Cessna 560 Reference manual

Citation SERVICE BULLETIN
REVISION
Revision 2 SB560-34-114
TRANSMITTAL SHEET
This sheet transmits Revision 2 to SB560-34-114.
A. Changes the illustrations for Figure 1, Sheet 1 and Figure 2, Sheet 1.
NOTE: This revision replaces the original issue of SB560-34-114 and all previous revisions in their 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 Jun 24/2004
Revision 1 Mar 29/2005
Revision 2 Jan 02/2007

Citation SERVICE BULLETIN
REVISION
Revision 1 SB560-34-114
TRANSMITTAL SHEET
This sheet transmits Revision 1 to SB560-34-114.
A. Added Step 5B to add instructions to replace the multifunction display controller.
B. Added Steps 5C through 5F to give instructions to replace the display guidance computers for affected
airplanes.
C. Added 9690583 to the REFERENCES section in the Main TCAS II Installation Engineering Drawing List.
D. Added the upgraded multifunction display controller and display guidance computers to the MATERIAL
INFORMATION section.
E. Corrects part number in the SB560-34-114-0 kit.
NOTE: This revision replaces the original issue of SB560-34-114 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 Jun 24/2004
Revision 1 Mar 29/2005

Citation SERVICE BULLETIN SB560-34-114
TITLE
NAVIGATION - TRAFFIC COLLISION AND AVOIDANCE SYSTEM (TCAS) II AND HONEYWELL PRIMUS
INSTALLATION FOR ELEMENTARY SURVEILLANCE
EFFECTIVITY
MODEL SERIAL NUMBERS
560 -0260 thru -0538 with Honeywell Primus radios
NOTE: This service bulletin may only be accomplished at a Cessna owned or authorized Citation Service
Center.
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.
NOTE: The Cessna RVSM installation is assumed for all instructions, parts and drawings listed in this service
bulletin.
NOTE: SB560-23-25 (Honeywell 8.33 KHZ Communication Radio Installation) needs to be accomplished prior
to or in conjunction with this service bulletin. If the above service bulletin is done in conjunction with
this bulletin, it will only be necessary to return the integrated communications once.
NOTE: An electrical loads analysis (ELA) must be conducted to make sure that this service bulletin is
compatible with the existing electrical loads. The installer should make sure that adequate capacity
exists for the loads being added to the circuit breaker panel and distribution system electrical loads
prior to modification of the power distribution system. Refer to the Maintenance Manual, Chapter
24, Electrical Load Analysis - Description and Operation for the aircraft base load report. Additional
electrical system changes may have occurred since the airplane left the factory and will need to
be accounted for in the electrical loads review conducted during this modification. If the installer
determines that additional electrical loads have been added and are not assessed in the base ELA,
please contact Cessna ACMT (Mod Engineering) for assistance if further analysis is necessary.
NOTE: Contact Cessna Customer Support if the installation data contained in this service bulletin is not
suitable for a specific airplane.
NOTE: In all cases where electrical bonding is necessary, refer to the Maintenance Manual, Chapter 20,
Electrical Bonding - Maintenance Practices.
REASON
To upgrade the transponder to accommodate Elementary Surveillance mandates and add TCAS II
change 7 (ACAS II).
DESCRIPTION
This service bulletin provides parts and instructions to install TCAS II and Honeywell comm units with
elementary surveillance capabilities.
Aug 13/2004 560-34-114
Revision 2 - Jan 2/2007 Page 1 of 44
Cessna Aircraft Company, Citation Marketing Division, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-6000, Fax [phone]
COPYRIGHT © 2004

Aug 13/2004 560-34-114
Revision 2 - Jan 2/2007 Page 2
Citation SERVICE BULLETIN SB560-34-114
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.
2) 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.
3) The mechanic or airplane owner must use the technical data in the service bulletin only as
approved and published.
4) 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.
5) The mechanic or airplane owner must use maintenance practices that are identified as acceptable
standard practices in the aviation industry and governmental regulations.
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.

Citation SERVICE BULLETIN SB560-34-114
MANPOWER
WORK PHASE MAN-HOURS
Modification *
MATERIAL - Cost and Availability
PART NUMBER AVAILABILITYCOST
SB560-34-114-0 **
SB560-34-114-1 * *
SB560-34-114-2 * *
SB560-34-114-3 * *
SB560-34-114-4 * *
SB560-34-114-5 * *
SB560-34-114-6 **
SB560-34-114-7 * *
SB560-34-114-8 * *
SB560-34-114-9 * *
SB560-34-114-10 * *
* Refer to the attached Service Bulletin Supplemental Data sheet for man-hours, material cost and
availability, and warranty information.
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Revision 2 - Jan 2/2007 Page 4
Citation SERVICE BULLETIN SB560-34-114
CONSUMABLE MATERIAL
In addition to the above kit(s), the following materials, or equivalent, are necessary for the accomplishment
of this service bulletin.
NAME NUMBER MANUFACTURERUSE
Hook Fabric Fas-
tener F990118 Cessna Aircraft Company Citation Parts Distribution
7121 Southwest Boulevard
Wichita, KS 67215
To bond the rain cover to the
tray assembly.
Loop Fabric Fastener F990048 Cessna Aircraft Company
Citation Parts Distribution
7121 SouthwestBoulevard
Wichita, KS 67215
To bond the rain cover to the
tray assembly.
Adhesive EA9309.3NA The Dexter Corporation
Aerospace Materials Division
2850 Willow Pass Road
Pittsburgh, CA 94565
To attach grommets.
Color Chem Film
Treatment Alodine 1201 Henkel Surface Technologies
32100 Stephenson Highway
Madison Heights, MI 48071
To treat bare aluminum.
Corrosion Resistant
Primer 513 x 419/910 x 942 PRC-DeSoto Inc.
1608 Fourth St.
Berkeley, CA 94710
To treat bare aluminum.
Sealant Type 1, Class
B-1/2 (CMNP021
CLASSB1/2)
Cessna Citation Parts Distribution
7121 Southwest Boulevard
Wichita, KS 67215
For pressure and fay seal
applications.

Citation SERVICE BULLETIN SB560-34-114
TOOLING
NAME NUMBER MANUFACTURER USE
Transponder Test Set ATC-601 software
version 2.22 or
Equivalent
IFR Systems Incorporated
10200 West YorkStreet
Wichita, KS 67125
To test Mode S transponders.
TCAS Test Set TCAS-201 IFR Systems Incorporated
10200 West YorkStreet
Wichita, KS 67125
To test TCAS II.
Air Data Test Set Model 6520 or
equivalent Labersab Incorporated 10435 Greenbough Suite 300
Stafford, TX 77477
To test pitot-static systems.
Squat Switch Simu-
lator 6588006-1 Cessna Citation Parts Distribution 7121 SouthwestBoulevard
Wichita, KS 67215
To simulate airplane ground
and air modes.
Laptop Personal
Computer Commercially available To program the TCAS II configuration module.
RS232 diagnostic
connector Commercially available To connect the personal computer to the RS232
comm port connection.
Radio Altimeter Sim-
ulator Commercially available To simulate radio altimeter altitiudes.
CHANGE IN WEIGHT AND BALANCE
Weigh the airplane after modification to calculate weight and balance information.
REFERENCES
Cessna Model 560 Maintenance Manual
Order the following engineering drawings. The latest revision and all applicable drawing change notices
for each document must be used.
MAIN TCAS II INSTALLATION ENGINEERING DRAWING LIST
DOCUMENT NUMBER TITLE
9690561 DUAL MODE-S TRANSPONDERS SYSTEM
PROGRAMMING
9608042 UPPER BENDIX TCAS ANTENNA INSTL
9608043 LOWER BENDIX TCAS ANTENNA INSTL
9608044 TRANSPONDER LOWER ANTENNA INSTL
9690536 TCAS II SYSTEM PROGRAMMING
9690476 TEST PORT INSTL-MOD TCAS II
9690574 FEED THRU PLATE FOR TCAS
9690575 TCAS II INSTRUMENT PANEL MOD
9690583 P1000 HARDWARE UPGRADE FOR TCAS
CAPABILITY-MOD
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Citation SERVICE BULLETIN SB560-34-114
(Airplanes that do not have the TCAS I system installed and are installing the TCAS II system.) In addition
to the drawings listed in the main engineering drawing list, you must order one of the following groups
of engineering drawings based on the location of the TCAS II computer. The latest revision and all
applicable drawing change notices for each document must be used.
TCAS II INSTALLATION LOCATION A, TRANSPONDER OPTION 1
DOCUMENT NUMBER TITLE
9654207 AVN C/B OPTIONAL INSTL
9656060 NOSE BAGGAGE COMPARTMENT INSTL
9690551 TCAS INSTALLATION
9690555 PRIMUS II CABLE ASSEMBLY
9690568 TCAS II CABLE ASSEMBLY
TCAS II INSTALLATION LOCATION A, TRANSPONDER OPTION 2
DOCUMENT NUMBER TITLE
9654207 AVN C/B OPTIONAL INSTL
9690551 TCAS INSTALLATION
9690558 PRIMUS II CABLE ASSEMBLY
9690568 TCAS II CABLE ASSEMBLY
TCAS II INSTALLATION LOCATION B, TRANSPONDER OPTION 1
DOCUMENT NUMBER TITLE
9654613 GROUND BLOCK INSTL
9654207 AVN C/B OPTIONAL INSTL
9690550 AFT BHD FEED THRU MOD
9622012 FLIGHT DATA RECORDER INSTL & VOICE
RECORDER INSTL
9690446 TCAS RAIN COVER INSTL-RH T/C MOD
9690555 PRIMUS II CABLE ASSEMBLY
9690560 TCAS IINSTALLATION
9690564 TCAS II CABLE ASSEMBLY
TCAS II INSTALLATION LOCATION B, TRANSPONDER OPTION 2
DOCUMENT NUMBER TITLE
9654613 GROUND BLOCK INSTL
9654207 AVN C/B OPTIONAL INSTL
9622012 FLIGHT DATA RECORDER INSTL & VOICE
RECORDER INSTL
9690446 TCAS RAIN COVER INSTL-RH T/C MOD
9690550 AFT BHD FEED THRU MOD
9690560 TCAS INSTALLATION