# TCDS E-298: Continental Aerospace Technologies, Inc. - Type: Type certificate data sheet - Status: Current - Holder: Continental Aerospace Technologies, Inc. - Revision: 15 - Revised: September 19, 2022 - Product: Engine - Certification basis: Part 1, CAR 13 - Registered aircraft: 814, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/60/e3/60e373ae711148c8f74a2b926d9e1fdee50ccbc55c18b0b84bdd19dece1b8b4f - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F89C95C9311DA9D5862588C6006A0A98.0001 - Page: https://openairdocs.org/tcds/E-298 ## Models (6) As the data sheet lists them. - GO-300-A - GO-300-F - GO-300-D - GO-300-E - GO-300-C - GO-300-B ## 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-298 Revision 15 CONTINENTAL AEROSPACE TECHNOLOGIES, INC. GO-300-A, -B -C, -D -E, -F September 19, 2022 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. E-298 Engines of models described herein conforming with this data sheet (which is part of type certificate No. 298) and other approved data on file with the Federal Aviation Agency, 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 GO-300-A, -B, -C, -F GO-300-D, -E Type 6HOA, reduction gear ratio 0.750:1 - - Rating ICAS or ARDC standard atmosphere Max. continuous hp., r.p.m., full throttle at sea level pressure altitude 175-3200 - - Takeoff hp., 5 min., r.p.m., full throttle at sea level pressure altitude 175-3200 - - Fuel (aviation gasoline, minimum grade) 80/87, ASTM D7547 (UL91), - - ASTM D7547 (UL94) Lubricating oil Below 40F Aviation Grade 1040 (SAE20) - - Above 40F Aviation Grade 1080 (SAE 40) - - Bore and stroke, in. 4.0625 x 3.875 - - Displacement, cu. in. 301.37 - - Compression ratio 7.3:1 - - Weight (dry), lb. (see NOTE 4) 312 318 (includes starter adapter) C.G. location (with starter and generator installed) Fwd. of rear face of mounting lug, in. 9.71 9.13 Below crankshaft center line, in. 0.62 0.90 Beside crankshaft center line (toward 1-3-5 side), in. 0.08 0.36 Propeller shaft Special integral flange - - 4-7/8 in. O.D. with six 1/2 in. bolt holes in 4 in. diameter circle Carburation Marvel-Schebler MA-4-5, - - Continental P/N 626789 Ignition, dual magnetos Two J.I. Case 667 or Continental S6RN-21 or Continental S6RSC-21 or 1 ea. Continental S6RN-200 and -204 Timing BTC Right 28, Left 28 - - Spark plugs See NOTE 7 - - Oil sump capacity, qt. 10, 7 usable at 20 nose-up and 15 nose-down attitudes - - NOTES 1 thru 7 1, 2, 3, 4, 5, 7 “- -” indicates “same as preceding model” Page No. 1 2 Rev. No. 15 14 E-298 2 Certification basis CAR 13, effective June 15, 1956 as amended by 13-1 Type Certificate No. 298 issued December 6, 1957; GO-300-B added May 9, 1958, GO-300-C added April 23, 1959, GO-300-D added June 1, 1960, GO-300-E added June 9, 1961, GO-300-F added December 5, 1963. Date of Application for Type Certificate August 22, 1957 Production basis Production Certificate Nos. 7 and 508. NOTE 1. Maximum permissible temperatures Cylinder Head Cylinder Barrel Oil Inlet 525F 290F 225F (Spark plug gasket-downdraft cooling) NOTE 2. Pressure limits for normal operation Fuel inlet: min. 12 in. Fuel head, max. 6 p.s.i. 30 to 60 p.s.i. min. idling 5 p.s.i. (with hot oil) NOTE 3. The following accessory drive provisions are available Engine Direction Speed Ratio Max. Torque (in.-lb.) Max. Overhang Moment Accessory Models of Rotation* to Crankshaft Cont. Static (in. -lb.) Tachometer All CC 0.5:1 15 100 100 **Propeller Governor -B, -E CC 0.8963:1 29 825 50 Generator All C 2.035:1 60 600 100 ***Starter -A,-B, -C, -F C 35.777:1 ****Starter -D, -E CC 24.727:1 Vacuum pump -A, -B, -C, -F C 0.8947:1 40 825 25 Vacuum pump -D, -E C 1.545:1 100 800 25 Optional -D, -E C 0.895:1 40 825 25 *C - Clockwide viewing drive pad; CC - Counterclockwise ** Modified AND 20010 pad *** Delco-Remy gear reduction drive and starter (CMC P/N 626292) eligible **** Delco-Remy starter (Continental P/N 627842 with Continental adapter P/N 628157) eligible NOTE 4. Six 3rd order dampers are provided on crankshaft. Engine S/N 6134, 6136, 6142, 6143, 6146 and up incorporate heavy type counterweights with an increase of 2 lb. in engine dry weight. NOTE 5. GO-300-B is identical to GO-300-A except incorporates provisions for hydraulic propeller control. GO-300-C is identical to GO-300-A except height of oil filler neck and breather tube assembly has been reduced. GO-300-D is identical to GO-300-C except for provisions for Continental right angle automatic engagement starter drive which incorporates a vacuum pump drive. GO-300-E is identical to GO-300-D except incorporates provisions for hydraulic propeller control. GO-300-F is identical to GO-300-A except incorporates provisions for pusher operation and propeller reversing. NOTE 6. GO-300-A engines, S/N 5276-B-A, 5277-8-A, 5776-8-A, 6314-0-A, 6316-3-A, 6317-3-A, 6318-3-A are identical to the Model GO-300-F. Existing nameplates may be replaced with nameplates bearing this designation. NOTE 7. The following spark plugs and/or those listed in the Section 6-4.9 of the latest revision of M-0, Standard Practice Maintenance Manual, are approved on this engine: AC HSR83P, SR83P, HSR87, SR87 BG RB485S, RB919SR5, RB955S Champion RC26S, REM38E, REM38P, RHM38E, RHM38P, RED39N, REM39N, RHD39M, RHM39N, REM40E, RHM40E Red Seal 632507, 632508, 632511, 632512, 632513, 632514 Auto Lite 627892, 632461, 632462, 632463, 635146, 635147 NOTE 8. Engine model numbers may include a suffix to define minor specification changes and/or accessory packages. Example: GO-300-A(10). ...END... ``` ## ADs (5, in force first) - [AD 2023-17-04](https://openairdocs.org/ad/2023-17-04): Reciprocating Engine Oil System · F & M Enterprises' Model C6LC, C6LC-S or C6LC-L oil filter… (Stratus Tool Technologies STC SE09356SC or 2 others). Effective Oct 26, 2023 - [AD 94-05-05 R1](https://openairdocs.org/ad/94-05-05-R1): Cylinder Rocker · Continental Motors C-125-1, C-125-2, C145-2 and 59 more. Effective Feb 13, 1996 - [AD 95-21-15](https://openairdocs.org/ad/95-21-15): Aviation Gasoline · Continental Motors A-65-8, C85-12F, C85-12FJ and 77 more. Effective Nov 28, 1995 - [AD 63-22-03](https://openairdocs.org/ad/63-22-03): Carburetors · Continental Motors GO-300-A, GO-300-B, GO-300-C and 143 more. Effective Dec 2, 1963 - [AD 94-14-12](https://openairdocs.org/ad/94-14-12) (historical): Octane Aviation Gasoline · Teledyne Continental Motors A-65-8, C85-12, E185-11 and 68 more ## Registered aircraft by registry model (OpenAirDocs) - [Continental GO-300 series](https://openairdocs.org/engine/continental-go-300-series): 808 aircraft (registry code 17024) - [Continental GO-300-D](https://openairdocs.org/engine/continental-go-300-d): 3 aircraft (registry code 17202) - [Continental GO-300-A](https://openairdocs.org/engine/continental-go-300-a): 1 aircraft (registry code 17198) - [Continental GO-300-C](https://openairdocs.org/engine/continental-go-300-c): 1 aircraft (registry code 17200) - [Continental GO-300-E](https://openairdocs.org/engine/continental-go-300-e): 1 aircraft (registry code 17203) - [Continental GO-300-B](https://openairdocs.org/engine/continental-go-300-b): 0 aircraft (registry code 17199) - [Continental GO-300-F](https://openairdocs.org/engine/continental-go-300-f): 0 aircraft (registry code 17201) ## STCs approved under this data sheet (32) - [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 SE2932SW](https://openairdocs.org/stc/SE2932SW): Install carburetor air temperature indicator. Approved for Aircooled Motors (Franklin Engine Co.) equipped with float carburetors. Model eligibility included here may not be inclusive.. Alcor LLC - [STC SE208SO](https://openairdocs.org/stc/SE208SO): Installation of ice indicator in the carburetor.. LegacySTC.com - [STC SE04349CH](https://openairdocs.org/stc/SE04349CH): Installation of SureFly electronic ignition. SureFly Partners Ltd. - [STC SE00145WI](https://openairdocs.org/stc/SE00145WI): Installation of B&C Specialty Products Model BC 320-( ) Engine Starter.. B & C Specialty Products Inc. - [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 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 SE00533SE](https://openairdocs.org/stc/SE00533SE): Installation of Real Gasket Corporation Continental Engine Pushrod Tube Modification.. Real Gaskets Tennessee - [STC SE8409SW](https://openairdocs.org/stc/SE8409SW): Installation of P/N CO-300-1 Oil Filter Adaptor with spin-on filter as a replacement for the existing oil screen. Stratus Tool Technologies LLC - [STC SE10076SC](https://openairdocs.org/stc/SE10076SC): Modify engine by installation of C12ST2/S starter.. Hartzell Engine Technologies, LLC - [STC SE10129SC](https://openairdocs.org/stc/SE10129SC): Installation of rotocoil, valve springs, ni-resist valve guide, exhaust valve with chrome flash on stem, and rocker shaft with thrust buttons.. Continental Motors, Inc. - [STC SE34WE](https://openairdocs.org/stc/SE34WE): Installation of Electro-Coatings, Inc., piston rings on Continental pistons.. Continental Motors, Inc. - [STC SE8110SW](https://openairdocs.org/stc/SE8110SW): Installation of any of all parts identified by Drawing/Parts Application List AEC9109-2.. Continental Motors, Inc. - [STC SE3330NM](https://openairdocs.org/stc/SE3330NM): Continental valve cover gasket. Real Gaskets Tennessee - [STC SE1306GL](https://openairdocs.org/stc/SE1306GL): Replacement of Slick Model 667 magnetos with Slick Model 6267 magnetos or installation of Model 6367 magneto.. 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 SE1-201](https://openairdocs.org/stc/SE1-201): Installation of the Richter Aero Equipment Type B-4 or B-5 Temperature Probe. (O-360 SERIES (excl. A1C, C2B, C2D)). MidContinent Instru Co Inc - [STC SE00577NY](https://openairdocs.org/stc/SE00577NY): Installation of Canadian Aero Mfg. (C.A.M.) Oil Coolers.. Canadian Aero Manufacturing - [STC SE00350SE](https://openairdocs.org/stc/SE00350SE): Installation of sump mounted chip detector.. Aviation Development Corporation - [STC SE00427NY](https://openairdocs.org/stc/SE00427NY): Installation, operation and inspection of CAM oil coolers.. Canadian Aero Manufacturing - [STC SE8669SW](https://openairdocs.org/stc/SE8669SW): Installation of roller rocker arm.. Performance Engineering - [STC SE4316NM](https://openairdocs.org/stc/SE4316NM): Replacement of original engine oil screen with an external mounted full flow oil adapter and spin-on filter.. Aviation Products Development Co. - [STC SE452NE](https://openairdocs.org/stc/SE452NE): Installation and usage of 'Mobil AV 1' aviation oil.. Mobil Research & Development Corp - [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 SE2105CE](https://openairdocs.org/stc/SE2105CE): Add approved fuel: unleaded automotive gasoline, 87 minimum antiknock index and leaded automotive gasoline, 88 minimum antiknock index(RON+MON)/2.. Petersen Aviation Inc - [STC SE1445SO](https://openairdocs.org/stc/SE1445SO): Use of Aero-blend oil additive in Teledyne (non turbocharged) aircraft engines.. ProTec - [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 --- 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.