Ilyushin Il-14

Length
22.3 m
Flat Wing Span
31.7 m
Height
7.9 m
Flat Wing Area
99.7 m²
Max Seating
32
Max Speed
417 km/h
Max Ceiling
7400 m
Number of Engines
2
First Flight
1950-10-01
Entry Into service
1954-01-01
Number Built
1348
Maximum Take-Off Weight
18 t (paragliders: kg)
Maximum Range
1305 km

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Maximum Range (km)
Ilyushin Il-14 18 1305

Similar airplanes

Name Aircraft Engine Length (m) Flat Wing Span (m) Max Seating
Henschel Hs 130 22 33.01 Compare
Ilyushin Il-12 21.31 31.7 32 Compare
Martin 2-0-2 21.6408 28.3464 40 Compare
Nord Noroit Junkers Jumo 213 22.05 31.6 Compare
Heinkel He 177 Greif Daimler-Benz DB 605 22 31.44 Compare
Tachikawa Ki-92 22 32 34 Compare
All data (27 fields)
Name
Ilyushin Il-14
Manufacturer
Avia Motors
Description
The Ilyushin Il-14 (NATO reporting name: Crate) is a Soviet twin-engine piston commercial and military personnel and cargo transport aircraft that first flew in 1950, and entered service in 1954.
ICAO Code
IL14
First Flight
1950-10-01
Entry Into service
1954-01-01
Service End
1998-01-01
Designer
Avia Motors
Type
Airliner, transport aircraft
Length (m)
22.3
Height (m)
7.9
Cockpit Crew
4
Max Seating
32
Max Speed (km/h)
417
Max Ceiling (m)
7400
Rate of Climb (m/s)
5
Capacity Description
24-32 passengers with flight attendant
National Origin
Soviet Union
Number Built
1348
Powerplant Description
2 × Shvetsov ASh-82T 14-cylinder air-cooled radial piston engines, 1417 kW (1900 hp) each
Primary Users
Soviet Air Force, Aeroflot , People's Liberation Army Air Force , Egyptian Air Force
Status
Retired
Wikipedia Article (URL)
en.wikipedia.org/wiki/Ilyushin_Il-14
Flat Wing Span (m)
31.7
Flat Wing Area (m²)
99.7
Wake Category
M
Number of Engines
2