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1973 CESSNA 310Q

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


Performance specifications


Horsepower:

2 x 260 HP

Best Cruise Speed:

192 KIAS

Best Range (i):

680 NM

Fuel Burn @ 75%:

25.5 GPH

Stall Speed:

63 KIAS

Rate of climb:

1,495 FPM

Rate of climb (1 engine out):

327 FPM

Ceiling:

19,500 FT

Ceiling (1 engine out):

6,680 FT

Takeoff distance:

1,519 FT

Landing distance:

582 FT

Takeoff distance over 50ft obstacle:

1,795 FT

Landing distance over 50ft obstacle:

1,697 FT


Weights


Gross Weight:

5,300 LBS

Empty Weight:

3,214 LBS

Maximum Payload:

1,749 LBS

Fuel capacity:

102 GAL


Ownership costs


1973 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 = $230.15
Cost Per Mile = $1.20

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Fuel cost per hour:
(25.5 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-470-VO

Horsepower:

260 HP

Overhaul (HT):

1,500 Hrs

Years before overhaul:

12

Also Consider


CESSNA 310P (1969 - 1969)

Image description

Best Cruise: 193 KIAS ( 1 )
Best Range: 676 NM ( 4 )
Fuelburn: 25.5 GPH ( 0.0 )

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