Airbus A340-200 vs. North American T-6 Texan

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Airbus A340-200 versus North American T-6 Texan
59.4 m 194 ft 11 in length 9.0 m 29 ft 6 in
16.8 m 55 ft 1 in height 3.56 m 11 ft 8 in
60.3 m 197 ft 9 in wingspan 12.8 m 42 ft
4 x CFM International CFM56-5C4 engines 1 x Pratt & Whitney R-1340-AN-1 radial engine
34,000 lbf thrust per engine Approximately 600 hp
136,000 lbf total thrust Approximately 600 hp
275,000 kg 606,300 lb MTOW 5,617 lb 2,548 kg
12,400 km 6,699 nm range 1,175 km 634 nm
880 km/h 547 mph cruise speed 145 mph 233 km/h
Typical seating 3-class 210-250 capacity Pilot and one passenger
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.