Cessna 310D

The Cessna 310D is a four seat, low-wing, twin piston engine aircraft with a conventional tail produced by Cessna in 1960 with 268 produced. Distinguishing features are: retractable landing gear, constant-speed propellers. The 310D seats up to 3 passengers and 1 pilot.




Exterior Dimensions

Wing span: 36 ft 11 in
Length: 29 ft 6 in
Height: 9 ft 11 in


Manufacturer: Continental
Model: IO-470-D
Horsepower: 260 hp
Overhaul (HT): 1500 TBO or 12 years



Horsepower: 260.00 Gross Weight: 4,830
Top Speed: 191 Empty Weight: 2,850
Cruise Speed: 178 Fuel Capacity: 102
Stall Speed (dirty): 71 Range: 640
Rate of Climb: 1,700 Rate of Climb (One Engine): 415
Service Ceiling: 19,500 Ceiling (One Engine): 7,700
Takeoff Landing
Ground Roll: 1,120 Ground Roll 1,285
Takeoff Roll Over 50 ft: 1,375 Landing Roll Over 50 ft: 1,710





The 1960 Cessna 310D was equipped with the Continental IO-470-D 260 hp fuel-injected engine and a Maximum take-off weight of 4,830 lbs. This model also had the rounded nose and ‘tuna' style wingtip fuel tanks just as the Cessna 310C.. The 1960 model was the first year for the swept-back vertical stabilizer, as they were doing across the fleet, and individual seats. A total of 268 were built in the 1960 model year.



Search for Cessna 310D Aircraft for sale now!

This article uses material from this Wikipedia article, which is released under the Creative Commons Attribution-Share-Alike License 3.0.
Get FREE Aircraft Market Alerts

Get FREE Aircraft Market Alerts

Join our mailing list to receive the latest Exclusive Aircraft Market Alerts from our team.

IMPORTANT: You must check your email and confirm after you subscribe to receive alerts from our system!

I want to receive...

Success! Now, please check your email to confirm!