Airbus A310-300 vs. Piper PA-34 Seneca
... or view the full comparison list
here.
Airbus A310-300 |
versus |
Piper PA-34 Seneca |
46.66 m |
153 ft 1 in |
length |
8.71 m |
28 ft 7 in |
15.8 m |
51 ft 10 in |
height |
2.99 m |
9 ft 10 in |
43.9 m |
144 ft |
wingspan |
11.64 m |
38 ft 2 in |
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan |
engines |
2 x Continental IO-360 |
52,000 lb |
thrust per engine |
220 lbs |
104,000 lb |
total thrust |
440 lbs |
148,768 kg |
328,000 lb |
MTOW |
4,750 lb |
2,155 kg |
8,050 km |
4,348 nm |
range |
980 nm |
1,815 km |
482 knots |
279 mph |
cruise speed |
165 kts |
103 mph |
190-230 passengers |
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.