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IL-76 (Candid) Russian Cargo Transport Aircraft

IL-76

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Basic Information
Name
IL-76 (Candid) Russian Cargo Transport Aircraft
Designation
IL-76
Alternate Designation
Equipment Type
Manufacturer
Date of Introduction
1974
Description

The Ilyushin Il-76 (Russian: Илью́шин Ил-76; NATO reporting name: Candid) is a multi-purpose four-engine turbofan strategic airlifter designed by the Soviet Union's Ilyushin design bureau. It was first planned as a commercial freighter in 1967, as a replacement for the Antonov An-12. It was designed to deliver heavy machinery to remote, poorly served areas. Military versions of the Il-76 have been widely used in Europe, Asia and Africa, including use as an aerial refueling tanker or command center. The Il-76 has seen extensive service as a commercial freighter for ramp-delivered cargo, especially for outsized or heavy items unable to be otherwise carried. It has also been used as an emergency response transport for civilian evacuations as well as for humanitarian aid and disaster relief around the world. Because of its ability to operate from unpaved runways, it has been useful in undeveloped areas. Specialized models have also been produced for aerial firefighting and zero-G training. The aircraft was first conceived by Ilyushin in 1967 to meet a requirement for a freighter able to carry a payload of 40 tons (88,000 lb) over a range of 5,000 km (2,700 nmi; 3,100 mi) in less than six hours, able to operate from short and unprepared airstrips, and capable of coping with the worst weather conditions likely to be experienced in Siberia and the Soviet Union's Arctic regions. It was intended to replace the Antonov An-12. Another intended version was a double-decked 250-passenger airliner but that project was cancelled. The Il-76 first flew in March 1971. Production of Il-76s was allocated to the Tashkent Aviation Production Association in Tashkent, Uzbekistan, then a republic of the Soviet Union. Some 860 of the basic transport variants were manufactured. In the 1990s, modernized variants also equipped with Soloviev D-30 turbofan engines were developed (MF, TF), with a cargo compartment 20 m (66 ft) long by 3.4 m (11 ft) wide by 3.4 m (11 ft) tall; these larger variants were not produced in significant quantity due to the financial difficulties being experienced by the Russian Air Force, which was the primary operator of the type. The prototype of the Il-76MF, conducted its first flight on 1 August 1995.

Air & Air Defense Specifications
Crew 2
Variants
IL-76 Candid-A: First production model.
IL-76M Candid-B: Added rear turret with two 23-mm NR-23 guns and small ECM fairings each side of navigator’s windows.
IL-76MD Candid-B: Military version of IL-76T.
IL-76MF: Military variant with stretched fuselage and more powerful engine.
IL-76MF-100: A derivative of the IL-76M with CFM56-5C turbofans. Range increased to 7,000 km with 40,000 kg load.
IL-76PP: Electronic countermeasures aircraft
IL-76PS/IL-84: Search and rescue capable of 3-hour patrol with radius of 3,000 km.
IL-76VPK/IL-82 airborne command post: Variant of IL-76MD. Fitted with specialized communications equipment.
A-50 Mainstay: AWACS version.
Midas: Aerial tanker version.
IL-76: A-60 ASAT Aircraft A-60 Anti-Satellite Direct Energy Weapon System.
System
Alternative Designations See Variants
Crew 2 pilots, 1 navigator, 1 radio operator, 1 flight engineer
Engines Rybinsk D-30KP II turbofan with thrust reversers; 4 each
Max Ceiling 10,500 m
Speed
Maximum 919 km/h
Cruise 780 km/h
Fuel
Internal Tanks 109,480 liters in 12 tanks
External Tanks None liters
Dimensions
Length 46.6 m
Wingspan 50.5 m
Height 14.5 m
Weight Empty: 89,000 kg General Max: 190,000 kg Allowable Max: 210,000 kg Unprepared runway max weight: 157,500 kg
Width 3.45 m
Flight Range
With 20 ton payload 6,100 km
With 47 ton payload 3,000 km
Cargo Hold
Dimensions
Length to Ramp 20 m
Length with Ramp 24.5 m
Width 3.5 m
Height 3.4 m
Standard Payload
Internal 47,000 kg
Troops 140
Paratroopers 125
Survivability / Countermeasures
Entire Aircraft Pressurized Yes
Crew Emergency Escape Hatch Forward of Main Entry Door Yes
Flares for Illuminating Landing Area Yes
Radar Warning Receiver Yes
Electronic Jammers Yes
Chaff and Flares Yes
Armament
GSh-23L twin-barreled cannon in tail turret Yes
1LK222 Anti-Satellite Laser (A-60E variant)
Max Effective Range 1500 km
Target Set LEO Satellites
Notes Used to dazzle adversary satellites or burn through sensitive optics and sensors using intensive energy laser bursts.
Avionics / Sensor / Optics
Standard Fllight Controls Yes
Weather Radar in Nose Yes
Navigation and Ground Mapping Radar in Radome Yes
Night / Weather Capabilities Yes
Details
Country of Origin Russia
Category Fixed Wing Aircraft
Air > Fixed Wing Aircraft
Filter Label
I
Classification
Domain
Air & Air Defense
Equipment Status
Active
Operators (35)
Russia
China
United States
Ukraine
India
Iran
North Korea
Serbia
Belarus
Algeria
Angola
Armenia
Azerbaijan
Bahrain
Burkina Faso
Cambodia
Congo, Republic of the
Cuba
Egypt
Equatorial Guinea
Georgia
Hungary
Iraq
Jordan
Kazakhstan
Kyrgyzstan
Latvia
Libya
Mali
Sierra Leone
Sudan
Turkmenistan
United Arab Emirates
Uzbekistan
Yemen
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