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1965 CESSNA 310J

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


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Performance specifications


Horsepower:

2 x 260 HP

Best Cruise Speed:

194 KIAS

Best Range (i):

687 NM

Fuel Burn @ 75%:

25.0 GPH

Stall Speed:

65 KIAS

Rate of climb:

1,590 FPM

Rate of climb (1 engine out):

360 FPM

Ceiling:

20,300 FT

Ceiling (1 engine out):

7,500 FT

Takeoff distance:

1,385 FT

Landing distance:

960 FT

Takeoff distance over 50ft obstacle:

1,640 FT

Landing distance over 50ft obstacle:

1,540 FT


Weights


Gross Weight:

5,100 LBS

Empty Weight:

3,094 LBS

Fuel capacity:

102 GAL


Engine (x2)


Manufacturer:

Cont Motor

Model:

IO-470-U

Horsepower:

260 HP

Overhaul (HT):

1,500 Hrs

Years before overhaul:

12

Also Consider


CESSNA 310I (1964 - 1964)

Image description

Best Cruise: 194 KIAS ( 0 )
Best Range: 687 NM ( 0 )
Fuelburn: 25.0 GPH ( 0.0 )

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