BRAND and MODEL
YAKOVLEV YAK 52TW And YAK 52TD
TYPE
Two-seat training and touring monoplane
ORIGIN
Romania
Romania
One 269 kw (360 hp) Vedeneyev M-14PF nine-cylinder supercharged air-cooled radial engine
SPECIFICATIONS
Wingspan: 9.9 m (32 ft 5¾ in)
Length: 7.7 m (25 ft 3 in)
Height: 2.5 m (8 ft 2 in)
Wing area: 15.3 m² (163 sq ft)
Max speed: 335 km/h (208 mph)
Max cruising speed: 325 km/h (202 mph)
Economical cruising speed (70% power): 250 km/h (155 mph)
Stalling speed clean: 105 km/h (65 mph)
Max rate of climb at sea level: 366 m/min (1,200 ft/min)
Max ceiling: 4,000 m (13,000 ft)
Range with 160 litres (35 Imp gals) of fuel: 600 km (373 miles)
Range with 260 litres (57 Imp gals) fuel: 1,200 km (746 miles)
Take-off run: 200 m (656 ft)
Landing run: 260 m (853 ft)
Empty weight: 950 kg (2,094 lb)
Payload: 425 kg (937 lb)
Loaded weight:1,360 kg (2,998 lb)
PHOTO
Airliners.net:Source of phothograph
