2001 Cessna 172S
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
Description
Aircraft in very good condition, purchased in Europe in 2022. Still in CAMO. Engine overhaul done a year ago at LOMA AIR in Belgium (Part 145). Aircraft used for flights in ATO and SPO. Taxes: Owner – Aviation Company (net sales (VAT)
Delivery: Worldwide delivery possible
Domage History: No damage history
Interior
Visual condition: 8/10 Interior: Dark brown leather seats, with light beige headliner
Exterior
Visual condition: 9/10
Modifications / STCs
• Contact: +48 602 440 133
• +48 601 262 113
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 |
|---|---|---|---|---|---|---|
|
Cedronski Michal
planecheck.com
|
$299,904 *
€ 255,000
|
Poland | May 03, 2026 | — | Active |
* Converted to USD at daily European Central Bank (ECB) exchange rates
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 172S
This 2001 Cessna 172S (SP-LAP) is a 4-seat single engine piston . There are currently 5 172S aircraft listed for sale with asking prices ranging from $299,904 to $401,436. This aircraft is priced below the market average at $299,904.
Operating costs: Fuel burn is 8.5 GPH (32 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $47/hr in fuel alone. Total variable cost including maintenance reserves is approximately $130/hr. Annual fixed costs (hangar, insurance, crew, annual inspection) average $18,000.
NTSB records show 0 incidents for this airframe — a clean safety record. There are 8 airworthiness directives 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 172S — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateCESSNA 172S
AeroGurus estimates based on industry averages for the CESSNA 172S. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
FAA registry covers US-registered aircraft (N-numbers).
This aircraft (SP-LAP) is registered outside the US.
Location & Ownership
Aircraft Location
Poland
PL
Seller reportedTitle 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 SP-LAP against the NTSB accident database.
Airworthiness Directives — Cessna 172S
ADs are mandatory safety instructions issued by the FAA. 8 recent ADs found for this aircraft type.
Cessna Aircraft Company Models 172R, 172S, 182T, T182T, 206H, and T206H Airplanes
View full AD →Cessna Aircraft Company Models 172R, 172S, 182S, 182T, T182T, 206H, and T206H Airplanes
View full AD →The Cessna Aircraft Company Models 172R, 172S, 182T, T182T, 206H, and T206H Airplanes
View full AD →Cessna Aircraft Company Models 172R, 172S, 182T, T182T, 206H, and T206H Airplanes
View full AD →The Cessna Aircraft Company Models 172R, 172S, 182T, and T182T Airplanes
View full AD →Cessna Aircraft Company Models 172R, 172S, 182S, 206H, and T206H Airplanes
View full AD →Source: FAA Airworthiness Directives database. Showing most recent ADs for this aircraft type.
Service Difficulty Reports — Cessna 172S
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
ENGINE WAS REPORTED RUNNING ROUGH, WAS FOUND TO HAVE A CRACK ON THE CYLINDER HEAD ON #4 CYLINDER. THE SAME PROBLEM WAS FOUND ON ANOTHER ENGINE, SAME TYPE AIRCRAFT, ENGINE AND CYLINDER.
UPON DISASSEMBLY FOR ITS FIRST OVERHAUL, DAMAGE WAS FOUND ON THE LEFT HAND CRANCASE TO ONE THRU STUD LOCATION. THE DAMAGE APPEARS TO BE A GOUGE WITH DISPLACED METAL JUST UNDER THE CYLINDER PAD INSIDE THE THRU STUD BORE. SIMILAR DAMAGE ON OTHER ENGINE...
UPON DISASSEMBLY FOR IT'S FIRST OVERHAUL, DAMAGE WAS FOUND ON ONE OF THE THRU STUDS. THE DAMAGE APPEARS TO BE DISPLACED STEEL UNDER THE THREADED PORTION ON THE SHOULDER OF THE THRU STUD. THE DAMAGE IS MINOR BUT DUE TO THE SIMILAR LOCATION AND SEVERIT...
UPON DISASSEMBLY FOR ITS FIRST OVERHAUL, DAMAGE WAS FOUND ON THE LEFT HAND CRANCASE TO ALL 4 THRU STUD LOCATIONS. THE DAMAGE APPEARS TO BE A GOUGE WITH DISPLACED METAL JUST UNDER THE CYLINDER PAD INSIDE THE THRU STUD BORE. ON THREE OF THE THRU STUD B...
UPON DISASSEMBLY FOR IT'S FIRST OVERHAUL, DAMAGE WAS FOUND ON 2 OF THE THRU STUDS. THE DAMAGE APPEARS TO BE DISPLACED STEEL UNDER THE THREADED PORTION ON THE SHOULDER OF THE THRU STUD. THE DAMAGE IS MINOR BUT DUE TO THE SIMILAR LOCATION AND SEVERITY ...
THIS IS TO REPORT POSSIBLE DEFECTS IN PN 259-P-04. THE AIRCRAFT DRAIN PLUGS WERE LOCATED ON THE DRAIN TEE FOR THE GDC74A. A POSSIBLE FAULT COULD BE THE INSTALLATION. WHILE THE AIRCRAFT HAS NOT HAD THE PITOT OR STATIC SYSTEMS LEAKED CHECK SINCE T...
UPON DISASSEMBLY FOR ITS FIRST OVERHAUL, DAMAGE WAS FOUND ON THE LEFT HAND CRANCASE TO ALL 4 THRU STUD LOCATIONS. THE DAMAGE APPEARS TO BE A GOUGE WITH DISPLACED METAL JUST UNDER THE CYLINDER PAD INSIDE THE THRU STUD BORE. IN ADDITION, 1 OF THE THRU ...
UPON DISASSEMBLY FOR IT'S FIRST OVERHAUL, DAMAGE WAS FOUND ON 1 OF THE THRU STUDS. THE DAMAGE APPEARS TO BE DISPLACED STEEL UNDER THE THREADED PORTION ON THE SHOULDER OF THE THRU STUD. THE DAMAGE IS MINOR BUT DUE TO THE SIMILAR LOCATION AND SEVERITY ...
WE HAVE NOTICED A TREND IN (STAINLESS STEEL) AILERON CABLE WEAR ON RH AILERON CROSSOVER CABLE P/N: 0510106-365 AT FAIRLEAD P/N 0560065-2 RH WING STATION 57.68. ON OUR AIRCRAFT, N172HG 172S S/N 11139 TT: 7109.8, THE CABLE HAS FRAYED WIRES DUE TO WEARI...
WE HAVE NOTICED A TREND IN (STAINLESS STEEL) AILERON CABLE WEAR ON RH AILERON CROSSOVER CABLE P/N 0510106-365 AT FAIRLEAD P/N 0560065-2 RH WING STATION 57.68. ON OUR AIRCRAFT, N9347T 172S S/N 11166 TT: 6524, THE CABLE HAS FRAYED WIRES DUE TO WEARING ...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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