Airbus A321-200 vs. North American T-6 Texan
... or view the full comparison list
here.
Airbus A321-200 |
versus |
North American T-6 Texan |
44.51 m |
146 ft 0 in |
length |
9.0 m |
29 ft 6 in |
11.76 m |
38 ft 7 in |
height |
3.56 m |
11 ft 8 in |
35.8 m |
117 ft 5 in |
wingspan |
12.8 m |
42 ft |
2 GE CFM56-5B3 |
engines |
1 x Pratt & Whitney R-1340-AN-1 radial engine |
31,600 lbs |
thrust per engine |
Approximately 600 hp |
63,200 lbs |
total thrust |
Approximately 600 hp |
89,000 kg |
196,200 lb |
MTOW |
5,617 lb |
2,548 kg |
4,000 nmi |
7,408 km |
range |
1,175 km |
634 nm |
871 km/h |
541 mph |
cruise speed |
145 mph |
233 km/h |
185 to 220 |
capacity |
Pilot and one passenger |
|
|
rotor diameter |
|
|
|
|
rate of climb |
|
|
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.