Airbus A321LR vs. Bell 206
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Airbus A321LR |
versus |
Bell 206 |
44.51 m |
146 ft 0 in |
length |
12.11 m |
39 ft 9 in |
11.76 m |
38 ft 7 in |
height |
2.88 m |
9 ft 5 in |
35.8 m |
117 ft 5 in |
wingspan |
|
|
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
1 × Allison 250-C20B |
Over 33,000 lbs (147 kN) |
thrust per engine |
420 shp (313 kW) |
66,000 lbs (294 kN) |
total thrust |
420 shp (313 kW) |
97,000 kg |
213,800 lb |
MTOW |
1,451 kg |
3,199 lb |
7,400 km |
4,000 nm |
range |
374 km |
202 nm |
832 km/h |
517 mph |
cruise speed |
222 km/h |
138 mph |
180-220 passengers |
capacity |
1 pilot + 4 passengers |
|
|
rotor diameter |
11.00 m |
36 ft 1 in |
|
|
rate of climb |
425 m/min |
1,395 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.