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Hawker 400A

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Date Taken:
25th October 2019
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Aircraft Data

The Beechcraft 400 is a twin engined short to medium range light business jet. It was derived from the Mitsubishi Mu300 Diamond, rights to which were bought by Beechcraft in the 1980s.

the 400A was the first major version, a higher max takeoff weight and greater operating ceiling improved performance, while repositioning the rear fuselage fuel tank increased cabin volume. 180 were built for the USAF as trainers.

Summary data for Hawker Beechcraft Hawker 400 400A
Country of originFirst flightNo. builtNo. in serviceCrewPassengers
USA199017217026 - 7


2 x Pratt & Whitney Canada JT15D (2500 - 2965 lbf) turbofan engines.

Uses the JT15D with a thrust of 2500lb.


Dimensions for Hawker Beechcraft Hawker 400 400A
Length48 ft. 5 in.
Wing Span43 ft. 6 in.
Height13 ft. 6 in.
Empty Weight10,626 lbs.
Max Weight16,100 lbs.


Performance of Hawker Beechcraft Hawker 400 400A
Max Speed468 kts
Cruise Speed392 kts
Ceiling43,400 ft.
Normal Range1,574nm
Max Range1,690nm

Updated 22nd November 2008

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