Fokker 100 - Specifications

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)

Notes: Data are provided for reference only. Tay 620=Rolls-Royce Tay Mk 62015 and Tay 650=Rolls-Royce Tay Mk 65015
Sources: airliners.net, aer.ita.br