Service Support Manual - CSOBeech

IGNITION SWITCHESSTARTER SWITCHESAND DOOR LOCK KITSCONTINENTAL IGNITION SYSTEMSSERVICESUPPORTMANUALPublication X43002-1 2011 CONTINENTAL MOTORS, INC.AUG 2011

Supersedure NoticeThis manual revision replaces the front cover and list of effective pages for Publication Part No. X43002, datedOctober 1989. Previous editions are obsolete upon release of this manual.Effective Changes for this Manual0 . October 19891 . 30 August 2011List of Effective PagesDocument Title: Ignition/Starter Switches and Door Lock Kits Service Support ManualPublication Number: X43002-1Initial Publication Date: October 1989PageChangePageChangePageChangePageChangeCover. 1A. 1B. 1ii thru vi. 01 thru 11 . 0Published and printed in the U.S.A. by Continental Motors, Inc.Available exclusively from the publisher: P.O. Box 90, Mobile, AL 36601Copyright 2011 Continental Motors, Inc. All rights reserved. This material may not be reprinted, republished, broadcast, or otherwisealtered without the publisher's written permission. This manual is provided without express, statutory, or implied warranties. The publisher willnot be held liable for any damages caused by or alleged to be caused by use, misuse, abuse, or misinterpretation of the contents. Content issubject to change without notice. Other products and companies mentioned herein may be trademarks of the respective owners.AIgnition/Starter Switches and Door Lock Kits Service Support Manual31 August 2011

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WARN(Please note the following statements from FAA Advisory Circular 2 W 2 C entitled "EUGIBIUTY, QUALITY, AND IDENTIFICATIONOF APPROVED REPlACEMENTPAKIS):3.BACKGROUND. An increasingamount of replacement parts (including standard parts), materials,appliances, and instruments are offered for sale as being of aircraft quality when actually the quality andoriginof these unitsare unknown. Usersofsuch unttsareusuallynot awareof the potentialhazardsinvolvedwith replacement parts that are not eligible for use on certificated aircraft. Frequently such units aredeceptively advertised or presentedas "unused,""iike new," or "remanufactured."lhis impliesthat thequality of such units is equal to an original or appropriately repairedor overhauled unit.The performance rules for replacement of parts and materials used in the maintenance and alteration ofU.S. certificated aircraft are specified in FederalAviation Regulations (FAR) 43.13 and FAR 145.57. Theresponsibilityfor the continued airworthinessof the aircraft, which includes the replacement of parts, is theresponsibllityofthe ownerJoperatoras outlined in FAR 91.163, FAR 129.363, FAR 123.45, FAR 127.131and FAR 135.143 (a).4.IDENTIFICATIONOF THE APPROVED PARTS. Approved serviceable replacementparts are identified as follows:a.By an FAA Form 8130-3 (Formerly FAA Form 186), Airworthiness Approval Tag. An AirworthinessApproval Tag identifies a part or group of parts that have been approved by authorized FAArepresentatives.b.By an FAA Technical Standard Order (TSO) number and identiiicationmarkthat indicatesthe part orappliance has been manufacturedunder the requirementsof FAR 37.c.By an FAAlPMAsymbol, together with the manufacturer's name, trademark or symbol, part number,and the make and model of the type certificated product on which the part is eligible for installation,stamped on the part. An FAA Parts ManufacturerApproval (FAAIPMA) is issued under FAR 21.305.The make and model information may be on a tag attachedto the part.d.By shipping ticket, invoice, or other document which provides evidence that the part was producedby a manufacturer holding an FAA Approved Production InspectionSystem issued under FAR 21,Subpart F, or by a manufacturerholding an FAA ProductionCertificateissuedunder FAR 21, SubpartG.e.By a certificate of aiworthiness for export issued by a foreign government under the provisions ofFAR 21, Subpart NoKNOW YOUR SUPPLIER. lt has come to our attention that many reproduced parts andcomponents, particularly instruments which have been manufactured by persons other than the originalmanufacturer, are availablefor purchase and installationon U.S. certificatedaircraft. Often, an original partis usedas a sample to produce duplicates. The reproducedpartsappear to be as good as the original part;however, there are many unknown factors to be considered that may not be readily apparent to thepurchaser, i.e., heat treating, plating, inspections, tests and calibrations. All too often the faulty part is notdiscovered until a malfunction or an accident occurs.2-SUMMARY. In accordance with FAR'S, certification of materials, parts, and appliancesforreturnto servlce, for use on aircraft, is the responsibilityof the person or agency who signs the approval.The owner/operator, as denoted in paragraph 3 of this advisory circular, is responsible for the continuedairworthiness of the aircraft. To assure continued safety in aircraft Operation, it is essential that great carebe used when inspecting, testing, and determining the acceptability of all parts and materials. Particularcaution should be exercised when the identity of materials, parts, and appliances cannot be establishedor when their origin is in doubt.iiOctober, 3 989

System Support ManualIGNITIONISTARTER SWITCHES AND DOOR LOCK KITSTABLE OF CONTENTS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . iiINTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ivDESCRIPTION AND OPERATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . vDISASSEMBLY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Disassemble lgnitionlstarter Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Disassemble Type GM Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Disassemble Door Locks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1CLEANING AND INSPECTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1ASSEMBLY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2Assemble IgnitionIStarter Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2Assemble GM Type Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2TESTING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3Testing Ignitionlstarter Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3Testing GM Type Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3Testing Door Locks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3WARNINGINSTALLATION. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4ILLUSTRATED PARTS LIST . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5Equipment Covered . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .5Ignition Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6Switch and Door Lock Kits . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8Numerical Parts List . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .10Superseded and Discontinued Items . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .llIgnRionSwitchiLeadingParticularsRated to handle magneto primaryvoltage and/or 24 volts DC, 5 amps1,000 volts DC to ground. UseInsulationTest11-8950-2High Tension LeadTesterKi.Has removable leverto facilitateLever Type SwitchmountingHas disc tumbler iock with removableKey Type Switchkey. Available with matching doorlocks.50 hr salt test per Fed. linPasteType 20KdAdjustable for panelthickness toMounting.312 in.Position Indicating Dial Available as desired7 02.WeightHousingDie castContactsiiiOctober, 1989

System Support ManualIGNITION/STARTER SVVITCWES AND DOOR LOCK KITSINTRODUCTIONyour localTCM distributor or TCM field representative.Requests for copies of Teledyne Continental AircraftEngine Service publications should be made throughyour distributoror Teledyne Continental Motors, P. 0.Box 90, Mobile, AL 36601, Attn: Publications Department.GENERALA.This manual provides complete maintenance instructions with illustrated parts list for IgnitionIStarterSwitches and Door Lock Kis, manufactured byTeledyne Continental Motors, Aircraft Products, Mobile, Alabama 36601. TCM lgnition Switches controlmagneto operation. Many switches also include con- D. Good standardshop practices and safety precautionstrols for starting and eledric primer circuits. Doorshould be observed at all times to avoid damage tolocks are usedto secure cabin doors andlor baggageequipment and or injury to personnel.compartment doors. Switch and door lock kits incorporate matching lock mechanisms and are operated E. All maintenance instructions inthis manualhave beenby a single key for maximum convenience.shop verified. Shop verified procedures are those bywhich the manufacturer has accomplished all DisasB. This manual is subdivided with sub-heads as listed insembly, Assembly, Testingand Fault Isolationby perthe Table of Contents. Revision service may be proforming the functions described in this manual onvided by ordering Master Service Manual Formequipment identical in configurationto that described.X40000. TCM Ignition Systems Service Bulletins includedin Master Sewice Manualprovidecurrent infor- F. Dimensions are given in Standard Units. For refermation related to service, maintenance and technicalence, abbreviations used are listed in Table 1.support of the product. Service Bulletins 583 and 615have been incorporated intothis manual. This manual G. Numbers in parentheses following part nomqnclaturerefer to item numbers in illustrated Parts Llst Figure 1may be includedin Chapter 74-30of applicableGAMAformat publications.and 2 unless otherwise specified. Example: (1-5) isitem 5 in IPL Figure 1;(2-1) is item 1 in IPL Figure 2.C. These instructionsdo not cover all details or variationsin equipment nor do they provide for every possible Recommendations, cautions and warnings regardingcontingency to be met in connection with installation, maintenanceof this equipment are not intendedto imposeoperation, or maintenance. Shouldfurther information undue restrictions. They are inserted to obtain maximumbe desired or particular problems arise which are not performancefromthe equipment in accordance with safetycovered sufficiently for purchaser's purpose, contact and efficiency. Abuse, misuse, or neglect of any piece ofequipment can cause eventual failure. For an aircraft enTable 1gine it is obvious that a failure may have disastrous conseAbbreviationsquences. Failure to observe the instructions contained inthis manual constitutes unauthorized operation in areasunexplored during development of the engine, or in areasin which experience has proved to be undesirable or detrimental.Pound Incheslb in.NOTES, CAtmONS and WARNINGS are includedPound FourceIbfthroughout this manual. Application is as follows:IIIIIPounds per HourPPh1NOTE. .Special interest informationwhich may facilitatethe operation of equipment.IPounds per Square InchGagePsisICAUTION. . . lnformation issued to emphasize certainimtructions or to prevent possible damage to engine ber, 1989.Information which, If disregarded, rnayresult insevere damageto or destnrctionof the engineor endangementto personnet.WARNING.