Ilyushin Il-103 vs Soko G-2 Galeb: Specs Compared

ATrainer aircraft

Soko G-2 Galeb

Jet trainer and ground-attack

First system

Second system

At a glance

Side by side

Length comparisonOne shared metre scale

Ilyushin Il-103Il-103 · Length

8 m

Length source ↗

Soko G-2 GalebG-2-A · Length

10.34 m

Length source ↗

Lengths retain their source configuration and measurement scope.

Measured figures

Head to head

22 of 44 rows sourced on both sides

8mIl-103 · Length

10.34mG-2-A · Length

LengthScopes differ

All recorded figures & sources

8 m

Il-103 · Length

Single source

8 m (26 ft 3 in)^[source]

10.34 m

G-2-A · Length

Single source

10.34 m (33 ft 11 in)^[source]

10.56mIl-103 · Wingspan

11.62mG-2-A · with tip-tanks

WingspanScopes differ

All recorded figures & sources

10.56 m

Il-103 · Wingspan

Single source

10.56 m (34 ft 8 in)^[source]

11.62 m

G-2-A · with tip-tanks

Single source

11.62 m (38 ft 1 in) with tip-tanks^[source]

3.14mIl-103 · Height

3.28mG-2-A · Height

HeightScopes differ

All recorded figures & sources

3.135 m

Il-103 · Height

Single source

3.135 m (10 ft 3 in)^[source]

3.28 m

G-2-A · Height

Single source

3.28 m (10 ft 9 in)^[source]

1.3t

3.4t

MassScopes differ

All recorded figures & sources

900 kg

Empty; Il-103 · Empty weight

Single source

1,310 kg

Maximum take-off; Il-103 · Max takeoff weight

Single source

900 kg (1,984 lb)^[source]

1,310 kg (2,888 lb)^[source]

2,620 kg

Empty; G-2-A · equipped

Single source

3,374 kg

Maximum take-off; G-2-A · clean aerobatic trainer

Single source

1Il-103 · Crew

2G-2-A · Crew

CrewScopes differ

All recorded figures & sources

1 people

Il-103 · Crew

Single source

1^[source]

2 people

G-2-A · Crew

Single source

2^[source]

220km/hMaximum; Il-103 · Maximum speed

756km/hMaximum; G-2-A · at sea level

SpeedScopes differ

All recorded figures & sources

180 km/h

Cruise; Il-103 · Cruise speed

Single source

220 km/h

Maximum; Il-103 · Maximum speed

Single source

220 km/h (140 mph, 120 kn)^[source]

180 km/h (110 mph, 97 kn)^[source]

756 km/h

Maximum; G-2-A · at sea level

Single source

756 km/h (470 mph, 408 kn) at sea level^[source]

800km

669km

RangeScopes differ

All recorded figures & sources

800 km

Il-103 · (at cruising speed, pilot and 270 kg (600 lb) payload with 30 min fuel reserve)

Single source

800 km (500 mi, 430 nmi) (at cruising speed, pilot and 270 kg (600 lb) payload with 30 min fuel reserve)^[source]

669 km

G-2-A · at 9,000 m (30,000 ft) with full tip-tanks

Single source

669 km (416 mi, 361 nmi) at 9,000 m (30,000 ft) with full tip-tanks^[source]

157kW

—

Power

All recorded figures & sources

157 kW

Il-103 · 1 × Teledyne Continental IO-360-ES2B 6-cyl. air-cooled horizontally-opposed piston engine

Single source

1 × Teledyne Continental IO-360-ES2B 6-cyl. air-cooled horizontally-opposed piston engine, 157 kW (211 hp)^[source]

—

11.1kN

Thrust

All recorded figures & sources

11.12 kN

G-2-A · 1 × DMB license-built Rolls-Royce Viper ASV.11 Mk 22-6 turbojet engine thrust

Single source

1 × DMB license-built Rolls-Royce Viper ASV.11 Mk 22-6 turbojet engine, 11.12 kN (2,500 lbf) thrust^[source]

14.7m²Il-103 · Wing area

19.4m²G-2-A · Wing area

Wing areaScopes differ

All recorded figures & sources

14.71 m²

Il-103 · Wing area

Single source

14.71 m 2 (158.3 sq ft)^[source]

19.43 m²

G-2-A · Wing area

Single source

19.43 m 2 (209.1 sq ft)^[source]

3,000mIl-103 · maximum certified altitude

12,000mG-2-A · Service ceiling

Service ceilingScopes differ

All recorded figures & sources

3,000 m

Il-103 · maximum certified altitude

Single source

3,000 m (9,840 ft) (maximum certified altitude)^[source]

12,000 m

G-2-A · Service ceiling

Single source

12,000 m (39,000 ft)^[source]

3.2m/sIl-103 · 623.4 ft/min

23m/sG-2-A · 4,494 ft/min

Rate of climbScopes differ

All recorded figures & sources

3.167 m/s

Il-103 · 623.4 ft/min

Single source

3.167 m/s (623.4 ft/min)^[source]

22.83 m/s

G-2-A · 4,494 ft/min

Single source

22.83 m/s (4,494 ft/min)^[source]

Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.

Configuration

Details

Ilyushin Il-103 and Soko G-2 Galeb configuration
Specification	Ilyushin Il-103	Soko G-2 Galeb
Type	Training aircraft^[source]	Jet trainer and ground-attack^[source]G-2 Galeb
National origin	Soviet Union / Russia^[source]	Yugoslavia^[source]G-2 Galeb
Manufacturer	Ilyushin^[source]	SOKO^[source]G-2 Galeb
Designer	Genrikh Novozhilov^[source]	Aeronautical Technical Institute^[source]G-2 Galeb
Status	In service^[source]	Limited service^[source]G-2 Galeb
Primary user	see Operators^[source]	—
Number built	66^[source]	248^[source]G-2 Galeb
Manufactured	1994–present^[source]	1965–1985^[source]G-2 Galeb
Introduction date	1996^[source]	—
First flight	17 May 1994^[source]	3 July 1961^[source]G-2 Galeb
Capacity	4 pax ( max payload: 270 kg (600 lb))^[source]	—
Aspect ratio	7.6^[source]	5.55^[source]
Fuel capacity	150 kg (330 lb) / 200 L (53 US gal; 44 imp gal) in two wing tanks^[source]	780 kg (1,720 lb) internal + 340 kg (750 lb) in two optional wing-tip drop tanks^[source]
Propellers	2-bladed Hartzell BHC-C2YF-1BF/F8459A-8R^[source]	—
Stall speed	117 km/h (73 mph, 63 kn) flaps up; 111 km/h (69 mph; 60 kn) 10° flaps^[source]	158 km/h (98 mph, 85 kn) flaps down and airbrakes out^[source]
Never exceed speed	340 km/h (210 mph, 180 kn)^[source]	—
g limits	Utility: =4.4 / -1.8; Aerobatic: +6 / -3^[source]	+ 8 - 4^[source]
Wing loading	89.1 kg/m 2 (18.2 lb/sq ft)^[source]	—
Power/mass	8.37 kg/kW (13.75 lb/hp)^[source]	—
Role	single-engine, low-wing training aircraft^[source]	—
Source measurement	The Ilyushin Il-103 is a single-engine, low-wing training aircraft developed by the Ilyushin Design Bureau that started in 1990 in the Soviet Union . The aircraft is now produced in Russia . It was the first Russian aircraft to achieve Federal Aviation Administration certification in 1998, it is for sale in the United States .^[source]Ilyushin Il-103 · Lead; only the objects and conditions stated in this passage Russia’s United Aircraft Corporation reached an agreement with Aviation Engineering Zrt of Pécs, Hungary, to develop and licence produce a modernised version of the Ilyushin Il-103 in Hungary in March 2021.^[source]Ilyushin Il-103 · Operational history / Hungary; only the objects and conditions stated in this passage Capacity: 4 pax ( max payload: 270 kg (600 lb))^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Length: 8 m (26 ft 3 in)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Wingspan: 10.56 m (34 ft 8 in)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Height: 3.135 m (10 ft 3 in)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Wing area: 14.71 m 2 (158.3 sq ft)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Empty weight: 900 kg (1,984 lb)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Max takeoff weight: 1,310 kg (2,888 lb)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Fuel capacity: 150 kg (330 lb) / 200 L (53 US gal; 44 imp gal) in two wing tanks^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Powerplant: 1 × Teledyne Continental IO-360-ES2B 6-cyl. air-cooled horizontally-opposed piston engine, 157 kW (211 hp)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Maximum speed: 220 km/h (140 mph, 120 kn)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Cruise speed: 180 km/h (110 mph, 97 kn)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Stall speed: 117 km/h (73 mph, 63 kn) flaps up; 111 km/h (69 mph; 60 kn) 10° flaps^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Never exceed speed : 340 km/h (210 mph, 180 kn)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Range: 800 km (500 mi, 430 nmi) (at cruising speed, pilot and 270 kg (600 lb) payload with 30 min fuel reserve)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Service ceiling: 3,000 m (9,840 ft) (maximum certified altitude)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Rate of climb: 3.167 m/s (623.4 ft/min)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage	—
Primary users	—	Yugoslav Air Force Libyan Air Force^[source]G-2 Galeb
Variant	—	J-21 Jastreb^[source]G-2 Galeb
Airfoil	—	root: NACA 64A213.5 ; tip: NACA 64A212^[source]
Endurance	—	2 hours30 minutes at 7,000 m (23,000 ft)^[source]
Time to altitude	—	3,000 m (9,800 ft) in 2 minutes 24 seconds 6,000 m (20,000 ft) in 5 minutes 30 seconds 9,000 m (30,000 ft) in 10 minutes 12 seconds^[source]
Take-off run	—	490 m (1,610 ft) on grass^[source]
Landing run	—	400 m (1,300 ft) on grass^[source]
Take-off run to 15 m (49 ft)	—	640 m (2,100 ft)^[source]
Landing run from 15 m (49 ft)	—	710 m (2,330 ft)^[source]
Guns	—	2× 12.7 mm (0.500 in) machine guns in nose with 80 rpg^[source]
Hardpoints	—	4 with a capacity of 300 kg (661 lb) total^[source]

FORCETALLY

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Ilyushin Il-103

Soko G-2 Galeb

Type

Training aircraft^[source]

Jet trainer and ground-attack^[source]G-2 Galeb

National origin

Soviet Union / Russia^[source]

Yugoslavia^[source]G-2 Galeb

Manufacturer

Ilyushin^[source]

SOKO^[source]G-2 Galeb

Designer

Genrikh Novozhilov^[source]

Aeronautical Technical Institute^[source]G-2 Galeb

Status

In service^[source]

Limited service^[source]G-2 Galeb

Primary user

see Operators^[source]

—

Number built

66^[source]

248^[source]G-2 Galeb

Manufactured

1994–present^[source]

1965–1985^[source]G-2 Galeb

Introduction date

1996^[source]

—

First flight

17 May 1994^[source]

3 July 1961^[source]G-2 Galeb

Capacity

4 pax ( max payload: 270 kg (600 lb))^[source]

—

Aspect ratio

7.6^[source]

5.55^[source]

Fuel capacity

150 kg (330 lb) / 200 L (53 US gal; 44 imp gal) in two wing tanks^[source]

780 kg (1,720 lb) internal + 340 kg (750 lb) in two optional wing-tip drop tanks^[source]

Propellers

2-bladed Hartzell BHC-C2YF-1BF/F8459A-8R^[source]

—

Stall speed

117 km/h (73 mph, 63 kn) flaps up; 111 km/h (69 mph; 60 kn) 10° flaps^[source]

158 km/h (98 mph, 85 kn) flaps down and airbrakes out^[source]

Never exceed speed

340 km/h (210 mph, 180 kn)^[source]

—

g limits

Utility: =4.4 / -1.8; Aerobatic: +6 / -3^[source]

+ 8 - 4^[source]

Wing loading

89.1 kg/m 2 (18.2 lb/sq ft)^[source]

—

Power/mass

8.37 kg/kW (13.75 lb/hp)^[source]

—

Role

single-engine, low-wing training aircraft^[source]

—

Source measurement

The Ilyushin Il-103 is a single-engine, low-wing training aircraft developed by the Ilyushin Design Bureau that started in 1990 in the Soviet Union . The aircraft is now produced in Russia . It was the first Russian aircraft to achieve Federal Aviation Administration certification in 1998, it is for sale in the United States .^[source]Ilyushin Il-103 · Lead; only the objects and conditions stated in this passage

Russia’s United Aircraft Corporation reached an agreement with Aviation Engineering Zrt of Pécs, Hungary, to develop and licence produce a modernised version of the Ilyushin Il-103 in Hungary in March 2021.^[source]Ilyushin Il-103 · Operational history / Hungary; only the objects and conditions stated in this passage

Capacity: 4 pax ( max payload: 270 kg (600 lb))^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage

Length: 8 m (26 ft 3 in)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage

Wingspan: 10.56 m (34 ft 8 in)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage

Height: 3.135 m (10 ft 3 in)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage

Wing area: 14.71 m 2 (158.3 sq ft)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage

Empty weight: 900 kg (1,984 lb)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage

Max takeoff weight: 1,310 kg (2,888 lb)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage

Fuel capacity: 150 kg (330 lb) / 200 L (53 US gal; 44 imp gal) in two wing tanks^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage

Powerplant: 1 × Teledyne Continental IO-360-ES2B 6-cyl. air-cooled horizontally-opposed piston engine, 157 kW (211 hp)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage

Maximum speed: 220 km/h (140 mph, 120 kn)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage

Cruise speed: 180 km/h (110 mph, 97 kn)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage

Stall speed: 117 km/h (73 mph, 63 kn) flaps up; 111 km/h (69 mph; 60 kn) 10° flaps^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage

Never exceed speed : 340 km/h (210 mph, 180 kn)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage

Range: 800 km (500 mi, 430 nmi) (at cruising speed, pilot and 270 kg (600 lb) payload with 30 min fuel reserve)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage

Service ceiling: 3,000 m (9,840 ft) (maximum certified altitude)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage

Rate of climb: 3.167 m/s (623.4 ft/min)^[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage

—

Primary users

—

Yugoslav Air Force Libyan Air Force^[source]G-2 Galeb

Variant

—

J-21 Jastreb^[source]G-2 Galeb

Airfoil

—

root: NACA 64A213.5 ; tip: NACA 64A212^[source]

Endurance

—

2 hours30 minutes at 7,000 m (23,000 ft)^[source]

Time to altitude

—

3,000 m (9,800 ft) in 2 minutes 24 seconds 6,000 m (20,000 ft) in 5 minutes 30 seconds 9,000 m (30,000 ft) in 10 minutes 12 seconds^[source]

Take-off run

—

490 m (1,610 ft) on grass^[source]

Landing run

—

400 m (1,300 ft) on grass^[source]

Take-off run to 15 m (49 ft)

—

640 m (2,100 ft)^[source]

Landing run from 15 m (49 ft)

—

710 m (2,330 ft)^[source]

Guns

—

2× 12.7 mm (0.500 in) machine guns in nose with 80 rpg^[source]

Hardpoints

—

4 with a capacity of 300 kg (661 lb) total^[source]