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, for sales in the United States.

General characteristics

Crew: 1
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 m2 (158.3 sq ft)
Aspect ratio: 7.6
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)
Propellers: 2-bladed Hartzell BHC-C2YF-1BF/F8459A-8R
Performance

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: 9,840 m (32,280 ft)
g limits: Utility: =4.4 / -1.8; Aerobatic: +6 / -3
Rate of climb: 3.167 m/s (623.4 ft/min)
Wing loading: 89.1 kg/m2 (18.2 lb/sq ft)
Power/mass: 8.37 kg/kW (13.75 lb/hp)

All rights to this mod belong to Sergey Golosov

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