Airbus A220-100 vs. Bell 412
... or view the full comparison list
here.
Airbus A220-100 |
versus |
Bell 412 |
35.0 m |
114 ft 10 in |
length |
17,10 m |
56 ft 1 in |
11.5 m |
37 ft 9 in |
height |
3,48 m |
11 ft 5 in |
35.1 m |
115 ft 2 in |
wingspan |
|
|
2 Turbofans (wing mounted) |
engines |
2 x Pratt & Whitney Canada PT6T-3D turboshaft engines |
21,000–23,000 lb |
thrust per engine |
1,800 hp |
42,000–46,000 lb |
total thrust |
3,600 hp |
63,100 kg |
139,100 lb |
MTOW |
5,400 kg |
11,905 lb |
6,390 km |
3,451 nm |
range |
659 km |
356 nm |
871 km/h |
541 mph |
cruise speed |
259 km/h |
161 mph |
Typical seating 2-class 100-120 |
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.