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

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

SERVICE LETTER REVISION TRANSMITTAL

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

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

SERVICE LETTER REVISION TRANSMITTAL

SERVICE BULLETIN REVISION TRANSMITTAL

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

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

SERVICE BULLETIN REVISION TRANSMITTAL

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

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

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

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

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

Service Information Letter

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

ALERT SERVICE LETTER

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

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

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

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

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 SB

Single Engine. Service Bulletin TITLE ENGINE MOUNT BRACKET INSPECTION

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

SERVICE BULLETIN CERTIFICATION REQUIREMENTS - FOREIGN CERTIFICATION PLACARD INSTALLATION

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

SERVICE LETTER. COMPLIANCE DISCRETIONARY. This service letter should be accomplished at a scheduled Check 1, Check 2, or HSI. LABOR HOURS KEY WORD

SERVICE BULLETIN REVISION

SERVICE LETTER. Multi-engine MEL TITLE NACELLES/PYLONS - ENGINE BEAM INSPECTION

SERVICE BULLETIN MANDATORY. SB , Rev Planning Information

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

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

Single Engine MODIFICATION KIT

SERVICE BULLETIN SB

PROPELLERS - PROPELLER SLIP RING MOUNTING PLATE INSPECTION AND REPAIR

SERVICE BULLETIN REVISION

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

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

SERVICE BULLETIN SB

SERVICE BULLETIN. Citation SB TITLE DOORS - WIDE DOOR INSTALLATION MODIFICATION

SERVICE BULLETIN REVISION TRANSMITTAL

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

SERVICE BULLETIN REVISION TRANSMITTAL

EFFECTIVITY Serial Numbers thru , 698

SERVICE BULLETIN REVISION

SERVICE BULLETIN REVISION TRANSMITTAL

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

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

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

Revision Transmittal Sheet

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

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

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

SERVICE LETTER. REASON To incorporate new software changes to the engine electronic control and engine diagnostics unit.

41001 thru incorporating a retrofitted LA nose strut,

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

SERVICE LETTER. Hartzell Alert Service Bulletin No. 069, 200F, 201F, 202F Fuel Pump Leak Inspection And Diaphragm

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

SNS SUBJECT: NOSE GEAR - Nose Landing Gear Assembly Inspection and Reinforcement

Cessna Aircraft Company: Amendment ; Docket No. FAA ; Directorate Identifier 2012-NM-020-AD.

Alert Service Bulletin

TEMPORARY REVISION NUMBER

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

ALERT SERVICE BULLETIN NO.

TEMPORARY REVISION NUMBER

SERVICE BULLETIN FLIGHT CONTROLS - INSTALL FLAP INSPECTION ACCESS PANELS ON CERTAIN AERO CENTER PRODUCTS

MANDATORY SERVICE BULLETIN NO. MSB

CIRRUS SR2X SB 2X R2. Service Bulletin. Issued: Revised: June 26, 2012 July 31, 2012

TEMPORARY REVISION NUMBER

1154B. Piper Aircraft, Inc Piper Drive Vero Beach, Florida, U.S.A Date: March 28, 2007 (S)

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

MANDATORY SERVICE BULLETIN NO. MSB40-046/3 NO. MSBD4-046/3

201F Fuel Pump Valve Housing Cap Screw Replacement

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

REASON FOR REVISION: To clarify effectivity by including RAM P/N cross reference. INTRODUCTION:

Service Bulletin SB 07-03

Service Bulletin No: Ref No: 49 Modification No: EC ATA Chapter: 32

The Subject Matter Of This Service Bulletin Is Incorporated In Whole Or In Part In An FAA Issued Airworthiness Directive

SERVICE BULLETIN TITLE AIR CONDITIONING - R134A AIR CONDITIONER SYSTEM INSTALLATION FOR AIRPLANES EQUIPPED WITH G1000 AND 867 SHP ENGINE

SUBJECT: FUEL FITTING P/N AND , VERIFICATION OF.

PILATUS AIRCRAFT LTD. CH-6371 STANS, SWITZERLAND SERVICE BULLETIN SERVICE BULLETIN NO: REF NO: 184 MODIFICATION NO: ATA CHAPTER: 32

AVIAT AIRCRAFT INC. P.O. Box South Washington Afton, WY USA Fax:

CSB 665A TECHNICAL PORTIONS FAA APPROVED

Service Bulletin No: Ref No: 170 Modification No: EC ATA Chapter: 53

RECOMMENDED SERVICE BULLETIN NO. RSB /2

SERVICE BULLETIN OPTIONAL SB Beech. 1. Planning Information FUSELAGE - BATTERY DRAIN MAST REMOVAL. A. Effectivity

MANDATORY SERVICE BULLETIN

Director P. O. Box 1904 Service Engineering Operations Dearborn, Michigan Ford Customer Service Division

SUBJECT: MAIN ROTOR DRIVE, ENGINE-TO- TRANSMISSION DRIVE SHAFT RETAINING NUTS INSPECTION/REPLACEMENT

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

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

PILATUS AIRCRAFT LTD. CH-6371 STANS, SWITZERLAND SERVICE BULLETIN SERVICE BULLETIN NO: REF NO: 106 MODIFICATION NO: ATA CHAPTER: 28

FOR THE MOST RECENT REVISION LEVEL OF THIS SERVICE BULLETIN.

ALERT SERVICE LETTER ASL

Table 1: Alternator Models ES (CMI ), ALX-9524 (CMI ), ALX-9524R, & ALV-9610 Affected Serial Numbers

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

Service Bulletin. ATA 27-00: Flight Controls Rudder-Aileron Interconnect Modification

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

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

Transcription:

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 206H 20608350 thru 20608353 T206H T20609075 thru T20609105, T2069107, T20609110 thru T20609133 Group B Airplanes: The following airplane serials that have had a replacement 1243600-1 Drag Link Assembly installed that was purchased from Cessna Aircraft Company between August 1, 2012 and July 17, 2014. MODEL SERIAL NUMBERS 205 205-0001 thru 205-0577, 641, 648 206 206-0001 thru 206-0275 (T)U206 U206-0276 thru U206-1444, U20601445 thru U20607020, 676 (T)P206 P206-0001 thru P206-0603, P20600604 thru P20600647 (T)207 20700001 thru 20700788 206H 20608001 thru 20608349 T206H T20608001 thru T20609074 Also affected are all 1243600-1 Drag Link Assemblies in service facility stock that were purchased from Cessna Aircraft Company between August 1, 2012 and July 17, 2014. REASON Cessna has received reports of failure of the nose gear drag link. Failure of the nose gear drag link caused the nose landing gear to collapse forward and the propeller to strike the ground. DESCRIPTION This service letter provides parts and instructions to remove and replace the nose gear drag link assembly. COMPLIANCE MANDATORY. This service letter must be accomplished within 25 flight hours. August 15, 2014 Page 1 of 3 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-5800 This document contains technical data and is subject to U.S. export regulations. This information has been exported from the United States in accordance with export administration regulations. Diversion contrary to U.S. law is prohibited. ECCN: 9E991 COPYRIGHT 2014

SERVICE LETTER MATERIAL AVAILABILITY Order the parts below to remove and replace the nose gear drag link assembly:: NEW P/N QUANTITY KEY WORD OLD P/N INSTRUCTIONS/ DISPOSITION MS21042L5 1 Nut Same Discard MS21042L6 1 Nut Same Discard 1243600-1 1 Drag Link Assembly Same Return to Cessna NOTE: To receive warranty credit: Group A airplanes must return the removed drag link assembly to Cessna within the credit expiration dates shown below. Group B airplanes must return the removed drag link assembly to Cessna with proof of sale within the credit expiration dates shown below. REFERENCES Model 206H/T206H Maintenance Manual Model 200 Series Service Manual (1960-1965) Model 200 Series Service Manual (1966-1968) Model 206 & T206 Series Service Manual (1969-1976) Model 206 & T206 Series Service Manual (1977-1986) Model 207 & T207 Series Service Manual (1968-1984) ACCOMPLISHMENT INSTRUCTIONS NOTE: Group A Airplanes, go directly to Step 2. Group B Airplanes go to Step 1. 1. (Group B Airplanes only) Look at the airplane paperwork to see if the airplane has had a replacement 1243600-1 Drag Link Assembly installed that was purchased from Cessna Aircraft Company between August 1, 2012 and July 17, 2014. A. If a suspect replacement 1243600-1 Drag Link Assembly was installed on your airplane or if you cannot tell for sure if a suspect replacement 1243600-1 Drag Link Assembly was installed on your airplane,gotostep2. B. If a suspect replacement 1243600-1 Drag Link Assembly was not installed on your airplane, go to Step 5. 2. Prepare the airplane for maintenance. A. Make sure that the airplane is electrically grounded. B. Make sure that all switches are in the OFF/NORM position. C. Disconnect electrical power from the airplane. (1) Disconnect external electrical power. (2) Disconnect the airplane battery. D. Attach maintenance warning tags to the battery and external power receptacle that have "DO NOT CONNECT ELECTRICAL POWER - MAINTENANCE IN PROGRESS" writtenonthem. 3. Remove and replace the 1243600-1 Drag Link Assembly. (Refer to the applicable sections of the maintenance/service manual.) 4. Remove the maintenance warning tags and connect the airplane battery. Page 2 August 15, 2014

SERVICE LETTER 5. Make an entry in the airplane logbook that states compliance and method of compliance with this service letter. August 15, 2014 Page 3

OWNER ADVISORY TITLE LANDING GEAR - DRAG LINK REPLACEMENT TO: Cessna 206H, T206H, 205, 206, (T)U206, (T)P206, and (T)207 Owners REASON This owner advisory is to inform you that has been issued. Cessna has received reports of failure of the nose gear drag link. Failure of the nose gear drag link caused the nose landing gear to collapse forward and the propeller to strike the ground. DESCRIPTION provides parts and instructions to remove and replace the nose gear drag link assembly. COMPLIANCE MANDATORY. This service letter must be accomplished within 25 flight hours. LABOR HOURS 1.8 man-hours to remove and replace the nose gear drag link assembly. WARRANTY For all airplanes identified within the serial effectivity: Applicable parts credit and a labor allowance credit of 1.8 man-hours per airplane will be provided to remove and replace the nose gear drag link assembly. NOTE: To receive warranty credit: Group A airplanes must return the removed drag link assembly to Cessna within the credit expiration dates shown below. Group B airplanes must return the removed drag link assembly to Cessna with proof of sale within the credit expiration dates shown below. Freight will be credited at the most economical method unless pre-approved by Cessna. To receive credit, the work must be completed and a warranty claim submitted by a Cessna Authorized Service Facility within 30 calendar days of service bulletin compliance before the credit expiration dates shown below. Domestic... August 15, 2015 International... August 15, 2015 Please contact a Cessna Authorized Service Facility for detailed information and arrange to have Cessna service letter accomplished on your airplane. Access the QR code for the instructional video link that follows or use the URL address: August 15, 2014 Page 1 of 2 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-5800 This document contains technical data and is subject to U.S. export regulations. This information has been exported from the United States in accordance with export administration regulations. Diversion contrary to U.S. law is prohibited. ECCN: 9E991 COPYRIGHT 2014

Select this link: OWNER ADVISORY http://textron.vo.llnwd.net/o25/ces/customerservice//.html NOTE: As a convenience, service documents are now available online to all our customers through a simple, free-of-charge registration process. If you would like to sign up, please visit the "Customer Support Login" link at www.cessna.com to register. Page 2 August 15, 2014