YAKOVLEV YAK 52TW And YAK 52TD

 

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