Ilyushin Il-96

· Ilyushin · 4 × Aviadvigatel PS-90

Airplanes

Length

55.35 m

Flat Wing Span

60.12 m

Height

17.55 m

Max Seating

237

Cruise Speed

867.4364 km/h

Number of Engines

Aircraft Engine

First Flight

1988-09-28

Entry Into service

1992-12-29

Number Built

Maximum Take-Off Weight

250 t (paragliders: kg)

Total Fuel Capacity

152620

Maximum Range

10000 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Ilyushin Il-96	250	152620	10000

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Tupolev Tu-160		54.1	55.7		Compare
Ilyushin Il-106		57.6	58.5		Compare
Boeing C-17 Globemaster III	Pratt & Whitney PW2000	53.0352	51.5112	102	Compare
747SP	Pratt & Whitney JT9D	55.85	59.64	331	Compare
Tupolev Tu-126		56.5	51.4		Compare
Douglas C-132		55.7784	56.6928	800	Compare

All data (23 fields)

Name: Ilyushin Il-96
Manufacturer: Ilyushin
Description: The Ilyushin Il-96 () is a Russian four-engined long-haul wide-body jet airliner designed by Ilyushin in the former Soviet Union and manufactured by the Voronezh Aircraft Production Association in Voronezh, Russia.
ICAO Code: IL96
First Flight: 1988-09-28
Entry Into service: 1992-12-29
Designer: Ilyushin
Type: Widebody jet airliner
Length (m): 55.35
Height (m): 17.55
Max Seating: 237
Cruise Speed (km/h): 867.4364
Capacity Description: 237/263/300
National Origin: Soviet Union
Number Built: 34
Powerplant Description: Aviadvigatel PS-90A
Primary Users: Russian Air Force, Cubana de Aviación , Sky Gates Airlines , Aeroflot (historical)
Status: In service, in production
Wikipedia Article (URL): en.wikipedia.org/wiki/Ilyushin_Il-96
Flat Wing Span (m): 60.12
Wake Category: H
Aircraft Engine: Aviadvigatel PS-90
Number of Engines: 4