single engine - cessna

Single Engine

Service Bulletin

of 29

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 accomplishingthe 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

January 18, 2010 SB10-34-01

TITLE

GARMIN G1000 SYSTEM SOFTWARE UPGRADE TO GDU 9.05, VERSION 534.13

EFFECTIVITY

The following airplanes equipped with the Garmin G1000 avionics system:

Model Serial Numbers

350 (LC42-550FG) 42502 thru 42569, 421001 thru 421020.

400 (LC41-550FG) 41034, 41563 thru 41650, 41652 thru 41800, 411001 thru 411153.

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

! Flight Plan selection/transition enhancements

! TAWS system enhancements

! Single Cue aircraft representation symbol update

! More precise standard BARO

! The ability to select traffic only display on map inset

! Canadian XM weather support

! Display of airport “hot spots” from the SafeTaxi database

! TAWS flight phase logic upgrades for operation in airspace with multiple airports

! Flight Charts database cycle checking enhancements

! Automatic Flight Control System (AFCS) enhancements

! Updates horizon display for consistency with other Cessna models (disabled gradient horizon)

! Increases alternator out alert trigger threshold to avoid nuisance alerts during ground operation

! Provides resolution for the GPS/WAAS issue that involves a potential reset of the GPS/WAAS receiver

when operating in specific northern latitudes and Alaska, along with other updates

COPYRIGHT"2010

! Ensures communication is re-established between the CO Guardian and G1000 system in the event

of a data interruption

! Provides system readiness capability for the Garmin Synthetic Vision Technology (SVT) feature. The

enablement of SVT can be accomplished with Service Bulletin SB10-34-02

! Supports the capability of an Electronic Pilot’s Checklist

! Enhancement to allow simultaneous display of TOPO and NEXRAD on maps

! Incorporation of Garmin Service Alerts 0811 and 0816

! Incorporation of Garmin Service Advisories 0745, 0831, 0838, and 0908

DESCRIPTION

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

COMPLIANCE

Recommended: should be accomplished at the next 100 hour or 12 month (annual) inspection, whichever occurs first.

NOTE: Cessna Service Bulletin SB08-34-05: G1000 System Software Upgrade to GDU 8.10 Version 534.09 must be accomplished prior to installing the software described in this Service Bulletin on the following serial numbers only:

A. Airplane Model 350 (LC42-550FG) Serial Numbers 42502 thru 42569, 421001 thru 421010.

B. Airplane Model 400 (LC41-550FG) Serial Numbers 41034, 41563 thru 41650, 41652 thru 41800, 411001 thru 411061.

C. Prior accomplishment of Cessna Service Bulletin SB08-34-05 is not required for the following airplane serial numbers:

(1) Airplane Model 350 (LC42-550FG) Serial Numbers 421011 through 421020.


NOTE: Existing Garmin software backup CD’s shall be destroyed and discarded to help eliminate the possibility of loading the incorrect software at a later date.

APPROVAL

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

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MANPOWER

2.1 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:

! Ryan 9900BX / TAS 620 Traffic Systems! Oxygen ! Becker 3502 Automatic Direction Finder (ADF) ! Honeywell KN63 Distance Measuring Equipment (DME)! Fuel Tank option

If necessary, 0.2 man-hour to do the applicable configuration upload for airplanes equipped with the Garmin G1000 Terrain Awareness System (TAWS-B).

If necessary, 0.3 man-hour to do the applicable configuration upload for airplanes equipped with the Garmin G1000 ChartView System.

REFERENCES

Model 350 Airplane Maintenance Manual.

Model 400 Airplane Maintenance Manual.

Garmin G1000 Cockpit Reference Guide for Cessna 350/400, Part Number 190-00567-03 Rev A (or latest revision)

Garmin G1000 Pilots Guide for Cessna 350/400, Part Number 190-00552-03 Rev A (or latest revision)

The following documents can be viewed by Cessna Service Stations by going to www.garmin.com:

! Garmin G1000 System Maintenance Manual, Cessna 350/400, Part Number 190-00577-03Rev E (or latest revision)

! Garmin G1000 System Installation Manual, Part Number 190-00303-00, Revision G

! 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)

NOTE: Make sure all publications used are complete and current. Refer to CessnaSupport.com

This information shall be considered an amendment to the Cessna Manufacturer's Service / Maintenance Manual and should be accomplished within the specified time requirement.

SB10-34-01 of 29 January 18, 2010

OTHER PUBLICATIONS AFFECTED

Model 350 and 400 Illustrated Parts Catalogs

NOTE: Make sure all publications used are complete and current. Refer to CessnaSupport.com

MATERIAL PRICE AND AVAILABILITY

Part Number Description Qty/Airplane Price

Required Materials

The applicable Garmin Installation Software CD listed below has been provided to the airplane owner in Owner Advisory SB10-34-01A at no charge.

350GSW00-02 Model 350 Cessna Garmin Installation Software CD

1 N/C

400GSW00-02 Model 400 Cessna Garmin Installation Software CD

1 N/C

The part below should be obtained by completing and returning the attached Model 350/400 G1000 System Software Upgrade Garmin Cockpit Reference Guide (CRG) Order Form

190-00567-03 Rev A (or later revision)

Garmin G1000 Cockpit Reference Guide For Cessna 350/400

1 N/C

If necessary, the parts below are available from Cessna Customer Service at Phone: 316-517-5800or Fax: 316-517-7271.

RB050005-I(or later revision)

Model 350 Pilot’s Operating Handbook (POH) Incorporating Revision I

1 (if necessary) $370.00

RC050005-I(or later revision)

Model 400 Pilot’s Operating Handbook(POH) incorporating Revision I

1 (if necessary) $370.00

Optional Materials

190-00552-03 Rev 1 Garmin G1000 Pilots Guide for Cessna 350/400

1 (if desired) $595.00

ALL PRICES SUBJECT TO CHANGE WITHOUT NOTICE

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CREDIT INFORMATION

For airplanes in warranty:

A labor allowance credit of 2.1 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 for each one of the following applicable configuration uploads:

! Ryan 9900BX / TAS 620 Traffic Systems! Oxygen ! Becker 3502 Automatic Direction Finder (ADF), ! Honeywell KN63 Distance Measuring Equipment (DME) ! Fuel Tank option

If necessary, a labor allowance credit of 0.2 man-hour will be provided to do the applicable configuration upload for airplanes equipped with the Garmin Terrain Awareness Warning System (TAWS-B).

If necessary, a labor allowance credit of 0.3 man-hour will be provided to do the applicable configuration upload for airplanes equipped with the Garmin G1000 ChartView option.

Freight will be credited at the most economical method unless pre-approved by Cessna. For pre-approval contact Cessna Parts Distribution Warranty Administration at Telephone: 316-831-4296, Fax: 316-206-2746 or E-mail: [email protected].

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………………………… January 18, 2011 International……………………... January 18, 2011

Special Note to Service Stations:

When you complete the Warranty Claim, the labor allowance claimed shall be itemized for each above action completed.

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ACCOMPLISHMENT INSTRUCTIONS

Weight and Balance Information Negligible

Material Information

To complete this Service Bulletin, use the parts below as applicable.

NEW P/N QUANTITY DESCRIPTION OLD P/N DISPOSITION

Required Materials 350GSW00-02 1 Model 350 Cessna

Garmin Installation Software CD

010-00545-01010-00545-02010-00535-08010-00534-09350GSW00-00350GSW00-01

Destroy and Discard

400GSW00-02 1 Model 400 Cessna Garmin Installation Software CD

010-00530-02010-00530-03010-00530-05010-00530-06010-00534-08010-00534-09400GSW00-00400GSW00-01

Destroy and Discard

190-00567-03Rev A (or later revision)

1 Garmin G1000 Cockpit Reference Guide for Cessna 350/400

190-00567-01 Rev B 190-00567-01 Rev A 190-00567-00 Rev A, B 190-00567-02

Destroy and Discard

In addition to the parts above, the following parts may be necessary:

RB050005-I(or later revision)

1 Model 350 Pilot’s Operating Handbook(POH) Incorporating Revision I.

RB050005 Rev G (and all previous)

Destroy and Discard

RC050005-I(or later revision)

1 Model 400 Pilot’s Operating HandbookRevision (POH) Incorporating Revision I.

RC050005 Rev H (and all previous)

Destroy and Discard

Optional Materials 190-00552-03Rev 1

1 Garmin G1000 Pilots Guide for Cessna 350/400 (optional)

190-00552-01 Rev A 190-00552-01 Rev A-C 190-00552-02 Rev A

May be ordered from Cessna Customer Service

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The equipment below, or equivalent, will be necessary.

NAME QUANTITY MANUFACTURER USE

PC Computer (NOTE 1) 1 Commercially

Available

To transfer software files from the CD-Rom to the SD card.

SD Card Reader 1 CommerciallyAvailable

To transfer software files from the CD-Rom to the SD card.

SD Card, 128 MB (NOTE 2) 1 SanDisk, STEC, or

ToshibaTo transfer software files to the Garmin G1000 system.

NOTE 1: The PC Computer used should have Windows XP SP2 (or later operating system) installed.

NOTE 2: Only use a SanDisk, Toshiba, or STEC manufacturer SD Card.

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.

NOTE: 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 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.

NOTE: For airplane serial numbers 42502 – 42569, 421001 – 421010, 41034, 41563 – 41650, 41652 – 41800, 411001 – 411061, Cessna Service Bulletin SB08-34-05 (latest revision): G1000 System Software Upgrade to GDU 8.10 Version 534.09 must be accomplished prior to installing the software described in this Service Bulletin.

NOTE: G1000 System Screen Shots are provided throughout this document as a reference only, as certain details may or may not reflect what you see on the PFD/MFD.

1. Do the software and paper documentation:

A. Remove, destroy, and discard the old Cessna Garmin 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 Garmin Installation Software CD to load the new software.

B. Remove the old Garmin G1000 Cockpit Reference Guide for Cessna 350/400 and replace it with the Garmin G1000 Cockpit Reference Guide for Cessna 350/400, Part Number190-00567-03 Rev A (or latest revision).

C. The applicable airplane model Cessna Garmin 350/400 Installation Software CD was sent to the airplane owner with Owner Advisory SB10-34-01A. You must use the new CD when you do the software upgrade on the airplane. When not in use, the CD should be stored in the Pilot's Operating Handbook sleeve for the Garmin Software.

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D. Check the part number and revision level of the currently installed Pilot’s Operating Handbook in the airplane. If the current POH version is at or above the revision levels listed below, then no further action is required.

Model 350 (LC42): RB050005-I (Complete POH incorporating Revision I) Model 400 (LC41): RC050005-I (Complete POH incorporating Revision I)

If the installed POH revision level does not meet the minimum required revision level listed above, contact Cessna Customer Service at telephone 316-517-5800 or FAX 316-517-7271, to order a new updated Pilot’s Operating Handbook.

2. Determine the following information and record in TABLE 1, as follows:

A. Locate and record the Airplane Serial Number in TABLE 1.

B. Do an identification of WAAS installation as follows

(1) Connect a 28-volt ground power unit to the airplane.

(2) Disengage the MFD (Avionics Bus) circuit breaker.

(3) Put the LEFT and RIGHT BATTERY MASTER switches to the ON position. (Overhead console)

(4) Turn on the CROSSTIE switch, and the AVIONICS MASTER switch. (Overhead console).

(5) Push and hold the ENT key on the Multi-Function Display (MFD) and engage the MFD (AVN BUS 2) circuit breaker.

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

(7) If necessary, use the FMS knob, go to the system group SYSTEM STATUS page on the MFD.

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

(9) Turn the small FMS knob to highlight GIA1 in the LRU field.

(10)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.

(11)Record which system is installed (GIA63W or GIA63) in TABLE 1.

(12)Disengage the PFD (Essential Bus) and MFD (Avionics Bus) circuit breakers that are located on the lower side panel, forward of the pilot’s seat.

(13)Wait a minimum of 15 seconds before going to the next step to allow the system to fully shut down.

C. Locate and record the Airframe System I.D. in TABLE 1 as follows:

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(1) Engage the PFD (Essential Bus) and MFD (Avionics Bus) and make sure that all of the necessary circuit breakers are engaged, and allow normal mode startup of the Garmin G1000 System.

(2) Push the ENT key when the splash screen is displayed.

(3) Turn the large FMS knob on the Multi-Function Display (MFD) to the AUX group page.

(4) Turn the small FMS knob on the FMS to go to the AUX-SYSTEM STATUS page.

(5) On the AUX-SYSTEM STATUS page, locate the AIRFRAME field in the upper right corner of the page and record the SYSTEM I.D. in TABLE 1.

D. Determine and record the System Software Version in TABLE 1 as follows:

(1) On the AUX-SYSTEM STATUS page, locate the AIRFRAME field in the upper right corner of the page and record the SYSTEM SOFTWARE VERSION in TABLE 1.

(2) If the software version is 0534.09 or later, go to step 2E. If software is not 0534.09 or later, perform latest revision of Service Bulletin SB08-34-05: G1000 System Software Upgrade to GDU 8.10 Version 534.09 and then go to step 2E.

E. Determine if Terrain Awareness Warning System – Class B (TAWS-B) is installed in the airplane and record in TABLE 1 as follows:

(1) Turn the large FMS knob on the MFD to go to the MAP group page.

(2) Turn the small FMS knob to go to the MAP-TAWS or MAP-TERRAIN PROXIMITY page.

(3) If the MAP page is MAP-TERRAIN PROXIMITY, then the airplane does NOT have TAWS-B installed. If the MAP page is MAP-TAWS, then the airplane DOES have TAWS-B installed. Record the information in TABLE 1.

NOTE: If the airplane has TAWS-B installed, the 010-00330-51 TAWS-B Enablement SD Card will be located in the blue Aircraft Software sheet in the back of the Pilot’s Operating Handbook (POH). The SD Card may also be found in an envelope inside the front cover of the Avionics section of the airplane logbook, with a logbook entry indicating that TAWS-B is installed in the airplane.

(4) Keep power on the airplane.

TABLE 1

Airplane Serial Number

Airframe System I.D.

System Software Version

Wide Area Augmentation System (WAAS) Yes No

TAWS-B Enable Card,P/N 010-00330-51 option installed

Yes No

3. Verify the Line Replacement Units (LRU) status as follows:

A. With the system power on, turn the large FMS knob on the MFD to go to the AUX group page.

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B. Turn the small FMS knob on the MFD to go to the AUX-SYSTEM STATUS page.

C. Push the small FMS knob to activate the cursor in the LRU INFO field.

D. Scroll down and verify that there is a green check in the STATUS column for each LRU item. If any of the LRU items shows a red X in the STATUS column, you must first correct the cause of the red X condition before continuing with this Service Bulletin.

E. Disengage the circuit breakers labeled PFD and MFD.

F. Put the AVIONICS MASTER switch and the CROSSTIE switch to the OFF position.

G. Put the LEFT and RIGHT BATTERY MASTER switches to the OFF position.

4. Remove and keep the 010-00330-42 (or later) GDU Supplemental Database SD Cards from the lower SD card slots in the PFD and MFD. Label each card “PFD” or “MFD” as appropriate and store them in a safe place for later installation.

5. Load the G1000 system software, using the applicable Cessna Aircraft Company – Garmin Installation Software CD-ROM, 400GSW00-02 (for model 400 airplanes) or 350GSW00-02 (for model 350 airplanes), as follows:

A. Transfer software from the Installation Software CD-ROM to a SD card as follows:

(1) Insert the Cessna Aircraft Company – Garmin Installation Software CD into the CD-ROM Drive of your computer.

(2) Right mouse click on the START button on the lower left hand corner of the computer screen and click on EXPLORE.

(3) Locate the CD drive on the computer and double click it to open the CD File.

(4) Double click on the file 006-B0534-13 on the CD.

(5) When the window opens, click the SETUP button.

(6) The installation help wizard will appear. Click the NEXT button.

(7) Install a blank SD card in the SD card reader.

NOTE: The SD card must be 128 MB or larger capacity. Garmin requires the use of SanDisk, STEC, or Toshiba brand SD cards. The use of other SD cards is not allowed.

(8) The next window will ask for your SD card reader location. Click the drive location of the SD card reader. Click the NEXT button.

(9) The next window warns you that all information on the SD card will be erased. Click NEXT.

(10) The data will start to transfer to the SD card.

(11) When the data has been transferred to the SD card, click the FINISH button.

(12) Remove the SD card from the SD card reader.

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(13) Remove the Cessna Aircraft Company Garmin Software Installation Software CD-ROM (400GSW00-02 or 350GSW00-02) from the CD Rom drive of the computer and put it in the protective CD sleeve in the Pilot’s Operating Handbook (POH).

B. Put the G1000 into configuration mode and update the system files as follows:

(1) If not previously done, disengage the following circuit breakers: PFD (Essential Bus), MFD (Avionics Bus).

(2) If not previously done, connect a 28-volt ground power unit to the external power receptacle and turn on the ground power unit.

(3) Put the LEFT and RIGHT BATTERY MASTER switches to the ON position. (Overhead console)

(4) Turn on the CROSSTIE switch, and the AVIONICS MASTER switch. (Overhead console)

(5) Insert the SD Card with the 006-B0534-13 software upgrade file installed on it into the Garmin GDU 1042 / 1044 MFD upper card slot.

(6) While holding the ENT key on the MFD, engage the MFD circuit breaker.

(7) When the words ‘INITIALIZATING SYSTEM’ appear in the upper left corner of the MFD, release the ENT key.

(8) When prompted, press the ENT key to update the system files.

NOTE: A soft key labeled ‘YES’ appears in the lower right corner of the MFD and may be used in lieu of the ENT key):

(9) When prompted to update the splash screen, press the YES softkey.

(10) The new system files update is completed when the MFD starts in configuration mode.

(11) With power still applied to the MFD, remove the SD Card from the MFD and insert it into the upper card slot on the PFD. Repeat Steps 5.B.(6) through 5.B.(9) for the PFD.

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(12) When the PFD load is complete, it starts in the configuration mode. Do not remove power from the PFD or MFD.

IMPORTANTFor the rest of the software/configuration procedure, do not operate the MFD while loading software or configuration files unless specifically instructed to do so. Perform all remaining operational steps on the PFD only. Otherwise, a failed or cancelled load may result.

C. Upload the Baseline System Software as follows:

(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 activate the cursor, and then turn the small FMS knob to expand the drop down menu, which highlights the airframe type in the AIRFRAME field. Select the appropriate airplane type (C400 or C350) and press the ENT key.

NOTE: Ensure that the correct airframe type is selected before proceeding; otherwise, incorrect configuration information will be loaded.

(3) Once an airframe type is selected the cursor moves to the FILE window. Turn the small FMS knob to expand the drop-down menu.

NOTE: Two baseline load options are available: WAAS Baseline and Non-WAAS Baseline.A baseline load is chosen based on whether the airplane is equipped for WAAS or Non-WAAS operation.

NOTE: Important. You will only be selecting the WAAS / Non-WAAS Baseline options at this stage. Do not select the fuel tank options until instructed to do so later.

CAUTION: MAKE SURE THAT YOU SELECT THE CORRECT FULL CONFIGURATION UPLOAD (WAAS OR NON-WAAS) THAT YOU RECORDED IN TABLE 1. 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.

(4) Use the FMS knob to scroll down and select the appropriate Baseline option from the FILE list in the Figure below. When the cursor is over top of the selection, press the ENT key.

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(5) After the Baseline FILE option is selected, the PRODUCT window will populate and display software and configuration file information for each G1000 LRU. The LRU VERS column shows the currently loaded software version in the LRU, the CARD VERS column shows the LRU software version stored on the SD Card. Each check designates a file to be loaded to the G1000.

(6) If an inequality exists between the LRU and CARD columns versions, the SOFTWARE and CONFIGURATION boxes will be pre-selected (checked). By default all of the CONFIGURATION boxes will be pre-selected.

NOTE: If the software for a particular LRU must be reloaded, without requiring a full software load, use the following keys to deselect the options to be loaded. Then select only the software that needs to be loaded for a specific LRU.

The following soft keys provide an easy way to select files: CHK ALL: Selects all files, both configuration and software

CHK SW: Selects all software files only.

CHK CFG: Selects all configuration files only.

CLR ALL: Clears all selections. (7) After verifying that the software and configuration files are checked, press the LOAD soft

key.

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NOTE: It is acceptable to simply load the pre-selected software and configuration files.

(8) Monitor the upload. When the “Upload Complete” message is shown, press the ENT key to select “OK”.

NOTE: This can take up to 60 minutes.

(9) Verify that each column indicates in green when the loading process has finished and inspect the SUMMARY window at the bottom of the screen as well to make sure that the load is successful.

(10) 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 5.C.(1) thru 5.C.(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.

D. Load the Fuel Tank Option File.

(1) Once a WAAS or Non-WAAS baseline file has been successfully loaded for a particular model airplane, an appropriate fuel option may need to be loaded per the instructions below.

(2) There are three FQIS (Fuel Quantity Indicating System) fuel tank options available: 49 Gallons Non-adjusted, 49 Gallons Adjusted, and 51 gallons. Only the 49 Gallons Adjusted should be selected, based on the directions in Table 2 below. Do not select the 49 Gallons Non-Adjusted option. Install the fuel option for the airplane as follows:

NOTE: The 51-Gallon option is configured by default. Additional software loads are only installed for the 49 Gallon Adjusted option.

(3) Look in the airplane maintenance records to determine if Service Letter SL-07-008 has been complied with.

49 Gallons Adjusted

If Service Letter SL-07-008 has been complied with, OR, if the airplane is in the serial number range below for 49 Gallons Adjusted:

Model 400 (LC41) serial numbers 41758-41799

Model 350 (LC42) serial numbers 42565-42567

51 Gallons

Model 400 (LC41) serial numbers 41800, 411001 and later

Model 350 (LC42) serial numbers 42568, 42569, 421001 and later

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(4) Based on the determination of airplane serial number and fuel tank option in step 5.D.(3) above, proceed in accordance with the loading instructions listed in TABLE 2.

NOTE: Do not attempt to reload the Baseline WAAS OR NON-WAAS file that was loaded in step 5.C.

TABLE 2

Airframe Adjusted 49 Gallon Tank Size

51 Gallon Tank Size

350 Non-WAAS No additional load required, proceed to Step 5.

This option is not supported for Non-WAAS. Proceed to Step 5.

350 WAAS Load Cessna 350 Adjusted 49 Gal Fuel Tank Option.

No additional load required, proceed to Step 5.

400 Non-WAAS No additional load required, proceed to Step 5.

This option is not supported for Non-WAAS. Proceed to Step 5.

400 WAAS Load Cessna 400 Adjusted 49 Gal Fuel Tank Option.

No additional load required, proceed to Step 5.

(5) If TABLE 2 requires no fuel tank load, go to Step 6. If TABLE 2 requires a fuel tank load, go to Step 5.D.(6).

NOTE: The technician must go back to the FILE field of the SYSTEM UPLOAD page for the following step. Do not attempt to reload the Baseline file that was loaded in Step 5.C.

(6) Turn the large FMS knob to highlight the FILE menu on the SYSTEM UPLOAD page.

(7) Turn the small FMS knob to expand the FILE pull down menu field and highlight the applicable Fuel Tank Option. Push the ENT key.

(8) The PRODUCT window will populate once the proper fuel tank option is loaded. By default, all of the CONFIGURATION boxes will be pre-selected.

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(9) After verifying that the fuel option configuration files are checked, press the LOAD soft key.

(10) The G1000 system automatically begins loading the configuration files to the selected LRUs in the proper order.

(11) Monitor the upload. When the “Upload Complete” message is shown, press the ENT key to select “OK”.

(12) Verify that each column indicates in green when the loading process has finished and inspect the SUMMARY window as well to ensure that the load is successful.

(13) If the Fuel Tank Configuration shows a failure, the upload process will stop, and you must do the configuration upload procedure again. Do Steps 5.D.(6) thru 5.D.(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.

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6. For airplanes equipped with the optional additional items shown in TABLE 3, do the necessary uploads as follows:

A. Turn the large FMS knob to highlight the AIRFRAME menu field on the SYSTEM UPLOAD page.

B. Turn the small FMS knob to expand the drop down menu in the AIRFRAME field.

C. Select ‘Options’ from the AIRFRAME field and press ENT.

TABLE 3Cessna Option: 9900BX / TAS 620 Traffic Systems Cessna Option: Oxygen Cessna Option: Honeywell KN63 DME Cessna Option: Becker 3502 ADF

NOTE: If the configuration for an optional system is inadvertently loaded for a system that isNOT installed, the baseline Cessna 350 or Cessna 400 configuration for GIA 2, GEA 1, GMA 1, and the Airframe file must be reloaded. Following this, the configuration for the optional systems may then be repeated.

D. (For airplanes equipped with the Becker AR 3502 ADF only). Configure the software for the Automatic Direction Finder as follows:

NOTE: If installed, an ADF system can be identified by the presence of a large antenna located on the bottom of the tail area of the airplane, below the baggage compartment, at approximately FS 202.0. The antenna is mounted with three screws.

(1) From the FILE field, select ‘Cessna Option – Becker 3502 ADF’ or “Cessna Option - KR87 ADF’ as applicable and press ENT.

(2) Press the LOAD soft key.

tus of the upload. When the upload is completed, press ENT to acknowledge.

(3) Monitor the sta

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(4) View the SUMMARY field and make sure that all items were successfully completed: Verify that PASS appears in green at the check box(es) as shown.

times until you successfully complete the configuration upload. If after five times the configuration fails, correct the hardware failure and start the

E. (For airplanes equipped with the Honeywell KN63 DME only). Configure the G1000 software for the H

f a 2-inch shark fin style Transponder/DME antenna located on the bottom of the airplane, aft and to the left of

(1) If the airplane is equipped with the Honeywell Model KN63 DME, follow this procedure to configure the G1000. If the airplane is not equipped with this option, go to step 6.F.

(2) urn the large FMS knob to highlight the FILE menu field on the SYSTEM UPLOAD

‘Cessna Option – KN63 DME’ and press ENT.

(6) Monitor the status of the upload. When the upload is completed, press ENT to acknowledge.

(5) If the ADF configuration upload shows a failure, the upload process will stop, and you must do the configuration upload procedure again. Do Steps 6.D.(1) thru 6.D.(4) again as necessary up to a total of five

configuration upload again.

oneywell KN 63 DME as follows:

NOTE: If installed, the DME system can be identified by the presence o

the Fuel System (Gascolator) access panel at approximately FS 111.0.

Tpage.

(3) Turn the small FMS knob to expand the drop down menu in the FILE field.

(4) From the FILE field, select


SB10-34-01 of 29 January 18, 2010

(7) View the SUMMARY field and make sure that all items were successfully completed. Verify that PASS appears in green at the check box(es) as shown.

load procedure again. Do Steps 6.E.(2) thru 6.E.(7) again as necessary up to a total of five times until you successfully complete the configuration

t the configuration upload again.

F. e Oxygen system as follows:

(1) the airplane being updated is a Model 400, follow this procedure to configure the 1000. If the airplane is a model 350, go to step 6.G.

PLOADpage.

e drop down menu in the FILE field.

the ‘Cessna Option – Oxygen Outlet Low Press (16.5 – 33 psi)’ in the FILE field and press ENT.

soft key.

(7) View the SUMMARY field and make sure that all items were successfully completed. Verify that PASS appears in green at the check box(es) as shown:

(8) If the DME configuration upload shows a failure, the upload process will stop, and you must do the configuration up

upload. If after five times the configuration fails, correct the hardware failure and star

(For all Model 400 airplanes only) Configure the software for th

IfG

(2) Turn the large FMS knob to highlight the FILE menu field on the SYSTEM U

(3) Turn the small FMS knob to expand th

(4) From the FILE field, select

(5) Press the LOAD

(6) Monitor the status of the upload. When the upload is completed, press ENT to acknowledge.

SB10-34-01 of 29 January 18, 2010

, and

il you successfully complete the configuration upload. If after five times the configuration fails, correct the hardware

G. (For airplanes equipped with the Ryan 9900 BX TCAD / TAS 620 Traffic systems). Configure the softw

y the presence of a small single 3-inch shark fin style antenna just above and aft of the cabin doors, and a dual 3-inch

(1) If the airplane is equipped with the Ryan TCAD/TAS Traffic system, follow this procedure

(2)

(3) he drop down menu in the FILE field.

(4) From the FILE field, select the ‘Cessna Option – 9900BX / TAS 620’ in the FILE field and

(6) Monitor the status of the upload. When the upload is completed, press ENT to

(8) If the OXYGEN configuration upload shows a failure, the upload process will stopyou must do the configuration upload procedure again. Do Steps 6.F.(2) thru 6.F.(7)again as necessary up to a total of five times unt

failure and start the configuration upload again.

are for the traffic system as follows:

NOTE: If installed, the TCAD/TAS system can be identified b

shark fin antenna mounted on the aft belly inspection panel.

to configure the G1000. If the airplane is not equipped with this option, go to step 7.

Turn the large FMS knob to highlight the FILE menu field on the SYSTEM UPLOAD page.

Turn the small FMS knob to expand t

press the ENT soft key.


acknowledge.

SB10-34-01 of 29 January 18, 2010

(7) View the SUMMARY field and make sure that all items were successfully completed: green at the check box(es) as shown:

procedure again. Do Steps 6.G.(2) thru 6.G.(7) again as necessary up to a total of five load. If after five times the

configuration fails, correct the hardware failure and start the configuration upload again.

(9) Push the small FMS knob on the PFD to stop the cursor.

7.

A. While in the maintenance pages of the PFD, turn the large FMS knob to select the GTX group page, and then turn the small FMS knob to select the TRANSPONDER CONFIGURATION page on the PFD.

The unique ICAO hexadecimal ID number can be found on the airplane registration certificate.) If the correct registration tail number or hexadecimal number

(1) Push the small FMS knob on the PFD to start the cursor and turn the large FMS knob to

.

Verify that PASS appears in

(8) If the Avidyne TAS 620 or Ryan 9900BX TCAD Traffic configuration upload shows a failure, the upload process will stop, and you must do the configuration upload

times until you successfully complete the configuration up

Do the airplane registration number configuration as follows:

B. 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.

C. Make sure that the airplane registration ADDRESS field has the correct tail number or hexadecimal number shown. (

is shown, go to Step 7.C.(7). If the correct registration tail number or hexadecimal number is not shown, do the following:

highlight the ‘ADDRESS’ field. Use the small/large FMS knobs to enter the airplane tail number or hexadecimal number as necessary

SB10-34-01 of 29 January 18, 2010

(2) Once the correct tail number or hexadecimal number is entered, press the ENT key. The transponder configuration process will begin.

(3) When the XPDR CONFIGURATION COMPLETE is displayed, select OK and push the ENT key.

decimal number is unsuccessful, repeat the procedure up to 5 times, and then contact Cessna Customer

b. Turn the small FMS knob to go to the system group SYSTEM UPLOAD page.

c. At the SYSTEM UPLOAD page, press the UPDT CFG softkey at the lower right

“Yes”.

r to acknowledge.

(8) Remove the system software SD card from the top slot of the PFD.

pt GDU Supplemental Database SD Cards into the lower slots of the PFD and MFD.

9. (Fo

NOTE: by

of the G1000 system to change and the new Airframe System I.D. number will not match the System I.D. number, which was permanently written to the TAWS-B

7-

(4) If the attempt to configure the airplane tail number or hexa

Service: Telephone 316-517-5800 or FAX 316-517-7271.

(5) Push the small FMS knob on the PFD to stop the cursor.

(6) Ensure the master configuration module has been updated as follows:

a. Turn the large FMS knob to select the SYSTEM group on the PFD.

corner of the PFD.

d. When prompted to update the Config Module, press the enter key to select

e. When the “Update Config Complete” window appears, press ente

(7) Pull the PFD and the MFD circuit breakers to remove power from the system.

8. Install the ke

r airplanes equipped with TAWS-B only) Install TAWS-B as follows:

It is possible that the original 010-00330-51 TAWS-B Enablement Card will not be recognizedthe G1000 system after installing the new software. The new software installation may cause the Airframe System I.D. number

card during initial installation in the airplane. If this happens, it will be necessary to obtain the Airframe System I.D. per Step 2.C. and contact Cessna Customer Service; Telephone; 316-515800 or FAX 316-517-7271.

SB10-34-01 of 29 January 18, 2010

NOTE: If the airplane has TAWS-B installed, the 010-00330-51 TAWS-B Enablement SD Card will normally be located in the blue Aircraft Software sheet in the back of the Pilot’s Operating

a corresponding logbook entry indicating the installation of the TAWS-B system.

A. With the system still powered on and the PFD and MFD circuit breakers pulled, push and hold

B. While holding the ENT key down, engage the MFD circuit breaker.

D upper slot.

the PFD circuit breaker.

ars:

group page.

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

and the drop down menu and select CONFIGURATION FILES in the AIRFRAME field. Press the ENT key, the cursor will drop down to the FILE field.

ENT key.

FILE option is selected, the PRODUCT window will populate and display software and configuration file information. All files should be checked; if not, press the

N. The Start Configuration Upload? Prompt will appear. Select YES and push the ENT key.

O. Monitor the status of the upload. When CONFIGURATION UPLOAD COMPLETE appears,

Q. Push the small FMS knob to stop the cursor.

R. On the overhead console, put the CROSSTIE switch, the AVIONICS MASTER switch, and the LEFT and RIGHT BATTERY MASTER switches in the OFF position.

S. Remove ground power from the airplane.

Handbook (POH). The TAWS-B SD card may also be in an envelope inside the front cover of theAvionics section of the airplane logbook, with

the ENT key on the MFD.

C. Release the MFD ENT key when the following message appears:

INITIALIZING SYSTEM

D. Install the TAWS-B (010-00330-51) Enablement SD Card in the PF

E. Push and hold the ENT key on the PFD and engage

F. Release the PFD ENT key when the following message appe

INITIALIZING SYSTEM

G. Turn the large FMS knob to go to the SYSTEM

H. Turn the small FMS knob to go to the SYSTEM UPLOAD page.

J. Turn the small FMS knob to exp

K. Turn the small FMS knob to expand the drop down menu and select ENABLE TAWS in the FILE field. Press the

L. Once the ENABLE TAWS

CHK ALL soft key.

M. Press the LOAD soft key.

push the ENT key.

P. Make sure that the SUMMARY field displays COMPLETE.

SB10-34-01 of 29 January 18, 2010

T. Remove the 010-00330-51 TAWS-B Enablement Card from the upper slot of the PFD and put it in the blue Aircraft Software sheet in the back of the Pilot’s Operating Handbook (POH) or in an envelope inside the front cover of the Avionics section of the airplane logbook from where it was removed.

U. Position the airplane outside where it has an unobstructed view of the sky to give the strongest GPS signal possible and do a test of the system. An indoor GPS repeater would be a suitable alternative.

NOTE: The TAWS-B system test will not pass the self-test without a good GPS signal.

V. Make sure the PFD and MFD circuit breakers are engaged. On the overhead console, put the CROSSTIE switch, the AVIONICS MASTER switch, and the LEFT and RIGHT BATTERY MASTER switches in the ON position.

W. While the PFD and MFD are powering up in the normal mode, the TAWS system will perform a pre-flight test.

X. Make sure the SPKR button on the audio panel is enabled and listen for the audible message “TAWS AVAILABLE.”

Y. On the MFD, turn the large FMS knob to the MAP group page.

Z. Turn the small FMS knob to go to the MAP-TAWS or MAP-TERRAIN PROXIMITY page.

AA. If the MAP-TAWS page is displayed, TAWS-B was loaded successfully; go to Step 10. If MAP - TERRAIN PROXIMITY is displayed, TAWS-B was not loaded successfully. Repeat Steps 9.A. thru 9.AA.

BB. If the attempt to load TAWS-B is unsuccessful, repeat the procedure up to 5 times, and then contact Cessna Customer Service: Telephone 316-517-5800 or FAX 316-517-7271.

10. Verify the Line Replacement Units (LRU) status as follows:

A. Turn the large FMS knob on the MFD to go to the AUX group page.

B. Turn the small FMS knob on the MFD to go to the AUX-SYSTEM STATUS page.

C. Push the small FMS knob to start the cursor in the LRU INFO field.

D. Scroll down and verify that there is a green check in the STATUS column for each LRU item. If any of the LRU items shows a red X in the STATUS column, correct the condition as needed and then check the status again.

11. Do the System Status LRU verification as follows:

A. If not already done, pull the PFD (Essential Bus) and the MFD (Avionics Bus) circuit breakers.

B. Push and hold the ENT key on the MFD and engage the MFD circuit breaker.

C. Release the ENT key when the message INITIALIZING SYSTEM appears on the MFD.

D. Allow the MFD to power up in the configuration mode.

E. Push and hold the ENT key on the PFD and engage the PFD circuit breaker.

F. Release the ENT key when the message INITIALIZING SYSTEM appears on the PFD.

SB10-34-01 of 29 January 18, 2010

G. Allow the PFD to power up in the configuration mode.

H. Turn the large FMS knob on the PFD to go to the SYSTEM group page.

I. Turn the small FMS knob on the PFD to go to the SYSTEM STATUS page.

J. Push the small FMS knob on the PFD to start the cursor.

K. Turn the small FMS knob to scroll through each LRU item and verify that the PART NUMBER and VERSION are the same as listed in Table 4 (Model 350 airplanes) or Table 5 (Model 400 airplanes).

(1) If the LRU PART NUMBERS and VERSIONS match those listed in Table 4 (Model 350 airplanes) or Table 5 (Model 400 airplanes), go to Step 11.L.

(2) If the LRU PART NUMBERS and VERSIONS do not match those listed in Table 4 (Model 350 airplanes) or Table 5 (Model 400 airplanes), reload the software for those items as needed. Refer to step 5.C.(6) for more information.

L. Put the LEFT and RIGHT BATTERY MASTER, CROSSTIE and AVIONICS MASTER Switches in the OFF position. Make sure that all the circuit breakers are engaged.

M. (For airplanes equipped with Chartview). Do the Garmin G1000 Avionics Charview Option Service Bulletin, SB08-34-06 (or latest revision).

NOTE: Airplanes equipped with 010-00330-43 GDU Supplemental Database SD Cards will do the same procedures as the 010-00330-42 cards described in SB08-34-06 (or latest revision).

N. If not previously done, disconnect ground power from the airplane.

12. Make an entry in the airplane logbook that states compliance with this Service Bulletin.

SB10-34-01 of 29 January 18, 2010

Table 4 – Model 350LINE REPLACEMENT UNIT (LRU) PART NUMBER VERSION STATUS

CO GUARDIAN N/A N/A OKCOM1 006-B0081-XX 7.00 OKCOM2 006-B0081-XX 7.00 OKGCU 006-B0472-20 3.01 OKGDC1 006-B0261-11 3.01 OKGDC1 FPGA 006-C0055-00 1.05 UNKNOWNGDL69 006-B0317-14 3.20.00 OKGEA1 006-B0193-05 2.07 OKGFC CERT GIA1 006-D0623-02 2.02 UNKNOWNGFC CERT GIA2 006-D0623-02 2.02 UNKNOWNGFC CERT P C 006-D0623-02 2.02 UNKNOWNGFC CERT PT 006-D0623-02 2.02 UNKNOWNGFC CERT R C 006-D0623-02 2.02 UNKNOWNGFC CERT R M 006-D0623-02 2.02 UNKNOWNGIA1 (GIA 63 Non-WAAS) 006-B0190-47 5.60 OKGIA1 (GIA 63W WAAS) 006-B0544-2A 5.61 OKGIA1 AUDIO 006-D0425-05 2.05 UNKNOWNGIA2 (GIA 63 Non-WAAS) 006-B0190-47 5.60 OKGIA2 (GIA 63W WAAS) 006-B0544-2A 5.61 OKGIA2 AUDIO 006-D0425-05 2.05 UNKNOWNGMA1 006-B0203-33 3.03 OKGMU1 006-B0224-00 2.01 OKGMU 1 FPGA 006-C0048-00 2.00 UNKNOWNGPS1* (non WAAS only) 006-B0329-01 3.03 OKGPS2* (non WAAS only) 006-B0329-01 3.03 OKGPS1* (WAAS only) 006-B0339-0A 3.2 OKGPS2* (WAAS only) 006-B0339-0A 3.2 OKGRS1 006-B0223-09 2.11 OKGRS1 FPGA 006-C0049-00 2.00 UNKNOWNGRS1 MV DB 006-D0159-01 2005.00 UNKNOWNGS1* 006-B0083-XX 4.00 OKGS2* 006-B0083-XX 4.00 OKGSA PTCH CTL 006-B0398-20 2.13 OKGSA PTCH MON 006-B0398-20 2.13 OKGSA ROLL CTL 006-B0398-20 2.13 OKGSA ROLL MON 006-B0398-20 2.13 OKGTA PTCH TRM 006-B0267-11 2.01 OKGTX1 006-B0172-01 4.06 OKMFD1 006-B0319-75 9.05 OKMFD1 FPGA 006-C0036-04 1.04 UNKNOWNNAV1* 006-B0082-XX 5.03 OKNAV2* 006-B0082-XX 5.03 OK

006-B0319-75 9.05 OKPFD1*** BB(BOOT BLOCK) VERSION ==> 006-00191-04 2.03

PFD1 FPGA 006-C0036-04 1.04 UNKNOWN*NOTE: The GPS, GS, and NAV software files may not be the same as indicated in the chart.

SB10-34-01 of 29 January 18, 2010

Table 5 – Model 400 LINE REPLACEMENT UNIT (LRU) PART NUMBER VERSION STATUS

CO GUARDIAN N/A N/A OKCOM1 006-B0081-XX 7.00 OKCOM2 006-B0081-XX 7.00 OKGCU 006-B0472-20 3.01 OKGDC1 006-B0261-11 3.01 OKGDC1 FPGA 006-C0055-00 1.05 UNKNOWNGDL69 006-B0317-14 3.20.00 OKGEA1 006-B0193-05 2.07 OKGFC CERT GIA1 006-D0456-04 2.04 UNKNOWNGFC CERT GIA2 006-D0456-04 2.04 UNKNOWNGFC CERT P C 006-D0456-04 2.04 UNKNOWNGFC CERT PT 006-D0456-04 2.04 UNKNOWNGFT CERT R C 006-D0456-04 2.04 UNKNOWNGFC CERT R M 006-D0456-04 2.04 UNKNOWNGIA1 (GIA 63 Non-WAAS) 006-B0190-47 5.60 OKGIA1 (GIA 63W WAAS) 006-B0544-2A 5.61 OKGIA1 AUDIO 006-D0425-05 2.05 UNKNOWNGIA2 (GIA 63 Non-WAAS) 006-B0190-47 5.60 OKGIA2 (GIA 63W WAAS) 006-B0544-2A 5.61 OKGIA2 AUDIO 006-D0425-05 2.05 UNKNOWNGMA1 006-B0203-33 3.03 OKGMU1 006-B0224-00 2.01 OKGMU 1 FPGA 006-C0048-00 2.00 UNKNOWNGPS1* (non WAAS only) 006-B0329-01 3.03 OKGPS2* (non WAAS only) 006-B0329-01 3.03 OKGPS1* (WAAS only) 006-B0339-0A 3.2 OKGPS2* (WAAS only) 006-B0339-0A 3.2 OKGRS1 006-B0223-09 2.11 OKGRS1 FPGA 006-C0049-00 02.00 UNKNOWNGRS1 MV DB 006-D0159-01 2005.00 UNKNOWNGS1* 006-B0083-XX 4.00 OKGS2* 006-B0083-XX 4.00 OKGSA PTCH CTL 006-B0398-20 2.13 OKGSA PTCH MON 006-B0398-20 2.13 OKGSA ROLL CTL 006-B0398-20 2.13 OKGSA ROLL MON 006-B0398-20 2.13 OKGTA PTCH TRM 006-B0267-11 2.01 OKGTX1 006-B0172-01 4.06 OKMFD1 006-B0319-75 9.05 OKMFD1 FPGA 006-C0036-04 1.04 UNKNOWNNAV1* 006-B0082-XX 5.03 OKNAV2* 006-B0082-XX 5.03 OK

006-B0319-75 9.05 OKPFD1*** BB(BOOT BLOCK) VERSION ==> 006-B0191-04 2.03

PFD1 FPGA 006-C0036-04 1.04 UNKNOWN*NOTE: The GPS, GS, and NAV software files may not be the same as indicated in the chart.

SB10-34-01 of 29 January 18, 2010

OWNER NOTIFICATION

On February 1, 2010 the following Owner Advisory message will be sent to applicable owners of record in SB10-34-01A.

Dear Cessna Owner:

This Owner Advisory is to inform you of a software upgrade for the Garmin G1000 System as provided in Service Bulletin SB10-34-01: Garmin G1000 System Software Upgrade to GDU 9.05, Version 534.13. The software upgrade includes the following changes:

! Flight Plan selection/transition enhancements

! TAWS system enhancements

! Single Cue aircraft representation symbol update

! More precise standard BARO

! The ability to select traffic only display on map inset

! Canadian XM weather support

! Display of airport “hot spots” from the SafeTaxi database

! TAWS flight phase logic upgrades for operation in airspace with multiple airports

! Flight Charts database cycle checking enhancements

! Automatic Flight Control System (AFCS) enhancements

! Updates horizon display for consistency with other Cessna models (disabled gradient horizon)

! Increases alternator out alert trigger threshold to avoid nuisance alerts during ground operation

! Provides resolution for the GPS/WAAS issue that involves a potential reset of the GPS/WAAS receiver

when operating in specific northern latitudes and Alaska, along with other updates

! Ensures communication is re-established between the CO Guardian and G1000 system in the event

of a data interruption

! Provides system readiness capability for the Garmin Synthetic Vision Technology (SVT) feature. The

enablement of SVT can be accomplished with Service Bulletin SB10-34-02

! Supports the capability of an Electronic Pilot’s Checklist

! Enhancement to allow simultaneous display of TOPO and NEXRAD on maps

! Incorporation of Garmin Service Alerts 0811 and 0816

! Incorporation of Garmin Service Advisories 0745, 0831, 0838, and 0908

Compliance is recommended: should be accomplished at the next 100 hour or 12 month (annual) inspection, whichever occurs first.

SB10-34-01 of 29 January 18, 2010

SB10-34-01 of 29 January 18, 2010

NOTE: Cessna Service Bulletin SB08-34-05: G1000 System Software Upgrade to GDU 8.10 Version 534.09 must be accomplished, prior to installing the software described in this Service Bulletin on the following serial numbers only.

A. Airplane Model 350 (LC42-550FG) Serial Numbers 42502 thru 42569, 421001 thru 421010.

B. Airplane Model 400 (LC41-550FG) Serial Numbers 41034, 41563 thru 41650, 41652 thru 41800, 411001 thru 411061.

C. Prior accomplishment of Cessna Service Bulletin SB08-34-05 is not required for the following airplane serial numbers:



The information contained in the referenced Cessna Service Bulletin shall be considered an amendment to the Cessna Manufacturer's Service / Maintenance Manual and should be accomplished within the specified time requirement.

Credit Information

For airplanes in warranty:

A labor allowance credit of 2.1 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 for each one of the following applicable configuration uploads:

! Ryan 9900BX / TAS 620 Traffic Systems ! Oxygen ! Becker 3502 Automatic Direction Finder (ADF), ! Honeywell KN63 Distance Measuring Equipment (DME) ! Fuel Tank option

If necessary, a labor allowance credit of 0.2 man-hour will be provided to do the applicable configuration upload for airplanes equipped with the Garmin Terrain Awareness Warning System (TAWS-B).

If necessary, a labor allowance credit of 0.3 man-hour will be provided to do the applicable configuration upload for airplanes equipped with the Garmin G1000 ChartView option.

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………………………… January 18, 2011 International……………………... January 18, 2011

The Cessna Garmin Software Installation CD is enclosed. The Cessna Service Station 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 Garmin G1000 Software.

Please contact a Cessna Single Engine Service Station for detailed information and make arrangements to have Service Bulletin SB10-34-01 accomplished on your airplane.

* * * * * * *

single engine - cessna

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