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Cessna 510 Citation Mustang SERVICE BULLETIN
Below you will find brief information for Citation Mustang 510. This document presents a mandatory service bulletin that must be completed by November 15, 2012 to upgrade the Garmin G1000 software to version 010-00435-24. It includes detailed instructions for installing the new software, including how to configure various options like DME, ADF, TAS, HF, TAWS, ChartView, Synthetic Vision System, and XM cockpit options, as well as verifying their functionality.
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Citation SERVICE BULLETIN SB510-34-14 TITLE NAVIGATION - GARMIN G1000 SOFTWARE VERSION 010-00435-24 UPGRADE EFFECTIVITY MODEL SERIAL NUMBERS 510 (Citation Mustang) -0001 thru -0402 The equivalent of this service bulletin has been incorporated on production airplanes -0403 and On. This service bulletin supersedes SB510-34-11 Navigation - Garmin G1000 Software Version 010-00435-21 Upgrade. REASON The 010-00435-24 software provides fixes and enhancements to the Garmin G1000 avionics system. This service bulletin corrects issues that are defined in the service letters that follow: • • • SL510-34-17Navigation - Transmittal Of Garmin Service Advisory No. 1101 - GDL 69/69A TFR (Temporary Flight Restrictions) Reporting Issue SL510-34-19 Navigation - Transmittal Of Garmin Service Advisory No. 1118 - Momentary Failure Indications (Red X) Can Occur When Sorting Stored Flight Plans SL510-34-20 Navigation - Transmittal Of Garmin Service Advisory No. 1129 - Momentary Loss Of GRS 77/77H And GDC 74A/74B/74H Functions DESCRIPTION This service bulletin provides parts and instructions to upgrade the Garmin G1000 software to version 010-000435-24. COMPLIANCE MANDATORY. This service bulletin must be accomplished by November 15, 2012. 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. SB510-34-14 Page 1 of 9 May 4, 2012 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-5800, Fax 1-316-517-7271, Email: [email protected] COPYRIGHT © 2012 Citation SERVICE BULLETIN SB510-34-14 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. 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. WEIGHT AND BALANCE INFORMATION Negligible REFERENCES Cessna Model 510 Maintenance Manual ICA-510-34-00010 Phase 12 G1000 Software Update ICA Supplement PUBLICATIONS AFFECTED Cessna Model 510 FAA Approved Airplane Flight Manual (510FM) ACCOMPLISHMENT INSTRUCTIONS 1. Prepare the airplane for maintenance: A. 2. (1) Connect the airplane battery. (2) Connect external electrical power. B. Move the battery switch to the BATT position. C. Move avionics power switch to the AVN PWR position. Load the Garmin G1000 software to 010-00435-24. A. 3. Make sure that all switches are in the OFF/NORM position. The cards that follow must be available before the software is installed: • The 010-00435-24 Garmin SD Card V.435-24. • The 010-00330-51 Garmin TAWS unlock card (in the blue software pouch included as loose equipment at the time of airplane delivery). • The 010-00330-50 Garmin ChartView unlock card (in the blue software pouch included as loose equipment if the ChartView option was purchased at the time of airplane delivery). • The 010-00330-55 SVT Unlock Data Card (in the blue software pouch included as loose equipment if installed). • The 010-00435-EO XM Cockpit Unlock Card (in the blue software pouch included as loose equipment if installed). Turn on the G1000 in normal mode to verify existing options. A. Record the basic empty weight as displayed on the MFD. B. Record which options are installed for later reference. (1) ADF – Make sure that the softkey 7 on both PFDs is labeled ADF/DME or ADF. (2) DME - Make sure that the softkey 7 on both PFDs is labeled ADF/DME or DME. (3) TAS – Turn to the MFD MAP – TRAFFIC page. Make sure that the operating mode is NOT TIS. TIS will have a cyan label in the upper left corner indicating TNA MUTE ON or TNA MUTE OFF. (4) HF – Make sure that COM3 is selectable on both audio panels. (5) XM in the cockpit - make sure that MUSIC is selectable on both audio panels. SB510-34-14 Page 2 May 4, 2012 SERVICE BULLETIN Citation SB510-34-14 (6) C. ChartView – Turn to the MFD AUX – SYSTEM STATUS page. (a) Press the MFD1 DB softkey and use the FMS knob to scroll down to the CHART database information. (b) Make sure that the chart listed is Jeppesen ChartView. Remove power from the airplane. CAUTION: Failure to follow the instructions in exact step-by-step order could result in damage to the GDU SUPPLEMENTAL database and/or SD cards. 4. Remove and keep the Cessna Diagnostics Maintenance System (CDMS) from the upper slot of the MFD for later installation. 5. With all aircraft power off, insert the 010-00435-24 Garmin SD Card V.435-24 into the top card slot of the PFD 2. 6. MFD/PFD software load: A. Pull the PFD 1, PFD 2, and MFD circuit breakers (primary & secondary). B. Move the battery switch to the BATT position. C. Move avionics power switch to the AVN PWR position. D. Press and hold the bottom right softkey on the PFD 2. Close both PFD 2 circuit breakers to power on the PFD 2. E. Release the softkey after the INITIALIZING SYSTEM message appears. F. Press the YES softkey to load GDU system files when the DO YOU WANT TO UPDATE SYSTEM FILES? prompt appears. G. When the software load is complete the message DO YOU WANT TO UPLOAD THE SPLASH SCREEN will appear. Press the YES softkey at the bottom of the display when the prompt appears. H. When the splash screen update is complete you will be asked to PRESS ANY SOFTKEY TO CONTINUE or allow the auto timer to count down and enter into configuration mode. NOTE: A UPDATING STANDBY NAVIGATION DATABASE WITH NEWER ACTIVE DATABASE message will appear on the display. After the database loads the display will verify that the database loaded correctly. I. Software load to the PFD 2 is complete when the display starts into configuration mode. J. Leave the display powered on. K. Remove the 010-00435-24 Garmin SD Card V.435-24 and insert it into the top MFD slot. L. Do Steps 6D thru 6J again for the MFD. (1) Use the MFD circuit breakers instead of the PFD 2 circuit breaker. M. Remove the 010-00435-24 Garmin SD Card V.435-24 and insert it into the top PFD 1 slot. N. Insert the Cessna Diagnostics Maintenance System (CDMS) into the top card slot of the MFD. NOTE: The Cessna Diagnostics Maintenance System (CDMS) card should remain in the MFD. O. Do Steps 6D thru 6J again for PFD 1. (1) 7. Use the PFD 1 circuit breakers instead of the PFD 2 circuit breaker. Initial software load and configuration. A. Use the FMS knob to go to the SYSTEM UPLOAD page on PFD 1. B. Use the small FMS knob to select MUSTANG from the AIRFRAME list and push the ENT softkey. May 4, 2012 SB510-34-14 Page 3 Citation SERVICE BULLETIN SB510-34-14 C. Turn small FMS knob and scroll down to CESSNA MUSTANG BASE CONFIGURATION and press enter. D. The software included on the 010-00435-24 Garmin SD Card V.435-24 will automatically determine which files must be loaded. NOTE: The 010-00435-24 Garmin SD Card V.435-24 may not select files to upload. If this occurs select clear all and then select all files. E. Turn small FMS knob and scroll down to GIA GAINS and press ENT to create a check mark in that field. F. Press the LOAD softkey to load selected software/config items. Periodically monitor the loading process for failures. A green PASS message is shown beside s/w and config items. NOTE: Periodically monitor the software load for progress. If the upload to a unit is unsuccessful, an UPLOAD FAIL message will be posted and the upload will stop. A red FAIL will be shown beside the software that failed. Press enter to acknowledge the fail message and to continue the same software load. If unable to load the software after several attempts, uncheck the software and configuration boxes using the ENT softkey and press the LOAD softkey to continue with the rest of the software load before troubleshooting cause of failure. G. 8. 9. Press the ENT button when all software loading is complete to acknowledge software upload is complete. (Airplanes -0001 thru -0379) Load the software configuration. A. Use the large FMS knob to go up to the ITEM box. B. Select CESSNA MUSTANG OLD NO TCAS II WIRING OPTION from the group list. C. Make sure that the GIA 1 and GIA 2 boxes are checked. D. Press the LOAD softkey to load selected software/config items. Periodically monitor the loading process for failures. A green PASS message is shown beside s/w and config items. E. Press the ENT button when all software loading is complete to acknowledge software upload is complete. F. Make sure that a green PASS appears next to each loaded item. G. Push the UPDT CFG softkey to update the system configuration files. Enable the DME option: WARNING: 10. Do not configure an option that is not installed on the airplane. A. Go to Step 10 if the DME option is not installed. B. Use the outer FMS knob to move the cursor to the ITEM box. C. Use the inner FMS knob to highlight the CESSNA MUSTANG KN-63 DME OPTION from the group list. D. Press the ENT softkey to select the option. E. The configuration box for GIA 2, GMA 1, and GMA 2 should be checked. F. Press the LOAD softkey to load the DME configuration parameters into GIA 2. G. Monitor the configuration load to make sure the green PASS message is next to GIA 2. H. Press the ENT button when all software loading is complete to acknowledge software upload is complete. Enable the ADF option: SB510-34-14 Page 4 May 4, 2012 Citation SERVICE BULLETIN SB510-34-14 WARNING: 11. A. Go to Step 11 if the ADF option is not installed. B. Use the outer FMS knob to move the cursor to the ITEM box. C. Use the inner FMS knob to highlight the CESSNA MUSTANG BECKER ADF OPTION from the group list. D. Press the ENT softkey to select the option. E. All configuration boxes should be checked. • GIA2 • GMA1 • GMA2 F. Press the LOAD softkey to load all software/config items. G. Monitor the configuration load to verify the green PASS message next to each item. H. Press the ENT button when all software loading is complete to acknowledge software upload is complete. TAS option configuration: WARNING: 12. Do not configure an option that is not installed on the airplane. A. Go to Step 12 if the TAS option is not installed. B. Use the outer FMS knob to move the cursor to the ITEM box. C. Use the inner FMS knob to highlight the CESSNA MUSTANG KTA 870 TAS OPTION from the group list. D. Press the ENT softkey to select the option. E. The configuration box for GIA 2 should be checked. F. Press the LOAD softkey to load the TAS configuration parameters into GIA 2. G. Monitor the configuration load to make sure the green PASS message is next to GIA 2. H. Press the ENT button when all software loading is complete to acknowledge software upload is complete. HF option configuration: WARNING: 13. Do not configure an option that is not installed on the airplane. Do not configure an option that is not installed on the airplane. A. Go to Step 13 if the HF option is not installed. B. Use the outer FMS knob to move the cursor to the ITEM box. C. Use the inner FMS knob to highlight the CESSNA MUSTANG KHF1050 HF OPTION from the group list. D. Press the ENT softkey to select the option. E. The configuration box for GMA 1 & 2 should be checked. F. Press the LOAD softkey to load the HF configuration parameters into GMA 1 and 2. G. Monitor the configuration load to verify the green PASS message next to GMA 1 and 2. H. Remove the 010-00435-24 Garmin SD Card V.435-24 from the top slot of the PFD. I. Keep the 010-00435-24 Garmin SD Card V.435-24 as loose equipment with the aircraft. TAWS enable configuration: A. Pull the primary and secondary PFD 1 circuit breakers. May 4, 2012 SB510-34-14 Page 5 Citation SERVICE BULLETIN SB510-34-14 B. Insert the 010-00330-51 TAWS Unlock Card into the top card slot of PFD 1. C. Press and hold the bottom right softkey on the PFD 1. D. Push both PFD 1 breakers to power on the PFD 1. E. Release the softkey after the INITIALIZING SYSTEM message appears. F. Use the FMS knob to go to the SYSTEM UPLOAD page on PFD 1. G. Push the inner FMS knob to activate the cursor. H. Use the inner FMS knob to select CONFIGURATION FILES in the AIRFRAME list and push the ENT softkey I. Use the outer FMS knob to move the cursor to the ITEM box. J. Use the inner FMS knob to select the ENABLE TAWS option and push the ENT softkey. NOTE: When the option is selected the configuration files in the PRODUCT field will be displayed. K. Push the CHK ALL softkey to select all files. L. Push the LOAD softkey. M. Monitor the status of the software upload. N. Push the ENT softkey to acknowledge the upload is complete. O. Make sure that COMPLETE is displayed in the SUMMARY field. P. Push the inner FMS knob to de-activate the cursor. Q. Remove the 010-00330-51 TAWS Unlock Card from the display. NOTE: Once the TAWS unlock card is used to unlock the TAWS on one airplane it cannot be used to unlock the TAWS on another airplane. R. 14. Keep the 010-00330-51 TAWS Unlock Card as loose equipment with the aircraft. Jeppesen ChartView option configuration: WARNING: Do not configure an option that is not installed on the airplane. A. Go to Step 15 if the Jeppesen ChartView option is not installed. B. Pull the primary and secondary PFD 1 circuit breakers. C. Insert the 010-00330-50 ChartView Unlock Card into the top card slot of PFD 1. D. Press and hold the bottom right softkey on the PFD 1. E. Push both PFD 1 breakers to power on the PFD 1. F. Release the softkey after the INITIALIZING SYSTEM message appears. G. Use the FMS knob to go to the SYSTEM UPLOAD page on PFD 1 . H. Push the inner FMS knob to activate the cursor. I. Use the inner FMS knob to select CONFIGURATION FILES in the AIRFRAME list and push the ENT softkey J. Use the outer FMS knob to move the cursor to the ITEM box. K. Use the inner FMS knob to select the ENABLE CHARTVIEW option and push the ENT softkey. NOTE: When the option is selected the configuration files in the PRODUCT field will be displayed. L. Push the CHK ALL softkey to select all files. M. Push the LOAD softkey. SB510-34-14 Page 6 May 4, 2012 Citation SERVICE BULLETIN SB510-34-14 N. Monitor the status of the software upload. O. Push the ENT softkey to acknowledge the upload is complete. P. Make sure that COMPLETE is displayed in the SUMMARY field. Q. Push the inner FMS knob to de-activate the cursor. R. Remove the unlock card. NOTE: Once the ChartView unlock card is used to unlock the ChartView on one airplane it cannot be used to unlock the ChartView on another airplane. 15. Synthetic Vision System option configuration: WARNING: Do not configure an option that is not installed on the airplane. A. Go to Step 16 if the Synthetic Vision System option is not installed. B. Pull the primary and secondary PFD 1 circuit breakers. C. Insert the 010-00330-55 SVT Unlock Data Card into the top slot of PFD 1. D. Press and hold the bottom right softkey on the PFD 1. E. Push both PFD 1 breakers to power on the PFD 1. F. Release the softkey after the INITIALIZING SYSTEM message appears. G. Use the FMS knob to go to the SYSTEM UPLOAD page on PFD 1. H. Push the inner FMS knob to activate the cursor. I. Use the inner FMS knob to select CONFIGURATION FILES in the AIRFRAME list and push the ENT softkey. J. Use the outer FMS knob to move the cursor to the ITEM box. K. Use the inner FMS knob to select the SVS ENABLE option and push the ENT softkey. NOTE: When the option is selected the configuration files in the PRODUCT field will be displayed. 16. L. Push the CHK ALL softkey to select all files. M. Push the LOAD softkey. N. Monitor the status of the software upload. O. Push the ENT softkey to acknowledge the upload is complete. P. Make sure that COMPLETE is displayed in the SUMMARY field. Q. Push the inner FMS knob to de-activate the cursor. R. Remove the 010-00330-55 SVT Unlock Data Card from PFD 1. XM cockpit option configuration: WARNING: Do not configure an option that is not installed on the airplane. A. Go to Step 17 if the XM cockpit option is not installed. B. Pull the primary and secondary PFD 1 circuit breakers. C. Install the 010-00435-EO XM Unlock Card in the upper slot on the pilot's PFD. D. Press and hold the bottom right softkey on the PFD 1. E. Close both PFD 1 circuit breakers to power on the PFD. F. Release the softkey after the INITIALIZING SYSTEM message appears. G. Use the inner FMS knob to go to the SYSTEM UPLOAD PAGE. May 4, 2012 SB510-34-14 Page 7 SERVICE BULLETIN Citation SB510-34-14 17. H. Select MUSTANG from the AIRFRAME list and push the ENT softkey. I. Select CESSNA MUSTANG COCKPIT XM OPTION GDU 11.XX & ON from the group list and push the ENT softkey. J. Make sure that the configuration boxes that follow are checked. • AIRFRAME • GIA2 • GMA1 • GMA2 • ALERTS K. Push the LOAD softkey to upload the software. L. Monitor the software load and make sure that a green PASS message is displayed. M. Remove and keep the 010-00435-EO XM Unlock Card as loose equipment with the aircraft. Verification: A. Move avionics power switch to the OFF position. B. Move the battery switch to the OFF position for one minute. C. Move the battery switch to the BATT position. D. Move avionics power switch to the AVN PWR position. E. Make sure that the MSG boxes in both PFDs are empty or only contain the message GPS NAV LOST if you are in a location without GPS signal. F. Make sure that all previously recorded options are functioning properly. G. ADF verification, if installed: • Make sure that the softkey 7 on both PFDs is labeled ADF/DME or ADF. • Make sure that the audio panel ADF buttons work on both GMA. H. DME verification, if installed: • Make sure that the softkey 7 on both PFDs is labeled ADF/DME or DME. I. TAS verification, if installed: (1) Turn to the MFD MAP – TRAFFIC page. (2) Make sure that the operating mode is NOT TIS. (3) The TIS will have a cyan label in the upper left corner indicating TNA MUTE ON or TNA MUTE OFF. J. HF verification, if installed: • Make sure that COM3 is selectable on both audio panels. K. TAWS verification L. (1) Turn to the MFD MAP – TAWS page. (2) TAWS has not been unlocked if a MAP – TERRAIN PROXIMITY page is in its place. XM in the cockpit, if Installed. NOTE: A valid XM satellite signal is required to verify the operation of the XM radio. (1) Make sure that MUSIC is selectable on both audio panels. (2) Push the MUSIC key on the audio control panel (3) Use the FMS cursor to select the AUX-XM RADIO page on the MFD. (4) Push the VOL softkey on the MFD. SB510-34-14 Page 8 May 4, 2012 SERVICE BULLETIN Citation SB510-34-14 (5) Push the VOL + softkey to enable volume control for the XM radio. NOTE: At every power up the XM radio volume will default to mute. (6) M. N. Make sure that the XM radio can be heard in the cockpit headsets. ChartView verification, if installed: (1) Turn to the MFD AUX – SYSTEM STATUS page. (2) Press the MFD 1 DB softkey and use the FMS knob to scroll down to the CHART database information. (3) Make sure that the chart listed is Jeppesen ChartView. SVT verification, if installed: (1) Press the PFD softkey on the pilot's PFD. (2) Press the SYN VIS softkey. (3) Make sure that PATHWAY SYN TERR, HRZN HDG, and APT SIGNS are displayed above the softkeys. NOTE: The G1000 avionics system must have valid heading values, attitude values, and 3D GPS position to display the SVT on the PFD. 18. Do the G1000 system architecture check. (Refer to the Model 510 Maintenance Manual, Chapter 34, Garmin G1000 Integrated Avionics System - Adjustment/Test.) 19. Do the AFCS check. (Refer to the Model 510 Maintenance Manual, Chapter 34, Garmin G1000 Integrated Avionics System - Adjustment/Test.) 20. Enter the aircraft basic weight on the MFD. 21. Remove power from the airplane. 22. Insert the 010-00435-24 Garmin SD Card V.435-24 into the software pouch in the airplane log book. 23. 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. 24. Make sure that ICA-510-34-00010 Phase 12 G1000 Software Update ICA Supplement is available for future maintenance. 25. 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 C/O Camp Systems International, 8200 East 34th Street North, Building 1600 Suite 1607 Wichita, KS 67226. MATERIAL INFORMATION Order the kit below to install this modification. NEW P/N QUANTITY KEY WORD OLD P/N INSTRUCTIONS/ DISPOSITION SB510-34-14 1 Kit, consisting of the following parts: 010-00435-24 1 Garmin SD Card V.435-24 010-00435-16 Discard 190-00600-04 1 Cockpit Reference Guide 190-00600-03 Discard May 4, 2012 SB510-34-14 Page 9 ATTACHMENT Citation SB510-34-14 GARMIN G1000 SOFTWARE CONFIGURATION CONTROL SOFTWARE PART NUMBER PRODUCTION EFFECTIVITY SERVICE BULLETIN EFFECTIVITY SERVICE BULLETIN SERVICE BULLETIN COMPLIANCE REPLACES SOFTWARE PART NUMBER 01000435-09 -0001 thru -0065 Not Applicable Not Applicable Not Applicable Not Applicable 01000435-10 -0066 thru -0152 -0001 thru -0065 SB510-34-02 Mandatory 010-00435-09 01000435-13 -0153 thru -0177 Not Applicable Not Applicable Not Applicable 010-00435-10 01000435-16 -0178 thru -0371 -0001 thru -0177 SB510-34-09 Recommended 010-00435-13 01000435-21 -0372 thru -0402 -0001 thru -0371 SB510-34-11 Mandatory 010-00435-16 01000435-24 -0403 and On -0001 thru -0402 SB510-34-14 Mandatory 010-00435-21 ATTACHMENT Citation SB510-34-14 LRU SOFTWARE AND VERSION LINE REPLACEABLE UNIT (LRU) SOFTWARE PART NUMBER VERSION COM1 006-B0081-XX 7.00 or 10.00 COM2 006-B0081-XX 7.00 or 10.00 GCU 006-B0387-20 3.00 GDC1 006-B0261-18 3.08 GDC1FPGA 006-C0055-00 1.05 GDC2 006-B0261-18 3.08 GDC2FPGA 006-C0055-00 1.05 GDL69 006-B0317-21 4.01 GEA1 006-B0193-05 2.07 GEA2 006-B0193-05 2.07 GFC CERT GIA1 006-D0356-15 2.06 GFC CERT GIA2 006-D0356-15 2.06 GFC CERT P C 006-D0356-15 2.06 GFC CERT P M 006-D0356-15 2.06 GFC CERT PT C 006-D0356-15 2.06 GFC CERT PT M 006-D0356-15 2.06 GFC CERT R C 006-D0356-15 2.06 GFC CERT R M 006-D0356-15 2.06 GFC CERT Y C 006-D0356-15 2.06 GFC CERT Y M 006-D0356-15 2.06 GIA 1 006-B0544-38 6.40 GIA 1 AUDIO 006-D0425-06 2.11 GIA 2 006-B0544-38 6.40 GIA 2 AUDIO 006-D0425-06 2.11 GMA1 066-B0203-43 4.03 GMA2 066-B0203-43 4.03 GMC 066-B0387-20 3.00 GMU1 006-B0224-01 2.05 GMU1 FPGA 006-C0048-00 2.00 GMU2 006-B0224-01 2.05 ATTACHMENT Citation SB510-34-14 LINE REPLACEABLE UNIT (LRU) SOFTWARE PART NUMBER VERSION GMU2 FPGA 006-C0048-00 2.00 GPS1 006-B0339-0A 3.2 GPS2 006-B0339-0A 3.2 GRS1 006-B0223-22 3.02 GRS1 FPGA 006-C0049-00 2.00 GRS1 MV DB 006-D0159-01 2xxx (*) GRS 2 006-B0223-22 3.02 GRS2 FPGA 006-C0049-00 2.00 GRS2 MV DB 006-D0159-01 2xxx (*) GS1 006-B0083-XX 4.00 or 6.01 GS2 006-B0083-XX 4.00 or 6.01 GSA PTCH CTL 006-B0398-32 2.30 GSA PTCH MON 006-B0398-32 2.30 GSA PTCH TRIM C 006-B0398-32 2.30 GSA PTCH TRIM M 006-B0398-32 2.30 GSA ROLL CTL 006-B0398-32 2.30 GSA ROLL MON 006-B0398-32 2.30 GSA YAW CTL 006-B0398-32 2.30 GSA YAW MON 006-B0398-32 2.30 GTX1 006-B0172-XX 6.11 GTX2 006-B0172-XX 6.11 GWX 006-B0266-10 2.11 GWX FPGA 006-C0042-06 3.01 MFD1 006-B0319-A3 12.03 MFD1 FPGA 006-C0036-04 1.04 NAV1 006-B0082-XX 5.01, 5.02, 5.03, or 6.01 NAV2 006-B0082-XX 5.01, 5.02, 5.03, or 6.01 PFD1 006-B0319-A3 12.03 PFD1 FPGA 006-C0036-04 1.04 PFD2 006-B0319-A3 12.03 PFD2 FPGA 006-C0036-04 1.04 (*) The GRS RGF is updated every five years. 2xxx defines the current year. Citation ATTACHMENT SB510-34-14 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. • XM Weather: NEXRAD and Icing/Turbulence is mutually exclusive on weather datalink page. Icing and Turbulence may be shown together, but NEXRAD will be turned off when either are enabled. When NEXRAD is enabled by the pilot, both Icing and Turbulence will be turned off. • Garmin Display Unit: Added a Selected Altitude Intercept Arc to the following moving maps: main Navigation map, PFD inset map, AUX - Trip Planning map, Active Flight Plan page map, and all NRST maps. A cyan arc shall be drawn on the map (when enabled via the Map Setup menu and not suppressed) to indicate the location at which the aircraft will reach the selected altitude based on current barometric altitude, vertical speed, and ground speed. The arc is drawn along the aircraft's current track. • The main NAV map page's profile view, which shows the airplane's vertical position over the terrain and obstacles along a swath centered on the current airplane ground track. When datalink weather is available, winds aloft information is also shown which depicts headwind or tailwind as a function of altitude. This vertical profile view is turned on or off via the PROFILE softkey under the MAP sub-tier of softkeys. This feature is only available if specifically enabled in the airframe configuration. • Flight Planning Improvements: If the VECTORS transition is chosen when an approach is loaded, or if ACTIVATE VECTOR-TO-FINAL is selected from the PROC menu, waypoints from one of the transitions that are near the course to the final approach fix will be loaded into the approach, however the course-to-fix leg to the FAF will still become the active leg when VTF is activated. The other waypoints will be loaded into the flight plan and shown on the map. In this case a gap will be inserted ahead of the first leg of the approach, so that if the pilot allows leg sequencing into the approach to occur, it will start with the first leg contained completely in the approach rather than connecting a leg from the last en route waypoint to the first waypoint of the approach. • Flight Planning Enhancements: • Added configurable options to improve waypoint insertion on the active flight plan page • A hollow box can be drawn with a dashed outline around the selected field, a precursor. When the precursor is enabled, functions that required the cursor to be active will work as though the cursor was active. For example, alphanumeric key will automatically start inserting a waypoint at the indicated location or edit the currently selected field. • An arrow can also be drawn indicating where in the current flight plan a new waypoint would be inserted based on the currently selected field. • The selected field (precursor or cursor) can be adjusted by using the joystick when it is not being used to pan the map. Pushing the joystick up moves the selection up a row while pushing the joystick down moves it down a row. Pushing the joystick right will move the selection right to the next highlightable column or down to the next row if the last column in the row is currently selected. Pushing the joystick to the left will move the selection left to the next highlightable column or up to the next row if the first column in the row is currently selected. • The blank entry can be selected the first time the active flight plan page is opened after a power-up rather than the first waypoint in the list. • Each of these improvements can be configured independently and are disabled unless configured by the airframe. • Graphical Weather Enhancements: • Added the display of graphical METARs to the moving maps and to the active flight plan page. Added the display of the raw METAR text to the active flight plan page and the moving maps (when highlighting the METAR flag with the map cursor). Added the display of a weather legend to maps that share the weather related softkeys (NEXRAD, XM LTNG, METAR). The legend is accessible via the LEGEND softkey in the MAP tier. The active flight plan page can be configured to show METAR Citation ATTACHMENT SB510-34-14 • • • • • • • • flags/reports from nearby reporting stations for waypoints in the flight plan without an active reporting station. The search radius is configurable from 0-99 NM, the Model 510 has a 30 NM search radius. • Decoded wind direction in METARs is now always reported as a three digit number to avoid any confusion (20 could be interpreted as 200 or 020). • Added time to decoded display of METAR on waypoint airport weather page. The METAR observation time was previously shown in the raw METAR text on the WPT-WEATHER INFORMATION page for airports. To assist the pilot in quickly determining the relevance of the observation, the "decoded METAR observation time" and the "elapsed time since the observation" have been added to the page. • The time displayed for temporary flight restrictions (TFRs) now includes a reference to the time format selected by the pilot on the SYSTEM SETUP page. When UTC time is selected, the TFR will include a suffix of UTC. When Local 24hr time is selected, the TFR time will include a suffix of LCL. When Local 12hr time is selected, the TFR time will include a suffix for AM/PM. • The logic to display the text of a METAR in yellow when it is more than 75 minutes old was removed so the color remains constant at all times. Also, METAR parsing logic was updated to correctly convert the altimeter field from HPA to inches of mercury. • Default corners for TFR boundary box were changed to include Eastern/Southern hemisphere points. Longitudinal correction was fixed when parsing arc shaped TFR's. Reference Garmin Service Advisory SA-1101. Radio Altimeter Display Location Improvement: Moved the locations of Radio Altitude Height and Radio Altitude Test Status. When the "RA" label is configured to be displayed adjacent to the Radio Altitude Height, the text sizing and coloration has changed for the "RA" label to harmonize with labels used elsewhere. SVT Improvement: SVT will now determine if a runway highlight should be rendered. If there is terrain between the current aircraft position and the runway, that would obscure the runway, then the highlight will not be displayed. Altitude Labeling Improvements: • Changed labeling according to AC 20-163 recommendation that systems display GPS geometric altitude relative to sea level using a label of "GSL" to denote information and prevent possible confusion. • This change applies to the MAP - TERRAIN PROXIMITY or MAP - TAWS page and the AUX - GPS STATUS page. The terrain/TAWS page has changed from 'GPS ALT MSL' to 'GPS ALT GSL' and the AUX - GPS STATUS page has changed from 'ALTITUDE' to 'ALT GSL'. Altitude Select Knob Enhancement: Added support for configurable acceleration on the altitude select (ALT SEL) knob. Standby Navigation Database Improvement: The standby navigation database loading function was modified to remove manual control of the DB SYNC function. Additionally the Garmin logo startup screen was modified to display a notification "Please Wait. Navigation Database Update in Progress. Do Not Remove Power from Displays." when a transfer occurs on startup to prevent the startup delay from causing concern. Updating the active navigation database in a GDU will also update the standby navigation database in the same GDU. Note, manual updates of the active navigation database must be performed on each GDU. With this Improvement the Standby Navigation Database Feature will be enabled on. Flight Plan Sorting Removed: The functionality that allowed sorting the stored flight plans was removed. New System Message: • When the intercept angle between heading and the armed NAV signal (LOC) exceeds 105 degrees of angular deviation, capture of the armed signal is suppressed. After the suppression logic is activated, the FD will not capture the signal until the angular deviation becomes 100 degrees or less. • This change incorporates a system message if the LOC cannot capture due to the intercept angle being greater than 105 degrees. The message is “NO NAV CAPTURE - Intercept angle too large for LOC/BC” • If the LOC mode will not capture due to an intercept angle greater than 105 degrees, then a message or indication should be provided to the pilot. (similar to how the VNAV mode provides messages and indications if there is something wrong). Vertical Constraints Improvement: All vertical constraints prior to the active vertical waypoint are now removed from the active flight plan when baro-VNAV is disabled by the pilot. As a result disabling and re-enabling baro-VNAV provides another way (in addition to modifying the FPA, the VS TGT, or initiating a vertical direct-to) to override the effects of any prior vertical constraint and quickly command the baro-VNAV system to base the computed vertical descent on only the current aircraft location and the Citation ATTACHMENT SB510-34-14 • next valid vertical constraint ahead of the aircraft. Note that this change to the vertical flight plan may also affect pathways in some systems that incorporate this navigation library. GFC Transitioning Improvement: Previously when an ILS approach with VECTORS transition was loaded and the FAF waypoint became active due to automatic leg sequencing the CDI immediately switched from GPS to LOC as designed. However, if this automatic transition occurred when the GFC 700 was GPS-coupled, it would cancel the GPS-coupled mode and transition to wings-level (ROL) mode. In GDU software version 11.10, the behavior of VECTORS transitions was changed to include waypoints before the FAF, making it more likely for the FAF to become active due to automatic leg sequencing while flying GPS-coupled. For example, flying direct to one of these approach waypoints prior to the FAF will result in the FAF eventually becoming active as a result of automatic leg sequencing. This change allows the autopilot to remain GPS-coupled until the LOC is captured seamlessly, rather than reverting to wings-level (ROL) mode, when an automatic GPS to ILS source change occurs as a result of automatically sequencing to a VECTORS transition. OWNER ADVISORY Citation SB510-34-14 TITLE NAVIGATION - GARMIN G1000 SOFTWARE VERSION 010-00435-24 UPGRADE TO: Cessna Aircraft Owner REASON The 010-00435-24 software provides fixes and enhancements to the Garmin G1000 avionics system. This service bulletin corrects issues that are defined in the service letters that follow: • • • SL510-34-17Navigation - Transmittal Of Garmin Service Advisory No. 1101 - GDL 69/69A TFR (Temporary Flight Restrictions) Reporting Issue SL510-34-19 Navigation - Transmittal Of Garmin Service Advisory No. 1118 - Momentary Failure Indications (Red X) Can Occur When Sorting Stored Flight Plans SL510-34-20 Navigation - Transmittal Of Garmin Service Advisory No. 1129 - Momentary Loss Of GRS 77/77H And GDC 74A/74B/74H Functions COMPLIANCE MANDATORY. This service bulletin must be accomplished by November 15, 2012. LABOR HOURS WORK PHASE MAN-HOURS Modification 3.5 MATERIAL AVAILABILITY PART NUMBER AVAILABILITY COST SB510-34-14 * * * 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: [email protected] or telefax at 1-316-517-7711. Based on availability and lead times, parts may require advanced scheduling. The customer will be responsible for the cost of parts and labor if this service bulletin is completed after November 15, 2012. SB510-34-14 Page 1 of 2 May 4, 2012 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-5800, Fax 1-316-517-7271, Email: [email protected] COPYRIGHT © 2012 Citation OWNER ADVISORY SB510-34-14 WARRANTY This bulletin is mandatory. Eligible airplanes may qualify for parts and labor coverage, as described below. Eligibility: All Citations identified within the serial number effectivity of this service bulletin. Parts Coverage: Cessna-owned and Cessna-authorized Citation Service Facilities, operators, or other maintenance facilities may submit a Citation Credit Claim Form for the parts required to accomplish this bulletin. Labor Coverage: Cessna-owned and Cessna-authorized Citation Service Facilities may submit a Citation Credit Claim Form for the labor necessary to accomplish this service bulletin. Please note Manpower Requirements for coverage guidelines. Credit Application: All work must be completed and the Citation Credit Claim Form submitted before the date shown below. Send the Citation Credit Claim, along with any required parts (see Material Information), to the point of purchase. Parts to be returned to Cessna Service Parts & Programs should be forwarded to: Citation Warranty Administration 7121 Southwest Boulevard Wichita, KS USA 67215 Expiration: December 31, 2012 NOTE: As a convenience, service documents are now available online to all our customers through a simple, free-of-charge registration process. If you would like to sign up, please visit the "Customer Access" link at www.cessnasupport.com to register. SB510-34-14 Page 2 May 4, 2012
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Key Features
- Garmin G1000 software upgrade
- Fixes and enhancements
- Configuration options
- Detailed installation instructions
- Verification procedures
- Mandatory compliance
Frequently Answers and Questions
What is the purpose of this service bulletin?
This service bulletin mandates upgrading Garmin G1000 software to version 010-00435-24, which includes fixes and enhancements.
When is this service bulletin due?
This service bulletin is mandatory and must be completed by November 15, 2012.
What is included in this service bulletin?
It includes parts and instructions for upgrading the Garmin G1000 software to version 010-00435-24. The document also covers the configuration of different options, verification steps, and compliance requirements.