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Soko G-4 Super Galeb

Yugoslav single-engine advanced jet trainer and light ground-attack aircraft, developed in the 1970s and utilized for both pilot training and close air support missions. Key figures: top speed 910 km/h, range 1,900 km, service ceiling 12,850 m, max takeoff weight 6,330 kg, built 85. In service with 1 air force as of 2026 — Serbia (20).

Max speed
910km/h
Range
1,900km
Produced
85units
Active worldwide
20
Soko G-4 Super Galeb military training aircraft side profile drawing
Side profile · Soko G-4 Super Galeb · length 12.3 m
Technical Specifications
Crew2 (student, instructor)
Length12.3 m (40.2 ft)
Wingspan9.9 m (32.4 ft)
Height4.3 m (14.1 ft)
Wing area19.5 m² (209.9 sqft)
Empty weight3,250 kg (7,165 lbs)
Max. takeoff weight6,330 kg (13,955 lbs)
Powerplant1 × Rolls-Royce Viper 632-46 turbojet 1,815 kgf each
Ejection seatMartin-Baker
Performance
Maximum speed910 km/h (565 mph)
Operational range1,900 km (1,181 mi)
Service ceiling12,850 m (42,159 ft)
Climb rate31.0 m/s (101.7 ft/s)
Operators — 2026
ActiveOn order
Armament
Missiles payload

GSh-23L 23mm gun pod; wingtip missile rails (G-4M variant)

Bombs payload

4 underwing hardpoints (350 kg inner, 250 kg outer) + 1 centerline (400 kg); BL755 cluster bombs, rockets, drop tanks

All Operators
🇧🇦 Bosnia and Herzegovina· 🇲🇲 Myanmar· 🇲🇪 Montenegro· 🇷🇸 Serbia

Description

The Soko G-4 Super Galeb, designated N-62, is a Yugoslav single-engine advanced jet trainer and light ground-attack aircraft. Developed during the 1970s by the Aeronautical Technical Institute at Žarkovo and manufactured by SOKO in Mostar, the aircraft was designed as a successor to the G-2 Galeb. The initial development aircraft, designated G-4 PPP, performed its maiden flight on July 17, 1978. The first production-standard G-4 flew in 1983, with quantity production commencing in 1984. Assembly continued until the breakup of Yugoslavia in 1991, with a total of 85 aircraft completed.

Design

The G-4 is a low-wing monoplane featuring swept wing and tail surfaces. It is powered by a single Rolls-Royce Viper turbojet; while early models used the basic Viper, production aircraft transitioned to the uprated Viper 632-46 engine. Design features include an all-moving anhedral tailplane, semi-circular air intakes, and JATO (jet-assisted take-off) attachment points. The crew of two sits in a tandem configuration on Martin-Baker ejection seats; the rear seat is elevated to improve instructor visibility. Avionics support flight in adverse weather and at night, including a radio altimeter and gyro-gunsight. To shorten landing distances, the aircraft utilizes a drogue parachute.

Armament

For combat operations, the G-4 is equipped with a removable centerline pod containing a twin-barrel 23mm GSh-23L cannon with 200 rounds. Four underwing hardpoints are provided, with the inboard pair rated for 350 kg and the outboard pair for 250 kg. The inboard pylons are plumbed for 70-gallon external fuel tanks. The aircraft can deploy Eastern and Western European munitions, including BL755 cluster bombs and air-to-air missiles.

Operational History

During the Yugoslav Wars, G-4s were utilized for ground-attack sorties, resulting in four recorded losses to air defenses. In February 1994, NATO aircraft shot down three G-4s for violating a UN no-fly zone. During the 1999 NATO bombing of Yugoslavia, 23 G-4s were destroyed on the ground. Outside of Yugoslavia, Myanmar was the sole export customer, receiving six aircraft in 1991 for counter-insurgency operations. The Serbian Air Force remains the primary operator and intends to operate an upgraded fleet through the 2030s.

Variants

  • G-4: Standard production advanced jet trainer and light ground-attack aircraft.
  • G-4Š: Unarmed jet trainer variant with five units produced.
  • G-4T: Dedicated target tug model.
  • G-4M: Upgraded variant featuring improved avionics, wingtip missile rails, and increased payload capacity.
  • G-4MD: Planned modernization program including LCD screens, HOTAS, HUD, and GPS-based navigation.
Wikipedia (CC BY-SA) and other open sources. Illustrations generated by AI. Last updated on 1 August 2026. Suggest a change

Frequently Asked Questions

What type of aircraft is the Soko G-4 Super Galeb?
The Soko G-4 Super Galeb is a military training aircraft aircraft developed by Soko and entered service in 1983.
What is the maximum speed of the Soko G-4 Super Galeb?
The Soko G-4 Super Galeb has a maximum speed of 910 km/h (565 mph).
What is the range of the Soko G-4 Super Galeb?
The Soko G-4 Super Galeb has an operational range of 1,900 km (1,180 miles). This range can vary based on payload, altitude, and mission profile.
When did the Soko G-4 Super Galeb first fly?
The Soko G-4 Super Galeb made its first flight on July 17, 1978. It entered operational service in 1983.
How many Soko G-4 Super Galeb have been built?
Approximately 85 units of the Soko G-4 Super Galeb have been produced since it entered service in 1983.
Which countries operate the Soko G-4 Super Galeb?
The Soko G-4 Super Galeb is operated by 1 countries with approximately 20 aircraft in active service. The largest operators include Serbia.
What is the service ceiling of the Soko G-4 Super Galeb?
The Soko G-4 Super Galeb has a service ceiling of 12,850 meters (42,158 feet). This is the maximum altitude at which the aircraft can maintain controlled flight.
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Latest Data Updates
  1. AUG 12026 Updated Manufacturer updated
  2. FEB 222026 Updated Description, number built and 21 more fields added; service entry year updated
  3. FEB 212026 Created Page created: Soko G-4 Super Galeb