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During celebrations held in November 1983 to mark the 25th anniversary of the F27 entering airline service, Fokker announced the launch of a 50-seat follow-on to be known as the Fokker 50. Based on the proven F27 airframe, but fitted with more fuel-efficient engines, six-bladed 'quiet' propellers, improved aerodynamics, a redesigned cockpit incorporating digital avionics and a new cabin interior, the external differences include extra windows, twin-nosewheel landing gear and upturned wingtips. Much use is made of lighter composite materials, and F50 commonality with the F27 is only 20%. Production is shared with Dassault, Fuji Heavy Industries, Deutsche Airbus, SABCA, Dowty
Rotol and Pratt & Whitney Canada with final assembly, systems integration and flight test carried out by Fokker at Schiphol. The first two prototypes were conversions of F27 airframes, with the first (PH-OSO), flying on 28 December 1985 followed by (PH-OSI) on 30 April 1986. The first production aircraft (PH-DMO) flew on 13 February 1987 and first delivery made (to DLT), on 7 August 1987. By mid-1991 Fokker held firm orders from 18 customers for 132 Fokker 50s, and had delivered 116. The standard production variant is the 46/50-seat Fokker 50-100 and the current build rate is 30 aircraft per year.
| PASSENGERS | 46-58 |
| ENGINE | 2 x Pratt & Whitney Canada PW125B turboprops, 1864kW |
| WEIGHTS |
| Take-off weight | 18990 kg | 41866 lb |
| Empty weight | 12570 kg | 27712 lb |
| DIMENSIONS |
| Wingspan | 29.0 m | 95 ft 2 in |
| Length | 25.2 m | 82 ft 8 in |
| Height | 8.3 m | 27 ft 3 in |
| Wing area | 70.0 m2 | 753.47 sq ft |
| PERFORMANCE |
| Cruise speed | 522 km/h | 324 mph |
| Ceiling | 7620 m | 25000 ft |
| Range | 2630 km | 1634 miles |
| nick, wqer(@)zda.com, 11.11.2007 this is not the real plane |
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