Continental Parts Catalog X30597A TSIO-LTSIO-360 Series

DEFINITIONS OF NOTES, CAUTIONS and WARNINGS NOTES, CA UTIONS and WARNINGS are defined for use in this manual as follows: NOTE ... Special interest information which may facilitate performance of a procedure or operation of equipment. CA UTION... .Used to emphasize certain information or instructions which if disregarded may result in damage to engine or accessories. WARNING Used to provide warning with respect to information and/or instructions which if disregarded will endanger personnel and/or severely damage the engine resulting in subsequent engine malfunction or failure. Notes, cautions and warnings do not impose undue restrictions. They are inserted to obtain maximum safety, efficiency and performance. Abuse, misuse or neglect of equipment can cause eventual engine malfunction or failure. Compliance with instructions and provisions in this manual is mandatory. Hi

CURRENT STATUS OF PAGES AS OF: JANUARY 1997 See "Manual Revisions," in the introduction section for distribution procedure. THE ORIGINAL DATE OF THIS PUBLICATION IS JANUARY 1997 INSERT LATEST PAGES; DESTROY SUPERSEDED PAGES WARNING If the user of this manual is uncertain whether all current revisions have been incorporated into the manual, contact Teledyne Continental Motors. DO NOT PERFORM ANY OPERATION. MAINTENANCE. INSTALLATION OR OTHER OP- ERATION UNTIL THE MANUAL HAS BEEN CONFIRMED TO BE CURRENT._ MODELS: LITSIO-360-RB FORM X30597A SUPPLEMENT I PAGE STATUS PAGE STATUS PAGE STATUS PAGE STATUS ALL ORIGINAL iii

WARNING BACKGROUND. Replacement parts, materials, appliances, and instruments may be sold as being of aircraft quality when actually the quality and origin of these units are unknown. Users of such units are usually unaware of potential hazards involved with replacement parts not eligible for use on certificated aircraft. Units may be deceptively advertised as "unused," "like new" or* "remanufactured." This implies the quality of such units is equal to an original, repaired or overhauled unit. Federal Aviation Regulations (FAR) 43.13 and FAR 145.57 specify performance rules for replacement of parts and materials used in maintenance and alteration of United States (US) certificated aircraft. As outlined in FAR 91.403, FAR 121.363, FAR 123.45, and FAR 135.143 (a), the ownerloperator is responsible for continued airworthiness of the aircraft which includes parts replacement. IDENTIFICATION OF THE APPROVED PARTS. Approved, serviceable replacement parts are identified by: a. A Federal Aviation Administration (FAA) Form 81 30-3 Airworthiness Approval Tag. An Airworthiness Approval Tag identifies a part or group of parts approved by authorized FAA representatives. b. An FAA Technical Standard Order (TSO) number and identification mark that indicates the part or appliance has been manufactured under the requirements of FAR 21 Subpart 0. C. An FAA Parts Manufacturer Approval (PMA) symbol, together with the manufacturer's name, part number and make and model of the type certified product on which the part might be installed, stamped on the part. An FAA I PMA is issued under FAR 21.305. The make and model information may be on a tag attached to the part. d. Shipping ticket, invoice or other document which verifies the part was manufactured by a facility holding an FAA Approved Production Inspection System issued under FAR 21 Subpart F or by a manufacturer holding an FAA Production Certificate issued under FAR 21 Subpart G. e. Certificate of airworthiness for export issued by a foreign govemnment under the provisions of FAR 21 Subpart N. KNOW YOUR SUPPLIER. Many reproduced parts and components are available for purchase and installation on US certified aircraft. Often, an original part is used as a sample to produce duplicates. The reproduced parts appear to be as good as the original part; however, many unknown factors are not readily apparent to the purchaser such as degree of heat treating, plating, inspections, tests and calibrations. Often the faulty part is not discovered until a malfunction or an accident occurs. SUMMARY. In accordance with FAR certification of materials, parts and appliances for return to service for use on aircraft is the responsibility of the person~iagency who signs the approval. The owner/operator is responsible for the continued airworthiness of the aircraft. To assure continued safety in aircraft operation, great care must be used when inspecting, testing and determining the acceptability of all parts and materials. Exercise extreme discretion to identify and establish the origin of materials, parts, and appliances. iv

NOTICE TO ALL USERS The following publication contains parts listings introduced by general information. It is important all personnel involved with part procurement and installation thoroughly read and understand the information provided. These instructions contain the information required to obtain replacement parts for the aircraft engine and must be followed carefully. Publication Format This publication is formatted for practical use and ease of reference. Chapter and page numbering are independent within each section so that revisions can be made by section without affecting the entire publication. A list of chapters is located at the begining of the manual and a chapter index is located at the begining of each chapter. This manual contains no warranties, either expressed or implied. Pnior to performing parts replacement, the mechanic must meet requirements of FAR 65 and must follow FAR Parts 43, 91 and 145 as applicable. Use this manual in conjunction with Teledyne Continental Motors (TCM) service documents, related publications, accessory manufacturer's instructions, FAR and FAA Advisory Circulars. WARNING This manual, the Service Documents, the Overhaul Manual and Maintenance Manual constitute the Instructions for Continued Airworthiness prepared by TCM as approved by the FAA, pursuant to FAR Part 33. As required by FAR § 43.13, each person performing maintenance, alteration or preventive maintenance on the engine or accessories must use the methods, techniques and practices prescribed in the Instructions for Continued Airworthiness. Failure to comply with the Instructions for Continued Airworthiness may result in engine malfunction, engine failure, injury or death. V

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Publication Table of Contents COVER PAGES Definition of Notes, Cautions and Warnings..... CFC Warning Statement.. .......... Status Page ................. Replacement Parts Warning........... Notice to all users . . . . . . . . . . . . . . PAGE *... ii ... ii .. iii . .iv Chapter Index CHAPTER F 1 Introduction....................... 2 Exhaust System..................... Ignition System ...... Fuel Injection System ... Induction System..... Air Conditioning ..... Electrical Charging System Starting System...... Accessory Case ..... Lubnication System .... Cylinders And Pistons ... Prankcase........ 13 Engine Drive Train 2AGE 1-1 2-1 3-1 4-1 5-1 6-1 7-1 8-1 9-1 10-1 11-1 12-1 13-1 3 4 5 6 7 8 9 10 1 1 12 vii ................ ................ ................ ................ ................ ..... ..... ..... ..... ..... ..... ..... ..... ..... ..... ..... ..... ..... ..... ..... ..... ..... .....

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CHAPTERI1 INTRODUCTION PAGE Introduction ....................... 1-2 Scope ......................... 1-2 Manual Revisions.....................1-2 List Of Abbreviations And Symbols . ............ 1-3 Related Publications....................1-3 Repair Parts Sets and Materials .. . . ... ... . . ... 14 SECTION 1-1 1-2 1-3 1-4 1-5 1-6 1-1

1-1 INTRODUCTION For a list of chapters contained in this manual refer to the Chapter Index on page vi. For a list of parts and figures contained in each chapter, see the first page of each chapter. The chapters, pages and figures contained in this publication are numbered consecutively. In this edition, currently available parts are listed for LITSIO-360-RB engines. If accessories or parts attached to any engine installed in an aircraft manufactured in the United States under a production model number do not appear in this catalog, determine whether they are available from the airframe manufacturer before placing an order with a Teledyne Continental Authorized Distributor. The system figure is followed by figures for assemblies that compose the particular system. The figures are illustrated in exploded form. Each figure has a figure index and parts listing of the components contained appearing on the same or adjacent page. WARNING The figures depicted in this publication are for illustration purposes only. They are not intended to be accurate detailed illustrations of any specific engine model, part or equipment. Index numbers that correspond with the numbers contained in the related figure are assigned to each part number. In the parts listings, the first column of each system or component identifies the figure number in the top left corner and the index number (following a dash) which identifies each part in numerical order. DO NOT ORDER PARTS BY INDEX NUMBERS. Use the part number which appears in the second column, and use the part name which appears in the third column under DESCRIPTION. Do not order a part that has "No Number' shown with the description, or that has "NS" (not sold) shown in the QUANTITY column. To replace a part "not sold," order the next higher level assembly. Pay particular attention to the quantity of parts required per engine or per assembly. Example: 6 cylinders per engine, 12 pushrods per engine, 2 pushrods per cylinder. Some customer specification model engines have certain part differences from the basic engine. Check the engine data plate model designation and specification number before ordering parts for the engine. When ordering parts use the description and model designation shown with the part number. This information is necessary to ensure correct part to assembly or assembly to engine application. Oversize parts must be ordered by the numbers listed herein with correct descriptions to avoid errors. Authorized Oversize parts are indicated by a suffix such as P003. Authorized Undersize parts are indicated by a suffix such as M005 after the part number. Repair Parts Sets are usually requested for overhaul work and should be ordered by set part numbers. See "Repair Parts Sets and Materials," Section 1-6. 1-2 SCOPE This publication contains information necessary to order factory replacement parts for the LITS10- 360-RB model engines. 1-3 MANUAL REVISIONS Teledyne Continental Motors Parts Catalogs are revised as necessary. Revisions to this catalog will be furnished to purchasers who fill out and return the registration post card located in the front of this catalog. The "Current Status of Pages" on Page iii contains a record of revisions to this catalog. Each issued change to this catalog includes an updated "Current Status of Pages." Upon receipt of a revision, remove the old "Current Status of Pages" and insert the new one. Each individual revised page contains the date of the change to that page. Accordingly, if the "Current Status of Pages" indicates that a page has been changed, that page in the catalog must be dated in agreement with the status page. Original pages in this catalog are not individually dated. 1-2

Continental Parts Catalog X30597A TSIO-LTSIO-360 Series

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