Ilyushin Il-108

· Ilyushin · 2 × Lotarev DV-2

Airplanes

Length

15.85 m

Flat Wing Span

15 m

Height

5.5 m

Max Seating

Number of Engines

Aircraft Engine

Entry Into service

1990-01-01

Maximum Take-Off Weight

14.3 t (paragliders: kg)

Maximum Range

5390 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Ilyushin Il-108	14.3	5390

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Sud-Est Grognard	Rolls-Royce Nene	15.4	13.57		Compare
Hawker 800 (Raytheon)		15.5448	15.5448		Compare
Mikoyan-Gurevich I-320	Klimov VK-1	15.775	14.2		Compare
Northrop Tacit Blue		16.764	14.6304		Compare
Dassault Falcon 20	General Electric CF700	17.15	16.3	14	Compare
Lockheed L-133	Lockheed J37	14.73	14.22		Compare

All data (16 fields)

Name: Ilyushin Il-108
Manufacturer: Ilyushin
Description: The Ilyushin Il-108 is a twin-jet business-aircraft project, drafted in 1990 by the Russian manufacturer Ilyushin.
Entry Into service: 1990-01-01
Designer: Ilyushin Design Bureau
Length (m): 15.85
Height (m): 5.5
Cockpit Crew: 2
Max Seating: 15
Capacity Description: 1600 kg payload / 9-15 passengers
Powerplant Description: 2 × Lotarev DV-2 turbofan engines, 21.6 kN thrust each
Status: Abandoned project
Wikipedia Article (URL): en.wikipedia.org/wiki/Ilyushin_Il-108
Flat Wing Span (m): 15
Aircraft Engine: Lotarev DV-2
Number of Engines: 2