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Military


Il-96


Specifications
Country of Origin Russia
Builder 
Role
Similar Aircraft
Model IL-96-300 IL-96-400
wing span (m) 57,66 (m) 60,105
length (overall) (m) 55,345 (m) 63,939
height (overall) (m) 17,55 (m) 15,717
wing area (m2) 350 (m2) 350
sweepback angle at 1/4-chord line (degree) 30 (degree) 30
fuselage diameter (m) 6,08 (m) 6,08
engine type PS-90A by-pass turbojet engine PS-90A by-pass turbojet engine
number of engines (pcs) 4 4
max take-off thrust (International Standard Atmosphere, ?=0) (kg) 4 ? 16000 (kg) 4 ? 16000
bypass ratio 4,4 4,4
ICAO standards compliance App.16, Ch.3 App.16, Ch.3
max take-off weight (t) 240 (t) 265
max payload (t) 40 (t) 58
max fuel tanks capacity (liter) 152620 (liter) 152620
cruise speed (km/h) 850-870 (km/h) 870
range with max passenger capacity (km) 9000 (km) 10000
flight altitude (m) 10000-12000 (m) 9000-12000
take-off run distance (m) 2700 (m) 2700
landing run distance (m) 1260 (m) 1650
flight crew 3 3
passengers in single class version 300436
two classes version 262386
three classes version 235 315
Service Life calendar 20 years 20 years
flights 12000 20000
flight hours 60000 60000
Cost 
User Countries 



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Page last modified: 17-04-2018 18:53:13 ZULU