1969 Cessna T-310P

1969 Cessna T-310P

Aircraft Summary​

The Cessna 310 is an American four-to-six-seat, low-wing, twin-engine monoplane produced by Cessna between 1954 and 1980. It was the first twin-engine aircraft that Cessna put into production after WW2. Version of 310P with turbocharged Continental TSIO-520-B or TSIO-520-BB engines producing 285 hp (213 kW) and maximum takeoff weight of 5,400 pounds (2,400 kg);

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Aircraft Summary​

The Cessna 310 is an American four-to-six-seat, low-wing, twin-engine monoplane produced by Cessna between 1954 and 1980. It was the first twin-engine aircraft that Cessna put into production after WW2. Version of 310P with turbocharged Continental TSIO-520-B or TSIO-520-BB engines producing 285 hp (213 kW) and maximum takeoff weight of 5,400 pounds (2,400 kg);

Horsepower:
2 x 285 HP
Best Cruise Speed:
226 KIAS
Best Range (i):
807 NM
Fuel Burn @ 75%:
27.2 GPH
Stall Speed:
66 KIAS
Rate of climb:
1,862 FPM
Rate of climb (1 engine out):
440 FPM
Ceiling:
28,600 FT
Ceiling (1 engine out):
18,100 FT
Takeoff distance:
1,250 FT
Landing distance:
640 FT
Takeoff distance over 50ft obstacle:
1,590 FT
Landing distance over 50ft obstacle:
1,790 FT

Manufacturer:

Cont Motor

Model:

TSIO-520-B

Horsepower:

285 HP

Overhaul (HT):

1,400 Hrs

Years before overhaul:

12

Weights


Gross Weight:
5,400 LBS
Empty Weight:
3,292 LBS
Fuel capacity:
102 GAL

This two motor Cessna has 6 seats well maintained and up kept.

Aircraft Details
Engine(s) Details
Airframe
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