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1969 CESSNA 310P

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


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Performance specifications


Horsepower:

2 x 260 HP

Best Cruise Speed:

193 KIAS

Best Range (i):

676 NM

Fuel Burn @ 75%:

25.5 GPH

Stall Speed:

62 KIAS

Rate of climb:

1,540 FPM

Rate of climb (1 engine out):

330 FPM

Ceiling:

19,900 FT

Ceiling (1 engine out):

6,850 FT

Takeoff distance:

1,451 FT

Landing distance:

558 FT

Takeoff distance over 50ft obstacle:

1,716 FT

Landing distance over 50ft obstacle:

1,673 FT


Weights


Gross Weight:

5,200 LBS

Empty Weight:

3,170 LBS

Fuel capacity:

102 GAL


Engine (x2)


Manufacturer:

Cont Motor

Model:

IO-470 Series

Horsepower:

260 HP

Overhaul (HT):

1,500 Hrs

Years before overhaul:

12

Also Consider


CESSNA 310Q (1970 - 1974)

Image description

Best Cruise: 192 KIAS ( 1 )
Best Range: 680 NM ( 4 )
Fuelburn: 25.5 GPH ( 0.0 )

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