1968 Cessna 210J
Single Engine Piston
Aircraft Details
Seller reportedDescription
1968 Cessna 210J N6187F Tach: 2621.8 TTAF: 2621.8 Annual Done: 3-17-2025 Engine: Continental IO-520 Engine TTSN: 258.78 - Installed 7-15-05 - All engine hoses replaced with new including hydraulic hoses forward and aft of firewall on 4-22-97 Prop: McCauley D3A32C88-MNO Prop TTSOH: 258.78 Spar AD done 10-17-23 Avionics; - Dual King KX 155/GS - KI 204 indicator - KMA24 Audio Panel/Marker receiver - King KT76A - Ameri-King Encoder AK-350 - Electronics International Digital EGT - Sigtronics SPA 400 Four place intercom Additional Items; - Whelen HDA-CF Wing Tip and Tail strobe system - SK 210-141A seat belt/shoulder harness kit for pilot/co-pilot - Both landing gear saddles replaced with 129415 -1 -2 Text Tyler Peters for any questions, info or more pictures $129,000
Engine
Continental IO-520 Engine TTSN: 258.78 - Installed 7-15-05 - All engine hoses replaced with new including hydraulic hoses forward and aft of firewall on 4-22-97
Inspection
Annual Done
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
|
$129,000
|
Lewiston, ID | Mar 20, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 210J
This 1968 Cessna 210J (N6187F) is a 6-seat single engine piston with 2,621 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 below the market average at $129,000.
The 210J cruises at 160 kts (296 km/h) with a range of 700 nm (1,296 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 2,621 hours on the airframe, this aircraft has exceeded TBO (1,700 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 N6187F.
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 N6187F 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.
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