1960 Cessna 182C
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
IFRPanel upgrades in 2018 GTN 650 ATT Garmin G5 DG/HSI Garming G5 ALT Kollsman Transponder Garmin GTX 345 Encoder Garmin GAE 12 ELT ACK Technologies E-04-ELT
Description
1960 182C Skylane 4135TT, 2114.9 SMOH. New panel 2018, GTN 650, ATT Garmin G5, DG/HSI Garmin G5, Garman GTX 345, Garmin GAE 12. New prop control cable, cowl flap cable, tires, engine oil heater, 2018. New ELT. rubber floor, 2020. Prop overhauled 2020, 917 hours. 2 Bose headsets. Last annual 5/8/24. All logs available.
Engine
Engine: Continental 0-470-L S/N 069689-R 2114.9 SMOH Compression at last annual: #1 74, #2 68, #3 72, #4 62, #5 74, #6 67. Engine overhauled in 1988. Propeller: McCauley Model 2A34C203-C 917.4 total hours, overhauled 12 hours ago.
Interior
New rubber floor 2020. New tires 2018.
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
|
$95,000
$115,000
|
Driggs, ID | Mar 20, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 182C
This 1960 Cessna 182C (N8682T) is a 4-seat single engine piston with 4,136 hours on the airframe. There are currently 6 182C aircraft listed for sale with asking prices ranging from $79,950 to $148,000. This aircraft is priced below the market average at $95,000.
The 182C cruises at 140 kts (259 km/h) with a range of 915 nm (1,695 km) — ideal for short hops and local flights. Service ceiling of 18,100 ft allows operation above most weather.
Operating costs: Fuel burn is 12.5 GPH (47 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $69/hr in fuel alone. Total variable cost including maintenance reserves is approximately $160/hr. Annual fixed costs (hangar, insurance, crew, annual inspection) average $20,000. With 4,136 hours on the airframe, this aircraft has exceeded TBO (2,000 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 182C — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateCESSNA 182
AeroGurus estimates based on industry averages for the CESSNA 182. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
FAA registration data pending for N8682T.
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 N8682T against the NTSB accident database.
Service Difficulty Reports — Cessna 182C
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
DURING INSPECTION, FOUND EVIDENCE OF FUEL LEAKING FROM WITHIN THE FUEL TRANSDUCER. FUEL STAINS WERE FOUND ON EXTERIOR OF THE TRANSDUCER AND ON THE FIRE SHIELD SURROUNDING IT. THERE WAS NO APPARENT LEAKING OUTSIDE OF THE FIRE SHIELD ITSELF. THE UNI...
ENG RUNS ROUGH. ENG MISFIRES. HISTORY: 2/25/2004; TACH 487.1 - REPLACED LT AND RT MAGNETOS. ACFT RUN UP CHECKED OUT OK. 4/26/2004 TACH 508 - CHECKED TIMING. 05/11/2005 (NO TACH) - TROUBLESHOOTING ROUGH ENGINE. REMOVED INTAKE MANIFOLD AND FLAT SAN...
(AUS) BOTH CONTROL WHEELS CRACKED FROM BOTTOM RIVET HOLE.
ELECTRIC TRIM SERVO AT ELEVATOR, FAILED.
DURING 100-HOUR INSPECTION, ONE LEG OF THE U-BOLT ON THE LT MAIN GEAR LEG WAS FOUND BROKEN IN THE THREAD AREA. SUBMITTER SUSPECTS IT WAS DUE TO FATIGUE. A CLOSER LOOK AT THESE BOLTS DURING INSPECTION WOULD BE IN ORDER.
TWO NEW SNAP-RING COUPLINGS INSTALLED AT ANNUAL INSPECTION. SEVEN HOURS LATER BOTH COUPLING SPRINGS FAILED ON CONSECUTIVE ENGINE STARTS. SPRING FAILURES APPEAR TO BE IDENTICAL. COUPLINGS WERE BOUGHT AND INSTALLED AS ASSEMBLIES PREVENTING INSPECTIO...
FUEL CAP LEAKED RAIN WATER THROUGH CAP WHICH HAS A BUILT-IN WATER TRAP. SUBMITTER RECOMMENDS REPLACEMENT OF CAP AND ADAPTER WITH DESIGN WHICH DOES NOT TRAP RAIN WATER.
BLADDER FUEL TANKS LEAKED FUEL WHEN FILLED ABOVE ONE-HALF FULL MARK. CAUSED BY ABRASION DURING COLLAPSING OF FUEL TANK. RECOMMEND REPLACEMENT WITH FIBERGLASS TANKS.
BLADDER FUEL TANKS LEAKED FUEL WHEN FILLED ABOVE ONE-HALF FULL MARK. CAUSED BY ABRASION DURING COLLAPSING OF FUEL TANK. RECOMMEND REPLACEMENT WITH FIBERGLASS TANKS.
PISTON WAS COMPLETELY DISINTEGRATING. ALL VALVES AND OTHER ENGINE PARTS COMPLETE AND ACCOUNTED FOR. SUSPECT CAUSE WAS METAL WAS TOO BRITTLE. PISTON PIN WAS IN ROD AND MOVING AROUND IN CYLINDER.
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.