1967 Cessna 172H
Single Engine Piston
Equipment & Features
- Seats
- 4
Aircraft Details
Seller reportedDescription
Highlights: NO RESERVE AUCTION! October Annual Affordable Time-Builder or Private Flyer For logbooks, more images, and to register to bid, visit: https://bids.airspaceauctions.com/Listing/828677 | Interior: (8) All photos (20) Price: Inquire Posted: 3 months ago Views: 266 Share Contact seller Ferry & Delivery Click Tap to get a quick and easy quote Make Cessna Model 172 Skyhawk Year 1967 Seller AirSpaceAuctions Contact Seller type Broker Location Cisco, TX, United States Condition Pre-owned Total Time 6100 h Engine Time 1340 h Undercarriage Tricycle Seats 4 Flight Rules VFR Day Serial Number 17255841 Registration N2641L | Known Flaws: Gaps/missing Logbooks: Missing before 1979 Known Flaws: Sat outside for a while so paint condition 5/10 with some touch up done. Known Corrosion: A couple of spots on the elevator, but have been addressed. Slight, typical surface corrosion on wings. | Maintenance: Airworthiness Until 10/31/2026
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 |
|---|---|---|---|---|---|---|
|
AirSpaceAuctions Contact
winglist.aero
|
Contact for Price
|
Cisco | May 03, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 172H
This 1967 Cessna 172H (N2641L) is a 4-seat single engine piston with 6,100 hours on the airframe.
The 172H 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 6,100 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 172H — 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 registration data pending for N2641L.
Location & Ownership
Aircraft Location
Cisco
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 database checked for N2641L.
Service Difficulty Reports — Cessna 172H
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
CYL €¢3 DEVELOPED/, CRACK IN THE CYLINDER HEAD BETWEEN COOLING FINS IIPPROXIMATEL Y 1 625 INCHED ABOVE LOWEST FINE AT HE/ID/ 81\RREL ATTACHMENT. IOCIITED IN LOWER CORNEER EDGE OF CLINDER HEAD ON INTAKE VALVE SIDE. PILOT NOFLCED CYL HEAD !HIP RISIN...
ROTATING SHAFT FOR ROTATING MAGNET. SHAFT BROKEN AT AFT FLANGE WHERE MAGNET IS PRESSED ON. FWD AND AFT BEARING ARE STILL GOOD. OIL IN MAG DUE TO SLOPE IN SHAFT. DUE TO THE WAY THE SHAFT WAS BROKEN THE MAGNETO STILL TRY TO FUNCTION.
(CAN) DURING A FLOATS TO WHEELS CHANGE OVER, A RIGID FUEL LINE WAS DISCOVERED CHAFED THRU 98 PERCENT OF THE WALL THICKNESS. THE CHAFE MEASURED 1" LONG BY .3750" LONG. THE LINE WAS THE MAIN ENGINE FUEL FEED LINE FROM THE FUEL SELECTOR VALVE TO THE FI...
THE CAM FOR THE MAGNETO WAS FOUND TO BE NON UNIFORM IN SHAPE. AFTER INSTALLATION OF THIS PART THE POINT GAP WAS DIFFERENT ON EACH CAM LOBE.
(CAN) DURING A ROUTINE INSP THERE WAS SOME PLAY FOUND IN RUDDER HINGES AND AFTER A CLEANING AND CLOSE VISUAL INSP THERE WAS A CRACK OBSERVED IN THE LWR HINGE BRACKETS BOTH THE UPPER AND LOWER BRACKETS PN 0531018-1 AND 0531018-2. THE BRACKETS WERE REP...
PROP SPINNER FWD, BULKHEAD CRACKED NEAR MOUNT BOLTS. PART PROBABLY NOT STURDY. RECOMMEND PART BE MADE OF THICKER METAL DOUBLER INSTALLED. ALSO, IT APPEARED THAT MOUNT BOLT HOLES MAY BE TOO LARGE. (K)
ROCKER COVERS REMOVED DURING 100 HOUR INSPECTION TO INSPECT INTAKE AND EXHAUST ROCKERS FOR CORRECT INSTALLATION. FOUND NR1 AND NR6 CYLINDERS HAD INTAKE ROCKER (P/N 639614) INSTALLED IN THE EXHAUST VALVE POSITION. PARTS MANUAL CALLS FOR P/N 639615 ROC...
PILOT REPORTED LOSS OF POWER (600 RPM DROP) SIGNIFICANT ENGINE ROUGHNESS DURING CLIMB. ENGINE RECOVERED SHORTLY AFTERWARDS. PILOT ELECTED TO CONTINUE AND HAD SAME PROBLEM AGAIN DURING CRUISE FLIGHT. ENGINE RECOVERED ON ITS OWN ONCE AGAIN. PILOT SAID ...
LEFT WING FUEL GAGE REGISTERED EMPTY. UPON INSPECTION OF THE FLOAT ASSEMBLY, FOUND FLOAT TO BE ONE THIRD FULL OF FUEL. METAL FLOAT HAS MULTIPLE PIN HOLES. RIGHT SIDE WAS FINE - NO LEAKS.
DURING NEWLY OVERHAULED ENGINE INSTALLATION AN OIL LEAK WAS DISCOVERED. WHEN BREAK-IN OIL WAS ADDED TO OIL SUMP FOR INITIAL ENGINE RUN, OIL WAS OBSERVED LEAKING ONTO NOSE TIRE. FURTHER EXAMINATION REVEALED OIL LEAK WAS ORIGINATING FROM LEFT REAR OF...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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