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Aircraft record

N5755P1959 Piper PA-24-250

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Jul 19, 2022.

Safety record in brief:1 NTSB accident (substantial damage, Nov 1993)3 ADs may apply1 service difficulty report

Registration
Deregistered
Last based in
Albuquerque, NM
owner city / state
Owners
1
since 2016
NTSB events
1
substantial, 1993
ADs may apply
3
confirm with A&P
Service reports
1
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Sky West Aviation INC Trustee
Owner type
Corporation
City, state
Albuquerque, NM
Certificate issued
Jun 22, 2016
Canceled
Jul 19, 2022
Airworthiness
Standard · Normal
Airworthiness date
Mar 10, 1959

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-24-250
Year
1959
Serial number
24-831
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
A76411

Engine

Make and model
Lycoming 0-540 Series
Type
Reciprocating
Power
250 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. 2016 – 2022Sky West Aviation INC TrusteeAlbuquerque, NM

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

Nov 21, 1993 · Labelle, FL

THE PILOT-IN-COMMAND EXCEEDING THE STRUCTURAL LIMITS OF THE AIRPLANE'S DESIGN LIMITS BY IN-FLIGHT OVER-STRESS THAT RESULTED IN DAMAGE TO THE GEAR EXTENSION SYSTEM, FUSELAGE AND CONTROL SURFACES.

Damage
Substantial
Injuries
None
Report
MIA94LA026

From NTSB records; matched by serial number.Read NTSB report (search CAROL for MIA94LA026)

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-24-250)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-24-250)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-24-250)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.

  • Landing gear · control cable · bentJan 20, 2019

    UPON TOUCH DOWN ON KMFE RUNWAY, RIGHT MAIN GEAR SLOWLY STARTED TO COLLAPSE. PILOT REACHED A FULL STOP SAFELY, ON FURTHER INVESTIGATION THE RIGHT SIDE MAIN GEAR CONTROL CABLE WAS FOUND BENT KEEPING THE GEAR FROM COMPLETELY EXTENDING TO THE DOWN AND LOCK POSITION.

    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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