TCDS TC 212

Type certificate data sheet · Lenape Aircraft and Motors Inc. · Engine

Holder
Lenape Aircraft and Motors 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.

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Models · 1

ModelAlso known asNote
Brave LM-5

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 · 2

What the data sheet saysOCR

This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.

MOLELS: Lenape Brave IM-5 1.C. NUMBER: T.C. 212 Model Brave LM-5 туре SRA Rating: Maximum continuous, bf. Ipm, at S.L. fressure altitude 95-2200-S.L. Take-off (one minute), np. Irm, at tuil throttle 95-2200 Fuel (minimum octane aviation gasoline) 73 Fore and stroke, in. 4.125 × 4.000 Cisflacement, cu. in. 267 compression ratio 5.1:1 weight (dry), lbs. 194 Crankshaft gearing None Fropeller shaft, Supercharging (imfeller gear ratio) Carburetion Stromberg NA-R3 carburetor with 1-5/16 in. venturi NA-S3 or N-SJA with 1-1/4 in. venturi Edison Splitdorf RM-5 magnetos Certification basis Type Certificate No. 212 NOTE 1. lenape engine mount assembly, Part No. 800-6, is eligible. NOTE 2. Maximum permissible cylinder head, barrel and oil inlet temperatures, 500 degrees F.. 300 degrees F.. and 200 degrees F.. respectively. NOTE 3. Approval expired 6/30/41. No engines of this model manufactured after this date eligitle for use ir certificated aircraft.