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BRAND and MODEL
YAKOVLEV YAK 50
TYPE
Single-seat high-performance aerobatic monoplane
ORIGIN
Union of Soviet Socialist Republics
ENGINE
One 269 kw (360 hp) Vedeneyev M-14P nine-cylinder supercharged air-cooled radial engine
SPECIFICATIONS
Wingspan: 9.50 m (31 ft 2 in)
Length: 7.80 m (25 ft 7 in)
Height: 3.2 m (10 ft 5 in)
Wing area: 15.0 m² (161.5 sq ft)
Never exceed speed: 450 km/h (280 mph)
Max cruising speed: 400 km/h (249 mph)
Economical cruising speed: 270 km/h (168 mph)
Rate of climb: 959 m/min (3,145 ft/min)
Service ceiling: 4,000 m (13,123 ft)
Take-off roll: 100 m (328 ft)
Landing roll: 250 m (820 ft)
Fuel capacity: 118 litres (26 Imp gals)
Range: 463 km (288 miles)
Empty weight: 775 kg (1,709 lb)
Useful load: 220 kg (485 lb)
Loaded weight: 995 kg (2,194 lb)
PHOTO
aviationsmilitaires.net:Source of phothograph
