TCDS E-241

E-241 Revision 8 CONTINENTAL AEROSPACE TECHNOLOGIES, INC. A100-1 A100-2 September 19, 2022 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. E-241 Engines of models described herein conforming with this data sheet (which is part of type certificate No. E-241) 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 provided they are installed, operated and maintained as prescribed 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.) Model A-100-1 A-100-2 Type 6H0A - - Rating, ICAO or ARDC standard atmosphere Max. continuous hp., r.p.m., in. Hg at sea level pressure altitude 100-2350 - - Takeoff hp. (5 min.) r.p.m., full throttle at sea level pressure altitude Fuel (min. grade aviation gasoline) 100-2350 73, ASTM D7547 (UL91), ASTM D7547 - - - - (UL94) Bore and stroke, in. 3.875 x 3.625 - - Displacement, cu. in. 256 - - Compression ratio 6.3:1 Weight (dry), lb. 249 250 C.G. location (with starter & generator) From rear mounting bushing centerline, in. 6.1 - - Below propeller shaft, in. 1.6 - - Propeller shaft, SAE No. 10 No. 3 flanged Carburetion Stromberg NA-S03A1 for gravity - - systems, Eq. No. 50335 for pump systems Eq. No. 36020 Ignition, dual magnetos Continental SF6LN-8 - - Timing, °BTC Right 28, Left 30 - - Spark plugs See NOTE 3 - - Oil sump capacity, qt. 8 - - NOTES 1,2,3 1,2,3 "- -" indicates "same as preceding model." Certification basis CAR 13 effective August 1, 1941 Type Certificate No. 241 issued October 11, 1945 for Model A-100-1; Model A-100-2 added October 9, 1946. Production basis Production Certificate No. 7 Page No. 1 2 Rev. No. 8 7 E-241 2 NOTE 1. Maximum permissible temperatures: Cylinder head bayonet thermocouple 550°F. Cylinder barrel 350°F. Oil inlet 220°F. NOTE 2. The following typical engine accessories are eligible at weight increases indicated: Starter Delco-Remy (No. 1109656) P/N 50309 Weight (lb.) 16 Generator Delco-Remy (No. 1101876) P/N 40435 10 Fuel Pump AC Diaphragm, P/N 40585 or 4552 2 NOTE 3. The following spark plugs or those listed in Section 6-4.9 of the latest revision of M-0, Standard Practice Maintenance Manual, are approved for use on these engines: Champion C-26-S, C-27, C-27-S, D41N, EM41N, M41N, M42E, EM42E .....END.....