Il-103 is a light multi-purpose aircraft for general aviation. This airplane has a highest safety level and exclusive manufacturing technology, which allows production in large batches at an affordable price. The aircraft combines high aerodynamic performance, comfortable and spacious cockpit, reliable engine and modern avionics.
The Il-103 boasts high cost efficiency and reliability and can be operated in any climatic conditions. It can be used asan air taxi, a patrol coastal guard aircraft, or an environmental monitoring vehicle.It is also designed for use by private usee and training aircraftby flying schools as the primary trainer.
Il-103 is easily operated from short airstrips and unpaved aerodromes, as this aircraft is easy to maintain and repair.
First flight took place on May 17, 1994. Test pilot was I.I.Gudkov.
Type Certificate No. 89-103 AR by IAC was granted in February 1996.
Type Certificate No. А45СЕ FAA was granted in December 1998.
Maximum shaft power (МСА, H=0)210kgf.
Maximum takeoff weight1 310kg
Maximum flight altitude4 000m
Main technical characteristics
Dimensional characteristics Length, m 8 Height, m 3,135 Wingspan, m 10,56 Wing area, sq. m. 14,71 Power plant parameters
Number x engine type 1 x reciprocating engine Engine model IO-360ES Maximum shaft power (МСА, H=0), kgf 210 Propeller diameter, m 1,93 Compliance with ICAO standards Appendix 16, Chapter 10 Weight parameters
Maximum takeoff weight, kg 1 310 Maximum payload, kg 350 Fuel tank capacity, l 200 Aircraft performance Cruising speed, km/h 180–225 Flight altitude, m up to 4 000 Practical flight range with a load of 240 kg, km 750 Takeoff distance, m 405 Landing distance, m 575 Number of seats
Crew, persons 1 Passengers, persons 3 Specified life
Calendar operating life, years 15 Number of flights 20 000 Number of flight hours, hr. 14 000