Cookie Consent by TermsFeed 1979 - 1985 MITSUBISHI MU-2B-40 - Specifications, Performance, Operating cost, Valuation, Brokers - planephd.com

1979 - 1985 MITSUBISHI MU-2B-40

Twin engine turboprop aircraft with retractable landing gear. The MU-2B-40 seats up to 8 passengers plus 1 pilot.


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Performance specifications


Horsepower:

2 x 665 HP

Best Cruise Speed:

313 KIAS

Best Range (i):

1,600 NM

Fuel Burn:

78.4 GPH

Stall Speed:

73 KIAS

Rate of climb:

2,300 FPM

Rate of climb (1 engine out):

475 FPM

Ceiling:

33,500 FT

Ceiling (1 engine out):

16,900 FT

Landing distance:

1,950 FT

Takeoff distance over 50ft obstacle:

1,800 FT


Weights


Gross Weight:

10,470 LBS

Empty Weight:

7,210 LBS

Maximum Payload:

2,400 LBS

Fuel capacity:

403 GAL


Engine (x2)


Manufacturer:

Honeywell

Model:

TPE331-10-501M

Horsepower:

665 HP

Overhaul (HT):

5,400 Hrs

Also Consider


CESSNA 441 Conquest II (1977 - 1987)

Image description

Best Cruise: 283 KIAS ( 30 )
Best Range: 2193 NM ( 593 )
Fuelburn: 75.8 GPH ( 2.6 )

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