Airbus A220-300 vs. Grumman OV-1 Mohawk
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Airbus A220-300 |
versus |
Grumman OV-1 Mohawk |
38.7 m |
127 ft 0 in |
length |
12.52 m |
41 ft 1 in |
11.5 m |
37 ft 9 in |
height |
3.89 m |
12 ft 9 in |
35.1 m |
115 ft 2 in |
wingspan |
14.63 m |
48 ft |
2 x Pratt & Whitney PurePower PW1500G |
engines |
2 x Lycoming T53 turboprop engines |
21,000–23,000 lb |
thrust per engine |
Approximately 1,100 hp each |
42,000–46,000 lb |
total thrust |
Approximately 2,200 hp total |
70,900 kg |
156,300 lb |
MTOW |
14,950 lb |
6,781 kg |
6,297 km |
3,402 nm |
range |
1,690 km |
913 nm |
Mach 0.82 |
101,3 km/h |
cruise speed |
230 mph |
370 km/h |
Typical seating 2-class 120-150 |
capacity |
Pilot and observer |
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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.