Airbus A321LR vs. Bell 412
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Airbus A321LR |
versus |
Bell 412 |
44.51 m |
146 ft 0 in |
length |
17,10 m |
56 ft 1 in |
11.76 m |
38 ft 7 in |
height |
3,48 m |
11 ft 5 in |
35.8 m |
117 ft 5 in |
wingspan |
|
|
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
2 x Pratt & Whitney Canada PT6T-3D turboshaft engines |
Over 33,000 lbs (147 kN) |
thrust per engine |
1,800 hp |
66,000 lbs (294 kN) |
total thrust |
3,600 hp |
97,000 kg |
213,800 lb |
MTOW |
5,400 kg |
11,905 lb |
7,400 km |
4,000 nm |
range |
659 km |
356 nm |
832 km/h |
517 mph |
cruise speed |
259 km/h |
161 mph |
180-220 passengers |
capacity |
13 |
|
|
rotor diameter |
14.0 m |
45 ft 11 in |
|
|
rate of climb |
9.5 m/s |
1,870 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.