North American T-6 Texan vs. Airbus A380-800F
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North American T-6 Texan |
versus |
Airbus A380-800F |
9.0 m |
29 ft 6 in |
length |
72.73 m |
238 ft 7 in |
3.56 m |
11 ft 8 in |
height |
24.09 m |
79 ft |
12.8 m |
42 ft |
wingspan |
79.75 m |
261 ft 8 in |
1 x Pratt & Whitney R-1340-AN-1 radial engine |
engines |
4 x Engine Alliance GP7200 turbofan engines |
Approximately 600 hp |
thrust per engine |
70,000 to 80,000 pounds of thrust (311 to 356 kilonewtons) |
Approximately 600 hp |
total thrust |
280,000 to 320,000 pounds |
5,617 lb |
2,548 kg |
MTOW |
590,000 kg |
1,300,733 lb |
1,175 km |
634 nm |
range |
14,800 km |
7,992 nm |
145 mph |
233 km/h |
cruise speed |
903 km/h |
561 mph |
Pilot and one passenger |
capacity |
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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.