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Fokker 50

The Fokker 50, certified as the F27 Mark 050 in 1987, is a high-wing, twin-engine turboprop for up to 62 passengers. Two Pratt and Whitney Canada PW125B or PW127B engines drive Dowty Rotol six-blade composite propellers 3.65 meters across. The maximum take-off weight is 20,820 kg on the highest-weight standard, and 19,950 kg on the lower one. Usable fuel is 5,136 liters and the maximum operating altitude 25,000 feet. The data sheet does not give the airplane's length or wingspan, so they are left blank.

Engines
Two Pratt and Whitney Canada PW125B or PW127B turboprops on the wings
Max takeoff weight
45,900 lb (20,820 kg)

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Specifications

Ceiling25,000 ft (7,600 m)
Fuel capacity1,360 US gal (5,136 L)
StatusStill flying with a few operators
Type codesICAO F50

Sources

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