 PREPARATION: LEADING EDGE PANEL 2 REMOVED; FLAPS EXTENDED; D 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 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 PREPARATION: FLAPS EXTENDED; COVER TAPES FROM INSPECTION HOLES REMOVED; ACCESS PANELS: 532AT, 532CB, 632AT, 632CB Sub 2 - Page 263 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 D 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. REV: 07 DATE: 29-Dec-2014 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. H. 1 1 1 1 0.30 0.30 0.30 0.30 1 1 0.30 0.30 1 1 0.75 0.75 APPL ALL SOURCE: MRB 575312-01-1 PREPARATION: LEADING EDGE PANEL 2; FLAPS EXTENDED; D 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 264 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 1 1 0.75 0.75 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1 1 1 1 0.10 0.10 0.10 0.10 1654 1679 1753 1 1 1 1 0.10 0.10 0.10 0.10 2465 2497 2930 2964 3044 2879 2913 SOURCE: MRB 575312-02-4 NOTE: INSPECTION IS THROUGH INSPECTION HOLES. PREPARATION: COVER TAPES FROM INSPECTION HOLES REMOVED; FLAPS EXTENDED; R 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 265 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 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. REV: 07 DATE: 29-Dec-2014 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. H. APPL 1 1 1 1 0.75 0.75 0.75 0.75 1654 1679 1753 1 1 1 1 0.75 0.75 0.75 0.75 2465 2497 2930 2964 3044 2879 2913 1 1 1 1 0.30 0.30 0.30 0.30 1654 1679 1753 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; R 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 266 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 R 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. REV: 07 DATE: 29-Dec-2014 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. H. APPL 1 1 1 1 0.30 0.30 0.30 0.30 2465 2497 2930 2964 3044 2879 2913 1 1 0.30 0.30 1654 1679 1753 1 1 0.30 0.30 2465 2497 2930 2964 3044 2879 2913 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 267 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R 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. REV: 07 DATE: 29-Dec-2014 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. H. APPL 1 1 0.75 0.75 1654 1679 1753 1 1 0.75 0.75 2465 2497 2930 2964 3044 2879 2913 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 268 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 576103-01-1 532 533 632 633 575 675 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; AILERON HINGE AND ACTUATOR FITTINGS AF DET DETAILED INSPECTION OF AILERON, HINGE FITTINGS AND ACTUATOR ATTACHMENT FITTINGS ACCESS PANELS: 575AT, 575KB, 575LB, 575MB, 675AT, 675KB, 675LB, 675MB 576104-01-1 500 600 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 AF DET REV: 07 DATE: 29-Dec-2014 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 ST: 30000 FC SI: 15800 FC T: 12 YE OR 38700 FC I: 12 YE OR 15800 FC T: 12 YE I: 12 YE ALI MRB CPCP TPS REFERENCES 575300-200-001 MEN TASKM. H. APPL 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 0.10 0.10 ALL 1 1 0.50 0.50 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 576000-200-002 SOURCE: ALI 576103-01-1 MRB 576103-01-1 MRB 576000-200-003 SOURCE: MRB 576104-01-1 Sub 2 - Page 269 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 576106-01-1 ZONE 500 600 DESCRIPTION AILERON UPPER AND LOWER SKINS SKILL TASK CODE CODE AF 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. REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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 576000-210-001 MEN TASKM. H. APPL 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 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 270 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 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 Sub 2 - Page 271 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 711300-01-1 712111-01-1 712111-02-1 ZONE 437 438 447 448 435 436 445 446 451 461 435 436 445 446 451 461 DESCRIPTION FAN COWL DOOR HINGE FITTINGS SKILL TASK CODE CODE AF GVI GENERAL VISUAL INSPECTION OF FAN COWL DOOR HINGE FITTINGS ACCESS PANELS: 437AL, 438AR, 447AL, 448AR FORWARD ENGINE MOUNT EN DET DETAILED INSPECTION OF FORWARD ENGINE MOUNT INSTALLATION ACCESS PANELS: 437AL, 438AR, 447AL, 448AR, 451AL, 452AR, 461AL, 462AR FORWARD ENGINE MOUNT 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 7500 FC I: 7500 FC ALI 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 ALI TPS REFERENCES 711313-220-040 SOURCE: ALI 711300-01-1 712111-210-040 SOURCE: ALI 712111-01-1 MRB CPCP NO 712111-210-042 SOURCE: MRB 712111-02-1 MEN TASKM. H. APPL 1 1 1 1 0.20 0.20 0.20 0.20 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 0.50 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 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 SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF FORWARD ENGINE MOUNT LINK LUGS ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR NDT SDI 712111-210-803 SOURCE: ALI 712111-05-4 ALI 712112-200-803 SOURCE: ALI 712112-01-1 Sub 2 - Page 272 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 712211-01-1 ZONE 451 453 454 461 463 464 DESCRIPTION AFT ENGINE MOUNT SKILL TASK CODE CODE EN DET 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 REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 12 YE I: 12 YE NOTE MRB CPCP 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 ALI TPS NO REFERENCES 712211-210-040 SOURCE: MRB 712211-01-1 MEN TASKM. H. APPL 1 1 1 1 1 1 0.50 0.50 0.50 0.50 0.50 0.50 ALL 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 1 1 0.63 0.63 ALL 1 1 0.80 0.80 ALL PREPARATION: ENGINE MOUNT DISASSEMBLED; ENGINE REMOVED; ACCESS PANELS: 451AL, 437AL, 438AR, 452AR, 461AL, 447AL, 448AR, 462AR 712211-03-1 712211-05-1 451 453 454 461 463 464 AFT ENGINE MOUNT 450 460 AFT ENGINE MOUNT 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 DETAILED INSPECTION OF AFT ENGINE MOUNT PINS ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR EN DET 712211-210-042 SOURCE: ALI 712211-03-1 ALI 712211-210-803 SOURCE: ALI 712211-05-1 ALI 712212-210-802 SOURCE: ALI 712212-01-1 ALI 712211-210-802 SOURCE: ALI 712213-01-1 Sub 2 - Page 273 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 781112-C1-2 ZONE 450 460 DESCRIPTION CENTERBODY SKILL TASK CODE CODE EN DET REV: 07 DATE: 29-Dec-2014 INTERVALS I: NOTE SOURCE AOL MRB 6 DETAILED INSPECTION OF THE EXHAUST CENTERBODY IN ACCORDANCE WITH ROHR AOL CFM56-003. 783001-01-1 451 452 461 462 NOTE: - TASK INTERVAL OF 400 FH IS APPLICABLE TO ENGINES WITH CENTERBODY P/N 238-0451-507 UNTIL 238-0451-509 WITH ROHR SB RA3207865 NOT EMBODIED - TASK INTERVAL OF 3000 FH IS APPLICABLE TO ENGINES WITH CENTERBODY P/N 238-0451-7R AND 238-0451-9R AND ALSO TO CENTERBODIES WITH ROHR SB RA32078-65 EMBODIED - CENTERBODY WITH P/N 238-0451-511 AND HIGHER DO NOT REQUIRE INSPECTION. THRUST REV 12 O´CLOCK BEAM JUNCTION AF DET DETAILED INSPECTION OF THRUST REVERSER 12 O´CLOCK BEAM JUNCTION WITH THE FORWARD FRAME ACCESS PANELS: 437AL, 451AL, 438AR, 452AR, 447AL, 461AL, 448AR, 462AR 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 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 AF REFERENCES 781112-210-041 AOL CFM 56-003 VSB RA32078-65 MEN TASKM. H. APPL 1 1 0.42 0.42 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 SOURCE: MRB 78.11.00/04-C5 PREPARATION: HEAT SHIELDS REMOVED; THRUST REVERSERS REMOVED; 783002-01-1 TPS DET 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: 10 YE OR 24000 FC I: 10 YE OR 12000 FC ALI MRB CPCP 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 Sub 2 - Page 274 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER 783004-01-1 ZONE 451 452 461 462 DESCRIPTION THRUST REVERSER FORWARD FRAME SKILL TASK CODE CODE NDT SDI SPECIAL DETAILED INSPECTION (HFEC) OF THRUST REVERSER FORWARD FRAME AT ACTUATOR ATTACHMENT REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE T: 24000 FC I: 12000 FC ALI T: 10 YE I: 10 YE MRB CPCP T: 7500 FC I: 7500 FC ALI I: 6 YE MRB TPS REFERENCES 783200-210-043 SOURCE: ALI 783004-01-1 MEN TASKM. H. APPL 1 1 1 1 TBD TBD TBD TBD ALL 1 1 1 1 0.20 0.20 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 2930 2964 3044 1 1 0.10 0.10 1654 1679 1753 2465 2497 2879 2913 1 1 0.10 0.10 1654 1679 1753 2465 2497 2879 2913 PREPARATION: ACTUATORS REMOVED; ACCESS PANELS: 437AL, 451AL, 438AR, 452AR, 447AL, 461AL, 448AR, 462AR 783004-02-1 451 452 461 462 THRUST REVERSER FORWARD FRAME AF DET DETAILED INSPECTION OF THRUST REVERSER FORWARD FRAME AT ACTUATOR ATTACHMENT 1+2 783200-210-046 SOURCE: MRB 783004-02-1 PREPARATION: ACTUATORS REMOVED; ACCESS PANELS: 437AL, 451AL, 438AR, 452AR, 447AL, 461AL, 448AR, 462AR 783200-01-1 451 452 461 462 "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 R ZL-833-02-1 833 834 843 844 FWD AND AFT EMERGENCY EXITS AF GVI 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) 052830-200-013 SOURCE: MRB ZL-834-05-1 AF GVI I: 6 YE MRB 052830-200-014 SOURCE: MRB ZL-834-06-1 ACCESS PANELS: 834, 834AZ, 834BZ, 844, 844AZ, 844BZ Sub 2 - Page 275 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 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 2930 2964 3044 1 1 1 0.20 0.20 0.20 1654 1679 1753 2465 2497 2879 2913 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) R 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 276 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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) REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE I: 6 YE OR 24000 FH MRB I: 24 MO MRB TPS REFERENCES 052120-200-008 MEN TASKM. H. APPL 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 ALL 1 1 0.20 0.20 2930 2964 3044 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) R 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: 6 YE OR 24000 FH MRB 052130-200-001 SOURCE: MRB ZL-131-01-1 052130-200-004 SOURCE: MRB ZL-131-02-1 ACCESS PANELS: 131AC, 131BC, 131FF, 131GF, 131GW, 131HW, 131JF, 131KF, 131MW, 132FF, 132GF, 132JF, 132MW, 825 Sub 2 - Page 277 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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) REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE I: 6 YE OR 24000 FH MRB I: 12 YE MRB TPS REFERENCES 052130-200-004 MEN TASKM. H. APPL 1 1 0.20 0.20 1654 1679 1753 2465 2497 2879 2913 1 1 0.30 0.30 ALL 1 1 0.25 0.25 ALL 1 1 0.20 0.20 ALL 1 1 0.30 0.30 ALL 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 I: 12 YE MRB 052130-200-002 SOURCE: MRB ZL-133-01-1 PREPARATION: FLOOR PANELS FROM FR 24 TO FR 34; ZL-137-01-1 137 138 ACCESS PANELS: 133AL, 825, 134AR BAY BEHIND FWD CARGO COMPARTMENT AF GVI GENERAL VISUAL INSPECTION OF BAY BEHIND FWD CARGO COMPARTMENT (EWIS) 052130-200-003 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 GENERAL VISUAL INSPECTION OF CENTER WING BOX (EWIS) AF GVI 052140-200-001 SOURCE: MRB ZL-141-01-1 ACCESS PANELS: 147AZ, 734, 148AZ, 744 Sub 2 - Page 278 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER ZL-145-01-1 ZONE 145 146 DESCRIPTION ZONE UNDER CABIN FLOOR SKILL TASK CODE CODE AF GVI REV: 07 DATE: 29-Dec-2014 INTERVALS I: 6 YE SOURCE MRB GENERAL VISUAL INSPECTION OF ZONE UNDER CABIN FLOOR (EWIS) TPS REFERENCES 052140-200-002 MEN TASKM. H. APPL 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 1 1 0.25 0.25 1 1 0.25 0.25 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 AF GVI GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT (AS FAR AS VISIBLE, IF ACT IS INSTALLED) (EWIS) D ZL-151-02-1 151 152 ACCESS PANELS: 826 AFT CARGO COMPARTMENT 052140-200-004 AF GVI GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT (EWIS) I: 6 YE OR 24000 FH MRB I: 4 MO OR 750 FH OR 750 FC I: 6 YE OR 24000 FH MRB I: 6 YE OR 24000 FH MRB 052140-200-005 SOURCE: MRB ZL-147-03-1 052150-200-001 SOURCE: MRB ZL-151-01-1 MRB 052150-200-003 SOURCE: MRB ZL-151-02-1 PREPARATION: ACT(S) REMOVED (IF INSTALLED); ZL-151-02-3 151 152 ACCESS PANELS: 151AC, 151AW, 151BW, 151CC, 151CW, 151DW, 151EW, 151HW, 151JW, 152BW, 152CW, 152DW, 152FW, 152GW, 152HW, 152JW, 826 AFT CARGO COMPARTMENT GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT (EWIS) AF GVI 052150-200-003 2930 2964 3044 SOURCE: MRB ZL-151-02-3 PREPARATION: ACT(S) REMOVED (IF INSTALLED); ACCESS PANELS: 151AC, 151AW, 151BW, 151CW, 151DW, 151EW, 151GC, 151HW, 151JW, 152BW, 152CW, 152DW, 152FW, 152GW, 152HW, 152JW, 826 Sub 2 - Page 279 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER ZL-151-02-5 ZONE 151 152 DESCRIPTION AFT CARGO COMPARTMENT SKILL TASK CODE CODE AF GVI GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT (EWIS) REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE I: 6 YE OR 24000 FH MRB I: 12 YE MRB TPS REFERENCES 052150-200-003 MEN TASKM. H. APPL 1 1 0.25 0.25 1654 1679 1753 2465 2497 2879 2913 1 1 0.20 0.20 ALL 1 1 0.20 0.20 ALL 1 1 0.10 0.10 ALL 1 1 0.20 0.20 ALL 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 I: 6 YE OR 24000 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 AF GVI GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT (AS FAR AS VISIBLE, IF ACT IS INSTALLED) (EWIS) ZL-161-02-1 161 162 ACCESS PANELS: 826 BULK CARGO COMPARTMENT GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT (EWIS) AF GVI 052160-200-001 SOURCE: MRB ZL-161-01-1 052160-200-003 SOURCE: MRB ZL-161-02-1 PREPARATION: ACT(S) REMOVED (IF INSTALLED); ACCESS PANELS: 161AC, 161AW, 161BW, 161CW, 162BW, 162CW, 162EW, 826 Sub 2 - Page 280 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER ZL-161-03-1 ZONE 161 162 DESCRIPTION BULK CARGO COMPARTMENT SKILL TASK CODE CODE AF GVI REV: 07 DATE: 29-Dec-2014 INTERVALS I: 12 YE SOURCE MRB GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT (EWIS) TPS REFERENCES 052160-200-004 MEN TASKM. H. APPL 1 1 0.20 0.20 1654 1679 1753 2465 2497 2879 2913 1 1 0.20 0.20 2930 2964 3044 1 1 0.30 0.30 2930 2964 3044 1 1 0.30 0.30 1654 1679 1753 2465 2497 2879 2913 1 1 0.25 0.25 1654 1679 1753 2465 2497 2879 2913 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 R 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; R 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 AF GVI I: 6 YE MRB GENERAL VISUAL INSPECTION OF UNDERFLOOR BAY OF BULK CARGO COMPARTMENT (EWIS) 052160-200-002 SOURCE: MRB ZL-163-01-2 PREPARATION: FLOOR PANELS FROM FR 59 TO FR 65; ACT(S) REMOVED (IF INSTALLED); ZL-171-01-1 171 172 ACCESS PANELS: 826 AFT CABIN UNDERFLOOR COMPARTMENT GENERAL VISUAL INSPECTION OF AFT CABIN UNDERFLOOR COMPARTMENT (EWIS) AF GVI I: 24 MO OR 7500 FH MRB 052170-200-001 SOURCE: MRB ZL-171-01-1 ACCESS PANELS: 161DW, 171AL, 162DW, 172AR, 826 Sub 2 - Page 281 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R ZL-171-01-2 ZONE 171 172 DESCRIPTION AFT CABIN UNDERFLOOR COMPARTMENT SKILL TASK CODE CODE AF GVI GENERAL VISUAL INSPECTION OF AFT CABIN UNDERFLOOR COMPARTMENT (EWIS) ZL-171-02-1 171 172 ACCESS PANELS: 161DW, 171AL, 162DW, 172AR, 826 AFT CABIN UNDERFLOOR COMPARTMENT AF GVI GENERAL VISUAL INSPECTION OF AFT CABIN UNDERFLOOR COMPARTMENT (EWIS) REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 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. H. APPL 1 1 0.25 0.25 2930 2964 3044 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 1 1 0.20 0.20 ALL 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 GVI I: 6 YE OR 24000 FH MRB I: 6 YE MRB 195 196 PREPARATION: ESCAPE SLIDE STOWAGE CONTAINER REMOVED; HYDRAULIC COMPARTMENT AND FAIRINGS GENERAL VISUAL INSPECTION OF HYDRAULIC COMPARTMENT AND FAIRINGS (EWIS) 052190-200-009 SOURCE: MRB ZL-191-02-1 GENERAL VISUAL INSPECTION OF OFFWING ESCAPE SLIDE STOWAGE AREA (EWIS) ZL-195-01-1 052190-200-001 052190-200-003 SOURCE: MRB ZL-193-01-1 AF GVI I: 24 MO MRB 052190-200-005 SOURCE: MRB ZL-195-01-1 ACCESS PANELS: 195BB, 196BB Sub 2 - Page 282 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R ZL-197-01-1 ZONE 197 198 DESCRIPTION REAR FAIRING SKILL TASK CODE CODE AF GVI REV: 07 DATE: 29-Dec-2014 INTERVALS I: 6 YE SOURCE MRB GENERAL VISUAL INSPECTION OF REAR FAIRING (EWIS) ZL-197-01-3 197 198 ACCESS PANELS: 197AB, 197BB, 197GB, 198BB, 198GB, 826GR REAR FAIRING 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 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 052190-200-007 MEN TASKM. H. APPL 1 1 0.30 0.30 2930 2964 3044 1 1 0.30 0.30 1654 1679 1753 2465 2497 2879 2913 1 0.30 ALL 1 1 0.10 0.10 ALL 1 1 0.20 0.20 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 REFERENCES SOURCE: MRB ZL-197-01-1 GENERAL VISUAL INSPECTION OF REAR FAIRING (EWIS) ZL-200-02-1 TPS SOURCE: MRB ZL-211-01-1 AF GVI I: 12 YE MRB GENERAL VISUAL INSPECTION OF COCKPIT (EWIS) 052210-200-002 SOURCE: MRB ZL-211-02-1 PREPARATION: INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED INSPECTION; ZL-221-02-1 221 222 ACCESS PANELS: 211BC, 211FC, 211HC, 831, 212BC, 212FC, 212KW FORWARD CABIN UTILITY AREA GENERAL VISUAL INSPECTION OF FWD CABIN UTILITY AREAS INCLUDING FLOOR STRUCTURE (EWIS) AF GVI I: 12 YE MRB 052220-200-006 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 Sub 2 - Page 283 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER ZL-223-01-1 ZONE 223 224 DESCRIPTION FWD CABIN UTILITY AREA OVERHEAD COMPARTMENT SKILL TASK CODE CODE AF GVI REV: 07 DATE: 29-Dec-2014 INTERVALS I: 12 YE SOURCE MRB TPS REFERENCES 052220-200-003 MEN TASKM. H. APPL 1 1 0.15 0.15 ALL 1 1 0.35 0.35 ALL 1 1 0.30 0.30 ALL 1 1 0.25 0.25 ALL 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 AF GVI I: 12 YE MRB GENERAL VISUAL INSPECTION OF FWD PASSENGER COMPARTMENT (EWIS) (INCLUDING FLOOR STRUCTURE) 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 ; ZL-233-01-1 233 234 ACCESS PANELS: 831, 841 FWD PASSENGER OVERHEAD COMPARTMENT AF GVI I: 12 YE MRB GENERAL VISUAL INSPECTION OF FWD PASSENGER OVERHEAD COMPARTMENT (EWIS) 052230-200-003 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 ; ZL-241-01-3 241 242 ACCESS PANELS: 831, 841 CENTER PASSENGER COMPARTMENT GENERAL VISUAL INSPECTION OF CENTER PASSENGER COMPARTMENT (EWIS) (INCLUDING FLOOR STRUCTURE) AF GVI I: 12 YE MRB 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 Sub 2 - Page 284 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER ZL-243-01-1 ZONE 243 244 DESCRIPTION CENTER PASSENGER OVERHEAD COMPARTMENT SKILL TASK CODE CODE AF GVI REV: 07 DATE: 29-Dec-2014 INTERVALS I: 12 YE SOURCE MRB GENERAL VISUAL INSPECTION OF CENTER PASSENGER OVERHEAD COMPARTMENT (EWIS) TPS REFERENCES 052240-200-003 MEN TASKM. H. APPL 1 1 0.25 0.25 ALL 1 1 0.35 0.35 ALL 1 1 0.40 0.40 ALL 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 ; ZL-251-01-3 251 252 ACCESS PANELS: 832, 842 AFT PASSENGER COMPARTMENT AF GVI I: 12 YE MRB GENERAL VISUAL INSPECTION OF AFT PASSENGER COMPARTMENT (EWIS) (INCLUDING FLOOR STRUCTURE) 052250-200-001 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 ; R ZL-253-50-1-SDM 253 254 ACCESS PANELS: 832, 842 LIVETV RADOME INSTL AREA-FRAME C52 TO C56 & STR 5L TO 5R AF GVI AF GVI EXTERNAL GENERAL VISUAL INSPECTION OF SKIN COVERED BY RADOME. R ZL-253-51-1-SDM 253 254 LIVETV RADOME INST AREA-FRAME C52 TO C56 & STR 5L TO 5R GENERAL VISUAL INSPECTION OF INTERNAL SUPPORT STRUCTURE FOR LIVETV INSTALLATION. T: 5 YE I: 5 YE T: 9 YE I: 8 YE S-ICA STC ST00788SE ICA BERG-151-701 JIC A320-53-41-00 1 1 TBD TBD 2465 2497 S-ICA STC ST00788SE ICA BERG-151-701 JIC A320-53-41-01 1 1 TBD TBD 2465 2497 Sub 2 - Page 285 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V R ZL-253-53-1-SDM ZONE 253 254 DESCRIPTION LIVETV WADL ANTENNA INSTL AREA-FRAME C60 TO C61 & STR P1 TO P´1 SKILL TASK CODE CODE R ZL-253-54-1-SDM ZL-261-02-1 253 254 261 262 INTERNAL GENERAL VISUAL INSPECTION OF STRINGERS AT LNA SUPPORT STRUCTURE FOR LIVETV INSTALLATION. AFT CABIN UTILITY AREAS INTERVALS SOURCE TPS REFERENCES MEN TASKM. H. APPL AF GVI T: 9 YE I: 8 YE S-ICA STC ST00788SE ICA BERG-151-701 JIC A320-53-41-02 1 1 TBD TBD 2465 2497 AF GVI T: 9 YE I: 8 YE I: 12 YE S-ICA STC ST00788SE ICA BERG-151-701 JIC A320-53-41-03 1 1 TBD TBD 2465 2497 MRB 052260-200-004 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 INTERNAL GENERAL VISUAL INSPECTION OF SKIN ADGACENT TO ANTENNA SUPPORT DOUBLERS. PREPARATION: LINING AND INSULATION REMOVED; OVERHEAD STOWAGE COMPARTMENTS REMOVED; LIVETV LNA INST AREA-FRAME C59 TO C60 & STR P´4 TO P´5 REV: 07 DATE: 29-Dec-2014 AF GVI GENERAL VISUAL INSPECTION OF AFT CABIN UTILITY AREAS INCLUDING FLOOR STRUCTURE (EWIS) 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 ; ZL-300-02-1 ZL-311-01-1 300 311 312 ACCESS PANELS: 832, 842 STABILIZERS AND CONE/REAR FUSELAGE GENERAL VISUAL INSPECTION OF STABILIZERS AND CONE/REAR FUSELAGE AFT FUSELAGE TAIL SECTION GENERAL VISUAL INSPECTION OF AFT FUSELAGE TAIL SECTION (EWIS) 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 SOURCE: MRB ZL-311-01-1 ACCESS PANELS: 312AR, 314AR Sub 2 - Page 286 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER ZL-313-01-1 ZONE 313 314 DESCRIPTION TAIL CONE APU AIR INTAKE AREA SKILL TASK CODE CODE AF GVI REV: 07 DATE: 29-Dec-2014 INTERVALS I: 24 MO SOURCE MRB GENERAL VISUAL INSPECTION OF TAIL CONE APU AIR INTAKE AREA (EWIS) ZL-315-01-1 315 316 ACCESS PANELS: 314AR TAIL CONE APU AND ACCESSORY COMPARTMENT R ZL-315-01-2 315 316 AF GVI I: 24 MO MRB 315 316 ACCESS PANELS: 315AL, 316AR TAIL CONE APU AND ACCESSORY COMPARTMENT AF GVI I: 24 MO MRB 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 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER LEADING EDGE (EWIS) 1 1 0.05 0.05 ALL 052310-200-003 1 1 0.10 0.10 1654 1679 1753 2465 2497 2879 2913 052310-200-003 1 1 0.10 0.10 2930 2964 3044 052310-200-003 1 1 0.10 0.10 052310-200-004 1 0.10 ALL 1 0.10 ALL 1 0.30 ALL SOURCE: MRB ZL-317-01-1 AF GVI I: 12 YE MRB GENERAL VISUAL INSPECTION OF DORSAL FIN (EWIS) ZL-322-01-1 APPL SOURCE: MRB ZL-315-01-3 GENERAL VISUAL INSPECTION OF TAIL CONE APU EXHAUST AREA (EWIS) ZL-321-01-1 TASKM. H. SOURCE: MRB ZL-315-01-2 GENERAL VISUAL INSPECTION OF TAIL CONE APU AND ACCESSORY COMPARTMENT (EWIS) ZL-317-01-1 052310-200-002 MEN SOURCE: MRB ZL-315-01-1 GENERAL VISUAL INSPECTION OF TAIL CONE APU AND ACCESSORY COMPARTMENT (EWIS) D ZL-315-01-3 REFERENCES SOURCE: MRB ZL-313-01-1 GENERAL VISUAL INSPECTION OF TAIL CONE APU AND ACCESSORY COMPARTMENT (EWIS) ACCESS PANELS: 315AL, 316AR TAIL CONE APU AND ACCESSORY COMPARTMENT TPS 052320-200-001 SOURCE: MRB ZL-321-01-1 AF GVI I: 12 YE MRB 052320-200-002 SOURCE: MRB ZL-322-01-1 ACCESS PANELS: 322AL, 322BL, 322CL Sub 2 - Page 287 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER ZL-323-01-1 ZONE 323 DESCRIPTION VERTICAL STABILIZER SPAR BOX SKILL TASK CODE CODE AF GVI REV: 07 DATE: 29-Dec-2014 INTERVALS I: 12 YE SOURCE MRB GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER SPAR BOX (EWIS) TPS REFERENCES 052320-200-003 MEN TASKM. H. APPL 1 0.50 ALL 1 0.10 ALL 1 0.20 ALL 1 0.40 ALL 1 0.40 ALL 1 0.60 ALL 1 1 0.30 0.30 ALL 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 AF GVI I: 12 YE MRB GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER TIP (EWIS) ZL-325-01-1 325 ACCESS PANELS: 324AT VERTICAL STABILIZER TRAILING EDGE SOURCE: MRB ZL-324-01-1 AF GVI I: 24 MO 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 052320-200-007 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 052320-200-005 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 052320-200-004 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 GENERAL VISUAL INSPECTION OF TRIMMABLE HORIZONTAL STABILIZER LEADING EDGE (EWIS) AF GVI I: 6 YE MRB 052330-200-001 SOURCE: MRB ZL-331-01-1 ACCESS PANELS: 331AB, 331BB, 331CB, 341AB, 341BB, 341CB Sub 2 - Page 288 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER ZL-332-01-1 ZONE 332 342 DESCRIPTION THS TIP SKILL TASK CODE CODE AF GVI REV: 07 DATE: 29-Dec-2014 INTERVALS I: 12 YE SOURCE MRB GENERAL VISUAL INSPECTION OF TRIMMABLE HORIZONTAL STABILIZER TIP (EWIS) ZL-333-01-1 333 343 ACCESS PANELS: 332AB, 342AB THS SPAR BOX TPS REFERENCES 052330-200-002 MEN TASKM. H. APPL 1 1 0.10 0.10 ALL 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 SOURCE: MRB ZL-332-01-1 AF GVI I: 12 YE MRB GENERAL VISUAL INSPECTION OF TRIMMABLE HORIZONTAL STABILIZER SPAR BOX (EWIS) 052330-200-003 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 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 SOURCE: MRB ZL-334-02-1 AF GVI I: 6 YE MRB GENERAL VISUAL INSPECTION OF ELEVATOR (EWIS) ZL-400-02-1 400 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 052330-200-007 052330-200-005 SOURCE: MRB ZL-335-01-1 EN GVI I: 4 MO MRB 052400-200-002 SOURCE: MRB ZL-400-02-1 Sub 2 - Page 289 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER ZL-411-01-1 ZL-415-01-1 ZONE 411 413 414 421 423 424 415 425 DESCRIPTION UPPER FORWARD PYLON SKILL TASK CODE CODE EN GVI REV: 07 DATE: 29-Dec-2014 INTERVALS I: 20 MO SOURCE MRB GENERAL VISUAL INSPECTION OF UPPER FWD PYLON (EWIS) TPS REFERENCES 052410-200-001 SOURCE: MRB ZL-411-01-1 ACCESS PANELS: 413AL, 413BL, 413CL, 413DL, 413EL, 414AR, 414AZ, 414BR, 414CR, 414FR, 423AL, 423AZ, 423BL, 423CL, 423DL, 423FL, 424AR, 424BR, 424CR, 424ER LOWER PYLON EN GVI I: 20 MO MRB GENERAL VISUAL INSPECTION OF LOWER PYLON (EWIS) 052410-200-002 MEN TASKM. H. APPL 1 1 1 1 1 1 0.03 0.03 0.03 0.03 0.03 0.03 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 0.10 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 0.03 0.03 0.03 0.03 0.03 0.03 0.03 0.03 0.03 0.03 0.03 0.03 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-471-01-1 471 472 473 475 476 477 481 482 483 485 486 487 ACCESS PANELS: 451AL, 452AR, 461AL, 462AR PYLON LEADING EDGE AND LOWER FAIRING GENERAL VISUAL INSPECTION OF PYLON LEADING EDGE AND LOWER FAIRING (EWIS) 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 EN GVI I: 24 MO MRB 052470-200-001 SIL 54-023 SOURCE: MRB ZL-471-01-1 Sub 2 - Page 290 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER ZL-500-02-1 ZONE 500 600 DESCRIPTION WING LOWER SURFACE SKILL TASK CODE CODE AF GVI REV: 07 DATE: 29-Dec-2014 INTERVALS I: 8 DY SOURCE MRB GENERAL VISUAL INSPECTION OF WING LOWER SURFACE INCLUDING UPPER AND LOWER SURFACES OF SLATS AND FLAPS (EWIS) ZL-500-03-1 500 600 PREPARATION: FLAPS EXTENDED; SLATS FULLY EXTENDED; WING UPPER SURFACE ZL-521-01-1 521 621 REFERENCES 052500-200-002 MEN TASKM. H. APPL 1 1 0.30 0.30 ALL 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 SOURCE: MRB ZL-500-02-1 AF GVI I: 48 MO MRB GENERAL VISUAL INSPECTION OF WING UPPER SURFACE INCLUDING SLATS, FLAPS AND SPOILERS (EWIS) PREPARATION: FLAPS EXTENDED; SPOILERS EXTENDED; SLATS FULLY EXTENDED; INBOARD FIXED LEADING EDGE STRUCTURE TPS 052500-200-003 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 GENERAL VISUAL INSPECTION OF FLAP TRACK NO 2 AND FAIRING (EWIS) AF GVI I: 24 MO MRB 052530-200-001 SOURCE: MRB ZL-531-01-1 PREPARATION: FLAPS EXTENDED; ACCESS PANELS: 531AT, 631AT Sub 2 - Page 291 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER ZL-531-02-1 ZONE 531 631 DESCRIPTION FLAP TRACK NO 2 AND FAIRING SKILL TASK CODE CODE AF GVI REV: 07 DATE: 29-Dec-2014 INTERVALS I: 6 YE SOURCE MRB GENERAL VISUAL INSPECTION OF FLAP TRACK NO 2 AND FAIRING (EWIS) TPS REFERENCES 052530-200-005 MEN TASKM. H. APPL 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 1 1 0.30 0.30 ALL SOURCE: MRB ZL-531-02-1 PREPARATION: FLAPS EXTENDED; ZL-532-01-1 532 632 ACCESS PANELS: 531AB, 531AL, 531AR, 531AT, 531BB, 531CB, 531DB, 631AB, 631AL, 631AR, 631AT, 631BB, 631CB, 631DB FLAP TRACK NO 3 AND FAIRING AF GVI I: 24 MO MRB GENERAL VISUAL INSPECTION OF FLAP TRACK NO 3 AND FAIRING (EWIS) 052530-200-002 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 GENERAL VISUAL INSPECTION OF FLAP TRACK NO 4 AND FAIRING (EWIS) AF GVI I: 6 YE MRB 052530-200-007 SOURCE: MRB ZL-533-02-1 PREPARATION: FLAPS EXTENDED; ACCESS PANELS: 533AB, 533AL, 533AR, 533AT, 533BB, 533CB, 533DB, 633AB, 633AL, 633AR, 633AT, 633BB, 633CB, 633DB Sub 2 - Page 292 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER ZL-534-01-2 ZONE 534 634 DESCRIPTION WING TIP SKILL TASK CODE CODE AF GVI REV: 07 DATE: 29-Dec-2014 INTERVALS I: 72 MO SOURCE MRB GENERAL VISUAL INSPECTION OF WING TIP (EWIS) ZL-540-01-1 540 640 ACCESS PANELS: 534AB, 534AL, 534BL, 634AB, 634AL, 634BL WING FUEL TANK TPS REFERENCES 052530-200-004 MEN TASKM. H. APPL 1 1 0.10 0.10 ALL 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 0.10 0.10 ALL SOURCE: MRB ZL-534-01-2 AF GVI GENERAL VISUAL INSPECTION OF WING FUEL TANK (EWIS) I: 6 YE NOTE MRB I: 12 YE MRB 052540-200-005 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-571-01-1-SDM 571 671 ACCESS PANELS: 560AB, 660AB MAIN LANDING GEAR BAY 052560-200-001 SOURCE: MRB ZL-560-01-1 AF GVI I: 8 DY SPECI 052570-200-001 GENERAL VISUAL INSPECTION OF LH AND RH MAIN LANDING GEAR BAY FROM GROUND AS FAR AS VISIBLE Sub 2 - Page 293 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R E V TASK NUMBER ZL-571-02-1 ZONE 571 671 DESCRIPTION MAIN LANDING GEAR BAY SKILL TASK CODE CODE AF GVI REV: 07 DATE: 29-Dec-2014 INTERVALS I: 48 MO SOURCE 572 672 SHROUD BOX AF GVI I: 48 MO REFERENCES MRB 052570-200-006 MRB SOURCE: MRB ZL-571-02-1 052570-200-002 GENERAL VISUAL INSPECTION OF MLG BAY (EWIS) D ZL-572-01-1 TPS GENERAL VISUAL INSPECTION OF SHROUD BOX (EWIS) MEN TASKM. H. APPL 1 1 0.20 0.20 ALL 1 1 0.10 0.10 1 1 0.10 0.10 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1 1 0.10 0.10 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; ZL-573-01-1 573 673 ACCESS PANELS: 571AB, 671AB 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 294 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 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 295 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 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 2930 2964 3044 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; R 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 296 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 REV: 07 DATE: 29-Dec-2014 INTERVALS I: 4 MO SOURCE MRB GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT DOOR INCLUDING FUSELAGE DOOR SILL, DOOR SEAL AND LOCK FITTINGS (EWIS) R ZL-826-02-1 826 ACCESS PANELS: 826 AFT CARGO COMPARTMENT DOOR TPS REFERENCES 052820-200-002 MEN TASKM. H. 1 0.10 1654 1679 1753 2465 2497 2879 2913 1 0.30 2930 2964 3044 1 0.30 1654 1679 1753 2465 2497 2879 2913 1 0.20 2930 2964 3044 1 0.20 2930 2964 3044 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 APPL 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; R 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) R 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 297 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II 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 REV: 07 DATE: 29-Dec-2014 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. H. APPL 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 2930 2964 3044 PREPARATION: INSULATION REMOVED; R ZL-833-01-1 N 251000-01-1-SDM N 252340-01-1-SDM N 252341-01-1-SDM N 252343-01-1-SDM N 252400-01-1-SDM N 252600-01-1-SDM 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) 052830-200-003 SOURCE: MRB ZL-833-01-1 200 ACCESS PANELS: 833, 834, 843, 844 COCKPIT CA GVI I: 400 FH SPECI 1 TBD ALL 200 GENERAL VISUAL INSPECTION OF THE COCKPIT INCLUDING SEATS, SEAT COVERS, CEILING, SIDEWALL PANELS AND FLOOR MATERIAL FOR CONDITION CLEANLINESS AND SECURITY OF INSTALLATION 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 200 GENERAL VISUAL INSPECTION OF PASSENGER COMPARTMENT CEILING PANELS FOR CONDITION AND SECURITY OF INSTALLATION 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 200 GENERAL VISUAL INSPECTION OF PASSENGER COMPARTMENT OVERHEAD STOWAGE BINS FROM INSIDE AND OUTSIED FOR CONDITION AND PROPER OPERATION PASSENGER COMPARTMENT CURTAINS CA DET I: 400 FH SPECI 1 TBD ALL DETAILED INSPECTION OF PASSENGER COMPARTMENT CURTAINS FOR CONDITION AND LABEL PRESENCE. REPLACE CURTAIN IN CASE LABEL ABSENCE OR WASHING REQUIRED Sub 2 - Page 298 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V N 252841-01-1-SDM N 253100-01-1-SDM N 253300-01-1-SDM N 252100-01-1-SDM ZONE DESCRIPTION SKILL TASK CODE CODE REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE TPS REFERENCES MEN TASKM. H. APPL 200 PASSENGER COMPARTMENT TEXTILE FLOOR CARPET CA GVI I: 400 FH SPECI 1 TBD ALL 200 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 FORWARD GALLEY CA 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 PASSENGER SEATS CA GVI I: 8 DY 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 N 252100-02-1-SDM N 252100-03-1-SDM N 252100-04-1-SDM 200 PASSENGER SEATS CA DET I: 7500 FH SPECI 1 TBD ALL 200 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 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 DETAILED INSPECTION OF FOOD TRAYS IN SEAT BACKS AND IAT FOR CRACKS AND DELAMINATION Sub 2 - Page 299 of 300 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: II SCHEDULED MAINTENANCE PROGRAM R TASK E NUMBER V N 252142-01-1-SDM N 353000-07-1-SDM ZONE DESCRIPTION SKILL TASK CODE CODE REV: 07 DATE: 29-Dec-2014 INTERVALS SOURCE 200 PASSENGER SEAT BELTS CA DET I: 750 FH SPECI 200 DETAILED INSPECTION OF PASSENGER SEAT BELTS FOR: CUT OR WORN EDGES, DAMAGED STITCHING, BROKEN FABRIC THREADS, EXCESSIVE CHAFE MARKS, EXCESSIVE WEAR/FUSING PORTABLE OXYGEN MASKS CA DET I: 4 MO SPECI TPS REFERENCES JIC A320-35-30-01 MEN TASKM. H. 1 TBD 1 0.20 APPL ALL ALL 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 300 of 300 SDM A319/A320 MAINTENANCE PROGRAM TIME CONTROLLED ITEMS III. MP-REF: SDM.A320.IRISH SECTION: III REV: 07 DATE: 29-Dec-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.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: III TIME CONTROLLED ITEMS R TASK E NUMBER V R 212652-01-1 ZONE 127 DESCRIPTION AVIONICS VENT SKIN AIR INLET VALVE (SAIV) REV: 07 DATE: 29-Dec-2014 SKILL TASK CODE CODE INTERVALS SOURCE TPS REFERENCES MEN TASKM. APPLICABI H. LITY AF RST I: 18000 FH OR 120 MO SIL LUR 212652-000-802 SIL 21-159 1 1.32 AF RST I: 7500 FH OR 24 MO NOTE MRB 6 LUR 212653-000-001 SIL 21-099 1 1.27 REMOVE SKIN AIR INLET VALVE FOR OVERHAUL ALL ACCESS PANELS: 824 D 212653-01-1 126 AVIONICS VENT SKIN AIR OUTLET VALVE (SAOV) 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 R 212653-02-1 126 SOURCE: MRB 21.26.00/23 AF RST I: 18000 FH OR 120 MO SIL LUR 212653-000-803 SIL 21-159 1 1.27 ALL AF FNC I: 24000 FH OR 80 MO CMR** MRB 6,9 213100-720-001 2 0.83 ALL I: 50000 FH OR 210 MO MRB 9 1 0.65 ALL AVIONICS VENT SKIN AIR OUTLET VALVE (SAOV) REMOVE SKIN AIR OUTLET VALVE FOR OVERHAUL 213100-05-1 210 PRESSURE CONTROL AND MONITORING 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; ACCESS PANELS: 312AR 213100-08-1 260 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 20 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: III TIME CONTROLLED ITEMS R TASK E NUMBER V R 215141-01-1 ZONE 130 DESCRIPTION AIR COOLING AND TEMPERATURE CONTROL REV: 07 DATE: 29-Dec-2014 SKILL TASK CODE CODE AF FNC REMOVE OZONE CONVERTER FOR FUNCTIONAL CHECK NOTE: DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED. 215200-01-1 191 192 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. 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 1654 1679 2465 2497 2930 2964 3044 2879 2913 2 2 1.00 1.00 ALL 215200-100-002 SIL 21-067 2 2 0.42 0.42 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 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 SOURCE: MRB 21.50.00/10 215200-100-001 SIL 21-067 SOURCE: MRB 21.50.00/12 ACCESS PANELS: 191KB, 192KB D 215200-02-1 191 192 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 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 AF DET 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 ALL ALL SOURCE: MRB 21.50.00/19 PREPARATION: REMOVE HEAT EXCHANGER; ACCESS PANELS: 191KB, 192KB Sub 2 - Page 2 of 20 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: III TIME CONTROLLED ITEMS R TASK E NUMBER V R 237135-01-1 ZONE DESCRIPTION 312 REV: 07 DATE: 29-Dec-2014 SKILL TASK CODE CODE RA DIS COCKPIT VOICE RECORDER INTERVALS I: 6 YE SOURCE MRB 9 DISCARD ULB BATTERY NOTE: CVR P/N 93A100-80, VENDOR: FAIRCHILD CVR P/N AP71232101, VENDOR: TEAM VENDOR DUKANE ULB: P/N ELP-362D, VENDOR BENTHOS CVR P/N 980-6022-001, VENDOR: HONEYWELL ULB: P/N DK120, VENDOR DUKANE TPS REFERENCES 237135-920-001 CMM 23-70-01 CMM 23-70-10 CMM 23-70-44 MEN TASKM. APPLICABI H. LITY 1 0.10 ALL 2 2 0.20 0.20 ALL 1 1 0.20 0.20 ALL 1 0.15 ALL SOURCE: MRB 23.71.00/03 ACCESS PANELS: 312AR 242100-04-1 438 448 INTEGRATED DRIVE GENERATOR AF OPC I: NOTE MRB 9 242100-710-040 SOURCE: MRB 24.20.00/11 OPERATIONAL CHECK OF INTEGRATED DRIVE GENERATOR (IDG) DISCONNECT AND RECONNECT FUNCTION. NOTE: TASK TO BE PERFORMED AT OPPORTUNITY OF ENGINE CHANGE OR IDG CHANGE. 242100-05-1 437 447 INTEGRATED DRIVE GENERATOR EN RST I: NOTE MRB 6 731160-100-040 SOURCE: MRB 24.20.00/12 CLEAN INTEGRATED DRIVE GENERATOR (IDG) OIL COOLER. NOTE: TASK TO BE PERFORMED AT OPPORTUNITY OF ENGINE SHOP VISIT. 243851-01-1 126 DC GENERATION EL RST I: 1 YE MRB 6 243851-280-001 CMM 24-38-51 REMOVE BATTERY FOR OVERHAUL NOTE: P/N 2758, VENDOR: SAFT SOURCE: MRB 24.30.00/05 ACCESS PANELS: 822 Sub 2 - Page 3 of 20 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: III TIME CONTROLLED ITEMS R E V TASK NUMBER 243851-02-1 ZONE 126 DESCRIPTION DC GENERATION REV: 07 DATE: 29-Dec-2014 SKILL TASK CODE CODE EL RST REMOVE BATTERY FOR CHECK IN WORKSHOP INTERVALS I: 6 MO NOTE SOURCE MRB 6 TPS REFERENCES 243851-280-802 CMM 24-38-51 MEN TASKM. APPLICABI H. LITY 1 0.15 ALL 2 2 2 2 0.30 0.30 0.30 0.30 ALL 2 2 2 2 0.30 0.30 0.30 0.30 ALL SOURCE: MRB 24.30.00/12 NOTE: VENDOR: SAFT P/N: 2758 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 ACCESS PANELS: 822 R 256241-02-1 831 832 841 842 AF FNC I: 3 YE MRB 6,8 256200-750-001 CMM 25-60-56 CMM 25-61-20 SOURCE: MRB 25.62.00/02 DOOR ESCAPE SLIDE REMOVE DOOR ESCAPE SLIDE/RAFT FOR HYDROSTATIC TEST OF INFLATION RESERVOIR ESCAPE SLIDES PN D31516-113, D31517-113, D31516-417, D31517-417, PN D30664-309, D30665-309, VENDOR : AIR CRUISERS COMPANY NOTE: - TASK TO BE PERFORMED WITH 256241-03-1 - TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW DOORS / EMERGENCY EXITS. 256241-03-1 831 832 841 842 DOOR ESCAPE SLIDE REMOVE DOOR ESCAPE SLIDE/RAFT FOR RESTORATION NOTE: - TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW DOORS / EMERGENCY EXITS. - AFTER 15 YEARS OF AGE, PERFORM RESTORATION EVERY 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 AF RST I: 3 YE MRB 8 256244-920-001 CMM 25-60-56 CMM 25-61-20 SOURCE: MRB 25.62.00/03 Sub 2 - Page 4 of 20 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: III TIME CONTROLLED ITEMS R E V TASK NUMBER 256241-04-1 ZONE 831 832 841 842 DESCRIPTION DOOR ESCAPE SLIDE REV: 07 DATE: 29-Dec-2014 SKILL TASK CODE CODE CA OPERATIONAL CHECK OF FWD AND AFT PAX/CREW DOOR ESCAPE SLIDE/RAFT DEPLOYMENT. INTERVALS OPC I: 3 YE NOTE SOURCE MRB 8 151 152 OFFWING ESCAPE SLIDE REFERENCES 256200-710-001 CMM 25-60-56 CMM 25-61-20 MEN TASKM. APPLICABI H. LITY 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 SOURCE: MRB 25.62.00/04 NOTE: - TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW DOORS. - ALTERNATE DOOR POSITION AT NEXT INTERVAL RECOMMENDED. - AFTER 15 YEARS OF AGE, PERFORM RESTORATION EVERY 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 MUSTBE PERFORMED, 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 R 256242-01-1 TPS AF FNC I: 3 YE MRB 6,8 REMOVE OFFWING ESCAPE SLIDE INFLATION RESERVOIR FOR HYDROSTATIC TEST. 256200-750-002 CMM 25-60-58 SOURCE: MRB 25.62.00/02 OFFWING SLIDES P/N D31865-209, D31865-210, D31865-111, D31865-112 VENDOR : AIR CRUISERS NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED EMERGENCY EXITS. R 256242-02-1 191 192 ACCESS PANELS: 151CW, 152CW OFFWING ESCAPE SLIDE AF RST I: 3 YE MRB 8 256242-920-001 CMM 25-60-58 REMOVE OFFWING ESCAPE SLIDE FOR RESTORATION NOTE: TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW DOORS / EMERGENCY EXITS. SOURCE: MRB 25.62.00/03 P/N D31865-111 AND D31865-112 VENDOR: AIR CRUISERS ACCESS PANELS: 193AT, 194AT Sub 2 - Page 5 of 20 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: III TIME CONTROLLED ITEMS R E V TASK NUMBER 256242-03-1 ZONE 830 840 DESCRIPTION OFFWING ESCAPE SLIDE REV: 07 DATE: 29-Dec-2014 SKILL TASK CODE CODE CA OPERATIONAL CHECK OF OFF WING EMERGENCY EXIT ESCAPE SLIDE DEPLOYMENT INTERVALS OPC I: 3 YE NOTE SOURCE MRB 8 TPS REFERENCES 256200-710-002 CMM 25-60-58 MEN TASKM. APPLICABI H. LITY 1 1 0.10 0.10 ALL 1 0.20 ALL 1 0.10 ALL SOURCE: MRB 25.62.00/04 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 MUST BE PERFORMED, 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 R 256532-01-1 200 CA PORTABLE EMERGENCY BEACON TRANSMITTER FNC I: 5 YE MRB 9 REMOVE THE EMERGENCY LOCATOR TRANSMITTER FOR WORKSHOP TEST (BATTERY CHECK & FUNCTIONAL CHECK) 256500-720-001 CMM 25-60-09 CMM 25-60-10 SOURCE: MRB 25.65.32/01 NOTE: P/N 1151324-1MXXX, 607690-5, VENDOR: HONEYWELL 256535-01-1 200 ELT (REAR FUSELAGE) OPERATIONAL CHECK OF ELT SYSTEM BY MANUAL ACTIVATION EL OPC I: 24 MO MRB 8 256500-710-001 SOURCE: MRB 25.65.35/01 Sub 2 - Page 6 of 20 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: III TIME CONTROLLED ITEMS R TASK E NUMBER V R 256535-02-1 ZONE 200 DESCRIPTION ELT (REAR FUSELAGE) REV: 07 DATE: 29-Dec-2014 SKILL TASK CODE CODE EL RST REMOVE ELT FOR BATTERY REPLACEMENT AND OPERATIONAL CHECK OF ACCELERATION SENSOR INTERVALS I: 5 YE NOTE SOURCE MRB 8 P/N 01N65900: VENDOR: ELTA P/N S1819502-02 VENDOR: THALES AVIONICS P/N 1152682-1 VENDOR: HONEYWELL ASCA INC P/N S1821502-02 VENDOR: THALES AVIONICS TPS REFERENCES 256500-720-004 CMM 23-24-02 CMM 25-60-10 CMM 25-63-02 CMM 25-63-05 MEN TASKM. APPLICABI H. LITY 2 0.50 ALL 1 0.40 2930 2964 3044 SOURCE: MRB 25.65.35/02 NOTE: BATTERY LIFE FOR P/N 01N65900 IS 5 YE BATTERY LIFE FOR P/N S1819502-02, S1821502-02 IS 6 YE BATTERY LIFE FOR P/N 1152682-1 IS 10 YE R 256600-01-1 200 AF SUPPLEMENTAL LIFE RAFT RESTORATION OF LIFE RAFT NOTE: THE RECOMMENDED HYDROSTATIC TEST AND INSPECTION SCHEDULE IS EVERY 3 YEARS UP TO AND INCLUDING 15 YEARS. AFTER 15 YEARS OF AGE, TEST ANNUALLY. RST I: 3 YE NOTE MRB 8 256641-920-001 CMM 25-62-02 CMM 25-60-20 SOURCE: MRB 25.66.41/01 Sub 2 - Page 7 of 20 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: III TIME CONTROLLED ITEMS R TASK E NUMBER V R 256652-01-1 ZONE DESCRIPTION 200 REV: 07 DATE: 29-Dec-2014 SKILL TASK CODE CODE CA RST LIFE VESTS INTERVALS I: 2 YE NOTE SOURCE MRB 8 RESTORATION OF LIFE VESTS PN: 63600-101 & 63600-501, VENDOR: AIR CRUISERS PN: 63600-501 (CREW) VENDOR : AIR CRUISERS PN: P0640-101W (INFANT) VENDOR : EASTERN AERO MARINE PN: P0723E105PW (PASSENGER) VENDOR : EASTERN AERO MARINE PN : P0723E105PWC (CREW) VENDOR : EASTERN AERO MARINE PN S10002-1300 (INFANT), S41150-7400 (CREW), S51150-6300 (PASSENGER) VENDOR : SWITLIK PARACHUTE, INC. TPS REFERENCES 256652-920-001 CMM 25-60-12 CMM 25-60-15 CMM 25-61-07 CMM 25-64-02 OM 25-61-03 OM 25-61-07 OM 25-61-17 MEN TASKM. APPLICABI H. LITY 1 0.40 ALL 1 1 1 0.20 0.20 0.20 ALL 1 0.30 ALL SOURCE: MRB 25.66.52/01 NOTE: - PERFORM RESTORATION EVERY 5 YEARS FOR P/N S-10002-1300-119103, 63600-101 - PERFORM RESTORATION EVERY 2 YEARS FOR P/N P0640-101(NOT LATER THAN 3 YEARS AFTER DATE OF MANUFACTURE) - PERFORM RESTORATION EVERY 2 YEARS FOR P/N216203-0 - PERFORM RESTORATION EVERY 60 MO FOR P/NP0723E105PW& P0723E105PWC - RECTIFICATION IS MANDATORY AFTER 10 YEARS FORP/N63600-()-SERIES - PERFORM RESTORATION EVERY 5 YE FOR P/N S10002-1300 - PERFORM RESTORATION EVERY 5 YE FOR P/N S41150-7400 - PERFORM RESTORATION EVERY 2 YE FOR P/N S51150-6300 R 261600-05-1 130 150 160 CARGO COMPARTMENT SMOKE DETECTION AV RST REMOVE CARGO COMPARTMENT SMOKE DETECTORS FOR CLEANING I: 18000 FH OR 120 MO MRB 8 LUR I: 12000 FH OR 80 MO MRB 9 LUR 261615-100-001 SOURCE: MRB 26.16.00/05 ACCESS PANELS: 825, 826 261700-04-1 200 LAVATORY SMOKE DETECTION REMOVE SMOKE DETECTOR FOR CLEANING EL RST 261715-100-003 SOURCE: MRB 26.17.00/04 Sub 2 - Page 8 of 20 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: III TIME CONTROLLED ITEMS R TASK E NUMBER V R 262141-02-1 ZONE DESCRIPTION 415 425 REV: 07 DATE: 29-Dec-2014 SKILL TASK CODE CODE CA FNC ENGINE FIRE EXTINGUISHER BOTTLES INTERVALS I: 10 YE NOTE SOURCE MRB 6,9 HYDROSTATIC TEST OF BOTTLES INCLUDING CHECK SETTING OF PRESSURE SWITCH TPS REFERENCES 262141-280-002 CMM 26-20-04 CMM 26-20-79 SIL 96-2 MEN TASKM. APPLICABI H. LITY 1 1 0.20 0.20 ALL 1 1 0.25 0.25 ALL SOURCE: MRB 26.21.00/07 BOTTLE P/N 472088-1, VENDOR: KIDDE INC BOTTLE P/N 34100005-1, VENDOR: PACIFIC NOTE: FOR P/N 472088-1: EVERY 10 YEARS: FOR HERMETIC STAINLESS STEEL EXTINGUISHERS USING ONLY KA-APPROVED PARTS AND MANUFACTURED UNDER THE DOT EXEMPTIONS DOT-E-7026, DOT-E-8495 OR DOT-E-6071 EVERY 5 YEARS: FOR ALL OTHER KIDDIE EXTINGUISHERS (TITANIUM EXTINGUISHERS EXCLUDED) ALSO REFER TO SIL NO.26-0237D ACCESS PANELS: 415BL, 415BR, 425BL, 425BR R 262142-01-1 415 425 EL ENGINE FIRE EXTINGUISHER BOTTLE CARTRIDGES DISCARD CARTRIDGE DIS I: 10 YE MRB 9 262141-920-001 CMM 26-20-04 CMM 26-20-79 SOURCE: MRB 26.21.00/06 BOTTLE P/N 472088-1, VENDOR: KIDDE INC CARTRIDGE; P/N 446158, VENDOR: KIDDE BOTTLE P/N 34100005-1, VENDOR: PACIFIC CARTRIDGE P/N 30903886, VENDOR: PACIFIC ACCESS PANELS: 415BL, 415BR, 425BL, 425BR Sub 2 - Page 9 of 20 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: III TIME CONTROLLED ITEMS R TASK E NUMBER V R 262241-01-1 ZONE DESCRIPTION 313 REV: 07 DATE: 29-Dec-2014 SKILL TASK CODE CODE CA FNC APU FIRE EXTINGUISHER BOTTLE INTERVALS I: 10 YE NOTE SOURCE MRB 6,8 TPS REFERENCES 262241-280-002 CMM 26-20-03 MEN TASKM. APPLICABI H. LITY 1 0.40 ALL 1 0.50 ALL 1 0.40 1654 1679 1753 2465 1 0.40 2930 2964 3044 SOURCE: MRB 26.22.00/03 HYDROSTATIC TEST OF BOTTLE INCLUDING CHECK OF PRESSURE SWITCH SETTING BOTTLE P/N 33600005-3, VENDOR: PACIFIC SCIENTIFIC NOTE: REFER TO SIL NO.26-0237D ACCESS PANELS: 314AR R 262242-01-1 313 EL DIS I: 10 YE MRB 8 APU FIRE EXTIR BOTTLE CARTRIDGE 262242-920-001 CMM 26-20-03 SOURCE: MRB 26.22.00/04 DISCARD CARTRIDGE BOTTLE P/N 33600005-3, VENDOR: PACIFIC CARTRIDGE P/N 30903827, VENDOR: PACIFIC ACCESS PANELS: 314AR 262300-04-1 132 CARGO COMPARTMENT FIRE EXTINGUISHING AV DIS I: 10 YE MRB 8 REMOVE AND DISCARD CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE CARTRIDGES 262341-920-001 CMM 26-20-06 SOURCE: MRB 26.23.00/05 NOTE: BOTTLE P/N 34600017, VENDOR: PACIFIC CARTRIDGE P/N 30900000M, VENDOR: PACIFIC ACCESS PANELS: 132SW, 825 R 262300-04-3 132 CARGO COMPARTMENT FIRE EXTINGUISHING REMOVE AND DISCARD CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE CARTRIDGES AV DIS I: 10 YE MRB 8 262341-920-001 CMM 26-20-06 SOURCE: MRB 26.23.00/05 NOTE: BOTTLE P/N 34600017, VENDOR: PACIFIC ACCESS PANELS: 132MW, 825 Sub 2 - Page 10 of 20 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: III TIME CONTROLLED ITEMS R E V TASK NUMBER 262300-04-4 ZONE 162 DESCRIPTION CARGO COMPARTMENT FIRE EXTINGUISHING REV: 07 DATE: 29-Dec-2014 SKILL TASK CODE CODE AV DIS INTERVALS I: VR SOURCE MRB 8 REMOVE AND DISCARD CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE CARTRIDGES TPS REFERENCES 262341-920-001 MEN TASKM. APPLICABI H. LITY 1 0.40 2497 2879 2913 1 0.40 1654 1679 1753 2465 1 0.40 2930 2964 3044 1 0.40 1654 1679 1753 2465 SOURCE: MRB 26.23.00/05 ACCESS PANELS: 162AW, 826 262341-01-1 132 CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE CA FNC REMOVE CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE FOR WEIGHT CHECK I: 22500 FH OR 72 MO MRB 8 I: 22500 FH OR 72 MO MRB 8 I: 10 YE MRB 6,8 262341-280-001 CMM 26-20-06 SOURCE: MRB 26.23.00/01 NOTE: BOTTLE P/N 34600017, VENDOR: PACIFIC ACCESS PANELS: 132SW, 825 R 262341-01-2 132 CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE CA FNC REMOVE CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE FOR WEIGHT CHECK 262341-280-001 CMM 26-20-06 SOURCE: MRB 26.23.00/01 NOTE: BOTTLE P/N 34600017, VENDOR: PACIFIC ACCESS PANELS: 132MW, 825 262341-02-1 132 CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE REMOVE CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE FOR HYDROSTATIC TEST AND CHECK OF PRESSURE SWITCH SETTING CA FNC 262341-280-002 CMM 26-20-06 SOURCE: MRB 26.23.00/06 NOTE: BOTTLE P/N 34600017, VENDOR: PACIFIC ACCESS PANELS: 132SW, 825 Sub 2 - Page 11 of 20 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: III TIME CONTROLLED ITEMS R TASK E NUMBER V R 262341-02-2 ZONE 132 DESCRIPTION CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE REV: 07 DATE: 29-Dec-2014 SKILL TASK CODE CODE CA FNC INTERVALS I: 10 YE SOURCE MRB 6,8 TPS REFERENCES 262341-280-002 CMM 26-20-06 MEN TASKM. APPLICABI H. LITY 1 0.40 2930 2964 3044 1 0.40 2497 2879 2913 1 0.60 2497 2879 2913 1 0.20 ALL SOURCE: MRB 26.23.00/06 REMOVE CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE FOR HYDROSTATIC TEST AND CHECK OF PRESSURE SWITCH SETTING NOTE: BOTTLE P/N 34600017, VENDOR: PACIFIC ACCESS PANELS: 132MW, 825 262342-01-2 162 CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE CA FNC REMOVE CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE FOR WEIGHT CHECK 262342-02-2 162 ACCESS PANELS: 162AW, 826 CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE CA FNC REMOVE CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE FOR HYDROSTATIC TEST AND CHECK OF PRESSURE SWITCH SETTING I: 22500 FH OR 72 MO NR MRB 8 I: VR OR NR MRB 6,8 I: 10 YE NOTE MRB 9 SIL 262342-280-001 SOURCE: MRB 26.23.00/01 262342-280-002 SOURCE: MRB 26.23.00/06 ACCESS PANELS: 162AW, 826 R 262441-02-1 200 CA PORTABLE FIRE EXTINGUISHER HYDROSTATIC TEST OF BOTTLES NOTE: - FOR P/N 898052, 466040 AND 466090,HYDROSTATICTESTEVERY 12 YEARS - FOR P/N 74-00, 74-20, 9821657, BA51015, AND H1-10-AIR, HYDROSTATIC TEST EVERY 10 YEARS - FOR P/N 892480 HYDROSTATIC EVERY 5 YEARS FNC 262400-280-001 CMM 26-21-39 CMM 26-24-05 CMM 26-20-20 SIL KIDDE AEROSPACE 96-2 SOURCE: MRB 26.24.00/02 Sub 2 - Page 12 of 20 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: III TIME CONTROLLED ITEMS R TASK E NUMBER V R 262441-04-1 ZONE 200 DESCRIPTION PORTABLE FIRE EXTINGUISHER REV: 07 DATE: 29-Dec-2014 SKILL TASK CODE CODE CA FNC INTERVALS I: 1 YE SOURCE MRB 9 TPS REFERENCES 262400-280-002 CMM 26-20-20 MEN TASKM. APPLICABI H. LITY 1 0.10 2465 2497 2879 2913 1 0.20 1654 1679 1753 2465 2497 1 0.20 ALL 1 0.20 ALL 1 0.30 ALL 1 1 TBD TBD ALL WEIGHT CHECK OF PROPELLANT CARTRIDGE SOURCE: MRB 26.24.00/04 NOTE: P/N 892480, VENDOR: KIDDE AEROSPACE R 262441-05-1 200 ACCESS PANELS: 831 PORTABLE FIRE EXTINGUISHER CA DIS I: 10 YE MRB 9 DISCARD PORTABLE FIRE EXTINGUISHER 262400-280-001 CMM 26-20-01 CMM 26-20-30 P/N: BA51015 VENDOR: FIRE FIGHTING ENTERPRISES SOURCE: MRB 26.24.00/05 P/N: H1-10AIR VENDOR: MAIP R 262541-02-1 200 ACCESS PANELS: 831 LAVATORY FIRE EXTINGUISHER BOTTLE CA FNC I: 72 MO MRB 9 REMOVE LAVATORY FIRE EXTINGUISHER BOTTLE FOR WEIGHT CHECK 272100-04-1 325 NOTE: PN A825100-3, VENDOR: KIDDE PN BA21758, VENDOR: FIRE FIGHTING ENTERPRISE PN BA24320A1 VENDOR: FIRE FIGHTING ENTERPRISES LTD RUDDER MECHANICAL CONTROL 262500-200-003 CMM 26-25-04 CMM 26-25-12 CMM 26-25-36 SOURCE: MRB 26.25.00/02 AF REMOVE YAW DAMPER SPRING ROD FOR WORKSHOP CHECK OPC I: 24000 FH OR 156 MO MRB 9 LUR 272641-280-001 FNC MRB 8 275117-280-001 MRB 8 SOURCE: MRB 27.50.00/07 MRB 27.50.01/07 MRB 27.80.00/05 282100-720-802 SOURCE: MRB 27.21.00/04 ACCESS PANELS: 325BL 275117-01-1 212 AF FLAP/SLAT COMMAND SENSOR UNIT I: 40 MO REMOVE CSU FOR WORKSHOP CHECK OF FRICTION BRAKE 282100-10-1 540 640 MAIN FUEL PUMP SYSTEM REMOVE AIR RELEASE VALVE FOR FUNCTIONAL CHECK OF FLOAT AF FNC I: 144 MO SOURCE: MRB 28.21.00/10 ACCESS PANELS: 540CB, 640CB Sub 2 - Page 13 of 20 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: III TIME CONTROLLED ITEMS R TASK E NUMBER V D 292000-06-1 ZONE 190 DESCRIPTION AUXILIARY HYDRAULIC POWER REV: 07 DATE: 29-Dec-2014 SKILL TASK CODE CODE AF FNC REMOVE RAM AIR TURBINE AGCM AND PUMP FOR FUNCTIONAL CHECK (BENCH TEST) INTERVALS SOURCE I: 24000 FH OR 144 MO CMR** MRB 8 195 AUXILIARY HYDRAULIC POWER AF RST T: 20 YE I: 20 YE ASM REMOVE RAT AND ACTUATOR FOR OVERHAUL AND REPLACE WITH NEW OR RECONDITIONED UNITS. T: 20 YE I: 20 YE ASM I: 6 YE NOTE MRB 9 REFERENCES 292200-920-002 ISB 29-1077 MEN TASKM. APPLICABI H. LITY 1 3.00 0 N/A 0 N/A 1 0.25 SOURCE: CMR 291000-00005-1-C MRB 29.10.00/26 ACCESS PANELS: 195BB, 195CB, 197EB, 197FB 292000-11-1 TPS 292200-960-001 SOURCE: ASM 292200-00001-1-E 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 PREPARATION: RAT; RAT ACTUATOR; ACCESS PANELS: 147BB, 147CB, 195BB, 734 D 292000-12-1 195 AF RST AUXILIARY HYDRAULIC POWER REMOVE RAT (INCLUDING TURBINE, LEG AND PUMP), EJECTION JACK AND AGCM FOR OVERHAUL AND REPLACE WITH NEW OR RECONDITIONED UNITS. 292200-960-002 SOURCE: ASM 292200-00002-1-E PREPARATION: AGCM; RAT; RAT JACK; ACCESS PANELS: 147BB, 147CB, 195BB, 734 313300-01-1 312 DFDR SYSTEM INTERCONNECTION DISCARD UNDERWATER LOCATOR BEACON BATTERY IF P/N N15F210B INSTALLED, A 2 YEARS INTERVAL CAN APPLY AV DIS 313355-920-001 CMM 31-31-36 CMM 31-30-40 ALL SOURCE: MRB 31.33.00/02 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 ACCESS PANELS: 312AR Sub 2 - Page 14 of 20 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: III TIME CONTROLLED ITEMS R E V TASK NUMBER 321111-01-2 ZONE DESCRIPTION 731 741 REV: 07 DATE: 29-Dec-2014 SKILL TASK CODE CODE AF SDI MAIN LANDING GEAR INTERVALS SOURCE 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 I: 10 YE OR 20000 FC ISB MRB CPCP VSB PREPARATION: AIRCRAFT JACKING; MAIN LANDING GEAR REMOVAL; ACCESS PANELS: 734, 744 710 NOSE LANDING GEAR AF SDI SPECIAL DETAILED INSPECTION (OVERHAUL) OF NOSE GEAR (OFF AIRCRAFT) PREPARATION: NLG REMOVED; AIRCRAFT JACKING; ACCESS PANELS: 713, 714, 734 323100-08-1 711 NORMAL EXTENSION AND RETRACTION AF SDI SPECIAL DETAILED INSPECTION (OVERHAUL) OF THE NOSE LANDING GEAR ACTUATING CYLINDER AND GEAR ATTACHMENT PIN (OFF AIRCRAFT). 731 741 ACCESS PANELS: 713, 714 NORMAL EXTENSION AND RETRACTION SOURCE: MRB 32.21.00/05 MRB 32.50.00/02 MRB 322105-03-1 MRB 322110-03-1 323122-920-001 ISB 32-1307 VSB 580-32-3160 APPENDIX 7 MEN TASKM. APPLICABI H. LITY 0 0 N/A N/A ALL 0 N/A ALL 0 N/A ALL 0 0 N/A N/A ALL 1 11.42 ALL SOURCE: MRB 322152-01-1 MRB 322158-01-1 PREPARATION: ACTUATING CYLINDER - NLG; 323100-09-1 REFERENCES I: 120 MO OR 20000 FC SPECIAL DETAILED INSPECTION (OVERHAUL) OF MAIN GEAR (OFF AIRCRAFT) 322111-01-1 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 I: 144 MO SIL 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 344211-920-001 SIL 34-097 RADIO ALTIMETER ANTENNAS AND COAXIAL CABLES REPLACEMENT. ACCESS PANELS: 151AG, 151UF, 152AG, 152GW, 152HW, 152MF, 152NF Sub 2 - Page 15 of 20 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: III TIME CONTROLLED ITEMS R TASK E NUMBER V R 351141-01-1 ZONE DESCRIPTION 125 REV: 07 DATE: 29-Dec-2014 SKILL TASK CODE CODE AF FNC INTERVALS I: 3 YE SOURCE MRB 5 CREW OXYGEN CYLINDER TPS REFERENCES 351141-750-002 CMM 35-21-93 CMM 35-11-41 MEN TASKM. APPLICABI H. LITY 1 0.20 ALL SOURCE: MRB 35.10.00/05 HYDROSTATIC TEST OF OXYGEN CYLINDER NOTE: PN 891511-14 VENDOR INTERTECHNIQUE SA ACCESS PANELS: 812 351241-02-1 210 CREW OXYGEN MASK REGULATORS AF FNC I: 6 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 1 0.30 ALL 1 0.20 ALL REMOVE FOR FUNCTIONAL CHECK OF MASK REGULATOR ASSEMBLY 352142-01-1 200 OXYGEN GENERATORS AF DIS I: 180 MO DISCARD OXYGEN GENERATORS R 353000-02-1 AF 200 FNC PORTABLE OXYGEN I: 5 YE MRB 9 REMOVE PORTABLE OXYGEN CYLINDER ASSEMBLY FOR HYDROSTATIC TEST (INCLUDING FUNCTIONAL CHECK OF OXYGEN REGULATOR AND LP RELIEF VALVE) SOURCE: MRB 35.20.00/03 353242-750-001 CMM 35-31-55 CMM 35-32-18 SOURCE: MRB 35.30.00/02 NOTE: P/N 5500-C1A-BF23A, VENDOR: SCOTT AVIATION P/N 9800-2D1A-F23AM, VENDOR : SCOTT AVIATION P/N 9700-C1A-BF23A, VENDOR : SCOTT AVIATION P/N 9700C1ABF23A, VENDOR: SCOTT AVIATION R 353000-06-1 200 AF PROTECT. BREATHING EQPT (CKPT & CABIN) DISCARD PROTECTIVE BREATHING EQUIPMENT NOTE: P/N 119003-01 & 119003, VENDOR: B/E AEROSPACE P/N : MR10049N VENDOR : ESSEX PB & R CORP P/N : 119003-11 VENDOR : B/E AEROSPACE INTERIOR SYSTEMS GROUP DIS I: 10 YE MRB 8 353000-920-001 CMM 35-10-25 CMM 35-32-17 SOURCE: MRB 35.30.00/05 Sub 2 - Page 16 of 20 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: III TIME CONTROLLED ITEMS R E V TASK NUMBER 492100-B5-1 ZONE 315 317 DESCRIPTION POWER SECTION REV: 07 DATE: 29-Dec-2014 SKILL TASK CODE CODE EN DIS INTERVALS I: NOTE SOURCE MRB 7 TPS REFERENCES 492100-920-007 MEN TASKM. APPLICABI H. LITY 0 0 N/A N/A 1654 1679 1753 2465 2497 2879 2913 0 0 N/A N/A ALL 0 0 N/A N/A ALL 0 0 N/A N/A ALL 1 1 0.60 0.60 ALL 0 0 N/A N/A ALL SOURCE: MRB 49.21.00/05-13 DISCARD LIFE LIMITED PARTS OF THE APU POWER SECTION IN ACCORDANCE WITH OEM RECOMMENDATION NOTE: REFER TO APPROVED ENGINE MANUAL FOR INTERVAL. PREPARATION: APU REMOVED; ACCESS PANELS: 315AL, 316AR, 317AL 722100-C1-1 430 440 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. PREPARATION: ENGINE REMOVED; 723000-C1-1 450 460 HP COMPRESSOR SECTION EN DIS I: NOTE MRB 5 723000-920-001 SOURCE: MRB 72.30.00/01-C5 DISCARD LIFE LIMITED HP COMPRESSOR ROTATING PARTS NOTE: REFER TO APPROVED ENGINE MANUAL FOR INTERVAL. PREPARATION: ENGINE REMOVED; 724000-C1-1 450 460 COMBUSTION SECTION EN SDI BORESCOPE INSPECTION OF COMBUSTION CHAMBER LINERS, DOME AREAS, HPT NOZZLE VANES AND SHROUDS (AS FAR AS VISIBLE THROUGH TWO OPPOSITE PORTS) I: 1600 FC OR 72 MO MRB 9 LUR I: NOTE MRB 5 724100-290-001 SOURCE: MRB 72.40.00/01-C5 ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR 725000-C2-1 450 460 TURBINE SECTION DISCARD LIFE LIMITED PARTS OF HPT AND LPT EN DIS 725000-920-001 SOURCE: MRB 72.50.00/02-C5 NOTE: REFER TO APPROVED ENGINE MANUAL FOR INTERVAL. PREPARATION: ENGINE REMOVED; Sub 2 - Page 17 of 20 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: III TIME CONTROLLED ITEMS R E V TASK NUMBER 725000-C6-1 ZONE 450 460 DESCRIPTION TURBINE SECTION REV: 07 DATE: 29-Dec-2014 SKILL TASK CODE CODE EN DET INTERVALS I: NOTE SOURCE MRB 6,9 SURVEILLANCE INSPECTION OF TURBINE FRAME AFT ENGINE MOUNT LUGS TPS REFERENCES 712212-210-001 MEN TASKM. APPLICABI H. LITY 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 2 5.00 ALL SOURCE: MRB 72.50.00/06-C5 NOTE: TASK TO BE PERFORMED AT OPPORTUNITY OF ENGINE SHOP VISIT. PREPARATION: ENGINE REMOVED; 730000-C4-1 435 445 ENGINE FUEL AND CONTROL EN DIS I: 4000 FH OR 36 MO NOTE MRB 6 SIL LUR OPC I: 7500 FH OR 50 MO GVI I: 7500 FH OR 50 MO MRB 9 LUR RST SPECI 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. 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. ACCESS PANELS: 437AL, 438AR, 447AL, 448AR 752000-C1-1 434 444 COOLING EN CHECK ECU AIR COOLING PIPE INLET/OUTLET FOR BLOCKAGE 752000-C3-1 452 462 COOLING EN GENERAL VISUAL INSPECTION OF PIPING OF LPT CASE AIR COOLING 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 752110-01-1-SDM 400 HIGH PRESSURE TURBINE CLEARANCE CONTROL VALVE (HPTCCV) REMOVE FOR RESTORATION HPTCCV AND REPLACE WITH THE OVERHAULED OR NEW ONE EN I: NOTE 752110-000-002 752110-400-002 752110-000-001 752110-400-001 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 Sub 2 - Page 18 of 20 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: III TIME CONTROLLED ITEMS R E V TASK NUMBER 753100-01-1-SDM-LH ZONE 430 450 DESCRIPTION VBV SYSTEM LUBRICATION REV: 07 DATE: 29-Dec-2014 SKILL TASK CODE CODE INTERVALS SOURCE TPS REFERENCES MEN TASKM. APPLICABI H. LITY 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 753120-000-002 753120-400-002 753120-000-001 753120-400-001 2 4.00 EN DET I: 3000 FH MRB 6 781112-210-041 1 1 0.42 0.42 1 1 0.30 0.30 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 LUBRICATE VBV SYSTEM OF THE ENGINE 753100-01-1-SDM-RH 440 460 PREPARATION: OPEN ENGINE COWLS VBV SYSTEM LUBRICATION LUBRICATE VBV SYSTEM OF THE ENGINE R 753120-01-1-SDM 400 PREPARATION: OPEN ENGINE COWLS BLEED VALVE STOP MECHANISM REMOVE FOR RESTORATION BLEED VALVE STOP MECHANISM AND REPLACE WITH THE OVERHAULED OR NEW ONE D 781112-C1-1 792000-C4-2 450 460 435 445 NOTE: PN 3282970-4 CENTERBODY DETAILED INSPECTION OF THE EXHAUST CENTERBODY IN ACCORDANCE WITH ROHR AOL CFM56-003. DISTRIBUTION EN DIS REMOVE AND DISCARD SUPPLY FILTER 792000-C7-1 435 445 ACCESS PANELS: 437AL, 447AL DISTRIBUTION EN DET CHECK OF FWD SUMP, AFT SUMP, AGB, AND TGB SCAVENGE SCREENS 792000-C8-1 435 445 ACCESS PANELS: 437AL, 447AL DISTRIBUTION EN DET CHECK MASTER MAGNETIC CHIP DETECTOR FOR PARTICLES I: 4000 FH OR 36 MO MRB 9 LUR I: 3000 FH OR 20 MO MRB 6 LUR I: 600 FH OR 6 MO MRB 6 LUR SOURCE: MRB 79.20.00/06-C5 435 445 DISTRIBUTION EN OPERATIONAL CHECK OF THE MASTER CHIP DETECTOR REMOTE INDICATION ZL-435-01-1 435 436 445 446 FAN AND ACCESSORY GEAR BOX GENERAL VISUAL INSPECTION OF FAN AND ACCESSORY GEAR BOX (EWIS) EN OPC I: 3000 FH OR 20 MO GVI I: 400 DY 790000-281-003 SOURCE: MRB 79.20.00/05-C5 ACCESS PANELS: 437AL, 447AL 792000-C9-1 SOURCE: MRB 78.11.00/04-C5 792110-920-002 MRB 9 LUR 790000-281-002 SOURCE: MRB 72.20.00/05-C5 MRB 79.20.00/07-C5 790000-200-001 SOURCE: MRB 79.20.00/08-C5 MRB 052430-200-002 SOURCE: MRB ZL-435-01-1 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 ALL 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 ALL ACCESS PANELS: 437AL, 438AR, 447AL, 448AR Sub 2 - Page 19 of 20 MP REF: SDM.A320.IRISH SDM A319/A320 MAINTENANCE PROGRAM SECTION: III TIME CONTROLLED ITEMS R E V TASK NUMBER ZL-453-01-1 ZONE 453 454 463 464 DESCRIPTION HOT SECTION REV: 07 DATE: 29-Dec-2014 SKILL TASK CODE CODE EN GVI INTERVALS I: 16 MO SOURCE MRB GENERAL VISUAL INSPECTION OF HOT SECTION (EWIS) TPS REFERENCES 052450-200-002 MEN TASKM. APPLICABI H. LITY SOURCE: MRB ZL-453-01-1 1 1 1 1 0.10 0.10 0.10 0.10 VSB CFM56-5 72-766 1 1 3.00 3.00 ALL ACCESS PANELS: 451AL, 452AR, 461AL, 462AR D 723200-C2-1 450 460 EN HIGH PRESSURE COMPRESSOR FRONT STATOR ASSEMBLY BORESCOPE INSPECTION FOR HPC STATOR-TO-ROTOR CONTACT SDI T: 24000 FH NOTE I: 600 FH NOTE VSB 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 20 of 20 SDM A319/A320 MAINTENANCE PROGRAM MOD CONTROLLED ITEMS MP-REF: SDM.A320.IRISH SECTION: IV REV: 07 DATE: 29-Dec-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.IRISH SECTION: IV REV: 07 DATE: 29-Dec-2014 SDM A319/A320 MAINTENANCE PROGRAM MOD CONTROLLED ITEMS R TASK E NUMBER V R 254000-03-1 ZONE 200 DESCRIPTION LAVATORIES SKILL TASK CODE CODE R 257100-02-1 273400-07-1 127 128 334 344 TPS REFERENCES MEN TASKM. APPLICABI H. LITY DET T: 2400 FH OR 15 MO I: 15 MO NOTE EASA AD FAA AD ISB 254000-220-001 EASA AD 2010-0148 FAA AD 2006-09-11 ISB 25-1365 1 2.00 1654 - 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 NDT SDI EASA AD ISB 257100-290-001 EASA AD 2012-0134 ISB 25A1555 1 1 1.75 1.75 BORESCOPE INSPECTION OF THE 80VU RACK LOWER LATERAL FITTINGS AND VISUAL INSPECTION OF THE UPPER FITTINGS AND CENTRAL SHELVE FITTINGS AVIONICS COMPARTMENT T: 20000 FC I: 500 FC 1654 1679 2497 2930 3044 2879 2913 NDT SDI EASA AD ISB 257100-290-002 EASA AD 2012-0134 ISB 25A1555 1 1 1.75 1.75 BORESCOPE INSPECTION OF THE 80VU RACK LOWER CENTRAL SUPPORT AND VISUAL INSPECTION OF THE UPPER FITTINGS AND CENTRAL SHELVE FITTINGS. ELEVATOR AND HYDRAULIC ACTUATION T: 20000 FC I: 500 FC 1654 1679 2497 3044 2879 2913 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 OPC T: 800 FC I: 425 FC AOT EASA AD FAA AD ISB 1 1 0.05 0.05 1753 2465 3044 2879 2913 T: NOTE I: NOTE EASA AD FAA AD ISB AOT 32A1390 EASA AD 2011-0069 FAA AD 2011-13-11 ISB 32-1390 533100-210-044 EASA AD 2011-0134 FAA AD 2004-13-06 ISB 53-1060 1 2.00 NOTE:- REFER TO ISB 25-1365 FIGURE 1 SHEET 1 FLOW CHART FOR FURTHER DETAILS 127 128 SOURCE AF DETAILED INSPECTION OF LAVATORY WALL R 257100-01-1 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 R 323105-02-1 730 740 ACCESS PANELS: 334DB, 344DB NORMAL EXTENSION AND RETRACTION OPERATIONAL CHECK OF THE MLG DOOR ACTUATOR D 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 NDT SDI NOTE: FOR THRESHOLD AND INTERVAL, REFER TO SB 53-1060 REV 02. ACCESS PANELS: 191KB, 192KB, 195BB, 196BB, 734, 744 Sub 2 - Page 1 of 4 MP REF: SDM.A320.IRISH SECTION: IV REV: 07 DATE: 29-Dec-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: 3000 FC NOTE I: 2250 FC 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 AF DET T: NOTE I: 500 FC EASA AD ISB EASA AD 2012-0032 ISB 57A1166 1 1 1.25 1.25 1654 1679 1753 AF DET T: NOTE I: 500 FC EASA AD ISB EASA AD 2012-0032 ISB 57-1168 1 1 1.25 1.25 2465 2497 2930 2964 3044 2879 2913 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 533154-04-1 147 148 PREPARATION: ACTUATOR REMOVED; 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 D 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; R 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 2 of 4 MP REF: SDM.A320.IRISH SECTION: IV REV: 07 DATE: 29-Dec-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: 10000 FC NOTE I: 5000 FC NOTE VSB VSB CFM56-5B 72-0727 1 1 1.00 1.00 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 EN SDI T: 24000 FH NOTE I: 600 FH NOTE VSB VSB CFM56-5B 72-553 1 1 3.00 3.00 1654 1679 1753 2497 EN SDI I: 1600 FC OR 72 MO NOTE MRB 6 VSB LUR 725200-290-001 VSB 72-0098 CFM 56-5B VSB 72-0240 CFM 56-5B 1 1 0.60 0.60 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 BORESCOPE INSPECTION OF HP COMPRESSOR STAGES 1, 3 AND 8 NOTE: TASK TO BE DONE ON ENGINES WITH GREATER THAN 10,000 CYCLES SINCE NEW OR SINCE LAST HPC BLADE PIECE-PART INSPECTION EXPOSURE PER CFM56-5B ENGINE SHOP MANUAL (ESM), 72-31-01, 72-31-02, AND 72-3103,BUT WITHIN THE NEXT 3,000 CYCLES, WITH A RECURRING INSPECTION AT 5,000 CYCLES INTERVALS WITH AN ADJUSTMENT OF PLUS OR MINUS 500 CYCLES. 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 USEDSERVICEABLE) 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 725000-C1-3 450 460 TURBINE SECTION BORESCOPE INSPECTION OF HPT BLADES (FROM THE FRONT AND THE REAR) 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 SOURCE: MRB 72.50.00/01-C5 ACCESS PANELS: 437AL, 438AR, 451AL, 452AR, 447AL, 448AR, 461AL, 462AR Sub 2 - Page 3 of 4 MP REF: SDM.A320.IRISH SECTION: IV REV: 07 DATE: 29-Dec-2014 SDM A319/A320 MAINTENANCE PROGRAM MOD CONTROLLED ITEMS R TASK E NUMBER V D 725100-C1-1 ZONE 450 460 DESCRIPTION HPT NOZZLE ASSEMBLY SKILL TASK CODE CODE INTERVALS SOURCE TPS REFERENCES MEN TASKM. APPLICABI H. LITY EN BSI I: NOTE VSB 725100-290-003 VSB CFM 72-170 1 1 1.00 1.00 EN SDI T: NOTE I: NOTE EASA AD FAA AD VSB 1 1 TBD TBD 1654 1679 1753 2465 2497 2930 2964 3044 2879 2913 T: 24000 FC OR 48000 FH I: 7500 FC OR 15000 FH ISB EASA AD 2007-0221 EASA AD 2009-0110 FAA AD 2009-18-01 VSB CFM 56-5B 72-0620 ISB 53-1258 1 15.00 ALL BORESCOPE INSPECTION OF HIGH PRESSURE TURBINE NOZZLE NOTE : - INITIAL AND SUBSEQUENT INSPECTIONS AS PER SB (CFM56-5) 72-170 725600-C3-1 450 460 TURBINE FRAME ASSEMBLY 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. 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 NDT SDI Sub 2 - Page 4 of 4 SDM A319/A320 MAINTENANCE PROGRAM INDIVIDUAL STRUCTURAL INSPECTIONS V. MP-REF: SDM.A320.IRISH SECTION: V REV: 07 DATE: 29-Dec-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. Sub 1 - Page 1 of 2 SDM A319/A320 MAINTENANCE PROGRAM INDIVIDUAL STRUCTURAL INSPECTIONS MP-REF: SDM.A320.IRISH SECTION: V REV: 07 DATE: 29-Dec-2014 6. LIMIT Workorder unique number and it’s limitation in FH/FC/Calendar Date. Document contains all necessary 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. Sub 1 - Page 2 of 2 SDM A319/A320 MAINTENANCE PROGRAM INDIVIDUAL STRUCTURAL INSPECTIONS R E V MSN ITEM REASON 1654 1 1654 9 Scratch on the fuselage skin at FR 1-2; 80mm from buttom center line Scratch at FR 8 below cokpit window LH 1654 10 Scratch on skin FR 12 LH 1654 11 Burn Mark Was Found on Rivet FR16 LH 1654 13 Dent on Skin FR21-23 LH 1654 14 Scratch on Skin FR22-23 LH 1654 15 Scratches on Skin FR23-24 LH (2 plases) 1654 16 Scratches on Skin FR25 LH (2 plases) 1654 20 Scratch on Skin FR67 LH Below L2 Door 1654 25 Dent on Skin FR20-21 LH 1654 28 Skratch on skin FR5 RH 1654 29 Nick on skin FR16 RH 1654 30 1654 FURTHER ACTION MP REF: SDM.A320.IRISH SECTION: V REV: 07 DATE: 02-Nov-2014 PERIODIC INSPECTION LIMIT IIR 53-11-11-1-002-00 First Inspection from Time of Rework Accomplishment 60000FC (WO 500465838) IIR 53-11-11-1-002-00 First Inspection from From A/C first flight 60000FC (WO 500465964) IIR 53-11-11-1-002-00 First Inspection from From A/C first flight 60000FC (WO 500465982) IIR 53-11-11-2-002-00 First Inspection after Repair Embodiment 48000FC (JIC 11856 Controlled) IIR 53-11-11-1-001-00 First Inspection from Time of dent occurrence 60000FC (WO 500466072) IIR 53-11-11-1-002-00 First Inspection from time of rework accomplishment 60000FC (WO 500466145) IIR 53-11-11-1-002-00 First Inspection from time of rework accomplishment 60000FC (WO 500466146) IIR 53-21-11-1-003-00 First Inspection from A/C first flight 48000FC (JIC 11859 Controlled) IIR 53-41-11-1-002-00 First Inspection from AC Delivery 60000FC (WO 500466648) IIR 53-11-11-1-001-00 First Inspection from Time of Dent Occurrence 60000FC (WO 500466658) IIR 53-11-11-1-002-00 First Inspection from A/C First Flight 60000FC (WO 500466663) IIR 53-11-11-1-002-00 First Inspection from A/C First Flight 60000FC (WO 500466667) N/A Scratces on skin FR22-23 RH (2 palces) IIR 53-11-11-1-002-00 First Inspection from time of rework accomplishment 60000FC (WO 500466672) N/A WO: 500466672 TAC: 77648 31 Scratces on skin FR25-26 RH IIR 53-21-11-1-002-00 First Inspection from A/C First Flight 60000FC (WO 500466678) N/A WO: 500466678 TAC: 60000 1654 34 Minor Damage around cutout frame lower side (10 places) IIR 53-41-11-1-006-00 First Inspection from A/C Delivery 60000FC / 75000FH (WO 500466711) N/A 1654 35 Blend out on skin FR59 RH N/A 1654 37 Old blend out on skin FR61 RH IIR 53-41-11-1-006-00 First Inspection from A/C Delivery 60000FC / 75000FH (WO 500466763) IIR 53-41-11-1-006-00 First Inspection from A/C Delivery 60000FC / 75000FH (WO 500468215) WO: 500466711 TAH: 75000 TAC: 60000 WO: 500466763 TAH: 75000 WO: 500468215 TAH: 75000 N/A N/A 11856 N/A N/A N/A 11859 N/A N/A N/A N/A N/A WO: 500465838 TAC: 77648 WO: 500465964 TAC: 60000 WO: 500465982 TAC: 60000 WO: 500465992 DATE: 2932167 WO: 500466072 TAC: 77648 WO: 500466145 TAC: 77648 WO: 500466146 TAC: 77648 WO: 500466493 DATE: 2932167 WO: 500466648 TAC: 60000 WO: 500466658 TAC: 77648 WO: 500466663 TAC: 60000 WO: 500466667 TAC: 60000 Sub 2 - Page 1 of 9 SDM A319/A320 MAINTENANCE PROGRAM INDIVIDUAL STRUCTURAL INSPECTIONS R E V MSN ITEM 1679 13 1679 29 1679 30 1679 31 1679 REASON FURTHER ACTION L/H MLG ACTUATOR ATTACHMENT BEARING FITTING MP REF: SDM.A320.IRISH SECTION: V REV: 07 DATE: 02-Nov-2014 PERIODIC INSPECTION LIMIT RDAS/70557421/003/2012/A REQUIREMENTS: LL AFTER REPAIR EMBODIMENT 42100FC (WO:500457752) R/H MLG ACTUATOR ATTACHMENT BEARING RDAS/70557421/004/2012/A REQUIREMENTS: LL FITTING AFTER REPAIR EMBODIMENT 34800FC DENT-FUS SKIN AT 38.1mm FWD FROM FR3 381mm IIR 53-11-11-1-004-00 - 60000 FC AFTER REPAIR LWR FROM S-27L EMBODIMENT WO:500456162 DENT-FUS SKIN AT 190.5 mm AFT FROM FR24 38.1 IIR 53-21-11-1-001-00 - 60000 FC AFTER REPAIR mm LWR FROM S-31L EMBODIMENT WO:500456353 N/A WO: 500457752 TAC: 59884 N/A WO: 500457820 TAC: 52584 WO: 500456162 TAC: 77784 WO: 500456353 TAC: 77784 32 DENT-FUS SKIN AT 127 mm AFT FROM FR24 50.8 mm LWR FROM S-33L IIR 53-21-11-1-001-00 - 60000 FC AFTER REPAIR EMBODIMENT WO:500456357 N/A WO: 500456357 TAC: 77784 1679 33 34 1679 52 1679 53 IIR 53-21-11-1-001-00 - 60000 FC AFTER REPAIR EMBODIMENT WO:500456358 IIR 53-41-11-1-007-00 - 60000FC or 105000 FH FIRST INSPECTION AFTER REPAIR EMBODIMENT IIR 53-21-11-1-003-00 - 60000 FC AFTER REPAIR EMBODIMENT WO:500456420 IIR 53-21-11-1-003-00 - 60000 FC AFTER REPAIR EMBODIMENT WO:500456436 N/A 1679 DENT-FUS SKIN AT 304.8 mm FWD FROM FR27 76.2 mm LWR FROM S-32L DENT-FUS SKIN AT 152.4 mm AFT FROM FR60 50.8 mm LWR FROM S-34L FUS SKIN AT 76.2 mm FWD FROM FR26,S6L FOUND INDICATION BLEND OUT. FUS SKIN AT 88.9 mm AFT FROM FR26,S5L FOUND INDICATION BLEND OUT. WO: 500456358 TAC: 77784 WO: 500457164 TAH: 135597 WO: 500456420 TAC: 77784 WO: 500456436 TAC: 77784 1679 54 55 IIR 53-21-11-1-003-00 - 60000 FC AFTER REPAIR EMBODIMENT WO:500456455 IIR 53-11-11-1-002-00 - 60000 FC AFTER REPAIR EMBODIMENT WO:500456487 N/A 1679 1679 56 FUS SKIN AT 12.7 mm AFT FROM FR24, 25.4 mm UPPER FROM BL0 FOUND INDICATION BLEND OUT. FUS SKIN AT 101.6 mm AFT FROM FR21, 76.2 mm UPPER FROM S18L FOUND INDICATION BLEND OUT. FUS SKIN AT 38.1 mm AFT FROM FR23, 101.6 mm LWR FROM S18L FOUND INDICATION BLEND OUT. IIR 53-11-11-1-002-00 - 60000 FC AFTER REPAIR EMBODIMENT WO:500456571 N/A WO: 500456571 TAC: 77784 1679 57 FUS SKIN AT 114.3 mm FWD FROM FR21, 76.2 mm LWR FROM S43L FOUND INDICATION BLEND OUT. IIR 53-11-11-1-002-00 - 60000 FC AFTER REPAIR EMBODIMENT WO:500456576 N/A WO: 500456576 TAC: 77784 1679 58 IIR 53-11-11-1-002-00 - 60000 FC AFTER REPAIR EMBODIMENT WO:500456581 N/A WO: 500456581 TAC: 77784 1679 59 L/H FWD FUS 63.5 MM AFT FROM FR2 NEAR CAPT WINDOWSHIELD FOUND INDICATION OF BLEND OUT. L/H FWD PAX DOOR ABOVE CABIN PRESSURE WINDOW FOUND INDICATION OF BLEND OUT. IIR 52-10-00-1-002-00 - 60000FC FIRST INSPECTION N/A AFTER REPAIR EMBODIMENT WO:500457128 WO: 500457128 TAC: 77784 N/A N/A N/A N/A N/A N/A WO: 500456455 TAC: 77784 WO: 500456487 TAC: 77784 Sub 2 - Page 2 of 9 SDM A319/A320 MAINTENANCE PROGRAM INDIVIDUAL STRUCTURAL INSPECTIONS R E V MSN ITEM REASON 1679 71 1679 81 1679 82 1679 83 DENT-FUS SKIN AT 50.8 MM AFT FROM FR17A 25.4 MM UPPER FROM S-35R FUS SKIN AT 38.1 MM AFT FROM FR23, 25.4 MM UPPER FROM S43R FOUND INDICATION OF BLEND OUT. FUS SKIN AT 152.4 MM AFT FORM FR21, 50.8 MM UPPER FROM S43R FOUND INDICATION OF BLEND OUT. FUS SKIN AT FR21, 12.7 MM LWR FROM S42R FOUND INDICATION OF BLEND OUT. 1679 84 1679 1679 1679 1679 1679 1679 1679 FUS SKIN AT 38.1 MM FWD FROM FR21, 76.2 MM UPPER FROM S43R FOUND INDICATION OF BLEND 85 FUS SKIN AT 38.1 MM AFT FROM FR64, 38.1 MM LWR FROM S18R FOUND INDICATION OF BLEND OUT. 87 FUS SKIN AT 76.2 MM AFT FROM FR10, 63.5 MM LWR FROM S19R FOUND INDICATION OF BLEND OUT. 88 FUS SKIN AT 45.72 MM FWD FROM FR69, 55.88 MM LWR FROM S18R FOUND INDICATION OF BLEND OUT. 89 FUS SKIN AT 63.5 MM AFT FROM FR69, 50.8 MM LWR FROM S17R FOUND INDICATION OF BLEND OUT. 90 FUS SKIN AT 50.8 MM AFT FROM FR69, 63.5 MM UPPER FROM S17R FOUND INDICATION OF BLEND OUT. 92 FUS SKIN AT 38.1 MM FWD FROM FR69,43.18 MM UPPER FROM S19R FOUND INDICATION OF BLEND OUT. 107 NICK-L/H PYLON SPIGOT FITTING SURFACE HOLE 1679 108 NICK-L/H PYLON SPIGOT FITTING SURFACE. FURTHER ACTION IIR 53-11-11-1-004-00 - 60000 FC AFTER REPAIR EMBODIMENT WO:500456260 IIR 53-11-11-1-002-00 - 60000 FC AFTER REPAIR EMBODIMENT WO:500456592 MP REF: SDM.A320.IRISH SECTION: V REV: 07 DATE: 02-Nov-2014 PERIODIC INSPECTION N/A N/A LIMIT WO: 500456260 TAC: 77784 WO: 500456592 TAC: 77784 IIR 53-11-11-1-002-00 - 60000 FC AFTER REPAIR EMBODIMENT WO:500456971 N/A WO: 500456971 TAC: 77784 IIR 53-11-11-1-002-00 - 60000 FC AFTER REPAIR EMBODIMENT WO:500456973 N/A WO: 500456973 TAC: 77784 IIR 53-11-11-1-002-00 - 60000 FC AFTER REPAIR N/A EMBODIMENT WO:500456974 IIR 53-41-11-1-005-00 - 60000 FC FIRST INSPECTION N/A FROM AIRCRAFT DELIVERY WO:500457077 WO: 500456974 TAC: 77784 WO: 500457077 TAC: 60000 IIR 53-11-11-1-002-00 - 60000 FC AFTER REPAIR EMBODIMENT WO:500456590 N/A WO: 500456590 TAC: 77784 IIR 53-41-11-1-005-00 - 60000 FC FIRST INSPECTION N/A FROM AIRCRAFT DELIVERY WO:500457121 WO: 500457121 TAC: 60000 IIR 53-41-11-1-005-00 - 60000 FC FIRST INSPECTION N/A FROM AIRCRAFT DELIVERY WO:500457123 WO: 500457123 TAC: 60000 IIR 53-41-11-1-005-00 - 60000 FC FIRST INSPECTION N/A FROM AIRCRAFT DELIVERY WO:500457126 WO: 500457126 TAC: 60000 IIR 53-41-11-1-005-00 - 60000 FC FIRST INSPECTION N/A FROM AIRCRAFT DELIVERY WO:500457127 WO: 500457127 TAC: 60000 IIR 54-51-18-1-001-00 - 21900FC FIRST INSPECTION N/A AFTER REPAIR EMBODIMENT WO: 500457502 WO: 500457502 TAC: 39684 IIR 54-51-18-1-002-00 - 18100FC FIRST INSPECTION N/A AFTER REPAIR EMBODIMENT WO:500457553 WO: 500457553 TAC: 35884 Sub 2 - Page 3 of 9 SDM A319/A320 MAINTENANCE PROGRAM INDIVIDUAL STRUCTURAL INSPECTIONS R E V MSN ITEM REASON FURTHER ACTION MP REF: SDM.A320.IRISH SECTION: V REV: 07 DATE: 02-Nov-2014 PERIODIC INSPECTION LIMIT 1679 117 DENT-R/H AFT SERVICE DOOR BETWEEN BEAM 1 AND BEAM2 FR67-FR68 OUTER SKIN SURFACE. IIR 52-10-00-1-001-00 - 60000FC FIRST INSPECTION N/A AFTER REPAIR EMBODIMENT WO:500457559 WO: 500457559 TAC: 77784 1679 119 DENT-R/H AFT SERVICE DOOR BETWEEN BEAM 1 AND BEAM2 FR66-FR67 OUTER SKIN SURFACE. IIR 52-10-00-1-001-00 - 60000FC FIRST INSPECTION N/A AFTER REPAIR EMBODIMENT WO:500457586 WO: 500457586 TAC: 77784 1753 1 FUSELAGE SKIN BLEND OUT. IIR 53-11-11-1-002-00, Due at 60,000 TAC (tracked by WO 500`457`124) N/A WO: 500457124 TAC: 60000 1753 2 FUSELAGE SKIN BLEND OUT. N/A 1753 4 FUSELAGE SKIN BLEND OUT. 1753 5 FUSELAGE SKIN BLEND OUT. 1753 6 FUSELAGE SKIN BLEND OUT. 1753 7 SMOOTH DENT. 1753 8 TWO REWORKS ON FUSELAGE SKIN. 1753 9 1753 10 FUSELAGE SKIN REWORK UNDER SCUFF PLATE, R1 DOOR. REWORK ON FUSELAGE SKIN. 1753 11 FUSELAGE SKIN BLEND OUT. 1753 12 BLEND OUT ON LOWER FUSELAGE SHELL. 1753 13 REWORK ON FUSELAGE SKIN. 1753 14 REWORK ON FUSELAGE SKIN. 1753 15 FIVE REWORKS ON FUSELAGE SKIN. 1753 16 THREE REWORKS ON FUSELAGE SKIN. IIR 53-21-11-1-003-00, Due at 77,506 TAC (tracked by WO 500`457`129) IIR 53-21-11-1-003-00, Due at 77,506 TAC (tracked by WO 500`457`198). IIR 53-21-11-1-003-00, Due at 77,506 TAC (tracked by WO 500`457`261). IIR 53-21-11-1-003-00, Due at 77,506 TAC (tracked by WO 500`457`265). IIR 53-11-11-1-001-00 at 77,506 TAC, controlled by WO 500`461`629. IIR 53-11-11-1-002-00 at 60,000 TAC, controlled by WO 500`461`796. IIR 53-11-11-1-002-00 at 60,000 TAC, controlled by WO 500`462`023. IIR 53-11-11-1-002-00 at 60,000 TAC, controlled by WO 500`462`352. IIR 53-11-11-1-002-00 at 77,506 TAC, controlled by WO 500`462`376. IIR 53-21-11-1-003-00 at 60,000 TAC controlled by WO 500`462`988. IIR 53-21-11-1-002-00 at 60,000 TAC, controlled by WO 500`463`217. IIR 53-21-11-1-003-00 at 60,000 TAC controlled by WO 500`463`306. IIR 53-41-11-1-005-00 at 60,000 TAC controlled by WO 500`463`384. IIR 53-41-11-1-005-00 at 60,000 TAC controlled by WO 500`463`384. WO: 500457129 TAC: 77506 WO: 500457198 TAC: 77506 WO: 500457261 TAC: 77506 WO: 500457265 TAC: 77506 WO: 500461629 TAC: 77506 WO: 500461796 TAC: 60000 WO: 500462023 TAC: 60000 WO: 500462352 TAC: 60000 WO: 500462376 TAC: 77506 WO: 500462988 TAC: 60000 WO: 500463217 TAC: 60000 WO: 500463306 TAC: 60000 WO: 500463384 TAC: 60000 WO: 500463384 TAC: 60000 1753 18 FUSELAGE SKIN REWORK. N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A IIR 53-11-11-1-002-00 at 60,000 TAC, controlled by WO N/A 500`464`579. WO: 500464579 TAC: 60000 Sub 2 - Page 4 of 9 SDM A319/A320 MAINTENANCE PROGRAM INDIVIDUAL STRUCTURAL INSPECTIONS R E V MSN ITEM REASON 1753 19 FUSELAGE SKIN REWORK. 1753 22 SMOOTH DENT. 1753 23 REWORK ON FUSELAGE SKIN. 1753 27 SKIN FLUSH INSERT REPAIR. 1753 33 FLUSH INSERT REPAIR, TOP SKIN OF RH SLAT 1. 1753 48 1753 49 LH PYLON SPIGOT FITTING BASEPLATE LOWER SURFACE REWORK. LH PYLON SPIGOT HOLE REWORK. 1753 67 External surface of skin scratch 2465 2 2465 FURTHER ACTION MP REF: SDM.A320.IRISH SECTION: V REV: 07 DATE: 02-Nov-2014 PERIODIC INSPECTION IIR 53-11-11-1-002-00 at 60,000 TAC, controlled by WO 500`464`581. IIR 53-11-11-1-001-00 at 77,506 TAC, controlled by WO 500`464`999. IIR 53-21-11-1-003-00 at 77,506 TAC controlled by WO 500`465`009. RAS/70562970/005/2012 issue B, inspection at 77,506 TAC / 150,428 TAH controlled by WO 500`465`128. RDAS 70562916/003/2012 ISSUE A: inspection at 54,600 FC / 234,700 FH from time of repair IIR 54-51-18-1-002-00 Due at 35,606 TAC, controlled by WO 500`466`720. IIR 54-51-18-1-001-00 Due at 39,406 TAC, controlled by WO 500466725. RDAS Requirements: Threshold 101600 FC/127000 FH; WO 500`933`782 controlled N/A FUSELAGE SKIN EXTERNAL DOUBLER. IIR 53-00-11-2-027-00, Due at 46`508 FH / 37`049 FC (tracked by WO 500`441`425). N/A 6 FUSELAGE SKIN EXTERNAL DOUBLER. N/A 2465 7 FUSELAGE SKIN EXTERNAL DOUBLER. 2465 8 SMOOTH BLEND OUT ON FUSELAGE SKIN. IIR 53-11-11-2-003-00, Due at 72`551 FC, FH not relevant (tracked by WO 500`449`507). IIR 53-11-11-2-003-00, Due at 68`244 FC, FH not relevant (tracked by WO 500`449`525). Threshold: 76`944 FC, 102`864 FH (tracked by WO 500`449`575) 2465 14 LIGHTINING STRIKE BURNING MARK. N/A 2465 15 LIGHTINING STRIKE BURNING MARK. 2465 16 LIGHTINING STRIKE BURNING MARK. 2465 17 LIGHTINING STRIKE BURNING MARK. 2465 18 LIGHTINING STRIKE BURNING MARK. 2465 19 LIGHTINING STRIKE BURNING MARK. IIR 53-11-11-2-002-00, Threshold: 58`537 TAC (tracked by WO 500`455`557); SMP: 70`537 TAC. IIR 53-11-11-2-002-00, Threshold: 58`537 TAC (tracked by WO 500`455`607); SMP: 70`537 TAC. IIR 53-11-11-2-002-00, Threshold: 58`537 TAC (tracked by WO 500`455`658); SMP: 70`537 TAC. IIR 53-11-11-2-002-00, Threshold: 65`437 TAC (tracked by WO 500`455`759); SMP: 70`537 TAC. IIR 53-11-11-2-002-00, Threshold: 65`437 TAC (tracked by 500`455`765); SMP: 70`537 TAC. IIR 53-11-11-2-002-00, Threshold: 65`437 TAC (tracked by 500`455`770); SMP: 70`537 TAC. N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A LIMIT WO: 500464581 TAC: 60000 WO: 500464999 TAC: 77506 WO: 500465009 TAC: 77506 WO: 500465128 TAH: 150428 WO: 500465936 TAH: 265128 WO: 500466720 TAC: 35606 WO: 500466725 TAC: 39406 WO: 500933782 TAH: 164839 TAC: 122507 WO: 500441425 TAH: 46508 TAC: 37049 WO: 500449507 TAC: 72551 WO: 500449525 TAC: 68244 WO: 500449575 TAH: 102863 TAC: 76943 WO: 500455557 TAC: 58537 WO: 500455607 TAC: 58537 WO: 500455658 TAC: 58537 WO: 500455759 TAC: 65437 WO: 500455765 TAC: 65437 WO: 500455770 TAC: 65437 Sub 2 - Page 5 of 9 SDM A319/A320 MAINTENANCE PROGRAM INDIVIDUAL STRUCTURAL INSPECTIONS R E V MSN ITEM REASON 2465 20 LIGHTINING STRIKE BURNING MARK. 2465 21 LIGHTINING STRIKE BURNING MARK. 2465 22 FUSELAGE SKIN DENT. 2465 36 2465 42 2465 44 2497 4 WO: 500747071 LH FUSELAGE FR23 STR23 SMOOTH DENT WO: 500896287 DENT ON THE LH FUSELAGE UNDER STBY STAT PORT WO: 500907580 L/H FUSELAGE BEETWEN FR2 AND 3 UNDER CAPT WINDSHILD SKIN FUSELAGE SKIN EXTERNAL DOUBLER. 2497 10 L2 DOOR LOWER SILL BEAM CORROSION. 2879 1 2879 2 2879 13 2879 14 2879 24 2879 39 2913 1 DENT ON NOSE FWD FUSELAGE OUTER SKIN BETWEEN FRAME 8-9, BELOW THE COCKPIT FLOOR LOWER SURFACE Z-650 DENT ON NOSE FWD FUSELAGE OUTER SKIN BETWEEN FRAME 6-7, STGR 21RH-22RH DENT WITH ABRASION ON THE RH FWD FUSELAGE OUTER SKIN BETWEEN FRAME 18-19 & STRINGER 30RH-31RH DENT WITH ABRASION ON THE RH FWD FUSELAGE OUTER SKIN BETWEEN FRAME 19-20 & STRINGER 31RH-32RH CORROSION AT LOWER FUSELAGE INNER SKIN SURFACE FR34 STGR 43LH and 43RH WO: 500879305 R/H FUSELAGE SKIN SCRATCH FR-24-25 STGR 3031 DENT WITH SCRATCH ON THE LH FWD NOSE FUSELAGE SKIN AT FRAME 2-3, ABOVE Z-1589 2913 6 REWORK LOCATED AT FWD CARGO DOOR SURROUNDING PANEL BETWEEN FR 24-28 and FURTHER ACTION IIR 53-21-11-2-002-00, Threshold: 58`537 TAC (tracked by WO 500`455`965); SMP: 70`537 TAC. IIR 53-21-11-2-002-00, Threshold: 58`537 TAC (tracked by WO 500`455`970); SMP: 70`537 TAC. IIR 53-11-11-1-001-00; INSP. Threshold & SMP: 72,551 FC (tracked by WO 500`456`011) Threshold 60000 FC WO:500975389 MP REF: SDM.A320.IRISH SECTION: V REV: 07 DATE: 02-Nov-2014 PERIODIC INSPECTION N/A N/A N/A N/A LIMIT WO: 500455965 TAC: 58537 WO: 500455970 TAC: 58537 WO: 500456011 TAC: 72551 WO: 500975389 TAC: 75357 WO: 500975396 TAC: 75357 IIR 53-11-11-1-001-00; Threshold 60000 FC WO:500975396 N/A Threshold 85500 FC WO:500975414 N/A WO: 500975414 TAC: 100857 IIR 53-11-11-2-003-00 DUE TAC: 68,129 (tracked by WO 500`454`260). Threshold: 100,848 FC (tracked by WO 500`454`262). Interval: TBD. IIR 53-11-11-2-003-00 First Inspection after Repair Embodiment 60000FC (WO 500468885) N/A WO: 500454260 TAC: 68129 WO: 500454262 TAC: 100848 WO: 500468885 TAC: 71936 N/A N/A IIR 53-11-11-2-003-00 First Inspection after Repair Embodiment 60000FC (WO 500468900) RDAS Requirement 49200FC From Time of Repair Embodiment (WO 500468902) N/A RDAS Requirement 49200FC From Time of Repair Embodiment (WO 500468902) N/A WO: 500468902 TAC: 61135 IIR 53-21-11-1-003-00 First Inspection 60000 From A/C N/A First Flight (WO 500468974) IIR 53-21-11-1-002-00 FIRST INSPECTION From A/C N/A first flight - 60000FC (WO:500881354) WO: 500468974 TAC: 60000 WO: 500881354 TAC: 60000 RDAS REQUIREMENT First Inspection From Time of Repair Embodiment 49200FC (WO 500469899) N/A WO: 500469899 TAC: 61124 RDAS Requirements: IIR 53-21-11-1-002-00 First inspection From A/C first flight 60000FC (WO 532137-01-1 WO: 500470193 TAC: 60000 N/A WO: 500468900 TAC: 66970 WO: 500468902 TAC: 61135 Sub 2 - Page 6 of 9 SDM A319/A320 MAINTENANCE PROGRAM INDIVIDUAL STRUCTURAL INSPECTIONS R E V MSN ITEM 2913 7 2913 37 2930 4 2930 REASON FURTHER ACTION MP REF: SDM.A320.IRISH SECTION: V REV: 07 DATE: 02-Nov-2014 PERIODIC INSPECTION LIMIT REWORK LOCATED AT RH AFT PAX DOOR OUTER SKIN (16EA) CORROSION ON FRAME FORKS (6 IN TOTAL) OF THE AFT CARGO COMPARTMENT DOOR Minor scratch between FR28 and FR29 and between STR 30 and 31RH smoothed, treated and reprotected IIR 52-10-00-1-002-00 First Inspection From Time of N/A Repair Embodiment 60000FC (WO 500470221) RDAS Requirement First Inspection from Time of Repair N/A Embodiment 51700FC (WO:500470382) IIR 53-21-11-1-002-00 – 60000 FC FIRST INSPECTION N/A FROM A/C FIRST FLIGHT WO: 500473434 WO: 500470221 TAC: 71924 WO: 500470382 TAC: 63624 WO: 500473434 TAC: 60000 6 Blend out of scratch on Rear RH door external surface at aft edge of door adjacent to STR 15RH IIR 52-10-00-1-002-00 – 60000 FC FIRST INSPECTION N/A AFTER REPAIR EMBODIMENT WO:500473446 WO: 500473446 TAC: 64062 2930 8 Dress out of dent on outer skin of bulk cargo door between FR60 and next rib located between FR60-61 IIR 52-30-00-1-002-00 FIRST INSPECTION AFTER REPAIR EMBODIMENT 60000FC (WO:500473457) N/A WO: 500473457 TAC: 69824 2930 10 N/A 2930 18 WO: 500473463 TAC: 65912 WO: 500473709 TAC: 67796 2930 19 2930 20 2930 21 2930 28 2964 1 2964 3 Dent dressed out on fuselage skin LH between FR10-11 IIR 53-11-11-1-004-00 FIRST INSPECTION AFTER REPAIR EMBODIMENT 60000FC (WO:500473463) Repair of damage caused by lightning strike on fuselage IIR 53-11-11-2-002-00 FIRST INSPECTION AFTER skin FR 5-8 LH REPAIR EMBODIMENT 48000 FC (JIC11898) SMP AFTER REPAIR EMBODIMENT 60000FC (WO:500473709) Repair of damage caused by lightning strike on rivet IIR 53-11-11-2-001-00 FIRST INSPECTION AFTER head and adjacent skin REPAIR EMBODIMENT 48000 FC (JIC11901) SMP AFTER REPAIR EMBODIMENT60000 FC (WO:500473795) Repair of damage caused by lightning strike on rivet IIR 53-21-11-2-001-00 FIRST INSPECTION AFTER head and adjacent skin FR 25-26 LH REPAIR EMBODIMENT 48000 FC (JIC:11902) SMP AFTER REPAIR EMBODIMENT 60000FC (WO:500473826) Rework of chafing on bulk cargo door outer skin at door IIR 52-33-00-1-001-00 – 140000 FC FIRST handle cutout edges INSPECTION AFTER REPAIR EMBODIMENT WO:500473391 Dent on fuselage skin FR10-11 STR 18L-19L IIR 53-11-11-1-001-00 FIRST INSPECTION FROM TIME OF DENT OCCURRENCE 60000FC (WO:500473106) Minor chafing at bulk cargo door handle cutout IIR 52-33-00-1-001-00 First Inspection after Repair Embodiment 140000FC (WO500473447) Nicks on fuselage skin aft of R2 door between STGR16- IIR 53-41-11-1-003-00 First Inspection from AC Delivery 17 at FR68 60000FC / 120000FH (WO500473698) SSI 53.41.31 11898 11901 WO: 500473795 TAC: 67796 11902 WO: 500473826 TAC: 67796 N/A WO: 500473391 TAC: 141908 N/A WO: 500473106 TAC: 64062 N/A WO: 500473447 TAC: 141708 WO: 500473698 TAH: 120000 TAC: 60000 N/A Sub 2 - Page 7 of 9 SDM A319/A320 MAINTENANCE PROGRAM INDIVIDUAL STRUCTURAL INSPECTIONS R E V MSN ITEM REASON FURTHER ACTION Burn Marks On Fastener Heads and Skin LH fuselage between FR1-24 (22EA) IIR 53-11-11-2-001-00 First Inspection after Repair Embodiment 48000FC (JIC11903) SMP After Repair Embodiment 60000FC (WO500473849) Burn Marks on Skin between FR 25-31 LH (9EA) IIR 53-21-11-2-001-00 First Inspection after Repair Embodiment 48000FC (JIC11904) SMP After Repair Embodiment 60000FC (WO500473888) Blend out of scratches on LH AFT door skin IIR 52-10-00-1-002-00 First Inspection after Repair Embodiement 60000FC (WO500473967) External doubler repair on fuselage skin between FR21- IIR 53-11-11-2-003-00 First Inspection after Repair 23 LH Embodiement 60000FC (WO500474059) On bulk cargo door external handle recess area has IIR 52-33-00-1-001-00 First Inspection after Repair chafing Embodiment - 140000FC (WO:500453438) MP REF: SDM.A320.IRISH SECTION: V REV: 07 DATE: 02-Nov-2014 PERIODIC INSPECTION LIMIT 2964 5 11903 WO: 500473849 TAC: 70205 2964 6 11904 WO: 500473888 TAC: 70205 2964 9 N/A WO: 500473967 TAC: 65868 WO: 500474059 TAC: 67948 WO: 500453438 TAC: 146042 2964 13 3044 9 3044 17 Small dent with nicks on fuselage skin IIR 53-21-11-1-004-00 First Inspection After Repair Embodiment - 60000FC (WO:500453487) N/A WO: 500453487 TAC: 67748 3044 21 External doubler repair on forward cargo compartment IIR 52-31-00-2-005-00 First Inspection after Repair Embodiment - 60000FC (WO:500453527) N/A WO: 500453527 TAC: 61000 3044 23 Rework of nicks on fuselage skin between IIR 53-21-11-1-003-00 First Inspection after Repair Embodiment - 60000FC (WO:500453530) N/A WO: 500453530 TAC: 70810 3044 38 Dent on fuselage skin IIR 53-41-11-1-007-00 FIRST INSPECTION AFTER REPAIR EMBODIMENT - 60000FC (WO:500453869) N/A WO: 500453869 TAC: 66042 3044 40 Dent on fuselage skin IIR 53-41-11-1-007-00 FIRST INSPECTION AFTER REPAIR EMBODIMENT - 60000FC (WO:500453871) N/A WO: 500453871 TAC: 66042 3044 41 Dent on fuselage skin IIR 53-41-11-1-007-00 FIRST INSPECTION AFTER REPAIR EMBODIMENT - 60000FC (WO:500453879) N/A WO: 500453879 TAC: 70811 3044 42 Dent on fuselage skin IIR 53-11-11-1-001-00 FIRST INSPECTION AFTER REPAIR EMBODIMENT - 60000FC (WO:500453886) N/A WO: 500453886 TAC: 69596 3044 43 Dent on fuselage skin IIR 53-11-11-1-001-00 FIRST INSPECTION AFTER REPAIR EMBODIMENT - 60000FC (WO:500453899) N/A WO: 500453899 TAC: 67748 N/A N/A Sub 2 - Page 8 of 9 SDM A319/A320 MAINTENANCE PROGRAM INDIVIDUAL STRUCTURAL INSPECTIONS R E V MSN ITEM REASON FURTHER ACTION MP REF: SDM.A320.IRISH SECTION: V REV: 07 DATE: 02-Nov-2014 PERIODIC INSPECTION LIMIT 3044 44 Dent on fuselage skin IIR 53-11-11-1-001-00 FIRST INSPECTION AFTER REPAIR EMBODIMENT - 60000FC (WO:500453902) N/A WO: 500453902 TAC: 64177 3044 45 Dent on fuselage skin IIR 53-11-11-1-001-00 FIRST INSPECTION AFTER REPAIR EMBODIMENT - 60000FC (WO:500454042) N/A WO: 500454042 TAC: 69596 3044 46 Dent on outer skin of AFT passenger door RH IIR 52-10-00-1-001-00 FIRST INSPECTION AFTER REPAIR EMBODIMENT - 60000FC (WO:500454044) N/A WO: 500454044 TAC: 70811 3044 47 Dent on fuselage skin N/A 3044 48 Dent on fuselage skin 3044 49 Dent on fuselage skin 3044 50 Dent on FWD cargo compartment door skin IIR 53-41-11-1-007-00 FIRST INSPECTION AFTER REPAIR EMBODIMENT - 60000FC (WO:500454050) IIR 53-41-11-1-007-00 FIRST INSPECTION AFTER REPAIR EMBODIMENT - 60000FC (WO:500454068) IIR 53-41-11-1-007-00 FIRST INSPECTION AFTER REPAIR EMBODIMENT -60000FC (WO:500454090) IIR 52-30-00-1-003-00 FIRST INSPECTION AFTER REPAIR EMBODIMENT - 60000FC (WO:500454116) WO: 500454050 TAC: 70811 WO: 500454068 TAC: 70811 WO: 500454090 TAC: 70810 WO: 500454116 TAC: 70811 N/A N/A N/A Sub 2 - Page 9 of 9 SDM A319/A320 MAINTENANCE PROGRAM APPENDIX I. EASA REQUIREMENTS REFERENCES MP-REF: SDM.A320.IRISH SECTION: VI REV: 07 DATE: 29-Dec-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 issue All pages and issue number. 1.1.4 A statement signed by the operator to the effect that the specified aeroplanes will Section I: be maintained to the program and that the program will be reviewed and updated Operator's Certification Statement as required by paragraph 5. 1.1.5 Contents/list of effective pages and their revision status of the document. 1.1.6 Check periods which reflect the anticipated utilization of the aeroplane. Such Section I: utilization should be stated and include a tolerance of not more than 25%. Where I. Introduction. C. Fleet Effectivity, Utilization and utilization cannot be anticipated, calendar time limits should also be included. Limit of Validity I. Introduction. D. Intervals and Checks Cover Page Section I: List of Effective Pages And Recording Procedure Page 1 of 6 SDM A319/A320 MAINTENANCE PROGRAM APPENDIX I. EASA REQUIREMENTS REFERENCES MP-REF: SDM.A320.IRISH SECTION: VI REV: 07 DATE: 29-Dec-2014 Section Requirements Means of Compliance 1.1.7 Procedures for the escalation of established check periods, where applicable and Section I: 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 in Section I: 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 issued Section I: 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 Page 2 of 6 SDM A319/A320 MAINTENANCE PROGRAM APPENDIX I. EASA REQUIREMENTS REFERENCES Section Requirements MP-REF: SDM.A320.IRISH SECTION: VI REV: 07 DATE: 29-Dec-2014 Means of Compliance Repair assessment 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 parts Section III 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 Instructions. OPERATOR’S CERTIFICATION STATEMENT: 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.IRISH SECTION: VI REV: 07 DATE: 29-Dec-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 Report, I. Introduction, B. Maintenance Program where available, and the Type Certificate holder’s Maintenance Planning Documents 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.IRISH SECTION: VI REV: 07 DATE: 29-Dec-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 of organization's Aircraft Maintenance Manual the aircraft or applicable component or part. 3 Amendments 3.1 Amendments (revisions) to the approved Program should be raised by the owner Section I: RECORDS AND REVISION or an M.A. subpart G approved organization, to reflect changes in the type HIGHLIGHTS certificate holder’s recommendations, modifications, service experience, or as B. Procedure of revisions 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 periods Section I. Introduction, D. Intervals and checks. prescribed by the Programme with the approval of the Authority or through a 5. Variations to maintenance periods 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 Maintenance Section RECORDS AND REVISION Programmes should be subject to periodic review to ensure that they reflect HIGHLIGHTS current Type Certificate holder’s recommendations, revisions to the Maintenance B. Procedure of revisions Review Board Report if applicable, mandatory requirements and maintenance needs of the aircraft. N/A N/A N/A Page 5 of 6 SDM A319/A320 MAINTENANCE PROGRAM APPENDIX I. EASA REQUIREMENTS REFERENCES MP-REF: SDM.A320.IRISH SECTION: VI REV: 07 DATE: 29-Dec-2014 Section Requirements Means of Compliance 5.2 The owner or an M.A. subpart G approved organization should review the Section RECORDS AND REVISION detailed requirements at least annually for continued validity in the light of HIGHLIGHTS operating experience. B. Procedure of revisions Page 6 of 6