Airbus A321-200 vs. Bell 206
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Airbus A321-200 |
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 |
|
|
2 GE CFM56-5B3 |
engines |
1 × Allison 250-C20B |
31,600 lbs |
thrust per engine |
420 shp (313 kW) |
63,200 lbs |
total thrust |
420 shp (313 kW) |
89,000 kg |
196,200 lb |
MTOW |
1,451 kg |
3,199 lb |
4,000 nmi |
7,408 km |
range |
374 km |
202 nm |
871 km/h |
541 mph |
cruise speed |
222 km/h |
138 mph |
185 to 220 |
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.