Fokker 50

Fokker

ICAOF50IATA50
Fokker 50 aircraft
FokkerFokker 50
Photo: kitmasterbloke · CC BY 2.0 · Modified

Details

The Fokker 50 is a twin-engine turboprop regional airliner developed by Fokker as an updated and improved version of the successful Fokker F27 Friendship. Introduced in 1987, the Fokker 50 features upgraded Pratt & Whitney Canada PW125B engines with six-bladed propellers, modernized avionics, improved cabin comfort, and enhanced performance. Seating 50-58 passengers, the aircraft was designed for short-haul regional routes with excellent fuel efficiency and reliability. The Fokker 50 inherited the F27's reputation for robustness and STOL capabilities while offering better cruise performance and lower operating costs. Production ended in 1997 when Fokker went bankrupt, with 213 aircraft delivered worldwide.

1

Variants

213

Built

Weightscompared to Airbus A318

MRW (Maximum Ramp Weight)

20,865kg
0
25k
50k
68k

MTOW (Maximum Takeoff Weight)

20,820kg
0
25k
50k
68k

MLW (Maximum Landing Weight)

19,730kg
0
25k
50k
56k

MZFW (Maximum Zero Fuel Weight)

18,600kg
0
25k
53k

Empty Weight

12,520kg
0
25k
40k

Capacitycompared to Airbus A318

Passenger Capacity

62passengers
0
100
132

47% of A318 maximum capacity

Crew

Total
4
Cockpit
2
Cabin
2

Dimensions

Length

25.2m

Wingspan

29.0m

Height

8.4m

Wing Area

70.0m²

Catalog Price

Base List Price

$15M USD

1995 catalog price

Note: Actual prices vary based on configuration, options, and negotiations. This represents the manufacturer's base catalog price.

Engine Specifications

Engine Count

2×

Engine Model

Pratt & Whitney Canada PW125B

Fuel & Cargo

Fuel Capacity

5,366 L

Cargo Volume

11.5 m³

Production & History

Total Produced

213

Production Status

Out of production

Manufacturing Period

1985–1997

First Flight

December 28, 1985

Entered Service

August 7, 1987

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