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Country of Origin: Netherlands. |
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Type: Short/medium-haul commercial transport. |
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Power Plant: Two 13,3201bst (6 042 kgp) Rolls-Royce RB183-03 Tay Mk 620-15 turbofans. |
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Performance: Max cruising speed, 497 mph (800 km/h) at 35,000ft (10670m) or Mach=0.75; econ cruise, 475mph (765km/h) or Mach=0.72; range (at 92,000-lb/41 730-kg MTOW with 107 passengers) at econ cruise, 1,330 mls (2140km), (at optional 95,000-lb/43092-kg MTOW), 1,698 mls (2733 km). |
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Weights: Operational empty, 51,260 Ib (23251 kg); standard max take-off, 92,0001b (41 730kg); optional max take-off, 95,0001b (43092kg). |
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Accommodation: Flight crew of two and standard seating for 107 passengers five abreast, optional arrangements including 60 business class and 45 economy class seats, or 12 first class and 80-85 economy class seats.
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Status: Two prototypes scheduled to enter flight test during second quarter of 1986, with certification following early 1987. First customer delivery (to Swissair) spring 1987, and anticipated production tempo of three monthly. Thirty-eight aircraft had been ordered by December 1985, with a further 31 on option. |
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Notes: The Fokker 100 is technically a derivative of the F28, but makes extensive use of technology developed from the abortive F29 and MDF-100. Apart from new engines, the Fokker 100 has new systems and equipment, a lenthened fuselage, and aerodynamically redesigned and extended wings. |
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FOKKER100 Dimensions: Span, 92 ft 11/2 in (28,08 m); length, 115 ft 1O in (35,31 m); height, 27ft 10 1/2in (8,60m); wing area, 977'4 sq ft (90,80m2). |
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Fonte: The New Observer's Book of Aircraft William Green |
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Sai o Fokker, entram os Airbus |
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Fokker100 REAL |
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