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Fokker 100
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Developing Nation: |
The Netherlands |
|
First
Flight: |
Fokker 100:
30 November 1986 (PH-MKH).
|
| Certification |
November 1987. |
|
First
Delivery: |
February 1988. |
|
Crew: |
2. |
| Passengers: |
107. |
|
Wing
Span: |
28,08 m. |
|
Wing
Area: |
93,50 mē. |
|
Length: |
35,53 m. |
|
Height: |
8,50. |
|
Engine(s): |
Two Rolls-Royce
Tay
Mk.620-15 or Mk.650-15. |
| Weight: |
25.500 kg. |
|
Max.
Take off weight: |
45.800 kg.
|
|
Max.
Landing weight: |
39.900 kg.
|
|
Cruise
Speed: |
780 Km/h |
|
Max. Speed: |
861 Km/h |
|
Operating altitude: |
10.670 m.
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Max.
Range: |
2.956 km. |
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