1969 Cessna 210J
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
BTHAttitude Indicator HSI Garmin GTN 650 GPS/NAV/COM Garmin GTR 225A COM2 Garmin GI 106A CDI Garmin GTX 345 Transponder (ADS-B In/Out) Garmin GFC 500 Digital Autopilot (fully coupled) GEM Engine Monitor Voice Alert 2040-1-2P enhanced stall and gear warning system This panel is exactly what you want in a cross-country 210
clean logical and all Garmin. Dual G5s drive the GFC 500 autopilot the GTN 650 handles GPS/NAV/COM dutiesand the GTX 345 provides full ADS-B traffic and weather plus a second NAV with the GTN225A driving a GI-106A CDI. Everything plays together flawlessly and makes IFR ops effortless.
Description
Garmin glass cockpit, w GFC-500. 568 hrs SMOH, 140 hrs SPOH - 1,252lb useful load. Recent Power pack and WIng Spar AD. Clean, no damage history. Flies regularly, times will change.
Engine
Engine Make/Model: Continental IO-520-J1B (285 HP) SMOH: 588 hours TBO: 1,700 hours (Continental SID97-3G) Overhaul Type: Factory Rebuild TCM Prop: McCauley 3 Blade PTSMO: 140 Hours Last Annual October 2025 Notes: Smooth, strong compressions, consistently flown and maintained
Propeller
Fully documented maintenance history, solid, corrosion free. Logs: Complete and continuous since new AD 2020-03-16 Carry-Through Spar: Complied with in 2021 Hydraulic Power Pack Overhaul: 2023 No Damage History
Interior
New interior and paint 1997. Overall condition in and out is good. Includes Bruces Custom Extended Canopy Cover (210-12)
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 |
|---|---|---|---|---|---|---|
|
Ovation Aviation
trade-a-plane.com
|
$179,500
|
Las Vegas, NV | May 12, 2026 | — | Active | |
|
Nicholas Geber
barnstormers.com
|
$169,500
|
Las Vegas, NV | Jun 01, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 210J
This 1969 Cessna 210J (N6195F) is a 6-seat single engine piston with 2,350 hours on the airframe. There are currently 2 210J aircraft listed for sale with asking prices ranging from $129,000 to $179,500. This aircraft is priced above the market average at $179,500.
The 210J cruises at 164 kts (304 km/h) with a range of 900 nm (1,667 km) — ideal for short hops and local flights. Service ceiling of 17,300 ft allows operation above most weather.
Operating costs: Fuel burn is 14.5 GPH (55 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $80/hr in fuel alone. Total variable cost including maintenance reserves is approximately $175/hr. Annual fixed costs (hangar, insurance, crew, annual inspection) average $22,000. With 2,350 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 210J — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateCESSNA 210
AeroGurus estimates based on industry averages for the CESSNA 210. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
FAA registration data pending for N6195F.
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 N6195F against the NTSB accident database.
Service Difficulty Reports — Cessna 210J
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
THE FOLLOWING IS THE INFORMATION FOR THE FAA FORM 8010-4 MALFUNCTION OR DEFECT REPORT REFERENCE CRACKS IN THE MLG ACTUATOR BULKHEAD DOUBLERS ON CESSNA 210J SN 21059120 N3320S TOTAL TIME AIRFRAME IS 3837.6 HOURS. THE EFFECTED DOUBLERS WERE REMOVED FR...
DURING THE ANNUAL INSPECTION REINFORCEMENT BRACKET (P/N 12 32623-1) WAS FOUND TO HAVE A CRACK RUNNING FROM THE BOTTOM BOLT HOLE TO THE EDGE OF THE BRACKET. THE BRACKET IS ATTACHED TO THE REAR SPAR OF THE LT HORIZ STABILIZER. AFFECTED PART REPLACED....
DURING THE ANNUAL INSPECTION A CRACK WAS DETECTED RUNNING FROM THE ANCHOR NUT RIVET HOLE TO THE EDGE OF THE DOUBLER PLATE, THIS BRACKET IS ATTACHED TO THE REAR FRAME AT STN 209, P/N 12120402-3. AFFECTED PART REPLACED. (TC NR 20080328004)
GEAR WARNING HORN WAS INOPERATIVE. AC LANDED WITH LANDING GEAR UP. SUBSEQUENT INVESTIGATION DETERMINED THROTTLE MICROSWITCH WAS MAKING INTERMITTENT CONTACT WHEN ENGAGED AND GROUND CONNECTION WAS INSUFFICIENT. CORRECTED BY REPLACING SWITCH AND REPA...
(CAN) DURING A MAINTENANCE FUNCTION SEVERE CORROSION WAS DISCOVERED ON THE BOTTOM OF THE WING SPAR ENTRE SECTION. THIS SECTION OF THE SPAR HAS HIGH DENSITY FOAM GLUED TO THE SPAR WHICH PREVENTS ADEQUATE INSPECTION. THE CORROSION WAS SUCH THAT THE WIN...
DURING A SCHEDULED MAINTENANCE INSPECTION, THE TECHNICIAN DISCOVERED A CRACK IN THE OIL COOLER ASSEMBLY AT THE WELD WHERE THE COOLER BODY MEETS THE MOUNTING FLANGE.
(CAN) VISUAL INSPECTION DETECTED CRACKED CASE. ONCE ENGINE DISMANTLED, EXCESSIVE CRACK FOUND IN THE FRONT MAIN JOURNAL AREA. LARGE SECTION OF JOURNAL COMPLETELY DETACTED FROM CASE.
DURING DISASSEMBLY FOR OVERHAUL, BLADE RETENTION FERRULE C4451 FOUND CRACKED IN BEARING FLANGE ON NR 2 BLADE. THE CRACK APPEARS TO HAVE STARTED AT AN OLD ACTUATING PIN HOLE AND IS OVER THREE INCHES LONG. S/B 196B HAD NOT BEEN ACCOMPLISHED ON THIS P...
WHILE MAKING A APPROACH TO THE AIRPORT FOR LANDING, THE PILOT ADDED POWER WITH NO ENGINE RESPONSE. THE THROTTLE CABLE DISCONNECTED FROM THE ENGINE CONTROL ARM DUE TO THE THROTTLE ATTACHING BOLT MISSING ALONG WITH THE WASHER, NUT AND COTTER PIN. THROT...
THE ORIGINAL HINGE MFG OF ALUMINUM WORE OUT AND DROPPED PIECES IN THE INTAKE, CAUSING DAMAGE TO THE TURBOCHARGER. SERIOUS DAMAGE WAS AVOIDED BY A TIMELY INSPECTION. THE NEW SUPPLIED PART IS STAINLESS STEEL WITH A HINGE PIN SECURED BY CRIMPING. THI...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
Price History
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