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Aircraft record

N5800U1967 Piper PA-28-140

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled May 26, 2020.

Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Dec 2018)5 ADs may apply1 service difficulty report

Registration
Deregistered
Last based in
Chino, CA
owner city / state
Owners
1
since 2009
NTSB events
2
substantial, 2018
ADs may apply
5
confirm with A&P
Service reports
1
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Dubois Aviation INC
Owner type
Corporation
City, state
Chino, CA
Certificate issued
Jun 1, 2009
Canceled
May 26, 2020
Airworthiness
Standard · Normal, Utility
Airworthiness date
Jul 26, 1967

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-28-140
Year
1967
Serial number
28-23502
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
A77853

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
  1. 2009 – 2020Dubois Aviation INCChino, CA

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 (2)

Accident · substantial damage

Dec 12, 2018 · Chino, CA

The flight instructor's failure to maintain directional control during landing.

Damage
Substantial
Injuries
None
Report
GAA19CA095

From NTSB records; matched by serial number.Read NTSB report (search CAROL for GAA19CA095)

Accident · substantial damage

Dec 10, 2010 · Chino, CA

Fatigue cracking of the upper torque-link attach lugs on the left main landing gear strut, which resulted in separation of the left main landing gear during taxi.

Damage
Substantial
Injuries
None
Report
WPR11LA074

From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR11LA074)

Accident history for this model

ADs published since 1998 that may apply (5)

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
2018-07-03Placard and MarkingsApr 20, 2018Airframe (PA-28-140)Serial numbers per Table 1 to paragraph (c) of this AD
2013-02-13Stabilizer Control SystemMar 11, 2013Airframe (PA-28-140)
2010-15-10Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series AirplanesAug 31, 2010Airframe (PA-28-140)Certain serial numbers: PA-28-140 28-20001–28-26946; PA-28-140 28-7125001–28-7725290; PA-28-150 28-03; PA-28-150 28-1–28-4377; PA-28-150 28-1760A; PA-28-160 28-03; …
99-05-09The New Piper Aircraft, Inc. PA-23, PA- 24, PA-28, PA-32, and PA-34 Series AirplanesMar 19, 1999Airframe (PA-28-140)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).
95-26-13The New Piper Aircraft, Inc. (Formerly Piper Aircraft Corporation) PA28 and PA32 Series…Feb 5, 1996Airframe (PA-28-140)Only with: Equipped with oil cooler hose assemblies that do not meet TSO-C53a, Type D requirements.

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 · strut · failedDec 10, 2010

    AFTER LANDING ON 12/10/2010, THE UPPER LINK ATTACH POINT FAILED ON THE MLG STRUT CLYLINDER, PN 65319-002. THIS FAILURE CAUSED THE OLEO STRUT TO BE EJECTED FROM THE CYLINDER CAUSING MAJOR DAMAGE TO ACFT. SB 1311 ADDRESSES THIS ISSUE.

    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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