Fokker 100

The short-haul jet built for efficient regional and trunk routes.

Overview

Fokker Netherlands ICAO: F100 1986–1997 Active $30 million

The Fokker 100 is a twin-engine regional jet developed in the Netherlands as a successor to the F28 Fellowship. Introduced in the 1980s, it offered improved fuel efficiency and a modernized cabin. The aircraft became a common sight on European and Australian routes.

Live Fleet Activity (F100)

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Specifications

Units
Engine
2 × Rolls-Royce Tay Mk.650 Turbofans
Engine type
Turbofan
Thrust
2 × 15,100 lbf · 67 kN
Avionics
Rockwell Collins DU-1000 EFIS
Wing tips
No winglets
Seats
122 economy · 107 business · 85 first
Crew
—
Cabin width
10 ft 2 in  ·  3.10 m
Cabin height
6 ft 7 in  ·  2.01 m
Cabin length
68 ft 3 in  ·  20.80 m
Exterior length
116 ft 7 in  ·  35.53 m
Tail height
27 ft 11 in  ·  8.50 m
Fuselage diameter
10 ft 10 in  ·  3.30 m
Wing span
92 ft 2 in  ·  28.08 m
Baggage volume
848 ft³  ·  24.0 m³
Gross weight
—
Empty weight
—
Max takeoff weight
101,000 lb  ·  45,800 kg
Max landing weight
88,000 lb  ·  39,900 kg
Max payload
26,400 lb  ·  12,000 kg
Fuel capacity
3,550 gal · 13,400 L · 10,700 kg (Jet A)
Max cruise speed
456 kt  ·  525 mph  ·  845 km/h
Maximum speed
—
Cruise speed
—
Approach speed
120 kt  ·  138 mph  ·  222 km/h
Range
1,680 nm  ·  1,930 mi  ·  3,110 km
Fuel burn
0.48 nm/gal  ·  0.23 km/L
Ceiling
35,000 ft  ·  10,700 m
Rate of climb
3,000 ft/min  ·  15 m/s
Takeoff distance
6,100 ft  ·  1,860 m
Landing distance
4,350 ft  ·  1,320 m
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Air Panama Fokker 100

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Operational Context

Fokker 100 — twin-engine regional jet airliner

The Fokker 100 first flew in 1986 and entered service in 1988. It was designed as a stretched and updated development of the earlier F28, featuring more efficient turbofan engines and improved avionics. The aircraft adopted a low-wing configuration with rear-mounted engines and a T-tail.

Powered by two Rolls-Royce Tay turbofan engines producing approximately 13,850 pounds of thrust (62 kN) each, the Fokker 100 cruises at around 460 knots (850 km/h). Maximum takeoff weight is roughly 100,000 pounds (45,360 kg). Typical seating capacity ranges from 85 to 109 passengers.

The Fokker 100 achieved strong sales before Fokker’s bankruptcy in the mid-1990s ended production. Many aircraft remain in service, particularly in Australia and parts of Europe. The type is regarded as one of the most successful regional jets of its generation.