Airbus A300-600F vs. Mil Mi-26
... or view the full comparison list
here.
Airbus A300-600F |
versus |
Mil Mi-26 |
54.08 m |
177 ft 5 in |
length |
40.03 m |
131.3 ft |
17.05 m |
55 ft 11 in |
height |
8.15 m |
26.7 ft |
44.84 m |
147 ft 1 in |
wingspan |
|
|
2 x General Electric CF6-80C2A5 turbofan engines |
engines |
2 x Lotarev D-136 turboshaft engines |
Approximately 59,000 lbf per engine |
thrust per engine |
8,380 kW |
Approximately 118,000 lbf total |
total thrust |
16,760 kW |
170,000 kg |
374,786 lb |
MTOW |
56,000 kg |
123,459 lb |
4,830 km |
2,608 nm |
range |
800 km |
432 nm |
860 km/h |
534 mph |
cruise speed |
255 km/h |
158 mph |
|
capacity |
Up to 90 passengers |
|
|
rotor diameter |
32.00 m |
105 ft 0 in |
|
|
rate of climb |
8 m/s |
1,574 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.