TCDS E-213

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

Holder
Continental Aerospace Technologies, Inc.
Revision
12
Revised
September 19, 2022
Status
Current
Product
Engine
Models
9
Registered
33 aircraft

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

On this page

Models · 9

ModelAlso known asNote
A75-3Formerly Continental, then Teledyne Continental Motors
A75-9Formerly Continental, then Teledyne Continental Motors
A75-6JFormerly Continental, then Teledyne Continental Motors
A75-8Formerly Continental, then Teledyne Continental Motors
A75-9JFormerly Continental, then Teledyne Continental Motors
A75-6Formerly Continental, then Teledyne Continental Motors
A75-8JFormerly Continental, then Teledyne Continental Motors
A75-8FJFormerly Continental, then Teledyne Continental Motors
A75-8FFormerly Continental, then Teledyne Continental Motors

Airworthiness directives · 9

ADs whose products are models on this data sheet, matched by model and maker.

Registered aircraft

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

STCs approved under this data sheet · 24

See all 24 STCs

What the data sheet says

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

E-213 Revision 12 CONTINENTAL AEROSPACE TECHNOLOGIES, INC. A75-3 A75-6, -6J A75-8, -8F, -8J, -8FJ A75-9, -9J September 19, 2022 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. E-213 Engines of models described herein conforming with this data sheet (which is part of type certificate No. 213) 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 specifications 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 A75 A75-3, -6 A75-8, -9 Type 4HOA - - Rating, standard atmosphere Max. continuous hp., r.p.m., sea level 75-2650 75-2600 pressure altitude Takeoff hp. (5 min.) r.p.m., full throttle 75-2650 75-2600 at sea level pressure altitude Fuel, aviation gasoline (min. grade) 73, ASTM D7547 (UL91), - - ASTM D7547 (UL94) Lubricating oil: Ambient Air Temperature, °F. Oil grade - - Below 40 SAE 20 - - Above 40 SAE 40 - - Bore and stroke, in. 3.875 x 3.625 - - Displacement, cu. in. 171 - - Compression ratio 6.3:1 - - Weight (dry), lb. 170, 173 - - Propeller shaft, SAE No. (Taper) 0 - - Carburetion Stromberg NA-S3A1 with 1-1/4 in. venturi or - - Marvel MA3-PA with 1-7/32 in. venturi Ignition, dual Scintilla SF4R, SF4RN-8; Case 47, 4 CAME; - - Eisemann AM-4 or LA-4 magnetos or Continental S4RSC-21 or S4RSC-204 Spark plugs See NOTE 6 - - Ignition timing, °BTC Right 29, Left 32 - - Oil sump and capacity (qt.) Wet - 4-1/2 - - Exhaust port Up Down NOTES 1,2,3,4,5,6 1,2,3,4,6 "- -" indicates "same as preceding model." "" indicates "does not apply." Page No. 1 2 Rev. No. 12 11 E-213 Page 2 Certification basis Type Certificate No. 213 Production basis Production Certificate No. 7 NOTE 1. Maximum permissible temperatures: Spark plug gasket thermocouple 550°F. Contact type thermocouple 350°F. Oil inlet 220°F. Oil pressure limits: 30 to 40 p.s.i. NOTE 2. Those models listed in the heading of this data sheet, suffixed by the letters "F" and "J", differ from the basic model as follows: "F" denotes an SAE No. 1 flanged crankshaft instead of "0" taper, at a weight increase of 1 lb. "J" denotes the High Model A Fuel Injector in place of the carburetor at an increased weight of 3 lb. NOTE 3. Engine S/N's 606993 and up incorporate originally a modified crankcase for rubber conical shock mountings which necessitates using a modified engine mount. These engines weight 3 lb. additional. NOTE 4. The following accessory provisions and typical accessories are eligible at the increased weights shown: Starter (Models -6, -6J, -9, -9J only) Eclipse, Type 635, Electric Weight (lb.) 16 Eclipse, Type E-80, Electric 18 Hummer, Type X, Mechanical 14 Fuel Pump (provisions optional) AC Type CP 8527 4 AC Type 1523843 or 3843 (Continental No. 4552) 2 Miscellaneous Oil Filter, Fram PB-500 (Continental No. 40581) 3 Air Filter and Scoop (Continental No. A-5810 or A-40522) 3 Radio Shielding 3 NOTE 5. Approvals for Models A75-3, -6, and -6J expired November 7, 1941. No engines of these models manufactured after this date, or with S/N's above the following, are eligible for use in certificated aircraft: Model Serial No. A75-3 631893 A75-6 624196 A75-6J 625796 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 A88, HS88, S88, SR88, HSR88, S88D, SR88D Auto-Lite 18A1, B4, B4S, BH4S, SH2K, SH2M, H15, SH15, SH15R, SH20, SH20A, SH200A Red Seal SE190, SE230, SJ230 BG 4B2, 4B2S, 417, 417S, RB485-S, 706, 706R, 706S, 706SR, RB955S Champion C26, C26S, M26, C27, C27S, M31A, LM31S, REM40E, RHM40E, D41N, ED41N, M41N, EM41N, EM42E, M42E, 62S Safir B57 .....END.....