TCDS E-269

E-269 Revision 18 CONTINENTAL AEROSPACE TECHNOLOGIES, INC. O-470-4, O-470-11, 11B, 11-CI (see NOTE 5), 11B-CI O-470-13, O-470-13A, O-470-15 September 19, 2022 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. E-269 Engines of models described herein conforming with this data sheet (which is part of type certificate No. 269) 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 O-470-11, -11B O-470-13, -13A O-470-4 O-470-15 Type Rating, ICAO or ARDC standard atmosphere Max. continuous hp., rpm, full throttle, at sea level pressure altitude Takeoff hp., 5 min., rpm, full throttle, at sea level pressure altitude Fuel (min. grade) aviation gasoline Lubricating oil Ambient air temperature Above 40° F. Below 40° F. Bore and stroke, in. Displacement, cu. in. Compression ratio Weight (dry), lb. 6HOA 190-2300 213-2600 80/87, ASTM D7547 (UL91), ASTM D7547 (UL94) Oil grade SAE 50 SAE 30 5.00 x 4.00 471 7:1 391 - - - 225-2600 225-2600 - - - - - - - - - - - - - - - - - - 415 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 190-2300 213-2600 - - - - - - - - - - - - - - - - - - 405 Page No. 1 2 3 Rev. No. 18 17 17 E-269 Page 2 Model (Continued) O-470-11, -11B O-470-13, -13A O-470-4 O-470-15 C.G. location (with starter, generator and fuel pump) Fwd. or rear face, engine crankcase, in. Below crankshaft, centerline, in. Beside crankshaft, centerline toward 1-3-5 side, in. Propeller shaft, SAE No. Carburetion Ignition, dual magnetos Timing, °BTC Spark plugs Oil sump capacity, qt. NOTES 8.8 .8  4 flange Bendix-Stromberg Model PS-5C (Continental No. 531857) Scintilla S6LN-21 (Continental NO. 531676) Right 26, Left 26 (See NOTE 6) 10; 7 usable 1, 2, 3, 4, 5, 6 9.8 .2 .1 Special integral flange 4-7/8 in. O.D. with six ½ in. bolt holes in 4 in. dia. circle - - - Scintilla S6LN-23 (Continental No. 533173) - - - - - - Dry 1, 2, 3, 4, 6 - - - - - - - - - - - - Bendix-Stromberg Model PS-5CD (Continental No. 538685) - - - - - - - - - - - - 1, 2, 3, 4, 6 - - - - - - - - - - - - Bendix-Stromberg Model PS-5C (Continental No. 625098) Scintilla S7LN-21 (Continental No. 531676) - - - - - - 10; 7 usable 1, 2, 3, 4, 6 “- - -“ indicates “same as preceding model” “” indicates “does not apply” Certification Basis Part 13 of the Civil Air Regulations effective August 1, 1949 as amended by 13-1. Type Certificate No. 269 issued January 19, 1951 Application for Type Certificate dated October 23, 1950 Production Basis P.C. 7 (All models except O-470-11B and -11B-C1) P.C. 508 (All models with “R” suffix on serial number except O-470-11B and -11B-C1) NOTE 1. Maximum permissible temperatures: Cylinder head O-470-11, -11B, -15 325° F. (spark plug gasket) 450° F. (bayonet thermocouple downdraft cooling) O-470-4, -13, -13A 465°F. (bayonet thermocouple downdraft cooling) Cylinder barrel 315° F. Oil inlet 225° F. NOTE 2. O-470-11, -11B, -13, -13A, -4, -15 O-470-11-CI, -11B-CI Fuel inlet pressure limits: Fuel inlet pressure limits: 9 to 15 p.s.i.g. Min. minus 2.25 p.s.i.g. Max. plus 10 p.s.i.g. Oil pressure limits: Oil pressure limits: 30 to 60 p.s.i.a. 30 to 60 p.s.i.a. E-269 Page 3 NOTE 3. The following accessory drive or mounting provisions are available: Original Accessory Type Dwg. No. Direction of Rotation* Speed Ratio to Crankshaft Maximum Torque (in.-lb.) Continuous Static Max. Overhang Moment (in.-lb.) Starter XIV-A AND 20004 C 1.0  3600 300 Generator (O-470-11 -11B, -15 XII-A AND 20002 C 2.37 500 2200 400 (O-470-13, -13A, -4) XII-A AND 20002 C 3.094 350 1000 400 Fuel Pump XIII-A AND 20003 CC .94 25 450  Tachometer XV-A AND 20005 CC .50 7 50  Fluid P Pump X AND 20000 C 1.43 100 800 25 Fluid P Pump XI-A AND 20001 C 1.45 250 1650 75 Spare XV-A AND 20005 CC .50 7 50  Governor XX AND 20010 C 1.03 125 825  *C - Clockwise viewing drive pad; CC - Counterclockwise NOTE 4. Model O-470-11B is identical to the O-470-11 except that it incorporates the model O-470-15 cylinder and piston assemblies. Model O-470-11 incorporates two 6th order dampers. Model O-470-13A is identical to the O-470-13 except that an additional tachometer drive is provided through the camshaft gear and incorporates one 5th and one 6th order crankshaft damper. Model O-470-15 is identical to the O-470-11 except that a four 6th order damper crankshaft is used with the same size propeller flange specified on the model O-470-13. Model O-470-15 incorporates propeller control provisions. Also, revised engine mount brackets and long skirt pistons are used with this engine. O-470-13 engines incorporating crankshaft with one 5th and one 6th order dampers have the numeral 5 stamped on the outer circumference of the crankshaft propeller flange. O-470-13 engines with two 6th order dampers have no numeral stamped on the flange. Model O-470-4 which was previously designated as O-470-13B is identical to the Model O-470-13A except for the carburetor. NOTE 5. Models O-470-11 and -11B are eligible for incorporation of Continental continuous flow fuel injection equipment No. 5843 replacing carburetion system, with a weight increase of approximately 3 lb. When this modification is accomplished the suffix letters “CI” are to be added to the model designation. 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: AC: SR83P, HSR83P, S88D, HS88, HSR88, SR88D Auto Lite: SH2M, SH15, SH15R, SH20, SH20A, SH200A BG: RB485S, 706S, 706SR, 919SR, 919SR5, RB955S, RB963S, HRB963S Champion RC26S, C27S, REM38P, RHM38P, RED39N, REM39N, RHD39N, RHM39N, RED40E, REM40E, RHM40E, ED41N, EM41N, EM42E Red Seal: SE190, SJ190, SE230, SJ230 NOTE 7. Model O-470-11 engines which have been modified in accordance with U.S. Army Aviation and Surface Material Command Work Requirement No. WR-55-2810-112-B(1) issued 5 April 1963 and revised 13 February 1964, and designated Model O-470-11A, are considered to be equivalent to and interchangeable with Model O-470-11. ...END...