Boeing 777-8 vs. de Havilland Canada DHC-2 Beaver
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Boeing 777-8 |
versus |
de Havilland Canada DHC-2 Beaver |
69.8 m |
229 ft 1 in |
length |
13.56 m |
44 ft 6 in |
19.5 m |
64 ft |
height |
5 m |
16 ft 5 in |
71.8 m |
235 ft 6 in |
wingspan |
16.56 m |
54 ft 4 in |
2 x GE9X-105B1A |
engines |
2 x Armstrong Siddeley Double Mamba turboprop engines |
105,000 lb |
thrust per engine |
Approximately 3,100 hp (2,312 kW) each |
210,000 lb |
total thrust |
Approximately 6,200 hp (4,624 kW) total |
351,500 kg |
775,000 lb |
MTOW |
24,200 lb |
10,977 kg |
16,000 km |
8,638 nm |
range |
2,535 km |
1,369 nm |
900 km/h |
559 mph |
cruise speed |
228 mph |
367 km/h |
365 (2-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.