Fokker 100

KLM Cityhopper Fokker 100

Austrian arrows Fokker 70 and Fokker 100

The Fokker 100 is a medium sized regional turbofan jet designed and built by Dutch aircraft manufacturer Fokker. First flight occurred on 30 November, 1986. 283 airframes were build. Production ran from 1986-1997. In 1993, Fokker 100 converted into smaller Fokker 70. A stretched and improved version of Fokker F28. Still in service.

Current Operators

As of July 2017, 113 Fokker 100 airliners are still used by the following airlines.

• Air Niugini
• Air Panama
• Alliance Airlines
• Avanti Air
• Bek Air
• Carpatair
• Helvetic Airways
• Iran Air
• Iran Aseman Airlines
• IRS Airlines
• Karun Airlines
• Kish Air
• Montenegro Airlines
• QantasLink
• Qeshm Airlines
• Skippers Aviation
• Trade Air
• Transwisata Air
• Tus Airways
• Virgin Australia Regional Airlines

Specifications

Tay 620

• Cockpit crew: 2
• 1-class max. seating: 122, 29 in (74 cm) pitch
• 1-class typical seating: 107, 32 in (81 cm) pitch
• 2-class typical seating: 97, 39 in (91 cm) & 32 in (81 cm) pitch
• Length: 116 ft 7 in (35.53 m)
• Wingspan: 92 ft 2 in (28.08 m)
• Wing area: 1,006 sq ft (28.08 m)
• Height: 27 ft 11 in (8.5 m)
• Fuselage diameter: 10 ft 10 in (3.3 m)
• Cabin width: 10 ft 2 in (3.1 m)
• Cabin height: 6 ft 7 in (2.01 m)
• Empty weight: 53,738 lb (24,375 kg)
• MTOW: 95,000 lb (43,090 kg)
• Max. payload weight: 24,784 lb (11,242 kg)
• Max. cruising speed: Mach 0.77 (525 mph, 456 kn, 845 km/h)
• Range fully loaded: 1,323 nautical miles (1,522 mi, 2,450 km)
• Take off run at MTOW: 4,988 ft (1,520 m)
• Fuel capacity: 3,531 US gal (13,365 L, 2,940 imp gal)
• Service ceiling: 35,000 ft (11,000 m)
• Powerplants (2x): Rolls-Royce Tay Mk 620-15
• Engine thrust: 13,850 lbf (61.6 kN)

Tay 650

• Cockpit crew: 2
• 1-class max. seating: 122, 29 in (74 cm) pitch
• 1-class typical seating: 107, 32 in (81 cm) pitch
• 2-class typical seating: 97, 39 in (91 cm) & 32 in (81 cm) pitch
• Length: 116 ft 7 in (35.53 m)
• Wingspan: 92 ft 2 in (28.08 m)
• Wing area: 1,006 sq ft (28.08 m)
• Height: 27 ft 11 in (8.5 m)
• Fuselage diameter: 10 ft 10 in (3.3 m)
• Cabin width: 10 ft 2 in (3.1 m)
• Cabin height: 6 ft 7 in (2.01 m)
• Empty weight: 54,104 lb (24,541 kg)
• MTOW: 100,990 lb (45,810 kg)
• Max. payload weight: 26,440 lb (11,993 kg)
• Max. cruising speed: Mach 0.77 (525 mph, 456 kn, 845 km/h)
• Range fully loaded: 1,710 nautical miles (1,970 mi, 3,170 km)
• Take off run at MTOW: 5,319 ft (1,621 m)
• Fuel capacity: 3,531 US gal (13,365 L, 2,940 imp gal)
• Service ceiling: 35,000 ft (11,000 m)
• Powerplants (2x): Rolls-Royce Tay Mk 650-15
• Engine thrust: 15,100 lbf (67.2 kN)