Airbus A340-500 vs. Mil Mi-26
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Airbus A340-500 |
versus |
Mil Mi-26 |
67.93 m |
222 ft 10 in |
length |
40.03 m |
131.3 ft |
17.53 m |
57 ft 6 in |
height |
8.15 m |
26.7 ft |
63.45 m |
208 ft 2 in |
wingspan |
|
|
4 Rolls-Royce Trent 500 |
engines |
2 x Lotarev D-136 turboshaft engines |
54,000 lbf (240 kN) |
thrust per engine |
8,380 kW |
216,000 lbf (960 kN) |
total thrust |
16,760 kW |
380,000 kg |
837,800 lb |
MTOW |
56,000 kg |
123,459 lb |
16,670 km |
9,000 nm |
range |
800 km |
432 nm |
475 knots |
880 km/h |
cruise speed |
255 km/h |
158 mph |
Typical seating 3-class 270-310 |
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.