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Aircraft record

N801PC1965 Piper PA-24-260

Registration validUnclaimedSource: FAA, updated Oct 17, 2026

Safety record in brief:No NTSB accidents or incidents since 19823 ADs may apply2 service difficulty reports

Registration
Valid
expires Oct 31, 2029
Based in
Palacios, TX
owner city / state
Engine
TI0-540 SER · 310 hp
Lycoming
Owners
1
since 2009
NTSB events
None
since 1982
ADs may apply
3
confirm with A&P
Service reports
2
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Registered owner
Individual owner
City, state
Palacios, TX
Certificate issued
Mar 10, 2009
Expires
Oct 31, 2029
Airworthiness
Standard · Normal
Airworthiness date
Jul 8, 1965

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
Piper
Model
PA-24-260
Year
1965
Serial number
24-4256
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
AAE6DC

Engine

Make and model
Lycoming Ti0-540 Ser
Type
Reciprocating
Power
310 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2009 – nowIndividual ownerPalacios, TX · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 16, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (3)

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.

ADSubjectEffectiveApplies to
2012-17-06Flight ControlsOct 22, 2012Airframe (PA-24-260)Certain serial numbers: PA-24 24-1–24-3687; PA-24-250 24-1; PA-24-250 24-103–24-3687; PA-24-260 24-3642; PA-24-260 24-4000–24-5034. Only with: Horn P/N 20397-00 (assembly P/N 20399) installed.
99-05-09The New Piper Aircraft, Inc. PA-23, PA- 24, PA-28, PA-32, and PA-34 Series AirplanesMar 19, 1999Airframe (PA-24-260)Certain serial numbers: PA-23-235 27-505–27-622; PA-23-250 27-01–27-2504; PA-24-180 24-103–24-3687; PA-24-250 24-103–24-3687; PA-24-260 24-3642; PA-24-260 24-4000–24-5028; …. Only with: Equipped with Purolator air filter P/N 638873, Model CA161PL, or Piper P/N 460-632 (PS60007-2).
97-01-01 R1The New Piper Aircraft, Inc. PA-24, PA- 28R, PA-30, PA-32R, PA-34, and PA-39 Series…Dec 8, 1998Airframe (PA-24-260)Certain serial numbers: PA-28R-180 28R-30002–28R-31135; PA-28R-180 28R-7130001–28R-7130013; PA-28R-200 28R-35001–28R-35820; PA-28R-200 28R-7135001–28R-7635539; PA-28R-201 28R-7737002–28R-7737096; PA-28R-201T 28R-7703001–28R-7703239; …. Only with: All serials of PA-24, PA-24-250, PA-24-260, PA-24-400, PA-30, PA-39; PA-28R, PA-32R, PA-34 models (all serials of PA-34-200) only if not equipped with Piper P/N 78717-02 (or FAA-approved equivalent) main gear sidebrace stud in both main gear sidebrace bracket assemblies.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (2)

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.

  • Flight controls · bellcrank · crackedDec 19, 2003

    DURING ANNUAL INSPECTION, A CRACK WAS FOUND IN THE BELLCRANK BOLT HOLE. ON CLOSER INSPECTION IT WAS FOUND THAT ALL FOUR BOLT HOLES HAD CRACKS IN VARIOUS STAGES OF PROGRESSION. THE CRACKS BEGIN AT THE END OF THE PART AND PROCEED TOWARDS THE BOLT HOLE, ONLY ONE HAS MADE IT ALL THE WAY TO THE BOLT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · bracket · crackedDec 19, 2003

    DURING RUDDER REMOVAL FOR REQUIRED MAINTENANCE, A CRACK WAS FOUND IN MIDDLE RUDDER HINGE BRACKET MOUNTED ON THE VERTICAL FIN. THE CRACK IS AT THE HINGE BEARING HOLE. DUE TO THE LOCATION, THIS CRACK WOULD NOT HAVE BEEN VISIBLE WITHOUT REMOVING THE RUDDER FIRST. THIS AIRCRAFT HAS SPEED MODS AND IS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 16, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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