Revision 3 REVISION TRANSMITTAL SHEET This sheet transmits Revision 3 to, which: A. Removes the 453-5000-999 ELT from the kits and makes it a stand alone part. B. Changes part numbers within the kits. NOTE: This revision replaces the original issue of 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 Oct 20/2003 Revision 1 Jun 7/2005 Revision 2 Apr 10/2007 Revision 3 Jun 11/2010
Revision 2 REVISION TRANSMITTAL SHEET This sheet transmits Revision 2 to, which: A. Adds the engineering drawing number for the ELT Access Panel Installation in the REFERENCES section B. Adds instructions in Step 7A for installation of an access panel C. Adds a -6 Kit to the MATERIAL INFORMATION section for access panel installation NOTE: This revision replaces the original issue of 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 Oct 20/2003 Revision 1 Jun 7/2005 Revision 2 Apr 10/2007
Revision 1 REVISION TRANSMITTAL SHEET 1. This sheet transmits Revision 1 to. A. Changes the EFFECTIVITY from -0001 and On to -0001 thru -0306. B. Adds NOTE to tell that airplanes -0307 and On which were previously covered by this service bulletin are now covered by SB560-25-31. C. Adds NOTE to tell that it is the owner's responsibility to acquire a Mode S code before this service bulletin is started. D. Changes the REASON statement. E. Adds CONSUMABLE MATERIAL section. F. Adds the Sartech Beacon Tester to the TOOLING section. G. Adds Cessna Engineering Drawings 9690368, 9603067, 9602614 and 9690640 to the REFERENCE section and the ACCOMPLISHMENT INSTRUCTIONS. H. Adds instructions to remove the existing ELT and components (if installed), install the ELT cable assembly, modify the instrument panel, install a NAV interface unit (if necessary) and modify the aft pressure bulkhead (if necessary). I. Adds instructions to disconnect the ELT circuit breaker (if installed) and program the ELT (airplanes with NAV interface). J. Changes Step 4 to make it apply to airplanes that are replacing a Artex ELT. K. Changes Step 5 to make it apply to airplanes that are replacing a Pointer ELT. L. Changes Step 6 to make it apply to airplanes that do not have an ELT installed. M. Changes the operational test of the ELT. N. Adds 9690460-1 Cable Assembly to the -0 Kit and the 9602614-1 Cable Assembly to the -1 Kit. O. Adds rivets to the -0 and -1 Kits. P. Changes the S3100-96 and S3100-97 ELT Transmitter to the 453-5000-999 ELT Transmitter in the -0 and -1 Kits. Q. Adds the 452-0010 Remote Switch and attaching hardware to the -0 and -1 Kits. R. Adds the 9693068-7 Plug Assembly to the -0 Kit. S. Removes the 9693064 and 9693067 drawings from the -0 and -1 Kits. T. Changes the -0 Kit to apply only to airplanes with NAV interface that have a Pointer ELT installed. U. Changes the -1 Kit to apply only to airplanes without NAV interface that have a Pointer ELT installed. V. Adds the -2 Kit which applies only to airplanes without NAV interface that do not currently have an ELT installed. W. Adds the -3 Kit which applies only to airplanes with NAV interface that do not currently have an ELT installed. X. Adds the -4 Kit which applies only to airplanes with NAV interface that have an Artex ELT installed per SB560-25-19.
TITLE EQUIPMENT/FURNISHINGS - ARTEX C406-2 THREE-FREQUENCY EMERGENCY LOCATOR TRANSMITTER (ELT) EFFECTIVITY MODEL SERIAL NUMBERS 560-0001 thru -0306 NOTE: This Service Bulletin may only be accomplished at a Cessna owned or authorized Service Center. NOTE: All model 560 airplanes were previously covered by this service bulletin. Airplanes -0307 and On will now need to comply with SB560-25-31 when installing a three-frequency ELT. This service bulletin is for airplanes -0001 thru -0306 only. NOTE: (Airplanes with NAV interface) It is the owner's responsibility to acquire a Mode S code before this service bulletin is started. The Mode S code is necessary to configure the Artex ELT. REASON To install an ELT to comply with FAA requirements. DESCRIPTION This service bulletin provides parts and instructions to install a three frequency emergency locator transmitter. COMPLIANCE OPTIONAL. This service bulletin may be accomplished at the discretion of the owner. FLIGHT CREW OPERATIONS No Change. 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. Revision 3 - Jun 11/2010 Page 1 of 14 Cessna Aircraft Company, Marketing Division, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-6000, Fax 1-316-517-8500 COPYRIGHT 1999
MANPOWER WORK PHASE MAN-HOURS Modification * MATERIAL - Cost and Availability PART NUMBER AVAILABILITY COST -0 * * -1 * * -2 * * -3 * * -4 * * -5 * * -6 * * 453-5000-999 * * * Refer to the attached Service Bulletin Supplemental Data sheet for man-hours, material cost and availability, and warranty information. CONSUMABLE MATERIAL The following materials, or equivalent, may be necessary for the accomplishment of this service bulletin. NAME NUMBER MANUFACTURER USE Color Chemical Film Treatment Fuel and Corrosion Resistant Primer Alodine 1203 10-P1-4 Base, EC-108 Catalyst, TR-19 Thinner Alchem Products Inc. Brookside Ave Ambler, PA 19002 Dexter Crown Metro Echelon Road Donaldson Center Greenville, SC 29606 Protective treatment of radio and instrument panels. Corrosion protection primer for retreating radio and instrument panels. TOOLING The following tool will be required for airplanes with NAV interface. NAME NUMBER MANUFACTURER USE Sartech Beacon Tester 453-0131 (or equivalent) Artex PO Box 1270 Canby, OR 97013 ELT functional test and programming. CHANGE IN WEIGHT AND BALANCE MODEL 560 560 560 SUBKIT -0 (with GNS-XLS, GNS-1ESP or GNS-1CSP) -0 (with UNSK-1K or UNS-1L) -0 (1C615 and Honeywell FMS) Revision 3 - Jun 11/2010 Page 2
WEIGHT INCREASE +11.42 pounds +11.20 pounds +11.17 pounds RESULTANT MOMENT +4983.65 inch-pounds +4995.04 inch-pounds +4872.89 inch-pounds MOMENT/100 +49.84 inch-pounds +48.95 inch-pounds +48.73 inch-pounds MODEL 560 SUBKIT -1 WEIGHT INCREASE +5.28 pounds RESULTANT MOMENT +2412.23 inch-pounds MOMENT/100 +24.12 inch-pounds MODEL 560 SUBKIT -2 WEIGHT INCREASE +9.92 pounds RESULTANT MOMENT +4394.23 inch-pounds MOMENT/100 +43.94 inch-pounds MODEL 560 560 560 SUBKIT -3 (with GNS-XLS, GNS-1ESP -3 (with UNSK-1K or UNS-1L) -3 (1C615 and Honeywell FMS) or GNS-1CSP) WEIGHT INCREASE +16.12 +15.90 +15.87 RESULTANT MOMENT +7116.28 inch-pounds +7027.67 inch-pounds +7005.52 inch-pounds MOMENT/100 +71.16 inch-pounds +70.28 inch-pounds +70.06 inch-pounds MODEL 560 SUBKIT -4 WEIGHT INCREASE +4.20 pounds RESULTANT MOMENT +1918.01 inch-pounds MOMENT/100 +19.18 inch-pounds MODEL 560 SUBKIT -5 WEIGHT INCREASE -0.12 pounds RESULTANT MOMENT -159.19 inch-pounds MOMENT/100-1.59 inch-pounds MODEL 560 SUBKIT -6 WEIGHT INCREASE +0.97 pounds RESULTANT MOMENT +468.41 inch-pounds MOMENT/100 +4.68 inch-pounds Revision 3 - Jun 11/2010 Page 3
REFERENCES The following Cessna Engineering Drawings and documents are required to accomplish this modification: NOTE: The latest revision of each document and all applicable amendments, drawing change notices, and parts lists released at the time of modification must be used. PUBLICATIONS AFFECTED DRAWING NUMBER DRAWING TITLE S3237 CUTOUT - SWITCH 9602614 CABLEASSY-ARTEX110-406ELTW/ONAV 9690364 ELT MODIFICATION INSTL 9690460 LOCATOR BEACON-ARTEX ELT C406-2 W/NAV I/F MOD 9603067 AIRCRAFT SYSTEMS PROGRAMMING-ARTEX C406-2 ELT (560) 9690364 ELT MODIFICATION INSTALLATION 9690367 EMERGENCY LOCATOR TRANSMITTER ANTENNA INSTL (MOD) 9690368 110-406 ELT MOD INSTALLATION MODELS 550 & 560 9690648 ELT ACCESS PANEL INSTALLATION Cessna Model 560 Illustrated Parts Catalog Cessna Model 560 Maintenance Manual ACCOMPLISHMENT INSTRUCTIONS 2. 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. 3. (Airplanes that are replacing a Pointer ELT) Go to Step 5. 4. (Airplanes that do not have an ELT installed) Go to Step 6. 5. (Airplanes that are replacing an Artex ELT) Install the ELT and ELT antenna. A. Disengage the ELT circuit breaker. B. Remove the ELT, ELT antenna and ELT antenna doubler. Keep the screws and washers that attach the ELT to the mounting tray and shelf. (Refer to the Maintenance Manual, Chapter 25, Artex ELT110-4, Emergency Locator Transmitter System - Maintenance Practices.) NOTE: Only the ELT itself must be removed. The rack and hardware will be used for the new installation. C. Remove and discard the ELT cable assembly. Revision 3 - Jun 11/2010 Page 4
D. Install the ELT with the kept hardware. (Refer to Cessna Engineering Drawing 9690364) E. (Airplanes with NAV interface) Install the NAV interface unit. (Refer to Cessna Engineering Drawing 9690364.) F. Install the ELT antenna. (Refer to Cessna Engineering Drawing 9690367-1.) G. Go to Step 7. 6. (Airplanes that are replacing a Pointer ELT) Install the ELT and ELT antenna. A. Disengage the ELT circuit breaker. B. Remove and discard the ELT, ELT antenna and ELT antenna doubler. (Refer to the Maintenance Manual, Chapter 25, C-3000 Locator Beacon - Maintenance Practices.) C. Remove and discard the ELT cable assembly. D. Install the ELT. (Refer to Cessna Engineering Drawing 9690364) E. (Airplanes with NAV interface) Install the NAV interface unit. (Refer to Cessna Engineering Drawing 9690364.) F. Install the ELT antenna. (Refer to Cessna Engineering Drawing 9690367-1.) G. Go to Step 7. 7. (Airplanes that do not already have an ELT installed) Install the ELT transmitter, ELT Antenna, and ELT switch. A. Do a modification to one side of the saddle assembly for an access panel. (Refer to Cessna Engineering Drawing 9690648.) B. Install the ELT. (Refer to Cessna Engineering Drawing 9690364.) C. (Airplanes with NAV interface) Install the NAV interface unit. (Refer to Cessna Engineering Drawing 9690364.) D. Install the ELT antenna. (Refer to Cessna Engineering Drawing 9690367-1.) E. Modify the aft pressure bulkhead. (Refer to Cessna Engineering Drawing 9690368.) (1) Deburr sharp edges and apply color chemical film treatment and corrosion resistant primer to the bare metal edges. (Refer to the Maintenance Manual, Chapter 20, Interior Finish - Cleaning/Painting.) F. Remove the right hand instrument panel. (Refer to the Maintenance Manual, Chapter 31, Instrument Panel - Maintenance Practices.) G. Do a modification to the right hand instrument panel. (Refer to Cessna Engineering Drawings 9690368 and S3237.) H. Install the right hand instrument panel. (Refer to the Maintenance Manual, Chapter 31, Instrument Panel - Maintenance Practices.) 8. Engage the ELT circuit breaker. 9. Install the ELT cable assembly. (Refer to Cessna Engineering Drawing 9690460 or 9602614.) 10. Remove maintenance warning tags and connect electrical power to the airplane by connecting the battery and external power. 11. (Airplanes with NAV interface) Configure the ELT. (Refer to Cessna Engineering Drawing 9603067-1.) Revision 3 - Jun 11/2010 Page 5
12. Do a test of the ELT system. A. Do a test of the ELT transmitter. NOTE: Do the ELT transmission test within the first five minutes after the hour. NOTE: To prevent satellite detection, do not keep the remote switch in the on position for more than 15 seconds. During the first 15 seconds, the satellite system will process the 406.025 mhz signal as a test and ignore the transmission. If the transmission is longer than 15 seconds, the satellite system will process the transmission as a real distress signal. (1) Put the avionics power switches to the ON position. (2) Tune the number one or number two comm radio to 121.5 and set the appropriate comm and cockpit speaker on the audio panel. Apply power to FMS 1 and initialize a valid GPS position. (3) Turn the ELT switch to the ON position. (a) (b) (c) (d) Wait for one second. NOTE: Observe the LED light when the switch is moved to the ARM position. Move the switch to the ARM position. If the LED light stays on for one second after the switch is moved to the ARM position, then no faults exist. If a problem is detected then the LED will provide a coded signal after the one second pulse. (4) Disengage the ELT/NAV INTERFACE circuit breaker in the aft power J-Box for a minimum of one minute. B. (Airplanes with NAV interface) Retrieve the 15 bit Hex ID. (Refer to Cessna Engineering Drawing 9603067 for test set-up procedures.) NOTE: For the purpose of identifying the 15 bit Hex ID, the FMS must stay off. (1) Engage the ELT/NAV INTERFACE circuit breaker. (2) Move the ELT switch to the ON position. NOTE: To prevent satellite detection, do not keep the remote switch in the on position for more than 15 seconds. During the first 15 seconds, the satellite system will process the 406.025 mhz signal as a test and ignore the transmission. If the transmission is longer than 15 seconds, the satellite system will process the transmission as a real distress signal. (3) Put the ELT switch in the ARM (OFF) position. (4) Make sure that the correct Mode S code was received on the SARSAT beacon test set. (5) Make sure that the 15 bit Hex ID was received on the SARSAT beacon test set. (6) Record the 15 bit hex ID on the label of the ELT. (7) Record the 15 bit hex ID on the Maintenance Transaction Report. (8) Do the test as necessary until satisfactory results are received with a 15-second delay between tries. C. (Airplanes with NAV interface) Do a test of the NAV interface. (1) Engage the ELT/NAV INTERFACE circuit breaker. (2) Initialize the FMS. Revision 3 - Jun 11/2010 Page 6
(3) Move the ELT switch to the ON position. NOTE: To prevent satellite detection, do not keep the remote switch in the on position for more than 15 seconds. During the first 15 seconds, the satellite system will process the 406.025 mhz signal as a test and ignore the transmission. If the transmission is longer than 15 seconds, the satellite system will process the transmission as a real distress signal. (4) Put the ELT switch in the ARM (OFF) position. (5) Make sure that the correct Mode S code was received on the SARSAT beacon test set. (6) Make sure that the latitude and longitude were received on the SARSAT beacon test set matches the FMS position. (7) Do the test as necessary until satisfactory results are received with a 15-second delay between tries. 13. 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 with the 15 digit hex code that was recorded from the SARSAT tester written on it. C. Send a copy of the completed Maintenance Transaction Report to CESCOM at the following address: CESCOM C/O, Camp Systems International, 8200 East 34 th Street North, Building 1600 Suite 1607, Wichita, KS 67226. MATERIAL INFORMATION Airplanes with NAV interface that have a Pointer ELT installed, order the kit below. -0 1 Kit, consisting of the following parts: CM2692-48J1S 1 Plug Button CM3558-4-12G 4 Screw CM3827AD5-5 1 Rivet H111F0C63-150 4 Insert MS20470AD4-4.5 6 Rivet MS20470AD4-4 10 Rivet MS20470AD4-5 10 Rivet MS20470AD5-5.5 10 Rivet MS21055L3 1 Nutplate MS21059L3 6 Nutplate MS21071L3 1 Nutplate MS24694S53 6 Screw MS27039C0810 4 Screw Revision 3 - Jun 11/2010 Page 7
MS27039-0808 26 Screw MS27039C1-12 6 Screw MS35206-246 4 Screw NAS1149CN832R 4 Washer S2456-4-6 9 Rivet S2457-4-6 67 Rivet 110-337 1 ELT Antenna ELT-177-1 and Discard ELT-177-2 130-4004 1 Buzzer 452-0010 1 Remote Switch 453-0150 Discard 452-3052 1 Frame Assembly 452-5050 1 Mounting Tray Assembly 2017 Discard 452-5052 1 Mounting Cap Assembly 453-6500 1 Digital Interface Unit 9255017-4 1 Box Assembly 9602010-2 1 Shelf Assembly 9602010-6 1 Angle 9602010-7 1 Angle 9602010-8 1 Angle 9602010-9 1 Clip 9602010-10 1 Clip 9602020-2 1 Shelf Assembly 9602020-3 1 LH Bracket Assembly 9602020-5 1 LH Zee Assembly 9602020-6 1 RH Zee Assembly 9602020-9 1 RH Bracket Assembly 9602020-10 1 Bracket 9690460-1 1 Cable Assembly 9690364-3 1 Cover Assembly 9690364-4 1 Cover Assembly 9690367-2 1 Doubler 9690368-7 1 Plug Assembly 1 Instructions Airplanes without NAV interface that have a Pointer ELT, order the kit below. Revision 3 - Jun 11/2010 Page 8
-1 1 Kit, consisting of the following parts: CM2692-48J1S 1 Plug Button CM3558-4-12G 4 Screw CM3827AD5-5 1 Rivet H111F0C63-150 4 Insert MS20470AD4-5 10 Rivet MS20470AD5-7 4 Rivet MS21055L3 1 Nutplate MS21059L3 6 Nutplate MS21071L3 1 Nutplate MS24694S50 18 Screw MS24694S53 6 Screw MS27039C0810 4 Screw MS27039C1-12 6 Screw MS35206-246 4 Screw NAS1149CN832R 4 Washer 110-337 1 ELT Antenna ELT-177-1 and Discard ELT-177-2 130-4004 1 Buzzer 452-0010 1 Remote Switch MS25089-3G Discard 452-3052 1 Frame Assembly 452-5050 1 Mounting Tray Assembly 2017 Discard 452-5052 1 Mounting Cap Assembly 9602010-2 1 Shelf Assembly 9602010-6 1 Angle 9602010-7 1 Angle 9602010-8 1 Angle 9602010-9 1 Clip 9602010-10 1 Clip 9602020-10 1 Bracket 9602614-1 1 Cable Assembly 9690364-3 1 Cover Assembly 9690364-4 1 Cover Assembly 9690367-2 1 Doubler Revision 3 - Jun 11/2010 Page 9
9690368-7 1 Plug Assembly 1 Instructions Airplanes without NAV interface that do not have an ELT installed, order the kit below. -2 1 Kit, consisting of the following parts: CM2692-48J1S 1 Plug Button CM3558-4-12G 4 Screw CM3827AD5-5 1 Rivet H111F0C63-150 4 Insert MS20470AD4-5 10 Rivet MS20470AD5-7 4 Rivet MS21055L3 1 Nutplate MS21059L3 6 Nutplate MS21071L3 1 Nutplate MS24694S50 18 Screw MS24694S53 6 Screw MS27039C0810 4 Screw MS27039C1-12 6 Screw MS35206-246 4 Screw NAS1149CN832R 4 Washer 110-337 1 ELT Antenna 130-4004 1 Buzzer 452-0010 1 Remote Switch 452-3052 1 Frame Assembly 452-5050 1 Mounting Tray Assembly 452-5052 1 Mounting Cap Assembly 9602010-2 1 Shelf Assembly 9602010-6 1 Angle 9602010-7 1 Angle 9602010-8 1 Angle 9602010-9 1 Clip 9602010-10 1 Clip 9602614-1 1 Cable Assembly Revision 3 - Jun 11/2010 Page 10
9690364-3 1 Cover Assembly 9690364-4 1 Cover Assembly 9690367-2 1 Doubler 1 Instructions Airplanes with NAV interface that do not have an ELT installed, order the kit below. -3 1 Kit, consisting of the following parts: CM2692-48J1S 1 Plug Button CM3558-4-12G 4 Screw CM3827AD5-5 1 Rivet H111F0C63-150 4 Insert MS20470AD4-4.5 6 Rivet MS20470AD4-4 10 Rivet MS20470AD4-5 10 Rivet MS20470AD5-5.5 10 Rivet MS21055L3 1 Nutplate MS21059L3 6 Nutplate MS21071L3 1 Nutplate MS24694S50 18 Screw MS24694S53 6 Screw MS27039C0810 4 Screw MS27039C1-12 6 Screw MS27039-0808 26 Screw MS35206-246 4 Screw NAS1149CN832R 4 Washer S2456-4-6 9 Rivet S2457-4-6 67 Rivet 110-337 1 ELT Antenna 130-4004 1 Buzzer 452-0010 1 Remote Switch 452-3052 1 Frame Assembly 452-5050 1 Mounting Tray Assembly 452-5052 1 Mounting Cap Assembly Revision 3 - Jun 11/2010 Page 11
453-6500 1 Digital Interface Unit 9255017-4 1 Box Assembly 9602010-2 1 Shelf Assembly 9602010-6 1 Angle 9602010-7 1 Angle 9602010-8 1 Angle 9602010-9 1 Clip 9602010-10 1 Clip 9602020-2 1 Shelf Assembly 9602020-3 1 LH Bracket Assembly 9602020-5 1 LH Zee Assembly 9602020-6 1 RH Zee Assembly 9602020-9 1 RH Bracket Assembly 9602020-10 1 Bracket 9690460-1 1 Cable Assembly 9690364-3 1 Cover Assembly 9690364-4 1 Cover Assembly 9690367-2 1 Doubler 1 Instructions Airplanes with Nav interface that have an Artex ELT per SB560-25-19 or from original factory installation, order the kit below. -4 1 Kit, consisting of the following parts: CM2692-48J1S 1 Plug Button MS20470AD4-5 4 Rivet MS20426AD3-4.5 12 Rivet MS20470AD4-4.5 6 Rivet MS21055L3 1 Nutplate MS21059L3 6 Nutplate MS21071L3 1 Nutplate MS24694S53 6 Screw MS27039C0810 4 Screw MS27039C1-12 6 Screw Revision 3 - Jun 11/2010 Page 12
MS27039-0808 26 Screw MS35206-246 4 Screw NAS1149CN832R 4 Washer S2456-4-6 9 Rivet S2457-4-2 63 Rivet 110-337 1 ELT Antenna DMQ18-3 Discard 130-4004 1 Buzzer 453-6500 1 Digital Interface Unit 9255017-4 1 Box Assembly 9602020-2 1 Shelf Assembly 9602020-3 1 LH Bracket Assembly 9602020-5 1 LH Zee Assembly 9602020-6 1 RH Zee Assembly 9602020-9 1 RH Bracket Assembly 9602020-10 1 Bracket 9690367-2 1 Doubler 9602011-2 Discard 9690460-1 1 Cable Assembly 9602609-1 Discard 1 Instructions Airplanes without NAV interface that have an Artex ELT installed per SB560-25-19 or from original factory installation, order the kit below. -5 1 Kit, consisting of the following parts: CM2692-48J1S 1 Plug Button MS20470AD4-5 4 Rivet MS21055L3 1 Nutplate MS21059L3 6 Nutplate MS21071L3 1 Nutplate MS24694S53 6 Screw MS27039C0810 4 Screw MS27039C1-12 6 Screw MS35206-246 4 Screw NAS1149CN832R 4 Washer S2457-4-2 63 Rivet Revision 3 - Jun 11/2010 Page 13
110-337 1 ELT Antenna DMQ18-3 Discard 130-4004 1 Buzzer 9602614-1 1 Cable Assembly 9602609-1 Discard 9690367-2 1 Doubler 9602011-2 Discard 9602020-10 1 Bracket 1 Instructions Airplanes without an access panel installed, order the kit below. -6 1 Kit, consisting of the following parts: 9602010-11 1 Access Panel 9602010-12 1 Doubler MS24694-S4 20 Screw MS21049L08 20 Nutplate 1 Instructions In addition to a combination of the above kits the part that follows will be required to complete this service bulletin. 453-5000-999 1 ELT 406-2 3000-1, 453-0150, or none Discard NOTE: Airplanes without NAV interface, contact Parts Distribution 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 to order. Provide the name of the country so that the applicable part number will be sent. Revision 3 - Jun 11/2010 Page 14
TITLE SUPPLEMENTAL DATA EQUIPMENT/FURNISHINGS - ARTEX C406-2 THREE-FREQUENCY EMERGENCY LOCATOR TRANSMITTER (ELT) EFFECTIVITY MODEL SERIAL NUMBERS 560-0001 thru -0306 NOTE: This Service Bulletin may only be accomplished at a Cessna owned or authorized Service Center. NOTE: All model 560 airplanes were previously covered by this service bulletin. Airplanes -0307 and On will now need to comply with SB560-25-31 when installing a three-frequency ELT. This service bulletin is for airplanes -0001 thru -0306 only. NOTE: (Airplanes with NAV interface) It is the owner's responsibility to acquire a Mode S code before this service bulletin is started. The Mode S code is necessary to configure the Artex ELT. MANPOWER WORK PHASE Modification MAN-HOURS As required Revision C - Jun 11/2010 Page 1 of 2 Cessna Aircraft Company, Marketing Division, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-6000, Fax 1-316-517-8500 COPYRIGHT 1999
SUPPLEMENTAL DATA MATERIAL - Cost and Availability PART NUMBER AVAILABILITY COST -0 * * -1 * * -2 * * -3 * * -4 * * -5 * * -6 * * 453-5000-999 * * * Please contact Parts Distribution for current cost and availability of parts listed in this service bulletin. Phone at 1-800-835-4000 (Domestic) or 1-316-517-7542 (International). Send Email to: citationparts@cessna.textron.com or telefax at 1-316-517-7711. Based on availability and lead times, parts may require advanced scheduling. In cases where the required part(s) are available as exchange, order the exchange part and, upon completion, expedite the return of the removed core to avoid return penalties. Contact the Parts Distribution Sales Desk for availability of exchange parts. Revision C - Jun 11/2010 Page 2