Boeing 747-8I vs. de Havilland Canada DHC-2 Beaver
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Boeing 747-8I |
versus |
de Havilland Canada DHC-2 Beaver |
76.25 m |
250 ft 2 in |
length |
13.56 m |
44 ft 6 in |
19.35 m |
63 ft 6 in |
height |
5 m |
16 ft 5 in |
68.45 m |
224 ft 7 in |
wingspan |
16.56 m |
54 ft 4 in |
4x General Electric GEnx 2B67 Turbofan |
engines |
2 x Armstrong Siddeley Double Mamba turboprop engines |
66,500 pounds |
thrust per engine |
Approximately 3,100 hp (2,312 kW) each |
266,000 pounds |
total thrust |
Approximately 6,200 hp (4,624 kW) total |
443,613 kg |
977,500 lb |
MTOW |
24,200 lb |
10,977 kg |
8,000 nm |
14,816 km |
range |
2,535 km |
1,369 nm |
Mach 0.86 |
1,062 km/h |
cruise speed |
228 mph |
367 km/h |
467 passengers (three-class configuration) |
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.