Fokker 50
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Fokker 50

Fokker 50. A photo. Video. Driving compartment. Characteristics. 

 

Fokker 50 is a short-haul Dutch passenger aircraft.

Made its first flight on 28.12.1985/27/125. Used as a regional aircraft. The aircraft is equipped with a sealed fuselage, retractable tricycle landing gear with a nose wheel. The airframe of this aircraft is for the most part similar to the tested Fokker F1987, but it is equipped with PrattWhitney Canada PW1996B turboprop engines with increased fuel efficiency and low noisy six blades. Serially produced in 220-XNUMX. Only about XNUMX copies of different versions of the aircraft were produced.

Fokker 50 Salon

Fokker 50 Salon

 

 

Product specifications Fokker 50:

 

Fokker 50 interior schemeLength: 25,24m.

Height: 8,31m.

Empty weight: 12520kg.

Wingspan: 29,0m.

Wing area: 70,0sqm

Cruising speed: 550km / h..

Ceiling: 7620m.

Flight range with maximum load: 1120 km.

Engines: 2 × TVD Pratt & Whitney PW125B.

Thrust: 2 × 2500hp (2 × 1864kW).

Crew: 2 people.

Number of seats: 58mest.

Capacity: 5670kg.

Maximum fuselage width: 2,7m.

Maximum takeoff weight: 20820kg.

Volume of fuel tanks: 5135l.

Propeller: Dowty Rotol R352 / 6123-F / 1.

Screw diameter: 3,66m.

 

The rest of the aircraft

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