YAKOVLEV YAK-52 Civil Aircraft Model Details

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General Information of YAKOVLEV YAK-52

Developed From : Yakovlev Yak-50; DOSAAF

First Flight : 1976

Introduction : 1979

Manufacturer : Yakovlev; Aerostar

Primary Users : Soviet Air Force

Role : Two-seat trainer aircraft

Status : Operational

General characteristics of YAKOVLEV YAK-52

Crew : 2

Empty Weight : 1,015 kg (2,238 lb)

Height : 2.70 m (8 ft 10¼ in)

Length : 7.745 m (25 ft 5 in)

Max Takeoff Weight : 1,305 kg (2,877 lb)

Powerplant : 1 × Vedeneyev M-14P 9-cylinder radial engine, 268 kW (360 hp)

Wing Area : 15 m² (161.5 ft²)

Wingspan : 9.30 m (30 ft 6¼ in)

Performance of YAKOVLEV YAK-52

Cruise Speed : 190 km/h (103 kn, 118 mph) econ cruise at 1,000 m (3,280 ft)

Maximum Speed : 285 km/h (154 kn, 177 mph) at sea level

Never Exceed Speed : 360 km/h (194 kn, 223 mph)

Power/Mass : 300W/kg (0.18hp/lb)

Range : 550 km (296 nmi, 341 mi)

Rate Of Climb : 7.0 m/s (1,378 ft/min)

Service Ceiling : 4,000 m (13,125 ft)

Stall Speed : 85-90 km/h (46-49 kn, 53-56 mph)

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