Ilyushin Il-76 Candid
Summary
Category | Transport aircraft |
Origin country | 🇨🇳 Ex-USSR |
First flight | 25 March 1971 |
Year of introduction | 1974 |
Number produced | 960 units |
Description
The Ilyushin Il-76 Candid is a multi-purpose, four-engine turbofan strategic airlifter designed by the Ilyushin design bureau in the Soviet Union. Its development began in the late 1960s to meet the Soviet Air Force's requirement for a heavy-lift cargo aircraft that could supplement the Antonov An-12. The Il-76 was intended to be capable of carrying heavy machinery, troops, and humanitarian aid over long distances, even to underdeveloped or remote areas with poor infrastructure.
The first prototype flew on March 25, 1971, and the aircraft entered service in 1974. It was initially produced at the Tashkent Aviation Production Association in Uzbekistan, then a part of the Soviet Union. Over the years, various versions have been produced, including specialized models for aerial refueling, firefighting, and even radar and surveillance.
The Il-76 has been widely exported and has seen service in various roles with several countries beyond Russia, such as India, China, and Ukraine. Its robust construction and versatility have made it a popular choice for civil and military operations worldwide.
The development of the Ilyushin Il-76 was a complex and multifaceted process that began with the articulation of the Soviet Air Force's requirements for a new heavy-lift cargo plane in the late 1960s. The aim was to create an aircraft that could perform a wide range of tasks, from the transport of heavy and oversized cargo to troop mobility. It was also to have the ability to operate from short and unpaved airstrips, making it ideal for deployment in remote or underdeveloped regions.
The Ilyushin design bureau, led by Sergey Ilyushin, took on the challenge and went through several design iterations before settling on the final configuration. The aircraft features a high-wing design, which allows for easier cargo loading and provides greater ground clearance. It is equipped with four Soloviev D-30KP turbofan engines, chosen for their reliability and performance.
The cargo hold was designed to be spacious, with a strong floor to accommodate a variety of payload types. It can be easily configured for different missions, be it carrying vehicles, palletized cargo, or personnel. The aircraft is equipped with a rear ramp that facilitates the loading and unloading of goods, and it can also perform airdrops.
The cockpit is designed for a crew of seven: two pilots, a navigator, a flight engineer, a radio operator, and two loadmasters. Advanced avionics were incorporated to assist with navigation and communication, but the Il-76 is also noted for its mechanical robustness, where more sensitive electronic systems might fail.
Operational history
The Ilyushin Il-76 has had a broad and varied operational history since its introduction in 1974. It has been employed in a range of roles across different theaters and for multiple purposes, both military and civilian.
In the military domain, the Il-76 has served as a primary strategic airlifter for the Russian (and prior, Soviet) Air Force, carrying everything from troops to heavy equipment. The aircraft has also been involved in numerous international conflicts and peacekeeping missions. For example, it played a role in the Soviet-Afghan War from 1979 to 1989, airlifting troops and supplies into Afghanistan and bringing wounded soldiers back home. It has also been utilized in UN humanitarian missions and in airlift operations during natural disasters. Countries like India and China have similarly employed the Il-76 for their own military needs, such as troop movements and disaster relief operations.
The Il-76 has also been adapted for specialized roles, including as an aerial refueling tanker (Il-78) and an airborne command post. Some versions are equipped with advanced radar and used for airborne early warning and control (AEW&C).
On the civilian front, the Il-76 has been extensively used in cargo transportation, especially for oversized or heavy cargo that cannot be accommodated by typical commercial freighters.
The Il-76's capacity to operate from less-than-ideal airfields—thanks to its rugged design—has made it a preferred choice for operations in remote areas, like Antarctica. Several countries have used the Il-76 for Antarctic resupply missions, taking advantage of its long range and heavy-lift capabilities.
Variants
- Il-76M: An improved version of the original Il-76, featuring increased maximum takeoff weight and other enhancements for military use.
- Il-76MD: Further improved variant with greater payload capacity and extended range, largely used by Russian and Indian military forces.
- Il-76MF: A stretched version of the Il-76MD, featuring a longer fuselage to accommodate more cargo and updated avionics.
- Il-76T: This is the basic civilian version used primarily for cargo transport.
- Il-76TD: An enhanced civilian version with more powerful engines and increased payload capacity.
- Il-78: Adapted for use as an aerial refueling tanker, this variant features additional fuel tanks and refueling pods.
- Il-76PP: Electronic warfare and jamming platform, designed to disrupt enemy communications and radar systems.
- Il-82/Il-76VKP: Also known as "Maxdome," this is an airborne command post variant equipped with advanced communications and command and control systems.
- Il-76MD-90A: An upgraded variant featuring new PS-90A-76 engines for better fuel efficiency and range, as well as modernized avionics.
- Il-76MDK: Used for cosmonaut training in zero-gravity maneuvers; the interior is modified to simulate a weightless environment during parabolic flights.
- Il-76 Firebomber: Adapted for firefighting purposes, capable of dropping large amounts of water or fire retardant.
- A-50 Mainstay: An Airborne Early Warning and Control (AEW&C) variant equipped with a large rotodome radar for long-range surveillance and command control functions.
Technical specifications
Version: Il-76MD-90A | |
---|---|
Maximum speed | 900 km/h (559 mph) |
Wing area | 300 m² (3229.2 sqft) |
Wingspan | 50.5 m (165.7 ft) |
Height | 14.8 m (48.4 ft) |
Length | 46.6 m (152.9 ft) |
Service ceiling | 13000 m (42651 ft) |
Empty weight | 92500 kg (203927 lbs) |
Max. takeoff weight | 195000 kg (429901 lbs) |
Powerplant | 4 × turbojets Aviadvigatel PS-90A-76 delivering 14500 kgp |
Current operating countries
Country | Units | ||
---|---|---|---|
Russia | 135 (+20) | ||
China | 30 | ||
India | 20 (+2) | ||
Algeria | 11 | ||
Iran | 8 | ||
Angola | 7 | ||
Uzbekistan | 3 | ||
Armenia | 2 | ||
Azerbaijan | 2 | ||
Belarus | 2 | ||
Egypt | 2 | ||
Syria | 2 | ||
Ukraine | 2 | ||
🇬🇶 | Equatorial Guinea | 1 | |
Libya | 1 | ||
Sudan | 1 |
Numbers in parentheses, e.g. '(+5)', indicate units ordered but not yet delivered.
All operators
Angola • Armenia • Azerbaijan • Burkina Faso • Belarus • China • Algeria • Egypt • Equatorial Guinea • India • Iran • Iraq • Kazakhstan • Libya • Russia • Sudan • Syria • Ukraine • Ex-USSR • Uzbekistan