NOTE: SB is a WAAS only supported build. If the autopilot is not WAAS equipped, the unlock card cannot be used at this time.

Similar documents
This Service Bulletin is applicable only to airplanes equipped with placards that are written in English.

Service Bulletin No.: D42L Rev 0 Date Issued: 06 June 2016 Title: GTX 33ES Installation Page: 1 of 6

The airplanes that follow that have incorporated SB (or latest revision) GARMIN G1000 GPS/WAAS Installation:

All KODIAK 100 Series Aircraft; see Compliance section below for details of applicability.

SUBJECT: Single Engine Service Bulletin SB Revision 1: Cosmetic Window Repair

Affected , RX, , and RX alternators in Service Station stock should be returned to Cessna.

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

Service Information Letter

It has been determined that some airplanes may have a hose plug installed in the inflatable belt assembly hose end.

SERVICE BULLETIN NAVIGATION - GARMIN G1000 SYSTEM UPGRADES INCLUDING TERRAIN AWARENESS AND WARNING SYSTEM (TAWS-B) FUNCTION PER STC SA01725SE

SERVICE BULLETIN REVISION TRANSMITTAL

*MANDATORY SERVICE BULLETIN*

Please replace any copy of SEB07-2 with the attached copy of SEB07-2 Revision 1 which is printed in its entirety.

Single Engine. Service Bulletin TITLE ENGINE MOUNT BRACKET INSPECTION

Single Engine. Service Bulletin TITLE ELEVATOR TRIM TAB ACTUATOR ASSEMBLY INSPECTION EFFECTIVITY. Group A airplanes: Serial Numbers

G1000 Synthetic Vision & Pathways Option

SERVICE NOTICE. 1. The configuration of each Garmin LRU specific to the KODIAK The Garmin LRU software.

SERVICE INFORMATION NO. SI

ATTACHMENT. Orders for the required parts listed below must be placed by using this form only. Service Station/Company Code: Company Name:

SERVICE BULLETIN. COMPLIANCE MANDATORY. This service bulletin must be accomplished at the next 100-hour or 12-month (annual-type) inspection.

Single Engine MODIFICATION KIT

Single Engine. Service Bulletin TITLE PILOT AND COPILOT SECONDARY SEAT STOP INSTALLATION

G600 PFD/MFD System Instructions for Continued Airworthiness as installed in

SERVICE INFORMATION NO. SI

SERVICE BULLETIN SB

Company Proprietary Information

ATTACHMENT DAMAGE REPORT FORM. Page: 1 of Pages Includes this cover sheet Date: (month/day/year) This form is for the: Left Wing: Right Wing: Other:

SERVICE BULLETIN REVISION

SERVICE LETTER. SERIAL NUMBERS 210 & T thru P thru P

SERVICE LETTER. Single Engine SEL TITLE LANDING GEAR - DRAG LINK REPLACEMENT

SERVICE BULLETIN. This service bulletin provides parts and instructions to install fuel caps that have a locking feature.

SERVICE BULLETIN SB

SERVICE LETTER REVISION TRANSMITTAL

Revision Transmittal Sheet

Indicating. 1. General. A. Fuel Quantity. B. Fuel Flow

SERVICE BULLETIN SERIAL NUMBERS. The equivalent of this service bulletin has been incorporated on production airplanes and On.

SERVICE BULLETIN. Citation CIB TITLE FUEL - FIREWALL SHUTOFF VALVE GROUND IMPROVEMENT

Cessna Distributors and Single Engine Authorized Service Facilities and CPC's

SERVICE BULLETIN REVISION

SERVICE BULLETIN. NO.: 0713 Revision C. All Garmin Aviation Service Centers and Aircraft OEM Service Centers DATE: 29 May 2007

SERVICE LETTER SERIAL NUMBERS. 550/ thru -0505, thru -0733, thru -0969

SERVICE BULLETIN. Beech ATA CODE PLACARDS AND MARKINGS - INSTALLATION OF FUEL SELECTOR PLACARD

LOG OF REVISIONS. Model G58 Baron (Serials TH-2125 and After) Pilot s Operating Handbook and FAA Approved Airplane Flight Manual

500W Series Instructions for Continued Airworthiness

SERVICE BULLETIN SB

SERVICE BULLETIN. The equivalent of this service bulletin has been incorporated on production airplanes and On.

SERVICE BULLETIN CERTIFICATION REQUIREMENTS - FOREIGN CERTIFICATION PLACARD INSTALLATION

September 8, Cessna Distributors, Authorized Service Facilities, CPC's, CSTARS, ASR's, and affected Owners of Record

MANDATORY SERVICE BULLETIN NO. MSB D4-045/9

SERVICE BULLETIN TITLE ENGINE CONTROLS - FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC) SOFTWARE UPGRADE VERSION C10

SERVICE BULLETIN REVISION TRANSMITTAL

SR22 Airplane Flight Manual (AFM) Temporary Change

The engine cowling installation and firewall should be inspected and modified as specified in this Service Bulletin.

SERVICE BULLETIN REVISION TRANSMITTAL

SUBJECT: ELECTRICAL POWER SYSTEM UNIT AND ROTORCRAFT FLIGHT MANUAL TEMPORARY REVISION, CANCELLATION OF

SERVICE BULLETIN REVISION TRANSMITTAL

500W Series Instructions for Continued Airworthiness

SERVICE BULLETIN REVISION

MODIFICATION KIT. Serial Numbers 300 (LC40-550FG) thru (LC42-550FG) thru (LC41-550FG) thru

SERVICE BULLETIN. To prevent the wing fuel boost pump wiring from chafing on the wing structure and/or fuel tube assemblies.

EFFECTIVITY Serial Numbers thru , 698

SERVICE BULLETIN. No. SB-AG-49 August 1, 2008 SEAT SUPPORT BRACKET INSPECTION AND REPAIR

SERVICE BULLETIN. To prevent the wing fuel boost pump wiring from chafing on the wing structure and/or fuel tube assemblies.

SERVICE BULLETIN MANDATORY. SB , Rev Planning Information

CIRRUS AIRPLANE MAINTENANCE MANUAL

Instructions for Continued Airworthiness

SECTION 3 ENGINE INDICATION SYSTEM (EIS)

PROPELLERS - PROPELLER SLIP RING MOUNTING PLATE INSPECTION AND REPAIR

Service Bulletin. Service Bulletin No. 064 Alternator Model ALV-9610 Series Through Bolt Inspection for Proper Torque

ATTITUDE AND DIRECTION

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

The parts that follow are available from Cessna Parts Distribution through an appropriate Cessna Service Station.

INTEGRATED ENGINE INSTRUMENT SYSTEMS

41001 thru incorporating a retrofitted LA nose strut,

SERVICE BULLETIN FUEL - MODIFICATION OF THE ENGINE DRIVEN FUEL PUMP SYSTEM

ALERT SERVICE LETTER

GNS 400W/500W Series SW Version 4.00 Upgrade Supplement

Pilot's Operating Handbook Supplement AS-03

SERVICE KIT. TITLE McCAULEY 2A34C203/90DCA-2 TWO BLADED THREADLESS PROPELLER INSTALLATION

SERVICE LETTER TITLE EXHAUST - TRANSMITTAL OF LYCOMING SERVICE BULLETIN NO 627C, EXHAUST SYSTEM INSPECTION SERIAL NUMBERS

CESSNA 172S NAV III VFR CHECKOUT POH EXAMINATION (Based on N1129K, serial no. 172S revised 10/05/06)

SERVICE FUEL WARNING PLACARD AND POH INSPECTION

SERVICE BULLETIN. EFFECTIVITY SERIAL NUMBERS 680 (Citation Sovereign) thru (Citation Sovereign+) thru -0549

Citation Mustang. Throttle Lever Rigging. TLA Rigging Guide REFERENCE ONLY

CIRRUS AIRPLANE MAINTENANCE MANUAL

(b) This AD supersedes AD R1, Amendment

SERVICE KIT thru , 631, 634, 675 R thru R F thru F FR thru FR

CESSNA AIRCRAFT COMPANY

[Docket No. FAA ; Directorate Identifier 2010-CE-058-AD; Amendment ; AD ]

FORM: 2391 DRAWING NO: ICA Cessna Aircraft Company P.O Box 7704 WICHITA, KS 67277

Rotary Speed Brake Actuation System ICA Supplement

ROTORCRAFT FLIGHT MANUAL SUPPLEMENT for AS350 Series Helicopter. Registration Number: _. Serial Number: -----

SERVICE BULLETIN. The equivalent of this service bulletin has been incorporated on production airplanes and On. REASON

Single Engine Service Bulletin SEB08-4 Revision 1, Unision Industries SLICK 4200/4300/6200/6300 Magnetos Inspection.

CIRRUS AIRPLANE MAINTENANCE MANUAL

SERVICE LETTER. Model 1A162 Propeller, and the McCauley Fixed Pitch Propeller Service Manual.

SERVICE LETTER. Multi-engine TITLE NACELLES/PYLONS - NACELLE FITTING INSPECTION EFFECTIVITY

SERVICE LETTER REVISION TRANSMITTAL

POWER TURBINE RPM (N2) STEADY STATE OPERATION AVOIDANCE, INTRODUCTION OF.

[Docket No. FAA ; Directorate Identifier 2010-CE-058-AD; Amendment ; AD ]

Transcription:

Single Engine Service Bulletin July 22, 2011 TITLE GARMIN G1000 / FLINT AERO, INC AUXILIARY FUEL GALLON REMAINING ENABLEMENT EFFECTIVITY The following airplanes equipped with the Garmin G1000 Nav III Avionics Option and the Flint Aero, Inc Auxiliary Fuel Tanks Supplemental Type Certificate (STC): Model Serial Numbers 206H T206H 20608216 and On T20608450 and On REASON To provide a configuration upgrade and enabling instructions for the optional Garmin G1000 auxiliary fuel enablement on the model 206H and T206H NAV III equipped airplanes which also have accomplished the Flint Aero, Inc Auxiliary Fuel Tanks Supplemental Type Certificate (STC). DESCRIPTION When you set up the fuel totalizer function, the configuration unlock card will allow the maximum fuel remaining value to be set to 116 gallons and shown as 116 on the engine indication system (EIS) - SYSTEM display. Currently the maximum fuel remaining value that you can set is 87. This configuration unlock card will allow the crew to input a gallons remaining value that includes 29 gallons of usable fuel available from the Flint Aero, Inc STC. There is no change to the EIS fuel quantity indicators, G1000 multi-function display (MFD) soft keys, or functionality of the gallons used calculations. COMPLIANCE Optional: May be accomplished if desired and if the Flint Aero Auxiliary Fuel Tanks are installed in accordance with the Flint Aero, Inc STC. NOTE: Airplane must have software version 563.20 (or later build) installed or Cessna Service Bulletin SB11-34-01 (or latest revision) Garmin G1000 System Software Upgrade to 563.21 must be accomplished before installation of the auxiliary fuel enablement. NOTE: SB11-34-01 is a WAAS only supported build. If the autopilot is not WAAS equipped, the unlock card cannot be used at this time. Page 1 of 5 To obtain satisfactory results, procedures specified in this publication must be accomplished in accordance with accepted methods and prevailing government regulations. Cessna Aircraft Company cannot be responsible for the quality of work performed in accomplishing the requirements of this publication. Cessna Aircraft Company, Customer Service, P.O. Box 7706, Wichita, Kansas 67277, U.S.A. (316) 517-5800, Facsimile (316) 517-7271 www.cessnasupport.com COPYRIGHT 2011

APPROVAL FAA approval has been obtained on technical data in this publication that affects airplane type design. MANPOWER 0.7 man-hour to accomplish this Service Bulletin. REFERENCES Model 206/T206 Series 1998 and On Maintenance Manual Garmin G1000 Cockpit Reference Guide for Cessna NAV III, Part Number 190-00384-11 Rev A (or later revision). The following documents can be viewed by Cessna Authorized Service Facilities at www.garmin.com: Garmin G1000 System Installation Manual, Part Number 190-00303-00, Revision H (or latest revision) Garmin GDU 1040 Installation Manual, Part Number 190-00303-01, Revision S (or latest revision) Garmin G1000 NAV III Line Maintenance Manual, Part Number 190-00352-00, Revision P (or latest revision) NOTE: Make sure all publications used are complete and current. Refer to cessnasupport.com. NOTE: This information shall be considered an amendment to the Cessna Manufacturer's Service/Maintenance Manual. OTHER PUBLICATIONS AFFECTED Model 206H & Model T206H Illustrated Parts Catalog NOTE: Make sure all publications used are complete and current. Refer to cessnasupport.com. MATERIAL AVAILABILITY The following part is available and can be ordered from Cessna Service Parts and Programs: Part Number Description Qty/Airplane 010-00905-02 (T)206 Auxiliary Fuel Unlock Card 1 CREDIT INFORMATION Not applicable Page 2 July 22, 2011

ACCOMPLISHMENT INSTRUCTIONS WEIGHT AND BALANCE INFORMATION Negligible Material Information The part below will be necessary: NEW P/N QUANTITY DESCRIPTION OLD P/N DISPOSITION 010-00905-02 1 (T)206 Auxiliary Fuel None None Unlock Card Instructions 1. Connect external electrical power to the airplane. 2. Make sure that approved system software is installed on your airplane: A. Make sure that all of the necessary circuit breakers are pushed in for normal mode startup of the G1000 System. B. Put both the MASTER BAT and AVIONICS MASTER switches to the ON position and let the system power up. C. Make sure that you have the 190-00384-11 Revision A (or later) Cockpit Reference Guide. D. On the Multifunction Display (MFD) startup (splash) screen, make sure that the system software version shown in the upper right corner of the screen is the same as that shown in Table 1or a later software version. NOTE: You can also find the system software version if you turn the large and the small FMS knobs on the MFD to go to the AUX-SYSTEM STATUS page. TABLE 1. Software Version 563.20 (or later) (1) If the software version is the same as that shown in Table 1, or later version, go to Step 2E. (2) If the software version is not that of Table 1, load the correct software per Cessna Service Bulletins SB11-34-01 (or latest revision) Garmin G1000 System Software Upgrade to 563.21 for Airplanes Equipped with NAV III. E. Put both the MASTER BAT and AVIONICS MASTER switches to the off position. 3. Do the auxiliary fuel enablement to the G1000 Avionics system as follows: NOTE: Auxiliary fuel enablement is done with the 010-00905-02(T)206AuxiliaryFuelUnlockCard. A. Remove and mark the Primary Flight Display (PFD) and the MFD GDU Supplemental Database SD cards from the bottom slots of the PFD and the MFD. B. Disengage the PFD (ESS and AVN BUS 1) and MFD (AVN BUS 2) circuit breakers. C. Put both the MASTER BAT and 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 MFD ENT key when the message that follows appears: INITIALIZING SYSTEM. F. Install the 010-00905-02 (T)206 Auxiliary Fuel Unlock Card in the PFD top slot. July 22, 2011 Page 3

G. Push and hold the ENT key on the PFD and engage the PFD (ESS and AVN BUS 1) circuit breakers. H. Release the PFD ENT key when the message that follows appears: INITIALIZING SYSTEM. I. Turn the small FMS knob on the PFD to go to the SYSTEM group SYSTEM UPLOAD page. Push the small FMS knob to activate the cursor and turn the small FMS knob to expand the drop down menu and highlight the (T)206H WITH FLINT AERO AUX FUEL TANK in the airframe field. J. Push the ENT key. K. Turn the small FMS knob on the PFD to select CESSNA 206/T206H FLINT AERO AUX FUEL TANK INSTALLATION in the file field and push the ENT key of the PFD. L. Push the LOAD soft key. M. Monitor the status of the upload to make sure that the UPLOAD COMPLETE message appears. N. When UPLOAD COMPLETE appears, push the ENT key to acknowledge it. O. Make sure that the summary field shows COMPLETED. P. Do Steps 3L through 3O again if the summary field shows not completed. Do not cancel an upload before it successfully loads or fails. Wait until a successful load or fail shows in the summary field before you begin Steps 3L through 3P again. NOTE: You can do Steps 3L through 3O again for a maximum of four times because of a failed or cancelled upload prompt message. If the system does not upload after the fourth attempt, contact Cessna Customer Care: Telephone 316-517-5800 or FAX 316-517-7271. Q. Push the UPDT CFG soft key and push the ENT key for Yes. R. After the update config is complete, push the ENT key for Yes. S. Disengage the PFD (ESS and AVN BUS 1) and MFD (AVN BUS 2) circuit breakers. T. Remove the auxiliary fuel unlock card from the PFD top slot and store it in the sleeve of the Pilot's Operating Handbook (POH). U. Insert the PFD and the MFD GDU 010-00330-43 Supplemental Database SD Cards into the bottom slots of the PFD and the MFD. 4. Make sure that you have done the auxiliary fuel enablement to the Garmin G1000 Avionics system correctlyasfollows: A. Engage the PFD (ESS and AVN BUS 1) and MFD (AVN BUS 2) circuit breakers. B. Push the ENT key on the MFD to remove the splash screen. C. Push the ENGINE key on the MFD. D. Push the SYSTEM soft key. E. Push the RST FUEL soft key. F. Make sure that the Gallons Remaining on the system page reads zero. G. Push the GAL REM soft key. H. Pushthe87GALsoftkey. I. Push the +10 GAL soft key. J. Push the +10 GAL soft key again. K. Push the +10 GAL soft key again. L. Make sure that the Gallons Remaining on the system page reads 116: (1) If the Gallons Remaining on the system page does not read 116, do Steps 4C thru 4K again. Then go to Step 4M. (2) If the Gallons Remaining on the system page does read 116, go to Step 5. Page 4 July 22, 2011

M. Make sure that the Gallons Remaining on the system page reads 116: (1) If the Gallons Remaining on the system page does not read 116, do Steps 3A thru 3T again. Then go to Step 4. (2) If the Gallons Remaining on the system page does read 116, go to Step 5. 5. Put both the MASTER BAT and AVIONICS BUS 1 & 2 in the OFF position. 6. Remove external electrical power from the airplane. 7. Make a logbook entry stating compliance with this Service Bulletin. OWNER NOTIFICATION On August 12, 2011 the following message will be sent to applicable owners of record in A. Dear Cessna 206H/T206H Owner: Service Bulletin Garmin G1000 / Flint Aero, Inc Auxiliary Fuel Gallon Remaining Enablement has been issued to provide a configuration upgrade and enabling instructions for the optional Garmin G1000 auxiliary fuel enablement on the model 206H and T206H NAV III equipped airplanes which also have accomplished the Flint Aero, Inc Auxiliary Fuel Tanks Supplemental Type Certificate (STC). When you set up the fuel totalizer function, the configuration unlock card will allow the maximum fuel remaining value to be set to 116 gallons and shown as 116 on the engine indication system (EIS) - SYSTEM display. Currently the maximum fuel remaining value that you can set is 87. This configuration unlock card will allow the crew to input a gallons remaining value that includes 29 gallons of usable fuel available from the Flint Aero, Inc STC. There is no change to the EIS fuel quantity indicators, G1000 multi-function display (MFD) soft keys, or functionality of the gallons used calculations. Compliance is Optional: May be accomplished if desired and if the Flint Aero Auxiliary Fuel Tanks are installed in accordance with the Flint Aero, Inc STC. NOTE: Airplane must have software version 563.20 (or later build) installed or Cessna Service Bulletin SB11-34-01 (or latest revision) Garmin G1000 System Software Upgrade to 563.21 must be accomplished before installation of the auxiliary fuel enablement. NOTE: SB11-34-01 is a WAAS only supported build. If the autopilot is not WAAS equipped, the unlock card cannot be used at this time. The information contained in the referenced Cessna Service Bulletin shall be considered an amendment to the Cessna Manufacturer's Service/Maintenance Manual. Please contact a Cessna Single Engine Authorized Service Facility for detailed information and arrange to have Cessna Service Bulletin accomplished on your airplane. * * * * * * * July 22, 2011 Page 5