1967 Cessna 172
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
Sportsman STOL leading edge kit dramatically increases the efficiency of the Cessna wing & enhances aircraft performance & safety. SP-STOL
FAA STC SA2256WE.The Sportsman STOL wing cuff is a state of the art modification originally designed by Lockheed Skunkworks to increase light plane utility & safety by increasing the wings efficiency & resistance to stalls & spins. The Sportsman STOL is not just a lip on the bottom
but is a re-engineered airfoil. The aim of the Sportsman STOL modification is to improve aerodynamics & enhance aircraft performance & safety. Kit includes: Leading edge skins
aileron gap seals (for applicable models) landing light cover assembly hardware & fiberglass wing tips. Micro Aerodynamics Vortex Generators FAA STC SA00831SE Knots To U Ailerons & Flaps Gap Seals FAA STC SA2382NM Taxi & Landing Lights on left wing leading edge Camera hole Opening rear side windows for aerial photography Tail hook for banner or glider towing (Currently Removed) Rosen Sun Visors Pilots Shoulder Harness Seat belts Covers for windows area Wheel Pants Interior Blue seats and side panels & green carpet recently refurbished in very good condition Exterior White end blue old but in good condition Remarks Annual Inspection completed 02/2025 at TT: 3398 hrs Aircraft in compliance with Cessna SID MTOW: 1045 kg Empty Weight: 656 kg (1442 Lbs) Weighed 14/03/2019 Fuel Capacity: 136 Liters (39 USG / Usable 36 USG) Average Consumption: 7 USG per Hour Specifications subject to verification by purchaser Aircraft subDescription
Airframe
Serial Number: 361
Total Time: 3430 hrs
Engine
Type: Continental 6 Cylinder O-300-D, 145 brake horsepower at 2700 RPM
S/N: 30-R-310
TSOH: 291 hrs
Overhauled: March 2007
TBO: 1800 hours
Propeller
Type2 Bladed, Metal, Fixed Pitch Propeller McCauley IC172/EM7653
S/N: 78245
TSOH: 304 hrs
Overhauled: 02/2019
Avionics
King KMA12 Audio Panel / Marker Beacon
TQ KRT2, 760 Channels, 6W, 8.33 VHF COM
King KX175 NAV-COM
King KI208 NAV VOR LOC Indicator
Sigtronic Intercom
Garmin GTX330 Transponder S
ACK A30 Altitude Encoder
ACK E-01 ELT with remote switch on instrument panel
Options
Nav Lights
Autofuel (MOGAS) STC
Stene Aviation Wings Leading Edge Cuffs & Aileron Gap Covers, Sportsman STOL leading edge kit dramatically increases the efficiency of the Cessna wing & enhances aircraft performance & safety. SP-STOL, FAA STC SA2256WE.The Sportsman STOL wing cuff is a state of the art modification originally designed by Lockheed Skunkworks to increase light plane utility & safety by increasing the wings efficiency & resistance to stalls & spins. The Sportsman STOL is not just a lip on the bottom, but is a re-engineered airfoil. The aim of the Sportsman STOL modification is to improve aerodynamics & enhance aircraft performance & safety. Kit includes: Leading edge skins, aileron gap seals (for applicable models), landing light cover assembly, hardware & fiberglass wing tips.
Micro Aerodynamics Vortex Generators FAA STC SA00831SE
Knots To U Ailerons & Flaps Gap Seals, FAA STC SA2382NM
Taxi & Landing Lights on left wing leading edge
Camera hole
Opening rear side windows for aerial photography
Tail hook for banner or glider towing (Currently Removed)
Rosen Sun Visors
Pilots Shoulder Harness Seat belts
Covers for windows area
Wheel Pants
Interior
Blue seats and side panels & green carpet, recently refurbished, in very good condition
Exterior
White end blue, old but in good condition
Remarks
Annual Inspection completed 02/2025 at TT: 3398 hrs
Aircraft in compliance with Cessna SID
MTOW: 1045 kg
Empty Weight: 656 kg (1442 Lbs)
Weighed 14/03/2019
Fuel Capacity: 136 Liters (39 USG / Usable 36 USG)
Average Consumption: 7 USG per Hour
Specifications subject to verification by purchaser
Aircraft subject to withdrawal from the market at any time & without notice
Engine
Type: Continental 6 Cylinder O-300-D, 145 brake horsepower at 2700 RPM S/N: 30-R-310 TSOH: 291 hrs Overhauled: March 2007 TBO: 1800 hours Propeller Type2 Bladed, Metal, Fixed Pitch Propeller McCauley IC172/EM7653 S/N: 78245 TSOH: 304 hrs Overhauled: 02/2019 Avionics King KMA12 Audio Panel / Marker Beacon TQ KRT2, 760 Channels, 6W, 8.33 VHF COM King KX175 NAV-COM King KI208 NAV VOR LOC Indicator Sigtronic Intercom Garmin GTX330 Transponder S ACK A30 Altitude Encoder ACK E-01 ELT with remote switch on instrument panel Options Nav Lights Autofuel (MOGAS) STC Stene Aviation Wings Leading Edge Cuffs & Aileron Gap Covers, Sportsman STOL leading edge kit dramatically increases the efficiency of the Cessna wing & enhances aircraft performance & safety. SP-STOL, FAA STC SA2256WE.The Sportsman STOL wing cuff is a state of the art modification originally designed by Lockheed Skunkworks to increase light plane utility & safety by increasing the wings efficiency & resistance to stalls & spins. The Sportsman STOL is not just a lip on the bottom, but is a re-engineered airfoil. The aim of the Sportsman STOL modification is to improve aerodynamics & enhance aircraft performance & safety. Kit includes: Leading edge skins, aileron gap seals (for applicable models), landing light cover assembly, hardware & fiberglass wing tips. Micro Aerodynamics Vortex Generators FAA STC SA00831SE Knots To U Ailerons & Flaps Gap Seals, FAA STC SA2382NM Taxi & Landing Lights on left wing leading edge Camera hole Opening rear side windows for aerial photography Tail hook for banner or glider towing (Currently Removed) Rosen Sun Visors Pilots Shoulder Harness Seat belts Covers for windows area Wheel Pants Interior Blue seats and side panels & green carpet, recently refurbished, in very good condition Exterior White end blue, old but in good condition Remarks Annual Inspection completed 02/
Propeller
McCauley IC172/EM7653
Interior
Blue seats and side panels & green carpet, recently refurbished, in very good condition Exterior White end blue, old but in good condition Remarks Annual Inspection completed 02/2025 at TT: 3398 hrs Aircraft in compliance with Cessna SID MTOW: 1045 kg Empty Weight: 656 kg (1442 Lbs) Weighed 14/03/2019 Fuel Capacity: 136 Liters (39 USG / Usable 36 USG) Average Consumption: 7 USG per Hour Specifications subject to verification by purchaser Aircraft subject to withdrawal from the market at any time & without notice
Exterior
White end blue, old but in good condition Remarks Annual Inspection completed 02/2025 at TT: 3398 hrs Aircraft in compliance with Cessna SID MTOW: 1045 kg Empty Weight: 656 kg (1442 Lbs) Weighed 14/03/2019 Fuel Capacity: 136 Liters (39 USG / Usable 36 USG) Average Consumption: 7 USG per Hour Specifications subject to verification by purchaser Aircraft subject to withdrawal from the market at any time & without notice
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 |
|---|---|---|---|---|---|---|
|
Stefano Scossa
avpay.aero
|
$86,202
$85,803
|
Italy | Mar 21, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 172
This 1967 Cessna 172 (SP-STOL) is a 4-seat single engine piston with 3,430 hours on the airframe. There are currently 115 172 aircraft listed for sale with asking prices ranging from $42,460 to $395,000. This aircraft is priced below the market average at $86,202.
The 172 cruises at 122 kts (226 km/h) with a range of 640 nm (1,185 km) — ideal for short hops and local flights. Service ceiling of 14,000 ft allows operation above most weather.
Operating costs: Fuel burn is 8.6 GPH (33 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. With 3,430 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. There are 10 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 172 — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateCESSNA 172
AeroGurus estimates based on industry averages for the CESSNA 172. 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-STOL) is registered outside the US.
Location & Ownership
Aircraft Location
Italy
IT
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-STOL against the NTSB accident database.
Airworthiness Directives — Cessna 172
ADs are mandatory safety instructions issued by the FAA. 10 recent ADs found for this aircraft type.
Cessna Aircraft Company 120, 140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 206, P206, U206, TP206, TU206, 207, T207, 210, T210, 336, 337, and T337 Series Airplanes
View full AD →Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190, 195, 206, 207, 210, T303, 336, and 337 Airplanes
View full AD →Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type Certificate (STC) SA01303WI
View full AD →Cessna Aircraft Company (Cessna) 172, 175, 177, 180, 182, 185, 206, 207, 208, 210, 303, 336, and 337 Series Airplanes
View full AD →Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series Airplanes
View full AD →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 →Source: FAA Airworthiness Directives database. Showing most recent ADs for this aircraft type.
Service Difficulty Reports — Cessna 172
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
UNDER NORMAL FLIGHT OPERATIONS, AT FIRST ROUTINE 500-HOUR INSPECTION FOUND COIL TAB WORN OUT OF LIMITS BECAUSE THE TAB WAS INCORRECTLY BEND AT FACTORY.
POSITION # 1 &2 CYLINDER EXHAUST PORT CRACK FROM THE INBOARD EXHAUST STUD EXTENDING TO THE BACK OF THE PORT. CRACK VISIBLE THROUGH THE FINS. SUPERIOR CYLINDERS PN: SL32006W-A1 SERIAL NUMBER 326W000003625 & 326W000003623.
FOUND FORWARD PROPELLER BULKHEAD P/N 0550321-4 CRACKED AT ONE BOLT HOLE LOCATION.
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 ...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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