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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
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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