REVISION TRANSMITTAL This sheet transmits Revision 2 to, which: A. Adds the CI401-460 GPS Antenna to Step 10A and Step 10B. B. Adds the CI401-460 GPS Antenna to Figure 5. C. Adds the CI401-460 GPS Antenna to Figure 7. 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 February 25/2014 Original Issue - January 14, 2010 Revision 2 - February 25, 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. 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 - February 25, 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 EFFECTIVITY REASON MODEL SERIAL NUMBERS 525B (CJ3) -0001 thru -0262, -0264 thru -0293 The equivalent of this service bulletin has been incorporated on production airplanes -0263 and -0294 and On. NOTE: Airplanes -0001 thru -0134 must incorporate SB525B-34-04 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 - February 25, 2014 Page 1 of 31 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 -0001 THRU -0134 KIT NUMBER WEIGHT CHANGE RESULTANT MOMENT MOMENT/100-0 + 0.81 pounds + 197.23 inch-pounds + 1.97 inch-pounds -1 + 0.16 pounds + 0.69 inch-pounds + 0.01 inch-pounds -2 Negligible Negligible Negligible AIRPLANES -0135 THRU -0262 AND -0264 THRU -0293 KIT NUMBER WEIGHT CHANGE RESULTANT MOMENT MOMENT/100-0 + 0.88 pounds + 207.32 inch-pounds + 2.07 inch-pounds -1 + 0.23 pounds + 11.52 inch-pounds + 0.12 inch-pounds REFERENCES Cessna Model 525B Maintenance Manual Cessna Model 525B Wiring Diagram Manual Cessna Model 525A/525B Structural Repair Manual PUBLICATIONS AFFECTED Cessna Model 525B Maintenance Manual Cessna Model 525B Wiring Diagram Manual Cessna Citation CJ3 FAA Approved Airplane Flight Manual (525BFM) Page 2 Revision 2 - February 25, 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 10, Detail A.) Remove two IOC modules and FMC-3000 cards from the IAPS card cage. (Refer to the Model 525B 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 525B Maintenance Manual, Chapter 34, Collins FMS-3000 Flight Management System - Maintenance Practices.) 5. Remove the furnishing from the right side of the airplane. (Refer to the applicable sections of the Model 525B Maintenance Manual and Interior Maintenance Manual and Illustrated Parts Catalog.) 6. Remove the headliner and sidewalls. (Refer to the Model 525B Maintenance Manual, Chapter 25, Headliner and Sidewall Maintenance Practices.) 7. Remove the floorboards that follow: (Refer to the Model 525B Maintenance Manual, Chapter 6, Access Plates and Panels Identification - Description and Operation.) 262GR 262GT 262FT 262ET 262DT 262CT 262BT 262AT 252DT 242AT 8. (Airplanes -0001 thru -0134) 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 NOTE: Contact Team CJ if a doubler other than a 9123029-3 Doubler is installed in the airplane for the left GPS antenna. (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 - February 25, 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 sheetmetal 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 525A/525B Structural Repair Manual, Chapter 51, Protective Treatment of Metal - Description and Operation.) Use Type I, Class B 2 Sealant to apply a fay seal to the 9190168-12 Doubler. (Refer to the Model 525B 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 B 2 Sealant to fill the open holes. (Refer to the Model 525B 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 525B 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 525B 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 525B 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 525B Maintenance Manual, Chapter 20, Adhesive and Solvent Bonding - Maintenance Practices.) Page 4 Revision 2 - February 25, 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 9123029-3 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 525B 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 525B 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 - February 25, 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 sheetmetal fasteners. 13 (Refer to Figure 1, 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 525A/525B 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 525B 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 525B 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 525B Maintenance Manual, Chapter 20, Fuel, Weather, Pressure, and High Temperature Sealing - Maintenance Practices.) Page 6 Revision 2 - February 25, 2014
(g) Use Type I Class B2 Sealant to overcoat the nutplates. (Refer to the Model 525B 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 525B 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 9123029-3 Doubler NOTE: Contact Team CJ if a doubler other than a 9123029-3 Doubler is installed in the airplane for the left GPS antenna. Revision 2 - February 25, 2014 Page 7
(b) (c) (d) (e) (f) (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 sheetmetal 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 525A/525B 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 525B 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 525B Maintenance Manual, Chapter 20, Fuel, Weather, Pressure, and High Temperature Sealing - Maintenance Practices.) 17 Install four NAS1473A08N Nutplates with eight MS20426AD3-4A Rivets. (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 525B 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 525B Maintenance Manual, Chapter 20, Fuel, Weather, Pressure, and High Temperature Sealing - Maintenance Practices.) Use Type I Class B2 Sealant to overcoat the nutplates. (Refer to the Model 525B Maintenance Manual, Chapter 20, Fuel, Weather, Pressure, and High Temperature Sealing - Maintenance Practices.) Page 8 Revision 2 - February 25, 2014
(g) Use Type V, Class A adhesive to fill the holes in the top of the antenna. (Refer to the Model 525B Maintenance Manual, Chapter 20, Adhesive and Solvent Bonding - Maintenance Practices.) 9. (Airplanes -0135 thru -0154) 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 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 525B 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 525B 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 525B 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 525B 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 525B Maintenance Manual, Chapter 20, Adhesive and Solvent Bonding - Maintenance Practices.) B. (Airplanes that have dual Rockwell Collins FMS.) (Refer to Figure 6, View A-A.) Install the right GPS antenna. (1) Remove and discard the parts that follow: Four MS27039-1-17 Screws One 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 525B 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 525B 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 525B 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 525B 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 525B Maintenance Manual, Chapter 20, Adhesive and Solvent Bonding - Maintenance Practices.) Revision 2 - February 25, 2014 Page 9
10. (Airplanes -0155 thru -0262 and -0264 thru -0293) Install the GPS antenna(s). A. (Refer to Figure 5, 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 525B 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 525B 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 525B 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 525B 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 525B Maintenance Manual, Chapter 20, Adhesive and Solvent Bonding - Maintenance Practices.) B. (Airplanes that have dual Rockwell Collins FMS.) (Refer to Figure 7, 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 525B 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 525B 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 525B 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 525B 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 525B Maintenance Manual, Chapter 20, Adhesive and Solvent Bonding - Maintenance Practices.) 11. (Refer to Figure 8.) Install the electrical wiring. A. Add the electrical wiring between the GPS1 (PT700) and the aft pressure bulkhead connector (PA700). Page 10 Revision 2 - February 25, 2014
B. Add the electrical wiring between the GPS1 (PT700) and the PT703 connector. C. Add the electrical wiring between the PT703 connector and the TGS508 ground stud. D. Add the electrical wiring between the aft pressure bulkhead connector (JA700) and the forward pressure bulkhead connector (JB402). E. Add the electrical wiring between the forward pressure bulkhead connector (PB402) and the IAPS (PN342). F. (Airplanes that have dual Rockwell Collins FMS) (Refer to Figure 9.) Install the electrical wiring. (1) Add the electrical wiring between the GPS2 (PN710) and the PN702 connector. (2) Add the electrical wiring between the GPS2 (PN710) and the PN709 connector. (3) Add the electrical wiring between the PN709 connector and the NGS302 ground stud. (4) Add the electrical wiring between the PN343 connector and the JN702 connector. 12. (Refer to Figure 10, Detail A.) Install two 822-1361-406 IOC Modules and one 822-0883-038 FMC-3000 Computer cards in the IAPS card cage. (Refer to the Model 525B Maintenance Manual, Chapter 34, Collins Pro Line 21 Integrated Avionics Processor System - Maintenance Practices.) NOTE: Airplanes with dual Rockwell Collins FMS will install two FMC-3000 Computers. A. (Refer to Figure 10, Detail A.) Remove two CSU-3100 Configuration Strapping Units from the IAPS card cage. (Refer to the Model 525B Maintenance Manual, Chapter 34, Collins Pro Line 21 Integrated Avionics Processor System - Maintenance Practices.) B. (Refer to Figure 10, Detail B.) Remove one OCM-3100 from each CSU-3100 Configuration Strapping Unit. C. (Refer to Figure 10, Detail B.) Install one 822-1484-228 OCM-3100 on each CSU-3100 Configuration Strapping Units. D. (Refer to Figure 10, Detail A.) Install two CSU-3100 Configuration Strapping Units in the IAPS card cage. (Refer to the Model 525B Maintenance Manual, Chapter 34, Collins Pro Line 21 Integrated Avionics Processor System - Maintenance Practices.) 13. Install one 822-2189-010 GPS-4000S receiver(s) (Refer to the Model 525B Maintenance Manual, Chapter 34, Collins FMS-3000 Flight Management System - Maintenance Practices.) NOTE: Airplanes with dual Rockwell Collins FMS will install two GPS-4000S. 14. Remove the maintenance warning tags and connect external electrical power. 15. Do the Collins FMS-3000 flight management system functional test. (Refer to the Model 525B Maintenance Manual, Chapter 34, Collins FMS-3000 Flight Management System - Adjustment/Test.) 16. Pressurize the airplane to check for leaks around the installed antenna(s). (Refer to the Model 525B Maintenance Manual, 21, Pressurization Control - Adjustment/Test.) 17. Install the access panels that were removed to install this modification. (Refer to the Model 525B Maintenance Manual, Chapter 6, Access Plates and Panels Identification - Description and Operation.) 18. Install the headliner and sidewalls. (Refer to the Model 525B Maintenance Manual, Chapter 25, Headliner and Sidewall Maintenance Practices.) 19. Install the furnishing that were removed to install this modification. (Refer to the applicable sections of the Model 525B Maintenance Manual and Interior Maintenance Manual and Illustrated Parts Catalog.) Revision 2 - February 25, 2014 Page 11
20. Update the CJ3 FAA Approved Airplane Flight Manual (525BFM). 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 25, Revision 3 or later is inserted into the CJ3 FAA Approved Airplane Flight Manual (525BFM). 21. 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. 22. (Owners/Operators) Go to the Rockwell Collins website and update your subscriptions for the FMS group from J6 to J7. 23. 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 12 Revision 2 - February 25, 2014
Figure 1. (Airplanes -0001 thru -0134) Left GPS Antenna Modification (Sheet 1) Revision 2 - February 25, 2014 Page 13
Figure 1. (Airplanes -0001 thru -0134) Left GPS Antenna Modification (Sheet 2) Page 14 Revision 2 - February 25, 2014
Figure 1. (Airplanes -0001 thru -0134) Left GPS Antenna Modification (Sheet 3) Revision 2 - February 25, 2014 Page 15
Figure 2. (-0001 thru -0134 with dual FMS and a teardrop GPS antenna) Right Antenna Modification (Sheet 1) Page 16 Revision 2 - February 25, 2014
Figure 2. (-0001 thru -0134 with dual FMS and a teardrop GPS antenna) Right Antenna Modification (Sheet 2) Revision 2 - February 25, 2014 Page 17
Figure 3. (-0001 thru -0134 with dual FMS and a rectangular GPS antenna) Right Antenna Modification (Sheet 1) Page 18 Revision 2 - February 25, 2014
Figure 3. (-0001 thru -0134 with dual FMS and a rectangular GPS antenna) Right Antenna Modification (Sheet 2) Revision 2 - February 25, 2014 Page 19
Figure 3. (-0001 thru -0134 with dual FMS and a rectangular GPS antenna) Right Antenna Modification (Sheet 3) Page 20 Revision 2 - February 25, 2014
Figure 4. (Airplanes -0135 thru -0154) Left GPS Antenna Modification (Sheet 1) Revision 2 - February 25, 2014 Page 21
Figure 5. (Airplanes -0155 thru -0262 and -0264 thru -0293) Left GPS Antenna Modification (Sheet 1) Page 22 Revision 2 - February 25, 2014
Figure 6. (Airplanes -0135 thru -0154) Left GPS Antenna Modification (Sheet 1) Revision 2 - February 25, 2014 Page 23
Figure 7. (Airplanes -0155 thru -0262 and -0264 thru -0293) Right GPS Antenna Modification (Sheet 1) Page 24 Revision 2 - February 25, 2014
Figure 8. WAAS Wiring Modification (Sheet 1) Revision 2 - February 25, 2014 Page 25
Figure 9. (Airplanes with dual FMS) WAAS Wiring Modification (Sheet 1) Page 26 Revision 2 - February 25, 2014
Figure 10. IAPS Card Cage Modification (Sheet 1) Revision 2 - February 25, 2014 Page 27
Figure 10. IAPS Card Cage Modification (Sheet 2) Page 28 Revision 2 - February 25, 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 MS25036-103 1 Terminal TGS508 MS3367-1-0 120 Tie Strap Same M27500-22ML2T08 135 inches Electrical Wire marked - 15PB402-55PN342 (WHT) 16PB402-56PN342 (BLU) M27500-22ML2T08 174 inches Electrical Wire marked - 11APT700-EPA700 (WHT) 11BPT700-FPA700 (BLU) M27500-22ML2T08 384 inches Electrical Wire marked - EJA700-15JB402 (WHT) FJA700-16JB402 (BLU) M39029/4-110 2 Pin PA700 M39029/57-354 2 Socket PN342 JB402 M39029/58-360 2 Pin PB402 M39029/5-115 2 Socket JA700 M81044/12-22-9 24 inches Electrical Wire marked - 5DPT703-4DPT700 M81044/12-22-9 50 inches Electrical Wire marked - 9CPT703-TGS508 M81824/1-2 1 Splice NAS1473A08N 4 Nutplate NAS1473A3 Discard S1367-2-6 6 Terminal S2209-1 16 Tie Strap Same S2974-8 6 Shield Termination Revision 2 - February 25, 2014 Page 29
NEW P/N QUAN- TITY KEY WORD WHERE USED 030-2259-000 4 Contact PT700 PT703 1 Instructions OLD P/N INSTRUCTIONS/ DISPOSITION (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 MS25036-103 1 Terminal NGS302 MS3367-1-0 60 Tie Strap Same M27500-22ML2T08 144 inches Electrical Wire marked - 11APN710-10PN702 (WHT) 11BPN710-11PN702 (BLU) M27500-22ML2T08 200 inches Electrical Wire marked - 55PN343-10JN702 (WHT) 56PN343-11JN702 (BLU) M39029/57-354 4 Socket PN343 JN702 M39029/58-360 2 Pin PN702 M81044/12-22-9 26 inches Electrical Wire marked - 5DPN709-4DPN710 M81044/12-22-9 108 inches Electrical Wire marked - 9CPN709-NGS302 M81824/1-2 1 Splice NAS1473A08N 4 Nutplate NAS1473A3 Discard S1367-2-6 4 Terminal S2209-1 20 Tie Strap Same S2974-8 4 Shield Termination 030-2259-000 4 Contact PN709 PN710 1 Instructions Page 30 Revision 2 - February 25, 2014
(Airplanes -0001 thru -0134) 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 tocessnafor Modification 822-1361-406 2 IOC Module 822-1361-405 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 - February 25, 2014 Page 31
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 25, Revision 3 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 * * 822-1361-406 * * 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