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Training aircraft
Ilyushin Il-103 is a training aircraft originating in Soviet Union / Russia. It was built by Ilyushin.
Soviet Union / RussiaTraining aircraft
Soviet Union / Russia
Ilyushin
Genrikh Novozhilov
In service
see Operators
66
1994–present
1996
17 May 1994
1
4 pax ( max payload: 270 kg (600 lb))
8 m (26 ft 3 in)
10.56 m (34 ft 8 in)
3.135 m (10 ft 3 in)
14.71 m 2 (158.3 sq ft)
7.6
900 kg (1,984 lb)
1,310 kg (2,888 lb)
150 kg (330 lb) / 200 L (53 US gal; 44 imp gal) in two wing tanks
1 × Teledyne Continental IO-360-ES2B 6-cyl. air-cooled horizontally-opposed piston engine, 157 kW (211 hp)
2-bladed Hartzell BHC-C2YF-1BF/F8459A-8R
220 km/h (140 mph, 120 kn)
180 km/h (110 mph, 97 kn)
117 km/h (73 mph, 63 kn) flaps up; 111 km/h (69 mph; 60 kn) 10° flaps
340 km/h (210 mph, 180 kn)
800 km (500 mi, 430 nmi) (at cruising speed, pilot and 270 kg (600 lb) payload with 30 min fuel reserve)
3,000 m (9,840 ft) (maximum certified altitude)
Utility: =4.4 / -1.8; Aerobatic: +6 / -3
3.167 m/s (623.4 ft/min)
89.1 kg/m 2 (18.2 lb/sq ft)
8.37 kg/kW (13.75 lb/hp)
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 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 .
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.
Capacity: 4 pax ( max payload: 270 kg (600 lb))
Length: 8 m (26 ft 3 in)
Wingspan: 10.56 m (34 ft 8 in)
Height: 3.135 m (10 ft 3 in)
Wing area: 14.71 m 2 (158.3 sq ft)
Empty weight: 900 kg (1,984 lb)
Max takeoff weight: 1,310 kg (2,888 lb)
Fuel capacity: 150 kg (330 lb) / 200 L (53 US gal; 44 imp gal) in two wing tanks
Powerplant: 1 × Teledyne Continental IO-360-ES2B 6-cyl. air-cooled horizontally-opposed piston engine, 157 kW (211 hp)
Maximum speed: 220 km/h (140 mph, 120 kn)
Cruise speed: 180 km/h (110 mph, 97 kn)
Stall speed: 117 km/h (73 mph, 63 kn) flaps up; 111 km/h (69 mph; 60 kn) 10° flaps
Never exceed speed : 340 km/h (210 mph, 180 kn)
Range: 800 km (500 mi, 430 nmi) (at cruising speed, pilot and 270 kg (600 lb) payload with 30 min fuel reserve)
Service ceiling: 3,000 m (9,840 ft) (maximum certified altitude)
Rate of climb: 3.167 m/s (623.4 ft/min)
Reference text from Wikipedia contributors, used under CC BY-SA 4.0.
Ilyushin Il-103 equipment records. Variants, orders and quantities are shown as reported in each inventory source; coverage is incomplete.
PeruArmy exact named equipment holdings: IL-103. Active, operational-reserve and training units excluding equipment in store; November 2025 IISS assessment. Named service only; no parent-force or national total inferred. Source role: AIRCRAFT / TRG. Original estimates, ranges, reporting names, reserve, lease and employment scopes retained; nested included counts are not added. Missile-system quantities mean launchers, not rounds. No readiness, crew, carried weapon, payload, factory-production or future order count inherited.