YAK 52 G-YAKR

 

 

 

 

 

.

Video Clips

G-YAKR taking off at North Weald

Click Hear to Leave a Message ------------

 

G-YAKR Details and specification

General Description

The Yakovlev Yak-52 first flew in 1976, and was produced in Bacau, Romania,by Aerostar. Designed as a primary trainer before moving onto jet aircraft. The aircraft is fully aerobatics capable of +7g / -5 g

The YAK 52 is a two seat piston engined primary trainer aircraft which is a tandem
cockpit variant of the single seat Yak 50 aeroplane. It was announced in 1978 as a
replacement for the Yak 18 and made it's first flight less than a year after
commencement of the design work. The Yak 52 is designed by the Russian
company, Yakovlev, although all Yak 52 aeroplanes have been produced in
Romania under license. Manufacture of the type began in 1979 and the 1000th
aeroplane was delivered in 1987.

G-YAKR (Formally LY-AOV) was constructed in 1989, and entered service with the Russian
DOSAAF (Military Sport Aviation) organisation with first flight on 11 August 1991. It
served with DOSAAF until 15 April 1994. A major overhaul was carried out by
Termikas on 18 April 2001 at 600:27 hours The aircraft was then ferried to the UK
on the Lithuanian register with a normal Category Certificate of Airworthiness.

Detail Description

General Data
Crew 2
Height 2.7 m
Length 7.745 m
Wing span 9.3 m
Wing area 15 sq. m
Propeller diameter 2.4 m (V530TA-D35 constant speed propeller)
Engine M-14P, 360 hp, 9 cylinder radial
Weights, Fuel & Oil
Dry weight 1035 kg
Maximum takeoff weight 1315 kg
Maximum landing weight 1315 kg
Weight of crew (Total) 180 kg
Maximum fuel load 120 L
Maximum oil load 16 L
C of G limits (%) 17.5 - 27.0
Performance
Maximum level airspeed (at altitude 1000 m) 270 km/h
Range (10% fuel reserve at 190 km/h) 465 km (2 h 30 min)
Takeoff roll 180 - 200 m
Landing roll 330 m
Stall speed, engine at idle - erect flight, clean 120 km/h
Stall speed, engine at idle - flaps, gear down 110 km/h
Stall speed, engine at idle - inverted 150 km/h
Approach speed 160 km/h
Touchdown speed 115 - 120 km/h
Takeoff speed 120 km/h
Climb speed 170 km/h
Maximum ceiling (no oxygen equipment fitted) 4000 m
Limitations
Never exceed speed (VNE) 420 km/h
Maximum manoeuvring speed 360 km/h
G limits +7/-5
Maximum gear extended speed 200 km/h
Maximum flaps extended speed 170 km/h
Minimum fuel qty for aerobatics 24 L
Maximum inverted flight time 2 min (followed by at least 3 min of erect flight)
Maximum oil load for cross-country 16 L
Maximum oil load for aerobatics 10 L
Minimum oil load 8 L

.


About Us | Site Map | Privacy Policy | Contact Us | ©2007 Roy Alexander