print preview - c:docume~1e3userlocals~1tempe3temp 3904

Single Engine

Service Bulletin

July 23, 2007 SB07-34-02

TITLE

GARMIN G1000 SYSTEM SOFTWARE UPGRADE TO VERSION 563.03

EFFECTIVITY

The following airplanes equipped with the Garmin G1000 Nav III Avionics Option.

Model Serial Numbers

172R 17281241 thru 17281251, 17281253 thru 17281258, 17281260,17281262 thru 17281264, 17281269, 17281271 thru 17281277 and17281298 thru 17281407

172S 172S9810, 172S9811, 172S9813 thru 172S9847, 172S9849,172S9851 thru 172S9857, 172S9859, 172S9860, 172S9862 thru172S9887, 172S9889 thru 172S9902, 172S9904, 172S9906thru 172S9920, 172S9922 thru 172S9951, 172S9953 thru172S9963, 172S9965, 172S9967, 172S9968, 172S9970 thru172S9979, 172S9982, 172S9985 thru 172S9997, 172S9999thru 172S10033, 172S10035 thru 172S10044, 172S10046 thru172S10056, 172S10061, 172S10064 thru 172S10069, 172S10071thru 172S10082, 172S10084 thru 172S10089, 172S10091thru 172S10097, 172S10099 thru 172S10108, 172S10110 thru172S10132 and 172S10134 thru 172S10574

182T 18281228, 18281318 thru 18281407, 18281409, 18281410,18281412 thru 18281435, 18281437 thru 18281446, 18281448 thru18281454, 18281456 thru 18281524, 18281526 thru 18281540,18281543 thru 18281550, 18281552 thru 18281580, 18281582 thru18281619, 18281621 thru 18281650 and 18281652 thru 18281954

T182T T18208232 thru T18208275, T18208277 thru T18208309,T18208311 thru T18208506 and T18208508 thru T18208769

206H 20608216 thru 20608218, 20608220 thru 20608227, 20608229,20608230, 20608233, 20608234, 20608237, 20608238, 20608240thru 20608244, 20608246, 20608247, 20608250 and 20608252thru 20608293

T206H T20608450 thru T20608594 and T20608596 thru T20608754

of 21

To obtain satisfactory results, procedures specified in this publication must be accomplished in accordance with accepted methods andprevailing government regulations. Cessna Aircraft Company cannot be responsible for the quality of work performed in accomplishing therequirements of this publication.

Cessna Aircraft Company, Product Support, P.O. Box 7706, Wichita, Kansas 67277, U.S.A. (316) 517-5800, Facsimile (316) 942-9006

COPYRIGHT © 2007

REASON

To provide a software upgrade for the Garmin G1000 System that includes the following changes:

Garmin Aerial Navigation Product Alert - Service Alert 070227-00 Resolution: Cessna Service BulletinSB07-25-03, Garmin G1000 Arrival and Departure Procedures Software Alert, transmitted Garmin’s ServiceAlert. These documents communicated the requirement to remove the active arrival or departure procedureprior to loading a new arrival or departure procedure. Compliance with this Service Bulletin (SB07-34-02) byloading software version 563.03 will no longer require the manual method to remove the active arrival ordeparture procedure as described above. Compliance with Garmin Service Bulletin No.: 0708 Revision A,AFM/AFMS Limitation for G1000 Systems, is not required as software version 563.03 includes the 8.02software for the PFD/MFD units.

Garmin GDL-69A XM® Radio/Weather System: Reference Cessna Service Newsletter SNL07-1/GarminService Advisory NO.: 0613 concerning the storm cell tracking limitation. The greater than 400 storm cells issueis resolved with this software upgrade. Enhancements are also provided for the pilot’s interface with the system.

Reversionary Mode Timing: Displays enter reversionary mode automatically and require 5 seconds of normaloperation before returning to normal display mode to prevent possible reversionary mode cycling events(change affects both automatic and manual reversionary mode).

Reversionary Mode Inset Map: Added functionality to the PFD/MFD reversionary mode to show the InsetMap if selected.

Barometric Altitude Minimum: Enable aural alert for this function.

Alternate Transponder Code Entry Procedure: Provides the pilot with another way to enter transpondercodes by using the FMS knob in addition to the existing softkey code method.

VHF COM Transmit Indications: Enabled RX and SQ indicators to be visible in the same location as the TXindicator when the specific VHF COM is either transmitting “TX”, receiving with automatic squelch active “RX”or when manual squelch is open “SQ”.

Track Vector: Added the ability to adjust the look ahead time for the track vector.

Victor Airways: Added Victor Airways to the flight plan capability.

TAWS-B System: Changes incorporated to reduce nuisance alerts. Added an “INHIBIT” softkey when on theTAWS Map Page for inhibiting TAWS-B aural alerts. Refer to SB06-34-03 Revision 1 (or latest revision).

MFD Splash Screen For Aviation Database Status: Refined the display format of the aviation databasename, version, and effective dates. This also affects the display format for Land, Obstacle, Terrain, SafeTaxi,FliteCharts and Jeppesen ChartView databases if installed.

Auto-Acknowledge Aural Alert: Configuration changes to ensure aural alerts are provided at systempower-on.

Fuel Calibration: Revised the Fuel Calibration Page in the G1000 Configuration Mode.

SB07-34-02 July 23, 2007

The following changes were incorporated on model year 2007 Nav III airplanes and are provided as newchanges to all Nav III equipped airplanes that are in compliance with Service Bulletin SB06-34-02 orSB06-34-02 Revision 1: Garmin G1000 System Software Update:

Jeppesen ChartView: Added support for the optional installation of the Jeppesen electronic terminalprocedures charts known as ChartView. Refer to SB07-34-01 Revision 1 (or latest revision).

Garmin SafeTaxi & FliteCharts: Added support for Garmin SafeTaxi and FliteChart electronic chart products.Refer to SB07-34-04 (or latest revision).

XM Radio Interface: Added the ability for inner and outer FMS knobs to input the channel number on theXM radio page. Added provisions for indicating on the XM radio page if the GDL 69 unit fails. Added mappanning capability of altitude information for cloud tops on the weather datalink page and text instructions forthe LOCK softkey on the XM information page. The XM activation page will now dynamically update thepresence of the radio softkey based upon whether the XM radio signal is present or not. The XM signalstrength status indicator has been added to aid in diagnostics. Added age information in all the maps thatcould depict the data link weather.

Current Track Bug: Feature added to display the airplane's current track on the HSI.

Wind Data Window: Includes an additional wind data window to provide various formats of wind magnitude,direction, crosswind and headwind components.

Vertical Navigation: Added support for assigning altitude constraints with vertical waypoints to give verticalnavigation guidance.

Barometric Altitude Minimum: New functionality added for setting a minimum descent altitude.

Transponder GND Softkey: Added a transponder GND softkey to allow manual selection of Ground Mode.

Traffic Information Service (TIS): Enhanced TIS functionality by disabling TIS on the ground to avoidnuisance alerts, and allow muting of the TIS Not Available (TNA) alert by use of a new TNA MUTE softkey.

Temporary Flight Restrictions (TFR) Display: Enhanced highlighting of waypoints beneath some TFR'sand TFR highlighting while using the map pointer.

ADF Superflag: Added support for the ADF relative bearing pointer display to be shown when an ADFSuperflag signal is sensed and removal of bearing pointer when signal is low.

Software & Configuration Loading: Enhanced and simplified the software loading procedures.

LRU Port Info: Added increased diagnostic support in configuration mode to allow quicker verification ofoperating or failed data paths.

ARINC 424 Database Leg Types: Added support for these procedures to be displayed on the MFD.

SB07-34-02July 23, 2007

DESCRIPTION

The Garmin G1000 system software shall be upgraded as described in this Service Bulletin.

COMPLIANCE

Mandatory: shall be accomplished within the next 100 hours of operation or 12 months, whichever occurs first.

NOTE: Existing Garmin Software Backup CDs should be destroyed and discarded to eliminate the possibilityof reloading the incorrect software at a later date.

NOTE: For airplanes affected by Cessna Service Bulletin SB06-34-02 or SB06-34-02 Revision 1 (GarminG1000 System Software Upgrade): SB06-34-02 Revision 1 if not already accomplished must beaccomplished prior to compliance with this service bulletin.

APPROVAL

FAA approval has been obtained on technical data in this publication that affects airplane type design.

MANPOWER

1.6 man-hours to load the software upgradeIf necessary, 0.1 man-hour for each one of the applicable configuration uploads for airplanes equipped withthe following: CO Guardian, Honeywell Traffic Advisory System (TAS), Honeywell Automatic Direction Finder(ADF), Honeywell Distance Measuring Equipment (DME), or Artex C406-N Emergency Locator Transmitter(ELT)If necessary, 0.3 man-hour to do the applicable configuration upload for airplanes equipped with the GarminG1000 Terrain Awareness Warning System (TAWS-B)If necessary, 0.4 man-hour to do the applicable configuration upload for airplanes equipped with the GarminG1000 ChartView System

REFERENCES

Model 172 Series 1996 and On Maintenance ManualModel 182/T182 Series 1997 and On Maintenance ManualModel 206/T206 Series 1998 and On Maintenance ManualGarmin G1000 Cockpit Reference Guide for Cessna NAV III, Part Number 190-00384-07 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 F (or latest revision)Garmin GDU 1040 Installation Manual, Part Number 190-00303-01, Revision H (or latest revision)Garmin GMA 1347 Installation Manual, Part Number 190-00303-20, Revision C (or latest revision)Garmin GIA 63 Installation Manual, Part Number 190-00303-05, Revision K (or latest revision)Garmin GRS 77/GMU 44 Installation Manual, Part Number 190-00303-10, Revision F (or latest revision)Garmin GDC 74A Installation Manual, Part Number 190-00303-15, Revision C (or latest revision)Garmin GEA 71 Installation Manual, Part Number 190-00303-40, Revision B (or latest revision)Garmin GTX 33 Installation Manual, Part Number 190-00303-61, Revision F (or latest revision)Garmin G1000 NAV III Line Maintenance Manual, Part Number 190-00352-00, Revision H (or latest revision)Garmin G1000 Line Maintenance Manual And Configuration Manual, Part Number 190-00303-04, Revision D(or latest revision)

NOTE: Make sure all publications used are complete and current.

NOTE: This information shall be considered an amendment to the Cessna Manufacturer's Service/MaintenanceManual or Instructions for continued airworthiness and should be accomplished for ongoingairworthiness compliance as required per 14 CFR Part 43.13.

SB07-34-02 July 23, 2007

OTHER PUBLICATIONS AFFECTED

Model 172 Illustrated Parts CatalogModel 182S/182T/T182T Illustrated Parts CatalogModel 206H & Model T206H Illustrated Parts Catalog

NOTE: Make sure all publications used are complete and current.

MATERIAL PRICE AND AVAILABILITY

Not applicable

CREDIT INFORMATION

A labor allowance credit of 1.6 man-hours per airplane will be provided to load the software upgrade.

1. If necessary, 0.1 man-hour for each one of the applicable configuration uploads for airplanes equippedwith the following: CO Guardian, Honeywell Traffic Advisory System (TAS), Honeywell AutomaticDirection Finder (ADF), Honeywell Distance Measuring Equipment (DME), or Artex C406-N EmergencyLocator Transmitter (ELT)

2. If necessary, 0.3 man-hour to do the applicable configuration upload for airplanes equipped with theGarmin Terrain Awareness Warning System (TAWS-B)

3. If necessary, 0.4 man-hour to do the applicable configuration upload for airplanes equipped with theGarmin G1000 ChartView System

To receive credit, the work must be completed and a Warranty Claim submitted by a Cessna Single EngineService Station within 30 calendar days of Service Bulletin compliance before the credit expiration datesshown below.

Domestic . . . . . . . . . . . . . . . . . . . . . . July 23, 2008International . . . . . . . . . . . . . . . . . . . . July 23, 2008

Special Note to Service Stations:When you complete the Warranty Claim, the labor allowance claimed shall be itemized for each above actioncompleted.

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

172RGSW00-05 1 Model 172RSoftware CD

172RGSW00-03 Destroy andDiscard

172SGSW00-05 1 Model 172SSoftware CD

172SGSW00-03 Destroy andDiscard

182TGSW00-08 1 Model 182TSoftware CD

182TGSW00-06 Destroy andDiscard

T182TGSW00-07 1 Model T182TSoftware CD

T182TGSW00-05 Destroy andDiscard

206HGSW00-08 1 Model 206HSoftware CD

206HGSW00-06 Destroy andDiscard

T206HGSW00-07 1 Model T206HSoftware CD

T206HGSW00-05 Destroy andDiscard

SB07-34-02July 23, 2007

General Information

NOTE 1: If the system software fails to upload correctly during accomplishment of this ServiceBulletin, do the software load again. Do not try to upload more than five times. If thesystem does not upload after the fifth attempt, contact Cessna Propeller Aircraft ProductSupport. Do not cancel a software upload that is in progress. Let the system eithersuccessfully load or fail.

Instructions

NOTE: As necessary, you can use a ground power unit as the power source when you do this Service Bulletin.

1. Do the software and paper documentation:

A. Remove the old Cessna NAV III Installation Software CD from the sleeve in the Pilot's OperatingHandbook (POH) and get the new Cessna NAV III Installation Software CD to load the new software.

B. The Garmin G1000 Cockpit Reference Guide for Cessna NAV III, Part Number 190-00384-07 Rev.A and the applicable airplane model Cessna Garmin NAV III Installation Software CD were sent tothe airplane owner in Owner Advisory SB07-34-02A. You must use the new CD when you do thesoftware upgrade on the airplane. When not in use, the CD should be stored in the Pilot's OperatingHandbook sleeve for the NAV III/Garmin Software.

NOTE: For U.S. registered owners of record only: a Garmin Cockpit Reference Guide will not besent to Duplicate Owner Advisory addresses, it will only be sent to the address as registeredwith the FAA.

C. Destroy and discard the existing Garmin Software Backup CD's to eliminate the possibility ofreloading the incorrect software at a later date.

D. Make sure that the airplane paperwork has the Garmin G1000 Cockpit Reference Guide for CessnaNAV III, with a document number of 190-00384-07 Rev. A.

(1) If the guide installed is not current, remove the guide and replace it with the current referenceguide.

NOTE: The 190-00384-07 Rev. A, Garmin G1000 Cockpit Reference Guide for Cessna NAVIII, was sent to the airplane owner of record with Owner Advisory SB07-34-02A. ForU.S. registered owners of record only: a Garmin Cockpit Reference Guide will not besent to Duplicate Owners Advisory addresses, it will only be sent to the address asregistered with the FAA.

2. Do an identification of WAAS installation:

A. Disengage the PFD (ESS BUS and AVN BUS 1) and MFD (AVN BUS 2) circuit breakers.

B. Put the BAT MASTER switch to the ON position

C. Put the AVIONICS MASTER switches to the ON position.

D. Push and hold the ENT key on the MFD and engage the MFD (AVN BUS 2) circuit breaker.

E. Release the ENT key when the message INITIALIZING SYSTEM shows on the MFD.

F. Push and hold the ENT key on the PFD, and engage the PFD (ESS BUS and AVN BUS 1) circuitbreakers.

G. Release the ENT key when the message INITIALIZING SYSTEM shows on the PFD.

H. If necessary, use the FMS knob, go to the system group SYSTEM STATUS page on the PFD.

I. Push the small FMS knob to start the cursor.

J. Turn the small FMS knob to highlight GIA1 in the LRU field.

SB07-34-02 July 23, 2007

K. 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.

L. Record which system (GIA63W or GIA63) you have for the correct system upload.

M. Disengage the PFD (ESS BUS and AVN BUS 1) and MFD (AVN BUS 2) circuit breakers.

3. (Refer to Tables 2, 3, and 4.) If you do not know which options are installed on your airplane, makesure you make a list of the installed options before you go to Step 4. This list is necessary to do theconfiguration procedures.

4. 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 forthe correct model airplane:

TABLE 1.

SD Software Loader Card Part Number andGarmin System Software (G1000) Part Number

File Version

006-B0563-03 1.00

(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 andclick 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-B0563-03.

(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.

(7) The next window will ask for your SD Card reader location. Click the location of the SD CardReader. 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 thePilot’s Operating Handbook (POH).

B. Load the GDU (PFD1 and MFD1) Software as follows:

(1) Disengage the PFD (ESS BUS and AVN BUS 1) and the MFD (AVN BUS 2) circuit breakers.

(2) Remove the obstacle/terrain 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 obstacle/terrain data SD Cards before reconfiguration canresult in obstacles that do not show on the display correctly.

(3) Put the SD Card with the 006-B0563-03 Cessna NAV III Installation Software into the upperslot of the MFD.

(4) Push and hold the ENT key on the MFD and engage the MFD (AVN BUS 2) circuit breaker.

SB07-34-02July 23, 2007

(5) Release the ENT key when the message INITIALIZING SYSTEM shows on the MFD.

(6) Push the YES soft key when either one or the other of the following messages show on theMFD:

DO YOU WANT TO UPDATE THE BOOT BLOCK FROM 2.02 TO 2.03?

NO WILL BE ASSUMED IN 30 SECONDS.

or

DO YOU WANT TO UPDATE SYSTEM FILES?


(7) Push the YES soft key when either one or the other of the messages that follow shows:

PRESS ANY KEY TO CONTINUE.

CONTINUING IN 10 SECONDS.

or

DO YOU WANT TO UPDATE SPLASH SCREEN?


(8) The software installation to the MFD is done when the screen shows the SYSTEM STATUSpage.

(9) Do not remove power from the MFD. Remove the SD Card from the MFD slot and put it intothe PFD upper SD Card slot.

(10) Push and hold the ENT key on the PFD and engage the PFD (ESS BUS and AVN BUS1)circuit breakers.

(11) Do Steps 4B(4) thru 4B(7) again for the PFD.

(12) The PFD will start in the SYSTEM STATUS page when you complete the update. Do notremove 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 typeand the aircraft model that you selected. You must then select NO, push the ENT key,and do Step 4C(3) again to correct the airplane model.

SB07-34-02 July 23, 2007

(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 ofthis upgrade.

NOTE: All NAV III 2006 and on airplanes are equipped with the CO Guardian.

TABLE 2 - Model 172.

172R/172S AIRPLANE MODEL CONFIGURATION FILE SELECTIONS- PULL-DOWN MENU

Cessna 172R (or 172S as applicable) - 006-B0563-03 Full Configuration (non-WAAS)

Cessna 172R (or 172S as applicable) - 006-B0563-03 Full Configuration (WAAS)

Cessna NAV III CO Guardian Installation Option

Cessna NAV III KR 87 ADF Installation Option

Cessna NAV III (Pre 2007 Model Year Airplanes) Comant CI 2480-400 Antenna Configuration

Cessna NAV III KN 63 DME Installation Option

Cessna NAV III Artex C406-N ELT Installation Option

Cessna NAV III GDL90 Installation Option

NOTE: The GDL90 is not the same equipment as the GDL69.


182T/T182T AIRPLANE MODEL CONFIGURATION FILE SELECTIONS- PULL-DOWN MENU

Cessna 182T (or T182T as applicable) - 006-B0563-03 Full Configuration (non-WAAS)

Cessna 182T (or T182T as applicable) - 006-B0563-03 Full Configuration (WAAS)


Cessna 182T (or T182T as applicable) GFC 700 Installation Option



Cessna NAV III KN63 DME Installation Option


Cessna NAV III KAP 140 Installation Option

Cessna NAV III KTA870 TAS Installation Option


206H/T206H AIRPLANE MODEL CONFIGURATION FILE SELECTIONS- PULL-DOWN MENU

Cessna 206H (or T206H as applicable) - 006-B0563-03 Full Configuration (non-WAAS)

Cessna 206H (or T206H as applicable) - 006-B0563-03 Full Configuration (WAAS)


Cessna 206H (or T206H as applicable) GFC 700 Installation Option

SB07-34-02July 23, 2007

206H/T206H AIRPLANE MODEL CONFIGURATION FILE SELECTIONS- PULL-DOWN MENU



Cessna NAV III KN63 DME Installation Option


Cessna NAV III KAP 140 Installation Option

Cessna NAV III KTA870 TAS Installation Option

CAUTION: MAKE SURE THAT YOU SELECT THE CORRECT FULL CONFIGURATIONUPLOAD (WAAS OR NON-WAAS). IF YOU SELECT THE INCORRECTFULL CONFIGURATION UPLOAD FOR YOUR AIRPLANE, THERE WILL BEDAMAGE TO THE GIA63 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 fieldand highlight the Cessna applicable model airplane 006-B0563-03 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 4C(7). If a GDL69A is not installedon your airplane, go to Step 4C(6)(b).

(b) Turn the small FMS knob to scroll to the GDL SOFTWARE check box.

(c) Press 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) Press 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 ENTkey to select OK.

NOTE: This may take several 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 4C(7) thru 4C(9) again asnecessary up to a total of five times until you successfully complete the configuration upload. Ifafter five times the software configuration fails, correct the hardware failure and start theconfiguration upload again.

(10) For airplanes equipped with additional items as shown in Tables 2, 3, or 4, do the necessaryuploads as follows:

(a) Push the small FMS knob to stop the cursor.

(b) Turn the small FMS knob to scroll to a different page and then back to the SYSTEMUPLOAD page.

(c) Push the small FMS knob on the PFD to start the cursor.

(d) Turn the small FMS knob to highlight the applicable airplane model and push the ENT key.

(e) Turn the small FMS knob to expand the FILE pull down menu field and highlight one ofthe Cessna Nav III software uploads that is applicable for your airplane.

(f) Push the ENT key.

(g) Push the LOAD soft key to install the software.

SB07-34-02 July 23, 2007

(h) Monitor the upload status. When the Upload Complete message is shown, push theENT key to select OK.

(i) If a software or configuration upload shows a failure, the software upload process willstop, and you must do the software upload procedure again. Do Steps 4C(10)g thru4C(10)i again as necessary up to a total of five times until you successfully completethe configuration upload. If after five times the software configuration fails, correct thehardware failure and start the configuration upload again.

(j) Do Steps 4C(10)(a) thru 4C(10)(i) again until all applicable software uploads are complete.

(11) Push the small FMS knob to stop the cursor.

(12) Disengage the PFD (ESS BUS and AVN BUS 1), MFD (AVN BUS 2) circuit breakers.

(13) Remove the SD Card from the PFD.

(14) Put the SD Card into the MFD upper card slot.

(15) Engage the MFD (AVN BUS 2) circuit breaker for power to the MFD.

(16) Push the NO soft key to stop the upload of the GDU system when this message shows:

DO YOU WANT TO UPDATE SYSTEM FILES?


(17) Push the YES soft key when this message shows:

DO YOU WANT TO UPDATE THE SPLASH SCREEN?


(18) Push any soft key when this message shows:

PRESS ANY KEY TO CONTINUE.

CONTINUING IN 10 SECONDS.

(19) With power still applied to the MFD, remove the SD Card from the MFD upper card slot andput it into the PFD upper card slot.

(20) Engage the PFD (ESS BUS and AVN BUS1) circuit breakers.

(21) Do Steps 4C(16) thru 4C(18) again for the PFD.

(22) Remove the SD Card from the upper PFD slot.

D. Do the aircraft registration number configuration:

(1) Disengage the PFD (ESS BUS and AVN BUS 1) and the MFD (AVN BUS 2) circuit breakers.

(2) Push and hold the ENT key on the PFD and engage the PFD (ESS BUS and AVN BUS 1)circuit breakers.

(3) Release the ENT key when the message INITIALIZING SYSTEM shows on the PFD.

(4) Push and hold the ENT key on the MFD and engage the MFD (AVN BUS 2) circuit breaker.

(5) Release the ENT key when the message INITIALIZING SYSTEM shows on the MFD.

(6) On the PFD, turn the large FMS knob to go to the GTX group. Turn the small FMS knob to goto the TRANSPONDER CONFIGURATION page.

(7) Look at the SET and ACTIVE columns in the configuration field to make sure that theADDRESS TYPE is US TAIL or HEX ID, whichever is applicable.

SB07-34-02July 23, 2007

(8) Make sure that the aircraft registration ADDRESS field has the correct tail number orhexadecimal number shown.

(a) If the tail number or hexadecimal number is correct, go to Step 4E.

(b) If the tail 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 largeFMS 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 registrationnumber or hexadecimal number.

5 Look for the message CONFIGURING XPDR #1 ...WAITING... to show.

6 After you see the XPDR #1 CONFIGURED COMPLETE message, push the ENTkey to select OK.

7 Make sure that the FLIGHT ID is correct. If the FLIGHT ID is not correct, do Steps4D(8)(b)1 thru 4D(8)(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 togo to the SYSTEM CONFIGURATION page.

(2) In the OTHER LRUS PRESENT field, find the GDL69. On airplanes equipped with GDL69 theGDL69 box in the OTHER LRUS PRESENT field must be green. On airplanes not equippedwith 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 4F.

(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 OTHERLRUS PRESENT field.

2 Push the ENT key to change the color of the box to the correct color for yourairplane (green for airplanes equipped with GDL69 and black for airplanes notequipped with GDL69).


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 goto 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 GUARDIANin all of the columns.

(a) If the CHNL 4 box is green and shows CO GUARDIAN in all of the columns, push thesmall FMS knob to stop the cursor and go to Step 4G.

(b) If the CHNL 4 box is not green or does not show CO GUARDIAN in all of the columns,do as follows:

1 Disengage the PFD (ESS BUS and AVN BUS 1) circuit breakers.

SB07-34-02 July 23, 2007

2 Put the SD Card in the upper PFD slot.

3 Push and hold the ENT key on the PFD and engage the PFD (ESS BUS and AVNBUS 1) circuit breakers.

4 Release the ENT key when the message INITIALIZING SYSTEM shows on the PFD.

5 When the message UPDATE SYSTEM FILES shows on the PFD, push the NO key.

6 On the PFD, turn the large FMS knob to go to the SYSTEM group. Then turn thesmall FMS knob to go to the SYSTEM UPLOAD page.

7 Do Steps 4C(10)(a) thru 4C(10)(i) again to upload the Cessna NAV III CO GuardianInstallation Option.

8 Remove the SD Card from the upper slot of the PFD.

9 Do Step 4F again.


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 togo 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.

5. Install the obstacle/terrain data SD Card in the bottom slots of the PFD and MFD units that were removedin Step 4.B.(2).

6. Do the software and system verification procedures that follow:

A. Do the software and status verification:

(1) With the large and the small FMS knobs, go to the SYSTEM group SYSTEM STATUS page onthe PFD.

(2) Make sure that the MFD1 and the PFD1 in the GDUS ONLINE field have green boxes.

(a) If the MFD1 and the PFD1 in the GDUS ONLINE field have green boxes, go to Step 6A(3).

(b) If the MFD1 and the PFD1 in the GDUS ONLINE field do not have green boxes, doas follows:

1 Do a check of the power.

2 Make sure that the PFD and the MFD screens are in the configuration mode.

3 Do troubleshooting as necessary.

(3) Make sure that the GIA1 and the GIA2 in the GIAS ONLINE field have green boxes.

(a) If the GIA1 and the GIA2 in the GIAS ONLINE field have green boxes, go to Step 6A(4).

(b) If the GIA1 and the GIA2 in the GIAS ONLINE field do not have green boxes, do asfollows:



SB07-34-02July 23, 2007

(4) (For airplanes equipped with GDL69) Make sure that the GDL69 in the OTHER LRUS ONLINEfield has a green box.

NOTE: For airplanes not equipped with GDL69, the GDL69 in the OTHER LRUS ONLINEfield has a black box.

(a) If the GDL69 in the OTHER LRUS ONLINE field has a green box, go to Step 6A(5).

(b) If the GDL69 in the OTHER LRUS ONLINE field does not have a green box, do as follows:



(5) Push the small FMS knob to start the cursor.

(6) Turn the small FMS knob to scroll through to the LRU window.

(7) Refer to Tables 5, 6, or 7. Scroll through each item in the LRU field to do a check of the columninformation to make sure that it is correct.

NOTE: If any LRU software versions or status modes do not match those shown in Tables 5,6, and 7, then the system has not loaded correctly. Load the software again to correctthe system version and status modes as necessary. If the software fails to load afterfive attempts, contact Cessna Propeller Aircraft Product Support.


EQUIPMENT VERSION STATUS

CO GUARDIAN (if installed) OK

COM1 (GIA-63 only) 7.00 OK


COM1 (GIA-63W only) 7.00 OK


GDC1 3.01 OK

GDC1 FPGA 01.05 UNKNOWN

GDL69 (If installed) 3.10.00 OK

GEA1 2.07 OK

GIA1 (GIA-63 only) 5.31 OK


GIA1 AUDIO 2.02 UNKNOWN

GIA1 (GIA-63W only) 5.31 OK



GMA1 3.03 OK

GMU1 2.01 OK

GMU1 FPGA 2.00 UNKNOWN

GPS1 (GIA-63 only) 3.03 OK


GPS1 (GIA-63W only) 2.4 OK

SB07-34-02 July 23, 2007



GRS1 2.09 OK

GRS1 FPGA 02.00 UNKNOWN

GRS1 MV DB 2005.00 UNKNOWN

GS1 (GIA-63 only) 3.00 OK


GS1 (GIA-63W only) 4.00 OK


GTX1 4.06 OK

MFD1 8.02 OK

MFD1 FPGA 1.03 UNKNOWN

NAV1 (GIA-63 only) 4.01 or Later OK


NAV1 (GIA-63W only) 5.01 or Later OK


PFD1 8.02 OK

PFD1 FPGA 1.03 UNKNOWN








GDC1 3.01 OK



GEA1 2.07 OK

*GFC CERT GIA1 2.02 UNKNOWN


*GFC CERT P C 2.02 UNKNOWN

*GFC CERT P M 2.02 UNKNOWN

*GFC CERT PT C 2.02 UNKNOWN

*GFC CERT PT M 2.02 UNKNOWN

*GFC CERT R C 2.02 UNKNOWN

SB07-34-02July 23, 2007


*GFC CERT R M 2.02 UNKNOWN







GMA1 3.03 OK

GMU1 2.01 OK






GRS1 2.09 OK







*GSA PIT MON 2.10 OK

*GSA PIT CTL 2.10 OK

*GSA TRM M 2.10 OK

*GSA TRM C 2.10 OK

*GSA ROLL M 2.10 OK

*GSA ROLL C 2.10 OK

GTX1 4.06 OK

MFD1 8.02 OK






PFD1 8.02 OK


SB07-34-02 July 23, 2007


WX - 500 1.03 OK

*Only 2007 model airplanes with the GFC-700 option have this installed








GDC1 3.01 OK



GEA1 2.07 OK



*GFC CERT P C 2.01 UNKNOWN

*GFC CERT P M 2.01 UNKNOWN

*GFC CERT PT C 2.01 UNKNOWN

*GFC CERT PT M 2.01 UNKNOWN

*GFC CERT R C 2.01 UNKNOWN

*GFC CERT R M 2.01 UNKNOWN







GMA1 3.03 OK

GMU1 2.01 OK






GRS1 2.09 OK

SB07-34-02July 23, 2007








*GSA PIT MON 2.10 OK

*GSA PIT CTL 2.10 OK

*GSA TRM M 2.10 OK

*GSA TRM C 2.10 OK

*GSA ROLL M 2.10 OK

*GSA ROLL C 2.10 OK

GTX1 4.06 OK

MFD1 8.02 OK






PFD1 8.02 OK


WX - 500 1.03 OK

*Only 2007 model airplanes with the GFC-700 option have this installed

(8) Push the small FMS knob to stop the cursor.

B. 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 togo to the MANIFEST CONFIGURATION page.

(2) (Refer to Table 1.) Make sure that the information shown in Table 1 is shown in the SYSTEMfield window.

(3) Make sure that the information shown in Table 8 is shown in the MANIFEST field window.

NOTE: This data file is near the bottom of the list.

TABLE 8.

Data File File Version

006-D0579-03 4.03

SB07-34-02 July 23, 2007

(4) (For airplanes equipped with GFC700 Autopilot) Make sure that the information shown in Table9 is shown in the MANIFEST field window.

NOTE: This data file is near the bottom of the list.

TABLE 9.

Model Data File File Version

182T/T182T 006-D0270-12 2.02

206H/T206H 006-D0621-11 2.01

(5) Make sure that the MFD (AVN BUS 2) and the PFD (ESS BUS and AVN BUS 1) circuitbreakers are engaged.

(6) Turn the AVIONICS and BAT MASTER switches to the off position.

(7) (For airplanes equipped with TAWS B) Do the Enablement of Garmin G1000 Terrain AwarenessWarning System Class-B (TAWS-B), SB06-34-03 Revision 1 or later.

(8) (For airplanes equipped with ChartView) Do the Garmin G1000 Nav III Avionics ChartViewOption, SB07-34-01 Revision 1 or later.

7. Make sure no failures or alerts are shown:

A. Turn the AVIONICS and BAT MASTER switches to the ON position.

B. Make sure that there are no database, software, hardware failures or alerts shown on the PFD orthe MFD.

C. If there is one or more failure or alert shown on the PFD or the MFD, refer to the Garmin G1000 NAVIII Line Maintenance Manual, Part Number 190-00352-00, Revision H (or latest revision).

D. Turn the AVIONICS and BAT MASTER switches to the off position.

8. Make an entry in the airplane logbook that states compliance and method of compliance with thisService Bulletin.

OWNER NOTIFICATION

On July 23, 2007 the following message will be sent to applicable owners of record in SB07-34-02A.

Dear Cessna Owner:

This Owner Advisory is to inform you of a software upgrade for the Garmin G1000 System as announced inService Bulletin SB07-34-02: Garmin G1000 System Software Upgrade to Version 563.03. The softwareupgrade includes the following changes:

Garmin Aerial Navigation Product Alert - Service Alert 070227-00 Resolution: Cessna Service BulletinSB07-25-03, Garmin G1000 Arrival and Departure Procedures Software Alert, transmitted Garmin’s ServiceAlert. These documents communicated the requirement to remove the active arrival or departure procedureprior to loading a new arrival or departure procedure. Compliance with this Service Bulletin (SB07-34-02) byloading software version 563.03 will no longer require the manual method to remove the active arrival ordeparture procedure as described above. Compliance with Garmin Service Bulletin No.: 0708 Revision A,AFM/AFMS Limitation for G1000 Systems, is not required as software version 563.03 includes the 8.02software for the PFD/MFD units.

Garmin GDL-69A XM® Radio/Weather System: Reference Cessna Service Newsletter SNL07-1/GarminService Advisory NO.: 0613 concerning the storm cell tracking limitation. The greater than 400 storm cells issueis resolved with this software upgrade. Enhancements are also provided for the pilot’s interface with the system.

Reversionary Mode Timing: Displays enter reversionary mode automatically and require 5 seconds of normaloperation before returning to normal display mode to prevent possible reversionary mode cycling events(change affects both automatic and manual reversionary mode).

Reversionary Mode Inset Map: Added functionality to the PFD/MFD reversionary mode to show the InsetMap if selected.

SB07-34-02July 23, 2007

Barometric Altitude Minimum: Enable aural alert for this function.

Alternate Transponder Code Entry Procedure: Provides the pilot with another way to enter transpondercodes by using the FMS knob in addition to the existing softkey code method.

VHF COM Transmit Indications: Enabled RX and SQ indicators to be visible in the same location as the TXindicator when the specific VHF COM is either transmitting “TX”, receiving with automatic squelch active “RX”or when manual squelch is open “SQ”.

Track Vector: Added the ability to adjust the look ahead time for the track vector.

Victor Airways: Added Victor Airways to the flight plan capability.

TAWS-B System: Changes incorporated to reduce nuisance alerts. Added an “INHIBIT” softkey when on theTAWS Map Page for inhibiting TAWS-B aural alerts. Refer to SB06-34-03 Revision 1 (or latest revision).

MFD Splash Screen For Aviation Database Status: Refined the display format of the aviation databasename, version, and effective dates. This also affects the display format for Land, Obstacle, Terrain, SafeTaxi,FliteCharts and Jeppesen ChartView databases if installed.

Auto-Acknowledge Aural Alert: Configuration changes to ensure aural alerts are provided at systempower-on.

Fuel Calibration: Revised the Fuel Calibration Page in the G1000 Configuration Mode.

The following changes were incorporated on model year 2007 Nav III airplanes and are provided as newchanges to all Nav III equipped airplanes that are in compliance with Service Bulletin SB06-34-02 orSB06-34-02 Revision 1: Garmin G1000 System Software Update:

Jeppesen ChartView: Added support for the optional installation of the Jeppesen electronic terminalprocedures charts known as ChartView. Refer to SB07-34-01 Revision 1 (or latest revision).

Garmin SafeTaxi & FliteCharts: Added support for Garmin SafeTaxi and FliteChart electronic chart products.Refer to SB07-34-04 (or latest revision).

XM Radio Interface: Added the ability for inner and outer FMS knobs to input the channel number on theXM radio page. Added provisions for indicating on the XM radio page if the GDL 69 unit fails. Added mappanning capability of altitude information for cloud tops on the weather datalink page and text instructions forthe LOCK softkey on the XM information page. The XM activation page will now dynamically update thepresence of the radio softkey based upon whether the XM radio signal is present or not. The XM signalstrength status indicator has been added to aid in diagnostics. Added age information in all the maps thatcould depict the data link weather.

Current Track Bug: Feature added to display the airplane's current track on the HSI.

Wind Data Window: Includes an additional wind data window to provide various formats of wind magnitude,direction, crosswind and headwind components.

Vertical Navigation: Added support for assigning altitude constraints with vertical waypoints to give verticalnavigation guidance.

Barometric Altitude Minimum: New functionality added for setting a minimum descent altitude.

Transponder GND Softkey: Added a transponder GND softkey to allow manual selection of Ground Mode.

Traffic Information Service (TIS): Enhanced TIS functionality by disabling TIS on the ground to avoidnuisance alerts, and allow muting of the TIS Not Available (TNA) alert by use of a new TNA MUTE softkey.

Temporary Flight Restrictions (TFR) Display: Enhanced highlighting of waypoints beneath some TFR'sand TFR highlighting while using the map pointer.

ADF Superflag: Added support for the ADF relative bearing pointer display to be shown when an ADFSuperflag signal is sensed and removal of bearing pointer when signal is low.

Software & Configuration Loading: Enhanced and simplified the software loading procedures.

LRU Port Info: Added increased diagnostic support in configuration mode to allow quicker verification ofoperating or failed data paths.

ARINC 424 Database Leg Types: Added support for these procedures to be displayed on the MFD.

SB07-34-02 July 23, 2007

Compliance is mandatory: shall be accomplished within the next 100 hours of operation or 12 months,whichever occurs first.

NOTE: Existing Garmin Software Backup CDs should be destroyed and discarded to eliminate the possibilityof reloading the incorrect software at a later date.

NOTE: For airplanes affected by Cessna Service Bulletin SB06-34-02 or SB06-34-02 Revision 1 (GarminG1000 System Software Upgrade): SB06-34-02 Revision 1 if not already accomplished must beaccomplished prior to compliance with this service bulletin.

The information contained in the referenced Cessna Service Bulletin shall be considered an amendment tothe Cessna Manufacturer’s Maintenance Manual or Instructions for continued airworthiness, and should beaccomplished for ongoing airworthiness compliance as required per CFR Part 43.13.

A labor allowance credit of 1.6 man-hours per airplane will be provided to load the software upgrade.

1. If necessary, 0.1 man-hour for each one of the applicable configuration uploads for airplanes equippedwith the following: CO Guardian, Honeywell Traffic Advisory System (TAS), Honeywell AutomaticDirection Finder (ADF), Honeywell Distance Measuring Equipment (DME), or Artex C406-N EmergencyLocator Transmitter (ELT)

2. If necessary, 0.3 man-hour to do the applicable configuration upload for airplanes equipped with theGarmin Terrain Awareness Warning System (TAWS-B)

3. If necessary, 0.4 man-hour to do the applicable configuration upload for airplanes equipped with theGarmin G1000 ChartView System

To receive credit, the work must be completed and a Warranty Claim submitted by a Cessna Single EngineService Station within 30 calendar days of Service Bulletin compliance before the credit expiration datesshown below.

Domestic . . . . . . . . . . . . . . . . . . . . . . July 23, 2008International . . . . . . . . . . . . . . . . . . . . July 23, 2008

The Garmin G1000 Cockpit Reference Guide for Cessna NAV III, Part Number 190-00384-07 Rev. A and theapplicable airplane model Cessna Garmin NAV III Installation Software CD are enclosed. The Cessna ServiceStation will need to utilize the enclosed CD when accomplishing this software upgrade on your airplane. Whennot 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 toDuplicate Owner Advisory addresses, it will only be sent to the address as registered with the FAA.

Please contact a Cessna Single Engine Service Station for detailed information and arrange to have CessnaService Bulletin SB07-34-02 accomplished on your airplane.

* * * * * * *

SB07-34-02July 23, 2007

print preview - c:docume~1e3userlocals~1tempe3temp 3904

Documents