SERVICE BULLETIN REVISION TRANSMITTAL

REVISION TRANSMITTAL TO: Cessna Distributors, Single Authorized Service Facilities and CPC's SUBJECT: Single Service Bulletin Revision 2: Navigation - Garmin G1000 System Software Upgrade to Version 0563.26 for Airplanes Equipped with NAV III (WAAS-Enabled Installations Only) REASON To add airplane serials 18281869, T18208665, 20608279, and T20608682 to the Effectivity section. Miscellaneous changes as required. Please replace any copy of Revision 1 with the attached copy of Revision 2, which is printed in its entirety. NOTE: Compliance with Revision 2 is not required if in compliance with the Original Issue or Revision 1. LOG OF REVISIONS Page No. Date Page No. Date 1 March 13, 2013 9 March 13, 2013 2 March 13, 2013 10 March 13, 2013 3 March 13, 2013 11 March 13, 2013 1 March 13, 2013 12 March 13, 2013 5 March 13, 2013 13 March 13, 2013 6 March 13, 2013 14 March 13, 2013 7 March 13, 2013 15 March 13, 2013 8 March 13, 2013 16 March 13, 2013 Original Issue - March 27, 2012 Revision 2 - March 13, 2013 Page 1 of 1 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-5800, Fax 1-316-517-7271, Email: customercare@cessna.textron.com COPYRIGHT 2012

TITLE NAVIGATION - GARMIN G1000 SYSTEM SOFTWARE UPGRADE TO VERSION 0563.26 FOR AIRPLANES EQUIPPED WITH NAV III (WAAS-ENABLED INSTALLATIONS ONLY) EFFECTIVITY Group A airplanes The airplanes that follow that are equipped with the Garmin G1000 Nav III Avionics Option and the Wide Area Augmentation System (WAAS): MODEL SERIAL NUMBERS 172R 17281357 thru 17281612 172S 172S10432 thru 172S11183 182T 18281869, 18281876 thru 18282323 T182T T18208354, T18208665, T18208669 thru T18209067 206H 20608279, 20608284 thru 20608339 T206H T20608682, T20608705 thru T20609052 Group B airplanes The airplanes that follow that have incorporated SB07-34-07 (or latest revision) GARMIN G1000 GPS/WAAS Installation: MODEL SERIAL NUMBERS 172R 17281241 thru 17281356 172S 172S9810 thru 172S10431 182T 18281228, 18281318 thru 18281868, 18281870 thru 18281875 T182T T18208232 thru T18208353, T18208355 thru T18208664, T18208666 thru T18208668 206H 20608216 thru 20608278, 20608280 thru 20608283 T206H T20608450 thru T20608681, T20608683 thru T20608704 REASON This version 0563.26 software service bulletin provides an upgrade that includes the following changes: Resolution for Garmin Service Advisory No. 1129 Rev A Momentary loss of GRS 77 and GDC 74A functions as addressed in Cessna Service Newsletter SNL11-15. 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. Original Issue - March 27, 2012 Revision 2 - March 13, 2013 Page 1 of 16 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: customercare@cessna.textron.com 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 2012

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. 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. Profile View The profile view option is added to the MFD Navigation Map. When enabled, the airplane's vertical position over terrain and obstacles is shown centered on the current ground track. When datalink weather is available, winds aloft information is also shown, which depicts a headwind or tailwind as a function of altitude. This vertical profile view is pilot configurable. Circular SAR Pattern A circular search and rescue pattern is now available with the accomplishment of Cessna Service Bulletin SEB-34-01 Garmin G1000 Enhanced Search and Rescue Enablement. 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. Improved Lighting Curve The lighting curve has been updated for the displays and their bezels to provide more optimal dimming characteristics while under manual control with the dimming potentiometer. 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. Waypoint Arrival Alerts This configuration item enables the 'arriving at [waypoint]' advisory alert when the aircraft is 10 seconds away from reaching the arrival alert distance to the destination waypoint. DESCRIPTION This service bulletin provides parts and instructions to upgrade the Garmin G1000 software on WAAS-enabled installations to version 0563.26. Page 2 Revision 2 - March 13, 2013

COMPLIANCE MANDATORY. This service bulletin must be accomplished within the next 200 hours of operation or 12 months, whichever occurs first. NOTE: For NAV III airplanes equipped with GFC-700 autopilot, Cessna Service Bulletin SB09-34-05 (Garmin G1000 System Software Upgrade to 563.14 for Airplanes Equipped with NAV III and GFC 700 AFCS Autopilot) (or later revision) must be accomplished before compliance with this service bulletin. NOTE: For NAV III airplanes equipped with KAP-140 autopilot, Cessna Service Bulletin SB07-34-02 (Garmin G1000 System Software Upgrade to 563.03) (or later revision) must be accomplished before compliance with this service bulletin. 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: Compliance with Revision 2 is not required if in compliance with the Original Issue or Revision 1. 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. REFERENCES Model 172 Series 1996 and On Maintenance Manual Model 182/T182T Series 1997 and On Maintenance Manual Model 206/T206 Series 1998 and On Maintenance Manual Garmin G1000 Cockpit Reference Guide for Cessna NAV III, Part Number 190-00384-12 Rev. A. Garmin G1000 Pilot's Guide for Cessna NAV III, Part Number 190-00498-07 Rev. A. The following documents can be viewed by Cessna Authorized Service Facilities by going to www.garmin.com: Garmin G1000 System Installation Manual, Part Number 190-00303-00, Revision H (or latest revision) Garmin GDU 1040 Installation Manual, Part Number 190-00303-01, Revision V (or latest revision) Garmin GMA 1347 Installation Manual, Part Number 190-00303-20, Revision E (or latest revision) Garmin GIA 63 Installation Manual, Part Number 190-00303-05, Revision J (or latest revision) Garmin GRS 77/GMU 44 Installation Manual, Part Number 190-00303-10, Revision Q (or latest revision) Garmin GDC 74A Installation Manual, Part Number 190-00303-15, Revision H (or latest revision) Garmin GEA 71 Installation Manual, Part Number 190-00303-40, Revision G (or latest revision) Garmin GTX 33 Installation Manual, Part Number 190-00303-61, Revision J (or latest revision) Garmin G1000 NAV III Line Maintenance Manual, Part Number 190-00352-00, Revision P (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. Revision 2 - March 13, 2013 Page 3

PUBLICATIONS AFFECTED Model 172R & Model 172S Illustrated Parts Catalog Model 182S/182T/T182T Illustrated Parts Catalog Model 206H & Model T206H Illustrated Parts Catalog NOTE: Make sure all publications used are complete and current. Refer to www.cessnasupport.com. WEIGHT AND BALANCE INFORMATION Negligible ACCOMPLISHMENT INSTRUCTIONS General Information NOTE 1: This software update only supports NAV III 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-34-03, Garmin G1000 System Software Update to Version 0563.26 for Airplanes Equipped with NAV III (Non- WAAS Installations Only) supports NAV III installations that are for Non-WAAS airplanes. 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 Garmin Line Maintenance Manual, Revision P or later, Appendix B.3 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. Make the 006-B0563-26 Software SD Loader Card as follows: A. Use the new Cessna NAV III Installation software CD shown in TABLE 1 and update the SD Card for the correct model airplane: TABLE 1 INSTALLATION SOFTWARE CD AND GARMIN SYSTEM SOFTWARE (G1000) PART NUMBER 006-B0563-26 FILE VERSION 0563.26 (or later version) B. Right mouse click on the START button in the lower left corner of the computer screen and click on EXPLORE. C. Find the CD drive with the CD in it on your computer and double click it to open the CD file. D. Double click on the file labeled 006-B0563-26_OA.exe. E. When the window opens, click the SETUP button. F. Install a blank SD Card into the SD card reader and click the NEXT button. NOTE: SanDisk is the SD card brand that is recommended by Garmin for use in their G1000 system. G. The next window will ask for your SD card reader location. Select the location of the SD card reader and then click the NEXT button. H. Click the NEXT button when the window opens. NOTE: If there is information on the SD card, it will be erased by the Software Application Builder. Page 4 Revision 2 - March 13, 2013

I. The software will begin to transfer from the CD to the SD Card. J. When the data has transferred to the SD card, click the FINISH button. K. Remove the SD card from the SD card reader and identify the SD card as 006-B0563-26. L. Remove the CD from the computer and install it in the Nav III/Garmin Software sleeve in the Pilot s Operating Handbook (POH). 2. Turn on the G1000 in configuration and / or normal mode to verify existing options. A. (Refer to TABLES 2, 3, and 4.) Record which options are installed for later reference. If you do not know which options are installed on your airplane, use TABLE 5 to make a list of the installed options before you go to Step 5. This list is necessary to do the correct software upload and configuration. Record in TABLE 5 all installations and configuration options necessary for the airplane. NOTE: To stop the alert chime in configuration mode, on the Alert Configuration page in the GDU page group, push the soft key that is below ACK. Revision 2 - March 13, 2013 Page 5

TABLE 2- Model 172R and 172S 172R/172S AIRPLANE MODEL CONFIGURATION FILE SELECTIONS - PULL-DOWN MENU Cessna 172R - 006-B0563-26 Full Configuration (WAAS) or Cessna 172S - 006-B0563-26 Full Configuration (WAAS) NOTE: All GFC-700-equipped 172R/172S airplanes are WAAS airplanes. Cessna 172R - GFC-700 Installation Option (if applicable) or Cessna 172S - GFC-700 Installation Option (if applicable) NOTE: Factory Kits FK172-604, FK172S604, FK172-604E, FK172S604E, FK172-604F, FK271S604F, FK172-604G, and FK172S604G are not equipped with the GFC-700 option. All other 172S and 172R NAV III 2008 and on airplanes are equipped with the GFC-700. Cessna NAV III CO Guardian Installation Option (if applicable) NOTE: All NAV III 2006 and on Model Year airplanes have the CO Guardian installed. Cessna NAV III CAN BUS FUEL LEVEL SENSORS (if applicable) NOTE: All NAV III 2008 and on Model Year airplanes have the CAN BUS FUEL LEVEL SENSORS installed. Cessna NAV III INITIALIZE FUEL CAL DATA (only for CAN Bus sensors before fuel cal) NOTE: Only use if CAN Bus fuel sensors are installed and you do a full fuel calibration for the airplane. Do not select this option unless a fuel calibration is necessary. Loss of fuel calibration data will result, and you will have to do a full fuel calibration. Cessna NAV III GDL90 Installation Option (if applicable) NOTE: The GDL90 is not the same equipment as the GDL69. Cessna NAV III KAP 140 Installation Option (if applicable) NOTE: Use only if a Honeywell KAP 140 AFCS is installed. A KC140 controller is installed in the instrument panel. All 2008 and later Models only installed the Garmin GFC-700 AFCS autopilot. Cessna NAV III KN 63 DME Installation Option (if applicable) NOTE: All airplanes equipped with the Cessna NAV III KN 63 DME installation option have a DME antenna installed on the bottom of the fuselage below the cabin. Cessna NAV III KR 87 ADF Installation Option (if applicable) NOTE: Airplanes equipped with the NAV III KR 87 ADF installation option have a receiver installed on the instrument panel. Cessna NAV III BP 2007 Comant CI 2580-410 Antenna Configuration NOTE: For WAAS equipped airplanes without a stand alone XM Antenna (CI 420-10) Cessna NAV III (Pre 2007 Model Year Airplanes) Comant CI 2480-400 Antenna Configuration NOTE: All Pre 2007 Model Year Airplanes not equipped with WAAS are equipped with the Comant CI 2480-400 antenna. Cessna NAV III Disable SVT Pathways Option (if desired) NOTE: Most installations will not use this option. Cessna Enhanced Vision System (EVS) Option (if applicable) NOTE: EVS-equipped airplanes have an EVS camera installed outboard of right WS 100.00. Page 6 Revision 2 - March 13, 2013

TABLE 3- Model 182T and T182T 182T/T182T AIRPLANE MODEL CONFIGURATION FILE SELECTIONS - PULL-DOWN MENU Cessna 182T - 006-B0563-26 Full Configuration (WAAS) or Cessna T182T - 006-B0563-26 Full Configuration (WAAS) NOTE: All GFC-700 equipped 182T/T182T airplanes are WAAS airplanes. Cessna 182T GFC-700 Installation Option (if applicable) or Cessna T182T GFC-700 Installation Option (if applicable) as applicable NOTE: All 182T and T182T NAV III 2007 and on airplanes are equipped with the GFC-700. Cessna NAV III CO Guardian Installation Option (if applicable) NOTE: All NAV III 2006 and on Model Year airplanes have the CO Guardian installed. Cessna NAV III CAN BUS FUEL LEVEL SENSORS (if applicable) NOTE: All NAV III 2008 and on Model Year airplanes have the CAN BUS FUEL LEVEL SENSORS installed. Cessna NAV III INITIALIZE FUEL CAL DATA (only for CAN Bus sensors before fuel cal) NOTE: Only use if CAN Bus fuel sensors are installed and a full fuel calibration must be performed on the aircraft. Do not select this option unless a fuel calibration is required, otherwise loss of fuel calibration data will result and a full fuel calibration must be performed. Cessna NAV III KTA 870 TAS Installation Option (if applicable) NOTE: All airplanes equipped with the Cessna NAV III KTA 870 TAS have a TAS circuit breaker installed on the circuit breaker panel. NOTE: All airplanes equipped with the Cessna NAV III KTA 870 TAS have a directional TAS antenna installed on the top of the airplane and a TAS antenna installed on the bottom of the airplane. Cessna NAV III KAP 140 Installation Option (if applicable) NOTE: Only use if a Honeywell KAP 140 AFCS is installed. A KC140 controller is installed in the instrument panel. All 2007 and later Models only installed the Garmin GFC-700 AFCS autopilot. Cessna NAV III KN63 DME Installation Option (if applicable) NOTE: All airplanes equipped with the Cessna NAV III KN 63 DME installation option have a DME antenna installed on the bottom of the fuselage below the cabin. Cessna NAV III KR 87 ADF Installation Option (if applicable) NOTE: Airplanes equipped with the NAV III KR 87 ADF installation option have a receiver installed on the instrument panel. Cessna NAV III BP 2007 Comant CI 2580-410 Antenna Configuration NOTE: For WAAS equipped airplanes without a stand alone XM Antenna (CI 420-10). Cessna NAV III (Pre 2007 Model Year Airplanes) Comant CI 2480-400 Antenna Configuration NOTE: All Pre 2007 Model Year Airplanes not equipped with WAAS are equipped with the Comant CI 2480-400 antenna. Revision 2 - March 13, 2013 Page 7

182T/T182T AIRPLANE MODEL CONFIGURATION FILE SELECTIONS - PULL-DOWN MENU Cessna NAV III Disable SVT Pathways Option (if desired) NOTE: Most installations will not use this option. Cessna Enhanced Vision System (EVS) Option (if applicable) NOTE: EVS-equipped airplanes have an EVS camera installed outboard of right WS 100.00. Page 8 Revision 2 - March 13, 2013

TABLE 4- Models 206H and T206H 206H/T206H AIRPLANE MODEL CONFIGURATION FILE SELECTIONS - PULL-DOWN MENU Cessna 206H - 006-B0563-26 Full Configuration (WAAS) or Cessna T206H - 006-B0563-26 Full Configuration (WAAS) as applicable NOTE: All GFC-700 equipped 206H/T206H airplanes are WAAS airplanes. Cessna 206H GFC-700 Installation Option or Cessna T206H GFC-700 Installation Option as applicable NOTE: All 206H and T206H NAV III 2007 and on Model Year airplanes are equipped with the GFC-700. Cessna NAV III CO Guardian Installation Option NOTE: All NAV III 2006 and on Model Year airplanes have the CO Guardian installed. Cessna NAV III CAN BUS FUEL LEVEL SENSORS (if applicable) NOTE: All NAV III 2008 and on Model Year airplanes have the CAN BUS FUEL LEVEL SENSORS installed. Cessna NAV III INITIALIZE FUEL CAL DATA (only for CAN Bus sensors before fuel cal) NOTE: Only use if CAN Bus fuel sensors are installed and a full fuel calibration must be performed on the aircraft. Do not select this option unless a fuel calibration is required, otherwise loss of fuel calibration data will result and a full fuel calibration must be performed. Cessna NAV III KTA 870 TAS Installation Option (if applicable) NOTE: All airplanes equipped with the Cessna NAV III KTA 870 TAS have a TAS circuit breaker installed on the circuit breaker panel. NOTE: All airplanes equipped with the Cessna NAV III KTA 870 TAS have a directional TAS antenna installed on the top of the airplane and a TAS antenna installed on the bottom of the airplane. Cessna NAV III KAP 140 Installation Option (if applicable) NOTE: Only use if a Honeywell KAP 140 AFCS is installed. A KC140 controller is installed in the instrument panel. All 2007 and later Models only installed the Garmin GFC-700 AFCS autopilot. Cessna NAV III KN63 DME Installation Option NOTE: All airplanes equipped with the Cessna NAV III KN 63 DME installation option have a DME antenna installed on the bottom of the fuselage below the cabin. Cessna NAV III KR 87 ADF Installation Option NOTE: Airplanes equipped with the NAV III KR 87 ADF installation option have a receiver installed on the instrument panel. Cessna NAV III BP 2007 Comant CI 2580-410 Antenna Configuration NOTE: For WAAS equipped airplanes without a stand alone XM Antenna (CI 420-10) Cessna NAV III Disable SVT Pathways Option (if desired) NOTE: Most installations will not use this option. Cessna Enhanced Vision System (EVS) Option (if applicable) NOTE: EVS-equipped airplanes have an EVS camera installed outboard of right WS 100.00. Revision 2 - March 13, 2013 Page 9

TABLE 5- Configuration Selections Cessna (Model) 006-B0563-26 Full Configuration (WAAS) NOTE: Use this table to list the necessary configuration uploads for the specified airplane installation. 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 the MFD units. B. Mark the SD Cards PFD or MFD. 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 file must be installed if you want an AOPA database. A. Airplanes that have installed software version 0563.21 with Cessna Service Bulletin SB11-34-01 Garmin G1000 System Software Upgrade to 0563.21 for Airplanes Equipped with NAV III and WAAS, go to Step 5. The AOPA database was removed with the accomplishment of SB11-34-01. B. Airplanes that have not installed software version 0563.21 with Cessna Service Bulletin SB11-34-01 Garmin G1000 System Software Upgrade to 0563.21 for Airplanes Equipped with NAV III and WAAS, do as follows to remove the AOPA database from the 010-00330-43 database cards: (1) Put the 010-00330-43 database card into a PC card reader. (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 Steps 4B(1) thru 4B(5) again for all 010-00330-43 cards. (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. Page 10 Revision 2 - March 13, 2013

B. Connect the airplane to an external power unit. C. Make sure that no SD cards are installed in the PFD and MFD slots. D. Make sure that the PFD (ESS BUS and AVN BUS 1) and the MFD (AVN BUS 2) circuit breakers are disengaged. E. Insert the 006-B00563-26 SD card into the top card slot of the MFD. F. Put the BAT MASTER switch to the ON position. G. Put the AVIONICS MASTER switches to the ON position and put the STDBY BATT switch to ARM. H. Push and hold the ENT key on the MFD and engage the MFD (AVN BUS 2) circuit breaker. I. Release the softkey after the INITIALIZING SYSTEM message appears. J. Push the YES soft key to upload GDU system files when the messages that follows shows: DO YOU WANT TO UPDATE SYSTEM FILES? K. If the message that follows shows, push the YES soft key: DO YOU WANT TO UPLOAD THE SPLASH SCREEN? L. Push the ENT key when the splash screen update is complete and you are asked to PRESS ANY SOFTKEY TO CONTINUE. M. Software load to the MFD is complete when the display starts into configuration mode. N. Leave the MFD display powered on. O. Remove the 006-B00563-26 Garmin SD Card from the MFD and insert it into the top PFD slot. P. Engage the PFD (ESS and AVN BUS 1) circuit breakers and do Steps 5H thru 5M again for the PFD. 6. Initial software load and configuration upload. A. Turn the small FMS knob on the PFD to go to the system group SYSTEM UPLOAD page. 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) 006-B0563-26 Full Configuration (WAAS) item menu option and push the ENT key. NOTE: The software included in the 006-B0563-26 SD 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 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 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. NOTE: This can take up to 60 minutes. Revision 2 - March 13, 2013 Page 11

7. For airplanes equipped with additional items as shown in TABLES 2, 3, or 4 (refer to TABLE 5), do the necessary uploads as follows: NOTE: This can take several minutes for each option. 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 Nav III 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 5) software uploads are complete. G. Press the FMS knob to unselect the cursor. 8. Push the UPDT CFG softkey and then the ENT key to select YES to update the PFD Config module, and push the ENT key to select OK when complete. 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 6.) Make sure that the data file and file version shown in TABLE 6 are shown in the SYSTEM field window. TABLE 6 DATA FILE FILE VERSION 006-B0563-26 0563.26 (3) For NAV III airplanes equipped with GFC-700 autopilot) Make sure that the applicable information shown in TABLE 7 is shown in the MANIFEST field window. NOTE: This data file is near the bottom of the list. TABLE 7 MODEL DATA FILE FILE VERSION 172R/172S 006-D0887-03 2.03 182T/T182T 006-D0270-16 2.06 206H/T206H 006-D0621-15 2.05 B. (For airplanes equipped with CAN BUS Fuel Level Sensors only) Do the fuel configuration verification: (1) On the PFD, turn the large FMS knob to go to the CAL page group. Turn the small FMS knob to go to the FUEL TANK CALIBRATION page. (2) Push the TNK SEL soft key to highlight the CURRENT TANK field. (3) Turn the small FMS knob to expand the drop down menu to highlight the LEFT tank. Page 12 Revision 2 - March 13, 2013

(4) Push the ENT key. (5) On the PFD, make sure that several values in 2.00GL ACTUAL QUANTITY increments are shown in the CALIBRATION TABLE. (a) (b) If several values in 2.00GL ACTUAL QUANTITY increments are shown in the CALIBRATION TABLE, go to Step 9B(6). If several values in 2.00GL ACTUAL QUANTITY increments are not shown in the CALIBRATION TABLE, do as follows: 1 Turn the large FMS knob on the PFD to go to the SYSTEM group and turn the small FMS knob to go to the SYSTEM UPLOAD page. 2 Push the small FMS knob on the PFD to start the cursor. 3 Turn the small FMS knob to highlight the applicable airplane model and push the ENT key. 4 Turn the large FMS knob counterclockwise to go to the FILE menu. 5 Turn the small FMS knob to expand the FILE pull down menu field and highlight the NAV III CAN BUS FUEL LEVEL SENSORS option. 6 Push the ENT key. 7 Push the LOAD soft key to install the software. 8 Monitor the upload status. When the Upload Complete message is shown, push theentkeytoselectok. 9 If a software or configuration upload shows a failure, the software upload process will stop, and you must do the software upload procedure again. Do Steps 9B(5)(b)7 thru 9B(5)(b)9 again as necessary up to a total of five times until you successfully complete the configuration upload. If after five times the software configuration fails, correct the hardware failure and start the configuration upload again. 10 Push the small FMS knob to stop the cursor. 11 Push the UPDT CFG soft key. 12 Select YES and push the ENT key when the UPDATE CONFIG MODULE? message shows. 13 Push the ENT key to select OK after you see the UPDATE CONFIG COMPLETE message. 14 Push the small FMS knob to stop the cursor. (6) Push the TNK SEL soft key to highlight the CURRENT TANK field. (7) Turn the small FMS knob to highlight the RIGHT tank. (8) Push the ENT key. (9) On the PFD, make sure that several values in 2.00GL ACTUAL QUANTITY increments are shown in the CALIBRATION TABLE. (a) If several values in 2.00GL ACTUAL QUANTITY increments are shown in the CALIBRATION TABLE, go to Step 10. Revision 2 - March 13, 2013 Page 13

(b) If several values in 2.00GL ACTUAL QUANTITY increments are not shown in the CALIBRATION TABLE, do as follows: 1 Turn the large FMS knob on the PFD to go to the system group SYSTEM UPLOAD page. 2 Push the small FMS knob on the PFD to start the cursor. 3 Turn the small FMS knob to highlight the applicable airplane model and push the ENT key. 4 Turn the large FMS knob counterclockwise to go to the FILE menu. 5 Turn the small FMS knob to expand the FILE pull down menu field and highlight the NAV III CAN BUS FUEL LEVEL SENSORS option. 6 Push the ENT key. 7 Push the LOAD soft key to install the software. 8 Monitor the upload status. When the Upload Complete message is shown, push the ENT key to select OK. 9 If a software or configuration upload shows a failure, the software upload process will stop, and you must do the software upload procedure again. Do Steps 9B(9)(b)7 thru 9B(9)(b)9 again as necessary up to a total of five times until you successfully complete the configuration upload. If after five times the software configuration fails, correct the hardware failure and start the configuration upload again. 10 Push the small FMS knob to stop the cursor. 11 Push the UPDT CFG soft key. 12 Select YES and push the ENT key when the UPDATE CONFIG MODULE? message shows. 13 Push the ENT key to select OK after you see the UPDATE CONFIG COMPLETE message. 14 Push the small FMS knob to stop the cursor. 10. Put the AVIONICS and BAT MASTER switches in the off position. 11. Make sure that the STDBY BATT switch is in the off position. 12. Remove the SD card from the top slot on the PFD. 13. Do the system checks as follows: A. Install the GDU Supplemental Data SD Cards in to the bottom slot on the PFD and the MFD units. B. Install the Electronic Checklist SD Card in to the top slot on the MFD. C. Put the BAT MASTER switch to the ON position. D. Put the AVIONICS MASTER switches to the ON position. E. 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 190-00352-00 Revision P (or later revision) for troubleshooting instructions. F. If installed, remove the gust lock. G. Do the GFC-700 Autopilot Operation Checks in accordance with Section 4.10.2.5 of the Garmin G1000 NAV III Line Maintenance Manual. (Refer to the Garmin G1000 NAV III Line Maintenance Manual, Part Number 190-00352-00, Revision P (or latest revision).) Page 14 Revision 2 - March 13, 2013

H. If you removed the gust lock to do the GFC-700 Autopilot Operation Checks, install it. 14. Put the AVIONICS and BAT MASTER switches in the off position. 15. Make sure that the STDBY BATT switch is in the off position. 16. Remove external power receptacle. 17. (For airplanes equipped with TAWS-B) Do the enablement of Garmin G1000 Terrain Awareness Warning System Class-B (TAWS-B), SB06-34-03 Revision 1 or later revision. 18. (For airplanes equipped with Chartview) Do the Garmin G1000 NAV III Avionics Chartview Option, SB07-34-01 Revision 1 or later. NOTE: Airplanes equipped with 010-00330-43 GDU Supplemental Database SD Cards will do the same procedures as 010-00330-42 cards described in SB07-34-01 Revision 1 or later. 19. (For airplanes equipped with Garmin Synthetic Vision Technology) Do the enablement of Garmin G1000 Synthetic Vision Installation, SB09-34-07 (or latest revision). 20. (For airplanes equipped with Garmin Search and Rescue) Do the Garmin G1000 Search and Rescue Enablement, SB07-34-05 (or latest revision) or the Garmin G1000 Enhanced Search and Rescue Enablement, SEB-34-01. 21. (For airplanes equipped with Max-Viz Enhanced Vision System (EVS) Use the Aux Video Unlock SD card to do the enablement of Garmin G1000 Auxiliary Video Input I. 22. If necessary, do the Standby Battery Ammeter Calibration Procedure. (Refer to Section 2.2 of the Garmin G1000 NAV III Line Maintenance Manual 190-00352-00 Revision P (or latest revision).) NOTE: GDU software version is 12.03 with version 0563.26 installed. 23. (For airplanes equipped with Dual GMA 1347 Audio Panels) Do the configuration of the dual audio panels in accordance with the latest revision of Garmin Installation Bulletin No.: 0614. 24. System software build 0563.26 supports AOPA database display. The database is available for purchase at www.flygarmin.com. Refer to Cessna Service Newsletter 11-1. 25. Do the software and paper documentation: A. After successful completion of this service bulletin, remove, destroy, and discard the old Cessna NAV III Installation Software CD from the sleeve in the Pilot's Operating Handbook (POH) to eliminate the possibility of reloading the incorrect software at a later date, and get the new Cessna NAV III Installation Software CD to load the new software. B. Remove the old Garmin G1000 Cockpit Reference Guide for Cessna NAV III and replace it with the Garmin G1000 Cockpit Reference Guide for Cessna NAV III, Part Number 190-00384-12. C. The Garmin G1000 Cockpit Reference Guide for Cessna NAV III, Part Number 190-00384-12 and the Garmin NAV III Installation Software CD may be ordered through Cessna Service Parts and Programs. You must use the new CD when you do the software upgrade on the airplane. When not in use, the CD should be stored in the Pilot's Operating Handbook sleeve for the NAV III Garmin Software. 26. Make an entry in the airplane logbook that states compliance and method of compliance with this Service Bulletin. Revision 2 - March 13, 2013 Page 15

MATERIAL INFORMATION Order the parts below to install this service bulletin: NOTE: 190-00498-07REVA Garmin G1000 Pilot's Guide for Cessna NAV III is optional. NOTE: Airplanes with version 0563.24 installed do not need a new Garmin G1000 Integrated Flight Deck Cockpit Reference Guide for Cessna NAV III. NEW P/N QUANTITY KEY WORD OLD P/N INSTRUCTIONS/ DISPOSITION NAVIIIGSW00-03 1 System Software CD with Garmin 006-B0563-26 190-00384-12REVA 1 Garmin G1000 Integrated Flight Deck Cockpit Reference Guide for Cessna NAV III 190-00498-07REVA 1 Garmin G1000 Pilot s GuideforCessnaNAVIII NAVIIIGSW00-02 and prior revisions 190-00384-11 and prior revisions 190-00498-06REVA Destroy and Discard Remove and Replace Remove and Replace Page 16 Revision 2 - March 13, 2013

OWNER ADVISORY TITLE NAVIGATION - GARMIN G1000 SYSTEM SOFTWARE UPGRADE TO VERSION 0563.26 FOR AIRPLANES EQUIPPED WITH NAV III (WAAS-ENABLED INSTALLATIONS ONLY) TO: Cessna 172, 182, and 206 Owners REASON This owner advisory is to inform you that Revision 2 has been issued. Version 0563.26 software service bulletin provides an upgrade that includes the following changes: Resolution for Garmin Service Advisory No. 1129 Rev A Momentary loss of GRS 77 and GDC 74A functions as addressed in Cessna Service Newsletter SNL11-15 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. 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. Profile View The profile view option is added to the MFD Navigation Map. When enabled, the airplane's vertical position over terrain and obstacles is shown centered on the current ground track. When datalink weather is available, winds aloft information is also shown, which depicts a headwind or tailwind as a function of altitude. This vertical profile view is pilot configurable. Circular SAR Pattern A circular search and rescue pattern is now available with the accomplishment of Cessna Service Bulletin SEB-34-01 Garmin G1000 Enhanced Search and Rescue Enablement. 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. Original Issue - March 27, 2012 Revision 2 - March 13, 2013 Page 1 of 3 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: customercare@cessna.textron.com 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 2012

OWNER ADVISORY 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. Improved Lighting Curve The lighting curve has been updated for the displays and their bezels to provide more optimal dimming characteristics while under manual control with the dimming potentiometer. 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. Waypoint Arrival Alerts This configuration item enables the 'arriving at [waypoint]' advisory alert when the aircraft is 10 seconds away from reaching the arrival alert distance to the destination waypoint. Revision 2 provides parts and instructions to upgrade the Garmin G1000 software on WAAS-enabled installations to version 0563.26. COMPLIANCE MANDATORY. This service bulletin must be accomplished within the next 200 hours of operation or 12 months, whichever occurs first. NOTE: For NAV III airplanes equipped with GFC-700 autopilot, Cessna Service Bulletin SB09-34-05 (Garmin G1000 System Software Upgrade to 563.14 for Airplanes Equipped with NAV III and GFC 700 AFCS Autopilot) (or later revision) must be accomplished before compliance with this service bulletin. NOTE: For NAV III airplanes equipped with KAP-140 autopilot, Cessna Service Bulletin SB07-34-02 (Garmin G1000 System Software Upgrade to 563.03) (or later revision) must be accomplished before compliance with this service bulletin. 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: Compliance with Revision 2 is not required if in compliance with the Original Issue or Revision 1. LABOR HOURS 2.0 man-hours to load the software upgrade If necessary, 0.2 man-hour to do the applicable configuration upload for airplanes equipped with the Garmin G1000 Terrain Awareness System (TAWS-B) If necessary, 0.2 man-hour to do the applicable configuration upload for airplanes equipped with the Garmin G1000 Chartview System If necessary, 0.2 man-hour to do the applicable configuration upload for airplanes equipped with Garmin G1000 Synthetic Vision Technology (SVT) If necessary, 0.2 man-hour to do the applicable configuration upload for airplanes equipped with Garmin G1000 Search and Rescue If necessary, 0.2 man-hour to do the standby battery ammeter battery calibration procedure If necessary, 0.2 man-hour to do the dual audio panel configuration procedure Page 2 Revision 2 - March 13, 2013

OWNER ADVISORY If necessary, 0.2 man-hour to do the applicable configuration upload for airplanes equipped with Garmin G1000 Enhanced Vision System (EVS) WARRANTY For airplanes identified within the serial effectivity and complying within 200 hours or twelve months from the original date of this service bulletin: Applicable Cockpit Reference Guide (CRG) and software CD parts credit and a labor allowance credit of 2.0 man-hours per airplane will be provided to load the software upgrade. If necessary, a labor allowance credit of 0.2 man-hour will be provided to do the applicable configuration upload for airplanes equipped with the Garmin G1000 Terrain Awareness System (TAWS-B). If necessary, a labor allowance credit of 0.2 man-hour will be provided to do the applicable configuration upload for airplanes equipped with the Garmin G1000 Chartview System. If necessary, a labor allowance credit of 0.2 man-hour will be provided to do the applicable configuration upload for airplanes equipped with Garmin G1000 Synthetic Vision Technology (SVT). If necessary, a labor allowance credit of 0.2 man-hour will be provided to do the applicable configuration upload for airplanes equipped with Garmin G1000 Search and Rescue. If necessary, a labor allowance credit of 0.2 man-hour will be provided to do the standby battery ammeter battery calibration procedure. If necessary, a labor allowance credit of 0.2 man-hour will be provided to do the dual audio panel configuration procedure. If necessary, a labor allowance credit of 0.2 man-hour will be provided to do the applicable configuration upload for airplanes equipped with Garmin G1000 Enhanced Vision System (EVS). Freight will be credited at the most economical method unless pre-approved by Cessna. For pre-approval contact Cessna Service Parts and Programs Warranty Administration at Telephone: 316-517-4296, Fax: 316-206-2746 or E-mail: cpd2claims@cessna.textron.com. 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. For airplanes identified within the serial effectivity per Revision 1: Domestic... April 27, 2013 International... April 27, 2013 For airplanes added into the serial effectivity per Revision 2: Domestic...March 13, 2014 International...March 13, 2014 Special Note to Authorized Service Facilities: When you complete the Warranty Claim, the labor allowance claimed shall be itemized for each above action completed. Please contact a Cessna Authorized Service Facility for detailed information and arrange to have Cessna service bulletin Revision 2 accomplished on your airplane. 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. Revision 2 - March 13, 2013 Page 3