Airbus A220-100 vs. North American Rockwell OV-10 Bronco
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Airbus A220-100 |
versus |
North American Rockwell OV-10 Bronco |
35.0 m |
114 ft 10 in |
length |
12.7 m |
41 ft 7 in |
11.5 m |
37 ft 9 in |
height |
4.62 m |
15 ft 2 in |
35.1 m |
115 ft 2 in |
wingspan |
12.19 m |
40 ft |
2 Turbofans (wing mounted) |
engines |
2 x Garrett T76-G-420/421 turboprop engines |
21,000–23,000 lb |
thrust per engine |
Approximately 715 hp each |
42,000–46,000 lb |
total thrust |
Approximately 1,430 hp total |
63,100 kg |
139,100 lb |
MTOW |
14,444 lb |
6,553 kg |
6,390 km |
3,451 nm |
range |
1,931 km |
1,043 nm |
871 km/h |
541 mph |
cruise speed |
244 mph |
393 km/h |
Typical seating 2-class 100-120 |
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.