Il-76 CANDID
| 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 ( 50.50-50.6 m) |
| Aspect ratio | 8.5 |
| Wing area | 300.00m2 |
| Length | 152 ft, 10 in (46.6 m) / 53.194 meters IL-76MF |
| Height | 48.43 ft (14.76 m) |
| maximum diameter of fuselage | 4.80m |
| Main Track | 8.16m |
| Front and rear | 14.17m |
| Tail loading entrance | Width × height 3.40m × 3.40m |
| Fuselage door | Width × height 0.86m × 1.90m |
| Cargo Cabin Dimensions |
Length (m) 31,1 Cargo length (excluding goods containing bridge, Il-76MF) 24.54m Cargo length (excluding cargo bridge, except Il-76MF) 20.00m Long cargo (including cargo bridge, only IL-76MF) 31.14m Cargo length (excluding cargo bridge, only IL-76MF) 26.60m Maximum width (m) 3,40-3.45 Maximum height (m) 3.40-3.46 Cargo volume 235.3m3 |
| empty weight |
MD 89,000kg MF 101,000kg |
| Maximum Take-Off Weight |
LL, T 170,000kg
MD, TD (on a conventional runway takeoff and landing) 190,000kg TD (never laid off and landing on the runway) 152,000kg MD (never laid off and landing on the runway) 157,500kg MF 200,000kg |
| Payload Weight |
T 40,000kg TD 50,000kg MD 47,000kg |
| Maximum fuel weight | T 84840kg |
| Maximum landing weight |
LL 140,000kg TD 151,500kg MD 155,000kg |
| Maximum wing loading |
T 566.7kg/m2 TD 633.3kg/m2 |
| The maximum allowable load floor | T 1450 ~ 3100kg/m2 |
| 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) LL 600km / h T, TD 850km / h |
| Cruising speed |
760km/h to 780km/h @ 9km to 12km T, TD 750 ~ 800km / h MD, MF 750 ~ 780km / h |
| Range | 6,100km With 20t Payload 3,000km With 47t Payload |
| Maximum payload range |
TD 3650km MD 3800km |
| Maximum fuel range |
T 6700km MD 7800km |
| Service Ceiling | (15,500 m) |
| Cruising altitude | 9,000 ~ 12,000m |
| Service ceiling | 12,000m |
| Absolute ceiling | 15,500m / 50,855 ft |
| Fuel Efficiency | 231.5g/tkm |
| Take-Off Run on Concrete Runway |
1,600m T 850m MD, TD 1700m MF 1000m |
| landing Roll on Concrete Runway |
780m to 1,000m T 450m MD, TD 900 ~ 1000m |
| Armament | Rear gun turret on military model |
| Crew | Seven |
| Cost | |
| User Countries | CIS, Cuba, Iraq, India, Libya, Syria |
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