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An-124 Ruslan (Condor) Large Cargo Aircraft

Crew

An-124: Seven; An-124-100: Four; An-124-100M: Four; An-124-210: Three

Designer

Antonov ASTC, Ukraine

Manufacturer

Aviant State Aviation Plant, Kiev, and Aviastar, Ulyanovsk, Russia

Operator

Russian Air Force, Antonov Airlines and Volga Dnepr Airlines

Maiden Flight

December 1982

Service Entry

January 1986

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)

Quantity

Four

Turbofan Engines

An-124-100 - D-18t turbofans<br />An-124-100M - D-18t series 3<br />An-124-210 - RB211-524H-t

Thrust

229kN (264kN for An-124-210)

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 Hold Floor Length Including Ramps

36.5m

Width at Floor Level

6.4m

Height

21.08m

Volume

1,270m³
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