We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type data
Airframe
Manufacturer
Cessna
Model
172N
Year
1976
Serial number
17268069
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
4
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
AA3EA0
Engine
Make and model
Lycoming 0-320 Series
Type
Reciprocating
Power
180 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records
until 2012Individual ownerXxx, OK
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 2026 · SDRs · Oct 16, 2026
NTSB events (2)
Accident · substantial damage
Mar 24, 2000 · Maud, OK
the loss of engine power while maneuvering as a result of the separation of the exhaust rocker arm retaining stud due to fatigue, which resulted in a precautionary landing.
THE ACFT COLLIDED WITH A FENCE DURING A FORCED LANDING AFTER THE ENGINE QUIT. THE PLT WAS DESCENDING FROM AIRWORK AT 10800 FT MSL TO RETURN TO THE ARPT. THE ENGINE WAS REDUCED TO IDLE AND THE CARBURETOR HEAT WAS ON BUT THE ENGINE WOULD NOT RESPOND WHEN THE THROTTLE WAS ADVANCED. EMERGENCY PROCEDURES WERE INTITATED AND A LANDING SITE CHOSEN. THE DIRT ROADCHOSEN HAD A CROSSWIND SO AN ALTERNATE…
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (1)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
Reciprocating engine · rocker boss · failedMar 24, 2000
VALVE ROCKER RETAINING STUD, PN 31-16, SHEARED FLUSH WITH THE CYL HEAD SURFACE. THIS CAUSED PARTS TO MOVE AROUND AT RANDOM IN THE HEAD. IT IS SUSPECTED THESE LOOSE PARTS INTERFERRED WITH OPER OF INTAKE VALVE MECHANISM CAUSING THE INTAKE PUSH ROD TO BEND, CREATING AN OIL LEAK AT THE PUSH ROD…
From FAA Service Difficulty Reports; matched by N-number and serial number.