TITLE NAVIGATION - GARMIN G1000 SYSTEM SOFTWARE UPGRADE TO VERSION 0534.21 (WAAS-ENABLED INSTALLATIONS ONLY) EFFECTIVITY Group A airplanes The airplanes that follow that are equipped with the Garmin G1000 Integrated Avionics System and thewideareaaugmentationsystem(waas): MODEL SERIAL NUMBERS 350 (LC42 550FG) 42559, 421001, 421003 thru 421020 400 (LC41 550FG) 41581, 411002 thru 411087, 411089 thru 411158, 411160, 411161 Group B airplanes The airplanes that follow that have incorporated SB09-34-03 (or latest revision) GARMIN G1000 GPS/WAAS Installation: MODEL SERIAL NUMBERS 350 (LC42 550FG) 42502 thru 42558, 42560 thru 42569, 421002 400 (LC41 550FG) 41034, 41563 thru 41580, 41582 thru 41650, 41652 thru 41800, 411001 REASON This version 0534.21 software service bulletin provides an upgrade that includes the following changes: Enabled Flight Plan Enhancements To simplify flight plan entry, a precursor and an arrow are added to the flight plan page. They are displayed to the left of the waypoint or blank entry that the cursor or the precursor currently inhabits. NEXRAD and Stormscope Display The display of Stormscope (an active lightning sensor) and NEXRAD (a data link weather product) are no longer exclusive. Inset Map Restoration The state of the inset map will now be restored correctly on power cycle. Map Range Limits Minimum zoom range is now limited to 10 nautical miles for XM and to 25 nautical miles for Stormscope. Vertical Waypoints at Holding Fix The correct along-track distance is now used to compute the vertical deviation, which eliminates discontinuity. METAR Observation Time Time is now added to the decoded display of METAR information on the waypoint airport weather page. TFR Time Format 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. Winds Aloft Legend An added winds aloft legend is added to the legend that is displayed on the main navigation page. Terrain Map Aviation Data Changed the MAP - TERRAIN PROXIMITY page (also known as the TAWS map page) to display aviation data (non-flight plan airports and runways) by default. METAR Display The logic to display the text of a METAR in yellow when it is more than 75 minutes old was removed. Now the color stays constant at all times. Display of Weather Information Enhanced the display of weather information on the weather and map pages. July 15, 2014 Page 1 of 9 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 2014
Selected Unit Consistency Added support for pilot selected units to be used more consistently throughout the weather pages and in weather information. METAR Wind Direction Digits Decoded wind direction in METARs is now always reported as a three-digit number to avoid any confusion. Weather Product Cursor Select Priority Cursor select order was changed to allow point products to have higher priority than area products. Resolution for Garmin Service Advisory No. 1129 Rev A Momentary loss of GRS 77 and GDC 74A functions as addressed in Cessna Service Newsletter SNL11-18. Approach Identifiers Added the ability to check for approaches with 3-numeric approach identifiers so that WAAS LPV approaches with 3-numeric identifiers would be available; software fix to Garmin Service Advisory No.: 0825. Flight Plan Sorting The functionality of sorting the stored flight plans was removed; software fix to Garmin Service Advisory No.: 1118. Graphical METARs The display of graphical METARs is added to the active flight plan page and moving maps. METAR Text RawMETARtextisdisplayedontheactiveflightplanpageandmovingmapswhena METAR flag is highlighted with the map cursor. Weather Legend A weather legend is added to the maps that share the weather-related soft keys (NEXRAD, XM, LTNG, and METAR). The display of this legend is controlled via the Legend soft key in the MAP tier of soft keys. METAR Search Radius The active flight plan page can now be configured to show a METAR flag (and corresponding report) from a nearby location for any waypoint in the flight plan without an active reporting station. The search radius is set to 30 NM. Selected-Altitude Intercept Arc A Selected-Altitude Intercept Arc is displayed on the moving maps that follow: Navigation map, PFD inset map, AUX - Trip Planning map, Active Flight Plan page map, and all NRST maps. A cyan arc is drawn across the active leg (when enabled via the Map Setup) to indicate the location at which the aircraft will reach the selected altitude based on the current barometric altitude, vertical speed, and ground speed. Runway Highlights SVT no longer renders a runway highlight on the PFD synthetic view when there is obscuring terrain between the current aircraft position and the runway. Dual Navigation Databases This feature allows a future navigation database to be stored in a standby location on the SD card in the bottom slot of each GDU. When the standby database becomes effective (as determined by the system date and time) the standby database will be automatically loaded into the active location internal to the GDU. This allows users to proactively update their aircraft with the next navigation cycle as soon as it becomes available, rather than having to wait until the first effective date to switch over. Database Crossfill This feature allows most databases to be automatically cross-filled from the bottom SD card in one GDU to the bottom SD card in the other GDU. The following databases are supported: Basemap, Terrain, Airport Terrain, Obstacle, SafeTaxi, Airport Directory, and Standby Navigation. Startup Screen When the dual navigation database feature is active, the Garmin startup screen is now displayed for up to 150 seconds at power up, when necessary, while the internal navigation database is updating. The following message is displayed on the screen: "Please Wait. Navigation Database Update in Progress. Do Not Remove Power from Displays". If the database update has not completed during the allotted time, an error message is then displayed on the MFD and the navigation database is disabled for that power cycle. DB SYNC Manual control of the DB SYNC function is removed. Geometric Altitudes All GPS-derived geometric altitudes that are referenced to sea level are now displayed using the label "GSL". Voice Call-Out Alerts Voice call-out alerts issued within 5 NM of a runway threshold are now based only upon the GPS height above that runway threshold. Pilot-Selectable MGRS Position Format This configuration item enables the ability to display GPS position according to the Military Grid Reference System, and is controlled by a new setting on the AUX System Setup page. DESCRIPTION This service bulletin provides parts and instructions to upgrade the Garmin G1000 software on WAAS-enabled installations to version 0534.21. Page 2 July 15, 2014
COMPLIANCE MANDATORY. This service bulletin must be accomplished within the next 200 hours of operation or 12 months, whichever occurs first. NOTE: Existing Garmin software backup CDs shall be destroyed and discarded to eliminate the possibility of loading the incorrect software at a later date. NOTE: Cessna Service Bulletin SB08-34-05 (G1000 System Software Upgrade to GDU 8.10 Version 534.09), if not already accomplished, must be accomplished prior to compliance with this service bulletin. SD cards of 2 GB or smaller capacity must be used to complete SB08-34-05. APPROVAL Cessna received FAA approval for the technical data in this publication that changes the airplane type design. Cessna received EASA approval for the technical data in this publication that changes the airplane type design. WEIGHT AND BALANCE INFORMATION Negligible REFERENCES Model LC42-550FG Maintenance Manual Model LC41-550FG Maintenance Manual Cessna Service Newsletter SNL11-13, Garmin G1000 AOPA Database Display for Airplanes Equipped with the Garmin G1000 Integrated Avionics System Garmin G1000 Integrated Flight Deck Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT, Part Number 190-00567-05 Revision A (or latest revision) G1000 Integrated Flight Deck Pilot's Guide for the Cessna Corvalis/Corvalis TT, Part Number 190-00552-05 Rev. A (or latest revision) The following document can be viewed by Cessna Authorized Service Facilities by going to www.garmin.com: Garmin G1000 Line Maintenance Manual, (Cessna 350/400), Part Number 190-00577-03, Revision H (or latest revision) NOTE: Make sure all publications used are complete and current. Refer to www.cessnasupport.com. NOTE: This information shall be considered an amendment to the Cessna Manufacturer's Service/Maintenance Manual and should be accomplished within the specified time requirement. PUBLICATIONS AFFECTED Model 350 Illustrated Parts Catalog Model 400 Illustrated Parts Catalog NOTE: Make sure all publications used are complete and current. Refer to www.cessnasupport.com. ACCOMPLISHMENT INSTRUCTIONS General Information NOTE 1: This software update only supports installations that are WAAS-enabled airplanes. If the aircraft is not a WAAS-enabled aircraft do not perform this software update. Cessna Service Bulletin SEB-34-06, Garmin G1000 System Software Update to Version 0563.21 (Non- WAAS Installations Only) supports installations that are for Non-WAAS airplanes. July 15, 2014 Page 3
NOTE 2: If the system software or configuration fails to upload correctly during accomplishment of this Service Bulletin, do the upload again. Do not try to upload more than five times. If the system does not upload after the fifth attempt, refer to the Line Maintenance Manual, (Cessna 350/400), Part Number 190-00577-03, Revision H or later, chapter 4 Software / Configuration Troubleshooting. If the system still does not upload, contact Cessna Propeller Aircraft Product Support: Telephone 316-517-5800 or FAX 316-517-7271. Do not cancel a software or configuration upload that is in progress. Let the system either successfully load or fail. NOTE 3: If the alert chime comes on at any time during the accomplishment of this Service Bulletin, you can go to the Alert Configuration page in the GDU page group, push the soft key directly below the ACK, and this should make the chime stop. 1. Apply power to the airplane using an external power unit. 2. Turn on the G1000 in configuration and / or normal mode and look at the MFD to verify existing options. A. (Refer to TABLE 1.) Record which options are installed for later reference. If you do not know which options are installed on your airplane, use TABLE 2 to make a list of the installed options before you go to Step 3. This list is necessary to do the correct software upload and configuration. Record in TABLE 2 all installations and configuration options necessary for the airplane. TABLE 1 Model 350/400 350/400 AIRPLANE MODEL CONFIGURATION FILE SELECTIONS Cessna (Model) WAAS Baseline NOTE: Model is either 350 or 400. It is critical to select the correct model baseline. Cessna (Model) Non-Adjusted 49 Gal Fuel Tank Option or Cessna (Model) Adjusted 49 Gal Fuel Tank Option NOTE: Model is either 350 or 400. NOTE: The 51-gallon option is configured by default with the baseline. These configuration files are only installed for the 49-gallon option. If the airplane serial number is in the serial range that follows, then it is equipped with 51-gallon tanks, and it is not necessary to load either configuration file listed above. Model 350 (LC42): 42568, 42569, 421001 and later Model 400 (LC41): 41800, 411001 and later. NOTE: If Service Letter SL-07-008 has been accomplished on the airplane, OR if the airplane serial number is in the serial range that follows, then it is equipped with 49-gallon adjusted option: Model 350 (LC42): 42565 thru 42567 Model 400 (LC41): 41758 thru 41799. NOTE: If Service Letter SL-07-008 has not been accomplished on the airplane AND the airplane serial number is in the serial range that follows, then it is equipped with the Cessna (Model) Non-Adjusted 49 Gal Fuel Tank Option: Model 350 (LC42): 42502 thru 42564 Model 400 (LC41): 41563 thru 41650, 41652 thru 41757. TCAD 9900BX / TAS 620 NOTE: The TCAD /TAS system can be identified by the presence of a single, small, 3-inch shark fin antenna just above and aft of the cabin doors and a dual 3-inch shark fin antenna mounted on the belly inspection panel. Oxygen Outlet Low Press (16.5-33 PSI) NOTE: Load this configuration file on all Model 400 airplanes. Do not load this configuration file on Model 350 airplanes. Page 4 July 15, 2014
350/400 AIRPLANE MODEL CONFIGURATION FILE SELECTIONS KN63 DME NOTE: If the airplane is equipped with a DME system, there is a 2-inch (shark fin) transponder / DME antenna on the belly of the airplane forward of the left main landing gear leg at approximately FS 111.00. Becker 3502 ADF NOTE: If the airplane is equipped, there is a large antenna on the belly of the airplane in the tail area, below the baggage compartment at approximately FS 202.00. It is installed with three screws. NOTE: Do not load both the KR 87 ADF option and the Becker 3502 ADF option. KR 87 ADF NOTE: If the airplane is equipped with a KR 87 ADF system, there will be a Bendix/King KR 87 control unit mounted in the instrument panel. NOTE: Do not load both the KR 87 ADF option and the Becker 3502 ADF option. GDL 69A Removal NOTE: This applies only to airplanes that do not use the GDL 69A. Look at the Aux System Status page on the MFD. If the airplane is equipped with GDL-69A, "GDL 69" will be shown in the LRU info window. Load this configuration file if a GDL-69A is not installed. Disable SVT Pathways Option NOTE: This configuration option is obsolete. Do not load this configuration file. WX 500 NOTE: Install this option if Tactical Weather Detection System TWX670 is installed and communicates with the G1000 by emulating the WX 500. This aftermarket STC installation can typically be identified by a pill-shaped antenna on the top of the aircraft near FS 168.00. Do not select this option if a standalone display, such as the Avidyne MHD300, is installed to display the TWX670 data. TABLE 2 Configuration Selections Cessna (Model) WAAS Baseline NOTE: Use this table to list the necessary configuration uploads for the specified airplane installation. B. GotothesystemstatuspageontheMFDtomakesurethattheCOdetectorisconfigured. July 15, 2014 Page 5
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. 3. Do the preparation of the airplane for the software update as follows: A. Remove the GDU Supplemental Data SD Cards from the bottom slot of the PFD and mark it as a PFD card. B. Do Step 3A again for the MFD, and mark the SD card as an MFD card. C. Remove the electronic checklist SD card from the top slot of the MFD as applicable. (1) If the SD cards are Garmin P/N 010-00330-43, go to Step 4. (2) If the SD cards are not Garmin P/N 010-00330-43, go to Step 5. 4. Remove the AOPA database from the 010-00330-43 database cards. If you do not remove the AOPA database file, a system error will occur because the previous system software will make the AOPA database invalid. A new AOPA database must be downloaded for access to the AOPA Airport Directory, and is available for purchase at www.flygarmin.com. Refer to Cessna SNL11-13 for more information. A. Airplanes that have installed software version 0534.16 with Cessna Service Bulletin SB11-34-03 GARMIN G1000 SYSTEM SOFTWARE UPGRADE TO VERSION 0534.16, go to Step 5. The AOPA database was removed with the accomplishment of SB11-34-03. B. Airplanes that have not installed software version 0534.16 with Cessna Service Bulletin SB11-34-03 GARMIN G1000 SYSTEM SOFTWARE UPGRADE TO VERSION 0534.16, do as follows to remove the AOPA database from the 010-00330-43 database cards: (1) Put the first 010-00330-43 database card into a PC card reader and install the card reader in a Windows PC. (2) Use Windows Explorer to navigate through the contents of the database card. (3) Go to Tools, then Folder Options, and then View tab. (a) Select Show hidden files and folders. (b) Uncheck Hide protected operating system files (Recommended)". (4) Look for the file apt_dir.gca. If it shows, select and delete it. (5) Remove the database card from the PC. (6) Do Step 4B(1) thru 4B(5) again for the second 010-00330-43 card. (7) Store the cards in a safe location for later installation. 5. Load the GDU (PFD and MFD) software as follows: A. Make sure that all switches are in the OFF/NORM position. B. Make sure that no SD cards are installed in the PFD and MFD slots. C. Make sure that the PFD and the MFD circuit breakers are disengaged. D. Insert the 010-00530-21 Software Loader Card into the top card slot of the MFD. E. Put the left and the right BATTERY MASTER switches (on the overhead console) to the ON position. F. Put the CROSSTIE switch and the AVIONICS MASTER switch to the ON position. G. Push and hold the ENT key on the MFD and engage the MFD circuit breaker. H. Release the softkey after the INITIALIZING SYSTEM message appears on the MFD. I. Push the YES soft key to upload GDU system files when the DO YOU WANT TO UPDATE SYSTEM FILES? message appears. Page 6 July 15, 2014
J. If the DO YOU WANT TO UPDATE THE SPLASH SCREEN? message appears, push the YES soft key. K. Push the ENT key when the splash screen update is complete and you are asked to PRESS ANY SOFTKEY TO CONTINUE. L. Software load to the MFD is complete when the display starts into configuration mode. M. Leave the MFD display powered on. N. Remove the 010-00530-21 Software Loader Card from the MFD and insert it into the top PFD slot. O. Engage the PFD circuit breaker and do Steps 5G thru 5M again for the PFD. 6. Initial software load and configuration upload. A. TurnthesmallFMSknobonthePFDtogotothesystemgroupSYSTEMUPLOADpage. B. Push the small FMS knob to start the cursor. C. Turn the small FMS knob to highlight the applicable airplane model from the group menu option and push the ENT key. D. Turn the small FMS knob, select the applicable Cessna (Model Number) WAAS Baseline menu option and push the ENT key. NOTE: The software included in the 010-00530-21 Software Loader Card will automatically determine which files must be loaded. E. Press the LOAD softkey to load selected software/config items. Periodically monitor the loading process for failures. A green PASS message is shown beside software and configuration 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/configuration item that failed. Press enter to acknowledge the fail message and to continue the same software/configuration load. If unable to load the software/configuration item after several attempts, uncheck the software and configuration boxes associated with the item using the ENT soft key and FMS knobs and press the LOAD soft key to continue with the rest of the software load before troubleshooting cause of failure. F. Monitor the upload status. When the Upload Complete message is shown, push the ENT key to select OK. 7. For airplanes equipped with additional items as shown in TABLE 1 (refer to TABLE 2), do the necessary uploads as follows: NOTE: While you select additional items, you may have to change the Group menu from specific model (C350 or C400) to options menu. NOTE: Thiscantakeupto90minutes. WARNING: Do not configure an option that is not installed on the airplane. A. Turn the large FMS knob counterclockwise to go to the ITEM menu. B. Turn the small FMS knob to expand the ITEM pull down menu field and highlight one of the Cessna software uploads that is applicable for your airplane. C. Push the ENT key. D. Push the LOAD soft key to install the software. E. Monitor the upload status. When the Upload Complete message is shown, push the ENT key to select OK. F. Do Steps 7A thru 7E again until all applicable (refer to TABLE 2) software uploads are complete. G. Press the FMS knob to unselect the cursor. July 15, 2014 Page 7
8. Do the PFD configuration module update: A. Push the UPDT CFG softkey. B. Select YES and push the ENT key when the UPDATE CONFIG MODULE? message shows. C. Push the ENT key to select OK after you see the UPDATE CONFIG COMPLETE message. 9. Complete the basic software load and system verification procedures as follows: A. Do the manifest configuration verification: (1) On the PFD, turn the large FMS knob to go to the SYSTEM group. Turn the small FMS knob to go to the MANIFEST CONFIGURATION page. (2) (Refer to TABLE 3.) Make sure that the data file and file version shown in TABLE 3 are shown in the SYSTEM field window. TABLE 3 DATA FILE FILE VERSION 006-B0534-21 0534.21 (3) Make sure that the applicable information shown in TABLE 4 is shown in the MANIFEST field window. NOTE: This data file is near the bottom of the list. TABLE 4 MODEL DATA FILE FILE VERSION 350 006-D0623-03 2.03 400 006-D0456-08 2.08 B. If the Splash Screen did not update in Step 5J, do Step 5 again. This time in Step 5I when the DO YOU WANT TO UPDATE SYSTEM FILES? message appears, push the NO soft key. Now you shouldbeabletoloadthesplashscreeninstep5j. 10. Put the CROSSTIE switch and the AVIONICS MASTER switch in the off position. 11. Put the left and the right BATTERY MASTER switches in the off position. 12. Disengage the PFD circuit breaker. 13. Remove the SD card from the top slot on the PFD. 14. Do the system checks as follows: A. Install the GDU Supplemental Data SD Card in to the bottom slot on the PFD and the MFD units from which they were removed. B. Install the Electronic Checklist SD Card in to the top slot on the MFD, if applicable. C. Engage the PFD circuit breaker. D. Put the left and the right BATTERY MASTER switch to the ON position. E. Put the CROSSTIE and the AVIONICS MASTER switches in the ON position. F. After the system has fully initialized, make sure that no G1000 system messages, alerts, annunciations, or Red X s are shown on the PFD or the MFD on the AUX-SYSTEM STATUS page. NOTE: Reference Garmin Line Maintenance Manual 190-00577-03 Revision H (or later revision) for troubleshooting instructions. Page 8 July 15, 2014
G. Make sure that the GFC-700 Pre-Flight Test completed successfully. If not, refer to Section 2.10 of the Garmin G1000 System Maintenance Manual. (Refer to the Garmin G1000 System Maintenance Manual, Part Number 190-00577-03, Revision H (or latest revision.) 15. (For airplanes equipped with TAWS-B) Do the Enablement of Garmin G1000 Terrain Awareness Warning System Class-B (TAWS-B). Refer to SB10-34-01 Original Revision or later and do the steps that install TAWS-B. 16. (For airplanes equipped with Chartview) Do the Garmin G1000 Avionics Chartview Option, SB08-34-06 Revision 1 or later. 17. (For airplanes equipped with Garmin Synthetic Vision Technology) Do the Enablement of Garmin G1000 Synthetic Vision Installation, SB10-34-02 (or latest revision). 18. Put the CROSSTIE and the AVIONICS MASTER switches in the off position. 19. Put the left and the right BATTERY MASTER switches in the off position. 20. Remove external power. 21. Make an entry in the airplane logbook that states compliance and method of compliance with this service bulletin. MATERIAL INFORMATION Order the parts below to install this service bulletin: NOTE: 190-00552-05REVA Garmin G1000 Pilot's Guide for Cessna 350/400 is optional. NEW P/N QUAN- TITY KEY WORD OLD P/N INSTRUCTIONS/ DISPOSITION 010-00530-21 1 Software Loader Card CORGSW00-01 and prior revisions 190-00567- 05REVA 190-00552- 05REVA 1 Garmin G1000 Integrated Flight Deck Cockpit Reference Guide for Cessna 350/400 1 Garmin G1000 Pilot s Guide for Cessna 350/400 190-00567-04 and prior revisions 190-00552-04 and prior revisions *You are replacing a CD (CORGSW00-01 and prior revisions) with an SD card (010-00530-21). Destroy and Discard* Remove and Replace Remove and Replace July 15, 2014 Page 9
OWNER ADVISORY TITLE NAVIGATION - GARMIN G1000 SYSTEM SOFTWARE UPGRADE TO VERSION 0534.21 (WAAS-ENABLED INSTALLATIONS ONLY) TO: Cessna Corvalis Owner REASON This owner advisory is to inform you that has been issued. This version 0534.21 software service bulletin provides an upgrade that includes the following changes: Enabled Flight Plan Enhancements To simplify flight plan entry, a precursor and an arrow are added to the flight plan page. They are displayed to the left of the waypoint or blank entry that the cursor or the precursor currently inhabits. NEXRAD and Stormscope Display The display of Stormscope (an active lightning sensor) and NEXRAD (a data link weather product) are no longer exclusive. Inset Map Restoration The state of the inset map will now be restored correctly on power cycle. Map Range Limits Minimum zoom range is now limited to 10 nautical miles for XM and to 25 nautical miles for Stormscope. Vertical Waypoints at Holding Fix The correct along-track distance is now used to compute the vertical deviation, which eliminates discontinuity. METAR Observation Time Time is now added to the decoded display of METAR information on the waypoint airport weather page. TFR Time Format 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. Winds Aloft Legend An added winds aloft legend is added to the legend that is displayed on the main navigation page. Terrain Map Aviation Data Changed the MAP - TERRAIN PROXIMITY page (also known as the TAWS map page) to display aviation data (non-flight plan airports and runways) by default. METAR Display The logic to display the text of a METAR in yellow when it is more than 75 minutes old was removed. Now the color stays constant at all times. Display of Weather Information Enhanced the display of weather information on the weather and map pages. Selected Unit Consistency Added support for pilot selected units to be used more consistently throughout the weather pages and in weather information. METAR Wind Direction Digits Decoded wind direction in METARs is now always reported as a three-digit number to avoid any confusion. Weather Product Cursor Select Priority Cursor select order was changed to allow point products to have higher priority than area products. Resolution for Garmin Service Advisory No. 1129 Rev A Momentary loss of GRS 77 and GDC 74A functions as addressed in Cessna Service Newsletter SNL11-18. Approach Identifiers Added the ability to check for approaches with 3-numeric approach identifiers so that WAAS LPV approaches with 3-numeric identifiers would be available; software fix to Garmin Service Advisory No.: 0825. Flight Plan Sorting The functionality of sorting the stored flight plans was removed; software fix to Garmin Service Advisory No.: 1118. Graphical METARs The display of graphical METARs is added to the active flight plan page and moving maps. METAR Text Raw METAR text is displayed on the active flight plan page and moving maps when a METAR flag is highlighted with the map cursor. July 15, 2014 Page 1 of 3 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 2014
OWNER ADVISORY Weather Legend A weather legend is added to the maps that share the weather-related soft keys (NEXRAD, XM, LTNG, and METAR). The display of this legend is controlled via the Legend soft key in the MAP tier of soft keys. METAR Search Radius The active flight plan page can now be configured to show a METAR flag (and corresponding report) from a nearby location for any waypoint in the flight plan without an active reporting station. The search radius is set to 30 NM. Selected-Altitude Intercept Arc A Selected-Altitude Intercept Arc is displayed on the moving maps that follow: Navigation map, PFD inset map, AUX - Trip Planning map, Active Flight Plan page map, and all NRST maps. A cyan arc is drawn across the active leg (when enabled via the Map Setup) to indicate the location at which the aircraft will reach the selected altitude based on the current barometric altitude, vertical speed, and ground speed. Runway Highlights SVT no longer renders a runway highlight on the PFD synthetic view when there is obscuring terrain between the current aircraft position and the runway. Dual Navigation Databases This feature allows a future navigation database to be stored in a standby location on the SD card in the bottom slot of each GDU. When the standby database becomes effective (as determined by the system date and time) the standby database will be automatically loaded into the active location internal to the GDU. This allows users to proactively update their aircraft with the next navigation cycle as soon as it becomes available, rather than having to wait until the first effective date to switch over. Database Crossfill This feature allows most databases to be automatically cross-filled from the bottom SD card in one GDU to the bottom SD card in the other GDU. The following databases are supported: Basemap, Terrain, Airport Terrain, Obstacle, SafeTaxi, Airport Directory, and Standby Navigation. Startup Screen When the dual navigation database feature is active, the Garmin startup screen is now displayed for up to 150 seconds at power up, when necessary, while the internal navigation database is updating. The following message is displayed on the screen: "Please Wait. Navigation Database Update in Progress. Do Not Remove Power from Displays". If the database update has not completed during the allotted time, an error message is then displayed on the MFD and the navigation database is disabled for that power cycle. DB SYNC Manual control of the DB SYNC function is removed. Geometric Altitudes All GPS-derived geometric altitudes that are referenced to sea level are now displayed using the label "GSL". Voice Call-Out Alerts Voice call-out alerts issued within 5 NM of a runway threshold are now based only upon the GPS height above that runway threshold. Pilot-Selectable MGRS Position Format This configuration item enables the ability to display GPS position according to the Military Grid Reference System, and is controlled by a new setting on the AUX System Setup page. provides parts and instructions to upgrade the Garmin G1000 software on WAAS-enabled installations to version 0534.21. COMPLIANCE MANDATORY. This service bulletin must be accomplished within the next 200 hours of operation or 12 months, whichever occurs first. NOTE: Existing Garmin software backup CDs shall be destroyed and discarded to eliminate the possibility of loading the incorrect software at a later date. NOTE: Cessna Service Bulletin SB08-34-05 (G1000 System Software Upgrade to GDU 8.10 Version 534.09), if not already accomplished, must be accomplished prior to compliance with this service bulletin. SD cards of 2 GB or smaller capacity must be used to complete SB08-34-05. LABOR HOURS 2.0 man-hours to load the software upgrade. WARRANTY For all airplanes identified within the serial effectivity and complying within 200 hrs or twelve months from the date of this service bulletin, whichever occurs first: Applicable CRG and Software CD parts credit and a labor allowance credit of 2.0 man-hours per airplane will be provided to accomplish this service bulletin. Page 2 July 15, 2014
OWNER ADVISORY Freight will be credited at the most economical method unless pre-approved by Cessna. To receive credit, the work must be completed within stated compliance timeframe and a warranty claim submitted by a Cessna Single- Authorized Service Facility within 30 calendar days of service bulletin compliance before the credit expiration dates shown below. Domestic... July 15, 2015 International... July 15, 2015 Please contact a Cessna Authorized Service Facility for detailed information and arrange to have Cessna service bulletin accomplished on your airplane. Special Note to Authorized Service Facilities: When you complete the warranty claim, the labor allowance claimed shall be itemized for each above action completed. Access the QR code for the instructional video link that follows or use the URL address: Select this link: http://textron.vo.llnwd.net/o25/ces/customerservice//.html NOTE: As a convenience, service documents are now available online to all our customers through a simple,free-of-chargeregistrationprocess.ifyouwouldliketosignup,pleasevisitthe"customer Support Login" link at www.cessna.com to register. July 15, 2014 Page 3