Airbus A319neo vs. de Havilland Canada DHC-2 Beaver
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Airbus A319neo |
versus |
de Havilland Canada DHC-2 Beaver |
33.84 m |
111 ft 0 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 |
110kN (PW 1100G) or 109-156kN (CFM LEAP-1A) |
thrust per engine |
Approximately 3,100 hp (2,312 kW) each |
220kN (PW 1100G) or 218-312kN (CFM LEAP-1A) |
total thrust |
Approximately 6,200 hp (4,624 kW) total |
75,500 kg |
166,400 lb |
MTOW |
24,200 lb |
10,977 kg |
6,850 km |
3,702 nm |
range |
2,535 km |
1,369 nm |
530 mph |
853 km/h |
cruise speed |
228 mph |
367 km/h |
120-150 |
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.