1964 Cessna 172
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
BTHGTN 650 GTN 430 (non-WAAS) GMA 345 audio panel Appareo Stratus transponder (ADS-B IN/Out) Overhauled DG installed 2025
Description
1964 172E VFR/IFR trainer with 25 SMOH engine, 5326 TT, GTN 650/430 (non-WAAS). Interior completely replaced except for seats. Based in Crossville, Tennessee.
Engine
Continental O-300D. Engine overhauled by Don George Aircraft out of Florida. Crank and cases both came back as meeting specs so those were reused. Engine has been run for 25 hours since installation and mineral oil has been replaced with conventional oil with no metal noted. Engine also has a remote oil cooler; see photos. Generator was removed 2018 and replaced with an alternator. Has the MOGAS STC but I've never bothered using it.
Propeller
Very straight and true airframe. I purchased it from an American Airlines Captain who purchased it from an A P/IA who owned it for about 25 years and took exceptional care of it. 39 gallons usable total fuel at 8 gph (conservative).
Interior
Selkirk interior plastics installed in 2019 along with a new headliner and new carpet. New upper stationary panel and lower stationary panels were installed in the last couple of years; when the lower was installed we also replaced all the fuses. The only thing we have not done to the interior is replace the seats. Don't know when it was last painted (originally it was White and Red with Gold accents) but the paint is a solid 8. It needs a good wash and wax in the photos (ran out of time) but will still polish nicely. There is one spot of hangar rash but they are on the plastic end caps so we never bothered to fix it. Been that way for about 6 years and we haven't noticed any sort of issue with it.
Description and equipment details provided by the seller. AeroGurus does not verify seller-provided information.
Price Comparison
| Source | Price | Location | Listed | Days on Market | Status | Action |
|---|---|---|---|---|---|---|
|
Adam Strachn
trade-a-plane.com
|
$130,000
|
Crossville, TN | Jul 06, 2026 | 15 days | Active |
Estimate Monthly Payment
Cessna 172 loan calculator
AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 172
This 1964 Cessna 172 (N5436T) is a 4-seat single engine piston with 5,326 hours on the airframe. There are currently 164 172 aircraft listed for sale with asking prices ranging from $10,000 to $395,000.
The 172 cruises at 118 kts (219 km/h) with a range of 520 nm (963 km) — ideal for short hops and local flights. Service ceiling of 15,100 ft allows operation above most weather.
Operating costs: Fuel burn is 8.5 GPH (32 L/h), which at current 100LL avgas prices (~$6.20/gal) means approximately $53/hr in fuel alone. With 5,326 hours on the airframe, this aircraft has exceeded TBO (1,800 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 Continental
AeroGurus estimates based on industry averages for the CESSNA 172 Continental. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
FAA registration data pending for N5436T.
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 N5436T 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.
Similar Aircraft for Sale
