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Military


IL-96 and foreign analogues

Features IL-96 MD-11 A-340-300
Dimensions:
Wingspan, m 60.1 51.66 60.3
length, m 63.94 61.2 63.65
height, m 15.72 17.6 16.74
wing area, sq.m 391.6 338.9 363.1
sweepback angle at line 1/4 chords, deg. 30 35 30
maximum fuselage width, m 6.08 6.01 5.64
Number of places:
Crew 2-3 2 2
Passengers in two classes 335-342 323 335
In three classes 311-318 276 295
In Economy Class 376-386 405 -
Cabin dimensions:
length, m 49.13 46.51 -
maximum width, m 5.7 5.72 5.28
maximum height, m 2.61 2.41 2.54
Engines Turbofan
Pratt & Whitney
PW2337
(4x17030kgs)
TRRD
General Electric
CF6-80C2D1F
(3x27920kgs)
or
Pratt & Whitney
PW4360
(3x27240 ruc)
Turbofan
CFM International
CFM56-5C2
(4x14160 kgf),
CFM56-5C3 (4x14755 kgf),
CFM56-5C4 (4x15435 kgf)
Weight and load capacity (maximum)
takeoff, t 270 286.2 271
unladen, t 132.4 131 129.3
aircraft without fuel, t 190.4 181.6 178
load fee, t 58 53.8 47.1
landing weight, t 210 195.2 190
fuel capacity, t 150.4 151.89 (capacity auxiliary fuel tank in the horizontal tail - 7.46) 141 (may be increased to 155.4)
In cargo compartments allowing the transport of 32 or LD3 containers 1AK-1, 5 - In cargo compartments allowing the transport of 32 containers LD3
Flight characteristics
Cruising speed, km / h 870 945 925
range, km 9,000 12,850, 293 passenger and baggage 13,300, with 295 passengers and luggage
Service ceiling, m 12100 12800 12000
Required runway length (ISA conditions at sea level), m 3350 2930 2790
Electronic Equipment By plane used digital EFIS avionics suite with six color multifunction displays, designed by the American firm "Rockwell Collins" with the participation of the Research Institute AS. Used wire control system, automatic piloting system (FMS), inertial navigation system with ring laser gyroscopes, collision warning system in flight TCAS and satellite navigation. Plane can land in weather conditions by category IIIm ICAO. The aircraft has a digital avionics suite with six EFIS displays, automatic piloting system (FMS), collision avoidance system in flight (TCAS), a system of wind shear warnings, satellite navigation The plane is equipped with digital avionics EFIS production French company "Thomson-CSF", consisting of six color multifunction displays for flight and navigation vyvola information as well as data on the on-board systems and warnings about failures. All Avionics ARINC 700 compliant.
Noise level ICAO Chapter 3 ICAO Chapter 3 takeoff - 86.5 dB, the side of the runway - 94.8 dB, while landing - 96 dB.



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Page last modified: 10-08-2014 19:52:45 ZULU