Airbus A320neo vs. de Havilland Canada DHC-2 Beaver
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Airbus A320neo |
versus |
de Havilland Canada DHC-2 Beaver |
37.57 m |
123 ft 3 in |
length |
13.56 m |
44 ft 6 in |
11.76 m |
38 ft 7 in |
height |
5 m |
16 ft 5 in |
35.8 m |
117 ft 5 in |
wingspan |
16.56 m |
54 ft 4 in |
2 x PW 1100G or 2 x CFM LEAP-1A |
engines |
2 x Armstrong Siddeley Double Mamba turboprop engines |
120kN (PW 1100G) or 109-156kN (CFM LEAP-1A) |
thrust per engine |
Approximately 3,100 hp (2,312 kW) each |
240kN (PW 1100G) or 218-312kN (CFM LEAP-1A) |
total thrust |
Approximately 6,200 hp (4,624 kW) total |
79,000 kg |
174,200 lb |
MTOW |
24,200 lb |
10,977 kg |
6,300 km |
3,403 nm |
range |
2,535 km |
1,369 nm |
M0.82 |
101,3 km/h |
cruise speed |
228 mph |
367 km/h |
150-180 |
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.