IL-76TD

Il-76TD aircraft is the evolution of the transport modification of the Il-76T aircraft.

The transportation efficiency of the aircraft has been improved, in comparison with Il-76T, by way of increasing maximum takeoff weight from 170 to 190 tons, maximum commercial load from 43.4 to 50 tons, and practical flying range with increased maximum load. Due to increased maximum takeoff weight and commercial load, and in order to improve operating life figures, the structures in the wing, fuselage and landing gear have been reinforced.

The aircraft is equipped with D-30KP series 2 engines ensuring maintenance of maximum takeoff thrust at higher temperatures of ambient air.

Implementation of methodologies developed by the State Research Institute of Civil Aviation and Design Engineering Bureau of Takeoff Methodsallow Il-76TD to operate from the same airstrips as the Il-76T, but with the increased takeoff weight, and its improved fuel efficiency ensures larger cargo transportation volumes, while consuming the same amount of fuel.

Il-76TD ensures transportation of a wide variety of cargoes in all kinds of conditions. Technical capabilities of the aircraft allow its operation in extreme conditions of the Antarctic, where it has been used successfully as the main transportation aircraft for many years already.

  • Maximum takeoff weight

    190 Ton’s
  • Maximum flight altitude

    12100 M
  • Top thrust (SI System, H=0)

    4x12000 KGF

Dimensional characteristics

  • Length

    46,6

  • Height, m

    14,76

  • Wingspan, m

    50,5

  • Wing area, sq. m

    300

  • Fuselage diameter, m

    4,8

Power plant parameters

  • Number x engine type

    4 x turbojet engine

  • Engine

    D-30KP series 2

  • Top thrust (SI system, H=0), kgf

    12 000

Weight parameters

  • Maximum takeoff weight, tons

    190

  • Maximum payload, tons

    50

  • Fuel tank capacity, l

    109 500

Aircraft performance

  • Cruising speed, km/h

    750 - 780

  • Flight altitude, m

    9 100–12 100

  • Flight range with payload of 40 tons, km

    4 900

  • Takeoff distance, m

    1 700

  • Landing distance, m

    930

Number of seats

  • Crew, persons

    7

Freight compartment parameters (upper deck)

  • Length x Width x Height, m

    24,54x3,45x3,4

  • Volume, cubic meters

    321

Specified life

  • Calendar operating life, years

    40

  • Number of flights

    10 000

  • Number of flight hours, hr

    35 000

News

Follow the latest news & events

Offices

Find out more about our offices

Contact us

We are Passion Movers