No longer listed as of April 2026. The price below is the last asking price — the final sale price is not disclosed.
1965 Cessna 310J
Multi Engine Piston
No longer listed
Contact for price
Location
Livermore, CA
Total Time
6,009 hrs
Engine SMOH
204 hrs
Seats
6
Serial #
310J0042
Reg #
N3042L
Engine
CONTINENTAL O-470-U
Cruise
190 kts (352 km/h)
ICAO Type
C310
✓ Clean NTSB
⚠ High time
Listing Details
Seller reported- Year
- 1965
- Make
- Cessna
- Model
- 310J
- Total Time
- 6,009 hr
- Location
- Livermore, CA
- Seller
- American Aircraft Sales
- Source
- trade-a-plane.com
SOLD - This New Updated Metal Instrument Panel With Garmin And Aspen Avionics Is Amazing Including New Modern Paint And Interior Giving The Airplane The Appearance Of A Brand New Airplane. Hangar Kept In Livermore California KLVK. Complete And Original Logbooks Since New.
Cessna 310J — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Seats
6
Cruise Speed
190 kts (352 km/h)
Max Speed
200 kts (370 km/h)
Range
800 nm (1,482 km)
Ceiling
20,000 ft (6,096 m)
Max Weight
5,100 lbs (2,313 kg)
Useful Load
1,700 lbs (771 kg)
Horsepower
260 HP
Fuel Capacity
100 gal (378 L)
Fuel Burn
26 GPH (98 L/h)
Engines
2
TBO
1,500 hrs
Estimated Cost of Ownership
AeroGurus estimateFuel Burn
26.0 GPH
~$169/hr
Variable Cost
$290/hr
fuel + mx + reserves
Annual Fixed
$26,000/yr
hangar + insurance + annual
Engine Overhaul
$38,000
every 1,500 hrs
AeroGurus estimates based on industry averages for the . Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
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About the Cessna 310J
The Cessna 310J is a mid-1960s member of the 310 light-twin line (1963-1965) — twin 260-hp Continental O-470 engines, five-to-six seats and the sleek tip-tank styling that made the 310 famous. It cruises near 190 kt, well above any piston single, at the cost of twin-engine fuel, maintenance and currency. The buy case is fast cabin travel on a piston-twin budget; pre-buy focus is engine and prop time on both sides plus the integrity of the tip-tank fuel system.
Produced 1963–1965.