1 Publication X30617 2011 CONTINENTAL MOTORS, 2011IO-360-A, ABC, CBD, DB, ESG, GBH, HBJ, JBK & KBCONTINENTAL AIRCRAFT ENGINE MAINTENANCEANDOPERATOR SMANUALTECHNICAL CONTENT ACCEPTED BY THE FAA AIO-360 Series Engine Maintenance and Operator s Manual31 August 2011 Supersedure NoticeThis Manual revision replaces the front cover and list of effective pages for Publication Part No. X30617, datedJanuary 1994. Previous editions are obsolete upon release of this Changes for this Manual0 .. January 19941 .. 31 August 2011 List of Effective PagesDocument Title: IO-360 Series Engine Maintenance and Operator s ManualPublication Number: X30617 Initial Publication Date: January 1A .. 1i .. 1ii thru iv .. 01-1 thru 02-1 thru 03-1 thru 04-1 thru 05-1 thru 06-1 thru 07-1 thru 08-1 thru 09-1 thru 010-1 thru 011-1 thru 11-2.
2 012-1 thru 0 Published and printed in the by Continental Motors, exclusively from the publisher: Box 90, Mobile, AL 36601 Copyright 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 NOTICEC ontinental Motors engine operating instructions are generated prior to and independently of the aircraft operating instructions established by the airframe manufacturer.
3 Continental Motors operating instructions are developed using factory controlled parameters that are not necessarily the same as those specifications required to satisfy a specific aircraft I engine installation. Because of this difference the aircraft operator should use the airframe manufacturers operating instructions found in the Pilots Operating Handbook (POH) while operating the aircraft unless otherwise specified by the original airframe manufacturer. The operator must comply with all the instructions contained in this Manual and related publications in order to assure safe and reliable engine performance. Failure to comply will be deemed misuse, thereby relieving the engine manufacturer of responsibility under its warranty.
4 This Manual contains no warranties, either expressed or implied. The information and procedures contained herein provide the operator with technical information and instructions applicable to safe INDEX Chapter Page 1 Introduction .. 1-1 2 Detailed Engine Description .. 2-1 3 Engine Specifications and Operating Umits.. 3-1 4 Unpacking, Installation, Testing & Removal.. 4-1 5 Normal Operating Procedures .. 5-1 6 Emergency Operating Procedures .. 6-1 7 Abnormal Environmental Conditions .. 7-1 8 Service and Unscheduled Maintenance .. 8-1 9 Troubleshooting .. 9-1 10 Engine Preservation and Storage .. 10-1 11 Airworthiness Umitations .. 11-1 12 Engine Performance and Cruise Control .. 12-1 Ii FIGURE INDEX Figure No. Page 2-3 2-4 2-5 2-6 2-6 4-4 8-6 8-7 8-8 8-9 2-1 2-2 2-3 2-4 2-5 4-1 8-1 8-2 8-3 8-4 8-5 12-1 12-2 12-3 12-4 12-5 12-6 12-7 12-8 12-9 12-10 12-11 12-12 12-13 12-14 12-15 Lubrication Diagram Ignition system .
5 Fuel system Schematic Air Throttle & Metering Unit .. Fuel Injection Nozzle .. Installation Drawing .. Idle Adjustment Points . Master Orifice .. Static & Dynamic Seal . Differential Pressure Tester .. Ring Gap Location for Dynamic Seal Fuel Pressure vs. Brake Horsepower (A,AB) Sea Level Performance (A,AB) Altitude Performance (A ,A B) .. Sea Level Performance (C,CB,D,DB,G,GB,H,HB) . Altitude Performance (C,DB,D,DB,G,GB,H,HB) . Sea Level Performance (K,KB) Altitude Performance (K,KB) .. Sea Level Performance (J,JB) .. 8-10 12-4 12-5 12-6 12-7 12-8 12-9 . 12-10 .. 12-11 Altitude Performance (J,JB) .. 12-12 Fuel Flow vs. Brake Horsepower (C,CB,CB,D,DB,G,GB,H,HB,J,JB) .. 12-13 Fuel Flow vs. Brake Horsepower (K,KB) .. 12-14 Fuel Flow vs.
6 Brake Horsepower (ES) .. 12-15 Sea Level Performance Curves (ES) o 12-16 Altitude Performance (ES) .. 12-17 Metered Fuel Pressure vs. Fuel Flow (ES) .. 12-18 iii INTENTIONALLY LEFT BLANK Iv CHAPTER 1 INTRODUCTION Section Index Section Page 1-1 Scope .. 1-2 1-2 Related Publications .. 1-3 1-3 Abbreviations and Glossary of Terms .. 1-4 1-4 Manual Revisions.. 1-1 0 1-1 1-1 SCOPE Requirements, cautions and warnings regarding Operation of this engine are not intended to impose undue restrictions, but are inserted to enable the pilot to obtain maximum performance from the engine commensurate with safety and efficiency. Abuse, misuse, or neglect of any piece of equipment can cause eventual failure. In the case of an aircraft engine it should be obvious that a failure may have disastrous consequences.
7 Failure to observe the instructions contained in this Manual constitutes unauthorized Operation in areas unexplored during development of the engine, or in areas which experience has proved to be undesirable or detrimental. Notes, Cautions and Warnings are included throughout this Manual . Application is as follows: NOTE .. Special interest information which may facilitate the Operation of equipment. CAUTION ..Information issued to emphasize certain instructions or to prevent possible damage to engine or accessories. WARNING lnformation which, if disregarded, may result in severe damage to or destruction of the engi ne or endangerment to personnel. 1 2 1-2 RELATED PUBLICATIONS 1. Overhaul Manual for 10-360 Series Aircraft Engine.
8 Form X30594A. 2. Illustrated Parts Catalog for 10-360 Series Aircraft Engine. Form X30595A. 3. Teledyne Continental Motors Aircraft Engine Service Bulletins. 4. Fuel Injection Manual . Form X30593A. The above publications can be ordered through your Teledyne Continental Motors Distributor or ordered directly, from: Teledyne Continental Motors Aircraft Products P. O. Box 90 Mobile, AL 36601 If Pre-Paying send to the attention of Accounts Receivable For COD via UPS send to the attention of Publication Sales or call (205) 438-3411 Ext. 298/132 Accessory Manuals: 1. Magnetos 2. Alternator 3. Starter Bulletins: Service Manual Form X40000 Alternator Service Instructions Form X30531-3 Starter Service Instructions Form X30592 Bulletins that are issued to Distributors and subscribers from Teledyne Contiental Motors are divided into three separate groups: (1) Customer Information Bulletins; (2) Service Bulletin and (3) Mandatory Service Bulletins.
9 (1) Customer Information Bulletins are published to help provide the latest information on TCM marketing procedures, polices and product information. (2) Service Bulletins provide current information related to service, Maintenance and technical sup-port of the product. (3) Mandatory Service Bulletins are issued with required compliance information that may affect safety of flight. These bulletins are also available to owners, operations or Maintenance personnel on an annual sub-scription basis. NOTE .. Teledyne Continental Bulletins are easily distinguished by their title color: (1) Customer Informaiton Bulletins -Blue. (2) Service Bulletins -Black. (3) Mandatory Service Bulletins -Red. 1 .. 3 1-3 ABBREVIATIONS AND GLOSSARY OF TERMS Abbreviation ADMP Approx.
10 Bar. BSFC BSOC CW CCW C of Dia. EGT FAA Fig. Front Ft. FT-LBS gms Hex H20 Hg. hr. IN-LBS in. (") Left Side Lbs. Lockwire Man. MAP Max. Min. Terms After Bottom Center Absolute Dry Manifold Pressure Approximately After Top Center Barometric Before Bottom Center Brake Horsepower Brake Specific Fuel Consumption Brake Specific Oil Consumption Before Top Center Civil Air Regulations Center of Gravity Cubic Feet Per Minute Cylinder Head Temperature Clockwise Rotation Counterclockwise Rotation Degrees Celsius Degrees Fahrenheit Degrees of Angle Diameter Exhaust Gas Temperature Federal Aviation Administration Figure (Illustration) Propeller End of Engine Foot or Feet Full Throttle Foot Pounds Torque Gallons Per Minute Grams Hexagon Water Mercury Hour Inside Diameter Inch Pounds Torque Inches Side on which No's 2, 4 and 6 cylinders are located.
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