Fokker · Netherlands · ICAO: F50 · 1987–1997 ·
$17.5 million

The Once Refined Turboprop Airliner The Fokker 50

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Engine:
2× Pratt & Whitney PW125B turboprops
Engine type:
Turboprop
Power:
2 × 2,500 shp  ·  1,864 kW
Avionics:
EFIS and Automatic Flight Control System
Wing Tips:
No winglets
Seats:
62
Cabin width:
ft 2 in · 2.50 m
Cabin height:
ft 5 in · 1.96 m
Cabin length:
51 ft 3 in · 15.63 m
Exterior length:
82 ft 10 in · 25.25 m
Tail height:
27 ft 4 in · 8.32 m
Fuselage diameter:
ft 10 in · 2.70 m
Wing span / rotor:
95 ft 2 in · 29.00 m
Baggage volume:
590 ft³  ·  16.7 
Max takeoff weight:
45,900 lb  ·  20,800 kg
Max landing weight:
44,200 lb  ·  20,000 kg
Max Payload:
12,100 lb  ·  5,500 kg
Fuel capacity:
1,360 gal  ·  5,100 L  ·  4,100 kg  (Jet A)
Max cruise speed:
286 kt  ·  329 mph  ·  530 km/h
Approach speed (Vref):
97 kt  ·  112 mph  ·  180 km/h
Range:
1,110 nm  ·  1,280 mi  ·  2,060 km
Fuel burn:
0.90 nm/gal  ·  0.44 km/L
Ceiling:
25,000 ft  ·  7,600 m
Rate of climb:
1,500 ft/min  ·  m/s
Takeoff distance:
4,450 ft  ·  1,350 m
Landing distance:
3,700 ft  ·  1,130 m
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