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Aircraft record

N9360PPiper PA-24-260

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Aug 14, 2023.

Safety record in brief:1 NTSB accident (substantial damage, Feb 2018)3 ADs may apply1 service difficulty report

Registration
Deregistered
Engine
TI0-540 SER · 310 hp
Lycoming
Owners
1
on record
NTSB events
1
substantial, 2018
ADs may apply
3
confirm with A&P
Service reports
1
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Individual owner
Canceled
Aug 14, 2023
Airworthiness
Standard · Normal
Airworthiness date
Jul 11, 1969

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
Serial number
24-4860
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
ACFE59

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. until 2023Individual owner

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (1)

Accident · substantial damage

Feb 8, 2018 · Fargo, ND

The pilot's failure to use the published emergency procedures to manually extend the landing gear when an electrical failure precluded normal extension of the landing gear, resulting in the gear collapse during landing. Contributing to the accident was the pilot’s failure to ensure, before takeoff, that the battery was fully charged after its depletion due to a faulty alternator.

Damage
Substantial
Injuries
None
Report
CEN18LA097

From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN18LA097)

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 (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.

  • Fuel · motor · burned outJun 6, 2012

    ELECTRIC FUEL PUMP FAILED AND CAUSED SMOKE AND BURNING SMELL IN AIRCRAFT. FUEL PUMP IS LOCATED BELOW CO-PILOT FEET FLOOR PANELS. PUMP HAD 27.2 TOTAL AIRFRAME HOURS OF OPERATION SINCE O/H. CURRENT FLIGHT WAS PATTERN WORK, WHERE PUMP WAS LEFT ON FOR ABOUT 30 MINUTES. THIS PUMP WAS RECENTLY OVERHAULED.

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

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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