- Holder
- Church Airplane and Manufacturing Company Inc.
- Revision
- 0
- Status
- Current
- Product
- Engine
- Models
- 1
The release keeps the latest revision of each data sheet. Model names are as the data sheet lists them.
On this page
Models · 1
| Model | Also known as | Note |
|---|---|---|
| V-8 248 |
Airworthiness directives · 0
ADs whose products are models on this data sheet, matched by model and maker.
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STCs approved under this data sheet · 1
What the data sheet says
From the PDF’s text layer, line by line: tables lose their columns. The PDF is the record.
CHURCH AIRPLANE AND MANUFACTURING COMPANY, INC
MODELS: Church V-8 248
T.C. NUMBER: T.C. 224
Model V-8 248
Type 8VA
Rating:
Maximum continuous,
hp, rpm, at S.L.
press. alt. 93-2900-S.L.
Take-off, hp, rpm,
at full throttle 93-2900
Fuel (minimum octane
aviation gasoline) 73
Bore and stroke, in. 3.25 x 3.75
Displacement, cu. in. 248
Compression ratio 5.7: 1
Weight (dry), lbs. 342 (See NOTE 1)
Propeller shaft Special
Carburetion Ford Stromberg dual down draft with 1-1/32 in. venturis
Ignition Ford battery ignition system
Certification basis Type Certificate No. 224
Production basis None. The manufacturer does not hold a production
certificate of engines under this type certificate and,
therefore, each engine so produced is subject to a detailed
inspection for workmanship and conformity with the
approved data by a CAA Agent. In addition, the engine
must have a satisfactory run-in including 5 hours at rated
power and speed. Upon satisfactory completion of the
above, the agent will tag the engine with Tag Form ACA
186.
NOTE 1. Weight (dry) also includes exhaust manifold, generator and fuel pump.