Country of Origin
Two and five seat light aircraft
The Il-103 is one of the Russian aerospace industry's first attempts at designing and building a light aircraft for both eastern and western certification. The Il-103 was originally conceived in response to a Russian requirement for 500 military and civil basic trainers. Program go-ahead for this new tourer and trainer was given in 1990. First flight was originally planned for the second half of 1993, although this was delayed until May 17 1994. The Il-103 is one of the first all new four seat piston engine light aircraft to be developed in the 1990s. Optimised for western markets, it is powered by a six cylinder Teledyne Continental IO360, while western avionics equipment is available optionally. Ilyushin is marketing tourer and trainer versions which differ only in seating capacity, the trainer seats two, the tourer four or five. Ilyushin has now received both Russian and US FAA FAR Part 23 certification. Russian AP23 certification was awarded in February 1996, with first deliveries to local customers taking place later that year, while US certification was awarded in December 1998. The Il-103 is being developed in three basic models. The basic Il-103 is intended for the Russian market. The Il-103-10 is the export version with upgraded avionics, while the Il-103-11 is for export but with partially upgraded avionics compared to the Russian baseline fit. Ilyushin is looking at certificating the Il-103 with a 1460kg (3218lb) max takeoff weight and a development with a 194kW (260hp) class Teledyne Continental or Textron Lycoming. The Il-103 is one of a small number of promising Russian designs that looks capable of realistically achieving sales success in western markets and thus earning much needed foreign currency.
One 157kW (210hp) Teledyne Continental IO360ES2B fuel injected flat six piston engine driving a two blade variable pitch Hartzell propeller.
Max speed 220km/h (143kt), cruising speed 180km/h (97kt). Initial rate of climb 623ft/min. Max range with pilot, 270kg (595lb) payload and reserves 800km (432nm).
Empty 900kg (1984lb), max takeoff (utility) 1285kg (2832lb).
Wing span 10.56m (34ft 8in), length 8.00m (26ft 3in), height 3.13m (10ft 4in). Wing area 14.7m2 (158.4sq ft).
Seating for four or five, with rear bench seat for either two or three.
Russian certification was granted in early 1996, with first deliveries to Russian customers shortly after. Western certification and sales are planned. Approximately 15 were flying by late 1998. Unit price approx $US156,000.
The backbone of this section is from the The International Directory of Civil Aircraft by Gerard Frawley and used with permission. To get your own copy of the book click here.