SERVICE BULLETIN. This service bulletin provides parts and instructions to install fuel caps that have a locking feature.
|
|
- Lynette Peters
- 6 years ago
- Views:
Transcription
1 TITLE FUEL - LOCKING FUEL CAP INSTALLATION EFFECTIVITY MODEL SERIAL NUMBERS 510 (Citation Mustang) and On NOTE: If the marketing designation for your airplane does not appear in the EFFECTIVITY section, this service document does not apply to your airplane. REASON Customers have requested a locking fuel cap installation. DESCRIPTION This service bulletin provides parts and instructions to install fuel caps that have a locking feature. COMPLIANCE OPTIONAL. This service bulletin can be accomplished at the discretion of the owner. A service bulletin published by Cessna Aircraft Company may be recorded as completed in an aircraft log only when the following requirements are satisfied: 1) The mechanic must complete all of the instructions in the service bulletin, including the intent therein. 2) The mechanic must correctly use and install all applicable parts supplied with the service bulletin kit. Only with written authorization from Cessna Aircraft Company can substitute parts or rebuilt partsbeusedtoreplacenewparts. 3) The mechanic or airplane owner must use the technical data in the service bulletin only as approved and published. 4) The mechanic or airplane owner must apply the information in the service bulletin only to aircraft serial numbers identified in the Effectivity section of the bulletin. 5) The mechanic or airplane owner must use maintenance practices that are identified as acceptable standard practices in the aviation industry and governmental regulations. No individual or corporate organization other than Cessna Aircraft Company is authorized to make or apply any changes to a Cessna-issued service bulletin, service letter, or flight manual supplement without prior written consent from Cessna Aircraft Company. Cessna Aircraft Company is not responsible for the quality of maintenance performed to comply with this document, unless the maintenance is accomplished at a Cessna-owned Citation Service Center. FLIGHT CREW OPERATIONS No Changes Page1of4 Cessna Aircraft Company, Citation Marketing Division, P.O. Box 7706, Wichita, KS 67277, U.S.A , Fax COPYRIGHT 2008
2 APPROVAL Cessna received FAA approval for the technical data in this publication that changes the airplane type design. This information is an amendment to the applicable maintenance manual. MANPOWER MATERIAL - Cost and Availability WORK PHASE MAN-HOURS Modification * PART NUMBER AVAILABILITY COST * * * Refer to the Manpower, Material - Cost and Availability, and Warranty sections in the attached Service Bulletin Supplemental Data sheet. CHANGE IN WEIGHT AND BALANCE Negligible REFERENCES Cessna Model 510 Maintenance Manual PUBLICATIONS AFFECTED Cessna Model 510 Illustrated Parts Catalog ACCOMPLISHMENT INSTRUCTIONS 1. Prepare the airplane for maintenance. A. Make sure that all switches are in the OFF/NORM position. B. Disconnect electrical power from the airplane. (1) Disconnect the airplane battery. (2) Disconnect external electrical power. C. Attach maintenance warning tags to the battery and external power receptacle that have "DO NOT CONNECT ELECTRICAL POWER - MAINTENANCE IN PROGRESS" writtenonthem. 2. Connect the static ground cable between a known good ground point and the airplane. 3. Remove and discard one Filler Assembly, one Gasket, and 12 MS24694C49 Screws from the left wing. 4. (Refer to Figure 1, Detail A.) Install one Locking Fuel Cap and one Gasket with 12 MS24694C49 Screws on the left wing. 5. Remove and discard one Filler Assembly, one Gasket, and 12 MS24694C49 Screws from the right wing. 6. (Refer to Figure 1, Detail A.) Install one Locking Fuel Cap and one Gasket with 12 MS24694C49 Screws on the right wing. Page 2
3 7. Fill the left and right wings to the bottom of the locking fuel caps with fuel and allow the airplane to sit for 12 hours. 8. Make sure that the fuel has not seeped around the locking fuel caps. 9. Record that this service bulletin has been completed. A. Complete a Maintenance Transaction Report. B. Put a copy of the completed Maintenance Transaction Report in the airplane logbook. C. Send a copy of the completed Maintenance Transaction Report to: CESCOM, P.O. Box 7706, Wichita, KS MATERIAL INFORMATION Order the kit below to install this modification. NEW P/N QUAN- TITY KEY WORD OLD P/N INSTRUCTIONS/ DISPOSITION 1 Kit, consisting of the following parts: Locking Fuel Cap Discard Gasket Same Discard MS24694C49 24 Screw Same Discard 1 Instructions Page 3
4 Figure 1. Locking Fuel Cap Installation (Sheet 1) Page 4
5 TITLE SUPPLEMENTAL DATA FUEL - LOCKING FUEL CAP INSTALLATION EFFECTIVITY MODEL SERIAL NUMBERS 510 (Citation Mustang) and On NOTE: If the marketing designation for your airplane does not appear in the EFFECTIVITY section, this service document does not apply to your airplane. MANPOWER WORK PHASE Modification MAN-HOURS As Necessary MATERIAL - Cost and Availability PART NUMBER AVAILABILITY COST * * * Please contact Citation Parts Distribution for current cost and availability of parts listed in this service bulletin. Phone at (Domestic) or (International). Send to: citationparts@cessna.textron.com or telefax at Based on availability and lead times, parts may require advanced scheduling. In cases where the required part(s) are available as exchange, order the exchange part and, upon completion, expedite the return of the removed core to avoid return penalties. Contact the Citation Parts Distribution Sales Desk for availability of exchange parts. Page1of1 Cessna Aircraft Company, Citation Marketing Division, P.O. Box 7706, Wichita, KS 67277, U.S.A , Fax COPYRIGHT 2008
6
SERVICE 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 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 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 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 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 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. 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. 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 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. 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 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. 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. Adds HDWR kit to the MATERIAL INFORMATION section. NOTE: This revision replaces the original issue of in its entirety. REVISION COMPLIANCE
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 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 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 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. 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 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 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 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 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 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 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 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 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 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 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 informationDESCRIPTION This service document provides instructions to inspect the Pre-2014 LH yokes.
PRE-2014 LH3600-5 YOKE SERVICE BULLETIN Date: 8 March 2018 REASON: Airglas has received 4 reports of the LH4000 yoke (PN LH3600-5) of the welds shearing off the outboard arm of the yoke. The common thread
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 informationService 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 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 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 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 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 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 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 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 informationSUBJECT: Single Engine Service Bulletin SB Revision 1: Cosmetic Window Repair
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
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 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 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 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 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 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 informationSERVICE BULLETIN. 560XL (Citation XLS+) thru -6055, thru -6066, thru -6071, thru -6077
Citation TITLE SB560XL-76-04 ENGINE CONTROLS - TRANSMITTAL OF PRATT & WHITNEY CANADA (P&WC) 30434 TURBOFAN ENGINE - ELECTRONIC ENGINE CONTROL/REPLACEMENT-MODIFICATION and P&WC 30438 TURBOFAN ENGINE ELECTRONIC
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 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 LETTER. REASON To incorporate new software changes to the engine electronic control and engine diagnostics unit.
Citation SERVICE LETTER SL680-76-02 TITLE ENGINE CONTROLS - TRANSMITTAL OF PRATT AND WHITNEY CANADA, ELECTRONIC ENGINE CONTROL AND ENGINE DIAGNOSTICS UNIT - REPLACEMENT/MODIFICATION EFFECTIVITY MODEL SERIAL
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 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 informationCessna Aircraft Company: Amendment ; Docket No. FAA ; Directorate Identifier 2012-NM-020-AD.
2013-09-11 Cessna Aircraft Company: Amendment 39-17453; Docket No. FAA-2012-1001; Directorate Identifier 2012-NM-020-AD. (a) Effective Date. This AD is effective July 5, 2013. (b) Affected ADs None. (c)
More information*MANDATORY SERVICE BULLETIN*
NUMBER: SB11-12 REVISION: 00 DATE: 08/05/2011 EFFECTIVITY: KODIAK 100 Series Aircraft Serial Numbers: 100-0001 through 100-0054. KO D I A K SUBJECT: FUEL QUANTITY CALIBRATION PROCEDURES SUMMARY: It has
More informationSERVICE LETTER. Multi-engine MEL TITLE NACELLES/PYLONS - ENGINE BEAM INSPECTION
TITLE NACELLES/PYLONS - ENGINE BEAM INSPECTION EFFECTIVITY MODEL SERIAL NUMBERS 402C 402C0001 thru 402C1020 414A 414A0001 thru 414A1212 REASON Cracks have been discovered on some engine beams. The cracks
More informationService Bulletin No: Ref No: 49 Modification No: EC ATA Chapter: 32
PILATUS AIRCRAFT LTD, STANS, SWITZERLAND Service Bulletin No: 32-006 Ref No: 49 Modification No: EC-10-0569 ATA Chapter: 32 LANDING GEAR - MAIN GEAR AND DOORS REPLACEMENT OF THE WASHER ON THE MAIN LANDING
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 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 informationCIRRUS SR2X SB 2X Service Bulletin. Issued: February 27, SNS SUBJECT: TEMPERATURE CONTROL - Cabin Air Coupler Actuator Rigging
CIRRUS SR2X Service Bulletin Number: Issued: February 27, 2012 SNS SUBJECT: 21-60 TEMPERATURE CONTROL - Cabin Air Coupler Actuator Rigging 1. COMPLIANCE Recommended, On Condition: Accomplish this Service
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 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 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 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 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 informationS E R V I C E B U L L E T I N
VALVE ASSEMBLY. RESERVOIR VENT P/N 1. Planning Information A. Effectivity This service bulletin is applicable to the following Valve Assembly Essex P/N (Boeing P/N) Serial No. Application (S271N301-2)
More informationService Bulletin No: Ref No: 165 Modification No: EC ATA Chapter: 21
PILATUS AIRCRAFT LTD. STANS, SWITZERLAND Service Bulletin No: 21-012 Ref No: 165 Modification No: EC-14-0359 ATA Chapter: 21 AIR CONDITIONING - COOLING INSTALL A COVER ASSEMBLY TO THE COMPRESSOR TO PROTECT
More informationSERVICE BULLETIN THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN
M20-327 SUBJECT: Mooney wing to fuselage attach fitting plates part number 340035-50 and 340035-502 MODELS/ SN M20R - 29-0523 thru 29-0525 AFFECTED: M20TN - 3-042, 3-043 TIME OF COMPLIANCE: INTRODUCTION:
More informationService Bulletin No: Ref No: 170 Modification No: EC ATA Chapter: 53
PILATUS AIRCRAFT LTD. STANS, SWITZERLAND Service Bulletin No: 53-014 Ref No: 170 Modification No: EC-15-0854 ATA Chapter: 53 FUSELAGE - MAIN FRAMES REPLACE THE LEFT AND / OR RIGHT FRAME 11 FITTINGS 1.
More informationTable 1: Alternator Models ES (CMI ), ALX-9524 (CMI ), ALX-9524R, & ALV-9610 Affected Serial Numbers
2900 Selma Highway Montgomery, AL 36108 USA Tel: 334-386-5400 Fax: 334-386-5450 Service Bulletin Alternator Inspection for Burrs in the Rotor Shaft Hex Key Socket 1. Planning Information A. Effectivity
More informationPOWER TURBINE RPM (N2) STEADY STATE OPERATION AVOIDANCE, INTRODUCTION OF.
SERVICE BULLETIN 206L-08-150 20 May 2008 Revision A, 3 March 2009 Revision B, 25 July 2018 MODEL AFFECTED: 206L-1, 206L-3, and 206 L-4 SUBJECT: HELICOPTERS AFFECTED: COMPLIANCE: POWER TURBINE RPM (N2)
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 Information Letter
Service Information Letter The technical content of this letter is FAA Approved Letter No. A-110B Issue Date: Dec. 20, 2004 RECOMMENDED SERVICE/INSPECTION FOR MODEL 91E93-1 & 91E92-1 HEATER FUEL PUMP REASON
More informationAVIAT AIRCRAFT INC. P.O. Box South Washington Afton, WY USA Fax:
DATE: 7 February 2000 REVISION: Orig. AIRCRAFT: PITTS SPECIAL S-2C P.O. Box 1240 672 South Washington Afton, WY 83110 USA 307-886-3151 Fax: 307-885-9674 aviat@aviataircraft.com SUBJECT: Elevator Forward
More informationFOR THE MOST RECENT REVISION LEVEL OF THIS SERVICE BULLETIN.
2900 Selma Highway Montgomery, AL 36108 USA Tel: 334-386-5400 Fax: 334-386-5450 SERVICE BULLETIN 1. Planning Information A. Effectivity (1) Plane-Power Jasco series alternators manufactured by Hartzell
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 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 informationService Bulletin No: Ref No: 331 Modification No: EC , EC ATA Chapter: 27
PILATUS AIRCRAFT LTD, STANS, SWITZERLAND Service Bulletin No: 27-021 Ref No: 331 Modification No: EC-14-0549, EC-14-0714 ATA Chapter: 27 FLIGHT CONTROLS - AILERON CONTROL SYSTEM AILERON TAB COUNTER BALANCE
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 TITLE AIR CONDITIONING - R134A AIR CONDITIONER SYSTEM INSTALLATION FOR AIRPLANES EQUIPPED WITH G1000 AND 867 SHP ENGINE
TITLE AIR CONDITIONING - R134A AIR CONDITIONER SYSTEM INSTALLATION FOR AIRPLANES EQUIPPED WITH G1000 AND 867 SHP ENGINE EFFECTIVITY DESCRIPTION MODEL 208B SERIAL NUMBERS 208B5000 and On To provide parts
More informationFJ44 SERVICE BULLETIN
Engine Indicating FADEC Engine Harness Assembly Re-route 1. Planning Information A. Effectivity: This service bulletin applies to the following Williams International turbofan engines: ENGINE MODEL NUMBER
More informationType Acceptance Report
TAR 8/21B/21 Pratt & Whitney Canada PW615F-A Aircraft Certification Unit TABLE OF CONTENTS EXECUTIVE SUMMARY 1 1. INTRODUCTION 1 2. ICAO TYPE CERTIFICATE DETAILS 1 3. TYPE ACCEPTANCE CERTIFICATE 1 4.
More informationBULLETIN INDEX LOCATOR
BULLETIN INDEX LOCATOR 72-20-00 Compliance: CATEGORY 7 PRATT & WHITNEY CANADA MODEL APPLICATION PT6A-42A P&WC S.B. No. 3445 Summary: In severe environmental conditions, corrosion can occur on the compressor
More informationService Bulletin. Service Bulletin No. 064 Alternator Model ALV-9610 Series Through Bolt Inspection for Proper Torque
2900 Selma Highway Montgomery, AL 36108 USA Tel: 334-386-5400 Fax: 334-386-5450 http://www.hartzell.aero Service Bulletin Alternator Model ALV-9610 Series Through Bolt Inspection for Proper Torque 1. Planning
More informationSERVICE BULLETIN THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN
SERVICE BULLETIN SERVICE BULLETIN M20-325 THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN SUBJECT: Service Instruction M20-88A - STABILIZER TRIM STOP/SCREW MODIFICATION Dated 12/14/2016. MODELS/ SN
More informationSERVICE BULLETIN THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN
MOONEY AIRPLANE COMPANY, INC. SERVICE BULLETIN Louis Schreiner Field Kerrville, Texas 78028 DATE: October 30, 2003 THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN SERVICE BULLETIN M20-282 DATE: October
More informationTO: HOLDERS OF THE ENGINE FIRE EXTINGUISHER SERVICE BULLETIN , DATED JAN 13/06. REVISION NO. 1, DATED JUN 22/06 HIGHLIGHTS
TO: HOLDERS OF THE ENGINE FIRE EXTINGUISHER SERVICE BULLETIN 51600-26-2, DATED JAN 13/06. REVISION NO. 1, DATED HIGHLIGHTS THIS PUBLICATION HAS BEEN REPRINTED IN ITS ENTIRETY. REPLACE ALL PREVIOUSLY ISSUED
More information201F Fuel Pump Shaft Seal Leak
2900 Selma Highway Montgomery, AL 36108 USA Tel: 334-386-5400 Fax: 334-386-5450 201F Fuel Pump Shaft Seal Leak 1. Planning Information A. Effectivity* (1) Hartzell Engine Technologies LLC (HET) 201F Series
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 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 information201F Fuel Pump Valve Housing Cap Screw Replacement
Service Bulletin 2900 Selma Highway Montgomery, AL 36108 USA Tel: 334-386-5400 Fax: 334-386-5450 http://www.hartzell.aero 201F Fuel Pump Valve Housing Cap Screw Replacement 1. Planning Information A. Effectivity
More information*MANDATORY SERVICE BULLETIN*
NUMBER: SB-022 REVISION: B DATE: 10/30/2009 SUBJECT: PITOT STATIC SYSTEM; MANDATORY MODIFICATION KODIAK MANDATORY SERVICE BULLETIN *MANDATORY SERVICE BULLETIN* SUMMARY *MANDATORY SERVICE BULLETIN* RECURRENT
More informationPILATUS AIRCRAFT LTD. CH-6371 STANS, SWITZERLAND SERVICE BULLETIN SERVICE BULLETIN NO: REF NO: 184 MODIFICATION NO: ATA CHAPTER: 32
PILATUS AIRCRAFT LTD. CH-6371 STANS, SWITZERLAND NO: 32-016 REF NO: 184 MODIFICATION NO: ATA CHAPTER: 32 LANDING GEAR LANDING GEAR - INSPECTION AND REPLACEMENT OF COMPONENTS 1. Planning Information A.
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 informationService Bulletin. ATA 27-00: Flight Controls Rudder-Aileron Interconnect Modification
Service Bulletin Issued: 09 May 2007 Models SR20 and SR22 ATA 27-00: Flight Controls Rudder-Aileron Interconnect Modification COMPLIANCE Mandatory: Accomplish this Service Bulletin within 25 Flight Hours
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 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 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 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 FLIGHT CONTROLS - INSTALL FLAP INSPECTION ACCESS PANELS ON CERTAIN AERO CENTER PRODUCTS
Beechcraft TITLE: FLIGHT CONTROLS - INSTALL FLAP INSPECTION ACCESS PANELS ON CERTAIN AERO CENTER PRODUCTS 1. Planning Information A. Effectivity (1) Airplanes Model 19 Series, Serials MB-1 through MB-905;
More information