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  • Yakovlev Yak-52

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    Description

    The Yakovlev Yak-52 (Russian: Яковлев Як-52) is a Soviet primary trainer aircraft which first flew in 1976.

    General Information

    It was produced in Romania from 1977 to 1998 by Aerostar, as Iak-52, which gained manufacturing rights under agreement within the former COMECON socialist trade organisation. The Yak-52 was designed as an aerobatic trainer for students in the Soviet DOSAAF training organisation, which trained civilian sport pilots and military pilots. Currently the Yak-52 is used in the Fédération Aéronautique Internationale (FAI) World Aerobatic Yak 52 Competition, a popular powered aircraft one-design World Aerobatic Championship.

     

    A descendant of the single-seat competition aerobatic Yakovlev Yak-50, the all-metal Yak-52 is powered by a 268 kW (360 hp) Vedeneyev M14P nine-cylinder radial engine.

     

    Since the aircraft was designed to serve as a military trainer, the development of the aircraft incorporates a number of features to be found on the early postwar fighters: notably the cockpit tandem layout (instrument panel, seat design, cockpit opening system), tail design, tricycle landing gear, fuselage mixed construction (monocoque with steel tube construction), inner flaps, controls position, access panels on sides of the fuselage, even the location of the radio antenna and overall dimensions of the airplane, which extensively match the Yakovlev Yak-17 UTI jet fighter trainer (NATO code name Magnet).

     

    For more details, including the 7 variants, click here.

     

    Yak-52

     

    YakovlevYak52VH-YLGYTYA.jpg_thumb.c425f25264ed5262ac35678def792fca.jpg YakovlevYak-52G-CBSS.jpg_thumb.acb2fa5a2d4d99abce27651f2640980f.jpg YakovlevYak-52ZK-ADM.jpg_thumb.ccf818939f55c63d591131f83105aa42.jpgYakovlev_Yak-52RF-00983.jpg_thumb.17bc3add080726a3a99cf1d4e8947857.jpg

     

    Yak-52TW tail wheel variant

     

    YakovlevYak52TWVH-YKKtouchdownYMEL20100320.jpg_thumb.06bf17f8a8505f7ea0d830f4e4255e71.jpg

    Specifications

    Seats:
    Two in tandem
    Length:
    7.745 m (25 ft 5 in)
    Wingspan:
    9.30 m (30 ft 6 in)
    Height:
    2.70 m (8 ft 10 in)
    Wing Area:
    15.00 m2 (161.5 sq ft)
    Empty Weight:
    1,015 kg (2,238 lb)
    MTOW:
    1,305 kg (2,877 lb)
    Fuel Capacity:
    122 L (32 US gal; 27 imp gal)
    Powerplant:
    1 × Vedeneyev M-14P nine-cylinder radial engine, 270 kW (360 hp)
    Vne:
    360 km/h (220 mph, 190 kn)
    Cruise Speed:
    190 km/h (120 mph, 100 kn) at 1,000 m (3,300 ft) (econ cruise)
    Stall Speed:
    85–90 km/h (53–56 mph, 46–49 kn) flaps down, engine idling
    Range:
    550 km (340 mi, 300 nmi) at 500 m (1,600 ft)
    Rate of Climb:
    5.00 m/s (985 ft/min)
    Service Ceiling:
    4,000 m (13,000 ft)

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