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The Aircraft

Pilatus PC-12

Pilatus PC-12 on runway

Aircraft Data:

Engine

The airplane incorporates a twin shaft turboprop engine with 4 axial and 1 centrifugal stages, an annular combustion chamber and a 3 stage turbine where one stage drives the compressor and two stages power the propeller. More about the engine at this site.

Engine Manufacturer : Pratt & Whitney

Engine Model Number: PT6A-67B

PT6A-67B Engine PT6A-67B

Horsepower Rating & Engine Speed:

Takeoff Power 1,200 shp

Maximum Climb/Cruise Power 1,000 shp

Propeller

The propeller assembly consists of a hub unit and four metal blades, and is a hydraulically actuated, constant speed, full feathering and reversible type.

Propeller Manufacturer : Hartzell

If you like to know about Hartzell, kindly visit their siteĀ  http://www.hartzellprop.com They go a long history, even before the Wright Brothers flying history.

Number of blades : 4

4blade_lightweight_turbine

Fuel

Approved Fuels : Jet A, Jet-A-1, Jet B, JP-4

Total Capacity: 406.8 USgal, 2,736.5lb (1,540 liters)

Usable Fuel: 402 US gal, 2,703.6lb (1,521.5 liters)

Oil

Total Capacity : 3.6 US gal (13.6 liters)

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