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1979 - 1985 MITSUBISHI MU-2B-60
Twin engine turboprop aircraft with retractable landing gear. The MU-2B-60 seats up to 10 passengers plus 1 pilot.
Market Stats
Performance specifications
Horsepower:
2 x 715 HP
Best Cruise Speed:
295 KIAS
Best Range (i):
1,395 NM
Fuel Burn:
81.6 GPH
Stall Speed:
76 KIAS
Rate of climb:
2,200 FPM
Rate of climb (1 engine out):
410 FPM
Ceiling:
29,750 FT
Ceiling (1 engine out):
14,800 FT
Landing distance:
2,200 FT
Takeoff distance over 50ft obstacle:
2,170 FT
Weights
Gross Weight:
11,575 LBS
Empty Weight:
7,850 LBS
Maximum Payload:
1,850 LBS
Fuel capacity:
403 GAL
Ownership Costs 1979
Total Cost of Ownership:
$86,261.10
Total Fixed Cost
$39,175.50
Storage:
$840.00
Weather service:
$604.89
Insurance:
$6,145.22
Pilot training
$7,812.00
Miscellaneous expenses:
$708.50
Refurbishing and modernization:
$3,562.45
Depreciation:
$19,502.44
-
Total Variable Cost (54.2 Hrs)
Cost Per Hour = $868.74
Cost Per Mile = $2.94
$47,085.60
-
Fuel cost per hour:
(81.6 gallons/hr @ $5.40/gal) $440.64
Oil cost per hour:
$0.00
Overhaul reserves:
$242.00
Hourly maintenance:
$100.01
Misc: landing, parking, supplies,
catering, etc$86.09
Engine (x2)
Manufacturer:
Honeywell
Model:
TPE331-10-501M
Horsepower:
715 HP
Overhaul (HT):
5,400 Hrs
Also Consider
MITSUBISHI MU-2B-36 (1974 - 1976)
Best Cruise: 276 KIAS
(
19
)
Best Range: 1261 NM
(
134
)
Fuelburn: 81.6 GPH
(
0.0
)