Airbus A321XLR vs. Beechcraft T-6 Texan II

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Airbus A321XLR 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 LEAP-1A and P&W PW1100G engines 1 x Pratt & Whitney Canada PT6A-68
33,000 lbs (147 kN) thrust per engine 1100 lbs
66,000 lbs (294 kN) total thrust 1100 lbs
101,000 kg 222,700 lb MTOW 6,250 lb 2,835 kg
4,700 nmi 8,704 km range 900 nm 1,667 km
963km/h 598mph cruise speed 320 kts 199 mph
180-220 seats (typical 2-class seating) 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.