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Ilyushin Il-114 ✕ Hawker Siddeley Andover ✕
Manufacturer Ilyushin Hawker Siddeley
Description The Ilyushin Il-114 (Russian Илью́шин Ил-114) is a twin-engine turboprop, short-haul regional airliner developed by the Ilyushin design bureau. The Hawker Siddeley HS 780 Andover is a twin-engined turboprop military transport aircraft produced by Hawker Siddeley for the Royal Air Force (RAF), developed from the Avro-designed HS 748 airliner.
ICAO Code I114 A748
First Flight 1990-03-29 1963-12-21
Entry Into service 1998-08-27
Service End 1998-01-01
Designer Ilyushin Hawker Siddeley
Type Turboprop Regional airliner Transport aircraft
Length (m) 26.88 23.7744
Height (m) 9.19 9.144
Cockpit Crew 2
Max Seating 64 52
Max Speed (km/h) 500 514.8556
Cruise Speed (km/h) 470 435.2196
Min Speed (km/h) 144.4559
Max Ceiling (m) 8000 7315.2
Rate of Climb (m/s) 6.096
Capacity Description 64 52 troops, 40 paratroops or 24 stretcher cases / 14365 lb payload
National Origin Soviet Union
Number Built 22 37
Powerplant Description TV7-117S 2 × Rolls-Royce RDa.12 Dart Mk 201 turboprop engines, 2420 kW (3245 hp) each
Primary Users Uzbekistan Airways (former), Vyborg Airlines (former) Royal Air Force, Royal New Zealand Air Force, 748 Air Services
Status Retired; to be reintroduced in Russia Retired
Wikipedia Article (URL) en.wikipedia.org/wiki/Ilyushin_Il-114 en.wikipedia.org/wiki/Hawker_Siddeley_Andover
Flat Wing Span (m) 30 29.8704
Flat Wing Area (m²) 81.9 77.2396
Wake Category M M
Aircraft Engine TV7-117
Number of Engines 2 2