Specifications - An-124 Condor Long-Range Heavy Transport Aircraft, Russia

Key Data
Crew	An-124 - 7 An-124-100 - 4 An-124-100M - 4 An-124-210 - 3
Weights
Maximum Take-Off Weight	392t
Load Carrying Capacity	Using a 2,800m runway (2,300m for An-124-210)
Load Carrying Capacity	150t using a 3,000m runway (2,500m for An-124-210)
Engines
Quantity	4
Turbofan Engines	An-124-100 - D-18t turbofans An-124-100M - D-18t series 3 An-124-210 - RB211-524H-t
Thrust	229kN (264kN for An-124-210)
Performance
Speed	800km/h to 850km/h
Cruise Speed at an Altitude of 9km	750km/h to 800km/h
Altitude	Up to 12,000m
Ferry Range With Maximum Fuel	13,300km (15, 250 for An-124-210)
Range With 40t Payload	10,960km (12,730km for An-124-210)
Range With 120t Payload	5,030km (5,950km for An-124-210)
Runway Length	3,000m (2,420m for An-124-210)
Take-Off Run on Concrete Runway	2,520m (2,050m for An-124-210)
Landing Roll on Concrete Runway	900m
Cargo Capacity
Cargo Hold Floor Length Including Ramps	36.5m
Width at Floor Level	6.4m
Height	21.08m
Volume	1,270m³