Single Engine Service Bulletin January 18, 2011 TITLE GARMIN G1000 SYSTEM SOFTWARE UPGRADE TO 0563.21 FOR AIRPLANES EQUIPPED WITH NAV III AND WAAS 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 17281570 172S 172S10432 thru 172S11063 182T 18281876 thru 18282250 T182T T18208669 thru T18209009 206H 20608284 thru 20608323 T206H T20608705 thru T20608985 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 T18208664, T18208666 thru T18208668 206H 20608216 thru 20608278, 20608280 thru 20608283 T206H T20608450 thru T20608681, T20608683 thru T20608704 Page 1 of 19 To obtain satisfactory results, procedures specified in this publication must be accomplished in accordance with accepted methods and prevailing government regulations. Cessna Aircraft Company cannot be responsible for the quality of work performed in accomplishing the requirements of this publication. Cessna Aircraft Company, Customer Service, P.O. Box 7706, Wichita, Kansas 67277, U.S.A. (316) 517-5800, Facsimile (316) 517-7271 www.cessnasupport.com COPYRIGHT 2011
REASON This version 0563.21 software Service Bulletin provides an upgrade that includes the following changes: TAWS-B Alerting If installed, implemented terrain clearance and destination airport algorithm changes to reduce nuisance alerts New XM Weather Product, Aviator Pro If installed, implemented display support for AIREP, PIREP, Turbulence, Icing Potential, and Super-Cooled Liquid Droplets Weather Map Orientation Enhanced to make orientation pilot selectable instead of always "north-up" Temporary Flight Restrictions (TFR) Enhanced depiction by combining overlapping TFR circles into a single-shape TFR Course Tracking and Intercept Logic Implemented navigation system changes to improve course intercept and navigation Flight Plan Sequencing Enhanced so that manual activation of a procedure turn will not result in a suspend-state after completing the turn GFC-700 Roll Steering Updated calculations to eliminate the possibility of a roll steering over-correction when engaging the GFC-700 Autopilot Dead Reckoning Mode Added option to allow GPS course and roll steering data to be valid for up to 20 minutes after entering Dead Reckoning (DR) mode Minimum Altitude Alerts Modified so that a previously entered value is cleared when an approach is added to or deleted from the active flight plan Flight Plan Import/Export Provides capability to import and export flight plans between an SD card and the GDU flight plan memory NAV III Engine Gauges Enhanced appearance of the engine gauges to Garmin s 3D EIS Inset Maps Corrected inset map depictions so that they are always synchronized on the PFD and MFD Flight Path Marker (FPM) If Synthetic Vision is installed, the marker was modified to render behind the aircraft symbol and flight director command bars Default Waypoint Storage Duration Updated to allow the pilot to create new user-defined waypoints as either persistent or temporary and to set the defaults NAV III System Configuration Bar END (endurance), FOB (fuel on board), and FOD (fuel over destination) options are now displayed on the MFD status bar Resolution for Garmin Service Advisory No. 0904A If Synthetic Vision is installed, Pathways is now enabled Fixed Content Data Logging Provides capability of logging flight data to a comma-separated-value (CSV) file on an SD card in the upper MFD slot GTS800 TAS System Input/Output Communication If installed via field approval, allows input/output communication on RS-232 and ARINC-429 interfaces Resolution for Garmin Service Advisory No. 0929 Change implemented to prevent the possibility of flagging primary flight data, COM frequency, and EIS information while all stored flight plans or user waypoints are being deleted Resolution for Garmin Service Advisory No. 0825 Change implemented to allow an LPV approach to be selected at airports with 3-character identifiers Multiple Waypoint Instances Modified the Flight Plan List so that any instance of a waypoint that appears multiple times can be selected, not just the first AOPA Airport Directory Information Support added for display on the "WPT-Airport Information" page. Field aircraft will need to purchase the AOPA directory via www.flygarmin.com Page 2 January 18, 2011
Auto Zoom Range On moving map enhanced to show active leg instead of the entire leg that is ahead of the aircraft GDU 1044B -10 Display Hardware Support Implemented software to support hardware that allows potential for external video inputs Approach Loading Cursor Operation When loading an approach, the cursor will no longer skip the "minimums" field after selecting a transition that prompts for whether to fly the course reversal Display of Groundspeed in DR Mode When DR mode is active, groundspeed is now displayed in yellow on the PFD MFD Page Navigation Updated the MFD selection window to show the Page Group and Page Title for selection. DESCRIPTION This Service Bulletin provides parts and instructions to upgrade the Garmin G1000 software to version 0563.21. COMPLIANCE Recommended: Should be accomplished within the next 100 hours of operation or 12 months, whichever occurs first. NOTE: For airplanes affected by Cessna Service Bulletin SB07-34-02 Revision 1 (Garmin G1000 System Software Upgrade to Version 563.03). If not already accomplished, SB07-34-02 Revision 1 must be accomplished before compliance with this Service Bulletin. NOTE: For airplanes affected by 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). If not already accomplished, SB09-34-05 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. APPROVAL FAA approval has been obtained on technical data in this publication that affects airplane type design. MANPOWER 3.5 man-hours to load the software upgrade If necessary, 0.3 man-hour to do the applicable configuration upload for airplanes equipped with the Garmin G1000 Terrain Awareness System (TAWS-B) If necessary, 0.3 man-hour to do the applicable configuration upload for airplanes equipped with the Garmin G1000 Chartview System If necessary, 0.3 man-hour to do the applicable configuration upload for airplanes equipped with Garmin G1000 Synthetic Vision Technology (SVT) If necessary, 0.3 man-hour to do the applicable configuration upload for airplanes equipped with Garmin G1000SearchandRescue If necessary, 0.3 man-hour to do the Standby Battery Ammeter Battery Calibration Procedure January 18, 2011 Page 3
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 190-00384-11 Rev. A. The following documents can be viewed by Cessna Service Stations 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 S (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 S (or latest revision) Garmin GRS 77/GMU 44 Installation Manual, Part Number 190-00303-10, Revision L (or latest revision) Garmin GDC 74A Installation Manual, Part Number 190-00303-15, Revision F (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. OTHER 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. Page 4 January 18, 2011
MATERIAL PRICE AND AVAILABILITY The following parts are available from Cessna Service Parts and Programs through a Cessna Single Engine Authorized Service Facility: NOTE: 190-00498-06 Garmin G1000 Pilot's Guide for Cessna NAV III is optional. Part Number Description Qty/Airplane Price 190-00384-11REVA Garmin G1000 Integrated Flight Deck Cockpit Reference Guide for Cessna NAV III Models 172R/172S, 182T/T182T and 206H/T206H 1 $295.00 190-00498-06REVA Garmin G1000 Pilot s Guide for Cessna NAVIII 1 $595.00 ALL PRICES SUBJECT TO CHANGE WITHOUT NOTICE January 18, 2011 Page 5
CREDIT INFORMATION For airplanes out of warranty: Applicable software CD parts credit will be provided to load the software upgrade. For airplanes in warranty: Applicable Cockpit Reference Guide (CRG) and software CD parts credit and a labor allowance credit of 3.5 man-hours per airplane will be provided to load the software upgrade. for airplanes equipped with the Garmin G1000 Terrain Awareness System (TAWS-B). for airplanes equipped with the Garmin G1000 Chartview System. for airplanes equipped with Garmin G1000 Synthetic Vision Technology (SVT). for airplanes equipped with Garmin G1000 Search and Rescue. If necessary, a labor allowance credit of 0.3 man-hour will be provided to do the Standby Battery Ammeter Battery Calibration Procedure. For airplanes with SVT previously installed (in or out of warranty): Applicable CRG and software CD parts credit and a labor allowance credit of 3.5 man-hours per airplane will be provided to load the software upgrade. Only Authorized Service Facilities providing proof of SVT installation may submit a Warranty Claim to accomplish this Service Bulletin. for airplanes equipped with the Garmin G1000 Terrain Awareness System (TAWS-B). for airplanes equipped with the Garmin G1000 Chartview System. for airplanes equipped with Garmin G1000 Synthetic Vision Technology (SVT). for airplanes equipped with Garmin G1000 Search and Rescue. If necessary, a labor allowance credit of 0.3 man-hour will be provided to do the Standby Battery Ammeter Battery Calibration Procedure. NOTE: Proof of SVT purchase is a logbook entry or a purchasing receipt. 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 and a Warranty Claim submitted by a Cessna Single Engine Authorized Service Facility within 30 calendar days of Service Bulletin compliance before the credit expiration dates shown below. Domestic... January18,2012 International... January18,2012 Special Note to Service Stations: When you complete the Warranty Claim, the labor allowance claimed shall be itemized for each above action completed. Page 6 January 18, 2011
ACCOMPLISHMENT INSTRUCTIONS WEIGHT AND BALANCE INFORMATION Negligible Material Information To complete this Service Bulletin, use the parts below as applicable: NEW P/N QUANTITY DESCRIPTION OLD P/N DISPOSITION NAVIIIGSW00-01 1 Model 172R Software CD NAVIIIGSW00-01 1 Model 172S Software CD NAVIIIGSW00-01 1 Model 182T Software CD NAVIIIGSW00-01 1 Model T182T Software CD NAVIIIGSW00-01 1 Model 206H Software CD NAVIIIGSW00-01 1 Model T206H Software CD 190-00384-11REVA 1 Garmin G1000 Integrated Flight Deck Cockpit Reference Guide for Cessna NAV III Models 172R/172S, 182T/T182T and 206H/T206H General Information Instructions 172RGSW00-08 and prior revisions 172SGSW00-08 and prior revisions 182TGSW00-11 and prior revisions T182TGSW00-10 and prior revisions 206HGSW00-11 and prior revisions T206HGSW00-10 and prior revisions 190-00384-09 and prior revisions Destroy and Discard Destroy and Discard Destroy and Discard Destroy and Discard Destroy and Discard Destroy and Discard Remove NOTE 1: This software update only supports NAV III installations that are WAAS airplanes. If the aircraft is not a WAAS-equipped aircraft do not perform this software update 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. Ifthe system does not upload after the fifth attempt, contact Cessna Aircraft Customer Service, 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. Do the software and paper documentation: A. 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. January 18, 2011 Page 7
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 190-00384-11. C. The Garmin G1000 Cockpit Reference Guide for Cessna NAV III, Part Number 190-00384-11 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. 2. Make the 006-B0563-21 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 File Version 006-B0563-21 0563.21 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-B0563-21_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. 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-B0563-21. L. Remove the CD from the computer and install it in the Nav III/Garmin Software sleeve in the Pilot s Operating Handbook (POH). 3. Turn on the G1000 in configuration 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 6. 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. Page 8 January 18, 2011
TABLE 2- Model 172R and 172S. 172R/172S AIRPLANE MODEL CONFIGURATION FILE SELECTIONS - PULL-DOWN MENU Cessna 172R - 006-B0563-21 Full Configuration (WAAS) or Cessna 172S - 006-B0563-21 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. January 18, 2011 Page 9
TABLE 3- Model 182T and T182T 182T/T182T AIRPLANE MODEL CONFIGURATION FILE SELECTIONS - PULL-DOWN MENU Cessna 182T - 006-B0563-21 Full Configuration (WAAS) or Cessna T182T - 006-B0563-21 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. Cessna NAV III Disable SVT Pathways Option (if desired) NOTE: Most installations will not use this option. Page 10 January 18, 2011
TABLE 4- Models 206H and T206H 206H/T206H AIRPLANE MODEL CONFIGURATION FILE SELECTIONS - PULL-DOWN MENU Cessna 206H - 006-B0563-21 Full Configuration (WAAS) or Cessna T206H - 006-B0563-21 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 Pre BP 2007 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. January 18, 2011 Page 11
TABLE 5- Configuration Selections Cessna (Model) 006-B0563-21 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. 4. 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 5. (2) If the SD cards are not Garmin P/N 010-00330-43, go to Step 6. 5. 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. Put the 010-00330-43 database card into a PC card reader. B. Use Windows Explorer to navigate through the contents of the database card. C. Go to Tools, then Folder Options, and then View tab. (1) Select Show hidden files and folders. (2) Uncheck Hide protected operating system files (Recommended). D. Look for the file apt_dir.gca. If it shows, select and delete it. E. Remove the database card from the PC. F. Do Step 5A thru 5E again for all 010-00330-43 cards. G. Store the cards in a safe location for later installation. 6. Load the GDU (PFD1 and MFD) software as follows: A. Make sure that all switches are in the OFF/NORM position. 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-B00563-21 SD card into the topcardslotofthemfd. F. Put the BAT MASTER switch to the ON position. Page 12 January 18, 2011
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-B00563-21 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 6H thru 6M again for the PFD. 7. 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. Use the FMS knob to select the correct airframe from the pull-down menu. C. Push the FMS knob to start the cursor. D. Turn the small FMS knob to highlight the applicable airplane model. E. Push the ENT key. F. Select the applicable Cessna (Model Number) 006-B0563-21 Full Configuration (WAAS) menu option and push the ENT key. NOTE: The software included in the 006-B0563-21 SD Card will automatically determine which files must be loaded. G. 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 softkey to continue with the rest of the software load before troubleshooting cause of failure. H. Monitor the upload status. When the Upload Complete message is shown, push the ENT key to select OK. NOTE: Thiscantakeupto60minutes. WARNING: DO NOT CONFIGURE AN OPTION THAT IS NOT INSTALLED ON THE AIRPLANE. 8. For airplanes equipped with additional items as shown in TABLES 2, 3, or 4 (refer to TABLE 5), do the necessary uploads as follows: A. Turn the large FMS knob counterclockwise to go to the FILE menu. B. Turn the small FMS knob to expand the FILE pull down menu field and highlight one of the Cessna Nav III software uploads that is applicable for your airplane. January 18, 2011 Page 13
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 8A thru 8E again until all applicable (refer to TABLE 5) software uploads are complete. G. Press the FMS knob to unselect the cursor. 9. 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. 10. 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-B0563-21 0563.21 (3) 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. (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) If several values in 2.00GL ACTUAL QUANTITY increments are shown in the CALIBRATION TABLE, go to Step 10B(6). Page 14 January 18, 2011
(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 and turn the small FMS knob to go to the SYSTEM UPLOAD page. 2 PushthesmallFMSknobonthePFDtostartthecursor. 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 10B(5)(b)7 thru 10B(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 PushthesmallFMSknobtostopthecursor. 11 Push the UPDT CFG soft key. 12 Select YES and push the ENT key when the UPDATE CONFIG MODULE? message shows. 13 PushtheENTkeytoselectOKafteryouseetheUPDATE CONFIG COMPLETE message. 14 PushthesmallFMSknobtostopthecursor. (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 11. (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 PushthesmallFMSknobonthePFDtostartthecursor. 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. January 18, 2011 Page 15
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 10B(9)(b)7 thru 10B(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. 11. Put the AVIONICS and BAT MASTER switches in the off position. 12. Make sure that the STDBY BATT switch is in the off position. 13. Remove the SD card from the top slot on the MFD. 14. 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. 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).) 15. Put the AVIONICS and BAT MASTER switches in the off position. 16. Make sure that the STDBY BATT switch is in the off position. 17. Remove external power receptacle. 18. Make an entry in the airplane logbook that states compliance and method of compliance with this Service Bulletin. 19. (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. 20. (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. 21. (For airplanes equipped with Garmin Synthetic Vision Technology) Do the enablement of Garmin G1000 Synthetic Vision Installation, SB09-34-07 (or latest revision). Page 16 January 18, 2011
22. (For airplanes equipped with Garmin Search and Rescue) Do the Garmin G1000 Search and Rescue Enablement, SB07-34-05 (or latest revision). 23. 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 10.01 with 0563.21 installed. OWNER NOTIFICATION On January 18, 2011 the following message will be sent to applicable owners of record in A. Dear Cessna Restart Owner: This Owner Advisory is to inform you that has been issued. Version 0563.21 software provides enhancements to the Garmin G1000 avionics system. provides a software upgrade that includes the following changes: TAWS-B Alerting If installed, implemented terrain clearance and destination airport algorithm changes to reduce nuisance alerts New XM Weather Product, Aviator Pro If installed, implemented display support for AIREP, PIREP, Turbulence, Icing Potential, and Super-Cooled Liquid Droplets Weather Map Orientation Enhanced to make orientation pilot selectable instead of always "north-up" Temporary Flight Restrictions (TFR) Enhanced depiction by combining overlapping TFR circles into a single-shape TFR Course Tracking and Intercept Logic Implemented navigation system changes to improve course intercept and navigation Flight Plan Sequencing Enhanced so that manual activation of a procedure turn will not result in a suspend-state after completing the turn GFC-700 Roll Steering Updated calculations to eliminate the possibility of a roll steering over-correction when engaging the GFC-700 Autopilot Dead Reckoning Mode Added option to allow GPS course and roll steering data to be valid for up to 20 minutes after entering Dead Reckoning (DR) mode Minimum Altitude Alerts Modified so that a previously entered value is cleared when an approach is added to or deleted from the active flight plan Flight Plan Import/Export Provides capability to import and export flight plans between an SD card and the GDU flight plan memory NAV III Engine Gauges Enhanced appearance of the engine gauges to Garmin s 3D EIS Inset Maps Corrected inset map depictions so that they are always synchronized on the PFD and MFD Flight Path Marker (FPM) If Synthetic Vision is installed, the marker was modified to render behind the aircraft symbol and flight director command bars Default Waypoint Storage Duration Updated to allow the pilot to create new user-defined waypoints as either persistent or temporary and to set the defaults NAV III System Configuration Bar END (endurance), FOB (fuel on board), and FOD (fuel over destination) options are now displayed on the MFD status bar Resolution for Garmin Service Advisory No. 0904A If Synthetic Vision is installed, Pathways is now enabled Fixed Content Data Logging Provides capability of logging flight data to a comma-separated-value (CSV) file on an SD card in the upper MFD slot January 18, 2011 Page 17
GTS800 TAS System Input/Output Communication If installed via field approval, allows input/output communication on RS-232 and ARINC-429 interfaces Resolution for Garmin Service Advisory No. 0929 Change implemented to prevent the possibility of flagging primary flight data, COM frequency, and EIS information while all stored flight plans or user waypoints are being deleted Resolution for Garmin Service Advisory No. 0825 Change implemented to allow an LPV approach to be selected at airports with 3-character identifiers Multiple Waypoint Instances Modified the Flight Plan List so that any instance of a waypoint that appears multiple times can be selected, not just the first AOPA Airport Directory Information Support added for display on the "WPT-Airport Information" page. Field aircraft will need to purchase the AOPA directory via www.flygarmin.com Auto Zoom Range On moving map enhanced to show active leg instead of the entire leg that is ahead of the aircraft GDU 1044B -10 Display Hardware Support Implemented software to support hardware that allows potential for external video inputs Approach Loading Cursor Operation Whenloadinganapproach,thecursorwillnolongerskipthe "minimums" field after selecting a transition that prompts for whether to fly the course reversal Display of Groundspeed in DR Mode When DR mode is active, groundspeed is now displayed in yellow on the PFD MFD Page Navigation Updated the MFD selection window to show the Page Group and Page Title for selection. provides parts and instructions to upgrade the Garmin G1000 software to version 0563.21. Compliance is Recommended: Should be accomplished within the next 100 hours of operation or 12 months, whichever occurs first. The information contained in the referenced Cessna Service Bulletin shall be considered an amendment to the Cessna Manufacturer's Service/Maintenance Manual and should be accomplished within the specified time requirement. Page 18 January 18, 2011
For airplanes out of warranty: Applicable software CD parts credit will be provided to load the software upgrade. For airplanes in warranty: Applicable Cockpit Reference Guide (CRG) and software CD parts credit and a labor allowance credit of 3.5 man-hours per airplane will be provided to load the software upgrade. for airplanes equipped with the Garmin G1000 Terrain Awareness System (TAWS-B). for airplanes equipped with the Garmin G1000 Chartview System. for airplanes equipped with Garmin G1000 Synthetic Vision Technology (SVT). for airplanes equipped with Garmin G1000 Search and Rescue. If necessary, 0.3 man-hour to do the Standby Battery Ammeter Battery Calibration Procedure For airplanes with SVT previously installed (in or out of warranty): Applicable CRG and software CD parts credit and a labor allowance credit of 3.5 man-hours per airplane will be provided to load the software upgrade. Only Authorized Service Facilities providing proof of SVT installation may submit a Warranty Claim to accomplish this Service Bulletin. for airplanes equipped with the Garmin G1000 Terrain Awareness System (TAWS-B). for airplanes equipped with the Garmin G1000 Chartview System. for airplanes equipped with Garmin G1000 Synthetic Vision Technology (SVT). for airplanes equipped with Garmin G1000 Search and Rescue. If necessary, a labor allowance credit of 0.3 man-hour will be provided to do the Standby Battery Ammeter Battery Calibration Procedure. NOTE: Proof of SVT purchase is a logbook entry or a purchasing receipt. 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 and a Warranty Claim submitted by a Cessna Single Engine Authorized Service Facility within 30 calendar days of Service Bulletin compliance before the credit expiration dates shown below. Domestic... January18,2012 International... January18,2012 Special Note to Service Stations: When you complete the Warranty Claim, the labor allowance claimed shall be itemized for each above action completed. * * * * * * * January 18, 2011 Page 19