TP400-D6 is a turboprop engine model used in aircraft.
Engine Family: turboprop
Dry weight: 1938 kilogram
Output shaft RPM: 842
Nh RPM: 18000
Ni RPM: 10000
Nl RPM: 8360
Max. continuous power: 7971 kilowatt
Max. takeoff power: 8251 kilowatt
Control system: FADEC
Power turbine stages: 3
Gas generator stages: 2
Length: 4.18 metre
Compressor stages: 11
ICAO: A400
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