- 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
| Model | Also known as | Note |
|---|---|---|
| Scarab Jr. Series 40 | Formerly Warner, then Olson, then George, then Company | |
| Scarab Jr. Series 50 | Formerly 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....