- Holder
- Monocoupe Corporation
- 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 |
|---|---|---|
| Lambert R-266 |
Airworthiness directives · 0
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STCs approved under this data sheet · 1
What the data sheet saysOCR
This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.
MONOCOUPE AEROPLANE CORPORATION OF AMERICA
MODELS: Monocoupe, Lambert R-266
I.C. NUMBER: 1.C. 38
Model Lambert R-266
Tyre 5RA
Rating:
Maximum continuous,
Dç. Ipm, at S.I.
pressure altitude 90-2375-S.L.
Take-off lone minute).
Dç. rpm, at full
throttle 90-2375
Fuel (minimum octane
aviation gasoline) 59
Fore and stroke, in. 4.25 × 3.75
cisplacement, cu. in. 266
Compression ratio 5.5:1
height (dry). lbs. 214
Crankshaft gearing Direct drive
Fropeller shaft,
SAE No. Special taper
supercharging None
carburetion stromberg NA-R3 carburetor with 1-5/16 in. venturi
Ignition, dual Scintilla PN5D or SB5L magnetos
Certification basis Type Certificate No. 38
NOIE and 200 degrees F.. respectively. Maximum permissicle cylinder head, barrel and oil inlet temperature, 550 degrees F., 300 degrees '•.
Approval expired 8/14/41. No engine of this model manufactured after this date or with serial numter: 3323 eligible for use in certificated aircraft