Boeing 777-200 vs. de Havilland Canada DHC-2 Beaver
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| Boeing 777-200 |
versus |
de Havilland Canada DHC-2 Beaver |
| 63.7 m |
209 ft 1 in |
length |
13.56 m |
44 ft 6 in |
| 18.6 m |
61 ft |
height |
5 m |
16 ft 5 in |
| 64.8 m |
212 ft 7 in |
wingspan |
16.56 m |
54 ft 4 in |
| General Electric GE90-77B or GE90-94B, Pratt & Whitney PW4077 & PW4090, Rolls-Royce Trent 877 & Trent 895 |
engines |
2 x Armstrong Siddeley Double Mamba turboprop engines |
| Up to 94,000 pounds |
thrust per engine |
Approximately 3,100 hp (2,312 kW) each |
| Up to 188,000 pounds |
total thrust |
Approximately 6,200 hp (4,624 kW) total |
| 299,370 kg |
660,000 lb |
MTOW |
24,200 lb |
10,977 kg |
| 5,240 nm |
9,711 km |
range |
2,535 km |
1,369 nm |
| 560 mph |
901 km/h |
cruise speed |
228 mph |
367 km/h |
| 305 |
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.
