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Fokker 100 introducted in 1988 and produced until 1997 . They were built 283 airplanes .Fokker 100 is a twin engine , jet airliner for medium range and developed from the Fokker F28 . Airplane is out of production but still in service and made its first flight in 30 Novemberl 1986.Airplanes were manufactured from Fokker in the Netherlands

 

 

Fokker-100 

 

Specifications

 

Fokker 100
Tay 620
Fokker 100
Tay 650
Cockpit crew Two
Seating capacity 122 (1-class, maximum)
107 (1-class, typical)
97 (2-class, typical)
Seat pitch 29 in (74 cm) (1-class, maximum)
32 in (81 cm) (1-class, typical)
36 in (91 cm) & 32 in (81 cm) (2-class, typical)
Length 35.53 metres (116 ft 7 in)
Wingspan 28.08 metres (92 ft 2 in)
Wing area 93.5 square metres (1,006 sq ft)
Height 8.50 metres (27 ft 11 in)
Fuselage diameter 3.30 m (10 ft 10 in)
Cabin width 3.10 m (10 ft 2 in)
Cabin height 2.01 m (6 ft 7 in)
Typical empty weight 24,375 kilograms (53,740 lb) 24,541 kilograms (54,100 lb)
Maximum take-off weight 43,090 kilograms (95,000 lb) 45,810 kilograms (101,000 lb)
Maximum payload weight 11,242 kilograms (24,780 lb) 11,993 kilograms (26,440 lb)
Max. cruising speed 845 km/h (525 mph, 456 kn), Mach 0.77
Range fully loaded 1,323 nautical miles (2,450 km; 1,522 mi) 1,710 nautical miles (3,170 km; 1,970 mi)
Take off run at MTOW 4,988 feet (1,520 m) 5,319 feet (1,621 m)
Fuel capacity 13,365 L (2,940 imp gal; 3,531 US gal)
Service ceiling 35,000 ft (11,000 m)
Powerplants (2x) Rolls-Royce Tay Mk 620-15 Rolls-Royce Tay Mk 650-15
Engine thrust 13,850 lbf (61.6 kN) 15,100 lbf (67.2 kN)

 

 

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