Ilyushin Il-114

· Ilyushin · 2 × TV7-117

Airplanes

Length

26.88 m

Flat Wing Span

30 m

Height

9.19 m

Flat Wing Area

81.9 m²

Max Seating

Cruise Speed

470 km/h

Max Speed

500 km/h

Max Ceiling

8000 m

Number of Engines

Aircraft Engine

First Flight

1990-03-29

Entry Into service

1998-08-27

Number Built

Maximum Take-Off Weight

23.5 t (paragliders: kg)

Total Fuel Capacity

8360

Maximum Range

1000 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Ilyushin Il-114	23.5	8360	1000

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
British Aerospace ATP	Pratt & Whitney Canada PW100	26	30.63	64	Compare
NAMC YS-11		26.3	32	64	Compare
Hawker Siddeley Andover		23.7744	29.8704	52	Compare
Antonov An-30		24.26	29.2		Compare
An-26		23.8	29.3	40	Compare
IPTN N250		28.15	28	68	Compare

All data (26 fields)

Name: Ilyushin Il-114
Manufacturer: Ilyushin
Description: The Ilyushin Il-114 (Russian Илью́шин Ил-114) is a twin-engine turboprop, short-haul regional airliner developed by the Ilyushin design bureau.
ICAO Code: I114
First Flight: 1990-03-29
Entry Into service: 1998-08-27
Designer: Ilyushin
Type: Turboprop Regional airliner
Length (m): 26.88
Height (m): 9.19
Max Seating: 64
Max Speed (km/h): 500
Cruise Speed (km/h): 470
Max Ceiling (m): 8000
Capacity Description: 64
National Origin: Soviet Union
Number Built: 22
Powerplant Description: TV7-117S
Primary Users: Uzbekistan Airways (former), Vyborg Airlines (former)
Status: Retired; to be reintroduced in Russia
Wikipedia Article (URL): en.wikipedia.org/wiki/Ilyushin_Il-114
Flat Wing Span (m): 30
Flat Wing Area (m²): 81.9
Wake Category: M
Aircraft Engine: TV7-117
Number of Engines: 2