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GARMIN G1000 SYSTEM SOFTWARE UPGRADE TO 563.14 FOR AIRPLANES EQUIPPED WITH NAV III AND GFC 700 AFCS AUTOPILOT
EFFECTIVITY
The following airplanes equipped with the Garmin G1000 Nav III Avionics Option and the Garmin GFC 700 AFCS:
Model Serial Numbers
182T 18281869, 18281876 thru 18282154
T182T T18208354, T18208665, T18208669 thru T18208922
206H 20608279, 20608284 thru 20608317
T206H T20608682, T20608705 thru T20608921
REASON
To provide a software upgrade for the Garmin G1000 System that includes the following changes:
• Garmin GFC-700 Pitch Trim Monitor Improvement: Removed a possible condition that could cause a Pitch Trim Failure when operating aircraft flaps while the GFC-700 is automatically trimming the aircraft.
• WAAS System Updates: Several GPS/WAAS system updates were implemented to improve the WAAS system using the GIA-63W. Supports removal of GPS-WAAS G1000 limitations.
• Fuel Level Sensor Updates: Implemented the support of CAN Bus Fuel Level Sensors and other fuel calibration page updates.
• CO Detector Interface: To ensure communication is re-established between the CO Guardian and the GIA-63(W).
• Resolution for Garmin Service Alert No. 0811: Implemented fix in GDU 9.02 to resolve Garmin Service Alert issue.
• Resolution for Garmin Service Advisory No. 0816B: Implemented fix in GDU 9.02 to resolve software handling of the issue transmitted in No.: 0816B.
• Resolution for Garmin Service Advisory No. 0831A: Implemented in GDU 9.00 and 9.01 to resolve the software issue transmitted in Garmin Service Advisory No. 0831A.
Page 1 of 23
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) 942-9006
COPYRIGHT © 2009
• Resolution for Garmin Service Advisory No. 0908: Implemented in GDU 9.02 to resolve the software issue transmitted in Garmin Service Advisory No. 0908 related to the DME system.
• Load Optional Airway Waypoints: Update which allows all airway waypoints (including optional waypoints) to be loaded when an airway segment is added to a flight plan.
• Resolution for Garmin Service Advisory No. 0745: Software fix removing the possible issue related to the selection of a CDI scale setting of 0.3 nm preventing WAAS vertical deviation from being displayed.
• NAVAID Frequency Loading: A software update which will automatically load the approach navaid frequency when an approach is loaded from a flight plan.
• Enhancement to Add Display of TOPO and NEXRAD Simultaneously: Allows both TOPO and NEXRAD data to be displayed on maps at the same time.
• Standard Baro Display Enhancement: Improved the precision of the Standard Barometric value (more than just 29.92), and now displays this value when selected by using the PFD1 Softkey STD BARO as ‘STD BARO’ in the baro setting window on the Altitude Tape.
• PFD Inset Map Display of TRFC-2: Added the ability to display a traffic only inset map display on the PFD; known as TRFC-2.
• Canadian XM Weather Support: Added the support of Canadian NexRad Weather Data, METAR, TAF and Winds/Temp Aloft display when XM Weather Data is available.
• TAS System Update: Updated the TAS softkey and user interface to utilize a STANDBY and NORMAL softkey operation.
• GPS Status on the AUX – GPS STATUS Page: Updated the GPS STATUS page to indicate GPS Fix, Signal Strength, Position Calculation Status, and Tracking.
• Hotspot Display: Added the display of hotspot information from the SafeTaxi database; geo-referenced overlaying the existing airport diagram and moving map.
• Map Pointer to Highlight Airways: Added the ability to highlight an Airway using the Map cursor/pointer to display the Minimum Enroute Altitude (MEA) and the Leg Distance.
• TAWS Flight Phase Transition Criteria: Modified the TAWS flight phase transition criteria to account for airports that are within close proximity of one another as to reduce TAWS nuisance alerts when entering and leaving the Departure and Approach phases of flight.
• Altitude Tape Limit: Extended the Altitude Tape lower limit from -1000 ft to -2000 ft to ease the testing of the Air Data Computer by Maintenance Personnel (reference FAR 91.411).
• High Side Current Monitor: Added High Side Current Monitor (HSCM) Calibration Page, reference the Garmin Line Maintenance Manual for additional details. Not a pilot interface change, ground use only item.
• HSDB Data Bus Resolution: Garmin fix to an issue introduced in GDU 8.20 that might suspend HSDB communication on a single Ethernet port for one minute.
• Resolution for Garmin Service Advisory No.: 0838: GPS/WAAS issue that involves a potential reset of the GPS/WAAS receiver when operating in specific northern latitudes.
DESCRIPTION
The Garmin G1000 system software should be upgraded as described in this Service Bulletin.
COMPLIANCE
Mandatory: shall be accomplished within the next 6 months or 100 hours of operation, 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: Existing Garmin software backup CDs shall be destroyed and discarded to eliminate the possibility of loading the incorrect software at a later date.
SB09-34-05 Page 2 June 22, 2009
APPROVAL
FAA approval has been obtained on technical data in this publication that affects airplane type design.
MANPOWER
2.0 man-hours to load the software upgrade
If necessary, 0.1 man-hour to load each one of the applicable configuration uploads for airplanes equipped with the following: CO Guardian, Honeywell Traffic Advisory System (TAS), Honeywell Automatic Direction Finder (ADF), Honeywell Distance Measuring Equipment (DME), Comant Antenna, GFC 700 Autopilot, or Fuel CAN BUS Fuel Level Sensors.
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, 0.4 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, 0.3 man-hour to do the applicable configuration upload for airplanes equipped with Garmin G1000 Search and Rescue.
REFERENCES
Model 172 Series 1996 and On Maintenance Manual
Model 182/T182 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 190-00384-09 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 G (or latest revision)
Garmin GDU 1040 Installation Manual, Part Number 190-00303-01, Revision M (or latest revision)
Garmin GMA 1347 Installation Manual, Part Number 190-00303-20, Revision D (or latest revision)
Garmin GIA 63 Installation Manual, Part Number 190-00303-05, Revision M (or latest revision)
Garmin GRS 77/GMU 44 Installation Manual, Part Number 190-00303-10, Revision H (or latest revision)
Garmin GDC 74A Installation Manual, Part Number 190-00303-15, Revision E (or latest revision)
Garmin GEA 71 Installation Manual, Part Number 190-00303-40, Revision D (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 N (or latest revision)
NOTE: Make sure all publications used are complete and current. Refer to cessnasupport.com.
NOTE: This information shall 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 43.13.
OTHER PUBLICATIONS AFFECTED
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 cessnasupport.com.
SB09-34-05 June 22, 2009 Page 3
MATERIAL PRICE AND AVAILABILITY
Additional copies of the parts listed below are available from Cessna Customer Service at Phone: 316-517-5800 or Fax: 316-517-7271 for the suggested list price shown.
NOTE: The 190-00384-09 Rev A Garmin G1000 Integrated Flight Deck Cockpit Reference Guide for Cessna NAV III Models and the applicable airplane model Cessna Garmin NAV III Installation Software CD are being sent to the affected airplane owners of record with Owner Advisory SB09-34-05A. The current 190-00498-04 Rev A Garmin G1000 Pilot's Guide for Cessna NAV III is optional.
Part Number Description Qty/Airplane Price
190-00384-09 Rev A Garmin G1000 Integrated Flight Deck Cockpit Reference Guide for Cessna NAV III Models 172R/172S, 182T/T182 and 206H, T206H
1 $295.00
190-00498-04 Rev A Garmin G1000 Pilot’s Guide for Cessna NAVIII
1 $595.00
CREDIT INFORMATION
For airplanes in warranty:
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 0.1 man-hour will be provided to load each one of the applicable configuration uploads for airplanes equipped with the following: CO Guardian, Honeywell Traffic Advisory System (TAS), Honeywell Automatic Direction Finder (ADF), Honeywell Distance Measuring Equipment (DME), Comant Antenna, GFC 700 Autopilot, or Fuel CAN BUS Fuel Level Sensors.
If necessary, a labor allowance credit of 0.3 man-hour will be provided to do the applicable configuration upload for airplanes equipped win the Garmin G1000 Terrain Awareness System (TAWS-B).
If necessary, a labor allowance credit of 0.4 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 0.3 man-hour will be provided to do the applicable configuration upload for airplanes equipped with Garmin G1000 Search and Rescue.
To receive credit, the work must be completed and a Warranty Claim submitted by a Cessna Single Engine Service Station within 30 calendar days of Service Bulletin compliance before the credit expiration dates shown below.
Domestic . . . . . . . . . . . . . . . . . December 22, 2009 International . . . . . . . . . . . . . . . December 22, 2009
Special Note to Service Stations:
When you complete the Warranty Claim, the labor allowance claimed shall be itemized for each above action completed.
SB09-34-05 Page 4 June 22, 2009
ACCOMPLISHMENT INSTRUCTIONS
Material Information
To complete this Service Bulletin, use one of the parts below as applicable:
NEW P/N QUANTITY DESCRIPTION OLD P/N DISPOSITION
172RGSW00-08 1 Model 172R Software CD
172RGSW00-07 and prior revisions
172SGSW00-07 and prior revisions
182TGSW00-10 and prior revisions
T182TGSW00-09 and prior revisions
206HGSW00-10 and prior revisions
T206HGSW00-09 and prior revisions
Destroy and Discard
190-00384-09 Rev A* 1 Garmin G1000 Integrated Flight Deck Cockpit Reference Guide for Cessna NAV III Models 172R/172S, 182T/T182 and 206H, T206H
190-00384-08 and prior revisions
Remove
*For serial numbers 17281545 and On, 172S10873 and On, 18282146 and On, T18208909 and On, 20608317 and On, and T20608901 and On, the Cockpit Reference Guide was provided at the time of airplane delivery from the factory.
SB09-34-05 June 22, 2009 Page 5
General Information
NOTE 1: If the system software fails to upload correctly during accomplishment of this Service Bulletin, do the software load again. Do not try to upload more than five times. If the 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 upload that is in progress. Let the system either successfully load or fail.
Instructions
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.
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.
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 190-00384-09 Revision A (or latest revision).
C. The Garmin G1000 Cockpit Reference Guide for Cessna NAV III, Part Number 190-00384-09 Rev A and the applicable airplane model Cessna Garmin NAV III Installation Software CD were sent to the aiplane owner with Owner Advisory SB09-34-05A. You must use the new CD when 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.
NOTE: For U.S. registered owners of record only: a Garmin Cockpit Reference Guide will not be sent to Duplicate Owner Advisory addresses, it will only be sent to the address as registered with the FAA.
2. Do an identification of WAAS installation and GDU boot block:
A. Connect a ground power unit to the airplane.
B. Disengage the PFD (ESS BUS and AVN BUS 1) and MFD (AVN BUS 2) circuit breakers.
C. Put the BAT MASTER switch to the ON position
D. Put the AVIONICS MASTER switches to the ON position.
E. If you have a ground power unit connected to the airplane, put the STDBY BATT switch to ARM.
F. Push and hold the ENT key on the MFD and engage the MFD (AVN BUS 2) circuit breaker.
G. Release the ENT key when the message INITIALIZING SYSTEM shows on the MFD.
H. Push and hold the ENT key on the PFD, and engage the PFD (ESS BUS and AVN BUS 1) circuit breakers.
I. Release the ENT key when the message INITIALIZING SYSTEM shows on the PFD.
J. If necessary, use the FMS knob, go to the system group SYSTEM STATUS page on the PFD.
K. Push the small FMS knob to start the cursor.
L. Turn the small FMS knob to highlight GIA1 in the LRU field.
M. In the DATA field, find the product number for the GIA.
NOTE: If the product number shown is GIA63W, WAAS is installed.
NOTE: If the product number shown is GIA63, WAAS is not installed.
N. Record which system (GIA63W or GIA63) you have for the correct system upload.
O. Turn the small FMS knob to highlight PFD1 in the LRU field.
SB09-34-05 Page 6 June 22, 2009
P. In the DATA field, find the boot block version for the PFD, shown as BB VERSION.
Q. Record the BB VERSION for the PFD1.
R. Push the FMS knob to stop the cursor.
S. Disengage the PFD (ESS BUS and AVN BUS 1) and MFD (AVN BUS 2) circuit breakers.
T. Wait a minimum of 15 seconds and then engage the PFD (ESS BUS and AVN BUS 1) and the MFD (AVN BUS 2) circuit breakers.
U. Let the system power on in normal mode.
V. On the MFD, push the ENT key when the splash screen shows.
W. Turn the large FMS knob to go to the system group and then turn the small FMS knob to go to the AUX-SYSTEM STATUS page.
X. In the AIRFRAME display box on the AUX-SYSTEM STATUS page on the MFD, find and record the SYSTEM ID.
Y. Put the AVIONICS BUS 1 and BUS 2 switches, MASTER BAT switch, and STDBY BATT switch to the off position and let the system power down.
3. (Refer to Tables 2, 3, and 4.) If you do not know which options are installed on your airplane, make sure you make a list of the installed options before you go to Step 5. This list is necessary to do the configuration procedures.
4. Install the correct PFD and MFD boot block before you install the system software version 563.14 as follows:
A. Look at the BB VERSION that you recorded:
(1) If the PFD1 BB VERSION was 2.03, go to Step 5.
(2) If the PFD1 BB VERSION was not 2.03, make sure that you have complied with Cessna Service Bulletin SB07-34-02 Revision 1 or latest revision.
(a) If the PFD1 BB VERSION is now 2.03, go to Step 5.
(b) If the PFD1 BB VERSION is not 2.03, go to Step 4B.
B. Create the boot block update SD card as follows:
(1) Put the new Cessna NAV III installation software CD in the CD drive of your computer.
(2) Right mouse click on the START button on the lower left corner of the computer screen and click on EXPLORE.
(3) Find the CD drive with the CD in it on your computer and double click it to open the CD files.
(4) Double click on the file labeled 006-B0874-00.exe.
(5) After the window opens, click the SETUP button.
(6) The next window should say that GDUIXXX, Boot Block Loader, Version v2.03 is the software.
(a) If v2.03 is the version shown, go to Step 4B(7).
(b) If v2.03 is not the version shown, go to Step 4B(4).
(7) Install a blank CD card in the SD card reader and click the NEXT button.
(8) After the next window asks for your SD reader location, click the location of the SD card reader and then click the NEXT button.
NOTE: SanDisk, Toshiba, and STEC are the three card brands that are recommended by Garmin for use in their G1000 system.
(9) When the window opens, click the NEXT button.
(10) The software will begin to transfer from the CD to the SD card, and when the data transfer is complete, click the FINISH button.
SB09-34-05 June 22, 2009 Page 7
(11) Remove the SD card from the SD card reader.
C. Load the PFD and the MFD boot block version 2.03 as follows:
(1) Disengage the PFD (ESS BUS and AVN BUS 1) and the MFD (AVN BUS 2) circuit breakers.
(2) Remove the GDU Supplemental Data SD cards from the bottom slot of the PFD and the MFD units.
(3) Mark the SD Cards PFD or MFD and store them in a safe place for later installation.
NOTE: Failure to remove the GDU Supplemental Data SD Cards before reconfiguration can result in cards that you cannot use.
(4) If installed, remove the electronic checklist SD card from the top slot of the MFD.
(5) Put the SD card with the 006-B0874-00 boot block 2.03 into the upper slot of the MFD.
(6) Put the BAT MASTER switch to the ON position.
(7) Put the AVIONICS MASTER switches to the ON position.
(8) If you have a ground power unit connected to the airplane, put the STDBY BATT switch to ARM.
(9) Push and hold the ENT key on the MFD and engage the MFD (AVN BUS2) circuit breaker.
(10) Release the ENT key when the message that follows shows on the MFD:
INITIALIZING SYSTEM
(11) Push the YES soft key when the message that follows shows on the MFD:
DO YOU WANT TO UPDATE THE BOOT BLOCK FROM 2.02 TO 2.03? NO WILL BE ASSUMED IN 30 SECONDS.
(12) When the screen shows the SYSTEM STATUS page, the boot block installation is complete.
(13) Disengage the MFD (AVN BUS2) circuit breaker and remove the SD card from the MFD slot and put it into the PFD upper SD card slot.
(14) Push and hold the ENT key on the PFD (ESS BUS and AVN BUS 1) circuit breakers.
(15) Release the ENT key when the message INITIALIZING SYSTEM shows on the PFD.
(16) Push the YES soft key when the message that follows shows on the PFD:
DO YOU WANT TO UPDATE THE BOOT BLOCK FROM 2.02 TO 2.03? NO WILL BE ASSUMED IN 30 SECONDS.
(17) The boot block installation is complete when the screen shows the SYSTEM STATUS page.
(18) Disengage the PFD (ESS BUS and AVN BUS 1) circuit breaker and remove the SD card from the PFD slot.
(19) Put the AVIONICS BUS 1 and BUS 2 switches, MASTER BAT switch, and STDBY BATT switch to the off position and let the system power down.
5. Do the NAV III (G1000) software / configuration procedures that follow:
A. Use the new Cessna NAV III Installation software CD shown in Table 1 and update the SD Card for the correct model airplane:
SB09-34-05 Page 8 June 22, 2009
TABLE 1.
Installation Software CD and Garmin System Software (G1000) Part Number
File Version
006-B0563-14 0563.14
(1) Insert the new Cessna NAV III Installation software CD into the CD drive of your computer.
(2) Right mouse click on the START button on the lower left corner of the computer screen and click on EXPLORE.
(3) Locate the CD drive with the CD in it on your computer and double click it to open the CD file.
(4) Double click on file labeled 006-B0563-14_OA.exe.
(5) When the window opens, click the SETUP button.
(6) Install a blank SD Card into the SD Card reader and click the NEXT button.
NOTE: SanDisk, Toshiba, and STEC are the three card brands that are recommended by Garmin for use in their G1000 system.
(7) The next window will ask for your SD Card reader location. Click the location of the SD Card Reader. Click the NEXT button.
(8) Click the NEXT button when the window opens.
NOTE: Any information on the SD Card will be erased.
(9) The software will begin to transfer from the CD to the SD Card.
(10) When the data has been transferred to the SD Card, click the FINISH button.
(11) Remove the SD Card from the SD Card Reader.
(12) Remove the CD from the computer and install it in the Nav III/Garmin Software sleeve in the Pilot’s Operating Handbook (POH).
B. Load the GDU (PFD1 and MFD) Software as follows:
(1) Make sure that the PFD (ESS BUS and AVN BUS 1) and the MFD (AVN BUS 2) circuit breakers are disengaged.
(2) If not previously done, remove the GDU Supplemental Data SD Cards from the bottom slot of both PFD and MFD units.
(a) Mark the SD Cards PFD or MFD and store them in a safe place for later installation.
NOTE: Failure to remove the GDU Supplemental Database SD Cards before reconfiguration can result in cards that you cannot use.
(3) Remove the electronic checklist SD card from the top slot of the MFD as applicable.
(4) Put the SD Card with the 006-B0563-14 Cessna NAV III Installation Software into the upper slot of the MFD.
(5) Put the BAT MASTER switch to the ON position.
(6) Put the AVIONICS MASTER switches to the ON position.
(7) If you have a ground power unit connected to the airplane, put the STDBY BATT switch to ARM.
(8) Push and hold the ENT key on the MFD and engage the MFD (AVN BUS 2) circuit breaker.
(9) Release the ENT key when the message that follows shows on the MFD.
INITIALIZING SYSTEM
SB09-34-05 June 22, 2009 Page 9
(10) Push the YES soft key to upload GDU system files when the messages that follows shows:
INITIALIZING SYSTEM
LOADER CARD:
-CESSNA SEP-
GPN 006-B0563-14
DO YOU WANT TO UPDATE SYSTEM FILES?
NO WILL BE ASSUMED IN 30 SECONDS.
(11) If the message that follows shows, push the YES soft key and write YES adjacent to this step.
DO YOU WANT TO UPDATE THE SPLASH SCREEN?
NOTE: You will refer to the "YES" later in these instructions.
(12) The software installation to the MFD is done when the screen goes into the configuration mode.
(13) Disengage the MFD (AVN BUS 2) circuit breaker.
(14) Remove the SD Card from the MFD slot.
(15) Push and hold the ENT key on the MFD and engage the MFD (AVN BUS 2) circuit breaker.
(16) Release the ENT key when the message that follows shows on the MFD:
INITIALIZING SYSTEM
(17) Put the SD Card into the PFD upper SD Card slot.
(18) Push and hold the ENT key on the PFD and engage the PFD (ESS BUS and AVN BUS 1) circuit breakers.
(19) Do Steps 5B(9) thru 5B(11) again for the PFD.
(20) The PFD will start in the configuration mode when you complete the update. Do not remove the power from the PFD. Keep the SD Card in the upper slot of the PFD.
C. Do the initial G1000 software and configuration upload:
(1) Turn the small 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.
NOTE: If you select the incorrect model, a message will show with the current aircraft type and the aircraft model that you selected. You must then select NO, push the ENT key, and do Step 5C(3) again to correct the airplane model.
(4) Load the full configuration software upgrade as follows:
(a) Make sure that the applicable file from Table 2, 3, or 4 is selected for the rest of this upgrade.
SB09-34-05 Page 10 June 22, 2009
CAUTION: MAKE SURE THAT YOU SELECT THE CORRECT FULL CONFIGURATION UPLOAD (WAAS OR NON-WAAS). IF YOU SELECT THE INCORRECT FULL CONFIGURATION UPLOAD FOR YOUR AIRPLANE, THERE WILL BE DAMAGE TO THE GIA63(W) AND YOU WILL HAVE TO REPLACE THE UNIT.
(5) (Refer to Table 2, 3, or 4.) Turn the small FMS knob to expand the FILE pull down menu field and highlight the Cessna applicable model airplane 006-B0563-14 Full Configuration (WAAS or non WAAS, as applicable).
(6) Push the ENT key.
(a) If a GDL69A is installed on your airplane, go to Step 5C(7). If a GDL69A is not installed on your airplane, go to Step 5C(6)(b).
(b) Turn the small FMS knob to scroll to the GDL SOFTWARE check box.
(c) Push the ENT button to deselect the GDL SOFTWARE check box.
(d) Turn the small FMS knob to scroll to the GDL CONFIGURATION check box.
(e) Push the ENT button to deselect the GDL CONFIGURATION check box.
(7) Push the LOAD soft key to install the software and configuration settings.
(8) 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.
(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 5C(7) thru 5C(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) For airplanes equipped with additional items as shown in Tables 2, 3, or 4, 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.
(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) 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 5C(10)(d) thru 5C(10)(f) 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.
(g) Do Steps 5C(10)(a) thru 5C(10)(g) again until all applicable software uploads are complete.
SB09-34-05 June 22, 2009 Page 11
TABLE 2 - Model 172.
Cessna 172S - 006-B0563-14 Full Configuration (WAAS) or Cessna 172R - 006-B0563-14 Full Configuration (WAAS) or Cessna 172S - 006-B0563-14 Full Configuration (non-WAAS) or Cessna 172R - 006-B0563-14 Full Configuration (non-WAAS) as applicable
NOTE: All GFC 700 equipped 172R/172S airplanes are WAAS airplanes.
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 172S - GFC 700 Installation Option or Cessna 172R - GFC 700 Installation Option as 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 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 (Pre 2007 Model Year Airplanes) Comant CI 2580-400 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 KN 63 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 GDL90 Installation Option
NOTE: The GDL90 is not the same equipment as the GDL69.
Cessna NAV III 2007 Model Year Airplanes equipped with Comant CI 2580-410 Antenna Configuration
NOTE: For WAAS equipped airplanes without a stand alone XM Antenna (CI 420-10)
SB09-34-05 Page 12 June 22, 2009
TABLE 3 - Model 182.
Cessna T182T - 006-B0563-14 Full Configuration (WAAS) or Cessna 182T - 006-B0563-14 Full Configuration (WAAS) or Cessna T182T - 006-B0563-14 Full Configuration (non-WAAS) or Cessna 182T - 006-B0563-14 Full Configuration (non-WAAS) as applicable
NOTE: All GFC 700 equipped 182/T182 airplanes are WAAS airplanes.
Cessna NAV III CO Guardian Installation Option
NOTE: All NAV III 2006 and on Model Year airplanes have the CO Guardian installed.
Cessna T182T GFC 700 Installation Option or Cessna 182T GFC 700 Installation Option as applicable
NOTE: All 182T and T182T NAV III 2007 and on airplanes are equipped with the GFC 700.
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 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 2007 Model Year airplanes) NAV III Comant CI 2580-410 Antenna Configuration
NOTE: Airplanes 18281869, 18281876 thru 18281977, and T18208669 thru T18208796 are equipped with the Comant CI 2480-410 antenna.
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 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 KTA 870 TAS Installation Option
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 2007 Model Year Airplanes equipped with Comant CI 2580-410 Antenna Configuration
NOTE: For WAAS equipped airplanes without a stand alone XM Antenna (CI 420-10)
SB09-34-05 June 22, 2009 Page 13
TABLE 4 - Model 206.
Cessna T206H - 006-B0563-14 Full Configuration (WAAS) or Cessna 206H -006-B0563-14 Full Configuration (WAAS) or Cessna T206H - 006-B0563-14 Full Configuration (non-WAAS) or Cessna 206H -006-B0563-14 Full Configuration (non-WAAS) as applicable
NOTE: All GFC 700 equipped 206/T206 airplanes are WAAS airplanes.
Cessna NAV III CO Guardian Installation Option
NOTE: All NAV III 2006 and on Model Year airplanes have the CO Guardian installed.
Cessna T206H GFC 700 Installation Option or Cessna 206H 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 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 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 2007 Model Year Airplanes Comant CI 2580-410 Antenna Configuration
NOTE: Airplanes 20608279, 20608284 thru 20608296, and T20608705 thru T20608774 are equipped with the Comant CI 2480-410 antenna.
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 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 KTA 870 TAS Installation Option
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.
(11) Push the small FMS knob to stop the cursor.
(12) If you wrote "YES" adjacent to Step 5B(11), go to Step 5D. If you did not write "YES" adjacent to Step 5B(11), go to Step 5C(13).
(13) Disengage the PFD (ESS BUS and AVN BUS 1), MFD (AVN BUS 2) circuit breakers.
SB09-34-05 Page 14 June 22, 2009
(14) Remove the SD Card from the PFD.
(15) Put the SD Card into the MFD upper card slot.
(16) Engage the MFD (AVN BUS 2) circuit breaker for power to the MFD.
(17) Push the NO soft key to stop the upload of the GDU system when this message shows:
INITIALIZING SYSTEM
LOADER CARD:
-CESSNA SEP-
GPN 006-B0563-14
(18) Look to see if this message shows:
INITIALIZING SYSTEM
LOADER CARD:
-CESSNA SEP-
GPN 006-B0563-14
NOT UPDATING SYSTEM FILES.
NO WILL BE ASSUMED IN 30 SECONDS.
(a) If the message above shows, push the YES soft key and then go to Step 5C(19).
(b) If the message above does not show, push any soft key when this message shows:
SB09-34-05 June 22, 2009 Page 15
INITIALIZING SYSTEM
LOADER CARD:
-CESSNA SEP-
GPN 006-B0563-14
NOT UPDATING SYSTEM FILES.
CONTINUING IN 10 SECONDS.
(19) Disengage the MFD (AVN BUS 2) circuit breaker after the upload is complete.
(20) Remove the SD Card from the MFD upper card slot.
(21) Push and hold the ENT key on the MFD.
(22) Engage the MFD (AVN BUS 2) circuit breaker.
(23) Release the ENT key when the message that follows shows on the MFD.
INITIALIZING SYSTEM
(24) Install the SD card into the top slot of the PFD.
(25) Engage the PFD (ESS BUS and AVN BUS 1) circuit breakers.
(26) Do Steps 5C(17) thru 5C(23) again for the PFD.
(27) Keep the SD Card in the upper PFD slot.
D. Do the aircraft registration number configuration:
(1) On the PFD, turn the large FMS knob to go to the GTX group. Turn the small FMS knob to go to the TRANSPONDER CONFIGURATION page.
(2) Look at the SET and ACTIVE columns in the configuration field to make sure that the ADDRESS TYPE is US TAIL or HEX ID, whichever is applicable.
(3) Make sure that the aircraft registration ADDRESS field has the correct registration number or hexadecimal number shown.
(a) If the registration number or hexadecimal number is correct, go to Step 5E.
(b) If the registration number or hexadecimal is not correct, do the steps that follow:
1 Push the small FMS knob to start the cursor.
2 Turn the large FMS knob to highlight the ADDRESS field.
3 Enter the airplane registration number or hexadecimal number.
NOTE: Turn the small FMS knob to change the letters and numbers and the large FMS knob to move to the next number or letter in the sequence.
4 Push the ENT key to configure the transponder to the new airplane registration number or hexadecimal number.
5 Look for the message CONFIGURING XPDR #1 ...WAITING... to show.
SB09-34-05 Page 16 June 22, 2009
6 After you see the XPDR #1 CONFIGURED COMPLETE message, push the ENT key to select OK.
7 Make sure that the FLIGHT ID is correct. If the FLIGHT ID is not correct, do Steps 5D(3)(b)1 thru 5D(3)(b)7 again.
8 Push the small FMS knob to stop the cursor.
E. (For airplanes equipped with the GDL69 XM Weather Data Link) Do the GDL69 configuration:
(1) On the PFD, turn the large FMS knob to go to the SYSTEM group. Turn the small FMS knob to go to the SYSTEM CONFIGURATION page.
(2) In the OTHER LRUS PRESENT field, find the GDL69. On airplanes equipped with GDL69 the GDL69 box in the OTHER LRUS PRESENT field must be green. On airplanes not equipped with GDL69, the GDL69 box in the OTHER LRUS PRESENT field must be black.
(a) If the GDL69 box is configured correctly for your airplane, go to Step 5F.
(b) If the GDL69 box is not configured correctly, do as follows:
1 Push the small FMS knob to start the cursor and highlight the GDL69 in the OTHER LRUS PRESENT field.
2 Push the ENT key to change the color of the box to the correct color for your airplane (green for airplanes equipped with GDL69 and black for airplanes not equipped with GDL69).
3 Push the small FMS knob to stop the cursor.
F. (For airplanes that are equipped with the CO Guardian) Do the CO Guardian configuration:
NOTE: All NAV III 2006 and on airplanes are equipped with the CO Guardian.
(1) On the PFD, turn the large FMS knob to go to the GIA group. Turn the small FMS knob to go to the RS-232 / ARINC 429 CONFIG page.
(2) Push the small FMS knob to start the cursor.
(3) Turn the small FMS knob to highlight GIA2 and push the ENT key.
(4) In the RS-232 field, make sure that the CHNL 4 box is green and shows CO GUARDIAN in all of the columns.
(a) If the CHNL 4 box is green and shows CO GUARDIAN in all of the columns, push the small FMS knob to stop the cursor and go to Step 5G.
(b) If the CHNL 4 box is not green or does not show CO GUARDIAN in all of the columns, do as follows:
1 Push the small FMS knob to stop the cursor.
2 Turn the large FMS knob to go to the SYSTEM group.
3 Turn the small FMS knob on the PFD to go to the SYSTEM group SYSTEM UPLOAD page.
4 Push the small FMS knob on the PFD to start the cursor.
5 Turn the small FMS knob to highlight the applicable airplane model and push the ENT key.
NOTE: If you select the incorrect model, a message will show with the current aircraft type and the aircraft model that you selected. You must then select NO, push the ENT key, and do Step 5C(3) again to correct the airplane model.
6 If the Cessna NAV III CO Guardian option is installed on your airplane, do Steps 5F(4)(b)7 thru 5F(4)(b)13. If it is not installed on your airplane, go to Step 5F(4)(b)12.
7 Turn the large FMS knob counterclockwise to go to the FILE menu.
SB09-34-05 June 22, 2009 Page 17
8 Turn the small FMS knob to expand the FILE pull down menu field and highlight the Cessna Nav III CO Guardian Installation Option.
9 Push the ENT key.
10 Push the LOAD soft key to install the software.
11 Monitor the upload status. When the Upload Complete message is shown, push the ENT key to select OK.
12 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 5F(4)(b)(10)f thru 5F(4)(b)(12) 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.
13 Push the small FMS knob to stop the cursor.
14 Do Steps 5F(1) thru 5F(4) again to make sure that CHNL 4 box is green.
G. Do the PFD configuration module update:
(1) On the PFD, turn the large FMS knob to go to the SYSTEM group. Turn the small FMS knob to go to the SYSTEM UPLOAD page.
NOTE: You do not have to select a file or an airframe for this update.
(2) Push the UPDT CFG soft key.
(3) Select YES and push the ENT key when the UPDATE CONFIG MODULE? message shows.
(4) Push the ENT key to select OK after you see the UPDATE CONFIG COMPLETE message.
6. Do the software and system verification procedures that follow:
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 8.) Make sure that the information shown in Table 8 is shown in the SYSTEM field window.
(3) Make sure that the information shown in Table 8 is shown in the SYSTEM field window.
TABLE 8.
006-B0563-14 0563.14
(4) Make sure that the information shown in Table 9 is shown in the MANIFEST field window.
NOTE: This data file is near the bottom of the list.
TABLE 9.
172R/172S 006-D0887-02 2.02
182T/T182T 006-D0270-15 2.05
206H/T206H 006-D0621-14 2.04
SB09-34-05 Page 18 June 22, 2009
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 6B(6).
(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 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.
NOTE: If you select the incorrect model, a message will show with the current aircraft type and the aircraft model that you selected. You must then select NO, push the ENT key, and do Step 6B(5)(b)3 again to correct the airplane model.
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 6B(5)(b)7 thru 6B(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.
SB09-34-05 June 22, 2009 Page 19
(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 6C.
(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.
NOTE: If you select the incorrect model, a message will show with the current aircraft type and the aircraft model that you selected. You must then select NO, push the ENT key, and do Step 6B(9)(b)3 again to correct the airplane model.
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 6B(9)(b)7 thru 6B(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.
C. Make sure that the MFD (AVN BUS 2) and the PFD (ESS BUS and AVN BUS 1) circuit breakers are engaged.
D. Put the AVIONICS and BAT MASTER switches in the off position.
E. Make sure that the STDBY BATT is in the off position.
F. Remove the SD Card from the upper slot of the PFD.
G. Put the kept database cards in the lower SD card slots on the PFD and the MFD.
H. Install the electronic checklist into the upper slot of the MFD as applicable.
7. Put the BAT MASTER switch to the ON position.
8. Put the AVIONICS MASTER switches to the ON position.
SB09-34-05 Page 20 June 22, 2009
9. Make sure that no G1000 system messages, alerts, annunciation, 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 N (or later revision) for troubleshooting instructions.
10. Put the AVIONICS and BAT MASTER switches in the off position.
11. Make sure that the STDBY BATT is in the off position.
12. Remove external power receptacle.
13. Make an entry in the airplane logbook that states compliance and method of compliance with this service bulletin.
14. (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.
15. (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.
16. (For airplanes equipped with Garmin Synthetic Vision Technology) Do the enablement of Garmin G1000 Synthetic Vision Installation, SB09-34-07 (or latest revision).
17. (For airplanes equipped with Garmin Search and Rescue) Do the Garmin G1000 Search and Rescue Enablement, SB07-34-05 (or latest revision).
OWNER NOTIFICATION
On June 22, 2009 the following message will be sent to applicable owners of record in SB09-34-05A.
Dear Cessna Owner:
This Owner Advisory is to inform you of a software upgrade for the Garmin G1000 System as provided in Service Bulletin SB09-34-05: Garmin G1000 System Software Upgrade to Version 563.14 for airplanes equipped with NAV III and GFC 700 AFCS Autopilot. The software upgrade includes the following changes:
• Garmin GFC-700 Pitch Trim Monitor Improvement: Removed a possible condition that would cause a Pitch Trim Failure when operating aircraft flaps while the GFC-700 is automatically trimming the aircraft.
• WAAS System Updates: Several GPS/WAAS system updates were implemented to improve the WAAS system using the GIA-63W. Supports removal of GPS-WAAS G1000 limitations.
• Fuel Level Sensor Updates: Implemented the support of CAN Bus Fuel Level Sensors and other fuel calibration page updates.
• CO Detector Interface: To ensure communication is re-established between the CO Guardian and the GIA-63(W).
• Resolution for Garmin Service Alert No. 0811: Implemented fix in GDU 9.02 to resolve Garmin Service Alert issue.
• Resolution for Garmin Service Advisory No. 0816B: Implemented fix in GDU 9.02 to resolve software handling of the issue transmitted in No.: 0816B.
• Resolution for Garmin Service Advisory No. 0831A: Implemented in GDU 9.00 and 9.01 to resolve the software issue transmitted in Garmin Service Advisory No. 0831A.
• Resolution for Garmin Service Advisory No. 0908: Implemented in GDU 9.02 to resolve the software issue transmitted in Garmin Service Advisory No. 0908 related to the DME system.
SB09-34-05 June 22, 2009 Page 21
• Load Optional Airway Waypoints: Update which allows all airway waypoints (including optional waypoints) to be loaded when an airway segment is added to a flight plan.
• Resolution for Garmin Service Advisory No. 0745: Software fix removing the possible issue related to the selection of a CDI scale setting of 0.3 nm preventing WAAS vertical deviation from being displayed.
• NAVAID Frequency Loading: A software update which will automatically load the approach navaid frequency when an approach is loaded from a flight plan.
• Enhancement to Add Display of TOPO and NEXRAD Simultaneously: Allows both TOPO and NEXRAD data to be displayed on maps at the same time.
• Standard Baro Display Enhancement: Improved the precision of the Standard Barometric value (more than just 29.92), and now displays this value when selected by using the PFD1 soft key STD BARO as ‘STD BARO’ in the baro setting window on the Altitude Tape.
• PFD Inset Map Display of TRFC-2: Added the ability to display a traffic only inset map display on the PFD; known as TRFC-2.
• Canadian XM Weather Support: Added the support of Canadian NexRad Weather Data, METAR, TAF and Winds/Temp Aloft display when XM Weather Data is available.
• TAS System Update: Updated the TAS softkey and user interface to utilize a STANDBY and NORMAL softkey operation.
• GPS Status on the AUX – GPS STATUS Page: Updated the GPS STATUS page to indicate GPS Fix, Signal Strength, Position Calculation Status, and Tracking.
• Hotspot Display: Added the display of hotspot information from the SafeTaxi database; geo-referenced overlaying the existing airport diagram and moving map.
• Map Pointer to Highlight Airways: Added the ability to highlight an Airway using the Map cursor/pointer to display the Minimum Enroute Altitude (MEA) and the Leg Distance.
• TAWS Flight Phase Transition Criteria: Modified the TAWS flight phase transition criteria to account for airports that are within close proximity of one another as to reduce TAWS nuisance alerts when entering and leaving the Departure and Approach phases of flight.
• Altitude Tape Limit: Extended the Altitude Tape lower limit from -1000 ft to -2000 ft to ease the testing of the Air Data Computer by Maintenance Personnel (reference FAR 91.411).
• High Side Current Monitor: Added High Side Current Monitor (HSCM) Calibration Page, reference the Garmin Line Maintenance Manual for additional details. Not a pilot interface change, ground use only item.
• HSDB Data Bus Resolution: Garmin fix to an issue introduced in GDU 8.20 that might suspend HSDB communication on a single Ethernet port for one minute.
• Resolution for Garmin Service Advisory No.: 0838: GPS/WAAS issue that involves a potential reset of the GPS/WAAS receiver when operating in specific northern latitudes.
Compliance is mandatory: shall be accomplished within the next 6 months or 100 hours of operation, 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), SB07-34-02 Revision 1, if not already accomplished, must be accomplished before installation of the 563.14 software.
NOTE: Existing Garmin software backup CDs should be destroyed and discarded to eliminate the possibility of loading the incorrect software at a later date.
The information contained in the referenced Cessna Service Bulletin shall be considered an amendment to the Cessna Manufacturer’s Maintenance Manual or Instructions for continued airworthiness, and must be accomplished for ongoing airworthiness compliance as required per CFR Part 43.13.
SB09-34-05 Page 22 June 22, 2009
Credit Information
For airplanes in warranty:
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 0.1 man-hour will be provided to load each one of the applicable configuration uploads for airplanes equipped with the following: CO Guardian, Honeywell Traffic Advisory System (TAS), Honeywell Automatic Direction Finder (ADF), Honeywell Distance Measuring Equipment (DME), Comant Antenna, GFC 700 Autopilot, or Fuel CAN BUS Fuel Level Sensors.
If necessary, a labor allowance credit of 0.3 man-hour will be provided to do the applicable configuration upload for airplanes equipped win the Garmin G1000 Terrain Awareness System (TAWS-B).
If necessary, a labor allowance credit of 0.4 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 0.3 man-hour will be provided to do the applicable configuration upload for airplanes equipped with Garmin G1000 Search and Rescue.
To receive credit, the work must be completed and a Warranty Claim submitted by a Cessna Single Engine Service Station within 30 calendar days of Service Bulletin compliance before the credit expiration dates shown below.
Domestic . . . . . . . . . . . . . . . . . December 22, 2009 International . . . . . . . . . . . . . . . December 22, 2009
The Garmin G1000 Cockpit Reference Guide for Cessna NAV III, Part Number 190-00384-09 Rev A (or latest revision) and the applicable airplane model Cessna Garmin NAV III Installation Software CD are enclosed. The Cessna Service Stations will need to utilize the enclosed CD when accomplishing this software upgrade on your airplane. When not in use, the CD should be stored in the Pilot's Operating Handbook sleeve for the NAV III Garmin Software.
NOTE: For U.S. registered owners of record only: a Garmin Cockpit Reference Guide will not be sent to Duplicate Owner Advisory addresses, it will only be sent to the address as registered with the FAA.
NOTE: For airplane serial numbers 17281545 and On, 172S10873 and On, 18282146 and On, T18208909 and On, 20608317 and On, and T20608901 and On, a current Cockpit Reference Guide was provided at the time of airplane delivery from the factory.
* * * * * * *
toc
EFFECTIVITY
REASON
DESCRIPTION
COMPLIANCE
APPROVAL
MANPOWER
REFERENCES
GARMIN G1000 SYSTEM SOFTWARE UPGRADE TO 563.14 FOR AIRPLANES EQUIPPED WITH NAV III AND GFC 700 AFCS AUTOPILOT
EFFECTIVITY
The following airplanes equipped with the Garmin G1000 Nav III Avionics Option and the Garmin GFC 700 AFCS:
Model Serial Numbers
182T 18281869, 18281876 thru 18282154
T182T T18208354, T18208665, T18208669 thru T18208922
206H 20608279, 20608284 thru 20608317
T206H T20608682, T20608705 thru T20608921
REASON
To provide a software upgrade for the Garmin G1000 System that includes the following changes:
• Garmin GFC-700 Pitch Trim Monitor Improvement: Removed a possible condition that could cause a Pitch Trim Failure when operating aircraft flaps while the GFC-700 is automatically trimming the aircraft.
• WAAS System Updates: Several GPS/WAAS system updates were implemented to improve the WAAS system using the GIA-63W. Supports removal of GPS-WAAS G1000 limitations.
• Fuel Level Sensor Updates: Implemented the support of CAN Bus Fuel Level Sensors and other fuel calibration page updates.
• CO Detector Interface: To ensure communication is re-established between the CO Guardian and the GIA-63(W).
• Resolution for Garmin Service Alert No. 0811: Implemented fix in GDU 9.02 to resolve Garmin Service Alert issue.
• Resolution for Garmin Service Advisory No. 0816B: Implemented fix in GDU 9.02 to resolve software handling of the issue transmitted in No.: 0816B.
• Resolution for Garmin Service Advisory No. 0831A: Implemented in GDU 9.00 and 9.01 to resolve the software issue transmitted in Garmin Service Advisory No. 0831A.
Page 1 of 23
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) 942-9006
COPYRIGHT © 2009
• Resolution for Garmin Service Advisory No. 0908: Implemented in GDU 9.02 to resolve the software issue transmitted in Garmin Service Advisory No. 0908 related to the DME system.
• Load Optional Airway Waypoints: Update which allows all airway waypoints (including optional waypoints) to be loaded when an airway segment is added to a flight plan.
• Resolution for Garmin Service Advisory No. 0745: Software fix removing the possible issue related to the selection of a CDI scale setting of 0.3 nm preventing WAAS vertical deviation from being displayed.
• NAVAID Frequency Loading: A software update which will automatically load the approach navaid frequency when an approach is loaded from a flight plan.
• Enhancement to Add Display of TOPO and NEXRAD Simultaneously: Allows both TOPO and NEXRAD data to be displayed on maps at the same time.
• Standard Baro Display Enhancement: Improved the precision of the Standard Barometric value (more than just 29.92), and now displays this value when selected by using the PFD1 Softkey STD BARO as ‘STD BARO’ in the baro setting window on the Altitude Tape.
• PFD Inset Map Display of TRFC-2: Added the ability to display a traffic only inset map display on the PFD; known as TRFC-2.
• Canadian XM Weather Support: Added the support of Canadian NexRad Weather Data, METAR, TAF and Winds/Temp Aloft display when XM Weather Data is available.
• TAS System Update: Updated the TAS softkey and user interface to utilize a STANDBY and NORMAL softkey operation.
• GPS Status on the AUX – GPS STATUS Page: Updated the GPS STATUS page to indicate GPS Fix, Signal Strength, Position Calculation Status, and Tracking.
• Hotspot Display: Added the display of hotspot information from the SafeTaxi database; geo-referenced overlaying the existing airport diagram and moving map.
• Map Pointer to Highlight Airways: Added the ability to highlight an Airway using the Map cursor/pointer to display the Minimum Enroute Altitude (MEA) and the Leg Distance.
• TAWS Flight Phase Transition Criteria: Modified the TAWS flight phase transition criteria to account for airports that are within close proximity of one another as to reduce TAWS nuisance alerts when entering and leaving the Departure and Approach phases of flight.
• Altitude Tape Limit: Extended the Altitude Tape lower limit from -1000 ft to -2000 ft to ease the testing of the Air Data Computer by Maintenance Personnel (reference FAR 91.411).
• High Side Current Monitor: Added High Side Current Monitor (HSCM) Calibration Page, reference the Garmin Line Maintenance Manual for additional details. Not a pilot interface change, ground use only item.
• HSDB Data Bus Resolution: Garmin fix to an issue introduced in GDU 8.20 that might suspend HSDB communication on a single Ethernet port for one minute.
• Resolution for Garmin Service Advisory No.: 0838: GPS/WAAS issue that involves a potential reset of the GPS/WAAS receiver when operating in specific northern latitudes.
DESCRIPTION
The Garmin G1000 system software should be upgraded as described in this Service Bulletin.
COMPLIANCE
Mandatory: shall be accomplished within the next 6 months or 100 hours of operation, 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: Existing Garmin software backup CDs shall be destroyed and discarded to eliminate the possibility of loading the incorrect software at a later date.
SB09-34-05 Page 2 June 22, 2009
APPROVAL
FAA approval has been obtained on technical data in this publication that affects airplane type design.
MANPOWER
2.0 man-hours to load the software upgrade
If necessary, 0.1 man-hour to load each one of the applicable configuration uploads for airplanes equipped with the following: CO Guardian, Honeywell Traffic Advisory System (TAS), Honeywell Automatic Direction Finder (ADF), Honeywell Distance Measuring Equipment (DME), Comant Antenna, GFC 700 Autopilot, or Fuel CAN BUS Fuel Level Sensors.
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, 0.4 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, 0.3 man-hour to do the applicable configuration upload for airplanes equipped with Garmin G1000 Search and Rescue.
REFERENCES
Model 172 Series 1996 and On Maintenance Manual
Model 182/T182 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 190-00384-09 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 G (or latest revision)
Garmin GDU 1040 Installation Manual, Part Number 190-00303-01, Revision M (or latest revision)
Garmin GMA 1347 Installation Manual, Part Number 190-00303-20, Revision D (or latest revision)
Garmin GIA 63 Installation Manual, Part Number 190-00303-05, Revision M (or latest revision)
Garmin GRS 77/GMU 44 Installation Manual, Part Number 190-00303-10, Revision H (or latest revision)
Garmin GDC 74A Installation Manual, Part Number 190-00303-15, Revision E (or latest revision)
Garmin GEA 71 Installation Manual, Part Number 190-00303-40, Revision D (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 N (or latest revision)
NOTE: Make sure all publications used are complete and current. Refer to cessnasupport.com.
NOTE: This information shall 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 43.13.
OTHER PUBLICATIONS AFFECTED
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 cessnasupport.com.
SB09-34-05 June 22, 2009 Page 3
MATERIAL PRICE AND AVAILABILITY
Additional copies of the parts listed below are available from Cessna Customer Service at Phone: 316-517-5800 or Fax: 316-517-7271 for the suggested list price shown.
NOTE: The 190-00384-09 Rev A Garmin G1000 Integrated Flight Deck Cockpit Reference Guide for Cessna NAV III Models and the applicable airplane model Cessna Garmin NAV III Installation Software CD are being sent to the affected airplane owners of record with Owner Advisory SB09-34-05A. The current 190-00498-04 Rev A Garmin G1000 Pilot's Guide for Cessna NAV III is optional.
Part Number Description Qty/Airplane Price
190-00384-09 Rev A Garmin G1000 Integrated Flight Deck Cockpit Reference Guide for Cessna NAV III Models 172R/172S, 182T/T182 and 206H, T206H
1 $295.00
190-00498-04 Rev A Garmin G1000 Pilot’s Guide for Cessna NAVIII
1 $595.00
CREDIT INFORMATION
For airplanes in warranty:
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 0.1 man-hour will be provided to load each one of the applicable configuration uploads for airplanes equipped with the following: CO Guardian, Honeywell Traffic Advisory System (TAS), Honeywell Automatic Direction Finder (ADF), Honeywell Distance Measuring Equipment (DME), Comant Antenna, GFC 700 Autopilot, or Fuel CAN BUS Fuel Level Sensors.
If necessary, a labor allowance credit of 0.3 man-hour will be provided to do the applicable configuration upload for airplanes equipped win the Garmin G1000 Terrain Awareness System (TAWS-B).
If necessary, a labor allowance credit of 0.4 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 0.3 man-hour will be provided to do the applicable configuration upload for airplanes equipped with Garmin G1000 Search and Rescue.
To receive credit, the work must be completed and a Warranty Claim submitted by a Cessna Single Engine Service Station within 30 calendar days of Service Bulletin compliance before the credit expiration dates shown below.
Domestic . . . . . . . . . . . . . . . . . December 22, 2009 International . . . . . . . . . . . . . . . December 22, 2009
Special Note to Service Stations:
When you complete the Warranty Claim, the labor allowance claimed shall be itemized for each above action completed.
SB09-34-05 Page 4 June 22, 2009
ACCOMPLISHMENT INSTRUCTIONS
Material Information
To complete this Service Bulletin, use one of the parts below as applicable:
NEW P/N QUANTITY DESCRIPTION OLD P/N DISPOSITION
172RGSW00-08 1 Model 172R Software CD
172RGSW00-07 and prior revisions
172SGSW00-07 and prior revisions
182TGSW00-10 and prior revisions
T182TGSW00-09 and prior revisions
206HGSW00-10 and prior revisions
T206HGSW00-09 and prior revisions
Destroy and Discard
190-00384-09 Rev A* 1 Garmin G1000 Integrated Flight Deck Cockpit Reference Guide for Cessna NAV III Models 172R/172S, 182T/T182 and 206H, T206H
190-00384-08 and prior revisions
Remove
*For serial numbers 17281545 and On, 172S10873 and On, 18282146 and On, T18208909 and On, 20608317 and On, and T20608901 and On, the Cockpit Reference Guide was provided at the time of airplane delivery from the factory.
SB09-34-05 June 22, 2009 Page 5
General Information
NOTE 1: If the system software fails to upload correctly during accomplishment of this Service Bulletin, do the software load again. Do not try to upload more than five times. If the 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 upload that is in progress. Let the system either successfully load or fail.
Instructions
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.
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.
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 190-00384-09 Revision A (or latest revision).
C. The Garmin G1000 Cockpit Reference Guide for Cessna NAV III, Part Number 190-00384-09 Rev A and the applicable airplane model Cessna Garmin NAV III Installation Software CD were sent to the aiplane owner with Owner Advisory SB09-34-05A. You must use the new CD when 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.
NOTE: For U.S. registered owners of record only: a Garmin Cockpit Reference Guide will not be sent to Duplicate Owner Advisory addresses, it will only be sent to the address as registered with the FAA.
2. Do an identification of WAAS installation and GDU boot block:
A. Connect a ground power unit to the airplane.
B. Disengage the PFD (ESS BUS and AVN BUS 1) and MFD (AVN BUS 2) circuit breakers.
C. Put the BAT MASTER switch to the ON position
D. Put the AVIONICS MASTER switches to the ON position.
E. If you have a ground power unit connected to the airplane, put the STDBY BATT switch to ARM.
F. Push and hold the ENT key on the MFD and engage the MFD (AVN BUS 2) circuit breaker.
G. Release the ENT key when the message INITIALIZING SYSTEM shows on the MFD.
H. Push and hold the ENT key on the PFD, and engage the PFD (ESS BUS and AVN BUS 1) circuit breakers.
I. Release the ENT key when the message INITIALIZING SYSTEM shows on the PFD.
J. If necessary, use the FMS knob, go to the system group SYSTEM STATUS page on the PFD.
K. Push the small FMS knob to start the cursor.
L. Turn the small FMS knob to highlight GIA1 in the LRU field.
M. In the DATA field, find the product number for the GIA.
NOTE: If the product number shown is GIA63W, WAAS is installed.
NOTE: If the product number shown is GIA63, WAAS is not installed.
N. Record which system (GIA63W or GIA63) you have for the correct system upload.
O. Turn the small FMS knob to highlight PFD1 in the LRU field.
SB09-34-05 Page 6 June 22, 2009
P. In the DATA field, find the boot block version for the PFD, shown as BB VERSION.
Q. Record the BB VERSION for the PFD1.
R. Push the FMS knob to stop the cursor.
S. Disengage the PFD (ESS BUS and AVN BUS 1) and MFD (AVN BUS 2) circuit breakers.
T. Wait a minimum of 15 seconds and then engage the PFD (ESS BUS and AVN BUS 1) and the MFD (AVN BUS 2) circuit breakers.
U. Let the system power on in normal mode.
V. On the MFD, push the ENT key when the splash screen shows.
W. Turn the large FMS knob to go to the system group and then turn the small FMS knob to go to the AUX-SYSTEM STATUS page.
X. In the AIRFRAME display box on the AUX-SYSTEM STATUS page on the MFD, find and record the SYSTEM ID.
Y. Put the AVIONICS BUS 1 and BUS 2 switches, MASTER BAT switch, and STDBY BATT switch to the off position and let the system power down.
3. (Refer to Tables 2, 3, and 4.) If you do not know which options are installed on your airplane, make sure you make a list of the installed options before you go to Step 5. This list is necessary to do the configuration procedures.
4. Install the correct PFD and MFD boot block before you install the system software version 563.14 as follows:
A. Look at the BB VERSION that you recorded:
(1) If the PFD1 BB VERSION was 2.03, go to Step 5.
(2) If the PFD1 BB VERSION was not 2.03, make sure that you have complied with Cessna Service Bulletin SB07-34-02 Revision 1 or latest revision.
(a) If the PFD1 BB VERSION is now 2.03, go to Step 5.
(b) If the PFD1 BB VERSION is not 2.03, go to Step 4B.
B. Create the boot block update SD card as follows:
(1) Put the new Cessna NAV III installation software CD in the CD drive of your computer.
(2) Right mouse click on the START button on the lower left corner of the computer screen and click on EXPLORE.
(3) Find the CD drive with the CD in it on your computer and double click it to open the CD files.
(4) Double click on the file labeled 006-B0874-00.exe.
(5) After the window opens, click the SETUP button.
(6) The next window should say that GDUIXXX, Boot Block Loader, Version v2.03 is the software.
(a) If v2.03 is the version shown, go to Step 4B(7).
(b) If v2.03 is not the version shown, go to Step 4B(4).
(7) Install a blank CD card in the SD card reader and click the NEXT button.
(8) After the next window asks for your SD reader location, click the location of the SD card reader and then click the NEXT button.
NOTE: SanDisk, Toshiba, and STEC are the three card brands that are recommended by Garmin for use in their G1000 system.
(9) When the window opens, click the NEXT button.
(10) The software will begin to transfer from the CD to the SD card, and when the data transfer is complete, click the FINISH button.
SB09-34-05 June 22, 2009 Page 7
(11) Remove the SD card from the SD card reader.
C. Load the PFD and the MFD boot block version 2.03 as follows:
(1) Disengage the PFD (ESS BUS and AVN BUS 1) and the MFD (AVN BUS 2) circuit breakers.
(2) Remove the GDU Supplemental Data SD cards from the bottom slot of the PFD and the MFD units.
(3) Mark the SD Cards PFD or MFD and store them in a safe place for later installation.
NOTE: Failure to remove the GDU Supplemental Data SD Cards before reconfiguration can result in cards that you cannot use.
(4) If installed, remove the electronic checklist SD card from the top slot of the MFD.
(5) Put the SD card with the 006-B0874-00 boot block 2.03 into the upper slot of the MFD.
(6) Put the BAT MASTER switch to the ON position.
(7) Put the AVIONICS MASTER switches to the ON position.
(8) If you have a ground power unit connected to the airplane, put the STDBY BATT switch to ARM.
(9) Push and hold the ENT key on the MFD and engage the MFD (AVN BUS2) circuit breaker.
(10) Release the ENT key when the message that follows shows on the MFD:
INITIALIZING SYSTEM
(11) Push the YES soft key when the message that follows shows on the MFD:
DO YOU WANT TO UPDATE THE BOOT BLOCK FROM 2.02 TO 2.03? NO WILL BE ASSUMED IN 30 SECONDS.
(12) When the screen shows the SYSTEM STATUS page, the boot block installation is complete.
(13) Disengage the MFD (AVN BUS2) circuit breaker and remove the SD card from the MFD slot and put it into the PFD upper SD card slot.
(14) Push and hold the ENT key on the PFD (ESS BUS and AVN BUS 1) circuit breakers.
(15) Release the ENT key when the message INITIALIZING SYSTEM shows on the PFD.
(16) Push the YES soft key when the message that follows shows on the PFD:
DO YOU WANT TO UPDATE THE BOOT BLOCK FROM 2.02 TO 2.03? NO WILL BE ASSUMED IN 30 SECONDS.
(17) The boot block installation is complete when the screen shows the SYSTEM STATUS page.
(18) Disengage the PFD (ESS BUS and AVN BUS 1) circuit breaker and remove the SD card from the PFD slot.
(19) Put the AVIONICS BUS 1 and BUS 2 switches, MASTER BAT switch, and STDBY BATT switch to the off position and let the system power down.
5. Do the NAV III (G1000) software / configuration procedures that follow:
A. Use the new Cessna NAV III Installation software CD shown in Table 1 and update the SD Card for the correct model airplane:
SB09-34-05 Page 8 June 22, 2009
TABLE 1.
Installation Software CD and Garmin System Software (G1000) Part Number
File Version
006-B0563-14 0563.14
(1) Insert the new Cessna NAV III Installation software CD into the CD drive of your computer.
(2) Right mouse click on the START button on the lower left corner of the computer screen and click on EXPLORE.
(3) Locate the CD drive with the CD in it on your computer and double click it to open the CD file.
(4) Double click on file labeled 006-B0563-14_OA.exe.
(5) When the window opens, click the SETUP button.
(6) Install a blank SD Card into the SD Card reader and click the NEXT button.
NOTE: SanDisk, Toshiba, and STEC are the three card brands that are recommended by Garmin for use in their G1000 system.
(7) The next window will ask for your SD Card reader location. Click the location of the SD Card Reader. Click the NEXT button.
(8) Click the NEXT button when the window opens.
NOTE: Any information on the SD Card will be erased.
(9) The software will begin to transfer from the CD to the SD Card.
(10) When the data has been transferred to the SD Card, click the FINISH button.
(11) Remove the SD Card from the SD Card Reader.
(12) Remove the CD from the computer and install it in the Nav III/Garmin Software sleeve in the Pilot’s Operating Handbook (POH).
B. Load the GDU (PFD1 and MFD) Software as follows:
(1) Make sure that the PFD (ESS BUS and AVN BUS 1) and the MFD (AVN BUS 2) circuit breakers are disengaged.
(2) If not previously done, remove the GDU Supplemental Data SD Cards from the bottom slot of both PFD and MFD units.
(a) Mark the SD Cards PFD or MFD and store them in a safe place for later installation.
NOTE: Failure to remove the GDU Supplemental Database SD Cards before reconfiguration can result in cards that you cannot use.
(3) Remove the electronic checklist SD card from the top slot of the MFD as applicable.
(4) Put the SD Card with the 006-B0563-14 Cessna NAV III Installation Software into the upper slot of the MFD.
(5) Put the BAT MASTER switch to the ON position.
(6) Put the AVIONICS MASTER switches to the ON position.
(7) If you have a ground power unit connected to the airplane, put the STDBY BATT switch to ARM.
(8) Push and hold the ENT key on the MFD and engage the MFD (AVN BUS 2) circuit breaker.
(9) Release the ENT key when the message that follows shows on the MFD.
INITIALIZING SYSTEM
SB09-34-05 June 22, 2009 Page 9
(10) Push the YES soft key to upload GDU system files when the messages that follows shows:
INITIALIZING SYSTEM
LOADER CARD:
-CESSNA SEP-
GPN 006-B0563-14
DO YOU WANT TO UPDATE SYSTEM FILES?
NO WILL BE ASSUMED IN 30 SECONDS.
(11) If the message that follows shows, push the YES soft key and write YES adjacent to this step.
DO YOU WANT TO UPDATE THE SPLASH SCREEN?
NOTE: You will refer to the "YES" later in these instructions.
(12) The software installation to the MFD is done when the screen goes into the configuration mode.
(13) Disengage the MFD (AVN BUS 2) circuit breaker.
(14) Remove the SD Card from the MFD slot.
(15) Push and hold the ENT key on the MFD and engage the MFD (AVN BUS 2) circuit breaker.
(16) Release the ENT key when the message that follows shows on the MFD:
INITIALIZING SYSTEM
(17) Put the SD Card into the PFD upper SD Card slot.
(18) Push and hold the ENT key on the PFD and engage the PFD (ESS BUS and AVN BUS 1) circuit breakers.
(19) Do Steps 5B(9) thru 5B(11) again for the PFD.
(20) The PFD will start in the configuration mode when you complete the update. Do not remove the power from the PFD. Keep the SD Card in the upper slot of the PFD.
C. Do the initial G1000 software and configuration upload:
(1) Turn the small 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.
NOTE: If you select the incorrect model, a message will show with the current aircraft type and the aircraft model that you selected. You must then select NO, push the ENT key, and do Step 5C(3) again to correct the airplane model.
(4) Load the full configuration software upgrade as follows:
(a) Make sure that the applicable file from Table 2, 3, or 4 is selected for the rest of this upgrade.
SB09-34-05 Page 10 June 22, 2009
CAUTION: MAKE SURE THAT YOU SELECT THE CORRECT FULL CONFIGURATION UPLOAD (WAAS OR NON-WAAS). IF YOU SELECT THE INCORRECT FULL CONFIGURATION UPLOAD FOR YOUR AIRPLANE, THERE WILL BE DAMAGE TO THE GIA63(W) AND YOU WILL HAVE TO REPLACE THE UNIT.
(5) (Refer to Table 2, 3, or 4.) Turn the small FMS knob to expand the FILE pull down menu field and highlight the Cessna applicable model airplane 006-B0563-14 Full Configuration (WAAS or non WAAS, as applicable).
(6) Push the ENT key.
(a) If a GDL69A is installed on your airplane, go to Step 5C(7). If a GDL69A is not installed on your airplane, go to Step 5C(6)(b).
(b) Turn the small FMS knob to scroll to the GDL SOFTWARE check box.
(c) Push the ENT button to deselect the GDL SOFTWARE check box.
(d) Turn the small FMS knob to scroll to the GDL CONFIGURATION check box.
(e) Push the ENT button to deselect the GDL CONFIGURATION check box.
(7) Push the LOAD soft key to install the software and configuration settings.
(8) 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.
(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 5C(7) thru 5C(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) For airplanes equipped with additional items as shown in Tables 2, 3, or 4, 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.
(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) 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 5C(10)(d) thru 5C(10)(f) 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.
(g) Do Steps 5C(10)(a) thru 5C(10)(g) again until all applicable software uploads are complete.
SB09-34-05 June 22, 2009 Page 11
TABLE 2 - Model 172.
Cessna 172S - 006-B0563-14 Full Configuration (WAAS) or Cessna 172R - 006-B0563-14 Full Configuration (WAAS) or Cessna 172S - 006-B0563-14 Full Configuration (non-WAAS) or Cessna 172R - 006-B0563-14 Full Configuration (non-WAAS) as applicable
NOTE: All GFC 700 equipped 172R/172S airplanes are WAAS airplanes.
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 172S - GFC 700 Installation Option or Cessna 172R - GFC 700 Installation Option as 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 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 (Pre 2007 Model Year Airplanes) Comant CI 2580-400 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 KN 63 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 GDL90 Installation Option
NOTE: The GDL90 is not the same equipment as the GDL69.
Cessna NAV III 2007 Model Year Airplanes equipped with Comant CI 2580-410 Antenna Configuration
NOTE: For WAAS equipped airplanes without a stand alone XM Antenna (CI 420-10)
SB09-34-05 Page 12 June 22, 2009
TABLE 3 - Model 182.
Cessna T182T - 006-B0563-14 Full Configuration (WAAS) or Cessna 182T - 006-B0563-14 Full Configuration (WAAS) or Cessna T182T - 006-B0563-14 Full Configuration (non-WAAS) or Cessna 182T - 006-B0563-14 Full Configuration (non-WAAS) as applicable
NOTE: All GFC 700 equipped 182/T182 airplanes are WAAS airplanes.
Cessna NAV III CO Guardian Installation Option
NOTE: All NAV III 2006 and on Model Year airplanes have the CO Guardian installed.
Cessna T182T GFC 700 Installation Option or Cessna 182T GFC 700 Installation Option as applicable
NOTE: All 182T and T182T NAV III 2007 and on airplanes are equipped with the GFC 700.
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 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 2007 Model Year airplanes) NAV III Comant CI 2580-410 Antenna Configuration
NOTE: Airplanes 18281869, 18281876 thru 18281977, and T18208669 thru T18208796 are equipped with the Comant CI 2480-410 antenna.
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 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 KTA 870 TAS Installation Option
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 2007 Model Year Airplanes equipped with Comant CI 2580-410 Antenna Configuration
NOTE: For WAAS equipped airplanes without a stand alone XM Antenna (CI 420-10)
SB09-34-05 June 22, 2009 Page 13
TABLE 4 - Model 206.
Cessna T206H - 006-B0563-14 Full Configuration (WAAS) or Cessna 206H -006-B0563-14 Full Configuration (WAAS) or Cessna T206H - 006-B0563-14 Full Configuration (non-WAAS) or Cessna 206H -006-B0563-14 Full Configuration (non-WAAS) as applicable
NOTE: All GFC 700 equipped 206/T206 airplanes are WAAS airplanes.
Cessna NAV III CO Guardian Installation Option
NOTE: All NAV III 2006 and on Model Year airplanes have the CO Guardian installed.
Cessna T206H GFC 700 Installation Option or Cessna 206H 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 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 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 2007 Model Year Airplanes Comant CI 2580-410 Antenna Configuration
NOTE: Airplanes 20608279, 20608284 thru 20608296, and T20608705 thru T20608774 are equipped with the Comant CI 2480-410 antenna.
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 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 KTA 870 TAS Installation Option
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.
(11) Push the small FMS knob to stop the cursor.
(12) If you wrote "YES" adjacent to Step 5B(11), go to Step 5D. If you did not write "YES" adjacent to Step 5B(11), go to Step 5C(13).
(13) Disengage the PFD (ESS BUS and AVN BUS 1), MFD (AVN BUS 2) circuit breakers.
SB09-34-05 Page 14 June 22, 2009
(14) Remove the SD Card from the PFD.
(15) Put the SD Card into the MFD upper card slot.
(16) Engage the MFD (AVN BUS 2) circuit breaker for power to the MFD.
(17) Push the NO soft key to stop the upload of the GDU system when this message shows:
INITIALIZING SYSTEM
LOADER CARD:
-CESSNA SEP-
GPN 006-B0563-14
(18) Look to see if this message shows:
INITIALIZING SYSTEM
LOADER CARD:
-CESSNA SEP-
GPN 006-B0563-14
NOT UPDATING SYSTEM FILES.
NO WILL BE ASSUMED IN 30 SECONDS.
(a) If the message above shows, push the YES soft key and then go to Step 5C(19).
(b) If the message above does not show, push any soft key when this message shows:
SB09-34-05 June 22, 2009 Page 15
INITIALIZING SYSTEM
LOADER CARD:
-CESSNA SEP-
GPN 006-B0563-14
NOT UPDATING SYSTEM FILES.
CONTINUING IN 10 SECONDS.
(19) Disengage the MFD (AVN BUS 2) circuit breaker after the upload is complete.
(20) Remove the SD Card from the MFD upper card slot.
(21) Push and hold the ENT key on the MFD.
(22) Engage the MFD (AVN BUS 2) circuit breaker.
(23) Release the ENT key when the message that follows shows on the MFD.
INITIALIZING SYSTEM
(24) Install the SD card into the top slot of the PFD.
(25) Engage the PFD (ESS BUS and AVN BUS 1) circuit breakers.
(26) Do Steps 5C(17) thru 5C(23) again for the PFD.
(27) Keep the SD Card in the upper PFD slot.
D. Do the aircraft registration number configuration:
(1) On the PFD, turn the large FMS knob to go to the GTX group. Turn the small FMS knob to go to the TRANSPONDER CONFIGURATION page.
(2) Look at the SET and ACTIVE columns in the configuration field to make sure that the ADDRESS TYPE is US TAIL or HEX ID, whichever is applicable.
(3) Make sure that the aircraft registration ADDRESS field has the correct registration number or hexadecimal number shown.
(a) If the registration number or hexadecimal number is correct, go to Step 5E.
(b) If the registration number or hexadecimal is not correct, do the steps that follow:
1 Push the small FMS knob to start the cursor.
2 Turn the large FMS knob to highlight the ADDRESS field.
3 Enter the airplane registration number or hexadecimal number.
NOTE: Turn the small FMS knob to change the letters and numbers and the large FMS knob to move to the next number or letter in the sequence.
4 Push the ENT key to configure the transponder to the new airplane registration number or hexadecimal number.
5 Look for the message CONFIGURING XPDR #1 ...WAITING... to show.
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6 After you see the XPDR #1 CONFIGURED COMPLETE message, push the ENT key to select OK.
7 Make sure that the FLIGHT ID is correct. If the FLIGHT ID is not correct, do Steps 5D(3)(b)1 thru 5D(3)(b)7 again.
8 Push the small FMS knob to stop the cursor.
E. (For airplanes equipped with the GDL69 XM Weather Data Link) Do the GDL69 configuration:
(1) On the PFD, turn the large FMS knob to go to the SYSTEM group. Turn the small FMS knob to go to the SYSTEM CONFIGURATION page.
(2) In the OTHER LRUS PRESENT field, find the GDL69. On airplanes equipped with GDL69 the GDL69 box in the OTHER LRUS PRESENT field must be green. On airplanes not equipped with GDL69, the GDL69 box in the OTHER LRUS PRESENT field must be black.
(a) If the GDL69 box is configured correctly for your airplane, go to Step 5F.
(b) If the GDL69 box is not configured correctly, do as follows:
1 Push the small FMS knob to start the cursor and highlight the GDL69 in the OTHER LRUS PRESENT field.
2 Push the ENT key to change the color of the box to the correct color for your airplane (green for airplanes equipped with GDL69 and black for airplanes not equipped with GDL69).
3 Push the small FMS knob to stop the cursor.
F. (For airplanes that are equipped with the CO Guardian) Do the CO Guardian configuration:
NOTE: All NAV III 2006 and on airplanes are equipped with the CO Guardian.
(1) On the PFD, turn the large FMS knob to go to the GIA group. Turn the small FMS knob to go to the RS-232 / ARINC 429 CONFIG page.
(2) Push the small FMS knob to start the cursor.
(3) Turn the small FMS knob to highlight GIA2 and push the ENT key.
(4) In the RS-232 field, make sure that the CHNL 4 box is green and shows CO GUARDIAN in all of the columns.
(a) If the CHNL 4 box is green and shows CO GUARDIAN in all of the columns, push the small FMS knob to stop the cursor and go to Step 5G.
(b) If the CHNL 4 box is not green or does not show CO GUARDIAN in all of the columns, do as follows:
1 Push the small FMS knob to stop the cursor.
2 Turn the large FMS knob to go to the SYSTEM group.
3 Turn the small FMS knob on the PFD to go to the SYSTEM group SYSTEM UPLOAD page.
4 Push the small FMS knob on the PFD to start the cursor.
5 Turn the small FMS knob to highlight the applicable airplane model and push the ENT key.
NOTE: If you select the incorrect model, a message will show with the current aircraft type and the aircraft model that you selected. You must then select NO, push the ENT key, and do Step 5C(3) again to correct the airplane model.
6 If the Cessna NAV III CO Guardian option is installed on your airplane, do Steps 5F(4)(b)7 thru 5F(4)(b)13. If it is not installed on your airplane, go to Step 5F(4)(b)12.
7 Turn the large FMS knob counterclockwise to go to the FILE menu.
SB09-34-05 June 22, 2009 Page 17
8 Turn the small FMS knob to expand the FILE pull down menu field and highlight the Cessna Nav III CO Guardian Installation Option.
9 Push the ENT key.
10 Push the LOAD soft key to install the software.
11 Monitor the upload status. When the Upload Complete message is shown, push the ENT key to select OK.
12 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 5F(4)(b)(10)f thru 5F(4)(b)(12) 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.
13 Push the small FMS knob to stop the cursor.
14 Do Steps 5F(1) thru 5F(4) again to make sure that CHNL 4 box is green.
G. Do the PFD configuration module update:
(1) On the PFD, turn the large FMS knob to go to the SYSTEM group. Turn the small FMS knob to go to the SYSTEM UPLOAD page.
NOTE: You do not have to select a file or an airframe for this update.
(2) Push the UPDT CFG soft key.
(3) Select YES and push the ENT key when the UPDATE CONFIG MODULE? message shows.
(4) Push the ENT key to select OK after you see the UPDATE CONFIG COMPLETE message.
6. Do the software and system verification procedures that follow:
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 8.) Make sure that the information shown in Table 8 is shown in the SYSTEM field window.
(3) Make sure that the information shown in Table 8 is shown in the SYSTEM field window.
TABLE 8.
006-B0563-14 0563.14
(4) Make sure that the information shown in Table 9 is shown in the MANIFEST field window.
NOTE: This data file is near the bottom of the list.
TABLE 9.
172R/172S 006-D0887-02 2.02
182T/T182T 006-D0270-15 2.05
206H/T206H 006-D0621-14 2.04
SB09-34-05 Page 18 June 22, 2009
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 6B(6).
(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 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.
NOTE: If you select the incorrect model, a message will show with the current aircraft type and the aircraft model that you selected. You must then select NO, push the ENT key, and do Step 6B(5)(b)3 again to correct the airplane model.
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 6B(5)(b)7 thru 6B(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.
SB09-34-05 June 22, 2009 Page 19
(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 6C.
(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.
NOTE: If you select the incorrect model, a message will show with the current aircraft type and the aircraft model that you selected. You must then select NO, push the ENT key, and do Step 6B(9)(b)3 again to correct the airplane model.
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 6B(9)(b)7 thru 6B(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.
C. Make sure that the MFD (AVN BUS 2) and the PFD (ESS BUS and AVN BUS 1) circuit breakers are engaged.
D. Put the AVIONICS and BAT MASTER switches in the off position.
E. Make sure that the STDBY BATT is in the off position.
F. Remove the SD Card from the upper slot of the PFD.
G. Put the kept database cards in the lower SD card slots on the PFD and the MFD.
H. Install the electronic checklist into the upper slot of the MFD as applicable.
7. Put the BAT MASTER switch to the ON position.
8. Put the AVIONICS MASTER switches to the ON position.
SB09-34-05 Page 20 June 22, 2009
9. Make sure that no G1000 system messages, alerts, annunciation, 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 N (or later revision) for troubleshooting instructions.
10. Put the AVIONICS and BAT MASTER switches in the off position.
11. Make sure that the STDBY BATT is in the off position.
12. Remove external power receptacle.
13. Make an entry in the airplane logbook that states compliance and method of compliance with this service bulletin.
14. (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.
15. (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.
16. (For airplanes equipped with Garmin Synthetic Vision Technology) Do the enablement of Garmin G1000 Synthetic Vision Installation, SB09-34-07 (or latest revision).
17. (For airplanes equipped with Garmin Search and Rescue) Do the Garmin G1000 Search and Rescue Enablement, SB07-34-05 (or latest revision).
OWNER NOTIFICATION
On June 22, 2009 the following message will be sent to applicable owners of record in SB09-34-05A.
Dear Cessna Owner:
This Owner Advisory is to inform you of a software upgrade for the Garmin G1000 System as provided in Service Bulletin SB09-34-05: Garmin G1000 System Software Upgrade to Version 563.14 for airplanes equipped with NAV III and GFC 700 AFCS Autopilot. The software upgrade includes the following changes:
• Garmin GFC-700 Pitch Trim Monitor Improvement: Removed a possible condition that would cause a Pitch Trim Failure when operating aircraft flaps while the GFC-700 is automatically trimming the aircraft.
• WAAS System Updates: Several GPS/WAAS system updates were implemented to improve the WAAS system using the GIA-63W. Supports removal of GPS-WAAS G1000 limitations.
• Fuel Level Sensor Updates: Implemented the support of CAN Bus Fuel Level Sensors and other fuel calibration page updates.
• CO Detector Interface: To ensure communication is re-established between the CO Guardian and the GIA-63(W).
• Resolution for Garmin Service Alert No. 0811: Implemented fix in GDU 9.02 to resolve Garmin Service Alert issue.
• Resolution for Garmin Service Advisory No. 0816B: Implemented fix in GDU 9.02 to resolve software handling of the issue transmitted in No.: 0816B.
• Resolution for Garmin Service Advisory No. 0831A: Implemented in GDU 9.00 and 9.01 to resolve the software issue transmitted in Garmin Service Advisory No. 0831A.
• Resolution for Garmin Service Advisory No. 0908: Implemented in GDU 9.02 to resolve the software issue transmitted in Garmin Service Advisory No. 0908 related to the DME system.
SB09-34-05 June 22, 2009 Page 21
• Load Optional Airway Waypoints: Update which allows all airway waypoints (including optional waypoints) to be loaded when an airway segment is added to a flight plan.
• Resolution for Garmin Service Advisory No. 0745: Software fix removing the possible issue related to the selection of a CDI scale setting of 0.3 nm preventing WAAS vertical deviation from being displayed.
• NAVAID Frequency Loading: A software update which will automatically load the approach navaid frequency when an approach is loaded from a flight plan.
• Enhancement to Add Display of TOPO and NEXRAD Simultaneously: Allows both TOPO and NEXRAD data to be displayed on maps at the same time.
• Standard Baro Display Enhancement: Improved the precision of the Standard Barometric value (more than just 29.92), and now displays this value when selected by using the PFD1 soft key STD BARO as ‘STD BARO’ in the baro setting window on the Altitude Tape.
• PFD Inset Map Display of TRFC-2: Added the ability to display a traffic only inset map display on the PFD; known as TRFC-2.
• Canadian XM Weather Support: Added the support of Canadian NexRad Weather Data, METAR, TAF and Winds/Temp Aloft display when XM Weather Data is available.
• TAS System Update: Updated the TAS softkey and user interface to utilize a STANDBY and NORMAL softkey operation.
• GPS Status on the AUX – GPS STATUS Page: Updated the GPS STATUS page to indicate GPS Fix, Signal Strength, Position Calculation Status, and Tracking.
• Hotspot Display: Added the display of hotspot information from the SafeTaxi database; geo-referenced overlaying the existing airport diagram and moving map.
• Map Pointer to Highlight Airways: Added the ability to highlight an Airway using the Map cursor/pointer to display the Minimum Enroute Altitude (MEA) and the Leg Distance.
• TAWS Flight Phase Transition Criteria: Modified the TAWS flight phase transition criteria to account for airports that are within close proximity of one another as to reduce TAWS nuisance alerts when entering and leaving the Departure and Approach phases of flight.
• Altitude Tape Limit: Extended the Altitude Tape lower limit from -1000 ft to -2000 ft to ease the testing of the Air Data Computer by Maintenance Personnel (reference FAR 91.411).
• High Side Current Monitor: Added High Side Current Monitor (HSCM) Calibration Page, reference the Garmin Line Maintenance Manual for additional details. Not a pilot interface change, ground use only item.
• HSDB Data Bus Resolution: Garmin fix to an issue introduced in GDU 8.20 that might suspend HSDB communication on a single Ethernet port for one minute.
• Resolution for Garmin Service Advisory No.: 0838: GPS/WAAS issue that involves a potential reset of the GPS/WAAS receiver when operating in specific northern latitudes.
Compliance is mandatory: shall be accomplished within the next 6 months or 100 hours of operation, 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), SB07-34-02 Revision 1, if not already accomplished, must be accomplished before installation of the 563.14 software.
NOTE: Existing Garmin software backup CDs should be destroyed and discarded to eliminate the possibility of loading the incorrect software at a later date.
The information contained in the referenced Cessna Service Bulletin shall be considered an amendment to the Cessna Manufacturer’s Maintenance Manual or Instructions for continued airworthiness, and must be accomplished for ongoing airworthiness compliance as required per CFR Part 43.13.
SB09-34-05 Page 22 June 22, 2009
Credit Information
For airplanes in warranty:
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 0.1 man-hour will be provided to load each one of the applicable configuration uploads for airplanes equipped with the following: CO Guardian, Honeywell Traffic Advisory System (TAS), Honeywell Automatic Direction Finder (ADF), Honeywell Distance Measuring Equipment (DME), Comant Antenna, GFC 700 Autopilot, or Fuel CAN BUS Fuel Level Sensors.
If necessary, a labor allowance credit of 0.3 man-hour will be provided to do the applicable configuration upload for airplanes equipped win the Garmin G1000 Terrain Awareness System (TAWS-B).
If necessary, a labor allowance credit of 0.4 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 0.3 man-hour will be provided to do the applicable configuration upload for airplanes equipped with Garmin G1000 Search and Rescue.
To receive credit, the work must be completed and a Warranty Claim submitted by a Cessna Single Engine Service Station within 30 calendar days of Service Bulletin compliance before the credit expiration dates shown below.
Domestic . . . . . . . . . . . . . . . . . December 22, 2009 International . . . . . . . . . . . . . . . December 22, 2009
The Garmin G1000 Cockpit Reference Guide for Cessna NAV III, Part Number 190-00384-09 Rev A (or latest revision) and the applicable airplane model Cessna Garmin NAV III Installation Software CD are enclosed. The Cessna Service Stations will need to utilize the enclosed CD when accomplishing this software upgrade on your airplane. When not in use, the CD should be stored in the Pilot's Operating Handbook sleeve for the NAV III Garmin Software.
NOTE: For U.S. registered owners of record only: a Garmin Cockpit Reference Guide will not be sent to Duplicate Owner Advisory addresses, it will only be sent to the address as registered with the FAA.
NOTE: For airplane serial numbers 17281545 and On, 172S10873 and On, 18282146 and On, T18208909 and On, 20608317 and On, and T20608901 and On, a current Cockpit Reference Guide was provided at the time of airplane delivery from the factory.
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EFFECTIVITY
REASON
DESCRIPTION
COMPLIANCE
APPROVAL
MANPOWER
REFERENCES