1963 Cessna 182F
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
Just installed with new wiring: Garmin 430 Garmin 106A Par200b audio panel/com Garmin 327 Tsp Previously installed: ADS-B Tail beacon JPI 700
Description
Super low time airframe 2150. 780hrs since factory reman in 2004. IFR capable GPS,ILS,VOR. Priced to sell!
Engine
780 in continental factory reman spin on oil filter bracket filter
Interior
Upholstery is very nice overall. BAS seat belts, Rosen sunvisors, new headliner.
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 |
|---|---|---|---|---|---|---|
|
Ken Schmick
trade-a-plane.com
|
$135,000
|
Fonddulac, WI | Apr 17, 2026 | — | Active |
Estimate Monthly Payment
Cessna 182F loan calculator
AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 182F
This 1963 Cessna 182F (N3317U) is a 4-seat single engine piston with 2,150 hours on the airframe. There are currently 4 182F aircraft listed for sale with asking prices ranging from $119,000 to $179,950. This aircraft is priced below the market average at $135,000.
The 182F 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 2,150 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 182F — 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 N3317U.
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 N3317U against the NTSB accident database.
Service Difficulty Reports — Cessna 182F
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
NOSE GEAR UPPER TORQUE LINK BROKE CAUSING GEAR TO COLLAPSE UPON TOUCHDOWN.
THE FUEL SELECTOR VALVE WOULD NOT STOP THE FLOW OF FUEL IN ANY OF THE FOUR DETENTS (OFF-LEFT-BOTH-RIGHT) AT THE FIREWALL FUEL GASCOLATOR DURING AN ANNUAL INSPECTION. THE AIRPLANE HAD SAT IDLE FOR APPROXIMATELY 8 YEARS WITH THE FUEL TANKS FULL. AS I...
LEFT MAIN GEAR SPRING BROKE ON TAXI TO TAKEOFF. CRACK WAS LOCATED INSIDE THE SADDLE AREA WHICH PREVENTED ABILITY TO SEE CRACK THROUGH THE ACCESS PANNELS. THE ONLY WAY TO INSPECT THIS SPRING STRUT IS TO REMOVE THE GEAR STRUT FROM THE ACFT AND VISUAL...
THE STARBOARD MUFFLER BAFFLE CONE BROKE LOOSE FROM THE MUFFLER HOUSING AND OBSTRUCTED THE EXHAUST PIPE, CREATING BACK PRESSURE IN THE EXHAUST SYSTEM WHICH CAUSED THE ENGINE TO LOSE POWER. THE SUBSEQUENT FORCED LANDING ACCIDENT SUBSTANTUALLY DAMAGED T...
ROCKER ARMS (2OFF) HAD HARD FACING FAILURE. FOUND DURING INSPECTION IAW AD/ENG/4 AMDT9.
(AUS) RT WING MAIN SPAR ANGLE CONTAINED EXFOLIATION CORROSION IN AREA OF WING ATTACHMENT ANGLE.
(CAN) CRANKCASE WAS DISCOVERED CRACKED NEAR OIL CAP LOCATION. CRANKCASE REPLACED.
(AUS) LT WING FRONT SPAR CAP DOUBLER PLATE CONTAINED INTERGRANULAR CORROSION.
(AUS) LT WING FRONT SPAR CAP ANGLE CORRODED.
ON ROUTINE SKYDIVING FLIGHT, THE APPROPRIATELY RATED AND QUALIFIED PILOT ENTERED A CROSS CONTROL MANEUVER TO CLOSE CABIN DOOR. UPON RETURNING TO NORMAL FLIGHT THE PIC EXPERIENCED LOSS OF AILERON CONTROL EXHIBITED BY CONTROL WHEEL ROTATING 360 DEGREE...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
Similar Aircraft for Sale
