Aircraft Information
| Years Manufactured: | 1982-1985 |
| Manufacturer: | Mitsubishi |
| Model: | Diamond IA |
| Active Fleet: | 73 |
| Average Ask Price - August 2010: | $858,200 |
| Range: | 1,140 1,200 nm |
| Contact Number: | 1-847-726-5000 |
| Current Market Price / Availability: | Request Market Update Report |
Description
In 1977 Mitsubishi embarked on the design of a new business jet known as the MU-300. This aircraft, subsequently called the “Diamond”, was a conventional low wing design with a T-tail and two P&W JT15D turbofans mounted on the rear fuselage. For a small jet, it had a large cabin for eight passengers, an aft lavatory and baggage. Initial testing was done in Japan and then the two prototypes were transferred to Mitsubishi’s facility in San Angelo, TX to complete its FAA testing for FAR Part 25. It received its Type Certificate on 6 November 1981. Thereafter, production Diamond Is were assembled in San Angelo from components produced in Nagoya, Japan. By late 1985 Mitsubishi had delivered 100 Diamonds from its San Angelo facility. At that time Mitsubishi sold the MU-300 package to Beechcraft where it became known as the Beechjet 400.
General Performance & Specifications
| Cabin Height: | 4.80 ft. |
| Cabin Width: | 4.90 ft. |
| Cabin Length: | 15.60 ft. |
| Baggage Volume Internal: | 20.0 cu.ft. |
| Baggage Volume External: | 33.0 cu.ft. |
| Seats Executive: | 2/7 |
| Max. Take-off Weight: | 14,630 lbs. |
| Max. Landing Weight: | 13,200 lbs. |
| Maximum Payload: | 1,720 lbs. |
| Balance Field Length: | 5,050 ft. |
| Landing Distance: | 4,600 ft. |
| ate of Climb - All Engines: | 3,050 ft./min. |
| Rate of Climb - One Engine Out: | 761 ft./min. |
| Normal Cruise Speed: | 406 ktas |
| Max. Cruise Speed: | 406 ktas |
| Service Ceiling Max. Weight: | 41,000 ft. |
| Number of Engines: | 2 |
| Engine Model: | JT15D-4D |
| Engine Manufacturer: | Pratt & Whitney |