TCDS TC 126

Type certificate data sheet · Wright Aeronautical Division Curtiss-Wright Corporation · Engine

Holder
Wright Aeronautical Division Curtiss-Wright 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.

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Models · 1

ModelAlso known asNote
Whirlwind R-760E-T

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

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MODELS: Wright Whirlwind R-760E-T 1.C. NUMBER: T.C. 126 Model - Whirlwind R-760E-1 Type - 7RA Direct drive Rating: Maximum continuous, br. Ipm, at s.L. fressure altitude 235-2000-S.L. Take-off (one minute). be, Ipm, at full thrcttle 235-2000 Fuel (minimum octane aviation gasoline) 73 Bore and stroke, in. 5.0 * 5.5 Cisplacement, cu. in. 756 Compression ratio 6-1:1 weight (dry) • 1b8- 540 ropeller shaft, SAE No. 20 or 30 (See NOTE 3) Carburetion Stromberg NA-RA carburetor with 2 in. venturi Ignition, dual Scintilla MN7-DF magnetos Ignition timing, degrees BTC Certification basis Type Certificate No. 126 Froduction basis The manufacturer does not hold a production certificate for the production of engines under this type certificate and, therefore, each engine so produced is subject to a detailed inspection for workmanshif and conformity with the approved data by a Civil Aeronautics Administration 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. OTE 1. Maximum permissible cylinder head, barrel, and oil inlet temperatures, 500 degrees Fa, 325 degrees F., and 200 degrees F., respectively. NOTE 2. pump and a starter. This model engine has provisions for mounting a hydraulically controllable two-position propeller, fuel NOIE 3. Engines with No. 20 spline propeller shaft incorporate a crankshaft torsional vibration damper.