1966 Cessna 310K
Multi Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
BTHNarco MK12E Nav/Com Narco MK12E Nav/Com King KT 76A Transponder Auto Panel Autopilot Navomatic 400 Sigtronics Intercom Davtron M877 Chronometer Davtron Clock
Description
1966 CESSNA 310K Based in Southern California with 5691.4 Aircraft Total Time, Both Engines have 462.7 Time Since Overhaul, and Both Props Overhauled in 2025.
Engine
Engines: Continental IO-470-U both with 462.7 Hours Since Overhaul Propellers: McCauley D3AF32C80-ANR/S-82NC-4 Both Overhauled in 2025
Description and equipment details provided by the seller. AeroGurus does not verify seller-provided information.
Price Comparison 1 active offer
| Source | Price | Location | Listed | Days on Market | Status | Action |
|---|---|---|---|---|---|---|
|
Listing Source
trade-a-plane.com
|
$84,900
|
Upland, CA | Apr 17, 2026 | — | Active |
Estimate Monthly Payment
Cessna 310K loan calculator
AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 310K
This 1966 Cessna 310K (N7098L) is a 5-seat multi engine piston with 5,691 hours on the airframe. There are currently 2 310K aircraft listed for sale with asking prices ranging from $84,900 to $179,000. This aircraft is priced below the market average at $84,900.
The 310K cruises at 190 kts (352 km/h) with a range of 800 nm (1,482 km) — ideal for short hops and local flights.
Operating costs: Fuel burn is 22 GPH (83 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $121/hr in fuel alone. Total variable cost including maintenance reserves is approximately $280/hr. Annual fixed costs (hangar, insurance, crew, annual inspection) average $25,000. With 5,691 hours on the airframe, this aircraft has exceeded TBO (1,500 hrs) — verify engine status and overhaul reserve.
NTSB records show 0 incidents for this airframe — a clean safety record. Mechanics have filed 10 service difficulty reports for this type — common maintenance items to discuss during pre-buy.
Pre-Purchase Checklist
Cessna 310K — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateCESSNA 310
AeroGurus estimates based on industry averages for the CESSNA 310. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
FAA registration data pending for N7098L.
Location & Ownership
Title Status
No FAA title records
Available for US-registered aircraft only
Source: FAA Aircraft Registry, FAA Civil Aviation Registry (DocIndex). Title data may be delayed. Always verify with an aviation attorney before purchase.
Safety Record
NTSB safety data coming soon.
We'll check N7098L against the NTSB accident database.
Service Difficulty Reports — Cessna 310K
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
THE FLOW DIVIDER ON TOP OF THE ENGINE AT THE SPINE HAS A SMALL COMPENSATION HOLE ABOVE THE DIAPHRAGM. IF THE DIAPHRAGM HAS A PERFORATION, RAW FUEL WILL RISE ABOVE THE DIAPHRAGM AND SPEW FROM THIS HOLE AND THUS CAUSE AND EXTREME FIRE HAZARD. I HAVE OB...
SCREW TO HOLD FAIRING BETWEEN WING AND TIP TANK TOO LONG AND POSSIBLE PENETRATING / RUBBING ON FUEL TANK. THE INNER AERODYNAMIC FAIRING BETWEEN TIP TANK AND UPPER SURFACE OF WING HAS A TINNERMAN NUT PLATE TO CONNECT TO ANOTHER FAIRING. SCREWS IN THIS...
ARM ASSY BELLCRANK IDLER BROKEN WHERE TUBE ASSY GEAR MAIN DRIVEIS BOLTED TO THE BELLCRANK.
AFTER LANDING, LT MLG STRUT WAS DISCOVERED TO BE FLAT. INITIAL INSPECTION REVEALED THAT THE SCHRADER VALVE HAD FAILED, BUT AFTER VALVE REPLACEMENT, THE STRUT WOULD STILL NOT REMAIN INFLATED. FURTHER INSPECTION REVEALED THAT THE STRUT WAS ALSO LEAKI...
LEFT THROTTLE CABLE SEPARATED FROM STATIONARY SWEDGE IN THE ENGINE COMPARTMENT REDUCING ENGINE POWER DURING ROTATION PHASE OF A TOUCH AND GO PROCEDURE. ACFT HAD DIFFICULITY MAINTAINING A POSITIVE RATE OF CLIMB DUE TO REDUCED ENGINE POWER AND A HIGH ...
INSTALLED NEW SHAFT, PN 0894000-12 ON BOTH MLG AT 3520.9 AND AT 3620.9. BOTH SHAFTS WERE CRACKED ON RT SIDE. THE NEW STYLE SHAFTS HAVE A LARGER DIAMETER ROLL PIN AND THIS HOLE IS WHERE THE CRACKS ARE STARTING FROM. THE NEW STYLE SHAFTS ARE MADE WE...
INSTALLED NEW SHAFT, ON BOTH MLG AT 3383.80 AND AT 3520.9 BOTH SHAFTS WERE CRACKED ON RT SIDE.
IDLER BELLCRANK FAILED DURING RETRACTION CYCLE. THIS BELLCRANK IS CAST ALLOY. IN MY OPINION IT SHOULD BE A MACHINE PART. (K)
AC EXPERIENCED FLAP ASYMMETRIC LIGHT IN CRUISE FLIGHT CREW DIVERTED TO ATL LIGHT WENT OUT AND FLAPS WORKED PROPERLY FOR AN UNEVENTFUL LANDING. PROBLEM COULD NOT BE DUPLICATED SO BOTH FLAP FOLLOW UPS WERE REPLACED IAW THE MM. AIRCRAFT OPS CHECK GOOD.
LT FUSELAGE BY LAP SEAM BULGE IN SKIN NEAR FRAME 61 AND 62 AND BETWEEN STRINGERS S-44L AND S-45L.
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
Similar Aircraft for Sale
