Airbus A380-800F vs. Beechcraft T-6 Texan II
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Airbus A380-800F |
versus |
Beechcraft T-6 Texan II |
72.73 m |
238 ft 7 in |
length |
10.18 m |
33 ft 4 in |
24.09 m |
79 ft |
height |
3.29 m |
10 ft 10 in |
79.75 m |
261 ft 8 in |
wingspan |
10.21 m |
33 ft 6 in |
4 x Engine Alliance GP7200 turbofan engines |
engines |
1 x Pratt & Whitney Canada PT6A-68 |
70,000 to 80,000 pounds of thrust (311 to 356 kilonewtons) |
thrust per engine |
1100 lbs |
280,000 to 320,000 pounds |
total thrust |
1100 lbs |
590,000 kg |
1,300,733 lb |
MTOW |
6,250 lb |
2,835 kg |
14,800 km |
7,992 nm |
range |
900 nm |
1,667 km |
903 km/h |
561 mph |
cruise speed |
320 kts |
199 mph |
|
capacity |
2 |
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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.