Airbus A220-100 vs. Bell 206
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Airbus A220-100 |
versus |
Bell 206 |
35.0 m |
114 ft 10 in |
length |
12.11 m |
39 ft 9 in |
11.5 m |
37 ft 9 in |
height |
2.88 m |
9 ft 5 in |
35.1 m |
115 ft 2 in |
wingspan |
|
|
2 Turbofans (wing mounted) |
engines |
1 × Allison 250-C20B |
21,000–23,000 lb |
thrust per engine |
420 shp (313 kW) |
42,000–46,000 lb |
total thrust |
420 shp (313 kW) |
63,100 kg |
139,100 lb |
MTOW |
1,451 kg |
3,199 lb |
6,390 km |
3,451 nm |
range |
374 km |
202 nm |
871 km/h |
541 mph |
cruise speed |
222 km/h |
138 mph |
Typical seating 2-class 100-120 |
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.