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Fokker Netherlands
/ Fokker 70
Fokker 70
The Fokker 70 is a narrow-body, twin-engine, medium-range, turbofan regional airliner produced as a smaller version of the Fokker 100.
The 70 is powered by two Rolls-Royce Tay 620 turbofans placed at the back of the fuselage, with 61.6 kN (13,849 lb) of thrust.
The weight varies from 22,673 kilograms (49,985 lb) when empty to 41,730 kilograms (92,000 lb) at maximum take-off weight (MTOW).
An airbrake on the 70’s tail section, similar to that found on the BAe 146, allows it to conform with the 5.5° glide slope at London City Airport.
Specifications
Crew
Two
Capacity
85 (1-class, maximum at 76 cm (30 in) seat pitch)
79 (1-class, typical at 81 cm (32 in) seat pitch)
72 (2-class, typical at 91 cm (36 in) and 81 cm (32 in) seat pitches)
Length
30.91 m (101 ft 5 in)
Wingspan
28.08 m (92 ft 2 in)
Width
3.30 m (10 ft 10 in)
Height
8.5 m (28 ft 10 in)
Wing area
93.5 m2 (1,006 sq ft)
Empty weight
22.673 kg (49.985 lb)
Max take-off weight
39.915 kg (87.998 lb) High weight option
Powerplant
2 × Rolls-Royce Tay 620 , 61.6 kN (13.850 lbf) thrust each
Performance
Cruise speed
845 km/h (525 mph, 456 kn)
Range
3,410 km (2,119 mi, 1,841 nmi)
Service ceiling
11,000 m (36,089 ft).
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