TCDS E3IN

E3IN Revision 8 CONTINENTAL AEROSPACE TECHNOLOGIES, INC. RR C90-8F, -8FJ RR C90-12F, -12FH, -12FJ, -12FP RR C90-14F, -14FH, -14FJ, -16F RR O-200-A, O-200-B, O-200-C September 19, 2022 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. E3IN Engines of models described herein conforming with this data sheet (which is part of type certificate no. E3IN) 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.) Rolls-Royce transferred ownership to Teledyne Continental Motors on December 12, 1983. Model RR C90-8F RR C90-12F, -14F, -16F RR O-200-A, -B, -C Type 4HOA - - - - Rating, standard atmosphere Maximum continuous hp, rpm 90-3475 - - 100-2750 at sea level pressure altitude Takeoff hp, 5 min, rpm, full throttle, 95-2625 - - 100-2750 at sea level pressure altitude Fuel (minimum grade aviation gasoline) 80/87, ASTM D7547 - - - - (UL91), ASTM D7547 (UL94) Lubricating oil, ambient air temperature Oil Grade Below 40°F SAE 20 - - - - Above 40°F SAE 40 - - - - Bore and stroke, in. 4.062 X 3.875 - - - - Displacement, cu. in. 201 - - - - Compression ratio 7:1 - - - - Weight (dry) lb. 184 188 190 C.G. location (with accessories) Fwd. of rear face of mounting lugs, in. 6.2 4.6 - - Below crankshaft center line, in. 1.5 1.3 1.2 Propeller shaft, SAE No. 1 Flange - - - - Carburetion (see Note 4 for injectors) Marvel Schebler MA-3SPA (Continental P/N 627367) or Marvel-Schebler MA-3SPA (Continental P/N 627143) Bendix-Stromberg NA-S3A1 (Continental P/N 530625, 530726, 531126, 530846, 531157) Page No. 1 2 3 Rev. No. 8 7 6 E3IN 2 Model RR C90-8F RR C90-12F, -14F, -16F RR O-200-A, -B, -C Ignition 2 Continental S4RN-21 or - 2 Continental S4LN-21 or - 1227, or 2 Continental 1227 or 1 ea. S4LN-200 and - S4LSC-21 204; Slick-Electro 447 magnetos or 2 Continental S4LSC-21 Timing, °BTC 26 Top, 28 Bottom - - 28 Top, 28 Bottom Spark plugs See Note 6. - - - - Oil sump capacity, qt. 5 or 6 - - - - NOTES 1 through 7 1, 2, 3, 4, 6, 7 1, 2, 3, 4, 6, 7 "- -" indicates "same as preceding model." Certification basis CAR 10 and British Civil Airworthiness Requirements Section C (BCAR Section C is equivalent to CAR part 13, effective June 15, 1956, as amended by 13-1 through 13-3, effective October 1, 1959). Type Certificate No. E3IN issued April 2, 1963, amended October 1, 1964, and August 14, 1967, Date of application for Type Certificate: May 18, 1962. NOTE 1. Maximum permissible temperatures: C90 Series O-200 Series Cylinder head 525°F 525°F Cylinder barrel 275°F 290°F Oil inlet 225°F 225°F NOTE 2. Carburetor fuel inlet pressure limits: MA-3SPA (Continental P/N 627367 and 627143) for gravity or pump system, minimum 7.5 in. fuel head differential between carburetor fuel inlet fitting and float bowl chamber, maximum 6 psig. NA-S3A1 (Continental P/N 530625, 530726 and 531126) for gravity system minimum 19 in. fuel head differential between carburetor fuel inlet fitting and float bowl chamber, maximum 4 psig. NA-S3A1 (Continental P/N 530846 and 531157) for pump system, minimum 2 psig, maximum 4 psig. C90 Series O-200 Series Oil pressure limits: 30 to 40 psig 30 to 60 psig Minimum idling with hot oil 10 psig NOTE 3. The following accessory drive or mounting provisions are available: Accessory Direction of Rotation Speed Ratio to Crankshaft Max. Torque (in.-lb.) Maximum Overhang Moment (in.-lb.) Continuous Static Tachometer Generator Starter **Vacuum pump ***Fuel pump (diaphragm) C 0.500:1 7 50 25 CC 2.035:1 60 600 100 C 35.7:1 CC 1.0:1 100 800 25 0.500:1 Accessories previously listed in Note 3 are satisfactory for continued use with C90 series engines. * C - Clockwise viewing drive pad: CC - Counterclockwise. ** C90 - 16F and O-200 series engines only. *** Continental Eq. 5809 incorporating Continental P/N 40585 pump approved as part of type design of the O-200 series engine, AC fuel pump Continental P/N 631391, available as optional equipment on C90-16F. NOTE 4. The C90-8F is identical to the C90-12F model except that the accessory section does not incorporate provisions for generator and starter drives. The C90-14 models incorporate Lord type engine mounts which are not interchangeable with C90-12 models due to different machining of the engine mounting lugs on the engine crankcase. The C90-16F is similar to the C90-12F except that vacuum pump drive provisions have been added. The Model O-200-B is similar to the O-200-A except for special crankshaft and crankcase providing for thrust application toward the engine only. The Model O-200-C is similar to the O-200-A except for incorporation of provisions to supply oil pressure to a controllable pitch propeller through the crankshaft from an external boss on the crankcase. 3 E3IN Those C90 series models listed in the heading of this data sheet, suffixed by letters H, J, and P, differ from the basic model designation as follows: "H" denotes a special SAE No. 1 flange crankshaft and special crankcase for the installation of a hydraulically operated controllable pitch propeller requiring oil supply through the crankshaft. "J" denotes incorporation of Model B-46 Ex-Cell-O fuel injector, P/N 530499, or American Bosch Model PGC-4A-95A2, P/N 534505, at a weight increase of 4 lbs. over the corresponding carburetor equipped engine. "P" denotes pusher installation incorporating special crankshaft and thrust bearing. Oil sump gauge rods will be marked as per installer's requirements. NOTE 5. Bendix-Stromberg NA-S3A1 carburetor, P/N 530726, eligible only on Piper PA-11 airplanes equipped with Piper mufflers. NOTE 6. The following spark plugs and/or those listed in Section 6-4.9 of the latest revision of M-0, Standard Practice Maintenance Manual are approved on this engine: C90-8F, -12F, -14F, -16F AC HS483IR, SR83IR, HSR83P, A88, SR83P, HS88, S88, S88D, HSR88, SR88, SR88D Auto Lite 18A1, BR4, BR4S, BR4SB, SH15, H15, SH15R, SH20A, SH150, SH200A BG RB485S, 706, 706R, 706S, 706SR, 919SR5, RB955S Champion C26, C26S, C27, C27S, REM38P, REM38W, RHM38P, RHM38W, REM40E, RHM40E, ED41N, D41N, EM41N, M41N, EM42E, M42E Red Seal SA190, SE190, SJ190, SE230, SJ230 O-200-A, -B, -C AC HSR83IR, SR83IR, HSR83P, SR83P, A88, HS88, S88, S88D, HSR88, SR88, SR88D Auto Lite 18A1, SH15, H15, SH15R, SH20A, SH150, SH200A BG RB485S, 706, 706S, 919SR5, RB955S Champion C27, C27S, REM38P, REM38W, RHM38P, RHM38W, REM40E, RHM40E, ED4IN, D4IN, EM4IN, M4IN,, EM42E, M42E Red Seal SA190, SE190, SJ190, SE230, SJ230 ....END.....