# TCDS E11EA: Lycoming Engines - Type: Type certificate data sheet - Status: Current - Holder: Lycoming Engines - Revision: 3 - Revised: June 23, 2010 - Product: Engine - Certification basis: CAR 13 - Data sheet PDF: https://openairdocs.org/files/sha256/c0/65/c065fb606ed08c3be217e646b3238b4f34e96cd7ef87310de697902d6c98e64f - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7AE6A09749A52149862577CF00521114.0001 - Page: https://openairdocs.org/tcds/E11EA ## Models (1) As the data sheet lists them. - IVO-540-A1A ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page No. 1 2 Rev. No. 3 3 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION E11EA Revision 3 Lycoming Engines IVO-540-A1A June 23, 2010 TYPE CERTIFICATE DATA SHEET NO. E11EA Engines of models described herein conforming with this data sheet (which is a part of type certificate No. E11EA) and other approved data on file with the Federal Aviation Administration, meet the minimum standards for use in certificated aircraft in accordance with pertinent aircraft data sheets, and applicable portions of the Civil Air Regulations/Federal Aviation Regulations provided they are installed, operated, and maintained as prescribed by the approved manufacturer’s manuals and other approved instruction. Type Certificate Holder Lycoming Engines An Operating Division of AVCO Corporation Williamsport, Pennsylvania 17701 Type Certificate Holder Record Lycoming Div., AVCO Co rporation, Williamsport, PA. transferred TC E11EA to Lycoming Engines, An Operating Division of AVCO Corporation on June 23, 2010 Model Lycoming IVO-540-A1A Type 6HOA Vertical Mounted Direct Drive Rating Max. continuous, hp., r.p.m., full throttle at: Sea level pressure altitude 305-3200-3000 ft. Takeoff (5 min.) hp., r.p.m., full throttle at Sea level pressure altitude 305-3200-3000 ft. Fuel (min. grade aviation gasoline) 100/130 Lubricating oil (Lubricants should conform to the specifications Lycoming Spec. No. 301-G# as listed or later revisions thereto) Bore and stroke, in. 5.125 x 4.375 Displacement, cu. in. 541.5 Compression ratio 8.7:1 Weight (dry) lb. 435 C. G. location (dry and in horizontal position) from front face of crankcase, in. 14.84 Off propeller shaft C. L., in. .09 below .26 left Propeller shaft Six bolt flange type power takeoff Fuel injection RSA-1OAD1* Ignition, dual S6RN-200+ S6LN-204+ Ignition timing BTC 25 Spark plugs See NOTE 6 Oil pump capacity Dry sump NOTES 1, 2, 3, 4, 5, 6, 7 # See latest edition of Lycoming Service Instruction 1014 PAC (Precision Airmotive Corp) formerly Bendix TCM (Teledyne Continental Motors) formally Bendix E11EA 2 Certification basis: Production basis: Production Certificate No. 3. NOTE 1. Maximum permissible temperatures: Cylinder head (well type) 500 F Cylinder base See NOTE 7 Oil inlet 235 F NOTE 2. Fuel pressure limits Minimum Maximum Idle (min .) (at inlet to injector) 20 p.s.i. 45 p.s.i. 12 p.s.i. Oil pressure limits 65 p. s.i. 85 p.s.i. 25 p.s.i. NOTE 3. The following accessory provisions are available: Rotation Speed Ratio Maximum Torque Facing to (in. - lb.) Maximum Overhand Accessory Drive Pad Crankshaft C ontinuous Static Moment (in.-lb.) Starter C 1.000:1 - 12,000 300 Generator * C 2.600:1 500 2,200 400 Fuel Pump CC .803:1 25 450 25 Vacuum Pump C 1.219:1 200 800 25 Hydraulic Pump C 1.083:1 400 1,650 175 Tachometer CC .500:1 7 50 - “C” - Clockwise, “CC” - counter-clockwise * Inoperative as generator drive when fitted with had crank jaw. NOTE 4. This engine is approved for helicopter a pplication and operation in a vertical installation. NOTE 5. Basic Model. Six cylinder air-cooled, horizonta lly apposed, vertical direct drive, fuel injected, dry sump engine with internal piston cooling oil jets and side mounted AN type accessory drives. NOTE 6. Spark plugs: See latest revision of Lycomi ng Service Instruction No. 1042 for approved equipment. NOTE 7. Cylinder base temperature limits are not appli cable to engine models which incorporate internal piston cooling oil jets. ...END... Data Type Certificate Regulations & Amendments Model Date of Application No. E11EA Issued CAR 13 effective June 15, 1956 IVO-540-A1A December 2, 1964 April 20, 1965 as amended by 13-1, 13-2, 13-3 ``` ## ADs (22, in force first) - [AD 2026-04-11](https://openairdocs.org/ad/2026-04-11): Engine (Reciprocating) · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 605 more. Effective Apr 8, 2026 - [AD 2015-19-07](https://openairdocs.org/ad/2015-19-07): Fuel injector fuel lines · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1B and 187 more. Effective Nov 3, 2015 - [AD 2012-03-06](https://openairdocs.org/ad/2012-03-06): Fuel servo diaphragm · Continental Motors 6-260-A, 6-285-A, 6-285-B and 482 more. Effective Feb 24, 2012 - [AD 2009-02-03](https://openairdocs.org/ad/2009-02-03): Fuel injection servos · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 261 more. Effective Feb 9, 2009 - [AD 2004-10-14](https://openairdocs.org/ad/2004-10-14): Crankshaft gear · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 642 more. Effective Jun 25, 2004 - [AD 97-15-11](https://openairdocs.org/ad/97-15-11): Cylinder kits · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 538 more. Effective Aug 12, 1997 - [AD 95-07-01](https://openairdocs.org/ad/95-07-01): Connecting Rod Bolt · Lycoming Engines AEIO-360-A1E, AEIO-360-B1G6, AEIO-360-H1A and 177 more. Effective Apr 12, 1995 - [AD 92-12-05](https://openairdocs.org/ad/92-12-05): Piston Pins · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 532 more. Effective Jul 10, 1992 - [AD 80-04-04 R1](https://openairdocs.org/ad/80-04-04-R1): Crankshaft Flange Bolts · Lycoming Engines IVO-540-A1A, TIVO-540-A2A, TVO-435-A1A and 38 more. Effective Aug 18, 1980 - [AD 79-04-05](https://openairdocs.org/ad/79-04-05): Regulator Diaphragm Stem Assembly · Lycoming Engines AEIO-320-D1B, AEIO-320-E1A, AEIO-320-E1B and 215 more. Effective Sep 26, 1979 - [AD 78-23-10](https://openairdocs.org/ad/78-23-10): Center Body Bellows Seal Assembly · Lycoming Engines AEIO-320-D1B, AEIO-320-E1A, AEIO-320-E1B and 218 more. Effective Nov 7, 1978 - [AD 75-09-15](https://openairdocs.org/ad/75-09-15): Fuel Starvation To The Engine · Lycoming Engines AIO-320-A1A, AIO-320-A1B, AIO-320-A2A and 130 more. Effective Apr 30, 1975 - [AD 73-05-01](https://openairdocs.org/ad/73-05-01): Connecting Rod Bearing Assemblies · Lycoming Engines IVO-540-A1A, TIVO-540-A2A, TVO-540-A1A and 21 more. Effective Jul 9, 1974 - [AD 73-10-02](https://openairdocs.org/ad/73-10-02): Bendix Fuel Injectors · Bendix Fuel Injectors, AIO-320-A1A, AIO-320-A1B and 88 more. Effective May 16, 1973 - [AD 66-06-03](https://openairdocs.org/ad/66-06-03): Connecting Rod Assemblies · Lycoming Engines GO-435-C2 (O-435-17), GO-435-C2A, GO-435-C2A2 and 317 more. Effective Jan 16, 1969 - [AD 68-08-08](https://openairdocs.org/ad/68-08-08): Hydraulic Valve · Lycoming Engines IGSO-480-A1A6, IGSO-480-A1B6, IGSO-480-A1C6 and 44 more. Effective May 19, 1968 - [AD 2024-21-02](https://openairdocs.org/ad/2024-21-02) (historical): Engine (Reciprocating) · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 548 more. Effective Dec 5, 2024 - [AD 2011-26-04](https://openairdocs.org/ad/2011-26-04) (historical): Externally mounted fuel injector fuel lines · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1B and 186 more. Effective Jan 25, 2012 - [AD 2011-15-10](https://openairdocs.org/ad/2011-15-10) (historical): Fuel servos · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 256 more. Effective Aug 16, 2011 - [AD 2008-14-07](https://openairdocs.org/ad/2008-14-07) (historical): Externally mounted fuel injector fuel lines · Textron Lycoming, AVCO AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1B and 185 more. Effective Aug 14, 2008 - [AD 2008-08-14](https://openairdocs.org/ad/2008-08-14) (historical): Fuel injection servo plugs · Superior Air Parts AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 242 more. Effective Apr 29, 2008 - [AD 2002-26-01](https://openairdocs.org/ad/2002-26-01) (historical): Fuel injector fuel lines · Textron Lycoming, AVCO IGO-480-A1B6, IGO-540-B1A, IGO-540-B1C and 178 more. Effective Jan 31, 2003 ## Registered aircraft by registry model (OpenAirDocs) - [Lycoming IVO-540-A1A](https://openairdocs.org/engine/lycoming-ivo-540-a1a): 0 aircraft (registry code 41965) ## STCs approved under this data sheet (16) - [STC SE04349CH](https://openairdocs.org/stc/SE04349CH): Installation of SureFly electronic ignition. SureFly Partners Ltd. - [STC SE01954SE](https://openairdocs.org/stc/SE01954SE): Installation of engine crankcase seal.. Ly-Con Rebuilding Company - [STC SE01966WI](https://openairdocs.org/stc/SE01966WI): Use of GAMI G100UL High Octane Unleaded Avgas in spark ignition piston aircraft engines. General Aviation Modifications Inc. - [STC SE8628SW](https://openairdocs.org/stc/SE8628SW): Installation of oil nozzles for lubrication of cam and filters.. Cygnet Aerospace Corp - [STC SE09445SC](https://openairdocs.org/stc/SE09445SC): Installation of fuel injector nozzles.. General Aviation Modifications Inc. - [STC SE1339SW](https://openairdocs.org/stc/SE1339SW): Modify pistons to Drawings 11007 and 11015; piston rings. Continental Motors, Inc. - [STC SE4408SW](https://openairdocs.org/stc/SE4408SW): Miscellaneous engine cylinder replacement parts.. Continental Motors, Inc. - [STC SE8776SW](https://openairdocs.org/stc/SE8776SW): Installation of coated cylinders and piston rings.. Continental Motors, Inc. - [STC SE7582SW](https://openairdocs.org/stc/SE7582SW): Grinding of high compression NITRIDED Cylinders to .010 oversize, as an alternative to chrome plating or rebarreling, and the installation of SL10207 P10 Piston, SL74241 P10 Top and second compression ring, and SL 73857 P10 oil control ring. Superior Air Parts, Inc - [STC SE00890LA](https://openairdocs.org/stc/SE00890LA): Installation of Nickson's cylinder barrels on Lycoming reciprocating engine models.. Nickson's Machine Shop Inc - [STC SE09492SC](https://openairdocs.org/stc/SE09492SC): Installation and usage of Exxon 20W50 multigrade aircraft engine oil conforming to Exxon Oil formulation WS-3013.. Exxon Company USA - [STC SE8023SW](https://openairdocs.org/stc/SE8023SW): Installation and usage of AEROSHELL. Shell Development Co - [STC SE452NE](https://openairdocs.org/stc/SE452NE): Installation and usage of 'Mobil AV 1' aviation oil.. Mobil Research & Development Corp - [STC SE5879SW](https://openairdocs.org/stc/SE5879SW): Use of Phillips X/C II 20W-50 and25W-60 oil (OSS 55875) in all Avco reciprocating aircraft engines from 65 to 450 BHP.. Phillips Petroleum Co - [STC SE5924SW](https://openairdocs.org/stc/SE5924SW): Installation of stainless steel replacement exhaust studs on AVCO engines.. Perrigo & Steele Aircraft Engr Company - [STC SE80NE](https://openairdocs.org/stc/SE80NE): Installation and usage of Bel-Ray synthetic aviation oil, Bel-Ray Aero 1, (nonsupercharged), horizontally opposed direct drive, aircraft engines of 350 hp. or less.. Bel-Ray Company, Inc --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.