TCDS E-245

Page No. 1 2 Rev. No. 6 6 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION E-245 Revision 6 CONTINENTAL AEROSPACE TECHNOLOGIES, INC. R9-A April 17, 2020 TYPE CERTIFICATE DATA SHEET NO. E-245 Engines of models described herein conforming with this data sheet (which is part of type certificate No. E-245) 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 R9-A Type R9-A - Direct Drive Impeller gear ratio 10.15:1 Rating, ICAO or ARDC, standard atmosphere Max. continuous hp., rpm, in.Hg. at: Critical altitude, ft. 500-2300-40.0-4000 Sea level pressure altitude 500-2300-41.5 Takeoff hp., 5 min., rpm, full throttle 525-2300-43.0 at sea level pressure altitude Fuel (aviation gasoline, minimum grade) 91 Lubricating oil Ambient air temperature Oil grade Above 40°F. SAE 50 Below 40°F. SAE 30 Bore and stroke, in. 5.0 X 5.5 Displacement, cu. in. 972 Compression ratio 6.3:1 Weight (dry), lb. 705 C.G. location Rear of center-line of cylinders 2.70 Below proeller shaft, in. .43 Propeller shaft, SAE No. 30 Carburetion Stromberg QD-9A3 Ignition, dual magnetos Continental SF9RN Timing, °BTC Right 29, Left 26 Spark plugs Champion RC-35S, R37S-1, REA37N, REB37N, RHA37N, RHB37E, RHB37N, R115 Applicable notes 1, 2, 3, 4 Certification basis CAR 13 effective August 1, 1941 Type Certificate No. 245 issued April 4, 1946 Production basis Production Certificate No. 7 E-245 Page 2 NOTE 1. Maximum permissible temperatures: Maximum Continuous Takeoff Cylinder head 450°F. 500°F. Cylinder barrel 320°F. 320°F. Oil inlet 185°F. 185°F. NOTE 2. The following accessory drive or mounting provisions are available: Direction of Speed Ratio to Maximum torque (in.-lb.) Original Accessory Rotation* Crankshaft Continuous Static Starter CC .8 6000 Generator C 3.12 150 1000 Fuel pump CC 1.0 25 450 Vacuum or hydraulic pump CC 1.333 100 1200 Vacuum or hydraulic pump CC 1.313 250 2250 Propeller governor C 1.118 125 1000 *C - Clockwise viewing drive pad; CC - Counter-clockwise NOTE 3. Shear type rubber mounts, P/N 402233, eligible for use with this engine with 15 lbs. additional weight per set of four mounts. NOTE 4. Engine P/N 105004 thru 105084 (excepting 105056, 105080, 105081 and 105082) incorporating rear counter weight damper pin P/N 401618 must have this pin replaced by damper pin P/N 402791 at first engine overhaul. .....END.....