Yakovlev "Yak 52" Propeller Blade - Price Before Discount £765 | Aeroart.co.uk

 This particular blade is from a Russian Yak 52TD and it’s one of only 2 Yak blades we’ve ever come across so we think its pretty unusual.  At some point this propeller has been damaged in a prop strike but that just adds to its history and we like it just the way it is. 

     This ones not available for polishing but can be mounted on a base  for an extra charge if required. 


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. 

Specifically 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 antena and overall dimensions of the airplane, which extensively match the Yakovlev Yak-17 UTI jet fighter trainer (NATO code name Magnet).

The aircraft has inverted fuel and oil systems permitting inverted flight for as long as two minutes. The engine drives a two-bladed counter-clockwise rotating, variable pitch, wood and fibreglass laminate propeller



Yakovlev Yak-52 ld.svg


  • Crew: 2
  • 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)
  • Airfoil: Clark YN
  • Empty weight: 1,015 kg (2,238 lb)
  • Max takeoff weight: 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)
  • Propellers: 2-bladed V-530TA-D35 constant-speed propeller


  • Maximum speed: 285 km/h (177 mph; 154 kn) at sea level
  • Cruise speed: 190 km/h (118 mph; 103 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
  • Never exceed speed: 360 km/h (224 mph; 194 kn)
  • Range: 550 km (342 mi; 297 nmi) at 500 m (1,600 ft)
  • Service ceiling: 4,000 m (13,000 ft)
  • g limits: +7/-5
  • Rate of climb: 5.00 m/s (985 ft/min)
  • Time to altitude: 15 min to 4,000 m (13,000 ft)


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