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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