ILYUSHIN 96-400T

The IL-96-400T aircraft is a cargo version of well-known IL-96-300 passenger aircraft with increased fuel capacity, stretched by 9.35 m and improved avionics. Designed by Ilyushin Aviation Complex (Moscow, Russia) and manufactured by Voronezh Aircraft Manufacturing Company (Voronezh, Russia), IL-96-400T is powered by new four turbofan two-shaft PS-90A1 engines, complying with the international ecological requirements. Aircraft has approved license to operate worldwide.

  • Maximum Payload: 92 tonnes
  • Cruising speed: 850-870 km/h
  • Range with 40 tonnes payload: 12000 km
New Aircraft, New Market

Polet Airlines is owning and operating the following registered IL-96-400 aircraft: RA-96101, RA-96102, RA-96103 and waiting for delivery of additional one by the end of 2011.

The IL-96-400T aircraft operated by 3 crew members is equipped with modern avionics which includes six multifunctional color-LCD displays (EFIS), Flight Management System (FMS), Inertial Navigation System, Collision avoidance System (CAS) including mode "S" transponder, EGPWS system, VHF communications (compliant with ICAO requirements of item 4.7 Appendix 10), and equipment permitting flights in RVSM conditions.

The avionics complex comply with modern requirements on international routes in Europe and North America (RNP-1, RNP-5, RNP-10, RNP-12.6, RNP-20) and allows to navigate and land under ICAO CAT II category, speed hold, automatic voice warning system (in English). The crew and cargo cabins correspond to aircraft requirements for protection against the illegal intrusion (the Amendment 27 to a Part 1 of the Appendix 6 to ICAO) and to safety requirements (Chapter 11 of the Appendix 8 to ICAO).

Operating Weights & Fuel Capacity
Max taxi weight: 266 / 271* tonnes
Max takeoff weight: 265 / 270* tonnes
Max landing weight: 220 tonnes
Max zero fuel weight: 208 / 210* tonnes
Max fuel: 116,3 tonnes
Aircraft Performance Characteristics (ISA)‏
Maximum flight altitude: 13.1 km
Required takeoff distance (with MTOW): 2450 m
Required landing distance (with MLW): 1700 m
Range with maximum payload: 4750 / 5000* km
Range with maximum fuel: 14500 km
Airfield elevation (relative to sea level)‏: -300 ÷ 1800
Range of operational temperatures: -45...+42 C
Maximum number of people on board: 9
Crew: 3
  IL-96-400 MD-11F:
Main Deck: 25PMC(P6) + 1PBJ(P2) 26PMC(P6)
Lower Deck: 9PMC(P6) 10PMC(P6)
Total Payload: 92 tonnes gross weight 89 tonnes gross weight
Total Volume: 580 cbm (as per the ULDs contour) 577 cbm
Main Deck Cargo Door dims: 4,85(W) x 2,87(H) m 3,5(W) x 2,6(H) m