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Yakovlev Yak-53

General Aviation and Light Aircraft

The Yakovlev Yak-53 was a single-seat aerobatic trainer produced in the Soviet Union in 1981 and 1982, of which only one prototype was built. It was derived from the two-seat Yak-52 by deleting the front cockpit and reshaping the canopy, and it used the flying controls of the Yak-50 without the spring loading of the Yak-52. The prototype used the undercarriage and tankage of the prototype Yak-52 to save weight, making it 100 kg lighter, with a Vedeneyev M-14P nine-cylinder radial engine of 360 hp. It set two world records for time to height in its class in February 1982.

Facts
Engine Class
Piston 1
Status
Prototype 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Yakovlev Yak-53 (Wikipedia)

Of Make

Source Yakovlev Yak-53 (Wikipedia)
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Manufactured By

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Source Yakovlev Yak-53 (Wikipedia)Lead, maker
Quote, Lead, maker
was a single seat aerobatic trainer aircraft produced in the USSR during 1981/2

Originated In

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Source Yakovlev Yak-53 (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
was a single seat aerobatic trainer aircraft produced in the USSR during 1981/2
Sources
1. Yakovlev Yak-53 (Wikipedia)
  • Lead, body style
    was a single seat aerobatic trainer aircraft produced in the USSR during 1981/2
  • Lead, status
    Only one prototype was produced
  • Specifications, powerplant
    Vedeneyev M-14P 9-cylinder air-cooled radial piston engine
  • Lead, maker
    was a single seat aerobatic trainer aircraft produced in the USSR during 1981/2
  • Lead, country of origin
    was a single seat aerobatic trainer aircraft produced in the USSR during 1981/2
  • In Group: Homebuilt, Kit and Aerobatic Aircraft, Lead, kind of aircraft
    was a single seat aerobatic trainer aircraft produced in the USSR during 1981/2
  • Exemplifies: Aviation, Lead, mode
    was a single seat aerobatic trainer aircraft produced in the USSR during 1981/2
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