Airbus A220-300 vs. Piper PA-34 Seneca
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Airbus A220-300 |
versus |
Piper PA-34 Seneca |
38.7 m |
127 ft 0 in |
length |
8.71 m |
28 ft 7 in |
11.5 m |
37 ft 9 in |
height |
2.99 m |
9 ft 10 in |
35.1 m |
115 ft 2 in |
wingspan |
11.64 m |
38 ft 2 in |
2 x Pratt & Whitney PurePower PW1500G |
engines |
2 x Continental IO-360 |
21,000–23,000 lb |
thrust per engine |
220 lbs |
42,000–46,000 lb |
total thrust |
440 lbs |
70,900 kg |
156,300 lb |
MTOW |
4,750 lb |
2,155 kg |
6,297 km |
3,402 nm |
range |
980 nm |
1,815 km |
Mach 0.82 |
101,3 km/h |
cruise speed |
165 kts |
103 mph |
Typical seating 2-class 120-150 |
capacity |
5 |
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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.