1970 Cessna 182N
Single Engine Piston
Aircraft Details
Seller reportedDescription
1970 182n 7130hr TT 776hr SMO 45hr since new melenuam cylinders Horton stol kit, flap and alirons seals Digital, engine, tach, fuel flow gages Hooker harnesses Garmin 375 gps, transponder Waas adsb in and out 3 blade prop Complete logs books Long range tanks 79 gallons Two coms New brake rotors Carburetor ice detector 4 place intercom Tow hook Wheel pants
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 |
|---|---|---|---|---|---|---|
|
Martin Del Giorgio
trade-a-plane.com
|
$145,000
|
Flagstaff, AZ | Apr 17, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 182N
This 1970 Cessna 182N (N182gg) is a 4-seat single engine piston with 7,130 hours on the airframe. This aircraft is listed at the market average at $145,000.
The 182N cruises at 140 kts (259 km/h) with a range of 640 nm (1,185 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 7,130 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. There are 1 airworthiness directive applicable to this aircraft type — review AD compliance carefully before purchase. Mechanics have filed 10 service difficulty reports for this type — common maintenance items to discuss during pre-buy.
Pre-Purchase Checklist
Cessna 182N — 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 N182gg.
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 N182gg against the NTSB accident database.
Airworthiness Directives — Cessna 182N
ADs are mandatory safety instructions issued by the FAA. 1 recent AD found for this aircraft type.
Cessna Aircraft Company Models 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, and 182R Airplanes
View full AD →Source: FAA Airworthiness Directives database. Showing most recent ADs for this aircraft type.
Service Difficulty Reports — Cessna 182N
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
THE AIRCRAFT HAD A OIL LEAK. WE FOUND THE THREADS IN THE OIL PUMP HOUSING WERE GAULDED AND THE OIL FILTER ADAPTER THREADS WERE DAMAGED. MOST LIKELY FROM OVER TORQUE. THE PUMP BODY P/N 632563 WAS REPLACED AND AIR WOLF REMOTE OIL FILTER KIT INSTALLE...
DURING A ROUTINE 500 HR INSPECTION OF THE MAGNETOS, FOUND BOTH IMPULSE COUPLINGS CRACKED AT HUB PLATE, NEAR FULL ADVANCE STOP NOTCH.
(CAN) LT AND RT CABIN DOOR RESTRAINTS BROKEN AND MISSING ALLOWING DOORS, REPEATEDLY CONTACT WING STRUTS. DAMAGE TO DOOR SKINS AND WING STRUTS OCCURRED.
(CAN) LT AND RT ELEVATOR HORN L/E DEFORMED AND COVERED IN A UNAPPROVED RUBBER L/E BOOT. VERY POOR HORIZONTAL STABILIZER TO ELEVATOR HORN CLEARANCE. WHEN UNAPPROVED RUBBER BOOTS REMOVED, FOUND SUBSTANTIAL SKIN DAMAGE. ELEVATOR BALANCE WITH UNAPPROVE...
(CAN) EXTERNAL GROUND POWER CIRCUIT PROTECTION UNAPPROVED. FOUND PREVIOUSLY TRIPPED GLASS FUSE WRAPPED IN ALUMINUM FOIL FROM A CIGARETTE PACKAGE AND INSTALLED IN FUSE HOLDER.
(CAN) ELT REMOTE POWER WIRING NOT CIRCUIT PROTECTED. FOUND POWER WIRE HARD WIRED TO CLOCK. CLOCK POWER CIRCUIT PROTECTION UNAPPROVED. FOUND CLOCK POWER FUSE WRAPPED IN ALUMINUM FOIL FROM A CIGARETTE PACKAGE.
(CAN) HOT CYLINDER DIFFERENTIAL COMPRESSION CHECK CARRIED OUT AND FOUND ALL CYLINDER COMPRESSIONS WELL BELOW MINIMUM ALLOWABLE. VIDEOSCOPE INSPECTION CARRIED OUT, AND FOUND ALL CYLINDER INTERNAL WALLS HEAVILY CORRODED IN THE CHOKE PORTION OF EACH CYL...
(CAN) ENGINE TEMPERATURE MONITOR PROBES ON THE ODD CYLINDER BANK REVERSED CAUSING THE INCORRECT CYLINDER DATA TO BE DISPLAYED TO PILOT. ALSO, FOUND MAIN POWER AND LIGHTING DIMMER POWER NOT CIRCUIT PROTECTED AND HARD WIRED TO ACFT MAIN BUSS.
CABIN FIRE EXTINGUISHER FOUND TO BE POORLY SECURED TO CABIN FLOOR. PK STYLE SHEET METAL SCREWS FASTENING MOUNT TO LIGHT ALUMINUM FLOOR. WEEK INSTALLATION UNABLE TO WITHSTAND "G" LOADS IN ANY NORMAL AXIS.
(CAN) ENGINE LOWER COWLING INDUCTION AIR DUCT CHAFED THOUGH BY ENGINE EXHAUST MUFFLER HEAT SHROUD. FOUND ENGINE RUBBER ISOLATION MOUNTS WEAK AND DAMAGED AND POOR CLEARANCE WITH MODIFIED ENGINE EXHAUST SYSTEM COMPONENTS.
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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