Airbus A300-600 vs. Beechcraft T-34 Mentor
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Airbus A300-600 |
versus |
Beechcraft T-34 Mentor |
54.10 m |
177 ft 6 in |
length |
7.92 m |
25 ft 11 in |
16.5 m |
54 ft 2 in |
height |
2.95 m |
9 ft 8 in |
44.84 m |
147 ft 1 in |
wingspan |
10.03 m |
32 ft 11 in |
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 |
engines |
1 x Continental Motors IO-520 engine |
56,000lb to 61,500lb |
thrust per engine |
Approximately 300 hp |
112,000–123,000 lb |
total thrust |
Approximately 300 hp |
171,700 kg |
378,600 lb |
MTOW |
3,100 lb |
1,406 kg |
7,500 km |
4,052 nm |
range |
1,111 km |
600 nm |
897 km/h |
557 mph |
cruise speed |
190 mph |
306 km/h |
210-250 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.