SUBJECT: Single Engine Service Bulletin SB Revision 1: Cosmetic Window Repair
|
|
- Easter Griffith
- 5 years ago
- Views:
Transcription
1 Revision Transmittal TO: Cessna Distributors, Single Engine Service Stations SUBJECT: Single Engine Service Bulletin Revision 1: Cosmetic Window Repair REASON FOR REVISION To revise the Compliance section to suspend compliance with until Revision 2 is issued. REQUIRED ACTION Please place a copy of Revision 1 with the Original Issue of. LOG OF EFFECTIVE PAGES Page No. Date * * * * * * * Page 1 of 1 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) Facsimile (316) COPYRIGHT 2009
2
3 Single Engine Service Bulletin Revision 1 TITLE COSMETIC WINDOW REPAIR EFFECTIVITY Model Serial Numbers 300 (LC40-550FG) thru (LC42-550FG) thru (LC41-550FG) thru REASON Reports have been received of cosmetic cracks being found in the paint and filler material located between the airplane windows and the fuselage. DESCRIPTION To provide instructions and required materials for the removal and replacement of the cosmetic filler and paint around an affected window as described in this Service Bulletin. COMPLIANCE Effective immediately, compliance with has been suspended until Revision 2 is issued. Do not start any work on an airplane using the original issue instructions. Only airplanes currently undergoing the repair process may be completed. The accomplishment instructions in the original issue of are being evaluated for potential changes and any changes will be communicated in Revision 2. APPROVAL FAA approval has been obtained on technical data in this publication that affects airplane type design. Original Issue: December 1, 2008 Page 1 of 3 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 Support Service, P.O. Box 7706, Wichita, Kansas 67277, U.S.A. (316) Facsimile (316) COPYRIGHT 2008
4 OWNER NOTIFICATION A. On December 15, 2008 the following Owner Advisory message was sent to applicable owners of record in A. Dear Cessna Owner: This Owner Advisory is to inform you that Cosmetic Window Repair has been issued. It has been reported that cosmetic cracks have been found in the paint and filler material located between the airplane windows and the fuselage. provides instructions and required materials for the removal and replacement of the cosmetic filler and paint around an affected window as described in. Compliance is Optional: if a cosmetic crack condition is found as described in the Service Bulletin. The information contained in the referenced Cessna Service Bulletin shall be considered an amendment to the Cessna Manufacturer s Service/Maintenance Manual. CREDIT INFORMATION For airplanes in warranty if the condition is present as described in this. If necessary, applicable parts credit and labor allowance credit of 7.5 man-hours per window will be provided to remove the cosmetic filler, replace the filler with Devcon Plastic Welder II, and paint around a left or right rear window. A photo of the cosmetic crack before the repair will be required. Include window location and airplane serial number in each photo. If necessary, applicable parts credit and labor allowance credit of 7.7 man-hours per window will be provided to remove the cosmetic filler, replace the filler with Devcon Plastic Welder II, and paint around a left or right door window. A photo of the cosmetic crack before the repair will be required. Include window location and airplane serial number in each photo. If necessary, applicable parts credit and labor allowance credit of 8.7 man-hours will be provided to remove the cosmetic filler, replace the filler with Devcon Plastic Welder II, and paint around the windshield. A photo of the cosmetic crack before the repair will be required. Include window location and airplane serial number in each photo. To receive credit, the work must be completed and a Warranty Claim submitted by a Cessna Single Engine Service Station within 30 calendar days of Service Bulletin compliance before the credit expiration dates shown below. Domestic.December 1, 2009 International December 1, 2009 NOTE: Include photos as described above with the warranty claim. Please contact a Cessna Single Engine Service Station for detailed information. Revision 1 Page 2
5 B. On the following Owner Advisory message will be sent to applicable owners of record in AR1. Dear Cessna Owner: This Owner Advisory is to inform you that Service Bulletin Revision 1 has been issued. Effective immediately, compliance with has been suspended until Revision 2 is issued. Do not start any window cosmetic repairs on an airplane using the original issue instructions. Only airplanes currently undergoing the repair process may be completed. The accomplishment instructions in the original issue of are being evaluated for potential changes and any changes will be communicated via Revision 2. Please contact a Cessna Single Engine Service Station for detailed information. * * * * * * * Revision 1 Page 3
Service Information Letter
Service Information Letter Open Rotor Circuit 9910591 Series Alternators Issue Date: December 20, 2006, Revision 1 Original Issue Date: November 29, 2006 INTRODUCTION: Kelly Aerospace Turbine Rotables
More informationThis Service Bulletin is applicable only to airplanes equipped with placards that are written in English.
Caravan Service Bulletin June 25, 2007 TITLE FUEL CAPACITY PLACARD REPLACEMENT EFFECTIVITY This Service Bulletin is applicable only to airplanes equipped with placards that are written in English. The
More informationIt has been determined that some airplanes may have a hose plug installed in the inflatable belt assembly hose end.
Single Engine Service Bulletin November 19, 2007 TITLE AMSAFE INFLATABLE RESTRAINTS HOSE PLUG INSPECTION EFFECTIVITY Group A airplanes: The following airplanes were delivered from the factory equipped
More informationFAA approval has been obtained on technical data in this publication that affects airplane type design.
Caravan Service Bulletin July 20, 2010 TITLE RIGHT INBOARD FLAP BELL CRANK BEARING INSPECTION / REPLACEMENT EFFECTIVITY The airplanes that follow that have had part number S3952-5 Bearing(s) installed
More informationAffected , RX, , and RX alternators in Service Station stock should be returned to Cessna.
Single Engine Service Bulletin December 18, 2006 TITLE 60 AMPERE ALTERNATOR BRUSH REPLACEMENT EFFECTIVITY The following airplanes currently equipped with part number 9910591-11, 9910591-11RX, 9910591-12
More informationPlease replace any copy of SEB07-2 with the attached copy of SEB07-2 Revision 1 which is printed in its entirety.
Revision Transmittal May 14, 2007 TO: Cessna Distributors, Single Engine Service Stations and CPC's SUBJECT: Single Engine Service Bulletin SEB07-2 Revision 1: Engine Mount Bracket Inspection. REASON FOR
More informationSingle Engine. Service Bulletin TITLE ELEVATOR TRIM TAB ACTUATOR ASSEMBLY INSPECTION EFFECTIVITY. Group A airplanes: Serial Numbers
Single Engine Service Bulletin March 12, 2007 TITLE ELEVATOR TRIM TAB ACTUATOR ASSEMBLY INSPECTION EFFECTIVITY Group A airplanes: Model Serial Numbers 172R 17281353 thru 17281364, 17281369 thru 17281372
More informationSingle Engine. Service Bulletin TITLE PILOT AND COPILOT SECONDARY SEAT STOP INSTALLATION
Single Engine Service Bulletin May 14, 2007 TITLE PILOT AND COPILOT SECONDARY SEAT STOP INSTALLATION EFFECTIVITY Model Year Serial Numbers 170 1948 18000 thru 18729 170A 1949 thru 1951 18730 thru 19400
More informationATTACHMENT 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:
ATTACHMENT DAMAGE REPORT FORM TO: Cessna Aircraft Company Propeller Aircraft Customer Service/Dept 753 P.O. Box 7706 Wichita, Kansas 67277-7706 Phone Number: 316-517-5800 Fax Number: 316-942-9006 Page:
More informationSingle Engine. Service Bulletin TITLE ENGINE MOUNT BRACKET INSPECTION
Single Engine Service Bulletin April 16, 2007 TITLE ENGINE MOUNT BRACKET INSPECTION EFFECTIVITY Model Year Serial Numbers 172 1956 thru 1959 28000 thru 29999 172 1956 thru 1959 36000 thru 36999 172 1956
More informationNOTE: SB is a WAAS only supported build. If the autopilot is not WAAS equipped, the unlock card cannot be used at this time.
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
More informationCessna Distributors and Single Engine Authorized Service Facilities and CPC's
Revision Transmittal June 11, 2015 TO: Cessna Distributors and Single Engine Authorized Service Facilities and CPC's SUBJECT: Single Engine Service Bulletin, Pilot and Copilot Secondary Seat Stop Installation.
More informationSERVICE LETTER. Single Engine SEL TITLE LANDING GEAR - DRAG LINK REPLACEMENT
SERVICE LETTER TITLE LANDING GEAR - DRAG LINK REPLACEMENT EFFECTIVITY Group A Airplanes: The following airplane serial numbers were delivered with a suspect 1243600-1 Drag Link Assembly: MODEL SERIAL NUMBERS
More informationSERVICE LETTER SERIAL NUMBERS. 550/ thru -0505, thru -0733, thru -0969
TITLE FUSELAGE - DORSAL FIN VANE INSPECTION EFFECTIVITY MODEL SERIAL NUMBERS 550/551-0002 thru -0505, -0550 thru -0733, -0801 thru -0969 REASON The equivalent of this service letter has been incorporated
More informationATTACHMENT. Orders for the required parts listed below must be placed by using this form only. Service Station/Company Code: Company Name:
Single Engine ATTACHMENT CREW SEAT RECLINE MODIFICATION SB04-25-01 Revision 4 Orders for the required parts listed below must be placed by using this form only. NOTE: All web orders for these kits/parts
More informationSERVICE LETTER REVISION TRANSMITTAL
REVISION TRANSMITTAL This sheet transmits Revision 1 to, which: A. Changes the Inspection warranty time to 0.2 from 3.0. B. Adds the note in the LABOR HOURS section. C. Adds the QR Code and internet address
More informationSERVICE BULLETIN. Citation CIB TITLE FUEL - FIREWALL SHUTOFF VALVE GROUND IMPROVEMENT
TITLE FUEL - FIREWALL SHUTOFF VALVE GROUND IMPROVEMENT EFFECTIVITY MODEL SERIAL NUMBERS 525 (CJ1+) -0680, -0685 thru -0799 525A (CJ2+) -0417, -0439 thru -0524 525B (CJ3) -0263, -0294 thru -0414 REASON
More informationSERVICE BULLETIN. COMPLIANCE MANDATORY. This service bulletin must be accomplished at the next 100-hour or 12-month (annual-type) inspection.
TITLE EQUIPMENT/FURNISHINGS - SEAT BELT BRACKET INSPECTION EFFECTIVITY MODEL SERIAL NUMBERS 120 8000 thru 15075 140 8000 thru 15075 REASON Cessna Aircraft Company wishes to update the seat belt bracket
More informationSERVICE LETTER REVISION TRANSMITTAL
REVISION TRANSMITTAL TO: Cessna Distributors, Multi-Engine Authorized Service Facilities, and CPC's SUBJECT: Multi-Engine Service Letter Revision 1: Hydraulic Power Pack Inspection REASON To add a coarse-threaded
More informationSERVICE LETTER. SERIAL NUMBERS 210 & T thru P thru P
TITLE SERVICE LETTER WINGS - LOWER MAIN SPAR CAP INSPECTION EFFECTIVITY REASON MODEL SERIAL NUMBERS 210 & T210 21058819 thru 21065009 P210 P2100001 thru P2100874 Reports have been received of cracks found
More informationSERVICE BULLETIN REVISION TRANSMITTAL
REVISION TRANSMITTAL This sheet transmits Revision 1 to, which: A. Adds HDWR kit to the MATERIAL INFORMATION section. NOTE: This revision replaces the original issue of in its entirety. REVISION COMPLIANCE
More informationSERVICE BULLETIN. EFFECTIVITY SERIAL NUMBERS 680 (Citation Sovereign) thru (Citation Sovereign+) thru -0549
TITLE DOORS - CABIN DOOR SUPPORT STRUT FITTING MODIFICATION EFFECTIVITY MODEL SERIAL NUMBERS 680 (Citation Sovereign) -0001 thru -0349 680 (Citation Sovereign+) -0501 thru -0549 REASON The equivalent of
More informationSERVICE BULLETIN REVISION TRANSMITTAL
REVISION TRANSMITTAL This sheet transmits Revision 1 to, which: A. Rearranges the sub-steps in Step 5 for better flow. NOTE: There are no technical changes in Step 5. B. Adds Steps 6 thru 9 to the Accomplishment
More informationSERVICE BULLETIN. This service bulletin provides parts and instructions to install fuel caps that have a locking feature.
TITLE FUEL - LOCKING FUEL CAP INSTALLATION EFFECTIVITY MODEL SERIAL NUMBERS 510 (Citation Mustang) -0001 and On NOTE: If the marketing designation for your airplane does not appear in the EFFECTIVITY section,
More informationSERVICE BULLETIN REVISION
Revision 1 REVISION TRANSMITTAL SHEET This sheet transmits Revision 1 to, which: A. Adds a Note to the EFFECTIVITY section and Step 1 to the ACCOMPLISHMENT INSTRUCTIONS section to include a reference to
More informationSingle Engine MODIFICATION KIT
Single Engine MODIFICATION KIT TITLE SECURITY LOCK INSTALLATION EFFECTIVITY Model Serial Numbers 172R 17280001 and On 172S 172S8001 and On 182S 18280001 thru 18280944 182T 18280945 and On T182T T18208001
More information41001 thru incorporating a retrofitted LA nose strut,
Service Newsletter SNL08-15 TITLE LA71325000 NOSE STRUT ASSEMBLY SEALS REPLACEMENT TO Cessna Distributors, Service Stations MODELS AFFECTED Model 300/LC40-550FG Serial Numbers 41001 thru 40079 incorporating
More informationSERVICE LETTER. Multi-engine TITLE NACELLES/PYLONS - NACELLE FITTING INSPECTION EFFECTIVITY
TITLE NACELLES/PYLONS - NACELLE FITTING INSPECTION EFFECTIVITY REASON MODEL 402C 414A SERIAL NUMBERS 402C0001 thru 402C1020 that have SK402-47 - Lower Front Wing Spar Cap Inspection/Modification (Original
More informationSERVICE BULLETIN SERIAL NUMBERS. The equivalent of this service bulletin has been incorporated on production airplanes and On.
TITLE FUSELAGE - TAILCONE GROUND RECEPTACLE INSTALLATION EFFECTIVITY MODEL SERIAL NUMBERS 560-0539 thru -0649 REASON The equivalent of this service bulletin has been incorporated on production airplanes
More informationALERT SERVICE LETTER
Citation TITLE ALERT SERVICE LETTER ASL525-32-21 LANDING GEAR - TRANSMITTAL OF GOODRICH 2-1559-32-4, MAIN LANDING GEAR - BRAKE ASSEMBLY - P/N S 2-1559-1 AND 2-1559-2 - CESSNA CITATION AIRCRAFT - INTRODUCTION
More informationSERVICE KIT. TITLE McCAULEY 2A34C203/90DCA-2 TWO BLADED THREADLESS PROPELLER INSTALLATION
TITLE McCAULEY 2A34C203/90DCA-2 TWO BLADED THREADLESS PROPELLER INSTALLATION EFFECTIVITY: The following airplanes that are in a landplane, ski plane, seaplane, or amphibian configuration. MODEL SERIAL
More informationThe parts that follow are available from Cessna Parts Distribution through an appropriate Cessna Service Station.
Service Newsletter June 15, 2010 TITLE MECHANICAL AIR CONDITIONER COMPRESSOR DRIVER SHEAVE / PULLEY ALIGNMENT TO Cessna Distributors and Single Engine Service Stations MODELS AFFECTED The following airplanes
More informationSERVICE BULLETIN. To prevent the wing fuel boost pump wiring from chafing on the wing structure and/or fuel tube assemblies.
TITLE FUEL - WING FUEL BOOST PUMP WIRE ROUTING IMPROVEMENT EFFECTIVITY MODEL SERIAL NUMBERS 560-0001 thru -0538 REASON To prevent the wing fuel boost pump wiring from chafing on the wing structure and/or
More informationEFFECTIVITY Serial Numbers thru , 698
Conquest TITLE AILERON HINGE BRACKET REPLACEMENT EFFECTIVITY Model Serial Numbers 441 441-0001 thru 441-0349, 698 DESCRIPTION To install stainless-steel aileron hinge brackets as a replacement for aluminum
More informationSingle Engine Service Bulletin SEB08-4 Revision 1, Unision Industries SLICK 4200/4300/6200/6300 Magnetos Inspection.
Revision Transmittal April 27, 2009 TO: Cessna Distributors, Single Engine Service Stations and CPC's SUBJECT: Single Engine Service Bulletin SEB08-4 Revision 1, Unision Industries SLICK 4200/4300/6200/6300
More informationSERVICE BULLETIN SB
TITLE LIGHTS - LED POSITION, TAIL POSITION, AND ANTI-COLLISION (PTA) LIGHT INSTALLATION EFFECTIVITY MODEL SERIAL NUMBERS 560 (Citation Encore) -0539 thru -0707 560 (Citation Encore+) -0751 thru -0802 NOTE:
More informationSERVICE BULLETIN CERTIFICATION REQUIREMENTS - FOREIGN CERTIFICATION PLACARD INSTALLATION
TITLE CERTIFICATION REQUIREMENTS - FOREIGN CERTIFICATION PLACARD INSTALLATION EFFECTIVITY MODEL UNIT NUMBERS 550-1040 NOTE: This Service Bulletin may only be accomplished at a Cessna-owned or an authorized
More informationSERVICE LETTER. Model 1A162 Propeller, and the McCauley Fixed Pitch Propeller Service Manual.
September 4, 2009 TITLE MODEL 1A162/TCD6754 PROPELLER SERVICE INFORMATION UPDATE TO: FAA-Approved Propeller Repair Stations, Aircraft Manufacturers, Owners and Operators EFFECTIVITY Model 1A162 Propeller,
More informationRevision Transmittal Sheet
2 APPROVED WHITE IN LEARJET 31 RT 31-32-24 Revision Transmittal Sheet This page transmits Revision 1 to No. 31-32-24, Main Landing Gear Torque Link Replacement. Rework: No rework is required for aircraft
More informationFAA approval has been obtained on technical data in this publication that affects airplane type design.
Single Engine Service Bulletin January 28, 2008 TITLE ENGINE COWLING ALIGNMENT INSPECTION AND MODIFICATION EFFECTIVITY Model Serial Numbers 172R 17280725 thru 17281262 172S 172S8202 thru 172S10006 REASON
More informationSeptember 8, Cessna Distributors, Authorized Service Facilities, CPC's, CSTARS, ASR's, and affected Owners of Record
Service Newsletter September 8, 2011 SNL11-23 TITLE P&WC PROPELLER-SHAFT OIL SEAL MODIFICATION TO Cessna Distributors, Authorized Service Facilities, CPC's, CSTARS, ASR's, and affected Owners of Record
More informationSERVICE BULLETIN. The equivalent of this service bulletin has been incorporated on production airplanes and On.
TITLE ICE AND RAIN PROTECTION - WING ANTI-ICE SYSTEM IMPROVEMENT EFFECTIVITY MODEL SERIAL NUMBERS 525B -0002 thru -0012 The equivalent of this service bulletin has been incorporated on production airplanes
More informationSERVICE BULLETIN REVISION
Revision 1 REVISION TRANSMITTAL SHEET This sheet transmits Revision 1 to. A. Adds Sheet 4 to Figure 1. B. Adds instructions to make the cutouts in the stiffener on the upper engine cowl larger. NOTE: This
More informationSERVICE BULLETIN. NO.: 0713 Revision C. All Garmin Aviation Service Centers and Aircraft OEM Service Centers DATE: 29 May 2007
SERVICE BULLETIN NO.: 0713 Revision C TO: All Garmin Aviation Service Centers and Aircraft OEM Service Centers DATE: 29 May 2007 SUBJECT: GSM 85 Inspection Procedure REVISION B: Revision C changes some
More informationThe engine cowling installation and firewall should be inspected and modified as specified in this Service Bulletin.
Single Engine Service Bulletin August 25, 2008 TITLE ENGINE COWLING ALIGNMENT INSPECTION AND MODIFICATION EFFECTIVITY Model Serial Numbers 172R 17280001 thru 17280724 172S 172S8001 thru 172S8201 REASON
More informationMODIFICATION KIT. Serial Numbers 300 (LC40-550FG) thru (LC42-550FG) thru (LC41-550FG) thru
Single Engine MODIFICATION KIT MK400-71-01 TITLE ENGINE OIL COOLER WINTERIZATION MODIFICATION EFFECTIVITY Model Serial Numbers 300 (LC40-550FG) 40004 thru 40079 350 (LC42-550FG) 42001 thru 421018 400 (LC41-550FG)
More informationSERVICE LETTER. COMPLIANCE DISCRETIONARY. This service letter should be accomplished at a scheduled Check 1, Check 2, or HSI. LABOR HOURS KEY WORD
Citation SERVICE LETTER SL525C-71-01 TITLE POWER PLANT - TRANSMITTAL OF WILLIAMS INTERNATIONAL SERVICE BULLETIN ENGINE OIL BREATHER TUBE ASSEMBLY & FRONT BYPASS DUCT RH BOSS ASSEMBLY INSTALL EFFECTIVITY
More informationSERVICE LETTER TITLE EXHAUST - TRANSMITTAL OF LYCOMING SERVICE BULLETIN NO 627C, EXHAUST SYSTEM INSPECTION SERIAL NUMBERS
Single Engine MANDATORY SERVICE LETTER SEL-78-03 TITLE EXHAUST - TRANSMITTAL OF LYCOMING SERVICE BULLETIN NO 627C, EXHAUST SYSTEM INSPECTION EFFECTIVITY REASON MODEL T206H SERIAL NUMBERS T20608001 and
More informationSERVICE BULLETIN. The equivalent of this service bulletin has been incorporated on production airplanes and On. REASON
Citation TITLE SERVICE BULLETIN SB560XL-73-02 ENGINE FUEL AND CONTROL - TRANSMITTAL OF PRATT & WHITNEY CANADA SERVICE BULLETIN PW500-72-30290 TURBOFAN ENGINE HYDROMECHANICAL FUEL CONTROL - REPLACEMENT/MODIFICATION
More informationWARNING OPERATION OF AN ENGINE WITH A RESTRICTED OIL PASSAGE CAN CAUSE LOSS OF LUBRICATION AND SUBSEQUENT ENGINE FAILURE.
TELEDYNE CONTINENTAL AIRCRAFT ENGINE CRITICAL SERVICE BULLETIN Compliance Necessary To Maintain Safety CATEGORY 2 CSB96-2 FAA APPROVED SUBJECT: PURPOSE: CRANKCASE OIL PASSAGE INSPECTION TCM has verified
More informationSERVICE BULLETIN. To prevent the wing fuel boost pump wiring from chafing on the wing structure and/or fuel tube assemblies.
TITLE FUEL - WING FUEL BOOST PUMP WIRE ROUTING IMPROVEMENT EFFECTIVITY MODEL UNIT NUMBERS 500/501-0001 thru -0689 REASON To prevent the wing fuel boost pump wiring from chafing on the wing structure and/or
More informationCESSNA AIRCRAFT COMPANY
Page 1 2011-06-02 CESSNA AIRCRAFT COMPANY Amendment 39-16626 Docket No. FAA-2010-1243; Directorate Identifier 2010-CE-058-AD PREAMBLE Effective Date (a) This AD is effective May 26, 2011. Affected ADs
More informationSERVICE BULLETIN MANDATORY. SB , Rev Planning Information
SERVICE BULLETIN TITLE: STABILIZERS - INSPECTION/REPLACEMENT OF ELEVATOR BALANCE WEIGHT ASSEMBLIES SYNOPSIS OF CHANGE This Service Bulletin has been revised to add a balance weight inspection every 100
More information[Docket No. FAA ; Directorate Identifier 2010-CE-058-AD; Amendment ; AD ]
[Federal Register Volume 76, Number 77 (Thursday, April 21, 2011)] [Rules and Regulations] [Pages 22298-22301] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc
More informationService Bulletin. ATA 52-10: Passenger and Crew Doors Door Latching Assembly Upgrade
Service Bulletin Issued: 5 Oct 00 Models SR0 and SR ATA 5-10: Passenger and Crew Doors Door Latching Assembly Upgrade COMPLIANCE Optional: Accomplishment of this Service Bulletin is at the owner s option.
More information[Docket No. FAA ; Directorate Identifier 2010-CE-058-AD; Amendment ; AD ]
[Federal Register Volume 76, Number 91 (Wednesday, May 11, 2011)] [Rules and Regulations] [Page 27239] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc No: 2011-11260]
More informationSERVICE BULLETIN SB
TITLE COMMUNICATIONS - AUTOMATIC FLIGHT INFORMATION SYSTEM (AFIS) DATA MANAGEMENT UNIT (DMU) UPGRADE EFFECTIVITY MODEL SERIAL NUMBERS 750 (Citation X) -0001 thru -0283 The equivalent of this service bulletin
More informationSERVICE BULLETIN REVISION
Revision 7 REVISION TRANSMITTAL SHEET This sheet transmits Revision 7 to Service Bulletin. A. Replaces the AN960PD10L Washers with NAS1149D0316K Washers. B. Removes the optional Aviation Brake System antiskid
More informationSERVICE KIT thru , 631, 634, 675 R thru R F thru F FR thru FR
TITLE SEAT BELT AND SHOULDER HARNESS KIT INSTALLATION EFFECTIVITY MODEL SERIES SERIAL NUMBERS 182 33000 thru 18268368 182 613, 631, 634, 675 R182 R18200001 thru R18201973 F182 F18200001 thru F18200169
More informationService Bulletin No.: DAC Date Issued: February 18, 2000 Title: Starting Vibrator Battery Installation Page: 1 of 6
Title: Starting Vibrator Battery Installation Page: 1 of 6 1. ATA Code: 7410 2. Effectivity: DA20-C1 s/n C0001 up to and including C0102. 3. General: This service bulletin addresses the installation of
More informationCOMPLIANCE: As required by Kelly Aerospace Service Bulletin 033 (Attached)
TELEDYNE CONTINENTAL AIRCRAFT ENGINE CRITICAL SERVICE BULLETIN COMPLIANCE NECESSARY TO MAINTAIN SAFETY Category 2 CSB08-11 Technical Portions FAA Approved SUBJECT: Kelly Aerospace Power Systems Service
More informationALERT SERVICE BULLETIN PSL September 2015 Revision A, 6 October 2017
MODEL AFFECTED: 212 ALERT SERVICE BULLETIN 212-15-155 PSL 7000000123 15 September 2015 Revision A, 6 October 2017 SUBJECT: FUEL CHECK VALVE 209-062-607-001, INSPECTION AND REPLACEMENT OF HELICOPTERS AFFECTED:
More informationRevision Transmittal Sheet
b 2 APPROVED WHITE IN LEARJET 23/24/25, 28/29, 35/36 RT 0980 Revision Transmittal Sheet This page transmits Revision 1 to, Replacement of Air Conditioning Evaporator Assembly. Rework: No rework is required
More informationG600 PFD/MFD System Instructions for Continued Airworthiness as installed in
Instructions for Continued Airworthiness as installed in (Make and Model Airplane) Reg. No. S/N Dwg. Number: 190-00601-00 Rev. A Garmin Ltd. Or its subsidiaries c/o Garmin International, Inc. 1200 E. 151st
More informationAVIAT AIRCRAFT INC. P.O. Box South Washington Afton, WY USA Fax:
DATE: 18 December 2000 REVISION: Orig. AIRCRAFT: PITTS SPECIAL P.O. Box 1240 672 South Washington Afton, WY 83110 USA 307-886-3151 Fax: 307-885-9674 aviat@aviataircraft.com SUBJECT: Propeller Accumulator
More informationSERVICE BULLETIN SB
TITLE LIGHTS - LED TAIL POSITION LIGHT INSTALLATION EFFECTIVITY MODEL UNIT NUMBERS 500 (Citation) -0001 thru -0349 with SB500-33-07 incorporated 500 (Citation I) -0350 thru -0528 with SB500-33-07 incorporated,
More informationSERVICE BULLETIN TITLE ENGINE CONTROLS - FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC) SOFTWARE UPGRADE VERSION C10
Citation SB750-76-12 TITLE ENGINE CONTROLS - FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC) SOFTWARE UPGRADE VERSION C10 EFFECTIVITY REASON MODEL SERIAL NUMBERS 750 (Citation X) -0001 thru -0313 NOTE: Airplanes
More informationSERVICE BULLETIN. No. SB-AG-49 August 1, 2008 SEAT SUPPORT BRACKET INSPECTION AND REPAIR
THRUSH AIRCRAFT, INC. P.O. Box 3149 300 Old Pretoria Rd. Albany, GA 31706-3149 Product Support 229-883-1440 ext. 341 FAX 229-436-4856 jbays@thrushaircraft.com SERVICE BULLETIN No. SB-AG-49 August 1, 2008
More informationMANDATORY SERVICE BULLETIN NO. MSB
Page 1 of 4 MANDATORY SERVICE BULLETIN NO. MSB-40-064 I TECHNICAL DETAILS I.1 Category Mandatory I.2 Airplanes affected Type: DA 40 Serial Numbers: 40.934, 40.942 40.950 through 40.972 40.974, 40.984,
More informationSERVICE LETTER. Model C290D3/T53, C290D4/T5, and DCFUS290D10/T8 governors, and the McCauley Governors and Accumulators Service Manual.
March 22, 2010 TITLE NEW GOVERNOR MODEL SERVICE INFORMATION UPDATE TO: FAA-Approved Propeller and Governor Repair Stations EFFECTIVITY Model C290D3/T53, C290D4/T5, and DCFUS290D10/T8 governors, and the
More informationPart A Describes the procedure for the replacement of the Mitchell type tachometer. These parts are supplied in Kit A as described below.
Title: Superior Labs Tachometer Installation Page: 1 of 7 1. ATA Code: 7700 2. Effectivity: DA20-A1 (including DA20/100) aircraft serial numbers 10003 up to and including 10331. 3. General: This service
More informationSERVICE BULLETIN. Citation SB TITLE DOORS - WIDE DOOR INSTALLATION MODIFICATION
TITLE DOORS - WIDE DOOR INSTALLATION MODIFICATION EFFECTIVITY MODEL SERIAL NUMBERS 560 (Citation Encore) -0539 thru -0707 560 (Citation Encore+) -0751 thru -0815 NOTE: This modification may only be accomplished
More informationService Bulletin No.: D42L Rev 0 Date Issued: 06 June 2016 Title: GTX 33ES Installation Page: 1 of 6
Title: GTX 33ES Installation Page: 1 of 6 1. ATA Code: 3450 2. Effectivity: All DA42 aircraft with TCCA STC SA09-54 or FAA STC SA02725NY installed with Garmin GIA 63W (WAAS). 3. General: This Service Bulletin
More informationCIRRUS SR2X SB 2X R2. Service Bulletin. Issued: Revised: June 26, 2012 July 31, 2012
CIRRUS SR2X Service Bulletin Number: Issued: Revised: June 26, 2012 SNS SUBJECT: 57-40 ATTACH FITTINGS - Lower Landing Gear Attach Bracket Torque 1. COMPLIANCE Mandatory: Cirrus Design considers this Service
More information500W Series Instructions for Continued Airworthiness
Instructions for Continued Airworthiness Document Number 190-00357-65 Rev. B Garmin Ltd. Or its subsidiaries c/o Garmin International, Inc. 1200 E. 151st Street Olathe, Kansas 66062 USA Record of Revision
More informationService Bulletin No.: DAC Rev 3 Date Issued: October 27, 1999 Title: 2-Speed Electric Prime Fuel Pump Page: 1 of 8
Title: 2-Speed Electric Prime Fuel Pump Page: 1 of 8 1. ATA Code: 2820 2. Effectivity: DA20-C1 Aircraft from S/N C0001 up to and including S/N C0089 3. General: This service bulletin addresses the installation
More informationSNS SUBJECT: NOSE GEAR - Nose Landing Gear Assembly Inspection and Reinforcement
CIRRUS SR22 Service Bulletin Number: Issued: SNS SUBJECT: 32-20 NOSE GEAR - Nose Landing Gear Assembly Inspection and Reinforcement 1. COMPLIANCE Mandatory: Cirrus Design considers this Service Bulletin
More informationService Bulletin No.: DA Rev 0 Date Issued: 8 January, 1999 Title: Nose Gear Fork, Fatigue Page: 1 of 6
Title: Nose Gear Fork, Fatigue Page: 1 of 6 1. ATA Code: 3220 2. Effectivity: DA20-A1 aircraft. 3. General: As a result of hard landings, cracks have appeared in the nose landing gear fork of some aircraft.
More informationSUBJECT: MAIN ROTOR DRIVE, ENGINE-TO- TRANSMISSION DRIVE SHAFT RETAINING NUTS INSPECTION/REPLACEMENT
ALERT SERVICE BULLETIN 212-14-151 2 September 2014 Revision A, 13 December 2017 MODEL AFFECTED: 212 SUBJECT: MAIN ROTOR DRIVE, ENGINE-TO- TRANSMISSION DRIVE SHAFT RETAINING NUTS INSPECTION/REPLACEMENT
More informationMANDATORY SERVICE BULLETIN
CONTINENTAL MOTORS AIRCRAFT ENGINE MANDATORY SERVICE BULLETIN The Subject Matter Of The Service Bulletin Is Incorporated In Whole Or In Part In An FAA Issued Airworthiness Directive CATEGORY 1 TECHNICAL
More informationSERVICE BULLETIN FUEL - MODIFICATION OF THE ENGINE DRIVEN FUEL PUMP SYSTEM
Beech TITLE: FUEL - MODIFICATION OF THE ENGINE DRIVEN FUEL PUMP SYSTEM 1. Planning Information A. Effectivity (1) Airplanes Beechcraft Bonanza Model A36, Serials E-1946, E-2104, and E-2111 through E-3144;
More informationSERVICE BULLETIN REVISION TRANSMITTAL
REVISION TRANSMITTAL REASON This sheet transmits Revision 1 to, which: A. Adds instructions and parts to change the Pulselite controller for airplanes with the Pulselite feature. NOTE: This revision replaces
More informationALERT SERVICE LETTER ASL
Citation TITLE ALERT SERVICE LETTER ASL550-72-29 ENGINE - TRANSMITTAL OF P&WC SERVICE DOCUMENTS - INTERCOMPRESSOR BLEED VALVE/SERVO-VALVE-INSPECTION/REPLACEMENT OF EFFECTIVITY MODEL SERIAL NUMBERS 550
More informationService Bulletin No.: DAC Rev 0 Date Issued: 29 June 2017 Title: Removal of OAT/Clock AA Battery Page: 1 of 5
Title: Removal of OAT/Clock AA Battery Page: 1 of 5 1. ATA Code: 3100 2. Effectivity: All DA20-C1 aircraft with the M803-14V OAT/Clock installed. 3. General: Addresses a magnetic interference issue on
More informationPROPELLERS - PROPELLER SLIP RING MOUNTING PLATE INSPECTION AND REPAIR
Beechcraft TITLE: PROPELLERS - PROPELLER SLIP RING MOUNTING PLATE INSPECTION AND REPAIR 1. Planning Information A. Effectivity (1) Airplanes Airplanes that have accomplished installation of Hartzell STC
More informationCONTINENTAL AIRCRAFT ENGINE service bulletin
CONTINENTAL AIRCRAFT ENGINE service bulletin M83-3 Technical Portions are FAA-DER Approved 14 February, 1983 TO: SUBJECT: MODELS AFFECTED: Aircraft Manufacturers, Distributors, Dealers, Engine Overhaul
More informationSERVICE BULLETIN REVISION TRANSMITTAL
REVISION TRANSMITTAL This sheet transmits Revision 2 to, which: A. Adds the CI401-460 GPS Antenna to Step 10A and Step 10B. B. Adds the CI401-460 GPS Antenna to Figure 5. C. Adds the CI401-460 GPS Antenna
More informationCRITICAL SERVICE BULLETIN Compliance Necessary to Maintain Safety
TELEDYNE CONTINENTAL AIRCRAFT ENGINE CRITICAL SERVICE BULLETIN Compliance Necessary to Maintain Safety CATEGORY 2 CSB04-6 TECHNICAL PORTIONS FAA APPROVED SUBJECT: INSPECTION OF TSIO-550 AND TSIOL-550 ENGINES
More informationMANDATORY SERVICE BULLETIN NO. MSB40-046/3 NO. MSBD4-046/3
Page 1 of 5 MANDATORY SERVICE BULLETIN NO. MSB40-046/3 Supersedes MSB 40-046/2 NO. MSBD4-046/3 Supersedes MSB D4-046/2 I TECHNICAL DETAILS I.1 Category Mandatory. I.2 Airplanes affected Type: DA 40 DA
More informationSERVICE BULLETIN REVISION TRANSMITTAL
REVISION TRANSMITTAL This sheet transmits Revision 2 to, which: A. Adds the reference to Figure 7, Sheet 1 and Sheet 2 to Step 10D. B. Adds Step 10D(7). C. Removes the After Modification view for PN343
More informationCal Pacific Airmotive, Inc.
Cal Pacific Airmotive, Inc. Title: Inspection of Flight Control System Mandatory Service Bulletin North American Aviation P-51B, P-51C, P-51D, P-51K, F-51D, F-51K S.B. No. P51-001 Revision: 0 Issue Date
More informationAccepted Means of Compliance; Airworthiness Standards: Normal Category. SUMMARY: This document announces the availability of 63 Means of Compliance
This document is scheduled to be published in the Federal Register on 05/11/2018 and available online at https://federalregister.gov/d/2018-09990, and on FDsys.gov [4910-13] DEPARTMENT OF TRANSPORTATION
More informationRECOMMENDED SERVICE BULLETIN NO. RSB /2
Page 1 of 4 RECOMMENDED SERVICE BULLETIN NO. RSB 42-072/2 SUPERSEDES RSB 42-072/1 I TECHNICAL DETAILS I.2 Category Recommended. I.3 Airplanes affected Type: DA 42 / DA 42 M powered by TAE engines Serial
More informationDiamond ALERT SERVICE BULLETIN AIRCRAFT
Title: Throttle Cables, Replacement Page: 1 of 7 1. ATA Code: 7610 2. Effectivity: DA 20 Katana Aircraft S/N 10002 through 10300. 3. General: This service bulletin supersedes S.B. #DA20-76-01A Rev 4. A
More informationAlert Service Bulletin
Alert Service Bulletin 2900 Selma Highway Montgomery, AL 36108 USA Tel: 334-386-5400 Fax: 334-386-5450 1. Planning Information A. Effectivity (1) All Hartzell Engine Technologies LLC (HET) turbochargers:
More informationService Bulletin No.: DAC Rev 2 Date Issued: Oct 04, 2016 Title: Installation of LED Anti-Collision and Position light Assembly
Page: 1 of 9 1. ATA Code: 3340 2. Effectivity: DA20-C1 Aircraft S/N C0001 to C0647 3. General: This Service Bulletin addresses the replacement of Whelen s Anti- Collision /Position Light assembly (A600PG-14/A600PR-14)
More informationSERVICE LETTER. Hartzell Alert Service Bulletin No. 069, 200F, 201F, 202F Fuel Pump Leak Inspection And Diaphragm
Single Engine SERVICE LETTER SEL-73-06 TITLE ENGINE FUEL AND CONTROL - TRANSMITTAL OF HARTZELL ALERT SERVICE BULLETIN NO. 069, 200F, 201F, 202F FUEL PUMP LEAK INSPECTION AND DIAPHRAGM REPLACEMENT EFFECTIVITY
More informationService Bulletin SB 07-03
Service Bulletin SB 07-03 BRS-600 Pick-up Collar Support Replacement Compliance Mandatory: BRS considers this service bulletin to be mandatory. Accomplish this service bulletin within the next 25 flight
More informationService Bulletin No.: DAC Rev. 3 Date Issued: August 28, 2002 Title: Sensenich Propeller Installation Page: 1 of 8
Title: Sensenich Propeller Installation Page: 1 of 8 1. ATA Code: 6100 2. Effectivity: DA20-C1 s/n C0001 up to and including C0192. 3. General: This service bulletin addresses the Sensenich propeller installation.
More informationSERVICE BULLETIN. No. SB-AG-54 Revision IR; 6/6/2011 S2R-T660 ELEVATOR PUSH-PULL TUBE END FITTING INSPECTION
THRUSH AIRCRAFT, INC. P.O. Box 3149 300 Old Pretoria Rd. Albany, GA 31706-3149 Product Support 229-789-0439 FAX 229-439-9790 jbays@thrushaircraft.com SERVICE BULLETIN No. SB-AG-54 Revision IR; 6/6/2011
More information