REVISION TRANSMITTAL This sheet transmits Revision 2 to, which: A. Adds the reference to Figure 7, Sheet 1 and Sheet 2 to Step 10D. B. Adds Step 10D(7). C. Removes the After Modification view for PN343 Electrical Connector from Figure 7, Sheet 1. D. Adds the Before Modification View for the PN343 Electrical Connector and moves the After Modification view for the PN343 Electrical Connector to a new Figure 7, Sheet 2. E. ChangesthewiringmodificationinFigure7,Sheet2. F. Changes the parts required in the -1 subkit. NOTE: This revision replaces the original issue and previous revisions of in their entirety. REVISION COMPLIANCE NO EFFECT. Airplanes previously modified by this service bulletin are not affected by this revision. LOG OF REVISIONS Original Issue January 14, 2010 Revision 1 August 14, 2013 Revision 2 May 30, 2014 Original Issue - January 14, 2010 Revision 2 - May 30, 2014 Page 1 of 1 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-5800 COPYRIGHT 2010
REVISION TRANSMITTAL This sheet transmits Revision 1 to, which: A. Adds the CI401-460 GPS Antenna to the instructions and illustrations. B. Changes the wire length from PN700 to PN342 from 36 inches to 180 inches. C. Changes the part number of the GPS-4000S computer from 822-2189-002 to 822-2189-010. NOTE: This revision replaces the original issue of in its entirety. REVISION COMPLIANCE NO EFFECT. Airplanes previously modified by this service bulletin are not affected by this revision. LOG OF REVISIONS Original Issue January 14, 2010 Revision 1 August 14, 2013 Original Issue - January 14, 2010 Revision 2 - May 30, 2014 Page 1 of 1 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-5800 COPYRIGHT 2010
TITLE NAVIGATION - COLLINS FMS-3000 WIDE AREA AUGMENTATION SYSTEM (WAAS) WITH FMS 4.0 SOFTWARE UPDATES EFFECTIVITY REASON MODEL SERIAL NUMBERS 525 (CJ1+) -0600 thru -0679, -0681 thru -0684 The equivalent of this service bulletin has been incorporated on production airplanes -0680 and -0685 and On. NOTE: Airplanes -0600 thru -0640 must incorporate SB525-34-79 Navigation - V-Speed Enable And Software Upgrade prior to or in conjunction with this service bulletin. A more precise satellite based augmentation system is required to fly LP, LPV, LNAV, and VNAV approaches. DESCRIPTION This service bulletin provides parts and instructions to install WAAS capable components to fly precision approaches. COMPLIANCE OPTIONAL. This service bulletin can 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. Original Issue - January 14, 2010 Revision 2 - May 30, 2014 Page 1 of 29 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-5800 This document contains technical data and is subject to U.S. export regulations. This information has been exported from the United States in accordance with export administration regulations. Diversion contrary to U.S. law is prohibited. ECCN: 9E991 COPYRIGHT 2010
APPROVAL Cessna received FAA approval for the technical data in this publication that changes the airplane type design. FLIGHT CREW OPERATIONS Refer to the attached Flight Crew Operations Summary. CONSUMABLE MATERIAL You must use the consumable materials that follow, or their equivalent, to complete this service bulletin. NAME NUMBER MANUFACTURER USE Adhesive U064002 Cessna Service Parts & Programs 7121 Southwest Boulevard Wichita, KS 67215 Sealant (Type I Class B2) U470641 Color Chemical Film U074093 Corrosion Resistant Primer K000574 WEIGHT AND BALANCE INFORMATION Cessna Service Parts & Programs 7121 Southwest Boulevard Wichita, KS 67215 Cessna Service Parts & Programs 7121 Southwest Boulevard Wichita, KS 67215 Cessna Service Parts & Programs 7121 Southwest Boulevard Wichita, KS 67215 To fill the holes for the fasteners in the antenna. To fay and fillet seal the components to the structure. To prepare aluminum surface for intermediate primer. Final finish for aluminum. AIRPLANES -0600 THRU -0640 KIT NUMBER WEIGHT CHANGE RESULTANT MOMENT MOMENT/100-0 Negligible Negligible Negligible -1 Negligible Negligible Negligible -2 Negligible Negligible Negligible AIRPLANES -0641 THRU -0679 AND -0681 THRU -0684 KIT NUMBER WEIGHT CHANGE RESULTANT MOMENT MOMENT/100-0 + 0.10 pounds + 3.09 inch-pounds + 0.03 inch-pounds -1 + 0.10 pounds + 27.47 inch-pounds + 0.27 inch-pounds REFERENCES Cessna Model 525 Maintenance Manual Cessna Model 525 Wiring Diagram Manual (-0600 and On) Cessna Model 525 Structural Repair Manual PUBLICATIONS AFFECTED Cessna Model 525 Maintenance Manual Cessna Model 525 Wiring Diagram Manual (-0600 and On) Cessna Citation CJ1+ FAA Approved Airplane Flight Manual (525FMB) Page 2 Revision 2 - May 30, 2014
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. (1) Disconnect the airplane battery. (2) Disconnect external electrical power. C. Attach maintenance warning tags to the battery and external power receptacle that have "DO NOT CONNECT ELECTRICAL POWER - MAINTENANCE IN PROGRESS" writtenonthem. 2. Contact Citation Customer Care to request a copy of the Rockwell Collins Operator's Guide for the FMS-3000 v4.0 (part number 523-0810168-001117 or later) at phone number 1-316-517-5800 or customercare@cessna.textron.com. 3. (Refer to Figure 8, Detail A.) Remove two IOC modules and FMC-3000 cards from the IAPS card cage. (Refer to the Model 525 Maintenance Manual, Chapter 34, Collins Pro Line 21 Integrated Avionics Processor System - Maintenance Practices.) 4. Remove the GPS-4000A GPS receiver(s). (Refer to the Model 525 Maintenance Manual, Chapter 34, Collins FMS-3000 Flight Management System - Maintenance Practices.) NOTE: Operators: The existing FMC-3000, IOC Module, and GPS-4000S can be modified. Contact the Cessna Service Parts & Programs Repair Team for RMA to schedule your unit at telefax 1-316-206-4068 or e-mail citationrepair@cessna.textron.com available 8:00 4:30 CST weekdays. Advance notification and coordination is required for Cessna Service Parts & Programs Repair Team to effectively schedule units, ship to supplier, and arrange return. The expected turn time for the supplier supporting this service document is five to seven days. 5. Remove the furnishing from the right side of the airplane. (Refer to the applicable sections of the Model 525 Maintenance Manual and Interior Maintenance Manual and Illustrated Parts Catalog.) 6. Remove the headliner and sidewalls. (Refer to the Model 525 Maintenance Manual, Chapter 25, Headliner and Sidewall Maintenance Practices.) 7. Remove the panels that follow: (Refer to the Model 525 Maintenance Manual, Chapter 6, Access Plates and Panels Identification - Description and Operation.) 211LZ 211DZ 211EZ 211FZ 211CZ 212DZ 212CZ 8. (Airplanes -0600 thru -0640) Install the GPS antenna(s). A. Install the left GPS antenna. (1) (Refer to Figure 1, View A-A.) Remove and discard the parts that follow: Four MS24694C54 Screws One 822-1330-001 GPS Antenna Four S2031-3 Nutplates One 9123029-3 Doubler (2) (Refer to Figure 1, View B-B.) Install the 9190168-12 Doubler. (a) Put the 9190168-12 Doubler in position and identify the hole locations. Revision 2 - May 30, 2014 Page 3
(b) (c) (d) (e) (f) (g) (h) (i) (j) (k) (l) (m) (n) (o) (p) Remove 14 fasteners from the airplane structure. Remove two fasteners from the 2L stringer. Remove two fasteners from the 1 stringer. Remove five fasteners from the 151.00 frame. Remove five fasteners from the 158.72 frame. Match drill 38 Number 30 (0.128 inch-diameter) holes in the 9190168-12 Doubler that align with the holes in the airplane structure. Drill 18 Number 30 (0.128 inch-diameter) holes in the 9190168-12 Doubler and airplane structure. Countersink 18 Number 30 (0.128 inch-diameter) holes 100 x 0.189 inch diameter. Match drill four 0.203 inch-diameter holes in the 9190168-12 Doubler that align with the holes in the airplane structure. Match drill eight Number 40 (0.098 inch-diameter) holes in the 9190168-12 Doubler that align with the holes in the airplane structure. Remove the 9190168-12 Doubler and deburr the drilled holes. Install the 9190168-12 Doubler with temporary sheet metal fasteners. (Refer to Figure 1, Detail A.) Make the existing cutout larger. Remove the 9190168-12 Doubler and deburr the cutout. Use the color chemical film treatment and corrosion resistant primer to protect all bare material. (Refer to the Model 525 Structural Repair Manual, Chapter 51, Protective Treatment of Metal - Description and Operation.) Use Type I Class B2 Sealant to apply a fay seal to the 9190168-12 Doubler. (Refer to the Model 525 Maintenance Manual, Chapter 20, Fuel, Weather, Pressure, and High Temperature Sealing - Maintenance Practices.) Install one 9190168-12 Doubler with 28 CM3827AD4-5 Rivets and 28 CM3827AD4-3.5 Rivets. Install four NAS1473A08N Nutplates with eight MS20426AD3-4A Rivets. Install three CM3827AD4-3.5 Rivets wet with Type I Class B2 Sealant to fill the open holes. (Refer to the Model 525 Maintenance Manual, Chapter 20, Fuel, Weather, Pressure, and High Temperature Sealing - Maintenance Practices.) (3) (Refer to Figure 1, View B-B.) Install one CI428-410 Antenna with four MS24693S54 Screws. (4) Make sure that there is a Type I electrical bond between the CI428-410 Antenna and the airframe structure. (Refer to the Model 525 Maintenance Manual, Chapter 20, Electrical Bonding - Maintenance Practices.) (5) Use Type I Class B2 Sealant to apply a fillet seal between the antenna and the skin. (Refer to the Model 525 Maintenance Manual, Chapter 20, Fuel, Weather, Pressure, and High Temperature Sealing - Maintenance Practices.) (6) Use Type I Class B2 Sealant to overcoat the nutplates. (Refer to the Model 525 Maintenance Manual, Chapter 20, Fuel, Weather, Pressure, and High Temperature Sealing - Maintenance Practices.) (7) Use Type V, Class A adhesive to fill the holes in the top of the antenna. (Refer to the Model 525 Maintenance Manual, Chapter 20, Adhesive and Solvent Bonding - Maintenance Practices.) Page 4 Revision 2 - May 30, 2014
B. Install the right GPS antenna. (1) (Airplanes that have a teardrop shaped (Garmin) GPS antenna) Install the right GPS antenna. (a) (Refer to Figure 2, View A-A.) Remove and discard the parts that follow: Four MS24694C49 Screws One 011-00147-00 GPS Antenna Four S2031-3 Nutplates One 9123029 Doubler (b) (Refer to Figure 2, View B-B.) Fill eight Number 40 (0.980 inch-diameter) holes and two 0.203 inch-diameter holes in the skin. 1 Identify the aft 0.203 inch-diameter holes. 2 Countersink the inner skin 100 x 0.232 inch-diameter in the skin. 3 Identify eight Number 40 (0.980 inch-diameter) holes in the skin. 4 Countersink the inner skin 100 x 0.136 inch-diameter. 5 Install two MS20426A6-4N Rivets wet with Type I Class B2 Sealant. (Refer to the Model 525 Maintenance Manual, Chapter 20, Fuel, Weather, Pressure, and High Temperature Sealing - Maintenance Practices.) 6 Install eight CM3827AD3-3 Rivets wet with Type I Class B2 Sealant. (Refer to the Model 525 Maintenance Manual, Chapter 20, Fuel, Weather, Pressure, and High Temperature Sealing - Maintenance Practices.) 7 Shave the heads and butts of the installed rivets flush with the skin. Revision 2 - May 30, 2014 Page 5
(c) (d) (e) (f) (Refer to Figure 2, View B-B.) Install the 9190168-12 Doubler. 1 Put the 9190168-12 Doubler in position and identify the hole locations. 2 Remove 12 fasteners from the airplane structure. Remove two fasteners from the 2R stringer. Remove two fasteners from the 1 stringer. Remove four fasteners from the 151.00 frame. Remove four fasteners from the 158.72 frame. 3 Match drill 31 Number 30 (0.128 inch-diameter) holes in the 9190168-12 Doubler that align with the holes in the airplane structure. 4 Drill 24 Number 30 (0.128 inch-diameter) holes in the 9190168-12 Doubler and airplane structure. 5 Countersink 24 Number 30 (0.128 inch-diameter) holes 100 x 0.189 inch diameter. 6 Match drill two 0.203 inch-diameter holes in the 9190168-12 Doubler that align with the holes in the airplane structure. 7 Countersink two 0.203 inch-diameter holes 100 x 0.266 inch diameter. 8 Drill four 0.203 inch-diameter holes in the airplane structure and 9190168-12 Doubler for the NAS1473A08N Nutplates. 9 Drill eight Number 40 (0.098 inch-diameter) holes in the airplane structure and 9190168-12 Doubler for the NAS1473A08N Nutplates. 10 Countersink eight Number 40 (0.098 inch-diameter) holes 100 x 0.180 inch diameter. 11 Remove the 9190168-12 Doubler and deburr the drilled holes. 12 Install the 9190168-12 Doubler with temporary sheet metal fasteners. 13 (Refer to Figure 2, View B-B.) Make the existing cutout larger. 14 Remove the 9190168-12 Doubler and deburr the cutout. 15 Use the color chemical film treatment and corrosion resistant primer to protect all bare material. (Refer to the Model 525 Structural Repair Manual, Chapter 51, Protective Treatment of Metal - Description and Operation.) 16 Use Type I Class B2 Sealant to apply a fay seal to the 9190168-12 Doubler. (Refer to the Model 525 Maintenance Manual, Chapter 20, Fuel, Weather, Pressure, and High Temperature Sealing - Maintenance Practices.) 17 Install one 9190168-12 Doubler with two MS20426A6-4N Rivets, 26 CM3827AD4-5 Rivets and 26 CM3827AD4-3.5 Rivets. 18 Shave the head of the MS20426A6-4N Rivets flush with the skin. 19 Install four NAS1473A08N Nutplates with eight MS20426AD3-4A Rivets. (Refer to Figure 2, View B-B.) Install one CI428-410 Antenna with four MS24693S54 Screws. Make sure that there is a Type I electrical bond between the CI428-410 Antenna and the airframe structure. (Refer to the Model 525 Maintenance Manual, Chapter 20, Electrical Bonding - Maintenance Practices.) Use Type I Class B2 Sealant to apply a fillet seal between the antenna and the skin. (Refer to the Model 525 Maintenance Manual, Chapter 20, Fuel, Weather, Pressure, and High Temperature Sealing - Maintenance Practices.) Page 6 Revision 2 - May 30, 2014
(g) Use Type I Class B2 Sealant to overcoat the nutplates. (Refer to the Model 525 Maintenance Manual, Chapter 20, Fuel, Weather, Pressure, and High Temperature Sealing - Maintenance Practices.) (h) Use Type V, Class A adhesive to fill the holes in the top of the antenna. (Refer to the Model 525 Maintenance Manual, Chapter 20, Adhesive and Solvent Bonding - Maintenance Practices.) (2) (Airplanes that have a rectangular shaped (Rockwell Collins) GPS antenna) Install the right GPS antenna. (a) (Refer to Figure 3, View A-A.) Remove and discard the parts that follow: Four MS24694C49 Screws One 822-1330-001 GPS Antenna Four S2031-3 Nutplates One 9123029 Doubler (b) (Refer to Figure 3, View B-B.) Install the 9190168-12 Doubler. 1 Put the 9190168-12 Doubler in position and identify the hole locations. 2 Remove 4 fasteners from the airplane structure. Remove two fasteners from the 2R stringer. Remove two fasteners from the 1 stringer. 3 Match drill 36 Number 30 (0.128 inch-diameter) holes in the 9190168-12 Doubler that align with the holes in the airplane structure. 4 Drill 18 Number 30 (0.128 inch-diameter) holes in the 9190168-12 Doubler and airplane structure. 5 Countersink 18 Number 30 (0.128 inch-diameter) holes 100 x 0.189 inch diameter. 6 Match drill four 0.203 inch-diameter holes in the 9190168-12 Doubler that align with the holes in the airplane structure. 7 Drill eight Number 40 (0.098 inch-diameter) holes in the airplane structure and 9190168-12 Doubler for the NAS1473A08N Nutplates. 8 Countersink eight Number 40 (0.098 inch-diameter) holes 100 x 0.180 inch diameter. 9 Remove the 9190168-12 Doubler and deburr the drilled holes. 10 Install the 9190168-12 Doubler with temporary sheet metal fasteners. 11 (Refer to Figure 3, Detail A.) Make the existing cutout larger. 12 Remove the 9190168-12 Doubler and deburr the cutout. 13 Use the color chemical film treatment and corrosion resistant primer to protect all bare material. (Refer to the Model 525 Structural Repair Manual, Chapter 51, Protective Treatment of Metal - Description and Operation.) 14 Use Type I Class B2 Sealant to apply a fay seal to the 9190168-12 Doubler. (Refer to the Model 525 Maintenance Manual, Chapter 20, Fuel, Weather, Pressure, and High Temperature Sealing - Maintenance Practices.) 15 Install one 9190168-12 Doubler with 26 CM3827AD4-5 Rivets and 28 CM3827AD4-3.5 Rivets. 16 Install three CM3827AD4-3.5 Rivets wet with Type I Class B2 Sealant to fill the open holes. (Refer to the Model 525 Maintenance Manual, Chapter 20, Fuel, Weather, Pressure, and High Temperature Sealing - Maintenance Practices.) 17 Install four NAS1473A08N Nutplates with eight MS20426AD3-4A Rivets. Revision 2 - May 30, 2014 Page 7
(c) (d) (Refer to Figure 3, View B-B.) Install one CI428-410 Antenna with four MS24693S54 Screws. Make sure that there is a Type I electrical bond between the CI428-410 Antenna and the airframe structure. (Refer to the Model 525 Maintenance Manual, Chapter 20, Electrical Bonding - Maintenance Practices.) (e) Use Type I Class B2 Sealant to apply a fillet seal between the antenna and the skin. (Refer to the Model 525 Maintenance Manual, Chapter 20, Fuel, Weather, Pressure, and High Temperature Sealing - Maintenance Practices.) (f) Use Type I Class B2 Sealant to overcoat the nutplates. (Refer to the Model 525 Maintenance Manual, Chapter 20, Fuel, Weather, Pressure, and High Temperature Sealing - Maintenance Practices.) (g) Use Type V, Class A adhesive to fill the holes in the top of the antenna. (Refer to the Model 525 Maintenance Manual, Chapter 20, Adhesive and Solvent Bonding - Maintenance Practices.) 9. (Airplanes -0641 thru -0679 and -0681 thru -0684) Install the GPS antenna(s). A. (Refer to Figure 4, View A-A.) Install the left GPS antenna. (1) Remove and discard the parts that follow: Four MS27039-1-17 Screws One CI401-460 or 822-1330-001 GPS Antenna Four NAS1473A3 Nutplates (2) Install four NAS1473A08N Nutplates with eight MS20426AD3-4A Rivets wet with Type I Class B2 Sealant. (Refer to the Model 525 Maintenance Manual, Chapter 20, Fuel, Weather, Pressure, and High Temperature Sealing - Maintenance Practices.) (3) Install one CI428-410 Antenna with four MS24693S54 Screws. (4) Make sure that there is a Type I electrical bond between the CI428-410 Antenna and the airframe structure. (Refer to the Model 525 Maintenance Manual, Chapter 20, Electrical Bonding - Maintenance Practices.) (5) Use Type I Class B2 Sealant to apply a fillet seal between the antenna and the skin. (Refer to the Model 525 Maintenance Manual, Chapter 20, Fuel, Weather, Pressure, and High Temperature Sealing - Maintenance Practices.) (6) Use Type I Class B2 Sealant to overcoat the nutplates. (Refer to the Model 525 Maintenance Manual, Chapter 20, Fuel, Weather, Pressure, and High Temperature Sealing - Maintenance Practices.) (7) Use Type V, Class A adhesive to fill the holes in the top of the antenna. (Refer to the Model 525 Maintenance Manual, Chapter 20, Adhesive and Solvent Bonding - Maintenance Practices.) B. (Airplanes that have dual Rockwell Collins FMS.) (Refer to Figure 5, View A-A.) Install the right GPS antenna. (1) Remove and discard the parts that follow: Four MS27039-1-17 Screws One CI401-460 or 822-1330-001 GPS Antenna Four NAS1473A3 Nutplates (2) Install four NAS1473A08N Nutplates with eight MS20426AD3-4A Rivets wet with Type I Class B2 Sealant. (Refer to the Model 525 Maintenance Manual, Chapter 20, Fuel, Weather, Pressure, and High Temperature Sealing - Maintenance Practices.) (3) Install one CI428-410 Antenna with four MS24693S54 Screws. Page 8 Revision 2 - May 30, 2014
(4) Make sure that there is a Type I electrical bond between the CI428-410 Antenna and the airframe structure. (Refer to the Model 525 Maintenance Manual, Chapter 20, Electrical Bonding - Maintenance Practices.) (5) Use Type I Class B2 Sealant to apply a fillet seal between the antenna and the skin. (Refer to the Model 525 Maintenance Manual, Chapter 20, Fuel, Weather, Pressure, and High Temperature Sealing - Maintenance Practices.) (6) Use Type I Class B2 Sealant to overcoat the nutplates. (Refer to the Model 525 Maintenance Manual, Chapter 20, Fuel, Weather, Pressure, and High Temperature Sealing - Maintenance Practices.) (7) Use Type V, Class A adhesive to fill the holes in the top of the antenna. (Refer to the Model 525 Maintenance Manual, Chapter 20, Adhesive and Solvent Bonding - Maintenance Practices.) 10. (Refer to Figure 6.) Install the electrical wiring. A. Add the electrical wiring between the GPS1 (PN700) and the IAPS (PN342). B. Add the electrical wiring between the GPS1 (PN700) and the PN703 connector. C. Add the electrical wiring between the PN703 connector and the NGS505 ground stud. D. (Airplanes that have dual Rockwell Collins FMS) (Refer to Figure 7, Sheet 1 and Sheet 2.) Install the electrical wiring. (1) Add the electrical wiring between the GPS2 (PT700) and the PT702 connector. (2) Add the electrical wiring between the GPS2 (PT700) and the PT703 connector. (3) Add the electrical wiring between the PT703 connector and the TGS503 ground stud. (4) Add the electrical wiring between the PN343 connector and the PB312 connector. (5) Add the electrical wiring between the JB312 connector and the JA305. (6) Add the electrical wiring between the PA305 connector and the JT702. (7) Remove the electrical wiring from 30PN343 and 31PN343 and cap and stow the wires using two TC4001 Capnuts.. 11. (Refer to Figure 8, Detail A.) Install one 822-1361-412 IOC Module and one 822-0883-038 FMC-3000 Computer cards in the IAPS card cage. (Refer to the Model 525 Maintenance Manual, Chapter 34, Collins Pro Line 21 Integrated Avionics Processor System - Maintenance Practices.) NOTE: Airplanes with dual FMS will install two FMC-3000 Computers. A. (Refer to Figure 8, Detail A.) Remove two CSU-3100 Configuration Strapping Units from the IAPS card cage. (Refer to the Model 525 Maintenance Manual, Chapter 34, Collins Pro Line 21 Integrated Avionics Processor System - Maintenance Practices.) B. (Refer to Figure 8, Detail B.) Remove one OCM-3100 from each CSU-3100 Configuration Strapping Unit. C. (Refer to Figure 8, Detail B.) Install one 822-1484-228 OCM-3100 on each CSU-3100 Configuration Strapping Units. D. (Refer to Figure 8, Detail A.) Install two CSU-3100 Configuration Strapping Units in the IAPS card cage. (Refer to the Model 525 Maintenance Manual, Chapter 34, Collins Pro Line 21 Integrated Avionics Processor System - Maintenance Practices.) 12. Install one 822-2189-010 GPS-4000S receiver(s). (Refer to the Model 525 Maintenance Manual, Chapter 34, Collins FMS-3000 Flight Management System - Maintenance Practices.) NOTE: Airplanes with dual FMS will install two GPS-4000S. 13. Remove the maintenance warning tags and connect external electrical power. Revision 2 - May 30, 2014 Page 9
14. Do the Collins FMS-3000 flight management system functional test. (Refer to the Model 525 Maintenance Manual, Chapter 34, Collins FMS-3000 Flight Management System - Adjustment/Test.) 15. Pressurize the airplane to check for leaks around the installed antenna(s). (Refer to the Model 525 Maintenance Manual, 21, Pressurization Control - Adjustment/Test.) 16. Install the access panels that were removed to install this modification. (Refer to the Model 525 Maintenance Manual, Chapter 6, Access Plates and Panels Identification - Description and Operation.) 17. Install the headliner and sidewalls. (Refer to the Model 525 Maintenance Manual, Chapter 25, Headliner and Sidewall Maintenance Practices.) 18. Install the furnishing that were removed to install this modification. (Refer to the applicable sections of the Model 525 Maintenance Manual and Interior Maintenance Manual and Illustrated Parts Catalog.) 19. Update the CJ1+ FAA Approved Airplane Flight Manual (525FMB). NOTE: Look at the configuration codes listed in the applicable supplement and/or in Section 1 of the FAA Approved Airplane Flight Manual to make sure all changed crew procedures or limitations are complied with. A. Make sure that Supplement 22, Revision 4 or later is inserted into the CJ1+ FAA Approved Airplane Flight Manual (525FMB). 20. Make sure the flight crew receives the Flight Crew Operations Summary, which shows the operational changes that are a result of the accomplishment of this service bulletin. 21. (Owners/Operators) Go to the Rockwell Collins website and update your subscriptions for the FMS group from J6 to J7. 22. 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. Page 10 Revision 2 - May 30, 2014
Figure 1. (-0600 thru -0640) Left GPS Antenna Modification (Sheet 1) Revision 2 - May 30, 2014 Page 11
Figure 1. (-0600 thru -0640) Left GPS Antenna Modification (Sheet 2) Page 12 Revision 2 - May 30, 2014
Figure 1. (-0600 thru -0640) Left GPS Antenna Modification (Sheet 3) Revision 2 - May 30, 2014 Page 13
Figure 2. (-0600 thru -0640 with dual FMS and a teardrop GPS antenna) Right Antenna Modification (Sheet 1) Page 14 Revision 2 - May 30, 2014
Figure 2. (-0600 thru -0640 with dual FMS and a teardrop GPS antenna) Right Antenna Modification (Sheet 2) Revision 2 - May 30, 2014 Page 15
Figure 3. (-0600 thru -0640 with dual FMS and a rectangular GPS antenna) Right Antenna Modification (Sheet 1) Page 16 Revision 2 - May 30, 2014
Figure 3. (-0600 thru -0640 with dual FMS and a rectangular GPS antenna) Right Antenna Modification (Sheet 2) Revision 2 - May 30, 2014 Page 17
Figure 3. (-0600 thru -0640 with dual FMS and a rectangular GPS antenna) Right Antenna Modification (Sheet 3) Page 18 Revision 2 - May 30, 2014
Figure 4. (-0641 thru -0679 and -0681 thru -0684) Left GPS Antenna Modification (Sheet 1) Revision 2 - May 30, 2014 Page 19
Figure 5. (-0641 thru -0679 and -0681 thru -0684) Right GPS Antenna Modification (Sheet 1) Page 20 Revision 2 - May 30, 2014
Figure 6. WAAS Wiring Modification (Sheet 1) Revision 2 - May 30, 2014 Page 21
Figure 6. WAAS Wiring Modification (Sheet 2) Page 22 Revision 2 - May 30, 2014
Figure 7. (Airplanes with dual FMS) WAAS Wiring Modification (Sheet 1) Revision 2 - May 30, 2014 Page 23
Figure 7. (Airplanes with dual FMS) WAAS Wiring Modification (Sheet 2) Page 24 Revision 2 - May 30, 2014
Figure 8. IAPS Card Cage Modification (Sheet 1) Revision 2 - May 30, 2014 Page 25
Figure 8. IAPS Card Cage Modification (Sheet 2) Page 26 Revision 2 - May 30, 2014
MATERIAL INFORMATION Order the kit below to install this modification. NEW P/N QUAN- TITY KEY WORD -0 1 Kit, consisting of the following parts: WHERE USED OLD P/N CI428-410 1 Antenna CI401-460, 822-1330- 001, or 011-00147-00 INSTRUCTIONS/ DISPOSITION Discard MS20426AD3-4A 8 Rivet Same Discard MS24693S54 4 Screw MS24694C54 Discard S1367-2-6 2 Terminal MS25036-103 1 Terminal NGS505 M27500-22ML2T08 180 inches Electrical Wire marked - 30PN342-11APN700 (WHT) 31PN342-11BPN700 (BLU) M39029/57-354 2 Socket PN342 M81044/12-22-9 48 inches Electrical Wire marked - 4DPN700-5DPN703 M81044/12-22-9 72 inches Electrical Wire marked - 9CPN703-NGS505 M81824/1-2 1 Splice NAS1473A08N 4 Nutplate NAS1473A3 Discard S2974-8 8 Shield Termination 030-2259-000 4 Contact PN700 PN703 MS3367-1-0 6 Tie Strap Same S2209-1 20 Tie Strap Same TC4001 2 Capnut 1 Instructions Revision 2 - May 30, 2014 Page 27
(Airplanes with dual Rockwell Collins FMS) Order the kit that follows in addition to the -0 Kit. NEW P/N QUAN- TITY KEY WORD WHERE USED OLD P/N INSTRUCTIONS/ DISPOSITION -1 1 Kit, consisting of the following parts: CI428-410 1 Antenna CI401-460, 822-1330- 001, or 011-00147-00 Discard MS20426AD3-4A 8 Rivet Same Discard MS24693S54 4 Screw MS24694C54 Discard S1367-2-6 8 Terminal MS25036-103 1 Terminal TGS503 M27500-22ML2T08 48 inches Electrical Wire marked - 11APT700-9PN702 (WHT) 11BPT700-10PT702 (BLU) M27500-22ML2T08 167 inches Electrical Wire marked - 30PN343-*FPB312 (WHT) 31PN343-YPB312 (BLU) M27500-22ML2T08 350 inches Electrical Wire marked - XJB312-MJA305 (WHT) YJB312-NJA305 (BLU) M27500-22ML2T08 144 inches Electrical Wire marked - MPA305-9JT702 (WHT) NPA305-10JT702 (BLU) M39029/4-110 4 Pin M39029/5-115 4 Socket M39029/57-354 4 Socket JT702 PN343 M39029/58-360 2 Pin PT702 M81044/12-22-9 48 inches Electrical Wire marked - 5DPT703-4DPT700 M81044/12-22-9 48 inches Electrical Wire marked - 9CPT703-TGS503 M81824/1-2 1 Splice NAS1473A08N 4 Nutplate NAS1473A3 Discard S2974-8 9 Shield Termination 030-2259-000 4 Contact PT703 PT700 MS3367-1-0 125 Tie Strap Same S2209-1 20 Tie Strap Same Page 28 Revision 2 - May 30, 2014
NEW P/N QUAN- TITY KEY WORD WHERE USED OLD P/N INSTRUCTIONS/ DISPOSITION TC4001 2 Capnut None 1 Instructions (Airplanes -0600 thru -0640) Order the kit that follows in addition to the -0 Kit. NOTE: Order one -2 Kit if you have a single Rockwell Collins FMS, order two -2 Kits if you have dual Rockwell Collins FMS. NEW P/N QUAN- TITY KEY WORD OLD P/N INSTRUCTIONS/ DISPOSITION -2 1 Kit, consisting of the following parts: CM3827AD3-3 8 Rivet CM3827AD4-3.5 29 Rivet Same Discard CM3827AD4-5 28 Rivet Same Discard S3898A6-4N 4 Rivet 9190168-12 1 Doubler 9123029-3 Discard 1 Instructions In addition to the above kit(s), it will be necessary to order the parts that follow. NEW P/N QUAN- TITY KEY WORD OLD P/N INSTRUCTIONS/ DISPOSITION 822-0883-038 1 FMC-3000 Computer 822-0883-031 Return to Cessna for Modification 822-1361-412 2 IOC Module 822-1361-410, 822-1361-411 Return to Cessna for Modification 822-1484-228 2 OCM-3100 822-1484-201 Return to Cessna for Deposit Credit 822-2189-010 1 GPS-4000S 822-1377-001 Return to Cessna for Modification NOTE: Airplanes with dual Rockwell Collins FMS will need to upgrade two FMC-3000 Computers and two GPS-4000S. NOTE: Operators: The existing FMC-3000, IOC Module, and GPS-4000S can be modified. Contact the Cessna Service Parts & Programs Repair Team for RMA to schedule your unit at telefax 1-316-206-4068 or e-mail citationrepair@cessna.textron.com available 8:00 4:30 CST weekdays. Advance notification and coordination is required for Cessna Service Parts & Programs Repair Team to effectively schedule units, ship to supplier, and arrange return. The expected turn time for the supplier supporting this service document is five to seven days. Revision 2 - May 30, 2014 Page 29
ATTACHMENT 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. Refer to Airplane Flight Manual Supplement 22, Revision 4 or later. Refer to Rockwell Collins Operator's Guide (part number 523-0810168-001117 or later) for LPV annunciations and other FMS v4.0 features. NOTE: Rockwell Collins recommends at an available opportunity that you make sure that the proper annunciations are displayed for an LPV approach.
OWNER ADVISORY TITLE NAVIGATION - COLLINS FMS-3000 WIDE AREA AUGMENTATION SYSTEM (WAAS) WITH FMS 4.0 SOFTWARE UPDATES TO: Cessna Aircraft Owner REASON Amoreprecise satellite based augmentation system is required to fly LP, LPV, LNAV, and VNAV approaches. COMPLIANCE OPTIONAL. This service bulletin can be accomplished at the discretion of the owner. LABOR HOURS WORK PHASE Modification MAN-HOURS As Necessary MATERIAL AVAILABILITY PART NUMBER AVAILABILITY COST -0 * * -1 * * -2 * * 822-0883-038 * * 822-1361-412 * * 822-1484-228 * * 822-2189-010 * * *Contact the Cessna Service Parts & Programs Repair Team for RMA to schedule your unit at telefax 1-316-206-4068 or e-mail citationrepair@cessna.textron.com available 8:00 4:30 CST weekdays. Advance notification and coordination is required for Cessna Service Parts & Programs Repair Team to effectively schedule units, ship to supplier, and arrange return. The expected turn time for the supplier supporting this service document is five to seven days. * Please contact Cessna Service Parts & Programs 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: dirop@cessna.textron.com or telefax at 1-316-517-7711. Based on availability and lead times, parts may require advanced scheduling. August 14, 2013 Page 1 of 1 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-5800 This document contains technical data and is subject to U.S. export regulations. This information has been exported from the United States in accordance with export administration regulations. Diversion contrary to U.S. law is prohibited. ECCN: 9E991 COPYRIGHT 2013