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);
- 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
- Price: Sold
- Year Of Manufacture : 1969
- Registration #:N5793M
- Serial #:310P0093
- Location:vancover
- Aircraft Type:Multi engine piston
Engine(s) Details
-
SMOH:
Manufacturer: Cont Motor Model: TSIO-520-B Horsepower: 285 HP Overhaul (HT): 1,400 Hrs Years before overhaul: 12
Airframe
- Total Time:3000
- Number of Seats:6
For more information contact:
- Jan Moon
- 360-480-9599
- jan@Oncenterline.net
