TCDS E-298

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...