In numbers Through the lens Video
Status: Testing
The twin-engine Il-114-300 is essentially an advanced version of the Il-114, it first flight in 2020. It can carry up to 68 passengers or 6.800/1.300 kg of cargo over a distance of 1.400/5.000 km.
The aircraft was developed with the main goal of replacing aircraft of similar class such as ATR-42, ATR-72, Bombardier Q-300, CRJ-100/200 used by Russian airlines and the aging An-24. The aircraft is composed exclusively of domestic systems and equipment of Russian origin. Power is provided by two 2.900 horsepower TV-7-117ST-01 turboprop engines, each of which drives newly designed six-blade AV112-114 type propellers with an increased thrust of 4.000 kg.
The Il-114-300 features a modern cockpit designed according to “glass cockpit” standards and adopting the most modern technological applications.
The aircraft will be produced by UAC enterprises in cooperation: by Aviastar, VASO - branches of PJSC Ilyushin, and Sokol Aircraft Plant. With its final assembly being carried out by JSC Russian Aircraft Corporation MiG.
Three-view drawing
Technical specifications
| DESIGNER | OKB Ilyushin |
| COUNTRY | Russia |
| TYPE |
Regional passenger turboprop aircraft
|
| CREW | 2 |
| POWER-PLANT | Two turboprop engines Klimov TV-7-117ST-01 |
| Power (ISA, H=0) e.h.p. | 2x2.900 |
| DIMENSIONS | |
| Length, m | 26,90 |
| Height, m | 9,05 |
| Wing span, m | 30,00 |
| Wing area, m2 | 81,90 |
| Fuselage diametr, m | 2,86 |
| WEIGHT | |
| Maximum take-off, kg | 23.500 |
| Normal take-off, kg | - |
| Empty aircraft, kg | 13.700 |
| Internal fuel, kg | 8.780 |
| Payload, kg | 6.800 |
| - max passengers | 68 |
| - basic equipment | 64 |
| PERFORMANCE | |
| Maximum speed, km/h | 500 |
| Economic speed, km/h | - |
| Cruising speed, km/h | 450 |
| Service ceiling, m | 7.600 |
| Range, km | |
| - with 68 passengers | 1.400 |
| - with maximum fuel reserve (with 1.300 kg of payload) | 5.000 |
| Takeoff run, m | 750 |
| Landing roll, m | 550 |
| ARMAMENT | Doesn't have (defensive). |