McDonnell-Douglas MD-11 vs. North American T-6 Texan

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McDonnell-Douglas MD-11 versus North American T-6 Texan
61.20 m 200 ft 10 in length 9.0 m 29 ft 6 in
17.6 m 57 ft 9 in height 3.56 m 11 ft 8 in
51.6 m 169 ft 4 in wingspan 12.8 m 42 ft
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines 1 x Pratt & Whitney R-1340-AN-1 radial engine
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine Approximately 600 hp
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust Approximately 600 hp
285,990 kg 630,400 lb MTOW 5,617 lb 2,548 kg
13,231 km 7,147 nm range 1,175 km 634 nm
961 km/h 597 mph cruise speed 145 mph 233 km/h
Max 410 passengers 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.