- Role: Narrow-body Regional jet airliner
- National origin: Netherlands
- Manufacturer: Fokker
- First flight: 30 November 1986
- Introduction: April 5, 1988 with Swissair
- Status: Out of production, in service
- Produced: 1986-1997
- Number built: 283
- Developed from: Fokker F28 Fellowship
- Variants: Fokker 70
Specifications
General characteristics
- Cockpit crew: Two
- Seating capacity: 122 (1-class, maximum)
- Overall 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)
- Overall height: 8.50 metres (27 ft 11 in)
- Fuselage width: 3.30 m (10 ft 10 in)
Fokker 100 with Rolls-Royce Tay Mk 620-15
- Operating empty weight: 24,375 kilograms (53,738 lb)
- Maximum payload weight: 11,242 kilograms (24,784 lb)
- Maximum take-off weight: 43,090 kilograms (95,000 lb)
- Engine (× 2): Rolls-Royce Tay Mk 620-15, thrust 13,850 lbf (61.6 kN)
Performance
- Service ceiling: 35,000 ft (11,000 m)
- 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)
Fokker 100 with Rolls-Royce Tay Mk 650-15
- Operating empty weight: 24,541 kilograms (54,104 lb)
- Maximum payload weight: 11,993 kilograms (26,440 lb)
- Maximum take-off weight: 45,810 kilograms (100,990 lb)
- Engine (× 2): Rolls-Royce Tay Mk 650-15 thrust 15,100 lbf (67.2 kN)
Performance
- Service ceiling: 35,000 ft (11,000 m)
- Cruising speed: 845 km/h (525 mph, 456 kn), Mach 0.77
- Range fully loaded: 1,710 nautical miles (3,170 km; 1,970 mi)
