| Role | Transport aircraft |
|---|---|
| National origin | Soviet Union |
| Manufacturer | Antonov, Aviastar-SP |
| First flight | 26 December 1982[1] |
| Introduction | 1986 |
| Status | In service |
| Primary users | Russian Air Force Antonov Airlines Volga-Dnepr Airlines |
| Produced | 1982–present |
| Unit cost | US$70–100 million |
General characteristics
- Crew: 4-6 (pilot, copilot, navigator,senior flight engineer (+flight engineer, radioman) + 2 loadmasters
- Capacity: 88 passengers or the hold can take an additional 350 on a palletised seating system
- Payload: 150,000 kg (330,000 lb)
- Length: 68.96 m (226 ft 3 in)
- Wingspan: 73.3 m (240 ft 5 in)
- Height: 20.78 m (68 ft 2 in)
- Wing area: 628 m² (6,760 sq ft)
- Empty weight: 175,000 kg (385,000 lb)
- Loaded weight: 405,000 kg (893,000 lb)
- Useful load: 230,000 kg (508,000 lb)
- Max. takeoff weight: 405,000 kg (893,000 lb)
- Powerplant: 4 × Ivchenko Progress D-18T turbofans, 229.5 kN (51,600 lbf) each
- Maximum speed: 865 km/h (467 kn (537 mph))
- Cruise speed: 800–850 km/h (430 kn (490 mph))
- Range: 5,400 km (2,900 nm, 3,360 mi (5,410 km))
- Service ceiling: 12,000 m (39,370 ft)
- Wing loading: 365 kg/m² (74.7 lb/sq ft)
- Thrust/weight: 0.23
Flight range
- An-124-100
- 0 tons of cargo = 15,000 km (8,100 nmi)[44]
- 10 tons of cargo = 14,100 km (7,613 nmi)
- 20 tons of cargo = 13,250 km (7,154 nmi)
- 30 tons of cargo = 12,300 km (6,641 nmi)
- 40 tons of cargo = 11,500 km (6,210 nmi)
- 72 tons of cargo = 8,700 km (4,698 nmi)
- 90 tons of cargo = 7,100 km (3,834 nmi)
- 97 tons of cargo = 6,500 km (3,510 nmi)
- 104 tons of cargo = 5,900 km (3,186 nmi)
- 108 tons of cargo = 5,550 km (2,997 nmi)
- 120 tons of cargo = 4,500 km (2,430 nmi)
- 122 tons of cargo = 4,300 km (2,322 nmi)
- Аn-124-100М-150
- 40 tons of cargo = 11,900 km (6,425 nmi)
- 92 tons of cargo = 7,500 km (4,050 nmi)
- 113 tons of cargo = 5,900 km (3,186 nmi)
- 120 tons of cargo = 5,400 km (2,916 nmi)
- 122 tons of cargo = 5,200 km (2,808 nmi)
- 150 tons of cargo = 3,200 km (1,728 nmi)