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

MTOW (Maximum Takeoff Weight)

1,150kg
0
25k
50k
68k

Capacitycompared to Airbus A318

Passenger Capacity

2passengers
0
100
132

2% of A318 maximum capacity

Crew

Total
1
Cockpit
1

Sources5 figures on this page

Engine Specifications

Engine Count

1×

Engine Model

Teledyne Continental IO-360ES

Production & History

Production Status

Out of production

Business jets and the API are coming

If you came here for the Ilyushin Il-103, you are the reader those are being built for. Leave an address and you will hear when they are ready.