Mitsubishi Marquise/Solitaire

Turboprop • twin engine • High Wing • Retractable gear

Range Visualization

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Payload vs. Range

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Default: 190 lbs (FAA standard)

Default: 30 lbs

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lbs @ lbs / pax
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Fuel on board
gal
+ Weight
Range
Available Range / nm
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Mission Profile

Endorsements & ratings:
  • High-Performance
  • Complex
  • High-Altitude
  • Pressurization
  • Multi-Engine
  • Instrument
295
KTAS
Cruise Speed
11
Occupants
1395
nm
Max Range
1466
lbs
Wet Payload

Estimated Ownership Costs

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About the Mitsubishi Marquise/Solitaire

Overview

The Mitsubishi MU-2B-60 Marquise is a pressurized, high-wing twin turboprop – the long-fuselage, top-of-line development of Mitsubishi’s MU-2, built into the mid-1980s on Garrett (now Honeywell) TPE331-10 engines. It is best known for going faster on less fuel than anything in its class: roughly 295 KTAS in cruise on about 74 GPH total, a speed-per-gallon the larger King Airs of its day could not match. The short-fuselage MU-2B-40 Solitaire shares this catalogue entry – it carries the same engines and systems in an airframe about six feet shorter, with a few seats fewer.

For the GA buyer, the Marquise is one of the fastest and most fuel-efficient pressurized cabin twins on the used market, and used prices run below a comparable King Air. The trade is a demanding airplane the FAA singles out for type-specific training: the MU-2 rewards a disciplined, current pilot and is unforgiving of a casual one.

Key Features for GA Buyers

  • Speed on little fuel. A 295-KTAS typical cruise – over 300 KTAS at higher power – on roughly 74 GPH total for both engines is the MU-2’s defining trait.
  • Twin Garrett TPE331-10. Two TPE331-10-501M turboprops, flat-rated to 715 shp each, on four-blade constant-speed propellers; the high-output Garrett core of the late MU-2 line.
  • Pressurized to the high 20s. A 6.1-psi cabin supports cruise to a 29,750-foot ceiling with a comfortable cabin altitude.
  • Strong load and climb. A useful load near 3,900 lb and a two-engine climb around 2,200 fpm at the 11,575-lb gross.

Trade-offs

  • Mandatory MU-2 type training (SFAR 108 / 14 CFR Part 91 Subpart N). The FAA requires type-specific initial and recurrent training, currency, and operating rules for every MU-2 pilot, a rule born of the type’s early accident record. Budget recurring training as a fixed cost of ownership, not an option.
  • Demanding handling. The MU-2 rolls with spoilers rather than ailerons, uses full-span flaps, carries a high wing loading, and is unforgiving of sloppy speed control on approach and in single-engine work.
  • 1980s airframes and Garrett discipline. The newest Marquises are mid-1980s; buyers inherit aging systems and the TPE331’s exacting hot-section and operating management, where an inexperienced operator runs up large bills.
  • Two turbines to feed. Even at the MU-2’s frugal flows, two turboprops carry the fuel, reserve, and overhaul costs of a twin.

See Also

Technical Specifications

Dimensions

Wingspan
39.2 ft
Length
39.4 ft
Height
13.7 ft
Parking area (ft2)
2184.48 ft2

Weights

Max Takeoff Weight
11,575 lbs
Max Landing Weight
11,025 lbs
Useful Load
3,925 lbs
Fuel Capacity
367 gal

Performance

Cruise Speed
295 KTAS
Never-Exceed (Vne)
250 KIAS
Max Structural Cruise (Vno)
250 KIAS
Approach Speed
105 KIAS
Stall, Clean (Vs1)
81 KIAS
Range
1395 NM
Service Ceiling
29,750 ft
Rate of Climb
2200 fpm

Engines

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