Airbus A321LR vs. North American Rockwell OV-10 Bronco
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| Airbus A321LR |
versus |
North American Rockwell OV-10 Bronco |
| 44.51 m |
146 ft 0 in |
length |
12.7 m |
41 ft 7 in |
| 11.76 m |
38 ft 7 in |
height |
4.62 m |
15 ft 2 in |
| 35.8 m |
117 ft 5 in |
wingspan |
12.19 m |
40 ft |
| CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
2 x Garrett T76-G-420/421 turboprop engines |
| Over 33,000 lbs (147 kN) |
thrust per engine |
Approximately 715 hp each |
| 66,000 lbs (294 kN) |
total thrust |
Approximately 1,430 hp total |
| 97,000 kg |
213,800 lb |
MTOW |
14,444 lb |
6,553 kg |
| 7,400 km |
4,000 nm |
range |
1,931 km |
1,043 nm |
| 832 km/h |
517 mph |
cruise speed |
244 mph |
393 km/h |
| 180-220 passengers |
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.
