Airbus A321LR vs. Cessna O-2 Skymaster
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Airbus A321LR |
versus |
Cessna O-2 Skymaster |
44.51 m |
146 ft 0 in |
length |
8.9 m |
29 ft 2 in |
11.76 m |
38 ft 7 in |
height |
2.87 m |
9 ft 5 in |
35.8 m |
117 ft 5 in |
wingspan |
11.58 m |
38 ft |
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
Two 210-hp Continental IO-360s |
Over 33,000 lbs (147 kN) |
thrust per engine |
210 hp |
66,000 lbs (294 kN) |
total thrust |
420 hp |
97,000 kg |
213,800 lb |
MTOW |
5,400 lb |
2,449 kg |
7,400 km |
4,000 nm |
range |
1,705 km |
921 nm |
832 km/h |
517 mph |
cruise speed |
144 mph |
232 km/h |
180-220 passengers |
capacity |
2 |
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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.