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1978 CESSNA 310R II

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Twin engine piston aircraft with retractable landing gear. The 310R II seats up to 5 passengers plus 1 pilot.


Performance specifications


Horsepower:

2 x 285 HP

Best Cruise Speed:

194 KIAS

Best Range (i):

661 NM

Fuel Burn @ 75%:

26.2 GPH

Stall Speed:

70 KIAS

Rate of climb:

1,662 FPM

Rate of climb (1 engine out):

370 FPM

Ceiling:

19,750 FT

Ceiling (1 engine out):

7,400 FT

Takeoff distance:

1,335 FT

Landing distance:

640 FT

Takeoff distance over 50ft obstacle:

1,700 FT

Landing distance over 50ft obstacle:

1,790 FT


Weights


Gross Weight:

5,500 LBS

Empty Weight:

3,603 LBS

Fuel capacity:

102 GAL


Ownership costs


1978 Typical Price:

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Total Cost of Ownership:

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Total Fixed Cost

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Annual inspection cost:

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Storage:

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Weather service:

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Insurance:

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Miscellaneous expenses:

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Refurbishing and modernization:

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Depreciation:

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Total Variable Cost (100 Hrs)
Cost Per Hour = $233.30
Cost Per Mile = $1.20

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Fuel cost per hour:
(26.2 gallons/hr @ $5.40/gal)

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Oil cost per hour:

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Overhaul reserves:

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Hourly maintenance:

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Misc: landing, parking, supplies,
catering, etc

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Engine (x2)


Manufacturer:

Cont Motor

Model:

IO-520-M

Horsepower:

285 HP

Overhaul (HT):

1,700 Hrs

Years before overhaul:

12

Also Consider


CESSNA 310Q (1970 - 1974)

Image description

Typical Price: $89,339.00
Total Cost of Ownership: $31,047.09
Best Cruise: 192 KIAS ( 2 )
Best Range: 680 NM ( 19 )
Fuelburn: 25.5 GPH ( 0.7 )

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