Airbus A310-300 vs. Max Holste M.H.1521 Broussard

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Airbus A310-300 versus Max Holste M.H.1521 Broussard
46.66 m 153 ft 1 in length 10.46 m 34 ft 4 in
15.8 m 51 ft 10 in height 2.74 m 9 ft
43.9 m 144 ft wingspan 12.86 m 42 ft 2 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 x Lycoming GSO-480-B1A6 flat-six engine
52,000 lb thrust per engine Approximately 295 hp
104,000 lb total thrust Approximately 295 hp
148,768 kg 328,000 lb MTOW 1,900 kg 4,189 lb
8,050 km 4,348 nm range 1,030 km 556 nm
482 knots 279 mph cruise speed 145 mph 233 km/h
190-230 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.