Airbus A321XLR vs. Beechcraft T-34 Mentor

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Airbus A321XLR versus Beechcraft T-34 Mentor
44.51 m 146 ft 0 in length 7.92 m 25 ft 11 in
11.76 m 38 ft 7 in height 2.95 m 9 ft 8 in
35.8 m 117 ft 5 in wingspan 10.03 m 32 ft 11 in
CFM LEAP-1A and P&W PW1100G engines 1 x Continental Motors IO-520 engine
33,000 lbs (147 kN) thrust per engine Approximately 300 hp
66,000 lbs (294 kN) total thrust Approximately 300 hp
101,000 kg 222,700 lb MTOW 3,100 lb 1,406 kg
4,700 nmi 8,704 km range 1,111 km 600 nm
963km/h 598mph cruise speed 190 mph 306 km/h
180-220 seats (typical 2-class seating) 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.