Boeing 747-400ER vs. de Havilland Canada DHC-2 Beaver
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| Boeing 747-400ER |
versus |
de Havilland Canada DHC-2 Beaver |
| 64.44 m |
211 ft 4 in |
length |
13.56 m |
44 ft 6 in |
| 19.4 m |
63 ft 8 in |
height |
5 m |
16 ft 5 in |
| 70.6 m |
231 ft 8 in |
wingspan |
16.56 m |
54 ft 4 in |
| 4 |
engines |
2 x Armstrong Siddeley Double Mamba turboprop engines |
| 258 kN (R-R RB211-524 G/H) or 252.4 kN (P&W PW4056) |
thrust per engine |
Approximately 3,100 hp (2,312 kW) each |
| 1032 kN (R-R RB211-524 G/H) or 1009.6 kN (P&W PW4056) |
total thrust |
Approximately 6,200 hp (4,624 kW) total |
| 396,895 kg |
875,300 lb |
MTOW |
24,200 lb |
10,977 kg |
| 14,205 km |
7,671 nm |
range |
2,535 km |
1,369 nm |
| 939 km/h |
584 mph |
cruise speed |
228 mph |
367 km/h |
| 416 passengers |
capacity |
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.
