Ilyushin Il-114
From Wikipedia, the free encyclopedia
| Il-114 |
|
|
| Il-114-100 at the MAKS Airshow in Moscow, 2007 |
| Role |
Airliner |
| National origin |
Russia |
| Design group |
Ilyushin |
| First flight |
29 March 1990 |
| Number built |
14 |
The Ilyushin Il-114 (Russian Илью́шин Ил-114) is a Russian twin-engine turboprop airliner designed for local routes. In the Antonov An-24 class, it first flew in 1990. Altogether, 14 Il-114s have been built.[1]
[edit] Operational history
Current operators are Vyborg in Russia and Uzbekistan Airways in Uzbekistan. Vyborg Airlines took delivery of an Ilyushin 114 at MAKS 2005.[citation needed]
[edit] Variants
- Il-114 – The first production model.
- Il-114-100 – First flown on 26-Jan-1999 in Tashkent. Two PW-127 by Pratt & Whitney Canada turboprops. 64 passengers.
- Il-114-120 – Two PW-127H by Pratt & 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[4] |
Il-114-100[5] |
Il-114-300[6] |
Il-114T[7] |
| 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 |
750 m (2,460 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) |
On the official site of Ilyushin, as per links provided above, both the -100 & -300 have a take off run of 750 Meters.
[edit] Accidents
- In 1999, a cargo version of Ilyushin Il-114 suffered a crash during testing.[8]
- On July 5, 1993, a test example of Ilyushin Il-114 suffered a crash during testing, due to crew error when pre-takeoff engine run-up protocol was not followed and both engines stalled on throttle-back during climbout. 7 of 9 crewmembers were killed.[9][10]
[edit] See also
- Aircraft of comparable role, configuration and era
- Related lists
[edit] References
The initial version of this article was based on material from aviation.ru. It has been released under the GFDL by the copyright holder.
[edit] External links
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