Airbus A321LR vs. Max Holste M.H.1521 Broussard

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Airbus A321LR versus Max Holste M.H.1521 Broussard
44.51 m 146 ft 0 in length 10.46 m 34 ft 4 in
11.76 m 38 ft 7 in height 2.74 m 9 ft
35.8 m 117 ft 5 in wingspan 12.86 m 42 ft 2 in
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 1 x Lycoming GSO-480-B1A6 flat-six engine
Over 33,000 lbs (147 kN) thrust per engine Approximately 295 hp
66,000 lbs (294 kN) total thrust Approximately 295 hp
97,000 kg 213,800 lb MTOW 1,900 kg 4,189 lb
7,400 km 4,000 nm range 1,030 km 556 nm
832 km/h 517 mph cruise speed 145 mph 233 km/h
180-220 passengers capacity 5-7 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.