1966 Cessna 150F
Single Engine Piston
Equipment & Features
- Seats
- 2
Aircraft Details
Seller reportedDescription
Airframe The airframe is solid and straight, no corrosion. Almost every cable, component, and piece of hardware for the control surfaces were just recently replaced during the annual.
Engine
Continental o200 with 1080 (approx) SMOH. Plane is flown regularly so times will go up.
Propeller
The airframe is solid and straight, no corrosion. Almost every cable, component, and piece of hardware for the control surfaces were just recently replaced during the annual.
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 |
|---|---|---|---|---|---|---|
|
Listing Source
trade-a-plane.com
|
$35,000
|
Michigan, MI | May 05, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 150F
This 1966 Cessna 150F (N8226F) is a single engine piston with 4,500 hours on the airframe. There are currently 10 150F aircraft listed for sale with asking prices ranging from $35,000 to $67,000. This aircraft is priced below the market average at $35,000.
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
Ownership & Registration
FAA registration data pending for N8226F.
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 N8226F against the NTSB accident database.
Service Difficulty Reports — Cessna 150F
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
TEST, TEST, TEST - AC LANDED SHORT OF RUNWAY AFTER ENGINE QUIT. AC HAD SUBSTANTIAL DAMAGE NO INJURIES. DETERMINED AC RAN OUT OF FUEL DUE TO FAULTY FUEL GUAGE. REMOVED FUEL QUANTITY TRANSMITTER FOR FUNCTIONAL TESTING. FOUND TWO RUB SPOTS ON FLOAT,...
TOOKOFF ON RUNWAWY ALL PARAMETERS WERE NORMAL. AIRSPEED, RATE OF CLIMB, AND OIL PRESSURE PREFORMANCE CHECK GOOD. AFTER PASSING BETWEEN 1000 TO 1200 FEET, I SAW THE ENGINE HESITATED APPROXIMATELY 1 TO 2 SECONDS. AFTER THAT, THE ENGINE CUT OFF. PERFORM...
ELT ACTIVATED WITHOUT ANY LOAD PLACED ON AIRCRAFT AT 3:21AM,FEB 5,2021 AIRCRAFT WAS IN HANGAR HAVING ANNUAL ACCOMPLISHED. WORK ON AIRCRAFT STOPPED FOR THE DAY AT 4:30PM ON FEB 4,2021,THE DAY PRIOR. AFCC TRIED TO CALL OWNER AT 3:30AM FEB5 BUT OWNER ...
POST ACCIDENT INSPECTION OF THE NOSE GEAR STEERING ASSY SHOWED THAT THE BEARING ROD END WAS BROKEN AT THE NUT. THE COLORING AT THE FRACTURE WAS 1 QUARTER SHINY AND 3 QUARTERS DULL DARK GREY. BOTH THE LT AND RT ROD ENDS FRACTURED UPON LANDING.
FOUR NEW CYLINDER ASSEMBLIES WERE INSTALLED. AFTER GROUND RUNS AND 1 BREAK IN FLIGHT THE ENGINE WAS INSPECTED. DURING THE INSPECTION THE PUSHROD TUBE SEAL WERE FOUND TO HAVE LARGE CRACKS AND SPLITS. THE SEALS AND GASKETS WERE SUPPLIED WITH THE CYL...
DURING ANNUAL INSP, FOUND ELEVATOR BELLCRANK PN 0411258 WITH A BEARING THAT CAME LOOSE FROM IT'S SWAGED MOUNTING. THE ONLY THING THAT KEPT IT FROM FALLING OUT COMPLETELY WAS THE FORK ROD THAT CONNECTS TO THE CONTROL COLUMN. ONCE THIS ROD WAS REMOVE...
ON TAKEOFF ROLL, LT FWD NOSE STEERING ROD END FAILED ALLOWING NOSE GEAR TO TURN FULL LT RESULTING IN LOSS OF CONTROL OF ACFT. ACFT DEPARTED RUNWAY EDGE AND FLIPPED OVER CAUSING SUBSTANTIAL DAMAGE.
DURING COMPLIANCE OF AD 2004-19-06, DETECT AND CORRECT FATIGUE CRACKING OR CORROSION OF THE FAIL SAFE STRAPS (S/B 767-53A0100) A CRACK WAS FOUND IN BOTH SIDES. THE RT T-FITTING WAS CRACKED FROM THE FWD SIDE OF THE BOLT HOLE APPROXIMATELY 22 DEGREES ...
DURING DAILY PREFLIGHT INSPECTION RUBBING SOUNDS HEARD UNDER CABIN FLOOR WHEN MOVING CONTROL YOLK LEFT AND RIGHT (ROLL AXIX). INVESTIGATION OF SOUND REVEALED THAT TWO SCREWS (P/N S1021Z8-10) HOLDING STAINLESS STEEL SCUFFBOARD PLATE (P/N 04130264-4) ...
SEAT PAN WAS FOUND CRACKED AT THE FORWARD END OF PILOTS OB SEAT RAIL STIFFENER, APPROXIMATELY 1 NR LONG ACROSS SCREW HOLES. STIFFENER PN 0411546-1 WAS ALSO CRACKED AT CUTOUT FOR FUEL LINE. TOTAL AIRFRAME TIME UNKNOWN, BUT GREATER THAN 1300 HOURS. THE...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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