Cookie Consent by TermsFeed 1972 - 1974 MITSUBISHI MU-2B-25 - Specifications, Performance, Operating cost, Valuation, Brokers - planephd.com

1972 - 1974 MITSUBISHI MU-2B-25

Twin engine turboprop aircraft with retractable landing gear. The MU-2B-25 seats up to 8 passengers plus 1 pilot.


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Performance specifications


Horsepower:

2 x 665 HP

Best Cruise Speed:

270 KIAS

Best Range (i):

1,461 NM

Fuel Burn:

78.4 GPH

Stall Speed:

71 KIAS

Rate of climb:

2,650 FPM

Rate of climb (1 engine out):

600 FPM

Ceiling:

33,200 FT

Ceiling (1 engine out):

19,800 FT

Landing distance:

1,800 FT

Takeoff distance over 50ft obstacle:

1,700 FT


Weights


Gross Weight:

9,920 LBS

Empty Weight:

6,500 LBS

Maximum Payload:

2,750 LBS

Fuel capacity:

366 GAL


Engine (x2)


Manufacturer:

Honeywell

Model:

TPE331-6-251M

Horsepower:

665 HP

Overhaul (HT):

5,400 Hrs

Also Consider


PIPER PA-31T-620 Cheyenne II XL (1981 - 1984)

Image description

Best Cruise: 270 KIAS ( 0 )
Best Range: 1336 NM ( 125 )
Fuelburn: 75.5 GPH ( 2.9 )

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