Boeing 747-400 vs. de Havilland Canada DHC-2 Beaver
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Boeing 747-400 |
versus |
de Havilland Canada DHC-2 Beaver |
70.56 m |
231 ft 10 in |
length |
13.56 m |
44 ft 6 in |
19.3 m |
63 ft 4 in |
height |
5 m |
16 ft 5 in |
59.49 m |
195 ft 4 in |
wingspan |
16.56 m |
54 ft 4 in |
Pratt & Whitney PW4000, General Electric CF6 -80C2 or Rolls-Royce RB211 -524G/H |
engines |
2 x Armstrong Siddeley Double Mamba turboprop engines |
Around 60,000 to 70,000 pounds |
thrust per engine |
Approximately 3,100 hp (2,312 kW) each |
Around 240,000 to 280,000 pounds |
total thrust |
Approximately 6,200 hp (4,624 kW) total |
396,834 kg |
875,000 lb |
MTOW |
24,200 lb |
10,977 kg |
13,492 km |
7,285 nmi |
range |
2,535 km |
1,369 nm |
939 km/h |
584 mph |
cruise speed |
228 mph |
367 km/h |
Typically accommodates 416 passengers in a three-class layout |
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.