Airbus A321LR vs. North American BT-9
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Airbus A321LR |
versus |
North American BT-9 |
44.51 m |
146 ft 0 in |
length |
8.79 m |
28 ft 10 in |
11.76 m |
38 ft 7 in |
height |
2.82 m |
9 ft 3 in |
35.8 m |
117 ft 5 in |
wingspan |
10.97 m |
36 ft |
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
1 x Wright R-975-3 radial engine |
Over 33,000 lbs (147 kN) |
thrust per engine |
Approximately 440 hp |
66,000 lbs (294 kN) |
total thrust |
Approximately 440 hp |
97,000 kg |
213,800 lb |
MTOW |
4,300 lb |
1,950 kg |
7,400 km |
4,000 nm |
range |
917 km |
495 nm |
832 km/h |
517 mph |
cruise speed |
150 mph |
241 km/h |
180-220 passengers |
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.