The Fokker 100 is a twinjet regional aircraft that was produced by Fokker in the Netherlands. The aircraft is capable of carrying just over 120 passengers in a single-class configuration to an average range of 1,500 nm (2,780 km).
The Fokker 100 was based on the Fokker F28 with a fuselage stretched by 5.7 m (18.8 ft) to seat up to 109 passengers, up from 85. It is powered by two newer Rolls-Royce Tay turbofans, and it has an updated glass cockpit and a wider wing and tail for increased maximum weights.
Fokker had financial troubles and went bankrupt in March 1996, and production ended in 1998 after 283 deliveries.
Systems
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Power Plant |
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Landing Gear |
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Ice & Rain |
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Hydraulic System |
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Fuel |
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Fokker 100 Automatic Flight Control and Augmentation System AFCAS |
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Flight Warning Systems |
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Flight Navigation Data Systems |
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Flight Management Systems |
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Flight Controls |
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Fire Protection |
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Emergency Equipment |
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Electrical System |
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Communications |
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Bleed Air System |
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Aircraft General |
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Air Cond & Press |
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APU |
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