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Soko G-4 Super Galeb

(Super Seagull)

Role: - basic/advanced training
- ground support
First flown: 17 July 1978
First production: 1983, SOKO's Mostar plant
Used by: 130 Yugoslavia (before the war)
12 Myanmar (Burma)

 

Technical data

G-4
Wing span: 9.88 meters (32 ft 5 in)
Length: 11.862 meters (38 ft 11 in)
Height: 4.28 meters (14 ft 0.5 in) 
Wing area: 19.5 sq meters
Crew: 1 or 2
Weight empty: 3,134 kg
Training weight: 4600 kg
Take-off weight: 6.300 kg - max. weapon load (13,900 lb)
Weapon load: 1700 kg underwing
1950 including detachable cannon pod
Internal fuel load: 1307 kg
Maximum speed: 910 km/h (565 mph)
Combat radius: 812 km with 625 liters of fuel in auxiliary fuel tanks
Ceiling: 15,000 meters
Rate of climb: 1,800 meters per minute
Radar: None
Engines: one license-built Rolls-Royce Viper 632-46 non-afterburning turbojet, rated at 1,814 (4000 lb or 17.8 kN) kg thrust

 

Weapons

one GSh-23L 23mm twin-barrel cannon in detachable pod under fuselage

 

Variants

G-4 Super Galeb

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