Mitsubishi
MU-300
Diamond

Photo: Robert Deering 5/6/2022
North Texas Regional Airport (GYI)
Denison, Texas

The Mitsubishi MU-300 Diamond was an all-new, all-jet development to complement and slot above the Mitsubishi MU-2 and provide Mitsubishi Heavy Industries with their top-of-the-line corporate aircraft model (hence the name "Diamond"). It first flew on August 29, 1978. 

Mitsubishi chose to certificate the Diamond in the United States under FAA Part 25 regulations for transport aircraft, but additional requirements introduced by the FAA resulted in significant delays in the certification process.  With required changes to the aircraft that added 600 lb (270 kg), the aircraft did not receive its certification until November 6, 1981. Mitsubishi went on to produce 97 MU-300s, all of which were assembled by the company's United States subsidiary.

In 1985, Mitsubishi sold the rights and a number of unfinished airframes to Beechcraft, who began manufacturing it as their own model, initially re-designated as the Beechjet 400, certificated by the Federal Aviation Administration in May 1986.

Raytheon/Beechcraft developed improvements for the 1990 400A for longer range, higher take-off weights, luxury appointments and offering an all-glass flight deck.

Beechcraft developed the T-1 Jayhawk version for the United States Air Force, used as a trainer for crew of large aircraft like tankers and strategic transports: 180 were delivered between 1992 and 1997. The Japan Air Self-Defense Force 400T trainer shares the T1-A Type certificate.

In 1993, Raytheon purchased the Hawker business jets from British Aerospace and renamed the Beechjet 400 as the Hawker 400 to include it in the line.

In 2003, Raytheon began to produce Hawker 400XP, which included: 200 lb (91 kg) gross weight increase, a nine-passenger seating option, thrust reversers, TCAS II, and an emergency locator beacon.

In 2008, Hawker Beechcraft announced an improved Hawker 450XP including new, more fuel-efficient Pratt & Whitney PW535Ds with 2,965 pounds of thrust each, but it was canceled in June 2009 due to poor economic conditions.

Nextant Aerospace re-manufactured Hawker 400XP as the Nextant 400XT, replacing the JT15Ds with Williams FJ44-3APs and adding new avionics and interior. It was FAA-certified in October 2011. Up to one-third of the 400A/400XP fleet could be retrofitted, enabling improved range, speed and fuel efficiency. It should keep their resale value to remain in economic service for another twenty to thirty years, like Falcon 20s reengined with TFE731s.

In 2012, Textron has first flown Hawker 400XPR, which improves 4-pax range to 1,950 nmi (3,610 km; 2,240 mi), has better hot and high performance, and can climb to FL450 at max takeoff weight in 19 min. The conversion features new avionics, interior, winglets, and Williams FJ44-4A-32 engines. Hawker 400XPR was certified in 2016, and first fully configured Hawker 400XPR was delivered in July 2017; the upgrade can be performed in 12 weeks with a choice of Rockwell Collins Pro Line 4 to 21 or Garmin G5000 avionics.

VARIANTS

Mitsubishi MU-300 Diamond I

Initial model, 
ICAO designator MU30. Two prototypes and 89 production aircraft built, 56 in active use as of 2014.

Mitsubishi MU-300-10 Diamond II
Improved version of Diamond I; 11 built, all subsequently redesignated as 
Beechjet 400s.

Beechcraft Model 400 Beechjet

The Diamond II built after Beechcraft bought the MU-300 production rights from Mitsubishi. 54 built in addition to the original 11 Diamond IIs. 
ICAO designator BE40.

Model 400A

Upgraded model, initially produced as the Beechcraft Beechjet 400A, then Raytheon Beechjet 400A, then Raytheon Hawker 400XP, then Hawker Beechcraft Hawker 400XP. One prototype converted from Model 400 and 593 built as of the end of 2009. 
ICAO designator BE40.

Model 400T

Military version of the Model 400A, 180 built for the United States Air Force as the T-1 Jayhawk and 13 built for the Japan Air Self-Defense Force. In Japanese service they are referred to as T-400. ICAO designator BE40.


Hawker 400XPR

A factory engineered and supported upgrade of Hawker 400XP, first flown May 2012, and certified in 2016. The conversion features new avionics, interior, winglets, and Williams FJ44-4A-32 engines. The upgrade can be performed in 12 weeks with a choice of Rockwell Collins Pro Line 4 to 21 or Garmin G5000 avionics. Hawker 400XPR increases ferry range to 2160nmi, provides better hot and high performance, and 16-20% decrease in specific fuel consumption. 400XPR has ICAO designator BE4W, which is shared with Nextant 400XT, a competing upgrade of Hawker 400 made by Nextant Aerospace.
SPECIFICATIONS: PERFORMANCE:
Span: 44 ft 6 in (13.26 m)
Length: 48 ft 5 in (14.75 m)
Height:  14 ft 9 in (4.19 m)
Empty Weight:  9,099 lb (4,127 kg)

Gross Weight: 14,630 lb (6,636 kg)
Crew: 2 pilots
Maximum speed:
Cruising speed: 460 mph (741 km/h)
Range:
1,740 miles (2,800 km)
Service ceiling:
41,000 ft (12,495 m)
Engines: 2 x Pratt & Whitney Aircraft of Canada JT15D-4 turbofans, 1,485 kg
   
SOURCE:  Wikipedia