Il-76 CANDID
Il-78 MIDAS
| Specifications | |
|---|---|
| Country of Origin | Russia |
| Builder | ILYUSHIN |
| Role | Heavy-transport, cargo (tanks, guns, and other equipment) |
| Similar Aircraft | C-141B Starlifter, C-5 Galaxy, C-17A Globemaster III |
| Wing Span | 165 ft, 8 in (50.6 m) |
| Length | 152 ft, 10 in (46.6 m) / 53.194 meters IL-76MF |
| Height | 48.43 ft (14.76 m) |
| Maximum Take-Off Weight | 170t |
| Payload Weight | 47 tons 57 tons maximum |
| Cargo Cabin Dimensions |
Length (m) 31,1 Maximum width (m) 3,40 Maximum height (m) 3,46 |
| Engine | 4 x D-30kp turbofans @ 12,000kgf each 4 x PS-90A-76 by-pass turbojet @ 14,000kgf each |
| Maximum speed | 530 mph (850 km/h) at 36,090 ft (11,000 m) |
| Cruising speed | 760km/h to 780km/h @ 9km to 12km |
| Range | 6,100km With 20t Payload 3,000km With 47t Payload |
| Service Ceiling | 50,855 ft (15,500 m) |
| Fuel Efficiency | 231.5g/tkm |
| Take-Off Run on Concrete Runway | 1,600m |
| landing Roll on Concrete Runway | 780m to 1,000m |
| Armament | Rear gun turret on military model |
| Crew | Seven |
| Cost | |
| User Countries | CIS, Cuba, Iraq, India, Libya, Syria |
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