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PLANEFILE

YakovlevSingle-engine piston · Malmesbury, Wiltshire, United Kingdom

1984 Yakovlev Yak-50

Price
£80,000 ≈ $106,946
Year
1984
Total time
270 hours
Location
United Kingdom
1984 Yakovlev Yak-50, photo 11984 Yakovlev Yak-50, photo 21984 Yakovlev Yak-50, photo 31984 Yakovlev Yak-50, photo 41984 Yakovlev Yak-50, photo 51984 Yakovlev Yak-50, photo 61984 Yakovlev Yak-50, photo 71984 Yakovlev Yak-50, photo 81984 Yakovlev Yak-50, photo 91984 Yakovlev Yak-50, photo 101984 Yakovlev Yak-50, photo 111984 Yakovlev Yak-50, photo 121984 Yakovlev Yak-50, photo 131984 Yakovlev Yak-50, photo 141984 Yakovlev Yak-50, photo 151984 Yakovlev Yak-50, photo 161984 Yakovlev Yak-50, photo 171984 Yakovlev Yak-50, photo 181984 Yakovlev Yak-50, photo 191984 Yakovlev Yak-50, photo 201984 Yakovlev Yak-50, photo 211984 Yakovlev Yak-50, photo 221984 Yakovlev Yak-50, photo 231984 Yakovlev Yak-50, photo 241984 Yakovlev Yak-50, photo 251984 Yakovlev Yak-50, photo 261984 Yakovlev Yak-50, photo 271984 Yakovlev Yak-50, photo 281984 Yakovlev Yak-50, photo 29

Specifications

General

Registration
G-SOCT
Total time
270.0
Seats
1

Engine

Engine
Vedeneyev Vedeneyev M-14P
Engines
1
Horsepower
450

Propeller

Propeller time
15

Performance

Range (nm)
267

Remarks

Airframe time
270 hours TSN
Engine
90 Hours TSOH (Overhaul is at 500 Hours)
Propeller
15 Hours TSO
Crew
1
Length
7.68 m (25 ft 2 in)
Wingspan
9.50 m (31 ft 2 in)
Height
3.16 m (10 ft 4 in)
Wing area
15.00 m2 (161.5 sq ft)
Empty weight
765 kg (1,687 lb)
Gross weight
900 kg (1,984 lb)
Max takeoff weight
900 kg (1,984 lb)
Powerplant
1 × Vedeneyev M-14P 9-cylinder air-cooled radial piston engine, 268 kW (359 hp)
Propellers
3 blade composite Hardzell propellor (new)
Maximum speed
320 km/h (200 mph, 170 kn)(VNO)
Never exceed speed
420 km/h (260 mph, 230 kn)
Range
495 km (308 mi, 267 nmi)
Service ceiling
5,500 m (18,000 ft)
G limits
+9 -6
Rate of climb
16.0 m/s (3,150 ft/min)
Stall Speeds
Takeoff speed of 130 km/h (70 knots), utilizing its 360 hp radial engine.

Weights

MTOW (kg)
900
Empty weight (kg)
765
Useful load (kg)
135

Description

A Russian single seat aerobatic aircraft with an all-metal airframe, low wing monoplane with retractable landing gear and supercharged Vedeneyev M14P engine developing between 360 HP to 450 HP depending on type.

It was developed in 1975 and was in production until 1986.

The Yak 50 has fine handling characteristics enhanced by a relatively high power-to-weight ratio. It has a tough and agile airframe – the type was twice World Aerobatic Champion.

It has been used as a military trainer by several countries.

G-SOCT is one of the few surviving Yak 50’s in the UK and one of the lowest timed airframes being built in 1984.

Remarks

Its clean stall speed is 100 km/h (54 knots) in straight-and-level flight, but can reach 125 km/h (67 knots) when inverted.

Shares considered

Aircraft record

G-SOCT

Registration

Registration
G-SOCT
Registered as
Yakovlev YAK-50
Serial number
842804
Registered since
2014-09-11

Accidents and incidents

None on record

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