TCDS TC 59

PHILLIPS AVIATION COMPANY MODELS: Phillips 333, 333A, 333B T.C. NUMBER: T.C. 59 Models 333, 333A, 333B Type 4LAI Rating: Maximum continuous, hp, rpm, at S.L. pressure altitude 120-2100-S.L. Take-off (one minute), hp, rpm, at full throttle 120-2100 Fuel (minimum octane aviation gasoline) 73 Bore and stroke, in. 4-1/2 x 5-1/4 Displacement, cu. in. 334 Compression ratio 5.3: 1 Weight (dry), lbs. 269 Propeller shaft, SAE No. 10 Carburetion Stromberg NA-R4D carburetor with 1-3/8 in. venturi, or Zenith No. 157 with 31 mm. venturi, or Zenith No. 156- ½ with 33 mm. Venturi Ignition, dual Scintilla PN4-DF1, SF4R-8, -9, or Bosch FU4A-1 magnetos (impulse coupling on right magneto) Certification basis Type Certificate No. 59 Production basis None. 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 workmanship and conformity with the approved data by a Civil Aeronautics Administrator 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. Maximum permissible cylinder head, barrel, and oil inlet temperatures 520 degrees F., 325 degrees F., and 200 degrees F., respectively. NOTE 2. Formerly manufactured by the Glenn L. Martin Co., Baltimore, Maryland.