# TCDS E-214: Warner Engine Company LLC - Type: Type certificate data sheet - Status: Current - Holder: Warner Engine Company LLC - Revision: 3 - Revised: September 27, 2000 - Product: Engine - Data sheet PDF: https://openairdocs.org/files/sha256/82/c2/82c20034a1512f276b9dd35a320344973f1ca2768637cfe48b54b893c5ee2dc1 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/71AE434259B9E9E986257642006084A6.0001 - Page: https://openairdocs.org/tcds/E-214 ## Models (4) As the data sheet lists them. - Super Scarab Series 165-A - Super Scarab Series 165-B - Super Scarab Series 165 - Super Scarab Series 165-D ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page No. 1 2 Rev. No. 3 3 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION E-214 Revision 3 WARNER ENGINE COMPANY WARNER SUPER SCARAB SERIES 165 (R-500-1, -7), 165-A, 165-B, 165-D September 27, 2000 TYPE CERTIFICATE DATA SHEET NO. E-214 Engine of models described herein conforming with this data sheet (which is a part of type certificate No. E-214) and other approved data on file with the Federal Aviation Administration, meet the minimum standards for use in certificated aircraft in accordance with pertinent aircraft data sheets and applicable portions of the Federal Aviation Regulations provided they are installed, operated and maintained as prescribed by the approved manufacturer's manuals and other approved instructions. Type Certificate Holder Warner Engine Company, LLC. P.O. Box 9 Palmer Lake, Colorado 80133 Type Certificate Holder Record: George Olson Company transferred TC E-214 to Warner Engine Company ,LLC on September 27, 2000. Models - Super Scarab 165, 165-A 165-B, 165-D Type 7 RA -- Rating,: Maximum continuous, hp., r.p.m at S.L. pressure altitude Take-off (5 minutes), hp, r.p.m., full throttle 165-2100 175-2250 -- Fuel (minimum octane aviation gasoline) 73 -- Bore and stroke, in. 4.625 x 4.250 -- Displacement, cu. in. 500 -- Compression ratio 6.4:1 -- Weight (dry), lbs. 341 348 C.G. location (dry) Forward of mounting lug face , in. 4.75 -- Propeller shaft, SAE No. 20 -- Carburetor Stromberg NA-R5A with 1-15/16 in. venturi or Holley 419 carburetor with 1-11/16 or 1-49/64 in. venturi -- Ignition, dual Scintilla MN7DF or VMN7DF magnetos -- Timing, degrees BTC 28.5 -- Spark plugs EG-5B2, 317-S; Champion C-26, S, C-27, S, M-4, S; Simmonds-Benton 3B5, S; K.L.G. V. 17/15-RL, R-V. 17/5; Firestone MA-3, -S: Auto-Lite 18-A-1, SH- 2K1, SH-2K -- Certification Basis Type Certificate No. 214 E-214 2 NOTES: NOTE 1. Maximum permissible cylinder head, barrel and oil inlet temperatures 525 degrees F., 300 degrees F., and 200 degrees F., respectively. NOTE 2. The following accessory provisions and typical engine accessories are eligible at the indicated weight increases: Starter Eclipse type 393, model 4 (hand inertia type complete with crank). Uses adapter 8144, bracket 8188 which covers generator drive jaw 8145. Eclipse type 397, model 20, style B (old designation E-80) Eclipse type 396, model 2, style A (old designation Y-150) Weight (lbs) 17 4 18 18 Generator Eclipse type 309, model 1, style A (15 volt, amp.) 22 Fuel Pump Titan model 200, type L2X3-10 or -12 or M2X3-13 (anti-clock rotation, square drive) 2 Vacuum Pump Pesco type B-6, P/N 3P-194D (cannot be used in models 165 and 165-B prior to serial number SS2034) Uses drive assembly number 8190-1 4 1 Miscellaneous Magneto impulse coupling - Apollo No. 8248 (denoted by engine serial number suffix "E") Short Nose crankcase and crankshaft, P/Ns 7484 and 7786, respectively for Models 165 and 165-A only are denoted by serial suffix letter "G". Net decrease Shielded ignition system Control valve for two-position hydraulic propeller (Model 165-B only) Propeller governor drive (Model 165-D only) 1 3 10 1 1 NOTE 3: Engine serial number suffix letters as indicated below should be added to the engine nameplate to denote when the following modificati ons have been incorporated. Suffix "A" to denote 3/8 in. cylinder base studs and 0 type cylinder base oil seals. Suffix "F" to denote special drive at starter pads - offset magneto drives, and opposite rotation magnetos. Suffix "L" to denote special crankshaft 1 in. longe r than standard between thrust nut and spline to accommodate 6-1/4 inch length propeller hubs. Suffix "p" to denote cylinder bores chrome plated by Spartan Eng. Company. NOTE 4: Military model R-500-1 is identical to model 165. Military model R-500-7 is similar to model P-500-1 except that it incorporates heavier pistons, 1-49/64 in. car buretor venturi (Holley ), and shielded ignitor with weight (dry) of 351 lbs. Prior to use of any engine of the above models in certificated aircraft, the generator drive gear , P/N 7859, should be removed and magnetically inspected for cranks. The Champion E-2411 generator used on these engines in military aircraft should not be reinstalle d in these engines or in any other Warner 165 series engine. Drive gear failures have been experienced when using this generator which does not incorporate a flexible torsion drive. The designation plate of a military engine used in certificated aircraft should be stamped with the corresponding certificated engine model designation and the Type Certificate No. If there is no room for this information on the existing plate, such information ma y be stamped on a plain thin metal plate and attached beneath the existing plate by at least two of the mounting screws. NOTE 5: Approval expired 9/7/50. No engines of these m odels manufactured after this date eligible for use in certificated aircraft. ..END.... ``` ## ADs (1, in force first) - [AD 51-04-02](https://openairdocs.org/ad/51-04-02): Cylinder Holddown Studs ยท Warner Engine Scarab Jr. Series 40, Scarab Jr. Series 50, Scarab Series 28 and 13 more ## STCs approved under this data sheet (4) - [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 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 SE2592 CE](https://openairdocs.org/stc/SE2592%20CE): Add unleaded automotive gasoline, 87 minimum antiknock index and leaded automotive gasoline, 88 minimum antiknock index(RON + MON)/2, per ASTM Specification D-439. (SUPER SCARAB SERIES 165 R-500-1, -7). Petersen Aviation Inc - [STC SE2592CE](https://openairdocs.org/stc/SE2592CE): Add unleaded automotive gasoline, 87 minimum antiknock index and leaded automotive gasoline, 88 minimum antiknock index(RON + MON)/2, per ASTM Specification D-439. (SUPER SCARAB SERIES 165 R-500-1, -7). Petersen Aviation 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.