Airbus A320-200 vs. Beechcraft T-34 Mentor
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Airbus A320-200 |
versus |
Beechcraft T-34 Mentor |
38.7 m |
127 ft 0 in |
length |
7.92 m |
25 ft 11 in |
17.4 m |
57 ft 1 in |
height |
2.95 m |
9 ft 8 in |
35.8 m |
117 ft 5 in |
wingspan |
10.03 m |
32 ft 11 in |
Choice between Pratt & Whitney GTFâ„¢ and the LEAP-1A from CFM International |
engines |
1 x Continental Motors IO-520 engine |
Between 21,000 - 33,000 lbf |
thrust per engine |
Approximately 300 hp |
Between 42,000 - 66,000 lbf |
total thrust |
Approximately 300 hp |
77,000 kg |
169,800 lb |
MTOW |
3,100 lb |
1,406 kg |
5,700 km |
3,078 nm |
range |
1,111 km |
600 nm |
530 mph |
853 km/h |
cruise speed |
190 mph |
306 km/h |
Typically between 140-180 passengers |
capacity |
Pilot and one passenger |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.