Voronezh Aircraft Production Association (Ilyushin) - Russia
Manufacturer(s)
Cuba; Russia
Operators
1992
Service Year
Russia
National Origin
Active, Limited
Project Status
3
Crew
30
Units
COMMERCIAL AVIATION
Used in roles serving the commercial aviation market, ferrying both passengers and goods over range.
182.1 ft
(55.50 meters)
Length
197.2 ft
(60.12 meters)
Width/Span
51.5 ft
(15.70 meters)
Height
265,657 lb
(120,500 kilograms)
Empty Weight
551,156 lb
(250,000 kilograms)
Maximum Take-Off Weight
+285,499 lb
(+129,500 kg)
Weight Difference
monoplane / low-mounted / swept-back
Mainplane Arrangement
Monoplane
Design utilizes a single primary wing mainplane; this represents the most popular modern mainplane arrangement.
Low-Mounted
Mainplanes are low-mounted along the sides of the fuselage.
Swept-Back
The planform features wing sweep back along the leading edges of the mainplane, promoting higher operating speeds.
4 x Aviadvigatel PS-90A turbofan engines developing 6,500lb of thrust each.
Propulsion
559 mph
(900 kph | 486 knots)
Max Speed
42,979 ft
(13,100 m | 8 miles)
Ceiling
7,456 miles
(12,000 km | 6,479 nm)
Range
MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030