Airbus A321-200 vs. Piper PA-34 Seneca
... or view the full comparison list
here.
Airbus A321-200 |
versus |
Piper PA-34 Seneca |
44.51 m |
146 ft 0 in |
length |
8.71 m |
28 ft 7 in |
11.76 m |
38 ft 7 in |
height |
2.99 m |
9 ft 10 in |
35.8 m |
117 ft 5 in |
wingspan |
11.64 m |
38 ft 2 in |
2 GE CFM56-5B3 |
engines |
2 x Continental IO-360 |
31,600 lbs |
thrust per engine |
220 lbs |
63,200 lbs |
total thrust |
440 lbs |
89,000 kg |
196,200 lb |
MTOW |
4,750 lb |
2,155 kg |
4,000 nmi |
7,408 km |
range |
980 nm |
1,815 km |
871 km/h |
541 mph |
cruise speed |
165 kts |
103 mph |
185 to 220 |
capacity |
5 |
|
|
rotor diameter |
|
|
|
|
rate of climb |
|
|
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.