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1977 - 1978 MITSUBISHI MU-2B-36A
Twin engine turboprop aircraft with retractable landing gear. The MU-2B-36A seats up to 10 passengers plus 1 pilot.
Market Stats
Performance specifications
Horsepower:
2 x 715 HP
Best Cruise Speed:
283 KIAS
Best Range (i):
1,261 NM
Fuel Burn:
81.6 GPH
Stall Speed:
76 KIAS
Rate of climb:
2,200 FPM
Rate of climb (1 engine out):
420 FPM
Ceiling:
27,100 FT
Ceiling (1 engine out):
11,000 FT
Landing distance:
2,200 FT
Takeoff distance over 50ft obstacle:
2,170 FT
Weights
Gross Weight:
11,575 LBS
Empty Weight:
7,896 LBS
Maximum Payload:
1,790 LBS
Fuel capacity:
364 GAL
Ownership Costs 1978
Total Cost of Ownership:
$84,919.99
Total Fixed Cost
$33,776.24
Storage:
$840.00
Weather service:
$604.89
Insurance:
$4,872.64
Pilot training
$7,812.00
Miscellaneous expenses:
$649.96
Refurbishing and modernization:
$2,824.72
Depreciation:
$16,172.04
-
Total Variable Cost (56.5 Hrs)
Cost Per Hour = $905.20
Cost Per Mile = $3.20
$51,143.75
-
Fuel cost per hour:
(81.6 gallons/hr @ $5.40/gal) $440.64
Oil cost per hour:
$0.00
Overhaul reserves:
$292.00
Hourly maintenance:
$82.85
Misc: landing, parking, supplies,
catering, etc$89.70
Engine (x2)
Manufacturer:
Honeywell
Model:
TPE331-5-252M
Horsepower:
715 HP
Overhaul (HT):
5,400 Hrs
Also Consider
MITSUBISHI MU-2B-30 (1969 - 1971)
Best Cruise: 261 KIAS
(
22
)
Best Range: 1348 NM
(
87
)
Fuelburn: 78.4 GPH
(
3.2
)