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Il-114

Il-114

Turboprop Airplanes
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Il-114
Operational Photo
deagel.com
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Basic Information
Name
Il-114
Designation
Il-114
Alternate Designation
Il-114-100 (Version powered by Pratt & Whitney PW-127H engines), Il-114LL (avionics testing aircraft)
Equipment Type
Turboprop Airplanes
Manufacturer
Ilyushin Aviaton Complex
Date of Introduction
1997
Description

The Ilyushin IL-114 is a twin-engine turboprop aircraft suitable for commercial and military applications such as regional airliner and patrol aircraft respectively. Ilyushin Aviation Complex carried out the maiden flight on March 29, 1990. The Il-114 is suitable for regional routes operating from small unpaved runways and flying at day/night in all-weather conditions. An auxiliary power system allows for autonomous operation at ill-equipped airports. Flight data was unified into a central multifunctional display system based on color LCDs. The Russian aviation authorities certified the aircraft type in April 1997. Two Klimov TV7-117S engines rated at 2,500-hp each provide power to six-bladed propellers with a 3.6-m diameter.

Air & Air Defense Specifications
Crew 2
Range 1500.0 km
Service Ceiling 7600 m
Wingspan 30.00 m
Overview (Deagel)
Group Turboprop Airplanes
Status Active
Also Known As Il-114-100 (Version powered by Pratt & Whitney PW-127H engines), Il-114LL (avionics testing aircraft)
Origin Russia
Contractor Ilyushin Aviaton Complex
Initial Operational Capability (IOC) April 1997
First Flight March 29, 1990
Total Production 20
Specifications (Deagel)
Crew 2
Number of Engines 2
Passengers 64
Service Life Flight Hours 30000
Service Life Flights 30000
Area — Wing Area 81.9 square meter
Dimensions — Fuselage Diameter 2.9 meter
Dimensions — Height 9.3 meter
Dimensions — Length 26.9 meter
Dimensions — Wingspan 30 meter
Mass — Max Takeoff Weight 23.5 ton
Mass — Payload 6.5 ton
Performance — Ceiling 7,600 meter
Performance — Landing Run Distance 900 meter
Performance — Max Range 1,500 kilometer
Performance — Take Off Run Distance 1,100 meter
Power — Max Power at TakeOff 5,000 hp
Speed — Cruise Speed 500 kph
Time — Service Life 30 year
Volume — Fuel Tank Capacity 8,360 liter
Gear (Deagel)
Item 1 Turboprop Engines: PW-127H (2)
Item 2 Turboprop Engines: TV7-117S (2)
Variants
Variant 1 Il-114
Variant 2 Il-114T
Variant 3 Il-114MP
Variant 4 Il-114-300
Details
Country of Origin Russia
Sources

deagel.com: https://www.deagel.com/x/x/a001753

Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
26.9 m
Width
30 m
Height
9.3 m
Weight
23500 kg
Operators (2)
Russia
Uzbekistan
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