Raytheon Aircraft Company

Similar documents
SERVICE BULLETIN FLIGHT CONTROLS - INSPECTION FOR CONTROL COLUMN INTERFERENCE WITH WIRING BEHIND THE INSTRUMENT PANEL

Raytheon Aircraft SERVICE BULLETIN MANDATORY. Beech

SERVICE BULLETIN EQUIPMENT/FURNISHINGS - PILOT AND COPILOT SHOULDER HARNESS GUIDE RETAINING WASHER INSPECTION AND/OR REPLACEMENT SYNOPSIS OF CHANGE

FLIGHT CONTROLS- RUDDER CABLE PULLEY BRACKET INSPECTION/REPAIR

SERVICE BULLETIN TIME LIMITS/MAINTENANCE CHECKS - AIRBORNE INSTRUMENT AIR SYSTEM COMPONENT REPLACEMENT SCHEDULE

LANDING GEAR - REPLACEMENT OF NOSE LANDING GEAR RETRACT PLUNGER ASSEMBLY

FLIGHT CONTROLS - FLAP FLEX SHAFT (CABLE) ASSEMBLY INSPECTION/ REPLACEMENT

SERVICE BULLETIN MANDATORY SB Planning Information TITLE:

SERVICE BULLETIN FLIGHT CONTROLS - CONTROL COLUMN HARDWARE REPLACEMENT

[Docket No. FAA ; Directorate Identifier 2007-CE-053-AD; Amendment ; AD ]

SERVICE BULLETIN FLIGHT CONTROLS - FLIGHT CONTROL (GUST) LOCK INSPECTION / REPLACEMENT SYNOPSIS OF CHANGE

SERVICE BULLETIN. EFFECTIVITY SERIAL NUMBERS 525 (CJ1+) thru with GPS-4000S installed

The following airplanes equipped with the Garmin G1000 Avionics system:

The FAA published Federal Regulation 14 CFR and 111 cm in May The final rule dictates that effective January 1, 2020, aircraft

SERVICE BULLETIN SERIAL NUMBERS

To add airplane serial numbers thru and 172S0001 thru 172S9974 to the Effectivity section.

SERVICE BULLETIN. Single Engine SEB TITLE FLIGHT CONTROLS - LOWER RUDDER HINGE HARDWARE INSPECTION

AIRCRAFT SERVICE CHANGE

SERVICE BULLETIN TITLE NAVIGATION - ENHANCED SURVEILLANCE TRANSPONDER STRAPPING MODIFICATION

SERVICE BULLETIN SB

TABLE OF CONTENTS 1.0 INTRODUCTION...

ATTACHMENT. Company Name: Initial Shipping Address (if different from the Revision

SERVICE BULLETIN. SERIAL NUMBERS thru B0001 thru 208B5178

SERVICE LETTER. This service letter applies to the models and serials that have 12,000 or more flight hours as follows

TRANSMITTAL SHEET. Concurrent Requirement Added G450 Customer Bulletin Number 141 (aircraft that have previously incorporated ASC 016)

NUMBER 903 RECORDING / INDICATING SYSTEMS (ATA 31) PLANEVIEW MASTER OPERATING SYSTEM SOFTWARE UPDATE

SERVICE LETTER. Conquest. WARNING: Further flight with a cracked carry through spar cap is prohibited. The carry

NUMBER 904 RECORDING / INDICATING SYSTEMS (ATA 31) PLANEVIEW MASTER OPERATING SYSTEM SOFTWARE UPDATE

SERVICE LETTER SL

Service Notification

[Docket No. 93-CE-37-AD; Amendment ; AD R1]

CAR 21 CERTIFICATION OF AIRCRAFT

Hawker 850XP. Supplement Pack

[Docket No. FAA ; Directorate Identifier 2016-NM-155-AD; Amendment. AGENCY: Federal Aviation Administration (FAA), DOT.

SERVICE BULLETIN TITLE NAVIGATION - GARMIN G1000 ENHANCED SEARCH AND RESCUE ENABLEMENT

NUMBER 008 PLACARDS AND MARKINGS (ATA 11) MAXIMUM ZERO FUEL GROSS WEIGHT - 48,000 POUNDS PLACARD INSTALLATION

SERVICE LETTER. Single Engine SEL TITLE NAVIGATION - ALTIMETER INSPECTION

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

GUERNSEY AVIATION REQUIREMENTS. (GARs) CERTIFICATION OF AIRCRAFT PART 21

[Docket No. FAA ; Directorate Identifier 2015-NM-101-AD; Amendment. AGENCY: Federal Aviation Administration (FAA), DOT.

[Docket No. FAA ; Product Identifier 2018-NM-047-AD; Amendment ; AD ]

SERVICE BULLETIN. The airplanes that follow that are equipped with the Garmin G1000 Nav III Avionics Option and the WAAS installed with SB

SERVICE BULLETIN TRANSMITTAL SHEET HC-SB Propeller - Hub Pitch Change Bore

[Docket No. FAA ; Directorate Identifier 2015-NM-101-AD; Amendment ; AD ]

SERVICE BULLETIN. NOTE: SL should be accomplished in conjunction with this service bulletin.

[Docket No. FAA ; Product Identifier 2017-NM-098-AD; Amendment ; AD ]

[Docket No. FAA ; Directorate Identifier 2012-NM-136-AD] AGENCY: Federal Aviation Administration (FAA), DOT.

SERVICE LETTER TITLE EQUIPMENT/FURNISHINGS - AMSAFE AIRPLANE FLIGHT MANUAL SUPPLEMENT

GULFSTREAM AEROSPACE CORPORATION

2. CANCELLATION. AC 39-7B, Airworthiness Directives, dated April 8, 1987, is canceled.

Single Engine Service Bulletin SEB07-5 Revision 1, Pilot and Copilot Secondary Seat Stop Installation.

[Docket No. FAA ; Product Identifier 2017-NM-094-AD; Amendment ; AD ]

SUPPORT SERVICES GMBH

Navigating your way through the process. Presented by: Mike Mertens DAR ODA MRA Administrator Manager of Regulatory Compliance Duncan Aviation

[Docket No. FAA ; Directorate Identifier 2014-NM-075-AD; Amendment. Airworthiness Directives; ATR GIE Avions de Transport Régional Airplanes

Major Repairs & Major Alterations MAJOR REPAIRS AND ALTERATIONS TO PROVIDE AVIATION TECHNICIANS A FRANK DISCUSSION ON MAJOR ALTERATIONS

[Docket No. FAA ; Directorate Identifier 2015-CE-018-AD] Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.

[Docket No. FAA ; Directorate Identifier 2007-CE-004-AD; Amendment ; AD ]

[Docket No. FAA ; Product Identifier 2018-NM-039-AD] AGENCY: Federal Aviation Administration (FAA), DOT.

COMPLIANCE WITH THIS PUBLICATION IS MANDATORY

AIRWORTHINESS NOTICE

[Docket No. FAA ; Product Identifier 2017-NM-095-AD; Amendment ; AD ]

Amendment Docket No. FAA ; Directorate Identifier 2010-NM-256-AD

SERVICE LETTER REVISION

Amendment Docket No. FAA ; Directorate Identifier 2010-NM-099-AD

INSTRUCTIONS FOR CONTINUED AIRWORTHINESS INSTRUCTIONS FOR CONTINUED AIRWORTHINESS. A/C Make: Model: S/N: Reg. #: Revision: Date:

[Docket No. FAA ; Directorate Identifier 2012-NM-006-AD; Amendment ; AD ]

RECOMMENDED FIELD APPROVAL APPLICATION Portland Flight Standards District Office

Amendment Docket No. FAA ; Directorate Identifier 2011-NM-234-AD

BAE SYSTEMS (OPERATIONS) LIMITED

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION N

BOMBARDIER, INC

SAAB AB, SAAB AEROSYSTEMS

[Docket No. FAA ; Directorate Identifier 2015-NM-006-AD; Amendment ; AD ]

[Docket No. FAA ; Product Identifier 2016-NM-200-AD; Amendment ; AD ]

CIRRUS AIRPLANE MAINTENANCE MANUAL

SERVICE LETTER COMMUNICATIONS - LINK CPDLC AND VHF ACARS CONFIGURATION VERIFICATION

Amendment Docket No. FAA ; Directorate Identifier 2002-NM-12-AD

FAA Technical Documentation Requirements

TABLE OF CONTENTS 1.0 INTRODUCTION...

AIRWORTHINESS ADVISORY CIRCULAR

[Docket No. FAA ; Product Identifier 2018-NM-030-AD; Amendment ; AD ]

[Docket No. FAA ; Directorate Identifier 2013-NM-063-AD; Amendment ; AD ]

[Docket No. FAA ; Product Identifier 2017-NM-050-AD; Amendment ; AD ]

[Docket No. FAA ; Product Identifier 2018-NM-129-AD; Amendment ; AD ]

[Docket No CE-24-AD; Amendment ; AD ] Airworthiness Directives; Cessna Aircraft Company Model 172RG Airplanes

[Docket No. FAA ; Directorate Identifier 2012-NM-065-AD; Amendment

[Docket No. FAA ; Product Identifier 2018-NM-176-AD; Amendment ; AD ]

[Docket No. FAA ; Product Identifier 2018-NM-075-AD; Amendment ; AD ]

[Docket No. FAA ; Product Identifier 2017-NM-072-AD; Amendment 39-

[Docket No. FAA ; Directorate Identifier 2016-NM-006-AD; Amendment ; AD ]

EXPORT AIRWORTHINESS APPROVALS

[Docket No. FAA ; Directorate Identifier 2015-CE-017-AD] SUMMARY: The FAA is correcting a notice of proposed rulemaking (NPRM) that

[Docket No. FAA ; Product Identifier 2018-NM-131-AD] AGENCY: Federal Aviation Administration (FAA), DOT.

[Docket No. FAA ; Product Identifier 2016-NM-208-AD; Amendment ; AD ]

[Docket No. FAA ; Product Identifier 2017-NM-111-AD; Amendment ; AD ]

[Docket No. FAA ; Product Identifier 2017-NM-107-AD; Amendment ; AD ]

[Docket No. FAA ; Product Identifier 2015-NM-195-AD; Amendment ; AD ]

[Docket No. FAA ; Directorate Identifier 2013-NM-081-AD] Airworthiness Directives; The Boeing Company Airplanes

HAWKER BEECHCRAFT CORPORATION MODELS B300 AND B300C (C-12W) AIRPLANES

Transcription:

Beec hcraft RECOMMENDED TITLE: ELECTRICAL POWER - CIRCUIT BREAKER SWITCH REPLACEMENT 1. Planning Information A. Effectivity (1) Airplanes Beechcraft Bonanza Models F33 and G33, Serials CD-1235 through CD-1304; F33A, Serials CE-290 through CE-1791; F33C, Serials CJ-26 through CJ-179; V35B, Serials D-9069 through D-10403; A36TC and B36TC, EA-1 through EA-695; Beechcraft Model A36 Bonanza, Serials E-185 through E-3629, E-3631 through E-3635. Beechcraft Baron Models 95-B55, Serials TC-1913, TC-1936 through TC-2456; D55, Serials TE-452 through TE-767; E55, Serials TE-768 through TE-1201; A56TC, Serials TG-84 through TG-94; 58P, Serials TJ-3 through TJ-497; 58TC, Serials TK-1 through TK-151; Beechcraft Model 58 Baron, Serials TH-1 through TH-2124. Beechcraft Model 77 Skipper, Serials WA-1 through WA-312. If you are no longer in possession of the airplane, please forward this information to the present owner. (2) Spares B. Reason Spare units according to the original part numbers listed in Paragraph 2.C Raytheon Aircraft Company (RAC) has received reports from piston ownerloperators of circuit breaker toggle switches becoming overheated. These switches are utilized in various electrical systems throughout the airplane. This Service Bulletin is being issued to announce a replacement circuit breaker toggle switch with improved internal isolation, therefore, eliminating the potential overheating condition. The export of these commodities technology or software are Subject to the US Export Admit- Both classes are mailed to lstration Regulations Diversion contrary to U S law is prohibited For guidance on export (a) RAC Authonzed Service Centers Control requirements contact the Commerce Departments Bureau of Export Administration (b) Owners of record on the FAA Aircraft Registration Branch Llst and the RAC at 202 482 4811 or at w w bxa doc QOV International Owner Notif~cation/Registration Service List Ravtheon Aircraft Comuanv (RACI issues Service lnformatlon for the benefit of owners and (c) Those having a publications subscnptlon fixed base operators in the form of two classes of Service Bulletins The flrst class Mandatory Service Bulletlns (red border) includes changes inspections and modiflcatlons that could Information On Owner Notification Service Or subscription can be Obtained any RAC Center As MandatoryServ'ce Bulletins and Buletlns are issued affect safety or crashworthlness RAC also Issues Service Bulletlns with no red border which are designated as recommended or In the section the temporary notlflcatlon In the Service Bulletin Master Index should be made unt1 the index 1s rev~sed Warranty will be allowed only when specifically defined in the Service Bulletin and in bulletln In the case of recommended Service Bulletins RAC feels the changes accordance with the RAC warranty pollcy modifications improvements or Inspections will benefit the ownerloperator and although highly recommended Recommended Servlce Bulletlns are not considered mandatory at the ~~$,"~~~~~~~~~~~~~~~~,",i,"n",", time Of issuance In the case Of Optional Bulietins compliance with the changes only RAC Mandatory Service Bulletins Service Bulletinsand Kits may not be compatible with mod~fications ~mprovements or inspections IS at the owner/operatois discretion airplanes modlfled by STC ~nstallat~ons or modlficat~ons other than RAC approved klts ~~d,"~~~,",",":~,"r~~~,"it1,"~r","cw~,"d~~f~,","

C. Description This Service Bulletin provides replacement part number information for the circuit breaker toggle switch used throughout piston airplanes. D. Compliance Raytheon Aircraft Company recommends that this Service Bulletin be accomplished on condition as part replacement is required. E. Approval The engineering data contained in this Service Bulletin is FAA approved. F. Manpower The following information is for planning purposes only: Estimated man-hours: time varies per location of circuit breaker toggle switch. Suggested number of men: 1 man. The above is an estimate based on experienced, properly equipped personnel complying with this Service Bulletin. Occasionally, after work has started, conditions may be found which could result in additional man-hours. G. Weight and Balance None. H. Electrical Load Data Not changed. I. Software Accomplishment Summary J. References The appropriate chapter of the applicable model MaintenanceIShop Manual K. Publications Affected It is recommended that a note "See Service Bulletin No. 24-3735" be made in the following: The appropriate chapter of the applicable model Illustrated Parts Catalog. The appropriate chapter of the applicable model Wiring Diagram Manual. L. Interchangeability of Parts M. Warranty Credit

RayFheon Aircraft Company 2. Material Information A. Materials - Price and Availability Contact a Raytheon Aircraft Authorized Service Center for information B. Industry Support Not applicable C. Airplanes The following parts required for this modification may be ordered through a Raytheon Aircraft Authorized Service Center or RAPID: Original Part Number 35-3801 32-1 35-3801 32-3 35-3801 32-5 35-3801 32-7 35-3801 32-9 35-3801 32-1 1 35-3801 32-1 3 35-3801 32-1 5 35-3801 32-1 7 35-3801 32-1 9 35-3801 32-21 35-3801 32-23 35-3801 32-25 35-3801 32-27 35-3801 32-29 35-3801 32-31 35-3801 32-33 35-3801 32-35 35-3801 32-37 35-3801 32-39 Description Replacement Part Number 35-3801 32-61 35-3801 32-63 35-3801 32-65 35-3801 32-67 35-3801 32-69 35-3801 32-71 35-3801 32-73 35-3801 32-75 35-3801 32-77 35-3801 32-79 35-3801 32-81 35-3801 32-83 35-3801 32-85 35-3801 32-87 35-3801 32-89 35-3801 32-91 35-3801 32-93 35-3801 32-95 35-3801 32-97 35-3801 32-99

Original Part Number 35-3801 32-41 35-380 1 32-43 35-3801 32-45 35-3801 32-47 35-3801 32-49 35-3801 32-51 35-3801 32-53 Description Replacement Part Number 35-3801 32-1 01 35-3801 32-1 03 35-3801 32-1 05 35-3801 32-1 07 35-3801 32-1 09 35-3801 32-1 1 1 35-3801 32-1 13 Raytheon Aircraft Company expressly reserves the right to supersede, cancel andlor declare obsolete, without prior notice, any parts or publications that may be referenced in this Service Bulletin. D. Spares Refer to Paragraph 2.C. E. Reidentified Parts None. F. Tooling - Price and Availability 3. Accomplishment Instructions This Service Bulletin shall be accomplished as follows: A. Airplane NOTE Should any difficulty be encountered in accomplishing this Service Bulletin, contact Raytheon Aircraft Company at 1-800-429-5372 or 31 6-676-31 40. Observe all Warnings and Cautions contained in the aircraft manuals referenced in this Service Bulletin. Whenever any part of this system is dismantled, adjusted, repaired or renewed, detailed investigation must be made on completion to make sure that distortion, tools, rags or any other loose articles or foreign matter that could impede the free movement and safe operation of the system are not present, and that the systems and installations in the work area are clean. S8 24-3735

-- - SERVICE BULLETIN (1) Remove all power from the airplane and disconnect the battery. Display warning notices prohibiting reconnection of airplane electrical power. (2) Remove the existing circuit breaker toggle switch and replace with the new switch. Refer to Paragraph 2.C. (3) Reconnect the airplane battery, remove warning notices and restore power. (4) Perform test procedures on the applicable system serviced by the replaced circuit breaker toggle switch. Refer to the appropriate chapter of the applicable model MaintenanceIShop Manual. (5) Ensure all work areas are clean and clear of tools and miscellaneous items of equipment. (6) Return airplane to service. 6. Spares C. Record of Compliance Upon completion of this Service Bulletin, make an appropriate maintenance record entry.