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The Hawker 400 is a small, low-winged twin-turbofan aircraft of all metal construction, flown by a crew of two pilots and accommodating eight passengers in a pressurised cabin. Its wings use a computer-designed supercritical airfoil in order to minimise drag. Its two Pratt & Whitney Canada JT15D turbofans are mounted on the rear fuselage.
The 400 can fly 1,351 nmi (2,502 km) with four passengers, cruising at Mach 0.71–0.73, and most pilots are comfortable flying it over three hours, about 1,175 nmi (2,176 km) cruising at Mach 0.73–0.76. Typical missions are 1.5 to 2.0 hours with 400 kn (740 km/h) block speeds. It burns 1,500 lb (680 kg) of fuel the first hour, dropping to 1,100–1,200 lb (500–540 kg) for the second. Basic operating weights range from 11,000 to 11,100 lb (4,990 to 5,030 kg), full tanks payload is less than 500–600 lb (230–270 kg) with an average passenger load of three, however its full capacity is six passengers 1,100 nmi (2,000 km)
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Light corporate jet. In Service since 1986. Beechcraft/Raytheon bought the MITSUBISHI MU-300 Diamond design and has developed it into the BEECH 400. Also built as military T-1A JAYHAWK trainer. The original BEECH 400 and 400A is now marketed by RAYTHEON, USA
The Hawker 400XPR modification, featuring new avionics, interior and winglets, is availabke since 2014
Remanufactured variants were built by Nextant Aerospace since 2010. The P&W JT15D-5 engines replaced with Williams FJ44-3AP ones and the aircraft EFIS and TAWS were upgraded.