Ilyushin IL-114

Ilyushin Aviation Complex

ICAOI114IATAI14
Ilyushin IL-114 aircraft
Ilyushin Aviation ComplexIlyushin IL-114
Photo: Kirill Borisenko · CC BY-SA 4.0 · Modified

Details

The Ilyushin IL-114 is a twin-engine turboprop regional airliner developed by the Ilyushin Aviation Complex in Russia. First flown in 1990, the IL-114 was designed to replace the aging Antonov An-24 and An-26 on regional routes across the Soviet Union and later Russia. The aircraft features a high-wing configuration with two Klimov TV7-117 turboprop engines, providing efficient operation on short to medium regional routes. Designed for 64 passengers in a typical single-class layout, the IL-114 can operate from unprepared runways and in harsh weather conditions. The family includes the original IL-114-100 with Western engines and the modernized IL-114-300 with Russian TV7-117ST engines and updated avionics. Production resumed in the 2020s with the IL-114-300 variant featuring domestically-produced components. The aircraft serves with operators including Uzbekistan Airways and is positioned as a modern regional turboprop for Russian and CIS markets.

3

Variants

20

Built

Weightscompared to Airbus A318

MRW (Maximum Ramp Weight)

23,600kg
0
25k
50k
68k

MTOW (Maximum Takeoff Weight)

23,500kg
0
25k
50k
68k

MLW (Maximum Landing Weight)

23,500kg
0
25k
50k
56k

MZFW (Maximum Zero Fuel Weight)

22,600kg
0
25k
53k

Empty Weight

15,900kg
0
25k
40k

Capacitycompared to Airbus A318

Passenger Capacity

64passengers
0
100
132

48% of A318 maximum capacity

Crew

Total
4
Cockpit
2
Cabin
2

Dimensions

Length

26.9m

Wingspan

30.0m

Height

9.2m

Wing Area

81.9m²

Cabin Width

2.64m

Cabin Height

1.92m

Sources6 figures on this page

Catalog Price

Base List Price

$18M USD

2023 catalog price

Note: Actual prices vary based on configuration, options, and negotiations. This represents the manufacturer's base catalog price.

Engine Specifications

Engine Count

2×

Engine Model

Klimov TV7-117S / TV7-117ST (2,750 shp)

Fuel & Cargo

Fuel Capacity

8,570 L

Cargo Volume

12.5 m³

Production & History

Total Produced

20

Production Status

In production

Manufacturing Period

1990–present

First Flight

March 29, 1990

Entered Service

January 1, 1998

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