SERVICE BULLETIN REVISION

Transcription

1 Revision 3 REVISION TRANSMITTAL SHEET This sheet transmits Revision 3 to, which: A. Removes the 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

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3 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

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5 Revision 1 REVISION TRANSMITTAL SHEET 1. This sheet transmits Revision 1 to. A. Changes the EFFECTIVITY from and On to thru B. Adds NOTE to tell that airplanes and On which were previously covered by this service bulletin are now covered by SB 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 , , and 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 Cable Assembly to the -0 Kit and the Cable Assembly to the -1 Kit. O. Adds rivets to the -0 and -1 Kits. P. Changes the S and S ELT Transmitter to the ELT Transmitter in the -0 and -1 Kits. Q. Adds the Remote Switch and attaching hardware to the -0 and -1 Kits. R. Adds the Plug Assembly to the -0 Kit. S. Removes the and 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 SB

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7 TITLE EQUIPMENT/FURNISHINGS - ARTEX C406-2 THREE-FREQUENCY EMERGENCY LOCATOR TRANSMITTER (ELT) EFFECTIVITY MODEL SERIAL NUMBERS thru 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 and On will now need to comply with SB when installing a three-frequency ELT. This service bulletin is for airplanes thru 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 , Fax COPYRIGHT 1999

8 MANPOWER WORK PHASE MAN-HOURS Modification * MATERIAL - Cost and Availability PART NUMBER AVAILABILITY COST -0 * * -1 * * -2 * * -3 * * -4 * * -5 * * -6 * * * * * 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 P1-4 Base, EC-108 Catalyst, TR-19 Thinner Alchem Products Inc. Brookside Ave Ambler, PA Dexter Crown Metro Echelon Road Donaldson Center Greenville, SC 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 (or equivalent) Artex PO Box 1270 Canby, OR ELT functional test and programming. CHANGE IN WEIGHT AND BALANCE MODEL 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

9 WEIGHT INCREASE pounds pounds pounds RESULTANT MOMENT inch-pounds inch-pounds inch-pounds MOMENT/ inch-pounds inch-pounds inch-pounds MODEL 560 SUBKIT -1 WEIGHT INCREASE pounds RESULTANT MOMENT inch-pounds MOMENT/ inch-pounds MODEL 560 SUBKIT -2 WEIGHT INCREASE pounds RESULTANT MOMENT inch-pounds MOMENT/ inch-pounds MODEL SUBKIT -3 (with GNS-XLS, GNS-1ESP -3 (with UNSK-1K or UNS-1L) -3 (1C615 and Honeywell FMS) or GNS-1CSP) WEIGHT INCREASE RESULTANT MOMENT inch-pounds inch-pounds inch-pounds MOMENT/ inch-pounds inch-pounds inch-pounds MODEL 560 SUBKIT -4 WEIGHT INCREASE pounds RESULTANT MOMENT inch-pounds MOMENT/ inch-pounds MODEL 560 SUBKIT -5 WEIGHT INCREASE pounds RESULTANT MOMENT inch-pounds MOMENT/ inch-pounds MODEL 560 SUBKIT -6 WEIGHT INCREASE pounds RESULTANT MOMENT inch-pounds MOMENT/ inch-pounds Revision 3 - Jun 11/2010 Page 3

10 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 CABLEASSY-ARTEX ELTW/ONAV ELT MODIFICATION INSTL LOCATOR BEACON-ARTEX ELT C406-2 W/NAV I/F MOD AIRCRAFT SYSTEMS PROGRAMMING-ARTEX C406-2 ELT (560) ELT MODIFICATION INSTALLATION EMERGENCY LOCATOR TRANSMITTER ANTENNA INSTL (MOD) ELT MOD INSTALLATION MODELS 550 & 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 (Airplanes that do not have an ELT installed) Go to Step (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

11 D. Install the ELT with the kept hardware. (Refer to Cessna Engineering Drawing ) E. (Airplanes with NAV interface) Install the NAV interface unit. (Refer to Cessna Engineering Drawing ) F. Install the ELT antenna. (Refer to Cessna Engineering Drawing ) G. Go to Step (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 ) E. (Airplanes with NAV interface) Install the NAV interface unit. (Refer to Cessna Engineering Drawing ) F. Install the ELT antenna. (Refer to Cessna Engineering Drawing ) G. Go to Step (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 ) B. Install the ELT. (Refer to Cessna Engineering Drawing ) C. (Airplanes with NAV interface) Install the NAV interface unit. (Refer to Cessna Engineering Drawing ) D. Install the ELT antenna. (Refer to Cessna Engineering Drawing ) E. Modify the aft pressure bulkhead. (Refer to Cessna Engineering Drawing ) (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 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 or ) 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 ) Revision 3 - Jun 11/2010 Page 5

12 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 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 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 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 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

13 (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 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 MATERIAL INFORMATION Airplanes with NAV interface that have a Pointer ELT installed, order the kit below Kit, consisting of the following parts: CM J1S 1 Plug Button CM G 4 Screw CM3827AD5-5 1 Rivet H111F0C Insert MS20470AD Rivet MS20470AD Rivet MS20470AD Rivet MS20470AD Rivet MS21055L3 1 Nutplate MS21059L3 6 Nutplate MS21071L3 1 Nutplate MS24694S53 6 Screw MS27039C Screw Revision 3 - Jun 11/2010 Page 7

14 MS Screw MS27039C Screw MS Screw NAS1149CN832R 4 Washer S Rivet S Rivet ELT Antenna ELT and Discard ELT Buzzer Remote Switch Discard Frame Assembly Mounting Tray Assembly 2017 Discard Mounting Cap Assembly Digital Interface Unit Box Assembly Shelf Assembly Angle Angle Angle Clip Clip Shelf Assembly LH Bracket Assembly LH Zee Assembly RH Zee Assembly RH Bracket Assembly Bracket Cable Assembly Cover Assembly Cover Assembly Doubler Plug Assembly 1 Instructions Airplanes without NAV interface that have a Pointer ELT, order the kit below. Revision 3 - Jun 11/2010 Page 8

15 -1 1 Kit, consisting of the following parts: CM J1S 1 Plug Button CM G 4 Screw CM3827AD5-5 1 Rivet H111F0C Insert MS20470AD Rivet MS20470AD5-7 4 Rivet MS21055L3 1 Nutplate MS21059L3 6 Nutplate MS21071L3 1 Nutplate MS24694S50 18 Screw MS24694S53 6 Screw MS27039C Screw MS27039C Screw MS Screw NAS1149CN832R 4 Washer ELT Antenna ELT and Discard ELT Buzzer Remote Switch MS G Discard Frame Assembly Mounting Tray Assembly 2017 Discard Mounting Cap Assembly Shelf Assembly Angle Angle Angle Clip Clip Bracket Cable Assembly Cover Assembly Cover Assembly Doubler Revision 3 - Jun 11/2010 Page 9

16 Plug Assembly 1 Instructions Airplanes without NAV interface that do not have an ELT installed, order the kit below Kit, consisting of the following parts: CM J1S 1 Plug Button CM G 4 Screw CM3827AD5-5 1 Rivet H111F0C Insert MS20470AD Rivet MS20470AD5-7 4 Rivet MS21055L3 1 Nutplate MS21059L3 6 Nutplate MS21071L3 1 Nutplate MS24694S50 18 Screw MS24694S53 6 Screw MS27039C Screw MS27039C Screw MS Screw NAS1149CN832R 4 Washer ELT Antenna Buzzer Remote Switch Frame Assembly Mounting Tray Assembly Mounting Cap Assembly Shelf Assembly Angle Angle Angle Clip Clip Cable Assembly Revision 3 - Jun 11/2010 Page 10

17 Cover Assembly Cover Assembly Doubler 1 Instructions Airplanes with NAV interface that do not have an ELT installed, order the kit below Kit, consisting of the following parts: CM J1S 1 Plug Button CM G 4 Screw CM3827AD5-5 1 Rivet H111F0C Insert MS20470AD Rivet MS20470AD Rivet MS20470AD Rivet MS20470AD Rivet MS21055L3 1 Nutplate MS21059L3 6 Nutplate MS21071L3 1 Nutplate MS24694S50 18 Screw MS24694S53 6 Screw MS27039C Screw MS27039C Screw MS Screw MS Screw NAS1149CN832R 4 Washer S Rivet S Rivet ELT Antenna Buzzer Remote Switch Frame Assembly Mounting Tray Assembly Mounting Cap Assembly Revision 3 - Jun 11/2010 Page 11

18 Digital Interface Unit Box Assembly Shelf Assembly Angle Angle Angle Clip Clip Shelf Assembly LH Bracket Assembly LH Zee Assembly RH Zee Assembly RH Bracket Assembly Bracket Cable Assembly Cover Assembly Cover Assembly Doubler 1 Instructions Airplanes with Nav interface that have an Artex ELT per SB or from original factory installation, order the kit below Kit, consisting of the following parts: CM J1S 1 Plug Button MS20470AD4-5 4 Rivet MS20426AD Rivet MS20470AD Rivet MS21055L3 1 Nutplate MS21059L3 6 Nutplate MS21071L3 1 Nutplate MS24694S53 6 Screw MS27039C Screw MS27039C Screw Revision 3 - Jun 11/2010 Page 12

19 MS Screw MS Screw NAS1149CN832R 4 Washer S Rivet S Rivet ELT Antenna DMQ18-3 Discard Buzzer Digital Interface Unit Box Assembly Shelf Assembly LH Bracket Assembly LH Zee Assembly RH Zee Assembly RH Bracket Assembly Bracket Doubler Discard Cable Assembly Discard 1 Instructions Airplanes without NAV interface that have an Artex ELT installed per SB or from original factory installation, order the kit below Kit, consisting of the following parts: CM J1S 1 Plug Button MS20470AD4-5 4 Rivet MS21055L3 1 Nutplate MS21059L3 6 Nutplate MS21071L3 1 Nutplate MS24694S53 6 Screw MS27039C Screw MS27039C Screw MS Screw NAS1149CN832R 4 Washer S Rivet Revision 3 - Jun 11/2010 Page 13

20 ELT Antenna DMQ18-3 Discard Buzzer Cable Assembly Discard Doubler Discard Bracket 1 Instructions Airplanes without an access panel installed, order the kit below Kit, consisting of the following parts: Access Panel 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 ELT , , or none Discard NOTE: Airplanes without NAV interface, contact Parts Distribution at (Domestic) or (International). Send to: citationparts@cessna.textron.com or telefax at to order. Provide the name of the country so that the applicable part number will be sent. Revision 3 - Jun 11/2010 Page 14

21 TITLE SUPPLEMENTAL DATA EQUIPMENT/FURNISHINGS - ARTEX C406-2 THREE-FREQUENCY EMERGENCY LOCATOR TRANSMITTER (ELT) EFFECTIVITY MODEL SERIAL NUMBERS thru 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 and On will now need to comply with SB when installing a three-frequency ELT. This service bulletin is for airplanes thru 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 , Fax COPYRIGHT 1999

22 SUPPLEMENTAL DATA MATERIAL - Cost and Availability PART NUMBER AVAILABILITY COST -0 * * -1 * * -2 * * -3 * * -4 * * -5 * * -6 * * * * * Please contact Parts Distribution for current cost and availability of parts listed in this service bulletin. Phone at (Domestic) or (International). Send to: citationparts@cessna.textron.com or telefax at 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