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Mitsubishi MU-300 Diamond IA, exterior
Light JetOut of production

Mitsubishi Heavy Industries

01 · Basic info

Mitsubishi MU-300 Diamond IA

Improved version of the Mitsubishi MU-300 Diamond I, announced in 1983 with uprated Pratt & Whitney Canada JT15D-4D turbofans, an EFIS cockpit, a higher maximum takeoff weight and an additional port-side cabin window. The first Diamond IA was delivered in January 1984, and the aircraft were assembled in San Angelo, Texas.

Manufacturer
Mitsubishi Heavy Industries
Class
Light Jet
Production
Out of production
First delivery
1984
Engines
2 × Pratt & Whitney Canada JT15D-4D
Mitsubishi MU-300 Diamond IA, exterior

Photo: Greg Goebel · Wikimedia Commons · CC BY-SA 2.0

02 · Specifications

Technical data

Capacity

Flight crew
2

External dimensions

Length
48.42 ft
Height
13.75 ft
Wingspan
43.5 ft

Powerplant

Engines
2 × Pratt & Whitney Canada JT15D-4D

Weights

Max take-off weight
16,230 lb

Manufacturer-published or publicly documented type data, for orientation only. Figures vary with configuration, serial number, modifications and operating conditions. Not for flight planning. Values not publicly documented are omitted.

03 · Cabin layout

Cabin plan & cross-section

Cross-section data not published

Cabin width

–

Cabin height

–

Cabin length 21.79 ft
Passenger cabinGalley / lavatoryBaggageEntrySchematic · indicative layout · not to scale
  • Club seating
  • Seating
  • Lavatory
  • Baggage

04 · Range map

Where the MU-300 Diamond IA can fly nonstop

Range data has not been published for this model.

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