Ilyushin Il-112

· Ilyushin

Airplanes

Length

24.15 m

Flat Wing Span

27.6 m

Height

8.89 m

Flat Wing Area

65 m²

Max Seating

Cruise Speed

450 km/h

Max Ceiling

7600 m

Number of Engines

First Flight

2019-03-30

Entry Into service

2023-01-01

Number Built

Maximum Take-Off Weight

21 t (paragliders: kg)

Total Fuel Capacity

7200

Maximum Range

2400 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Ilyushin Il-112	21	7200	2400

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
ATR 52		23.99	27.05	50	Compare
Antonov An-24	Ivchenko AI-24	23.53	29.2	50	Compare
Hamburger Flugzeugbau HFB 209	Napier Eland	23.32	28.55	48	Compare
Fokker 50		25.25	29	46	Compare
Xi'an Y-7		24.218	29.666	52	Compare
Xi'an MA60		24.71	29.2	62	Compare

All data (22 fields)

Name: Ilyushin Il-112
Manufacturer: Ilyushin
Description: The Ilyushin Il-112/Il-212 () is a high-wing light military transport aircraft being developed by Ilyushin Aviation Complex (JSC IL) for air landing and airdrop of military air cargo, equipment and personnel.
First Flight: 2019-03-30
Entry Into service: 2023-01-01
Designer: Ilyushin
Type: Light military transport
Length (m): 24.15
Height (m): 8.89
Max Seating: 44
Cruise Speed (km/h): 450
Max Ceiling (m): 7600
Capacity Description: 5,000 kg; 44 passengers
National Origin: Russia
Number Built: 2
Powerplant Description: 2 × Klimov TV7-117ST turboprop, 2610 kW (3500 hp) each
Primary Users: Russian Aerospace Forces
Status: In development
Wikipedia Article (URL): en.wikipedia.org/wiki/Ilyushin_Il-112
Flat Wing Span (m): 27.6
Flat Wing Area (m²): 65
Number of Engines: 2