SERVICE BULLETIN N F
|
|
- Martha Carson
- 5 years ago
- Views:
Transcription
1 SERVICE BULLETIN N F MANUFACTURER REFERENCE: N F N ATA: 27 Date: TITLE: Inspection of rudder control pedal torque tube EFFECTIVITY Model Serial Number F to 0098 PURPOSE A pilot rudder pedal became detached in flight. No change in aircraft attitude occurred and the flight continued back. Rudder was control normally by copilot rudder pedal until a safe landing. This service bulletin describes the procedure for detection of potential cracks on rudder control pedal torque tube. COMPLIANCE: APPLICATION : MANDATORY VISUAL AND PENETRANT INSPECTION MUST BE CARRIED OUT PRIOR TO NEXT FLIGHT. REFER TO PART A MAGNETIC PARTICLE INSPECTION MUST BE CARRIED OUT DURING NEXT SCHEDULED 100 FLIGHT HOURS MAINTENANCE CHECKS. REFER TO PART B APPROBATION This service bulletin has been approved under the privileges of the design organization approval EASA 21J.064. This ASI Aviation service bulletin is attached to the AD EASA approval number: E. REFERENCE None Service Bulletin N F Page 1/7
2 MAN-HOURS Approximately 20 man-hours. MATERIAL Not applicable CREDIT Not applicable OVERVIEW Service Bulletin N F Page 2/7
3 ACCOMPLISHMENT INSTRUCTIONS WARNING: WHENEVER MAINTENANCE IS CONDUCTED ON ANY FLIGHT CONTROL SYSTEM REQUIRING REMOVAL/INSTALLATION OF CONTROL CABLES, ENSURE CONTROL CABLES ARE NOT CROSSED DURING CONTROL CABLES REINSTALLATION. PART A : VISUAL AND PENETRANT INSPECTION Instruction VISA INSPECTION A.1 Remove flight compartment carpet and scuff plate following AMM Chapter page 201 to get access to rudder pedals. A Torque tubes shall be free from grease or other contaminates which could decrease contrast between a discontinuity and its background. A.3 Inspect visually both torque tube for cracks in welded joint areas. Carry out a penetrant inspection by a qualified personnel on rudder pedal torque tube (both side: pilot and copilot). Service Bulletin N F Page 3/7
4 A.4 If any defect is detected, please fill attached form and contact ASI Aviation customer support for further information. If no defect is detected, apply following steps. A.5 A.6 04 to remove all penetrant substance. Install flight compartment carpet and scuff plate following AMM Chapter page 201 to get access to rudder pedals. A.7 Perform adjustement/test of rudder control system following AMM Chapter page 501 Service Bulletin N F Page 4/7
5 PART B : MAGNETIC PARTICLE INSPECTION Instruction VISA INSPECTION B.1 Remove Rudder pedal assembly following AMM Chapter page 206. B Torque tubes shall be free from grease or other contaminates which could restrict particle movement. B.3 Carry out a magnetic particle inspection by a qualified personnel on rudder pedal torque tube (both side: pilot and copilot). Magnetic particle inspection can be performed using the fluorescent, wet continuous or direct current technique whichever possibilities. Cracks can occur at welded joint between torque tube and pedals. B.4 If any defect is detected, please fill attached form and contact ASI Aviation customer support for further information. Service Bulletin N F Page 5/7
6 If no defect is detected, apply following steps. B.5 Demagnetize parts after final inspection. B.6 B.7 04 to remove all magnetic substance. Install Rudder pedal assembly following AMM Chapter page 206. B.8 Perform adjustement/test of rudder control system following AMM Chapter page 501 OWNER NOTIFICATION The Service Bulletin F dated 28 th July 2015 will be addressed to the owners of the F406 airplanes. It is recommended to the customers to contact ASI AVIATION for any further information relating to the application of this Service Bulletin on your airplane. ASI AVIATION Aérodrome de Reims-Prunay Prunay France Tel : (33) Customer Support Website: Service Bulletin N F Page 6/7
7 INSPECTION FORM SB-F Company :... Adress :... Name :... Occupation : Telephone :... Actual configuration: Serial Number: F Defect is detected on LH rudder pedal torque tube: Yes (Visual / Penetrant / Magnetic particle inspection) No Defect is detected on LH rudder pedal torque tube: Yes (Visual / Penetrant / Magnetic particle inspection) No (Surround applied inspection) Maintenance Phase :... Date :... Total flight hours :... Total landings :... Commentary :... To send at : Or by letter at : ASI Aviation Support Client Aérodrome de Reims-Prunay Prunay, France Service Bulletin N F Page 7/7
SERVICE BULLETIN TITLE FLIGHT CONTROLS - RUDDER AND ELEVATOR AUTOPILOT SERVO CABLE REPLACEMENT
TITLE FLIGHT CONTROLS - RUDDER AND ELEVATOR AUTOPILOT SERVO CABLE REPLACEMENT EFFECTIVITY REASON MODEL SERIAL NUMBERS 525 (M2) -0685, -0800 thru -0870 The equivalent of this service bulletin has been incorporated
More informationAirworthiness Directive
Airworthiness Directive AD No.: 2018-0135 Issued: 26 June 2018 EASA AD No.: 2018-0135 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) 216/2008 on behalf
More informationAIRWORTHINESS DIRECTIVE
EASA AIRWORTHINESS DIRECTIVE AD No.: 2013-0288 Date: 06 December 2013 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) No 216/2008 on behalf of the European
More informationNotification of a Proposal to issue an Airworthiness Directive
Notification of a Proposal to issue an Airworthiness Directive PAD No.: 18-063 Issued: 30 April 2018 Note: This Proposed Airworthiness Directive (PAD) is issued by EASA, acting in accordance with Regulation
More informationSERVICE BULLETIN REVISION TRANSMITTAL
REVISION TRANSMITTAL TO: Cessna Distributors, Multi-Engine Authorized Service Facilities, and CPC's SUBJECT: Multi-Engine Service Bulletin Revision 1: Control Column Internal Glide Attach Screw Installation
More informationSERVICE BULLETIN. No. SB-CR-017 Rev.: - Date: Page: 1 of 7 Date: -
Page: 1 of 7 Date: - MODEL AFFECTED: SUBJECT: AIRCRAFT AFFECTED: COMPLIANCE: PS-28 Cruiser / SportCruiser / PiperSport Replacement of rivets for bolts in the area of the main landing gear attachment. All
More informationSERVICE BULLETIN SB-GL12-01R GREAT LAKES AIRCRAFT HORIZONTAL STABILIZER SPAR INSPECTION COMPLIANCE TIME: APPROVAL: PURPOSE: BACKGROUND:
SUBJECT: AFFECTED MODELS: 2T-1A 0501 and 0502 2T-1A-1 0503 through 0699 2T-1A-2 0701 through 1012 COMPLIANCE TIME: APPROVAL: PURPOSE: BACKGROUND: Released: 01/25/2012 Page 1 of 5 HORIZONTAL STABILIZER
More informationSERVICE LETTER. EFFECTIVITY Model 206H airplanes that have replaced the 10880A Oil Cooler after May SERIAL NUMBERS 206H thru
MANDATORY SERVICE LETTER TITLE OIL - OIL COOLER REPLACEMENT EFFECTIVITY Model 206H airplanes that have replaced the 10880A Oil Cooler after May 2014 MODEL SERIAL NUMBERS 206H 20608001 thru 20608353 REASON
More informationGTS 8XX Traffic System Instructions for Continued Airworthiness as installed in
GTS 8XX Traffic System Instructions for Continued Airworthiness as installed in (Make and Model Airplane) Reg. No. S/N Dwg. Number: 190-00993-01 Rev. 1 Garmin Ltd. Or its subsidiaries c/o Garmin International,
More informationP/N CABLE ASSEMBLY, ONE TIME INSPECTION FOR DEFECTIVE BODY, P/N PART I (Inspection): Within the next 25 flight hours
ALERT SERVICE BULLETIN 204B-12-68 10 October 2012 MODEL AFFECTED: SUBJECT: HELICOPTERS AFFECTED: 204B P/N 205-001-720-001 CABLE ASSEMBLY, ONE TIME INSPECTION FOR DEFECTIVE BODY, P/N 205-001-742-001 ALL
More informationSERVICE BULLETIN SB
TITLE NAVIGATION - RADIO ALTIMETER CONVERTER UPGRADE EFFECTIVITY MODEL SERIAL NUMBERS 525-0360 thru -0515 The equivalent of this service bulletin has been incorporated on production airplanes -0516 and
More informationSERVICE LETTER. EFFECTIVITY The Model T206H airplanes were delivered from Textron Aviation with a suspect 10865B Oil Cooler.
MANDATORY SERVICE LETTER TITLE OIL - OIL COOLER REPLACEMENT EFFECTIVITY The Model T206H airplanes were delivered from Textron Aviation with a suspect 10865B Oil Cooler. MODEL SERIAL NUMBERS T206H T20609001
More informationMandatory: shall be accomplished at the next scheduled 100 hour or annual/12 month type inspection, not to exceed 12 months, whichever occurs first.
Single Engine Service Bulletin February 26, 2007 TITLE WING STRUT TO FUSELAGE CUFF MODIFICATION EFFECTIVITY Model Serial Numbers 206H 20608001 thru 20608289 T206H T20608001 thru T20608734 REASON It has
More informationAirworthiness Directive
Airworthiness Directive AD No.: 2016-0108 Issued: 08 June 2016 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) 216/2008 on behalf of the European Union,
More informationHARTZELL PROPELLER INC. SERVICE BULLETIN
1. Planning Information A. Effectivity Hartzell propeller models HC-B(3,4,5)( )(P,N)-( )( ) that were installed on an aircraft, or that have had B-3339 mounting bolts replaced, between January 30, 2001
More informationSERVICE BULLETIN TITLE ELECTRICAL POWER - RIGHT HAND ENGINE WIRE BUNDLE ROUTING IMPROVEMENT
TITLE ELECTRICAL POWER - RIGHT HAND ENGINE WIRE BUNDLE ROUTING IMPROVEMENT EFFECTIVITY REASON MODEL SERIAL NUMBERS 560XL (Citation XLS+) -6001 thru -6232 The equivalent of this service bulletin has been
More informationSERVICE BULLETIN TITLE EQUIPMENT/FURNISHINGS - SEAT CONTROL CABLE ROUTING IMPROVEMENT
TITLE EQUIPMENT/FURNISHINGS - SEAT CONTROL CABLE ROUTING IMPROVEMENT EFFECTIVITY REASON MODEL SERIAL NUMBERS 525B (CJ3) -0451 thru -0504 The equivalent of this service bulletin has been incorporated on
More informationENGINEERING REPORT DATE. This Service Letter is applicable to all models and all serial numbers of Air Tractor aircraft.
WICHITA FS, TEXAS SUBJECT: Rudder Controls Inspection and Maintenance APPLICABILITY: 1 8 This Service Letter is applicable to all models and all serial numbers of Air Tractor aircraft. PURPOSE: The purpose
More information1625 North 1100 West SB Springville, UT SERVICE BULLETIN MANDATORY ACTION REQUIRED
SERVICE BULLETIN MANDATORY ACTION REQUIRED Subject: Chafing of Aileron Cable Assembly P/N 7227151-522WE. 1. Planning a. Effectivity Part Number NHA P/N NHA Description ATA Aircraft Application 7227151-522WE
More informationSERVICE LETTER SERIAL NUMBERS thru with Hydraulic Pump
TITLE HYDRAULIC POWER - ENGINE DRIVEN HYDRAULIC PUMP VERIFICATION EFFECTIVITY REASON MODEL 525B (CJ3) 525B (CJ3+) SERIAL NUMBERS -0001 thru -0415 with 9912062-8 Hydraulic Pump Installed -0451 thru -0485
More informationSERVICE BULLETIN. No. SB-AG-45 Rev. B JUNE 1, 2007 FIN SPAR & ATTACH FITTINGS INSPECTION AND UPGRADE IMPORTANT:
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-45 Rev. B JUNE
More informationBMAA Defect Alert #0063: EuroFox SB3 Replacement of Undercarriage Guide Bracket Bolts (Taildragger Variant)
BMAA Defect Alert #0063: EuroFox SB3 Replacement of Undercarriage Guide Bracket Bolts (Taildragger Variant) Dated: 03/11/2016 EuroFox Aviation has issued a Service Bulletin for all EuroFox taildragger
More informationFAA APPROVED AIRPLANE MAINTENANCE MANUAL SUPPLEMENT. Eyebrow Window Replacement
FAA APPROVED AIRPLANE MAINTENANCE MANUAL SUPPLEMENT AIRPLANE MAKE: Boeing AIRPLANE MODEL: 737-100, -200, -200C, -300, -400, -500, -600, -700, -700C, -800, -900 TO BE ADDED TO AMM CHAPTER 56-11-XX This
More information(VSP 116A supercedes and voids VSP 116 dated January 4, 1999)
(VSP 116A supercedes and voids VSP 116 dated January 4, 1999) All affected owners, all Piper Domestic and International Distributors, Authorized Piper Service Centers and publication subscribers. TEXTRON
More information*MANDATORY SERVICE BULLETIN*
NUMBER: SB-004 DATE: 1/26/2009 SUBJECT: ELECTRICAL; Potentiometer Replacement KODIAK MANDATORY SERVICE BULLETIN SUMMARY RECURRENT REQUIREMENTS No recurrent requirements associated with this Mandatory Service
More informationChapter 20. Standard Practices - Airframe
Chapter 20 Standard Practices - Airframe PAGE 1 Chapter 20 Table of Contents Chapter Title 20-00-00 GENERAL.................................. 3 20-10-00 STANDARD PRACTICES AIRFRAME........... 4 20-10-01
More informationRADAR ALTIMETER CABLES, REPLACEMENT OF. HELICOPTERS AFFECTED: Serial numbers through
TECHNICAL BULLETIN 42-7-24 23 October 207 MODEL AFFECTED: SUBJECT: 42EP RADAR ALTIMETER CABLES, REPLACEMENT OF. HELICOPTERS AFFECTED: Serial numbers 37002 through 3703. [Serial number 3704 and subsequent
More informationSERVICE BULLETIN
14401 Keil Road NE, Aurora, Oregon, USA 97002 PHONE 503-678-6545 FAX 503-678-6560 www.vansaircraft.com info@vansaircraft.com Service Letters and Bulletins: www.vansaircraft.com/public/service.htm SERVICE
More informationDEPARTMENT OF TRANSPORTATION
DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [61 FR 625 No. 6; 01/09/96][SN] [Docket No. 94-ANE-63; Amendment 39-9458; AD 95-03-10] Textron Lycoming AD 95-03-10 Amendment
More informationALERT SERVICE BULLETIN
January 28, 2010 TITLE INSPECTION OF MODEL 1A103/TCM PROPELLER HUB FOR CRACKING AND REWORK PROCEDURES TO: FAA-Approved Propeller Repair Stations, Cessna Aircraft Company, Aircraft Owners, and Operators
More informationNAVSEA STANDARD ITEM. 2.2 MIL-STD-1689, Fabrication, Welding, and Inspection of Ships Structure
NAVSEA STANDARD ITEM ITEM NO: 009-05 DATE: 18 JUL 2014 CATEGORY: I 1. SCOPE: 1.1 Title: Temporary Accesses; provide 2. REFERENCES: 2.1 Standard Items 2.2 MIL-STD-1689, Fabrication, Welding, and Inspection
More informationAirworthiness Directive
Airworthiness Directive AD No.: 2016-0018R1 Issued: 14 September 2016 EASA AD No.: 2016-0018R1 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) 216/2008
More informationThese Installation Instructions are valid for antennas in the following version:
Installation Instructions 4 ft CompactLine Antennas (with E-Mount 200 km/h) SB, SBX NMT 480-12(e) These installation instructions have been written for qualified, skilled personnel. The antenna shall be
More informationCIRRUS SR22 SB 2X R3. Service Bulletin. Issued: Revised: October 13, 2009 May 18, 2010
CIRRUS SR22 Service Bulletin Number: Issued: Revised: October 13, 2009 SNS SUBJECT: 30-10 ICE PROTECTION - AIRFOIL - Porous Panel Vent Inspection 1. COMPLIANCE Recommended: Accomplish this Service Bulletin
More informationSECTION 2. VISUAL INSPECTION
SECTION 2. VISUAL INSPECTION 5-15. GENERAL. Visual inspection is the oldest and most common form of NDI for aircraft. Approximately 80 percent of all NDI procedures are accomplished by the direct visual
More informationNomad CONTROL SYSTEM IMPROVED PULLEY MOUNTING AT STATION (MOD N137) Page No Rev No
CONTROL SYSTEM IMPROVED PULLEY MOUNTING AT STATION 67.95 (MOD N137) 1. PLANNING INFORMATION A. Effectivity (1) Aircraft Affected All Nomad N22 Series and N24 Series aircraft whose log books do not already
More informationservice bulletin WING SPAR INSPECTION AND FATIGUE LIFE EXTENSION
service bulletin Service Bulletin Number : SB-AG-39 September 17, 1996 WING SPAR INSPECTION AND FATIGUE LIFE EXTENSION MODELS AFFECTED: All S2R models and serial numbers manufactured and listed here, including
More informationPart 1: General principles
Provläsningsexemplar / Preview INTERNATIONAL STANDARD ISO 9934-1 Second edition 2015-09-01 Non-destructive testing Magnetic particle testing Part 1: General principles Essais non destructifs Magnétoscopie
More informationService Bulletin No: Ref No: 136 Modification No: INSPECTION ATA Chapter: 57
PILATUS AIRCRAFT LTD. STANS, SWITZERLAND Service Bulletin No: 57-015 Ref No: 136 Modification No: INSPECTION ATA Chapter: 57 WING - AILERON INSTALLATION INSPECTION OF THE AILERON OUTBOARD-BEARING SUPPORT
More informationManual for Propeller Type H40F
Manual for Propeller Type H40F Propeller Type: Propeller Serial No.: Date of Sale: Seal and signature of Manufacturer: Index 1 List of Modifications... 3 2 Description... 4 3 Specification of Helix Propeller
More informationINSTRUCTIONS FOR CONTINUED AIRWORTHINESS
823 McTavish Road NE Calgary, Alberta, Canada T2E 7G9 PH: (800) 564-6469 www.eaglecopters.com INSTRUCTIONS FOR CONTINUED AIRWORTHINESS FOR P139-HD DIGITAL AUDIO SYSTEM MDL GA212 FOR EUROCOPTER BK117 (EC145)
More informationNAVSEA STANDARD ITEM. 2.2 MIL-STD-1689, Fabrication, Welding, and Inspection of Ships Structure
NAVSEA STANDARD ITEM ITEM NO: 009-05 DATE: 18 NOV 2016 CATEGORY: II 1. SCOPE: 1.1 Title: Temporary Access; accomplish 2. REFERENCES: 2.1 Standard Items 2.2 MIL-STD-1689, Fabrication, Welding, and Inspection
More informationIMPORTANT - STATE AIRCRAFT REGISTRATION NUMBER IN ALL CORRESPONDENCE MOONEY AIRCRAFT, INC. M-l8 SERVICE LETTER NO.17
IMPORTANT - STATE AIRCRAFT REGISTRATION NUMBER IN ALL CORRESPONDENCE MOONEY AIRCRAFT, INC. M-l8 SERVICE LETTER NO.17 (This Service Letter is FAA. Approved) DATE: OCTOBER 24, 1959 SUBJECT: REAR BULKHEAD
More informationNMD Rev 1 2 August 1996 Page 1
FLIGHT CONTROLS - AILERON & FLAP CONTROL ROD FORK ENDS - INSPECTION 1. PLANNING INFORMATION A. Effectivity All Nomad N22 Series and N24 Series aircraft. B. Reason (1) Instances have occurred where Fork
More informationSERVICE BULLETIN. Date: Rev.: - Page: 1 of 6 Date: -
Page: 1 of 6 Date: - MODEL AFFECTED: SUBJECT: AIRCRAFT AFFECTED: COMPLIANCE: SportCruiser / PiperSport aircraft (excluding those operating under EASA rules) Installation of improved canopy guidance during
More informationSERVICE INFORMATION LETTER
CUSTOMER SERVICES DIRECTORATE 1 ROND POINT MAURICE BELLONTE 31707 BLAGNAC CEDEX FRANCE TELEPHONE + 33 (0)5 61 93 33 33 TELEX AIRBU 530526F AIRBUS SUBJECT: Radio-Altimeter antennas, protection against water
More informationSERVICE BULLETIN. NO.: 0713 Revision D. All Garmin Aviation Service Centers and Aircraft OEM Service Centers DATE: 13 June 2007
SERVICE BULLETIN NO.: 0713 TO: All Garmin Aviation Service Centers and Aircraft OEM Service Centers DATE: 13 June 2007 SUBJECT: GSM 85 Inspection Procedure REVISION D: corrects LRU Part Numbers listed
More informationDEPARTMENT OF TRANSPORTATION
DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 Textron Lycoming AD 92-12-05 Amendment 39-8265 Effective July 10, 1992 Recurring: No [Docket No. 91-ANE-48; Amendment 39-8265;
More informationService Bulletin. Fuel Systems. Bulletin No.: PRS-103. Date: 05/12/98. SUBJECT: RSA-10 Fuel Diaphragm Assembly, Part Number
3220 100TH ST. SW BLDG E EVERETT, WASHINGTON 98204 FAA-PMA FACILITY #PQ111NM Service Bulletin Fuel Systems Bulletin No.: PRS-103 SUBJECT: RSA-10 Fuel Diaphragm Assembly, Part Number 2541803. A. EFFECTIVITY:
More informationÖSTERREICHISCHER AERO-CLUB SEKTION FAA Blattgasse 6, A-1030 WIEN
ÖSTERREICHISCHER AERO-CLUB SEKTION FAA Blattgasse 6, A-1030 WIEN Sicherheitsmitteilung SM 060602 Datum: 08.06.2006 Hersteller: Parachutes de France Easa Bulletin: AD No : 2006-0160-E Betroffene Systeme:
More informationInstructions for Continued Airworthiness Supplement
CESSNA AIRCRAFT COMPANY AIRCRAFT DIVISION WICHITA, KANSAS 67277 Instructions for Continued Airworthiness Supplement MODEL NO: 510 REPORT NO: ICA-510-34-00001 REPORT: GA36 & GA37 GPS ANTENNAS REPORT DATE:
More informationJunction Box JB6101- (000) Installation and Operation. Manual DV Issue 1 June 2012
Junction Box JB6101- (000) Installation and Operation Manual DV 64494.03 Issue 1 June 2012 Becker Flugfunkwerk GmbH Baden Airpark 77836 Rheinmünster Germany Telephone +49 (0) 7229 / 305-0 Fax +49 (0) 7229
More informationC I R R U S EMERGENCY DESCRIPTION A. Emergency Locator Transmitter (ELT)
EMERGENCY 1. DESCRIPTION A. Emergency Locator Transmitter (ELT) This airplane is equipped with a self-contained ELT. The ELT transmitter is installed immediately behind the aft cabin bulkhead. The ELT
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
MODEL SR0 AUXILIARY STRUCTURE. DESCRIPTION This section describes those structural components which make up the auxiliary structure including fuselage floor structure, floor access panels, entry step,
More informationSERVICE BULLETIN. SERIAL NUMBERS thru A0001 thru 402A B0001 thru 401B thru
TITLE WINGS - ACCESS PANEL INSTALLATION FOR FORWARD SPAR EFFECTIVITY REASON MODEL SERIAL NUMBERS 401 401-0001 thru 401-0322 401A 401B 401A0001 thru 401A0132 401B0001 thru 401B0221 402 402-0001 thru 402-0322
More informationBX1956 Installation Instructions Chrysler PT Cruiser (Include Turbo)
BX1956 Installation Instructions 2001-04 Chrysler PT Cruiser (Include Turbo) Serial No. The front fascia and metal bumper are removed for baseplate installation. Factory metal bumper will not be reinstalled.
More informationInstallation Instructions 4 ft Antennas (with E-Mount) DA, DAX, UA, UDA, UXA SD, SDX, SU, SUX
Installation Instructions 4 ft Antennas (with E-Mount) DA, DAX, UA, UDA, UXA SD, SDX, SU, SUX NMT 553-01(e) These Installation Instructions are valid for antennas in the following version : Reflector Ø
More informationResearch Program Overview Maintenance & Inspection (M&I) Technical Community Representative Group (TCRG) Part of BLI A11e Continued Airworthiness
Research Program Overview Maintenance & Inspection (M&I) Technical Community Representative Group (TCRG) Part of BLI A11e Continued Airworthiness Presented to: 57 th Annual A4A NDT Forum By: David Westlund
More informationSERVICE BULLETIN. SERIAL NUMBERS thru
TITLE WINGS - ACCESS PANEL INSTALLATION FOR FORWARD SPAR EFFECTIVITY REASON MODEL SERIAL NUMBERS 425 425-0001 thru 425-0236 Customers have requested an access panel to gain easy access to the forward spar
More informationPlated Through Hole Fill:
Welcome to the EPTAC Webinar Series: Plated Through Hole Fill: Understanding the Process and Assembly Requirements You are connected to our live presentation delivered via the internet. The webinar will
More informationWelding Inspection Non-Destructive Testing Course Reference WIS 5
Welding Inspection Non-Destructive Testing Course Reference WIS 5 Non Destructive Testing A welding inspector should have a working knowledge of NDT methods and their applications, advantages and disadvantages.
More informationSERVICE BULLETIN NO. OSB
GROB Luft- und Raumfahrt OSB 817-47 Lettenbachstrasse 9 Page 1 of 5 D-86874 Tussenhausen-Mattsies 4. July 2005 SERVICE BULLETIN NO. OSB 817-47 I. TECHNICAL DETAILS 1.1 Category: Optional 1.2 Aircraft affected:
More informationSeychelles Civil Aviation Authority SAFETY NOTICE. Coding and registration of Seychelles 406 Mhz Emergency Locator Transmitters (ELTs)
Seychelles Civil Aviation Authority Safety Notice SAFETY NOTICE Number: Issued: 25 April 2018 Coding and registration of Seychelles 406 Mhz Emergency Locator Transmitters (ELTs) This Safety Notice contains
More informationBX3230 Installation Instructions Oldsmobile Silhouette Chevy Venture
BX3230 Installation Instructions 1997-2004 Oldsmobile Silhouette 1997-2003 Chevy Venture Serial No. The headlight assembly, front fascia, horn bracket and windshield washer reservoir are removed for baseplate
More information2017 CDM Smith All Rights Reserved November 2016 SECTION PROJECT MANAGEMENT INFORMATION SYSTEM (PMIS)
ATTACHMENT 5, CONTRACT 13, ADDENDUM 3 2017 CDM Smith 14955-109447 SECTION 01725 PROJECT MANAGEMENT INFORMATION SYSTEM (PMIS) PART 1 GENERAL 1.01 DESCRIPTION A. The Owner and Contractor shall utilize the
More informationSERVICE BULLETIN REVISION
Revision 3 REVISION TRANSMITTAL SHEET This sheet transmits Revision 3 to, which: A. Removes the 453-5000-999 ELT from the kits and makes it a stand alone part. B. Changes part numbers within the kits.
More informationNOV 16 Rev L
Terminating Modules 856196-[ ] for Use with Modular Plug Dual Terminators 1320840-[ ] Instruction Sheet 408-9743 17 NOV 16 Rev L Modular Plug Dual Terminator Automatic Circuit Tester (Terminators 1320840-1
More informationCH-SE-UN-FIG PAGE DATE
List of Effective Pages CH-SE-UN-FIG PAGE DATE Introduction-LOEP Feb 0/8 Introduction thru Feb 0/8 -LOEP Page FEB 0/8 Beechcraft Corporation SUPER KING AIR B00GT SERIES ILLUSTRATED PARTS CATALOG PAGE INTENTIONALLY
More informationMarathonNorco Aerospace, Inc Imperial Drive Waco, Texas SERVICE BULLETIN SB-SS Revision 2
MarathonNorco Aerospace, Inc. 8301 Imperial Drive Waco, Texas 76712-6588 SERVICE BULLETIN Revision 2 Subject: Product Improvement Escape Slide/Raft Add Positive Lock to Packboard Latch Revision 2- January
More informationSECTION 35 ANTENNAS AND TOWERS
SECTION 35 ANTENNAS AND TOWERS Section: 515-35-1 Purpose and Intent 515-35-2 General Standards 515-35-3 Certification, Inspection and Maintenance 515-35-4 Tower Design 515-35-5 Co-Location Requirement
More informationCAR Part IX Regulations for srpas Manufacturers. Presented by RPAS TF Eng to Industry, Jan. 24, 2019
CAR Part IX Regulations for srpas Manufacturers Presented by RPAS TF Eng to Industry, Jan. 24, 2019 Overview Regulatory responsibilities for srpas manufacturers; CAR Standard 922 Grandfathering TCCA processes
More informationBX2165 Installation Instructions Mercury Grand Marquis
BX2165 Installation Instructions 2003-06 Mercury Grand Marquis Serial No. 2003-06 Lincoln Town Car Drilling is necessary. No trimming of the fascia is needed. The BX8869 is available for this vehicle.
More informationTechtest. Limited. Crash Position Indicator System. Type Maintenance Manual. Techtest. L imited
Techtest Limited Crash Position Indicator System Type 15-503-134-1 Maintenance Manual Techtest L imited Preface This manual is a controlled document, and as such is subject to amendment. It is in the interest
More informationSERVICE BULLETIN EQUIPMENT / FURNISHING PASSENGER COMPARTMENT INSPECTION / REPLACEMENT OF EJECTOR BASE SERVICE BULLETIN NUMBER ISSUE 10
EQUIPMENT / FURNISHING PASSENGER COMPARTMENT INSPECTION / REPLACEMENT OF EJECTOR BASE SERVICE BULLETIN NUMBER ISSUE 10 ISSUED BY: AMSAFE INC. 1043 N. 47 th AVENUE PHOENIX, AZ USA 85043 TEL: (602) 850 2850
More informationBody Repair. Collision Repair. Specification. Fastener Specifications Fastener Specifications. Blind Rivet. Flow Drill Screw (FDS) Torque FDS
Body Repair Collision Repair Specifications Fastener Specifications Fastener Specifications Application Specification Metric English Cross-Car Brace Mounting Bolts 25 Y 18 lb ft Windshield Frame Mounting
More informationSD3-60 AIRCRAFT MAINTENANCE MANUAL SYSTEM - DESCRIPTION & OPERATION (POST MOD A8062)
AMM 19.0.0.0GYRO COMPASS SYSTEM - DESCRIPTION & OPERATION (POST MOD A8062) 1. General A. The Gyro compass system is a dual installation which provides heading data for: - one flight director system. Refer
More informationNondestructive Testing (CALIBRATION)
NONDESTRUCTIVE TESTING (CALIBRATION) HPI Nondestructive Testing (CALIBRATION) Hybrid Petroleum institute His allies at all times Calibration of Nondestructive Testing Devices (PND's) INTRODUCTION Nondestructive
More informationNomad. Page No Rev No
FUSELAGE STUB WING WING STRUT FITTING ASSEMBLY LOOSE ATTACHMENT BOLTS REPAIR 1. PLANNING INFORMATION A. Effectivity (1) Aircraft affected: (a) N22 Series line sequence numbers 1 to 9, 11 to 29, 31, 33,
More informationInstruction Manual. LSV36108A 3600# Vertical Lift LAKESHORE PRODUCTS, INC.
LAKESHORE PRODUCTS, INC. Quincy. MI. 49082. tel 517.639.3815 LSV36108A 3600# Vertical Lift Instruction Manual Read carefully. Failure to follow the instructions and safety rules could result in severe
More informationInstallation Instructions
Installation Instructions Feed Installation for 0.6m(2ft) Spread Spectrum Antennas Bulletin 239851 Revision F Antenna Assembly Sequence P2F/HP2F/PX2F/ HPX2F antenna 1 2 3 1a 1 Apply conductive grease (5)
More informationINSTRUCTIONS FOR CONTINUED AIRWORTHINESS
823 McTavish Road NE Calgary, Alberta, Canada.T2E 7G9 PH: (800) 564-6469 Website: www.eaglecopters.com INSTRUCTIONS FOR CONTINUED AIRWORTHINESS FOR P139-HD DIGITAL AUDIO SYSTEM MDL GA182 FOR MODEL EUROCOPTER
More information9800 Martel Road Lenoir City, TN PMA6000B
9800 Martel Road Lenoir City, TN 37772 www.ps-engineering.com PMA6000B Audio Control Panel Marker Beacon and Intercom Pilot s Guide and Operation Manual FAA-TSO C50c, C35d EASA ETSO C50c, 2C35d US Patent
More informationMD RA Minister's Delegates - Recreational Aviation Représentants du Ministre - Aviation de loisir
Think Safety Inspection Service MD RA Minister's Delegates - Recreational Aviation Représentants du Ministre - Aviation de loisir Pensons Securite Service d'inspection MDRA C20 MANUAL of PROCEDURES for
More informationManual for Propeller Type H60V
Manual for Propeller Type H60V Propeller Type: Propeller Serial No.: Date of Sale: Seal and Signature of Manufacturer: Index 1 List of Modifications... 3 2 Description... 4 3 Specification of the propeller
More informationComp-DS Driveshaft. User Manual B
Comp-DS Driveshaft User Manual 2010-1378B Driveshaft Parts List 1.22B 1.21C 1.22C 1.22D 1.21A 1.21B 1.22A 1.1 Figure 1 1.0 Complete Driveshaft 1.1 Tube and Flange Assembly 1.2 Coupling Assembly (2 required
More informationMINUTES OF MEETING. The following Questions were asked and answers were provided accordingly:
MINUTES OF MEETING Meeting Date : July 15, 2014 Place : Greenwood Shop Main Conference Room Contract Title : Supply of Reworked T1 Trip Switch Brackets Proposal No. : T31BG14139 Present : TTC - A. Mckay
More informationRole of DOA and AP-DOA Privileges for ICAs issuance and approval. ICA Workshop 19 January 2010
Role of DOA and AP-DOA Privileges for ICAs issuance and approval ICA Workshop 19 January 2010 Role of DOA An approved Design Organisation should ensure through its Design Assurance System: Preparation
More informationSide Sill Closure Inspection and Repair
INSPECTION BULLETIN Side Sill Closure Inspection and Repair This inspection Bulletin provides details for the inspection and modification of side sill closure plates on ACF built Center Flow covered hopper
More informationINSTALLATION, OPERATION MANUAL
Orolia S.A.S. Z.I. des Cinq Chemins CS10028 56520 GUIDEL - FRANCE Telephone: +33 (0)2 97 02 49 49 Fax: +33 (0)2 97 65 00 20 Web : http://www.mcmurdogroup.com E-mail : info@mcmurdogroup.com INTEGRA ARINC
More informationModel: PR-55. High Voltage Oscilloscope Probe 10 kv, 40 MHz USER MANUAL
Model: PR-55 High Voltage Oscilloscope Probe 10 kv, 40 MHz USER MANUAL 1 2017 All rights reserved. B&K Precision products are covered by US and foreign patents, issued and pending. Information is this
More informationDirector P. O. Box 1904 Service Engineering Operations Dearborn, Michigan Ford Customer Service Division
Michael A. Berardi Ford Motor Company Director P. O. Box 1904 Service Engineering Operations Dearborn, Michigan 48121 Ford Customer Service Division May 28, 2015 TO: SUBJECT: All U.S. Ford and Lincoln
More informationSERVICE LETTER HC-SL Blade - Damage Evaluation for NC10245( ) Blades Installed on (but not limited to) Pilatus PC-12 aircraft
HARTZELL PROPELLER INC. SERVICE LETTER Blade - Damage Evaluation for NC10245( ) Blades Installed on (but not limited to) Pilatus PC-12 aircraft 1. Planning Information A. Effectivity (1) Hartzell Propeller
More informationSECTION CABLE TRAYS
SECTION 16139 CABLE TRAYS PART 1 - GENERAL 1.1 RELATED DOCUMENTS A. Drawings and general provisions of the Contract, including General and Supplementary Conditions and Division 1 Specification Sections,
More information3 CHANNEL LOAD CELL SIGNAL CONDITIONER. Owner's Manual
3 CHANNEL LOAD CELL SIGNAL CONDITIONER Owner's Manual Boeing Helicopters Part Number 414ES230-SIG CON-1 Breeze-Eastern Part Number Y-1368-1 Onboard Systems Part Number 210-115-00 Manual Number 120-042-00
More informationAircraft Structure Service Life Extension Program (SLEP) Planning, Development, and Implementation
Structures Bulletin AFLCMC/EZ Bldg. 28, 2145 Monohan Way WPAFB, OH 45433-7101 Phone 937-255-5312 Number: EZ-SB-16-001 Date: 3 February 2016 Subject: Aircraft Structure Service Life Extension Program (SLEP)
More informationDelmec Engineering Limited
Delmec Engineering Limited DEL6 Tower Maintenance Specification Delmec Product Manual 2 Delmec Engineering Ltd. Approvals Name Signature Date Ivan Daly Kealan Delaney Delmec Engineering Ltd. Distribution
More informationBX1965 Installation Instructions 2004 Chrysler Sebring Convertible
BX1965 Installation Instructions 2004 Chrysler Sebring Convertible Serial No. The headlight assembly, front fascia, horn bracket and windshield washer reservoir are removed for baseplate installation.
More informationADDENDUM NO. 1 REQUEST FOR QUALIFICATIONS (RFQ) AND REQUEST FOR PROPOSALS (RFP) FOR. RFQ/RFP No. 15P40. Campus Center East HVAC Unit Replacement
ADDENDUM NO. 1 REQUEST FOR QUALIFICATIONS (RFQ) AND REQUEST FOR PROPOSALS (RFP) FOR RFQ/RFP 15P40 Campus Center East HVAC Unit Replacement CHAFFEY COMMUNITY COLLEGE DISTRICT February 26, 2015 CHAFFEY COMMUNITY
More informationRegistry Publication 62
Births, Deaths, Missing Persons Background The Civil Aviation (Births, Deaths and Missing Persons) Regulations 1948 1 place requirements on the pilot in command and owner of aircraft to report births deaths
More informationSERVICE BULLETIN. Date: Rev.: - Page: 1 of 7 Date: -
Page: 1 of 7 Date: - MODEL AFFECTED: SUBJECT: AIRCRAFT AFFECTED: COMPLIANCE: PS-28 Cruiser, SportCruiser / PiperSport - operating under EASA control Installation of improved canopy guidance during closing.
More information