Ilyushin Manual

Electronic manuals from Russia's 'doomsday plane'. Unknown thieves broke into the Ilyushin Il-80 plane at an airfield in the southern region of Rostov, the BBC reports. FSX Ilyushin Il-76 (-78zh), modified for FSX (VC fixed). IL76 VC build updated, basic missing gauges, autopilot, GPS, radios, engine sounds for FSX. Original file and all credits go to the author of 52774-Il76-78zh available online. Note: Turing on the FD in autopilot will activate ground vehicles; autopilot will not work if you turn on 2D panel even once.  Comes with a virtual cockpit. Ilyushin Ilyushin IL-10 'Beast' Flight Manual USAF Islander Israel Aircraft Industries (IAI) J-22 Orao J-22 Orao J33 J4F Widgeon Jacobs Jacobs R755-9 Service Instructions USAAF Jaguar Javelin Jet Provost Jetstream Ju-52 Ju160 Junkers Junkers 52 Aircraft Operating Manual CAF Junkers Ju160 Sales Booklet Kaman Kaman H-43B Huskie Flight Manual USAF.

Ilyushin Manual 2

Ilyushin Manual
  • Passenger
  • Transport
    • Military-transport
    • Civil
  • Special-purpose aircraft
  • Projects
Manual
  • Performance

    General Data

    The Il-96-400M is a wide-body long-range airliner which is created on the basis of the production Il-96 aircraft for the purpose of further development of this type of aircraft and increasing their transport capabilities due to the longer fuselage and more powerful PS-90A1 engines instead of PS-90A.

    The Il-96-400M can carry up to 370 passengers. Large diameter of the fuselage provides modern day level of comfort for passengers during long flights. In terms of reliability, safety and effectiveness the Il-96-400M is on the level with world analogues.

    Due to the usage of modern systems and “glass cockpit” the flight crew of the aircraft will consist of 3 people.

    The aerodynamic configuration, design and aircraft systems employ state-of-the-art engineering solutions, which ensure high level of safety and effectiveness of aircraft operation. Modern materials used in the structure allow for decrease of aircraft weight, at the same time providing necessary integrity and stiffness. Wing aerodynamic ensures reliable and safe flight within the whole operational speed range.

    • Top thrust (SI system, H=0)
      4х17 400kgf
    • Maximum takeoff weight
      270tons
    • Flight altitude
      13 100m

    Estimated technical characteristics

    Dimensional characteristics
    Length, m63,939
    Height, m15,717
    Wingspan, m60,105
    Wing area, sq. m.350
    Fuselage diameter, m6,08
    Power plant parameters
    Number x engine type4 x turbojet engine
    Engine modelPS-90A1
    Top thrust (SI system, H=0), kgf17 400
    Compliance with ICAO standardsAppendix 16, Chapter 4
    Weight parameters
    Maximum takeoff weight, tons270
    Maximum payload, tons58
    Fuel tank capacity, l150 000
    Aircraft performance
    Cruising speed, km/h830-850
    Flight altitude, m9 100–13 100
    Flight range with passengers, km8 750
    Takeoff distance, m2 020
    Landing distance, m1 200
    Number of seats
    Crew, persons3
    Passengers, personssingle-class configuration 370
    Specified life
    Calendar operating life, years20
    Number of flights20 000
    Number of flight hours, hr.60 000

Ilyushin Il-76 Manual

Ilyushin

Ilyushin May

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