PT6A-42A is a turboprop engine model used in aircraft.
Engine Family: turboprop
Compressor stages: 4
Control system: Hydromechanical
Dry weight: 190 kilogram
Gas generator stages: 1
Height: 0.46 metre
Length: 1.68 metre
Max. continuous power: 634 kilowatt
Max. takeoff power: 634 kilowatt
Ng RPM: 37468
Np RPM: 33235
Output shaft RPM: 2205
Power turbine stages: 2
Width: 0.46 metre
ICAO: P46T
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