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
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
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
