# TCDS E-267: Continental Aerospace Technologies, Inc. - Type: Type certificate data sheet - Status: Current - Holder: Continental Aerospace Technologies, Inc. - Revision: 13 - Revised: September 19, 2022 - Product: Engine - Certification basis: CAR 13 - Registered aircraft: 993, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/f7/25/f725c0fa618ac08e24eb1134d906a6847597b736133d669e3d123caf003a40e0 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/9F382452E3204985862588C600698E51.0001 - Page: https://openairdocs.org/tcds/E-267 ## Models (4) As the data sheet lists them. - E225-8 - E225-9 - E225-4 - E225-2 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text 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..... ``` ## ADs (8, in force first) - [AD 98-17-11](https://openairdocs.org/ad/98-17-11): Crankshafts · Continental Motors A-65-3, A-65-8, A75-8 and 90 more. Effective Oct 19, 1998 - [AD 97-21-02](https://openairdocs.org/ad/97-21-02): Cylinders · Continental Motors E165-2, E165-3, E165-4 and 61 more. Effective Oct 27, 1997 - [AD 63-15-01](https://openairdocs.org/ad/63-15-01): Exhaust Valves · Continental Motors E165-2, E165-3, E165-4 and 41 more. Effective Dec 31, 1969 - [AD 67-01-04](https://openairdocs.org/ad/67-01-04): Oil Filters · Full flow oil filter (Superior Flow STC SA401SW or 2 others). Effective Jan 2, 1967 - [AD 56-06-01](https://openairdocs.org/ad/56-06-01): Piston Pin Assembly · Continental Motors E165-2, E165-3, E165-4 and 41 more - [AD 60-06-04](https://openairdocs.org/ad/60-06-04): Generator Drive Gear · Continental Motors E165-2, E165-3, E165-4 and 12 more - [AD 60-12-01](https://openairdocs.org/ad/60-12-01): Piston Pins · Continental Motors E185-11, E185-8, E185-9 and 2 more - [AD 97-15-01](https://openairdocs.org/ad/97-15-01) (historical): Pistons · Teledyne Continental Motors E165-2, E165-3, E165-4 and 61 more ## Registered aircraft by registry model (OpenAirDocs) - [Continental E225 series](https://openairdocs.org/engine/continental-e225-series): 979 aircraft (registry code 17015) - [Continental E225-4](https://openairdocs.org/engine/continental-e225-4): 7 aircraft (registry code 17162) - [Continental E225-8](https://openairdocs.org/engine/continental-e225-8): 7 aircraft (registry code 17163) - [Continental E225-2](https://openairdocs.org/engine/continental-e225-2): 0 aircraft (registry code 17161) - [Continental E225-9](https://openairdocs.org/engine/continental-e225-9): 0 aircraft (registry code 17164) ## STCs approved under this data sheet (30) - [STC SE04651CH](https://openairdocs.org/stc/SE04651CH): To allow use of l00R grade aviation fuel meeting Swift Fuel, LLC specification SPEC-l00R-22. Swift Fuels LLC - [STC SE04349CH](https://openairdocs.org/stc/SE04349CH): Installation of SureFly electronic ignition. SureFly Partners Ltd. - [STC SE03309CH](https://openairdocs.org/stc/SE03309CH): Installation of Engine Preheat Kit, p/n TSP6CYL-2927-115 for 115 volt application. Hartzell Propeller Inc. - [STC SE01167SE](https://openairdocs.org/stc/SE01167SE): Installation of Teledyne Continental O-470 cylinders. CheckSix AeroSolutions, LLC - [STC SE04577CH](https://openairdocs.org/stc/SE04577CH): Install an electronic engine ignition system. Electroair Acquisition Corp - [STC SE01966WI](https://openairdocs.org/stc/SE01966WI): Use of GAMI G100UL High Octane Unleaded Avgas in spark ignition piston aircraft engines. General Aviation Modifications Inc. - [STC SE98WE](https://openairdocs.org/stc/SE98WE): Installation of oil filter adapter and oil filter.. Airwolf Filter Corporation - [STC SE34WE](https://openairdocs.org/stc/SE34WE): Installation of Electro-Coatings, Inc., piston rings on Continental pistons.. Continental Motors, Inc. - [STC SE8776SW](https://openairdocs.org/stc/SE8776SW): Installation of coated cylinders and piston rings.. Continental Motors, Inc. - [STC SE3330NM](https://openairdocs.org/stc/SE3330NM): Continental valve cover gasket. Real Gaskets Tennessee - [STC SE295CH](https://openairdocs.org/stc/SE295CH): Installation of Slick model 6377 or6379 magnetos.. CHAMPION AEROSPACE LLC - [STC SE1780NM](https://openairdocs.org/stc/SE1780NM): Installation of Precise Flight standby vacuum system (SVS III).. Precise Flight Inc - [STC SE01943CH](https://openairdocs.org/stc/SE01943CH): Add the following approved fuels: unleaded automotive gasoline 87 minimum antiknock index, per ASTM Specification D-439 or D-4814 of any volatility class, A through E, or 82UL AVGAS per ASTM D-6227.. Experimental Aircraft Association Inc. - [STC SE693GL](https://openairdocs.org/stc/SE693GL): Superseded by STC SE01943CH. Add the following approved fuel: unleaded automotive gasoline, 87 minimum antiknock index.. EAA Aviation Foundation - [STC SE5743NM](https://openairdocs.org/stc/SE5743NM): Intallation of adapter for externally mounted oil filter.. Aviation Development Corporation - [STC SE09513SC](https://openairdocs.org/stc/SE09513SC): Installation and usage of Exxon 20W50 Multigrade aircraft engine oil conforming to Exxon Oil Formulation WS-3013.. Exxon Company USA - [STC SE00350SE](https://openairdocs.org/stc/SE00350SE): Installation of sump mounted chip detector.. Aviation Development Corporation - [STC SE3375NM](https://openairdocs.org/stc/SE3375NM): Replacement of the original oil screen with an external mounted full flow oil adapter and spin-on oil filter.. Timberman Allen E - [STC SE886NE](https://openairdocs.org/stc/SE886NE): Installation of a modified Cont. Motor continuous flow fuel injection system which replaces the Bendix pressure carburetor Model PS-5C. The existing engine driven fuel pump(Thompson Model TF-1900) is retained and readjusted to provide a maximum pressure of 26 psi.. LeJambre Charles - [STC SE452NE](https://openairdocs.org/stc/SE452NE): Installation and usage of 'Mobil AV 1' aviation oil.. Mobil Research & Development Corp - [STC SE23SW](https://openairdocs.org/stc/SE23SW): Installation of Bendix RS-5BD1 or RSA-5AD1 fuel injection system.. Bendix Corporation - [STC SE5879SW](https://openairdocs.org/stc/SE5879SW): Use of Phillips X/C II 20W-50 and25W-60 oil (OSS 55875) in all Avco reciprocating aircraft engines from 65 to 450 BHP.. Phillips Petroleum Co - [STC SE1760SW](https://openairdocs.org/stc/SE1760SW): Replacement of original cylinder barrels with P/N G-534894A.. Gary Aerospace Corp - [STC SE2034CE](https://openairdocs.org/stc/SE2034CE): Add the following approved fuel: unleaded automotive gasoline, 87 minimum antiknock index and leaded automotive gasoline, 88 minimum antiknock index(RON+MON)/2. Intermixing with aviation gasoline also approved.. Petersen Aviation Inc - [STC SE80NE](https://openairdocs.org/stc/SE80NE): Installation and usage of Bel-Ray synthetic aviation oil, Bel-Ray Aero 1, (nonsupercharged), horizontally opposed direct drive, aircraft engines of 350 hp. or less.. Bel-Ray Company, Inc - [STC SE1445SO](https://openairdocs.org/stc/SE1445SO): Use of Aero-blend oil additive in Teledyne (non turbocharged) aircraft engines.. ProTec - [STC SE417GL](https://openairdocs.org/stc/SE417GL): Installation of a spin-on oil filter adapter and spin-on filter in lieu of original screen.. S & K Engineering - [STC SE3WE](https://openairdocs.org/stc/SE3WE): T-1106 turbocharger.. AiResearch Aivation Service Co - [STC SE44WE](https://openairdocs.org/stc/SE44WE): Use of Kling Aviation Oil, Specifications KL-100, KL-200 and KL-300 in Continental and Lycoming engines.. Kling Oil Company - [STC SE419SW](https://openairdocs.org/stc/SE419SW) (historical): Full flow oil filter.. A&E Manufacturing Inc. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.