| Technical data | ||
|---|---|---|
| Type | Il-76T 'Candid-A' | Il-76TD 'Candid-?' |
| Function | transport | |
| Year | 1974 | ? |
| Crew | 7 | ? |
| Engines | 4*120kN Soloviev D-30KP | |
| Wingspan | 50.5m | |
| Length | 46.59m | |
| Wing Area | 300m2 | |
| Weight | 170000kg | ? |
| Maximum Speed | 850km/h | ? |
| Cruise Speed | ? | 750km/h |
| Ceiling | 15500m | |
| Range | 6500km | 4000km |
| Maximum Load Range | ? | 2880km |
| PayLoad | 47000kg | 50000kg |
| Cargo volume | ? | 180m3 |
Similar in appearance to the U.S. C-141 but superior in many respects, the Il-76 is the main transport aircraft of the Soviet forces. It is also used by civil operators. The military version often has a tail gun turret and ECM equipment. It is a much-used platform for other missions, including the Il-78 'Midas' tanker and A-50 'Mainstay' AWACS aircraft.
A version of the Il-76 as a firefighting aircraft carrying 42000 liters of fire retardant also exists. Iraq development its own AWACS system, called 'Adnan', from the Il-76.
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| Three photos (17k, 22k, 15k) from report about North Pole Skydiving Expeditions. | ||
| Modified January 25, 1996 |
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