TCDS E11EA

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