Propellers: six-bladed Dowty Rotol composite propellers, 3.66 m (12 ft 0 in) diameter
Maximum speed: 565 km/h (351 mph, 305 kn)
Maximum speed: Mach 0.507
Cruise speed: 500 km/h (310 mph, 270 kn)
Range: 1,700 km (1,000 mi, 900 nmi)
Service ceiling: 7,620 m (25,000 ft)
Wing loading: 297.4 kg/m2 (60.9 lb/sq ft)
Takeoff: 1,350 m (4,430 ft) – ISA, SL, MTOW
Landing: 1,130 m (3,710 ft) – ISA, SL, MLW
The Fokker 50 is a turboprop-powered airliner, designed as an improved version of the successful Fokker F27 Friendship.
The Fokker 60 is a stretched freighter version of the Fokker 50.
F27 Mark 050
Marketed as the Fokker 50 (or sometimes referred to as the Fokker 50-100), based on the F27 Mark 500 with two Pratt & Whitney Canada PW125B or PW127B turboprop engines with six-bladed propellers, updated systems and cockpit instrumentation, increased use of composite structure, double the number of windows, change from pneumatic to hydraulic systems and addition of electronic engine and propeller controls and an electronic flight instrument system (EFIS) and integrated warning system.
F27 Mark 0502
Marketed as the Fokker 50, same as the 050 with reconfigured interior layout and change in type of aft emergency exits, six built (two for the Royal Netherlands Air Force, two for the Republic of Singapore Air Force and two for Royal Brunei Air Force).
MSN 20280 built 1993 was fitted with PW125B Engines and an APU.
F27 Mark 0604
Marketed as the Fokker 60, same as the 0502 with an increased fuselage length (1.02 m/3.34 ft in front of wing and 0.80 m/2.63 ft aft of wing), increased design weight and introduction of a large cargo door in the forward right side of the fuselage.
Two Pratt & Whitney PW127B turboprop engines, four built.