Airbus A220-300 vs. Lockheed Ventura
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Airbus A220-300 |
versus |
Lockheed Ventura |
38.7 m |
127 ft 0 in |
length |
15.7 m |
51 ft 5 in |
11.5 m |
37 ft 9 in |
height |
3.6 m |
11 ft 10 in |
35.1 m |
115 ft 2 in |
wingspan |
20 m |
65 ft 7 in |
2 x Pratt & Whitney PurePower PW1500G |
engines |
2 x Pratt & Whitney R-2800 radial engines |
21,000–23,000 lb |
thrust per engine |
2,000 hp |
42,000–46,000 lb |
total thrust |
4,000 hp |
70,900 kg |
156,300 lb |
MTOW |
15,000 kg |
33,100 lb |
6,297 km |
3,402 nm |
range |
2,670 km |
1,440 nmi |
Mach 0.82 |
101,3 km/h |
cruise speed |
230 mph |
370 km/h |
Typical seating 2-class 120-150 |
capacity |
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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.