TCDS E-54

Type certificate data sheet · Warner Engine Company LLC · Engine

Holder
Warner Engine Company LLC
Revision
3
Revised
September 27, 2000
Status
Current
Product
Engine
Models
2

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

On this page

Models · 2

ModelAlso known asNote
Scarab Jr. Series 40Formerly Warner, then Olson, then George, then Company
Scarab Jr. Series 50Formerly Warner, then Olson, George, Company

Airworthiness directives · 1

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

STCs approved under this data sheet · 2

What the data sheet says

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

Page No. 1 2 Rev. No. 3 3 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION E-54 Revision 3 WARNER ENGINE COMPANY WARNER SCARAB Jr. SERIES 40 and 50 September 27, 2000 TYPE CERTIFICATE DATA SHEET NO. E-54 Engine of models described herein conforming with this data sheet (which is a part of type certificate No. E-54) 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-54 to Warner Engine Company ,LLC on September 27, 2000. Models - Super Scarab 40 & 50 Type 5 RA Rating, standard atmosphere Max. continuous hp., r.p.m., 90-2050 at sea level pressure altitude Takeoff hp., 5 min., r.p.m., full 90-2050 throttle, at sea level pressure altitude Fuel (min. grade aviation gasoline) 54 Bore and stroke, in. 4.25 x 4.25 Displacement, cu. in. 301 Compression ratio 5.2:1 Weight (dry), lbs. 237 Less gene rator, starter and exhaust stacks Propeller shaft, SAE No. 1 Taper Carburetor Holley 429 with 1-7/16 in. venturi Ignition, dual Scintilla PN5-D,SB5R, or Boach JF-5ARS-20 magnetos Spark plugs Champion No. 13, C-26, -S, C-27, C27S, M-4, -S; BG-5B2, 317-S, AC-N; Simmonds-Benton 3B5 Certification Basis Type Certificate No. 54 NOTES: NOTE 1. Maximum permissible cylinder head, barrel and oil inlet temperatures 525 degrees F., 300 degrees F., and 200 degrees F., respectively. E-104 2 NOTE 2: Serial number suffix “E” should be added to the e ngine nameplate when austenitic type exhaust valves are installed. Serial number Suffix "A" should be added to the engine nameplate when 3/8 in. cylinder base studs and 0 type cylinder base oil seals have been incorporated. NOTE 3: The approval for Series 40 expired 7/10/41 and fo r Series 50 9/7/50. No engines of these models manufactured after this date are eligible for use in certificated aircraft. ..END....