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1969 Cessna T-310P

Reg # N5793M

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  • 1969 Cessna T-310P Photo 2
  • 1969 Cessna T-310P Photo 3
  • 1969 Cessna T-310P Photo 4
  • 1969 Cessna T-310P Photo 5
  • 1969 Cessna T-310P Photo 6
  • 1969 Cessna T-310P Photo 7
  • 1969 Cessna T-310P Photo 2
  • 1969 Cessna T-310P Photo 3
  • 1969 Cessna T-310P Photo 4
  • 1969 Cessna T-310P Photo 5
   
 

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).

Airframe:
TTAF: 3,000

Engines:
Continental
SMOH: 400/400
285 HP, Overhaul (HT): 1,400 Hrs, Years before Overhaul: 12

Interior

Number of Seats: 6
This Two Motor Cessna has 6 Seats well Maintained and Up kept

Remarks

Weights:
Gross Weight: 5,400 Lbs
Empty Weight: 3,292 Lbs
Fuel Capacity: 102 Gal

Performance:
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



On Centerline Aviation

Denver,CO



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