Canadair CL-415 vs. Mil Mi-26
... or view the full comparison list
here.
Canadair CL-415 |
versus |
Mil Mi-26 |
19.82 m |
65 ft 0 in |
length |
40.03 m |
131.3 ft |
8.66 m |
28 ft 5 in |
height |
8.15 m |
26.7 ft |
28.6 m |
93 ft 1 |
wingspan |
|
|
2 x Pratt & Whitney Canada PW123AF turboprop engines |
engines |
2 x Lotarev D-136 turboshaft engines |
2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW) |
thrust per engine |
8,380 kW |
4,300 to 4,760 shaft horsepower |
total thrust |
16,760 kW |
19,733 kg |
43,525 lb |
MTOW |
56,000 kg |
123,459 lb |
1,600 km |
864 nm |
range |
800 km |
432 nm |
290 km/h |
180 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.