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Cessna 560 Service Bulletin
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Cessna 560 Service Bulletin

Cessna 560 Service Bulletin

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Citation
Revision 2
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
Revision 1
Revision 2
SERVICE BULLETIN
REVISION
TRANSMITTAL SHEET
SB560-34-114
Jun 24/2004
Mar 29/2005
Jan 02/2007

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Summary of Contents for Cessna 560

  • Page 1 SERVICE BULLETIN REVISION Citation Revision 2 SB560-34-114 TRANSMITTAL SHEET This sheet transmits Revision 2 to SB560-34-114. 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.

  • Page 3: Summary Of Revisions

    SERVICE BULLETIN REVISION Citation Revision 1 SB560-34-114 TRANSMITTAL SHEET This sheet transmits Revision 1 to SB560-34-114. Added Step 5B to add instructions to replace the multifunction display controller. Added Steps 5C through 5F to give instructions to replace the display guidance computers for affected airplanes.
  • Page 5 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.
  • Page 6 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: The mechanic must complete all of the instructions in the service bulletin, including the intent therein.

  • Page 7: Work Phase

    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. Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 3...

  • Page 8: Consumable Material

    513 x 419/910 x PRC-DeSoto Inc. To treat bare aluminum. Primer 1608 Fourth St. Berkeley, CA 94710 Sealant Type 1, Class Cessna Citation Parts Distribution For pressure and fay seal B-1/2 (CMNP021 7121 Southwest Boulevard applications. CLASSB1/2) Wichita, KS 67215 Aug 13/2004...
  • Page 9 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.
  • Page 10 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 Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 6...
  • Page 11 TITLE 9622012 FLIGHT DATA RECORDER INSTL & VOICE RECORDER INSTL 9654613 GROUND BLOCK INSTL 9690446 TCAS RAIN COVER INSTL-RH T/C MOD 9690550 AFT BHD FEED THRU MOD 9690554 TCAS INSTALLATION Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 7...
  • Page 12 TCAS II CABLE ASSEMBLY 9690558 PRIMUS II CABLE ASSEMBLY PUBLICATIONS AFFECTED Cessna Model 560 Maintenance Manual Cessna Model 560 Illustrated Parts Catalog Cessna Model 560 Wiring Diagram Manual Cessna Model 560 Airplane Flight Manual Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007...
  • Page 13 Attach maintenance warning tags to the battery and external power receptacle that have "DO NOT CONNECT ELECTRICAL POWER - MAINTENANCE IN PROGRESS" written on them. Remove and return to Cessna the components that follow: (Refer to the Maintenance Manual, Chapter 23, Honeywell Primus Intergarted Radio System, Maintenance Practices.) •...
  • Page 14 9690576-1 and 9690558-1 Cable Assemblies. (Refer to Cessna Engineering Drawings 9690576 and 9690558.) Use the applicable subkit and Cessna Engineering Drawing to locate and install the 066-01146-1211 TCAS II Computer. (Refer to Cessna Engineering Drawing 9690551-1, 9690560-1, 9690559-2, 9690545-1, 9690554-1, 9690553-1 or 9690468-1.)
  • Page 15 (Airplanes that do not have the TCAS I installed and are installing the TCAS II Computer at location option B.) Install the ground blocks. (Refer to Cessna Engineering Drawing 9654613.) (Airplanes installing TCAS Install the circuit breakers as shown. (Refer to Cessna Engineering Drawing 9654207.) NOTE: The right hand circuit breaker panel will already have TCAS circuit breaker locations labeled and capped.
  • Page 16 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. Cessna Citation Repairs will schedule the units and arrange for their return. Allow ten to fourteen days for modification after receipt of parts from Citation Parts Distribution.
  • Page 17 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. Cessna Citation Repairs will schedule the units and arrange for their return. Allow ten to fourteen days for modification after receipt of parts from Citation Parts Distribution.
  • Page 18 Hold/mount the antenna so that no large metal objects are between the tester antenna and the aircraft XRDR 1 antenna. Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 14...
  • Page 19 Test Set and pilot’s EADI are within 125 feet. When the maximum altitude has been checked on increasing altitude, slowly descend while checking the same altitude transitions points while descending with the SEC ENC ALT Air Data Computer. Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 15...
  • Page 20 Make sure that a capability report is being transmitted and record the status of parameters: XPDR Level, SI Capability, Aircraft ID Capability, Squitter Capability, and Comm Use GICB Report received by the test set. Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 16...
  • Page 21 From the main menu screen select “Config Mod” from the top menu. Select “Initialize Config Module” and choose “Yes” to continue initialization of the module. Configure each option per the TCAS II configuration procedure. Press “OK” after configuring all options. Press “OK” Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 17...
  • Page 22 Line Select Key to hightlight the ATC window. Press and hold the TST function key for two seconds. The MFD/PFD will display “TCAS TEST”, the RMU will display "SYS TEST.". A test Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 18...
  • Page 23 Turn the TCAS-201 Test Set on and perform a self test by pressing the “Self Test” then “Run”. Make sure that all modules passed the self test (a pass or fail indication for each module will be displayed). Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 19...
  • Page 24 TCAS self-test begins (prior to hearing the test message). During TCAS self test, the only aural message heard is “TCAS System Test OK”. To make sure that GPWS Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 20...
  • Page 25 (signal absorbing material) or equivalent and the Nose Landing Gear logic must be UP and LOCKED (TA's appear as NO BEARING targets when gear logic is DOWN because the bottom antenna is in omni directional mode). Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 21...
  • Page 26 Repeat the Bearing Accuracy Test for the bottom antenna using the procedure from Step 12J using Table 4. Table 3 TCAS II BEARING ACCURACY TABLE TOP ANTENNA RAMP TESTER HEADING OR INTRUDER BEARING (from BEARING ERROR RELATIVE BEARING traffic display) Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 22...
  • Page 27 Set altitude reporting to OFF and initiate the intruder test scenario. No altitude number or trend arrow should appear beside any intruder that is NAR. Make sure of this on the MFD/PFD. Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 23...
  • Page 28 Test ADF, communication and navigation radios on at least one low, high, and mid-band frequency when possible. Make sure that there is no interference with the systems listed below. NOTE: X = Tested. Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 24...
  • Page 29 (Airplanes that use a UK Airplane Flight Manual.) Make sure that the Airplane Flight Manual Supplement 12, Revision 0 or later, Elementary Mode-S Transponder Upgrade, is inserted into the Airplane Flight Manual. Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 25...

  • Page 30: Material Information

    MS2469450 Screw MS27039-1-16 Screw MS35206-215 Screw MS35489-11 Grommet Fastener Assembly PFSC35-38A S1050-1-3.40 Grommet Anchor S1741-1 S1741-5 Anchor S2899L1.0 Circuit Breaker S2899L5.0 Circuit Breaker 9608090-1 Antenna Adapter 071-01548-0100 ANT67A Directional Antenna Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 26...
  • Page 31 MS20257H3-400 Hinge Half MS21043-3 Nutplate MS21056L08 Nutplate MS21069L08K MS21069L3 Nutplate MS21069-3 Nutplate Nutplate MS21069-08 Nutplate MS21075L06N MS21075L08N Nutplate MS24694S47 Screw MS24694S5 Screw MS27039-0805 Screw MS27039-0807 Screw MS27039-1-07 Screw MS35206-230 Screw Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 27...
  • Page 32 5513085-35 Inspection Lens 6313032-10 Right Stiffener 6313080-21 Center Support 6313080-22 Upper Right Support 6513005-17 Support Clip 6513005-21 Splice Plate 6513005-48 Support Clip 6513005-49 Right Side Support 6513006-4 Right Support Side Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 28...
  • Page 33 NOTE: In addition to SB560-34-114-0 Kit, the following kit will be necessary to accomplish this service bulletin on airplanes that do not have the TCAS I system installed and will have the 066-01146-1211 TCAS II Computer installed at location A Option 2. Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 29...
  • Page 34 In addition to SB560-34-114-0 Kit, the following will be necessary to accomplish this service bulletin on airplanes that do not have the TCAS I system installed and will have the 066-01146-1211 TCAS II Computer installed at location Option B. Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 30...
  • Page 35 TCAS II Processor 071-00097-0100 Configuration Module 6512055-57 Cover 9622012-2 Access Panel 9622012-6 Shear Clip 9622012-10 Angle 9622012-13 Hat Section 9622012-14 Angle 9622012-16 Channel 9622012-17 9622012-19 Plate 9622012-23 Clip 9622012-25 Clip 9622012-29 Angle Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 31...
  • Page 36 Nutplate MS24694S5 Screw MS27039-0808 Screw MS35206-230 Screw MS35207-261 Screw S1050-1 Grommet S1741-1 Anchor S2526-2 Block and Connector S2800-39 Connector Kit S2899L1.0 Circuit Breaker S2899L5.0 Circuit Breaker 066-01146-1211 TCAS II Processor Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 32...
  • Page 37 MS21069-08 Nutplate MS21075L06N Nutplate MS21075L08 Nutplate MS21075L3N Nutplate MS24694S47 Screw MS24694S4 Screw MS27039-0805 Screw MS27039-0808 Screw MS27039-1-08 Screw MS35206-229 Screw MS35206-243 Screw MS35206-245 Screw MS35207-266 Screw S1050-1-10.00 Grommet S1050-3-4.00 Grommet Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 33...
  • Page 38 Angle 9608054-6 Angle 9608054-7 Angle 9608054-8 Angle 9608054-9 Angle 9608054-11 Support Strip 9608054-13 Box Member 9608054-14 Angle 9608054-16 Angle 9608054-18 Angle 9608054-20 Hat Section 9608054-21 Angle 9608054-23 Cover 9608054-25 Cover Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 34...
  • Page 39 NEW P/N QUAN- KEY WORD OLD P/N INSTRUCTIONS/ TITY DISPOSITION SB560-34-114-6 Kit, consisting of the following parts: NAS1149D0363J Washer MS21042L06 MS21043-3 MS35206-230 Screw MS35206-231 Screw MS35207-266 Screw MS35338-157 Lock Washer Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 35...
  • Page 40 NEW P/N QUAN- KEY WORD OLD P/N INSTRUCTIONS/ TITY DISPOSITION SB560-34-114-8 Kit, consisting of the following parts: MS21042L06 MS24694S4 Screw MS27039-0808 Screw MS35206-229 Screw MS35206-245 Screw S1477-08 S1741-1 Anchor S2099-6 Contact Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 36...
  • Page 41 KEY WORD OLD P/N INSTRUCTIONS/ TITY DISPOSITION 4890307-2-1 Carpet (Medium Grey) 4890307-2-2 Carpet (Charcoal) 4890307-2-3 Carpet (Sand) In addition to the applicable kits above, the following parts must be upgraded. Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 37...
  • Page 42 316.206.4068 or email to: citationrepair@cessna.textron.com. This will require advance notification. Cessna Citation Repairs will schedule the units and arrange for their return. Allow ten to fourteen days for modification after receipt of parts from Citation Parts Distribution. This service bulletin may not be signed off as completed unless the units are scheduled through Cessna Citation Repairs.
  • Page 43 316.206.4068 or email to: citationrepair@cessna.textron.com. This will require advance notification. Cessna Citation Repairs will schedule the units and arrange for their return. Allow ten to fourteen days for modification after receipt of parts from Citation Parts Distribution. This service bulletin may not be signed off as completed unless the units are scheduled through Cessna Citation Repairs.
  • Page 44 SERVICE BULLETIN Citation SB560-34-114 Figure 1. TCAS Computer Location Options A and B (Sheet 1) Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 40...
  • Page 45 SERVICE BULLETIN Citation SB560-34-114 Figure 2. TCAS Computer Location Option C (Sheet 1) Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 41...
  • Page 46 SERVICE BULLETIN Citation SB560-34-114 Figure 3. TCAS Computer Location Option D (Sheet 1) Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 42...
  • Page 47 SERVICE BULLETIN Citation SB560-34-114 Figure 4. COMM Location Option 1 (Sheet 1) Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 43...
  • Page 48 SERVICE BULLETIN Citation SB560-34-114 Figure 5. COMM Location Option 2 (Sheet 1) Aug 13/2004 560-34-114 Revision 2 - Jan 2/2007 Page 44...
  • Page 49 ATTACHMENT Citation SB560-34-114 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.

  • Page 51: Power Consumption

    ATTACHMENT Citation SB560-34-114 POWER CONSUMPTION UNIT Part Number DISPOSITION POWER (AMPS) Radio Managment Unit Remove 1.2 (nominal) (RMU) RM-85X Radio Managment Unit 7012100-82X 1.2 (nominal) (RMU) RM-850 Intergrated 7510700-XXX Remove 7.5 (maximum) Communication Unit RCZ-8XX w/XS Module Intergrated 7510700-767 7.5 (maximum) Communication Unit RCZ-833K w/XS-852 Module...
  • Page 53 SB560-34-114-8 SB560-34-114-9 SB560-34-114-10 4890307-2-1 4890307-2-2 4890307-2-3 7012100-825SPEX 7510700-765SPEX 7513000-835SPEX Aug 13/2004 560-34-114 Revision A - Mar 29/2005 Page 1 of 2 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...
  • Page 54 * 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.