SERVICE BULLETIN TITLE NAVIGATION - GARMIN G1000 SYSTEM SOFTWARE UPGRADE TO VERSION

Transcription

1 TITLE NAVIGATION - GARMIN G1000 SYSTEM SOFTWARE UPGRADE TO VERSION EFFECTIVITY MODEL SERIAL NUMBERS , thru B 208B1190, 208B1216, 208B2000 thru 208B2261, 208B2263 thru 208B2323, 208B2325, 208B2326, 208B2328 thru 208B2357 REASON This version software service bulletin provides an upgrade that includes the following changes: Resolution for Garmin Service Advisory No Rev A Momentary loss of GRS 77 and GDC 74A functions as addressed in Cessna Service Newsletter SNL Flight Plan Sorting The functionality of sorting the stored flight plans was removed; software fix to Garmin Service Advisory No.: 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). 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. 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. Refer to Cessna Service Letter CAL-34-01, Garmin G1000 Loading Updated Databases (or latest revision), for additional details. 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. Refer to Cessna Service Letter CAL-34-01, Garmin G1000 Loading Updated Databases (or latest revision), for additional details. May 15, 2012 Page1of10 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A , Fax , 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

2 Startup Screen Displays for 150 seconds at power up when dual navigation database feature is active to allow the internal database to update and will provide an error message if unsuccessful. 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. 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.: Enhanced SAR Provides the base software level needed to install Enhanced Search and Rescue patterns via Cessna Service Bulletin CAB MFD Baro Knob Pressing the baro knob on the MFD during normal mode now sets STD BARO. Inset Map Settings on the inset map are now restored between power cycles. Departure Time Correctly displays the departure time when the time units are UTC. Radio Altimeter Altitude height window moved above course CRS window. MFD Status Bar Updated allowable items (BRG, XTK, DIS, DTK, END, ESA, ETA, ETE, FOD, FOB, GS, MSA, TAS, TKE, TRK, and VSR are now available). DESCRIPTION This service bulletin provides parts and instructions to upgrade the Garmin G1000 software to version from version (or later). COMPLIANCE MANDATORY. This service bulletin shall be accomplished at the next 100 hours or 6 months, whichever occurs first. APPROVAL Cessna received FAA approval for the technical data in this publication that changes the airplane type design. Cessna received EASA approval for the technical data in this publication that changes the airplane type design. WEIGHT AND BALANCE INFORMATION Negligible REFERENCES The following document can be viewed by Cessna Authorized Service Facilities by going to Garmin G1000 Caravan Line Maintenance Manual, Part Number , Revision E (or latest revision) NOTE: Make sure all publications used are complete and current. NOTE: This information shall be considered an amendment to the Cessna Manufacturer's Service/Maintenance Manual. ACCOMPLISHMENT INSTRUCTIONS NOTE 1: 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, refer to the Garmin Line Maintenance Manual, Revision E or later, Appendix B.3 Software / Configuration Troubleshooting. If the system still does not upload, contact Cessna Customer Care: Telephone or FAX Do not cancel a software or configuration upload that is in progress. Let the system either successfully load or fail. Page 2 May 15, 2012

3 NOTE 2: 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. You can also accomplish this on the MFD screen if you need to make the chime stop during a software load. 1. Connect a ground power unit to the airplane. 2. Do the pre-loading procedure as follows: A. Make sure that all of the necessary circuit breakers are pushed in for normal mode startup of the G1000 System. B. MakesurethattheEXTERNALPOWERswitchissettoBUSandtheAVIONICS1and2switches are set to ON. C. Let the system power on in normal mode. D. Disengage the PFD1 circuit breaker. E. Push and hold the ENT key on the PFD1 and engage the PFD1 circuit breaker. F. Release the ENT key when the message INITIALIZING SYSTEM shows on the PFD1. G. Turn the large FMS knob on the PFD1 to go to the GDU group. H. Turn the small FMS knob to go to the AIRFRAME CONFIGURATION page. I. Push the small FMS knob on the PFD to start the cursor and then turn the large FMS knob to scroll to the AIRFRAME box. J. Turn the small FMS knob on the PFD to scroll through the list of options shown on the PFD1 and use TABLE 2 to make a list of the options installed on the airplane. This list is necessary to do the configuration procedures. K. Disengage the PFD1, PFD2, and MFD circuit breakers. 3. Load the GDU (PFD1, PFD2, and MFD) Software as follows: CAUTION: Failure to remove the SD cards from the slots in the displays can result in damage to the cards. A. Remove the GDU Supplemental Database (SD) Cards from the bottom slot of the PFD1, PFD2, and MFD displays and identify each as PFD1, PFD2, or MFD. B. Keep the cards in a safe place for later installation. C. Install the G1000 Software Loader Card into the upper slot of the PFD2 display. D. Push and hold the ENT key on the PFD2 while you engage the PFD2 circuit breaker. E. Release the ENT key when the message INITIALIZING SYSTEM shows on the PFD2. F. Push the YES soft key to upload GDU system files when the message DO YOU WANT TO UPDATE SYSTEM FILES? shows. G. Push the NO soft key when the message DO YOU WANT TO UPDATE THE SPLASH SCREEN? shows. H. Push any key when the prompt PRESS ANY KEY TO CONTINUE shows on the PFD2. I. The software installation to the PFD2 is done when the screen goes into the configuration mode. J. Remove the software loader card from the PFD2 slot but do not remove power from the display. K. Put the software loader card into the MFD upper SD Card slot. L. Push and hold the ENT key on the MFD and engage the MFD circuit breaker. M. Release the ENT key when the message INITIALIZING SYSTEM shows on the MFD. May 15, 2012 Page 3

4 N. Do Steps 3F thru 3I again for the MFD. O. After the loading is complete, remove the SD Card from the MFD slot but do not remove power from the display. P. Put the software loader card into the PFD1 upper SD Card slot. Q. Push and hold the ENT key on the PFD1 and engage the PFD1 circuit breaker. R. Release the ENT key when the message INITIALIZING SYSTEM shows on the PFD1. S. Do Steps 3F thru 3I again for the PFD1. T. The PFD1 will start in the configuration mode when you complete the update. Do not remove power from the PFD1. Keep the software loader card in the upper slot of the PFD1. 4. Do the initial G1000 software and configuration upload: A. Turn the large FMS knob on the PFD1 to go to the SYSTEM group and then turn the small FMS knob to go to the SYSTEM UPLOAD page. B. Push the small FMS knob on the PFD to start the cursor. C. Turn the small FMS knob to expand the GROUP pull down menu and highlight the applicable 208 or 208B airframe. Push the ENT key, and turn the small FMS knob to highlight the applicable ITEM from TABLE 1 and push the ENT key. TABLE 1 GROUP ITEM 208 Cessna Baseline Configuration 208B Cessna 208B - Baseline Configuration D. Turn the small FMS knob and scroll through the PRODUCT window to the GIA CERT file. E. Make sure that the SOFTWARE column of the GIA CERT file is selected with a check mark beside it. F. Push the LOAD soft key to install the software and configuration settings. NOTE: The software included in the 006-B SD Card will automatically determine all other files that must be loaded. G. Monitor the upload status. When the upload message is shown, push the ENT key to select OK. NOTE: Thiscantakeupto60minutes. H. 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 4D thru 4H 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, do an inspection of and correct the hardware failures and start the configuration upload again. (Refer to Garmin Line Maintenance Manual, Revision E or latest revision.) 5. Use the list of options you made in TABLE 2 and load the applicable options installed on the airplane 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 GROUP file menu. B. Turn the small FMS knob clockwise to expand the GROUP file pull down menu and highlight INSTALLATION OPTIONS. C. Push the ENT key. Page 4 May 15, 2012

5 D. Turn the large FMS knob clockwise to go to the ITEM menu (if you are not already at the ITEM menu). E. Turn the small FMS knob to expand the ITEM pull down menu field and highlight one of the Cessna Caravan options from TABLE 2 that is applicable to your airplane. Highlight only those options from Table 2 that are installed on your airplane. NOTE: s found in the ITEM pull down menu that are not listed in Table 2 are not applicable to current field airplanes. F. Push the ENT key. G. Push the LOAD soft key to install the software. H. Monitor the upload status. When the Upload Complete message is shown, push the ENT key to select OK. I. If a software option upload shows a failure, the software upload process will stop, and you must do the software upload procedure again. Do Steps 5G thru 5I again as necessary for that option up to a total of five times until you successfully complete the configuration upload. If after five times the software configuration fails, do an inspection of and correct the hardware faults and start the software option upload again. (Refer to Garmin Line Maintenance Manual, Revision E or latest revision.) J. Do Steps 5A thru 5I again until all applicable software option uploads are complete. K. PushthesmallFMSknobtostopthecursor. L. Push the UPDT CFG and then the ENT keys to select YES to update the PFD1 configuration module. M. Push the ENT key to select OK after you see the UPDATE CONFIG COMPLETE message. May 15, 2012 Page 5

6 TABLE 2 INSTALLED (YES / NO) CONFIGURATION LABEL OPTIONS 300 A Gen KR87 ADF Artex ELT Beta FDR / CVR GDL 69A Cessna Caravan 300A Generator Installation Cessna Caravan KR87 ADF Installation Cessna Caravan Artex C406-N ELT Installation Cessna Caravan Beta Installation Cessna Caravan FDR /CVR Installation Cessna Caravan GDL 69A Installation Dual GTX 33 Cessna Caravan Dual GTX 33 Installation GWX 68 HF 2nd GMA1347 NiCd Batt Gn/Alt Ovht Prop Heat KRA 405B RA KTA 870 TAS TKS w/pod TKS LP WX 500 Cessna Caravan GWX 68 Installation Cessna Caravan HF Installation Cessna Caravan Dual GMA1347 Audio Installation Cessna Caravan NiCd Installation Cessna Caravan Gen/Alt Overheat Installation Cessna Caravan Prop Heat Installation Cessna Caravan KRA 405B Installation Cessna Caravan KTA 870 TAS Installation Cessna Caravan TKS Installation Cessna Caravan TKS Low Profile Installation Cessna Caravan WX 500 Installation 6. Do the manifest configuration verification as follows: A. 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. B. (Refer to TABLE 3.) Make sure that the data file and file version shown in TABLE 3 are shown in the SYSTEM field window. Page 6 May 15, 2012

7 TABLE 3 DATA FILE FILE VERSION 006-B C. Put the AVIONICS 1 and 2 switches to the OFF position and remove the software SD loader card from the top slot of the PFD1. Stow the software SD loader card in the blue aircraft software sleeve in the airplane's POH. D. Install the three GDU Supplement Database SD Cards into the bottom slots of the PFD1, PFD2, and MFD from which you removed them. E. Put the AVIONICS 1 and 2 switches to the ON position and let the system power on in normal mode. F. Make sure that no G1000 system messages, alerts, annunciations, or Red X's are shown on PFD1, PFD2, or the MFD on the AUX-SYSTEM STATUS page. (1) If there are no G1000 system messages, alerts, annunciations, or Red X's shown on PFD1, PFD2, or the MFD on the AUX-SYSTEM STATUS page, go to Step 6G. (2) If the system powers ON and a red AFCS or Red X s are shown on XPDR 1 or 2 on PFD1, PFD2, or the MFD on the AUX-SYSTEM STATUS page, do as follows and skip to Step 6G at any time that the errors are extinguished. Reference the Garmin Line Maintenance Manual Revision E (or later revision) for troubleshooting instructions of all other errors. (a) Put the AVIONICS 1 and 2 switches to the OFF position. (b) After no less than 10 seconds, put the AVIONICS 1 and 2 switches back to the ON position and look for errors. (c) Disengage the PFD1 circuit breaker. (d) After no less than 10 seconds, engage the PFD1 circuit breaker and look for errors. (e) Disengage the NAV1 circuit breaker. (f) After no less than 10 seconds, engage the NAV1 circuit breaker and look for errors. G. Look at TABLE 4. (1) If one or more options shown in TABLE 4 were ordered at the factory or installed by service bulletin, go to Step 7. (2) If no options shown in TABLE 4 were previously installed at the factory, go to Step Do the procedure that follows to re-enable the options from TABLE 4 that the owner had previously ordered. TABLE 4: OPTIONS TO ENABLE TAWS Configuration ( TAWS Unlock Card) Jepp Chartview Configuration ( Chartview Unlock Card) Synthetic Vision Technology (SVT) Configuration ( SVS Unlock Card) NOTE: An SD unlock card for each of the options shown in this table was delivered with the airplane as loose equipment or purchased from Cessna Service Parts and Programs and is necessary to enable the option. A. Disengage the PFD1, PFD2, and MFD circuit breakers. B. Remove the GDU Supplemental Database SD Cards from the bottom slot of the PFD1, PFD2, and MFD displays as applicable. C. Push and hold the ENT key on the PFD2 while you engage the PFD2 circuit breaker. May 15, 2012 Page 7

8 D. Release the ENT key when the message INITIALIZING SYSTEM shows on the PFD2. E. Push and hold the ENT key on the MFD and engage the MFD circuit breaker. F. Release the ENT key when the message INITIALIZING SYSTEM shows on the MFD. G. Put the TAWS Unlock Card ( Chartview Unlock Card, SVS Unlock Card) into the upper slot of the PFD1 display. H. Push and hold the ENT key on the PFD1 and engage the PFD1 circuit breaker. I. Release the ENT key when the message INITIALIZING SYSTEM shows on the PFD1. J. On the PFD1, turn the large FMS knob to go to the SYSTEM group and turn the small FMS knob to go to the SYSTEM UPLOAD page. K. Push the small FMS knob to activate the cursor. L. Turn the small FMS knob to expand the drop down menu and highlight CONFIGURATION FILES. M. Push the ENT key. N. Turn the small FMS knob to expand the drop down menu and highlight ENABLE TAWS (ENABLE CHARTVIEW or ENABLE SVS DUAL PFD). O. Push the ENT key. P. Push the LOAD soft key to start the upload. Q. Push the ENT key after you see the UPLOAD COMPLETE message. R. Push the UPDT CFG and then the ENT keys to select YES to update the PFD1 configuration module. S. Push the ENT key to select OK after you see the UPDATE CONFIG COMPLETE message. T. If you will enable more options from TABLE 4, disengage the PFD1 circuit breaker and do Steps 7G thru 7T for each of the remaining options as necessary. U. If a software option upload shows a failure, the software upload process will stop, and you must do the software upload procedure again. Do Steps 7G thru 7T again as necessary for that option up to a total of five times until you successfully complete the configuration upload. If after five times the software configuration fails, do an inspection of and correct the hardware faults and start the software option upload again. (Refer to Garmin Line Maintenance Manual, Revision E or latest revision.) V. Put the AVIONICS 1 and 2 switches to the OFF position and remove the SD unlock card from the upper slot of the PFD1. W. Keep all SD unlock cards with the airplane in the blue aircraft software sleeve in the airplane's POH. X. Install the three GDU Supplement Database SD Cards into the bottom slots of the PFD1, PFD2, and MFD from which you removed them. Y. Put the AVIONICS 1 and 2 switches to the ON position and let the system power on in normal mode. Z. Make sure that no G1000 system messages, alerts, annunciations, or Red X's are shown on PFD1, PFD2, or the MFD on the AUX-SYSTEM STATUS page. (1) If there are no G1000 system messages, alerts, annunciations, or Red X's shown on PFD1, PFD2, or the MFD on the AUX-SYSTEM STATUS page, go to Step 8. (2) If the system powers ON and a red AFCS or Red X s are shown on XPDR 1 or 2 on PFD1, PFD2, or the MFD on the AUX-SYSTEM STATUS page, do as follows and skip to Step 8 at any time that the errors are extinguished. Reference the Garmin Line Maintenance Manual Revision E (or later revision) for troubleshooting instructions of all other errors. (a) Put the AVIONICS 1 and 2 switches to the OFF position. Page 8 May 15, 2012

9 (b) After no less than 10 seconds, put the AVIONICS 1 and 2 switches back to the ON position and look for errors. (c) Disengage the PFD1 circuit breaker. (d) After no less than 10 seconds, engage the PFD1 circuit breaker and look for errors. (e) Disengage the NAV1 circuit breaker. (f) After no less than 10 seconds, engage the NAV1 circuit breaker and look for errors. 8. Change the date/time format as follows: A. With the displays in normal mode, go to the AUX SYSTEM SETUP page on the MFD. B. Push the small FMS knob to activate the cursor. C. Turn the small FMS knob to expand the drop down menu and highlight UTC. D. Push the ENT key. 9. (For European registered airplanes only) Turn the large FMS knob to highlight CHANNEL SPACING in the COM CONFIG field and turn the small FMS knob to expand the drop down menu and highlight 8.33KHz. Push the ENT key. 10. Remove power from the airplane and remove the external power source. 11. Do the software and the paper documentation as follows: A. Replace the Garmin G1000 Integrated Flight Deck Cockpit Reference Guide part number (or later) with part number NOTE: Replacement of the Garmin G1000 Integrated Flight Deck Cockpit Reference Guide may not be required for airplane serials thru and airplane serials 208B2340 thru 208B2357, depending on what was provided from the factory. B. If desired, replace the Garmin G1000 Pilot's Guide part number (or later) with the optional part number C. Remove, destroy, and discard the old Garmin G1000 Software SD Loader Card from the airplane to eliminate the possibility of reloading the incorrect software at a later date. 12. Make an entry in the airplane logbook that states compliance and method of compliance with this Service Bulletin. NOTE: This information must be considered an amendment to the Cessna Manufacturer's Service/Maintenance Manual or Instructions for Continued Airworthiness and must be accomplished for ongoing airworthiness compliance as necessary in accordance with 14 CFR Part May 15, 2012 Page 9

10 MATERIAL INFORMATION The following parts are available from Cessna Service Parts and Programs through a Cessna Authorized Service Facility: The parts below will be necessary: NEW P/N QUANTITY KEY WORD OLD P/N INSTRUCTIONS/ DISPOSITION Garmin G1000 Software Version SD Loader Card (or later) Destroy and Discard * Garmin G1000 Integrated Flight Deck Cockpit Reference Guide for the Cessna Caravan (or later) Remove and Replace *The Garmin G1000 Integrated Flight Deck Cockpit Reference Guide for the Cessna Caravan may not be required for airplane serials thru and airplane serials 208B2340 thru 208B2357, depending on what was provided from the factory. The part below is optional: NEW P/N QUAN- TITY Garmin G1000 Integrated Flight Deck Pilot's Guide - Cessna Caravan KEY WORD OLD P/N INSTRUCTIONS/ DISPOSITION (or later) Remove and Replace Page 10 May 15, 2012

11 OWNER ADVISORY TITLE NAVIGATION - GARMIN G1000 SYSTEM SOFTWARE UPGRADE TO VERSION TO: Cessna Caravan Owner REASON This version software service bulletin provides an upgrade that includes the following changes: Resolution for Garmin Service Advisory No Rev A Momentary loss of GRS 77 and GDC 74A functions as addressed in Cessna Service Newsletter SNL Flight Plan Sorting The functionality of sorting the stored flight plans was removed; software fix to Garmin Service Advisory No.: 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). 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. 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. Refer to Cessna Service Letter CAL-34-01, Garmin G1000 Loading Updated Databases (or latest revision), for additional details. 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. Refer to Cessna Service Letter CAL-34-01, Garmin G1000 Loading Updated Databases (or latest revision), for additional details. Startup Screen Displays for 150 seconds at power up when dual navigation database feature is active to allow the internal database to update and will provide an error message if unsuccessful. 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". May 15, 2012 Page1of2 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A , Fax , 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

12 OWNER ADVISORY 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. 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.: Enhanced SAR Provides the base software level needed to install Enhanced Search and Rescue patterns via Cessna Service Bulletin CAB MFD Baro Knob Pressing the baro knob on the MFD during normal mode now sets STD BARO. Inset Map Settings on the inset map are now restored between power cycles. Departure Time Correctly displays the departure time when the time units are UTC. Radio Altimeter Altitude height window moved above course CRS window. MFD Status Bar Updated allowable items (BRG, XTK, DIS, DTK, END, ESA, ETA, ETE, FOD, FOB, GS, MSA, TAS, TKE, TRK, and VSR are now available). provides parts and instructions to upgrade the Garmin G1000 software to version from version (or later). COMPLIANCE MANDATORY. This service bulletin shall be accomplished at the next 100 hours or 6 months, whichever occurs first. LABOR HOURS A maximum of 3.5 man-hours to load the software upgrade and the necessary options. WARRANTY For airplanes identified within the serial effectivity and complying within 100 hours or six months from the date of this service bulletin; whichever occurs first. Applicable parts credit and a labor allowance maximum credit of 3.5 man-hours per airplane will be provided to load the software upgrade and necessary options. To receive credit, the work must be completed within stated compliance timeframe and a Warranty Claim submitted by a Cessna Caravan or Propjet Authorized Service Facility within 30 calendar days of Service Bulletin compliance before the credit expiration dates shown below. Domestic... December 15, 2012 International... December 15, 2012 Please contact a Cessna Caravan or Propjet Authorized Service Facility for detailed information and arrange to have Cessna service bulletin 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 to register. Page 2 May 15, 2012