| |
An-124-100
|
An-124-150 |
| ENGINE TYPE | 4x Lotarev D-18 T | 4x Lotarev D-18 T |
| ENGINE TAKE-OFF THRUST | 4×24 T Σ = 96 T | 4×24 T Σ = 96 T |
| MAXIMUM TAKE-OFF WEIGHT | 392 000 kg | 402 000 kg |
| OPERATING EMPTY WEIGHT | 192 215 kg | 192 559 kg |
| MAXIMUM PAYLOAD INCL.EQUIPMENT WEIGHT | 120 000 kg | 150 000 kg |
| MAXIMUM LANDING WEIGHT | 330 000 kg | 360 000 kg |
| MAXIMUM ZERO FUEL WEIGHT | 306 000 kg | 335 000 kg |
| CRUISING SPEED | 750 km/h | 750 km/h |
| CRUISING ALTITUDE | 31 000 — 35 000 ft | 31 000 — 35 000 ft |
| RANGE | 4 500 km | 4 500 km |
| MAXIMUM SINGLE LIFT WITH INTERNAL CRANES | 20 000 kg | 20 000 kg |
| CARGO COMPARTMENT DIMENSIONS | 6,4×4,4×36,5 m | 6,4×4,4×36,5 m |
| ENGINEERING CREW | 7 crew members | 7 crew members |
| FLIGHT CREW | 6 crew members | 6 crew members |
