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Year
1986

Description

Aircraft Information General Performance & Specifications Description Aircraft Information Year: 1986 – 1989 Make: Beechjet Model: 400 Active Fleet: 54 – For Sale/Lease: 18 Average Asking Price – February 2014: $651,000 Range: 1,140 – 1,580 nm Contact Number: 1-847-726-5000 General Performance & Specifications Cabin Height: 4.8 Feet Cabin Width: 4.9 Feet Cabin Length: 14.4 Feet Baggage Volume Internal: 12.0 Cubic Feet Baggage Volume External: 33.0 Cubic Feet Seats Executive: 2/7 Max. Take-Off Weight: 15,780 lbs. Max. Landing Weight: 14,220 lbs. Maximum Payload: 2,070 lbs. Balance Field Length: 4,700 Feet Landing Distance: 4,450 Feet Rate of Climb – All Engines: 3,960 Feet / Minute Rate of Climb – One Engine Out: 1,110 Feet / Minute Normal Cruise Speed: 446 ktas Max. Cruise Speed: 461 ktas Service Ceiling Max. Weight: 40,750 Feet Number of Engines: 2 Engine Manufacturer: Pratt & Whitney Engine Model: JT15D-5 Description The Raytheon Beech 400/400A evolved from the Mitsubishi Diamond 2 design that was bought by Beech in the mid 1980s. The original Mitsubishi MU300 Diamond 1 flew for the first time in August 1978. Only 11 Diamond 2s were built before Beech purchased the design and production rights. The Diamond 2 was renamed the Beech 400. Beech equipped the Diamond 2 with JT15D5 turbofan engines, developed a new interior, and made other minor changes. The new Beech 400A has a higher max takeoff weight and greater operating ceiling along with improved performance. Moving the rear fuselage fuel tank increased cabin volume. The flight deck features Collins Pro Line 4 EFIS avionics suite. Raytheon introduced a new luxury standard interior for the Beech 400A in 1996.

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