INSTALLATION AND OPERATION MANUAL

Transcription

1 TSIO-550-B C E G CONTINENTAL AIRCRAFT ENGINE PERMOLD SERIES ENGINE INSTALLATION AND OPERATION MANUAL Publication OI-18 FAA APPROVED 2006 TELEDYNE CONTINENTAL MOTORS INCORPORATED NOV 2006

2 Supersedure Notice This manual revises information contained in TCM Form X30614, dated Oct 2005 to support TSIO-550 Permold series production engines. Previous editions are obsolete upon release of this manual. Effective Changes for this Manual Nov 2006 List of Effective Pages Document Title: Publication Number: OI-18 Initial Publication Date: 29 Nov 2006 Page...Change Page...Change Page... Change Page... Change i-viii thru thru thru thru thru thru thru A-1 thru A B-1 thru B C-1 thru C Published and printed in the U.S.A. by Teledyne Continental Motors. Available exclusively from the publisher: P.O. Box 90, Mobile, AL Copyright 2006 by Teledyne Continental Motors. All rights reserved. This material may not be reprinted, republished, broadcast, or otherwise altered without the publisher s written permission. This manual is provided without express, statutory, or implied warranties. The publisher will not be held liable for any damages caused by or alleged to be caused by use, misuse, abuse, or misinterpretation of the contents. Content is subject to change without notice. Other products and companies mentioned herein may be trademarks of the respective owners. ii

3 Service Document and Technical References Service Documents and technical information cited in this edition of TCM s Installation and Operation Manual (OI-18) are listed in the chart below. Information relevant to this engine series contained in these Service Documents has been incorporated in this manual. The full content of active TCM service documents is available on TCMLINK. Refer to Publication Access in Chapter 1 of this manual for TCMLINK details. Service Documents Incorporated in this Manual Service Document Subject Section Affected Chapter MHS-24, Ashless Dispersant Lubricating Oil Oil specifications Specifications and Operating Limits Chapter 2 MHS-24, Appendix Recommended Ashless Dispersant Aviation Engine Oils MHS-27,Engine Break-in and Preservation Oil M67-12, Overboost of Turbocharged Engines Break-in and preservation oil Break-in Oil Chapter 2 specifications Unscheduled Maintenance Inspections M88-10, Contaminated Fuels Unscheduled Maintenance Inspections M88-9, Lightning Strikes Unscheduled Maintenance Inspections M89-18, EGT Recommendations for Standard Engines Mixture Leaning Engine Operation Chapter 7 SIL93-11A, Service Document Format Service documents Publications Chapter 1 SIL93-15, General Practices for Installation of Lock Wire, Tab Washers, and Cotter Pins Standard Practices Standard Practices Appendix C MSB94-8A, Magneto to Engine Timing Engine timing Maintenance and Adjustments SB96-7C, Torque Limits Specific torque values Torque Values Appendix B SB96-11A, Propeller Strikes and Inspections Propeller Strikes Hydraulic Lock Hydraulic Lock SIL97-1, Airworthiness Limitations Airworthiness Limitations Airworthiness Limitations Chapter 3 SID97-3C, Procedures And Specifications For Adjustment Of Teledyne Continental Motors (TCM) Fuel Flow Calibration Fuel System Operational Check Continuous Flow Fuel Injection Systems SIL98-9A, Time Between Overhaul Periods SIL99-1, Engine Preservation for Active and Stored Aircraft Engine Specification and Service Life Engine preservation and returning an engine to service after storage Engine Description Periodic Inspections Placing an Engine in Service After Storage Chapter 2 Chapter 6 SIL99-2B, Current Listing of Sealants, Materials Throughout manual Chapter 2 Lubricants and Adhesives Authorized by TCM Chapter 6 iii

4 Service Documents Incorporated in this Manual Teledyne Continental Motors, Inc. Service Document Subject Section Affected Chapter SB99-8, Engine Fuel Injection System Fuel Injection system Engine Installation Chapter 4 Preservation storage SIL03-1, Cold Weather Operation Engine Preheating SIL03-2, Currently Active Approved Spark Plug Application Preheating procedures Spark plugs Engine Operation in Extreme Cold and subsections Engine Specifications and Operating Limits Chapter 7 Chapter 2 SB05-2, Overspeed Limitations Unscheduled Maintenance Inspections Chapter 7 SB05-7, TCM Position Tuned Fuel Injection Nozzles Scheduled maintenance, Fuel Injection System Parts Replacement SB05-10, TSIO-550-B, C, and E Maintenance and Overhaul Revision Turbocharger fastener torque SIL05-3, Engine Specification Numbers Engine Specifications Engine Description Chapter 2 SB06-1A, Fuel System Fuel Nozzle Fuel Injection System Parts Inspection and Replacement Replacement SIL06-3, Crankshaft Gear Retaining Screw Parts replacement SIL642B, Manufacturing Number Interpretation TCM (Bendix) Magneto Serial Numbers SB653, Hot Magneto Test Engine Operation Engine Shutdown Chapter 7 Service Bulletins Released After Publication TCM strives to provide clear, concise, and accurate information and instructions based on best known engineering data at the time of publication. Ongoing process improvements at TCM may change a specification or procedure after a manual is released. Service Documents, defined in Chapter 1, expedite customer notification and serve as the prevailing instruction over conflicting information until the new information is incorporated in the manual text. Such bulletins are part of TCM s Instructions for Continued Airworthiness. As bulletins are received, note the bulletin number, title, and applicable section affected by the bulletin in the blank cells below and insert a copy of the Service Bulletin behind the last page of this section. The following bulletins, released after this manual, affect and supplement the procedures herein. When performing procedures affected by the bulletins, review the bulletin content prior to commencing the task to ensure completion using the most current information and methods. TCM recommends placing a note at the beginning of the affected section in the manual as a reminder to review the service document. iv

5 Teledyne Continental Motors, Inc. Mandatory and Critical Service Bulletins Published After this Manual Document Number Title Affected Section(s) in this Manual Other Service Documents Published After This Manual Document Number Title Affected Section(s) in this Manual v

6 PREFACE Teledyne Continental Motors (TCM) provides Instructions for Continued Airworthiness based on the design, testing, and certification of engines and parts for which TCM is the holder of the Type Certificate (TC) or Parts Manufacturing Approval (PMA) issued by the Federal Aviation Administration (FAA). Instructions in TCM manuals, which include maintenance, repair limits, overhaul, and installation, are applicable only to engines and parts supplied by TCM. This manual, the Maintenance and Overhaul Manual, applicable service documents, and other related publications constitute the Instructions for Continued Airworthiness (ICAs) prepared by TCM and approved by the FAA. Pursuant to Federal Aviation Regulation (FAR) 43.13, each person performing maintenance, alteration, or preventive maintenance on the engine or accessories must use methods, techniques, and practices prescribed in the ICAs or other methods, techniques, and practices acceptable to the Administrator. Except for FAR part 43.3 authorized owner maintenance, TCM ICAs are written for exclusive use by FAA (or equivalent authority) licensed mechanics or FAA (or equivalent authority) certified repair center employees working under the supervision of an FAA licensed mechanic. Information and instructions contained in this manual anticipate the user possesses and applies the knowledge, training, and experience commensurate with the requirements to meet the prerequisite FAA license and certification requirements. No other use is authorized. Installation of non-tcm parts on a TCM engine constitutes a deviation from TCM type-design criteria. TCM has not participated in design, test, or certification of any non-tcm parts. TCM does not provide product manufacturing specifications to aftermarket parts manufacturers and accepts no liability for the suitability, durability, longevity, or safety of such parts installed on TCM engines. Installation of non-tcm parts on a TCM engine must be performed using Instructions for Continued Airworthiness prepared by the manufacturer and approved by the FAA for the subject installation. TCM ICAs must not be used for such parts. Service bulletins may contain general information or information specific to a group of engines or be in effect for a limited time frame. Service Bulletins may also contain advance changes to the ICAs. It is the responsibility of the organization/person maintaining or operating the engine to verify that current and complete information, including Service Bulletins, FAA Airworthiness Directives (ADs), and publications are used. To facilitate the use of current data, TCM provides information via the Internet on TCMLINK. The information available includes a listing of the latest manual versions, service bulletins, FAA ADs, and other information applicable to the ICAs. This information is free of charge to owners of TCM engines by registering as an Aviator Service Member. The latest manuals are available through TCMLINK to Fixed Base Operators (FBOs) who are TCM FBO Services subscribers. Information available through Aviator Services is also available through FBO Services. Hardcopies and service subscriptions are available from TCM. Refer to Publication Access listed in Chapter 1. vi

7 CONTENTS Chapter 1 - Introduction Chapter 2 - Engine Description Chapter 3 - Airworthiness Limitations Chapter 4 - Engine Installation Inspection and Service Chapter 6 - Engine Preservation and Storage Chapter 7 - Engine Operation Appendix A - Glossary... A-1 Appendix B - Torque Specifications... B-1 Appendix C - Standard Practices... C-1 vii

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