Cookie Consent by TermsFeed 1974 - 1976 MITSUBISHI MU-2B-26 - Specifications, Performance, Operating cost, Valuation, Brokers - planephd.com

1974 - 1976 MITSUBISHI MU-2B-26

Twin engine turboprop aircraft with retractable landing gear. The MU-2B-26 seats up to 8 passengers plus 1 pilot.


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Performance specifications


Horsepower:

2 x 665 HP

Best Cruise Speed:

308 KIAS

Best Range (i):

1,330 NM

Fuel Burn:

78.4 GPH

Stall Speed:

76 KIAS

Rate of climb:

2,350 FPM

Rate of climb (1 engine out):

475 FPM

Ceiling:

29,300 FT

Ceiling (1 engine out):

14,000 FT

Landing distance:

1,960 FT

Takeoff distance over 50ft obstacle:

1,800 FT


Weights


Gross Weight:

10,470 LBS

Empty Weight:

7,092 LBS

Maximum Payload:

2,300 LBS

Fuel capacity:

366 GAL


Engine (x2)


Manufacturer:

Honeywell

Model:

TPE331-6-251M

Horsepower:

665 HP

Overhaul (HT):

5,400 Hrs

Also Consider


MITSUBISHI MU-2B-26A (1977 - 1978)

Image description

Best Cruise: 310 KIAS ( 2 )
Best Range: 1461 NM ( 131 )
Fuelburn: 78.4 GPH ( 0.0 )

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