Airbus A321LR vs. Beechcraft T-6 Texan II

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Airbus A321LR versus Beechcraft T-6 Texan II
44.51 m 146 ft 0 in length 10.18 m 33 ft 4 in
11.76 m 38 ft 7 in height 3.29 m 10 ft 10 in
35.8 m 117 ft 5 in wingspan 10.21 m 33 ft 6 in
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 1 x Pratt & Whitney Canada PT6A-68
Over 33,000 lbs (147 kN) thrust per engine 1100 lbs
66,000 lbs (294 kN) total thrust 1100 lbs
97,000 kg 213,800 lb MTOW 6,250 lb 2,835 kg
7,400 km 4,000 nm range 900 nm 1,667 km
832 km/h 517 mph cruise speed 320 kts 199 mph
180-220 passengers capacity 2
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.