TCDS E11EU

Page No. 1 2 Rev. No. 4 4 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION E11EU Revision 4 CONTINENTAL AEROSPACE TECHNOLOGIES, INC. RR O-240-A June 01, 2020 TYPE CERTIFICATE DATA SHEET NO. E11EU Engines of models described herein conforming with this data sheet (which is part of engine type certificate No. E11EU) 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 Federal Aviation Regulations provided they are installed, operated, and maintained as described by the approved manufacturer's manuals and other approved instructions. Type Certificate Holder Continental Aerospace Technologies, Inc. (Continental®) 2039 South Broad St. Mobile, Alabama 36615 Type Certificate Holder Record Continental Motors, Inc. Company name change January 1, 2020 (Continental Aerospace Technologies, Inc.) Teledyne Continental Motors Ownership & name change as of April 19, 2011 (Continental Motors, Inc.) Rolls-Royce transferred ownership to Teledyne Continental Motors on December 12, 1983. Model RR O-240-A Type 4HOA Rating, ICAO or ARDC standard atmosphere Max. continuous hp., rpm, full throttle at sea level pressure altitude 130-2800 Takeoff hp., rpm, full throttle at sea level pressure altitude 130-2800 Fuel (min. grade aviation gasoline) 100/130 Lubricating oil Lubricating oils qualified under SAE-J1899 or J1966 are considered qualified under Continental Spec MHS-24 MIL-L-22851 D. Eng. RD 2450 Ambient air temperature Oil grade Below 5°C SAE 30 Above 5°C SAE 50 Bore and stroke, in. 4.438 X 3.875 Displacement, cu. in. 240 Compression ratio 8.5:1 Weight (dry), lb. 246 C.G. location (with accessories) Fwd of mounting lug rear face, in. 5.043 Below crankshaft, in. 1.630 Propeller shaft ARP 502 Type 1 flange 4-7/8 in. o.d. by .31 in. thick with six-1/2 in. bolt holes in 4 in. dia circle E11EU Page 2 Carburetion Marvel-Schebler MA-3SPA IO 5067 Ignition, dual, magnetos Continental S4LN-21 or Slick 4001 Timing, °BTDC 20 Spark plugs Champion REM 38-E Lodge RSE/23/2R Lodge RS/26/IR Oil sump capacity, U.S. qt. Max. capacity 6 usable at 10° nose-up attitude 4 usable at 10° nose-down attitude 4 Certification basis CFR Part 21.29 and British Civil Airworthiness Requirements, Section C, Issue 6 of 15 June 1966, with other requirements as necessary to be equivalent to CFR Part 33 as amended by 33-1, 33-2, and 33-3. Date of application for Type Certificate: 18 February 1971. Type Certificate No. E11EU issued 7 July 1971. Notes: 1, 2, 3, NOTE 1. Maximum permissible cylinder head, barrel and oil inlet temperatures, 460°F, 290°F, and 240°F respectively. NOTE 2. Pressure limits for normal operation: Fuel at carburetor inlet 6 psig max. 0.3 psig min. Oil 30 to 60 psig running 10 psig at idle min. NOTE 3. The following accessory drive or mounting provisions are available: Type of Direction of Speed to Max. Torque (in.-lb.) Maximum Overhang Accessory Drive Rotation Crankshaft Cont. Static (in.lb.) Generator Automotive CCW 2.035:1 60 100 100 Starter Automatic engagement CW 35.77:1 - - - Vacuum pump AND 20,000 CCW 1:1 40 800 25 Fuel pump Automotive diaphragm - 0.5:1 - - - "CW" - Clockwise and "CCW" - Counter Clockwise (viewing drive pad) .....END......