Airbus A220-300 vs. North American T-6 Texan
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Airbus A220-300 |
versus |
North American T-6 Texan |
38.7 m |
127 ft 0 in |
length |
9.0 m |
29 ft 6 in |
11.5 m |
37 ft 9 in |
height |
3.56 m |
11 ft 8 in |
35.1 m |
115 ft 2 in |
wingspan |
12.8 m |
42 ft |
2 x Pratt & Whitney PurePower PW1500G |
engines |
1 x Pratt & Whitney R-1340-AN-1 radial engine |
21,000–23,000 lb |
thrust per engine |
Approximately 600 hp |
42,000–46,000 lb |
total thrust |
Approximately 600 hp |
70,900 kg |
156,300 lb |
MTOW |
5,617 lb |
2,548 kg |
6,297 km |
3,402 nm |
range |
1,175 km |
634 nm |
Mach 0.82 |
101,3 km/h |
cruise speed |
145 mph |
233 km/h |
Typical seating 2-class 120-150 |
capacity |
Pilot and one passenger |
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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.