Citation
SERVICE BULLETIN
REVISION
Revision 1
SB560-34-122
TRANSMITTAL SHEET
This sheet transmits Revision 1 to SB560-34-122.
A. Added Step 13 to insert the flight manual supplements into the appropriate flight manuals and removed
the information from the FLIGHT CREW OPERATIONS SUMMARY.
B. Corrected some of the wire labelling in the MATERIAL INFORMATION section.
NOTE: This revision replaces the original issue of SB560-34-122 in its entirety.
NOTE: Change bars and pointing hands are not used in this publication to denote revised material. This
transmittal sheet provides a complete description of the changes made by this revision, except for
editorial changes.
REVISION COMPLIANCE
NO EFFECT. Airplanes previously modified by this service bulletin are not affected by this revision.
SUMMARY OF REVISIONS
Original Issue
Revision 1
Jul 26/2004
Aug 13/2004
SERVICE BULLETIN
Citation
SB560-34-122
TITLE
NAVIGATION - HONEYWELL TRANSPONDER UPGRADE FOR ENHANCED SURVEILLANCE
EFFECTIVITY
MODEL
SERIAL NUMBERS
560
-0260 thru -0538
NOTE: This service bulletin is only applicable to airplanes that have the MST-67A Transponders and the
KFS-578A TCAS Control Head installed and want to upgrade to enhanced surveillance.
NOTE: Limitations and Conditions: This Service Bulletin should not be extended to other specific airplanes
of these models on which other previously approved modifications are incorporated, unless it is
determined by the installer that the interrelationship between this change and any of those other
previously approved modifications will introduce no adverse effect upon the airworthiness of that
airplane.
REASON
To add enhanced surveillance capability to the Mode S transponders.
DESCRIPTION
This service bulletin provides parts and instructions to install upgraded transponder units for enhanced
surveillance.
Jul 26/2004
Revision 1 - Aug 13/2004
560-34-122
Page 1 of 8
Cessna Aircraft Company, Citation Marketing Division, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-6000, Fax 1-316-517-8500
COPYRIGHT © 2004
SERVICE BULLETIN
Citation
SB560-34-122
COMPLIANCE
OPTIONAL. This service bulletin may be accomplished at the discretion of the owner.
A service bulletin published by Cessna Aircraft Company may be recorded as “completed” in an aircraft
log only when the following requirements are satisfied:
1)
The mechanic must complete all of the instructions in the service bulletin, including the intent
therein.
The mechanic must correctly use and install all applicable parts supplied with the service bulletin
kit. Only with written authorization from Cessna Aircraft Company can substitute parts or rebuilt
parts be used to replace new parts.
The mechanic or airplane owner must use the technical data in the service bulletin only as
approved and published.
The mechanic or airplane owner must apply the information in the service bulletin only to aircraft
serial numbers identified in the “Effectivity” section of the bulletin.
The mechanic or airplane owner must use maintenance practices that are identified as acceptable
standard practices in the aviation industry and governmental regulations.
2)
3)
4)
5)
No individual or corporate organization other than Cessna Aircraft Company is authorized to make or
apply any changes to a Cessna-issued service bulletin, service letter, or flight manual supplement without
prior written consent from Cessna Aircraft Company.
Cessna Aircraft Company is not responsible for the quality of maintenance performed to comply with this
document, unless the maintenance is accomplished at a Cessna-owned Citation Service Center.
FLIGHT CREW OPERATIONS
Refer to the attached Flight Crew Operations Summary.
Make sure that the Flight Crew Operations Summary included with this service bulletin is given to the
crew to inform them of the operational changes that come from the incorporation of this service bulletin.
APPROVAL
FAA approval has been obtained on technical data in this publication that affects airplane type design.
This information shall be considered an amendment to the Cessna Manufacturer’s Maintenance Manual.
MANPOWER
WORK PHASE
MAN-HOURS
Modification
*
MATERIAL - Cost and Availability
PART NUMBER
AVAILABILITY
COST
SB560-34-122
*
*
* Refer to the attached Service Bulletin Supplemental Data sheet for man-hours, material cost and
availability, and warranty information.
Jul 26/2004
Revision 1 - Aug 13/2004
560-34-122
Page 2
SERVICE BULLETIN
Citation
SB560-34-122
TOOLING
In addition to the above kit, the following tools, or equivalent, are required for the accomplishment of this
service bulletin.
NAME
NUMBER
Transponder Test Set ATC-601 or
Equivalent
MANUFACTURER
IFR Systems Incorporated
10200 West York Street
Wichita, KS 67125
USE
To test Mode S transponders.
Pitot-Static Test Set 6520-10 or
Equivalent
Laversab Incorporated
10435 Greenbough Suite 300
Stafford, TX 77477
To test the pitot-static
systems.
CHANGE IN WEIGHT AND BALANCE
Negligible
REFERENCES
Cessna Model 560 Maintenance Manual
PUBLICATIONS AFFECTED
Cessna Model 560 Maintenance Manual
Cessna Model 560 Illustrated Parts Catalog
Cessna Model 560 Wiring Diagram Manual
ACCOMPLISHMENT INSTRUCTIONS
1.
Prepare the airplane for maintenance.
A.
Make sure that all switches are in the OFF/NORM position.
B.
Disconnect electrical power from the airplane.
C.
(1)
Disconnect the airplane battery.
(2)
Disconnect external electrical power.
Attach maintenance warning tags to the battery and external power receptacle that have "DO NOT
CONNECT ELECTRICAL POWER - MAINTENANCE IN PROGRESS" written on them.
2.
(Refer to Figure 1, Detail A.) Remove both 066-01143-0601 Transponders from the airplane.
3.
Return the removed 066-01143-0601 Transponders to Cessna Aircraft Company.
NOTE: Operators: The existing 066-01143-0601 Transponders may be modified. Contact Cessna
Citation Repairs to schedule modification at 1.866.349.8436 (US/Canada) or 1.316.517.8079
(International) or telefax 316.206.4068 or email to: citationrepair@cessna.textron.com. This will
require advance notification. Citation Repairs will schedule the units and arrange for their return.
Allow twenty days for modification. This service bulletin may not be signed off as completed
unless the units are scheduled through Cessna Citation Repairs.
4.
(Refer to Figure 1, Detail B.) Remove the 071-01507-4404 (KFS-578A) TCAS Control Head from the
airplane.
5.
(Refer to Figure 1, Detail B.) Install the 071-01618-0125 (PS578A) TCAS Control Head in the airplane.
6.
(Refer to Figure 2.) Change the electrical wiring as shown. (Refer to the following sections of the
Wiring Diagram Manual, Chapter 20: Wiring - Maintenance Practices, Splices and Terminals, Electrical
Connectors.)
7.
(Refer to Figure 1, Detail A.) Install both 066-01143-2101 Transponders in the airplane.
Jul 26/2004
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560-34-122
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SERVICE BULLETIN
Citation
SB560-34-122
8.
Remove maintenance warning tags and connect the airplane battery.
9.
Configure the 071-01618-0125 (PS578A) TCAS Control Head.
10.
A.
With a grounding wire, connect J1 (PI825) pin 24 to the airplane ground.
B.
Turn avionics power ON.
C.
With the A/N/B range selector dial in the PS-578A control head, dial in part number -4404.
D.
Turn avionics power OFF.
E.
Remove the grounding wire.
Enter the flight ID into the PS-578A control head.
A.
Select the FID push-button on the PS-578A control head.
(1)
11.
This will let you enter the alphanumeric flight identification and annunciates FID on the
PS-578A control head display.
B.
Select the right inner push-button to cycle through the eight characters to be changed.
C.
Rotate the right inner knob to change the contents of the selected FID (flashing) character. Select
FID when complete to disable the flight ID entry procedure.
Do a test of the MST-67A transponders.
A.
Connect the pitot/static test set to the airplane and simulate altitude and airspeed. (Refer to the
Maintenance Manual, Chapter 34, Pitot-Static System - Inspection/Check.)
B.
Put the FMS in DEMO mode and make sure that the GPS signal is received.
C.
Use the transponder test set to make sure that the MST-67A transponders send the correct Mode S
code, altitude, flight ID, magnetic heading ground speed, and indicated airspeed.
D.
Remove the pitot/static test set to the airplane. (Refer to the Maintenance Manual, Chapter 34,
Pitot-Static System - Inspection/Check.)
E.
Take the FMS out of DEMO mode.
12.
Make sure that the Flight Crew Operations Summary included with this service bulletin is given to the
crew to tell them of the operational changes resulting from incorporation of this service bulletin.
13.
Insert the Airplane Flight Manual Supplement into the flight manual.
14.
A.
(Airplanes that use a US Airplane Flight Manual.) Make sure that the Airplane Flight Manual
Supplement 71, Revision 0 or later, Dual Honeywell MST-67A Enhanced Mode S Transponders
, is inserted into the Airplane Flight Manual.
B.
(Airplanes that use a UK Airplane Flight Manual.) Make sure that the Airplane Flight Manual
Supplement 13, Revision 0 or later, Dual Honeywell MST-67A Enhanced Mode S Transponders
, is inserted into the Airplane Flight Manual.
C.
(Airplanes that use a Brazilian Airplane Flight Manual.) Make sure that the Airplane Flight Manual
Supplement 11, Revision 0 or later, Dual Honeywell MST-67A Enhanced Mode S Transponders
, is inserted into the Airplane Flight Manual.
Record that this service bulletin has been completed.
A.
Complete a Maintenance Transaction Report.
B.
Put a copy of the completed Maintenance Transaction Report in the airplane logbook.
C.
Send a copy of the completed Maintenance Transaction Report to: CESCOM, P.O. Box 7706,
Wichita, KS 67277.
Jul 26/2004
Revision 1 - Aug 13/2004
560-34-122
Page 4
SERVICE BULLETIN
Citation
SB560-34-122
MATERIAL INFORMATION
NOTE: The parts included in this service bulletin cover installation for one airplane.
NEW P/N
QUANTITY
KEY WORD
SB560-34-122
1
Kit, consisting of the following
parts:
071-01618-0125
1
TCAS Control Head
C489242
24 Inches
Jumper Wire
C733109
144 Inches
Wire - marked 69PN825 /12PN369 (WHT) and 70
PN825 - /25PN369 (BLU)
C733109
144 Inches
Wire - marked 83PN825
- /12PN370 (WHT) and
84PN825 - /25PN370 (BLU)
C733109
144 Inches
Wire - marked 69PN827
- /12PN369 (WHT) and
70PN827 - /25PN369 (BLU)
C733109
144 Inches
Wire - marked 83PN827
- /12PN370 (WHT) and
84PN827 - /25PN370 (BLU)
C733109
144 Inches
Wire - marked 99PN825
- /1PN381(WHT) and
100PN825 - /22PN381(BLU)
C733109
144 Inches
Wire - marked 99PN827
- /1PN381 (WHT) and
100PN827 - /22PN381 (BLU)
C489242
100 Inches
Wire - marked 92PN825 ANDC29
C489242
100 Inches
Wire - marked 92PN827 BNDC29
M39029/22-192
2
Contact
M83519/1-2
12
Splice
S2974-8
2
Shield Termination
030-01157-0011
1
Pin
030-2259-000
16
Pin
219-2220-079
4
Pin
M81824/1-1
7
Splice
SB560-34-122
1
Instructions
OLD P/N
INSTRUCTIONS/
DISPOSITION
071-015074404
Return to Cessna
NOTE: In addition to the SB560-34-122 Kit, the parts that follow will be needed to complete this service bulletin.
Jul 26/2004
Revision 1 - Aug 13/2004
560-34-122
Page 5
Citation
SERVICE BULLETIN
SB560-34-122
NEW P/N
066-01143-2101
QUANTITY
KEY WORD
OLD P/N
INSTRUCTIONS/
DISPOSITION
2
Transponder
066-011430601
Return to Cessna for
upgrade.
NOTE: Operators: The existing 066-01143-0601 Transponders may be modified. Contact Cessna Citation
Repairs to schedule modification at 1.866.349.8436 (US/Canada) or 1.316.517.8079 (International)
or telefax 316.206.4068 or email to: citationrepair@cessna.textron.com. This will require advance
notification. Citation Repairs will schedule the units and arrange for their return. Allow twenty days for
modification. This service bulletin may not be signed off as completed unless the units are scheduled
through Cessna Citation Repairs.
Jul 26/2004
Revision 1 - Aug 13/2004
560-34-122
Page 6
SERVICE BULLETIN
Citation
SB560-34-122
Figure 1. Transponder Upgrade for Enhanced Surveillance (Sheet 1)
Jul 26/2004
Revision 1 - Aug 13/2004
560-34-122
Page 7
Citation
SERVICE BULLETIN
SB560-34-122
Figure 2. Wiring Modification (Sheet 1)
Jul 26/2004
Revision 1 - Aug 13/2004
560-34-122
Page 8
Citation
ATTACHMENT
SB560-34-122
FLIGHT CREW OPERATIONS SUMMARY
This summary provides additional information for the flight crew regarding operational changes as a result
of accomplishment of this service bulletin. Please remove this summary from the service bulletin and give
it to the flight crew. This summary is informational only and does not supersede any information in the
FAA Approved Airplane Flight Manual.
1.
The airplane is now compliant with JAA TGL 8, Revision 2, Certification for ACAS II.
2.
The airplane is now compliant with JAA TGL 13, Revision 1, Certification for Mode S elementary
surveillance.
3.
The airplane is now compliant with JAA TGL 18, Certification for Mode S transponder systems for
enhanced surveillance.
SERVICE BULLETIN
SUPPLEMENTAL DATA
Citation
SB560-34-122
TITLE
NAVIGATION - HONEYWELL TRANSPONDER UPGRADE FOR ENHANCED SURVEILLANCE
EFFECTIVITY
MODEL
SERIAL NUMBERS
560
-0260 thru -0538
NOTE: This service bulletin is only applicable to airplanes that have the MST-67A Transponders installed
and want to upgrade to enhanced surveillance.
NOTE: Limitations and Conditions: This Service Bulletin should not be extended to other specific airplanes
of these models on which other previously approved modifications are incorporated, unless it is
determined by the installer that the interrelationship between this change and any of those other
previously approved modifications will introduce no adverse effect upon the airworthiness of that
airplane.
MANPOWER
WORK PHASE
MAN-HOURS
Modification
As Required
MATERIAL - Cost and Availability
PART NUMBER
AVAILABILITY
COST
SB560-34-122
*
*
* Please contact Citation Parts Distribution for current cost and availability of parts listed in this service
bulletin. Phone at 1-800-835-4000 (Domestic) or 1-316-517-7542 (International). Send Email to:
citationparts@cessna.textron.com or telefax at 1-316-517-7711.
Based on availability and lead times, parts may require advanced scheduling.
In cases where the required part(s) are available as exchange, order the exchange part and, upon
completion, expedite the return of the removed core to avoid return penalties. Contact the Citation Parts
Distribution Sales Desk for availability of exchange parts.
Jul 26/2004
560-34-122
Page 1 of 1
Cessna Aircraft Company, Citation Marketing Division, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-6000, Fax 1-316-517-8500
COPYRIGHT © 2004