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General
characteristics
- Crew: 5
- Capacity: 50,000 kg (Il-76)
- Payload: 42 tonnes (Il-76M), 48
tonnes(Il-76MD), 60 tonnes(Il-76MD-90A) ()
- Length: 46.59 m (152 ft 10 in)
- Wingspan: 50.5 m (165 ft 8 in)
- Height: 14.76 m (48 ft 5 in)
- Wing area: 300.0 m² (3,229.2 ft²)
- Empty weight: 92,500 kg
(Il-76TD-90)
(203,962 lb)
- Max. takeoff weight: 195,000 kg
(Il-76) (429,975 lb (Il-76TD-90))
- Powerplant: 4 × Aviadvigatel
PS-90-76 turbofans, 142 kN (32,000 lbf) or 14,500 kgf
each
Performance
- Maximum speed: 900 km/h (490 kt,
560 mph) Mach 0.82 depending on altitude
- Range: 4,300 km (Il-76) with 50
tonne max payload
- Service ceiling: 13,000 m (42,700
ft)
- Rate of climb: m/s (ft/min)
- Wing loading: 566.7 kg/m²
(Il-76M/T)
(116.05 lb/ft² (Il-76M/T), 129.72 lb/ft² (Il-76MD/TD))
- Thrust/weight: (Il-76)
- minimal landing run: 450 m with
thrust reversal
Armament
- Guns: 2× 23 mm cannon in
radar-directed manned turret at base of tail
- Bombs: Some military models have
2 hardpoints under each outer wing capable of supporting 500 kg bombs.
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