TCDS E-267

Type certificate data sheet · Continental Aerospace Technologies, Inc. · Engine

Holder
Continental Aerospace Technologies, Inc.
Revision
13
Revised
September 19, 2022
Status
Current
Product
Engine
Certification basis
CAR 13
Models
4
Registered
993 aircraft

The release keeps the latest revision of each data sheet. Model names are as the data sheet lists them.

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Models · 4

ModelAlso known asNote
E225-8Formerly Continental, then Teledyne Continental Motors
E225-9Formerly Continental, then Teledyne Continental Motors
E225-4Formerly Continental, then Teledyne Continental Motors
E225-2Formerly Continental, then Teledyne Continental Motors

Airworthiness directives · 8

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Registered aircraft

Registry models that point at this data sheet, with their registered aircraft.

STCs approved under this data sheet · 30

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What the data sheet says

From the PDF’s text layer, line by line: tables lose their columns. The PDF is the record.

E-267 Revision 13 CONTINENTAL AEROSPACE TECHNOLOGIES, INC. E225-2, -4, -8, -9 September 19, 2022 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. E-267 Engines of models described herein conforming with this data sheet (which is part of type certificate No. 267) and other approved data on file with the Federal Aviation Agency meet the minimum standards for sue 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 E225-2 E225-4 E225-8 E225-9 Type Rating, ICAO or ARDC standard atmosphere 6H0 - - - - - - Max. continuous hp., r.p.m., full throttle at sea level pressure altitude Takeoff hp., 5 min., r.p.m. full throttle at sea 225-2650 225-2650 - - - - - - - - - - - - level pressure altitude Fuel (min. grade aviation gasoline) 80/87, ASTM D7547 - - - - - - Lubricating oil (UL91), ASTM D7547 (UL94) Ambient air temperature Above 40°F. Oil grade SAE 50 - - - - - - Below 40°F. SAE 30 - - - - - - Bore and stroke, in. 5.00 x 4.00 - - - - - - Displacement, cu. in. 471 - - - - - - Compression ratio 7:1 - - - - - - Weight (dry), lb. C.G. location (basic engine) Fwd. of rear face engine crankcase, in. 359 11.75 355 11.51 347 11.75 363 11.51 Below crankshaft centerline, in. 1.42 1.76 1.42 1.76 Propeller shaft, SAE No. 20 (Spline) - - - - - - Carburetion Ignition, dual magnetos Timing, °BTC Bendix-Stromberg Model PS5C (Continental No. 531857) Continental S6LN-21 or S6LSC- 21 or 1 ea. S6LN-200 and -204 Right 26°, Left 26° - - - - - - - - - - - - - - - - - - Spark plugs See NOTE 7 - - - - - - Oil sump capacity, qt. NOTES Dry 1,2,3,4,6,7 10 (7 usable) 1,2,3,4,5,6,7 Dry 1,2,3,4,5,6,7 10 (7 usable) 1,2,3,4,6,7 “- -“ indicates “same as preceding model” Page No. 1 2 Rev. No. 13 12 E-267 2 Certification basis CAR 13 effective August 1, 1949 Type Certificate No. 267 issued July 12, 1950 for Model E225-8; E225-9 added October 30, 1950; E225-2 added July 19, 1951; E225-4 added June 5, 1952. Date of Application for Type Certificate June 2, 1950. Production basis Production Certificates Nos. 7 and 508. NOTE 1. Maximum permissible temperatures Cylinder head 525°F. (spark plug gasket), 450°F. (well type thermocouple, downdraft cooling only) Cylinder barrel 290°F. Oil inlet 225°F. NOTE 2. Fuel inlet pressure limit 9 to 15 p.s.i. Oil pressure limits (normal operation) 30 to 60 p.s.i. Maximum (cold oil) 100 p.s.i. NOTE 3. Accessories such as generators, starters, fuel and vacuum pumps, etc., previously listed in NOTE 3, are satisfactory for continued use with these engines. As these are not integral engine accessories, they are not evaluated for approval during engine certification testing. The airworthiness of such accessories is substantiated during aircraft installation system approvals. The suitability of the accessory to the engine mounting provisions as described below, must be determined when processing such approvals. Accessory Type of Drive Direction of Rotation Speed Ratio to Crankshaft Max. Torque Continuous (in. -lb.) Static Maximum Overhang Moment (in. -lb) Generator Automotive CC 2.25:1 60 800 100 Starter Aircraft CC 1.15:1 2400 Fuel Pump AND 10000 CC 1.67:1 26 400 25 Tachometer AS 54 C 0.5:1 Optional AND 10000 C 1.364:1 90 600 65 NOTE 4. The cylinder assemblies on the E225-2 and -9 models have increased cooling fin areas and increased overall length over the cylinders on the -4 and -8 models. NOTE 5. E225-4 and -8 engines with S/N 30,001 thru 30,086 have two each 6th order dampers. Engines with S/N 30,087 and above have one each 5th and 6th order dampers. NOTE 6. E225 series engines are eligible for both tractor and pusher installations. NOTE 7. 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 HSR83IR, SR83IR, HSR83P, SR83P, A88, HS88, HSR88, SR88, S88, SR88D, S88D Auto Lite H15, SH15, SH15R, SH20A, SH200A BG RB485S, 706, 706R, 706S, 706SR, RB919SR5, RB955S Champion C27, C27S, REM38P, RHM38P, REM39N, REM40E, RHM40E, ED41N, D41N, EM41N, M41N, EM42E, M42E Red Seal SA190, SE190, SJ190, SE230, SJ230 ....END.....