Airbus A321-200 vs. Bombardier CRJ1000
... or view the full comparison list
here.
Airbus A321-200 |
versus |
Bombardier CRJ1000 |
44.51 m |
146 ft 0 in |
length |
39.1 m |
128 ft 5 in |
11.76 m |
38 ft 7 in |
height |
7.5 m |
24 ft 7 in |
35.8 m |
117 ft 5 in |
wingspan |
26.2 m |
86 ft |
2 GE CFM56-5B3 |
engines |
2 GE CF34-8C5A1 turbofans |
31,600 lbs |
thrust per engine |
13,630 lb of force or 60.6 kN at takeoff, 14,510 lb of force or 64.5 kN thrust APR Automatic Power Reserve |
63,200 lbs |
total thrust |
27,260 lb of force or 121.2 kN at takeoff, 29,020 lb of force or 129 kN thrust APR Automatic Power Reserve |
89,000 kg |
196,200 lb |
MTOW |
41,640 kg |
91,800 lb |
4,000 nmi |
7,408 km |
range |
3,004 km |
1,623 nm |
871 km/h |
541 mph |
cruise speed |
515 mph |
829 km/h |
185 to 220 |
capacity |
100 (common) |
|
|
rotor diameter |
|
|
|
|
rate of climb |
|
|
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.