de Havilland Canada DHC-2 Beaver vs. Airbus A300-600F
... or view the full comparison list
here.
de Havilland Canada DHC-2 Beaver |
versus |
Airbus A300-600F |
13.56 m |
44 ft 6 in |
length |
54.08 m |
177 ft 5 in |
5 m |
16 ft 5 in |
height |
17.05 m |
55 ft 11 in |
16.56 m |
54 ft 4 in |
wingspan |
44.84 m |
147 ft 1 in |
2 x Armstrong Siddeley Double Mamba turboprop engines |
engines |
2 x General Electric CF6-80C2A5 turbofan engines |
Approximately 3,100 hp (2,312 kW) each |
thrust per engine |
Approximately 59,000 lbf per engine |
Approximately 6,200 hp (4,624 kW) total |
total thrust |
Approximately 118,000 lbf total |
24,200 lb |
10,977 kg |
MTOW |
170,000 kg |
374,786 lb |
2,535 km |
1,369 nm |
range |
4,830 km |
2,608 nm |
228 mph |
367 km/h |
cruise speed |
860 km/h |
534 mph |
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling |
capacity |
|
|
|
rotor diameter |
|
|
|
|
rate of climb |
|
|
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.