Ilyushin Il-103
| Ilyushin Il-103 | |
|---|---|
 Ilyushin Il-103 at the MAKS 1999 |
|
| Type: | Light aircraft |
| Design country: | |
| Manufacturer: | |
| First flight: |
May 17, 1994 |
| Production time: |
from 1997 |
The Ilyushin Il-103 ( Russian Ильюшин Ил-103 ) is a single-engine all-metal aircraft . The machine has been mass- produced by Ilyushin since July 9, 1997. The low-wing aircraft with non-retractable nose landing gear offers space for up to 4 people. The first flight took place on May 17, 1994.
The Russian air traffic license was granted on September 15, 1996. The US approval was granted on 9 December 1998 and was the first to a Russian aircraft was granted.
The machine is intended as a travel or light aircraft , but can also be used as a small transport machine .
The lifespan is 14,000 flight hours or 20,000 landings or 15 years. The base sales price is US $ 156,500 (10/2005).
Technical specifications
| Parameter | Data |
|---|---|
| Engine | 1 × 160 kW Continental IO-360ES 6-cylinder boxer engine. |
| Propeller | Hartzell BHS-C2YF / F8459F-8R, adjustable, 2 blades |
| length | 8 m |
| height | 3.13 m |
| span | 10.56 m |
| Wing area | 14.71 m² |
| Takeoff mass | 1310 kg |
| Top speed | 220 km / h |
| Cruising speed | 200 km / h |
| Take-off run | 380 m |
| Landing runway | 320 m |
| Load factor | +4.4 / −1.8 g (max. 5 s) |
| Range | 800 km |
Web links
Commons : Ilyushin Il-103 - collection of pictures, videos and audio files
- Il-103. www.ilyushin.org, accessed on May 6, 2018 .