Ilyushin Il-103
Ilyushin Aviation Complex
About
Ilyushin's only light aeroplane: a four-seat single-engine trainer and utility machine from a design bureau otherwise known for widebodies, certificated in the multipurpose category and sold in small numbers to Russian flying schools and to Peru. Interstate Aviation Committee type certificate 89-103 gives a maximum take-off mass of 1,150 kg, a maximum fuel load of 150 kg and a maximum operating speed of 340 km/h indicated, with a manoeuvring speed of 255 km/h and limit load factors of +4.4 and −1.8. The engine is an American Teledyne Continental IO-360ES of 210 hp turning a two-blade Hartzell propeller 1,930 mm across, restricted to 2,675 rpm on this airframe. The minimum crew is one pilot in the left seat and the base certificate allows two passengers; supplement № 2 covers aircraft cleared to 1,285 kg, which carry three.
Weightscompared to Airbus A318
Capacitycompared to Airbus A318
Passenger Capacity
2% of A318 maximum capacity
Crew
Sources5 figures on this page
- Карта данных сертификата типа № 89-103 (Ил-103)89-103Aviation Register of the Interstate Aviation Committee · tier 1 · 5 figures · pages 1, 2, 3
Engine Specifications
Engine Count
1×
Engine Model
Teledyne Continental IO-360ES
Production & History
Production Status
Out of production
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