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The Ilyushin Il-114 is a Russian airliner that first flew in 1990. It suffered from a crash during testing in 1993, due to engine failure. Another test crash with the cargo version happened in 1999. Initially, orders for the aircraft have been slow, but during the 2007 MAKS Airshow Ilyushin announced the signing of a contract with Venezuela for a large purchase of 98 planes. However, according to Agence France-Presse, the state company Rosoboronexport, which has the monopoly for the export of arms of that country, denied participating in such an agreement[citation needed]. Current operators are Vyborg Airlines in Russia and Uzbekistan Airways in Uzbekistan. Vyborg Airlines (www.aviavyborg.ru) took delivery of an Ilyushin 114 at MAKS 2005.
The Il-114 is a twin-engine turboprop for local routes in the Yak-40 class (to replace the Yak-40?). It is similar to the Saab 2000 in size and appearance. Altogether, 15 planes have been built.
[edit] Variants (built and proposed)
- Il-114 - The first production model.
- Il-114-100 - First flown on 26-Jan-1999 in Tashkent. Two PW-127 by Pratt and Whitney, Canada turboprops. 64 passengers.
- Il-114-120 - Two PW-127H by Pratt and Whitney, Canada turboprops. 64 passengers.
- Il-114T - Cargo transport version. Il-114T delivered to Zhukovski for certification tests in March 2001. Two aircraft have been built by April 2001.
- Il-114P - Maritime patrol version.
- Il-114MP - Maritime patrol/strike version.
- Il-114FK - Military reconnaissance, elint, photo builder or cartographic map version.
- Il-114PR - SIGINT/AEW
- Il-140 - AWACS
- Il-140M - maritime patrol, ecological monitoring, search and rescue.
[edit] Operators
- Russia
- Uzbekistan
[edit] Specifications
|
Il-114[1] |
Il-114-100[2] |
Il-114-300[3] |
Il-114T[4] |
Cockpit crew |
2 |
Seating capacity |
64 |
64 |
52 |
none |
Length |
26.877 m (88 ft 2 in) |
Wingspan |
30 m (98 ft) |
Wing Sweepback |
3.1° |
Height |
8.32 m (27 ft 4 in) |
Cabin Width |
2.64 m |
2.28 m |
Fuselage Width |
2.86 m |
Useful load |
6500 kg (14,000 lb) |
7000 kg (15,000 lb) |
Maximum take-off weight |
23,500 kg (51,800 lb) |
Cruising Speed |
500 km/h (310 mph) |
Cargo Capacity |
? |
76 m³ (2700 ft³) |
Max Payload Range |
1000 km (620 mi) |
1400 km (870 mi) |
2100 km (1302 mi) |
1000 km (620 mi) |
Takeoff run |
1100 m (3600 ft) |
1500 m (4950 ft) |
1160 m (3828 ft) |
1100 m (3600 ft) |
Max. Fuel Capacity |
8360 L (2210 US gal) |
Service Ceiling |
7600 m (25,000 ft) |
Engine (× 2) |
Klimov TV7-117S turboprop, 2500 hp (1900 kW) |
Pratt & Whitney PW127Н turboprop, 2645 hp (1972 kW) |
Klimov TV7-117SM turboprop, 2650 hp (1980 kW) |
Klimov TV7-117S turboprop, 2500 hp (1900 kW) |
[edit] References
[edit] Related Aircraft
-BAe 748
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[edit] External links
The initial version of this article was based on material from aviation.ru. It has been released under the GFDL by the copyright holder.