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Aircraft record

N924PA1999 Piper PA-28-181

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Mar 6, 2021.

Safety record in brief:1 NTSB accident (substantial damage, Dec 2019)8 ADs may apply6 service difficulty reports

Registration
Deregistered
Last based in
Crystal, MN
owner city / state
Owners
1
on record
NTSB events
1
substantial, 2019
ADs may apply
8
confirm with A&P
Service reports
6
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Individual owner
City, state
Crystal, MN
Canceled
Mar 6, 2021
Airworthiness
Standard · Normal, Utility
Airworthiness date
Oct 25, 1999

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-28-181
Year
1999
Serial number
2843286
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
ACCE4C

Engine

Make and model
Lycoming O&Vo-360 Ser
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. until 2021Individual ownerCrystal, MN

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

Dec 23, 2019 · Chandler, AZ

The student pilot's loss of directional control during the landing roll, which resulted in a collision with a taxiway sign.

Damage
Substantial
Injuries
None
Report
WPR20CA052

From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR20CA052)

Accident history for this model

ADs published since 1998 that may apply (8)

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
2024-10-04Wing, Attach FittingsJun 6, 2024Airframe (PA-28-181)Serial numbers per Piper Service Bulletin No. 1413, dated April 9, 2024
2018-07-03Placard and MarkingsApr 20, 2018Airframe (PA-28-181)Serial numbers per Table 1 to paragraph (c) of this AD
2016-07-21Wing Ribs/BulkheadApr 26, 2016Airframe (PA-28-181)Certain serial numbers: PA-28-161 2842393–2842395; PA-28-181 2843769–2843775; PA-28-181 2843779–2843791; PA-28R-201 2844152; PA-28-161 2842010–2842392; PA-28-181 2843021–2843768; …
2013-02-13Stabilizer Control SystemMar 11, 2013Airframe (PA-28-181)
2010-15-10Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series AirplanesAug 31, 2010Airframe (PA-28-181)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; …
Show all 8 ADs
ADSubjectEffectiveApplies to
2004-14-12The New Piper Aircraft, Inc., Models PA-28-161, PA-28-181, PA-28R-201, PA-32R-301 (HP)…Aug 10, 2004Airframe (PA-28-181)Certain serial numbers: PA-28-161 2842026–2842180; PA-28-181 2843112–2843565; PA-28R-201 2844014–2844099; PA-32R-301 3246098–3246214; PA-32R-301T 3257028–3257327; PA-34-220T 3449042–3449292; …
99-05-09The New Piper Aircraft, Inc. PA-23, PA- 24, PA-28, PA-32, and PA-34 Series AirplanesMar 19, 1999Airframe (PA-28-181)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-28-181)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 (6)

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 · cylinder head · crackedOct 9, 2018

    DURING A SCHEDULED INSPECTION, EXCESS OIL WAS OBSERVED ON THE COOLING FINS ABOVE THE EXHAUST FLANGE, ATTEMPTED TO FIND SOURCE OF OIL BUT NO SOURCE WAS VISIBLE, ROCKER COVER WAS REMOVED AS WELL AS THE EXHAUST ROCKER ARM AND PUSH ROD AND TUBE, A DYE CHECK WAS DONE AND A CRACK WAS LOCATED ON THE O/B…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · channel · crackedJun 4, 2018

    DURING AN INSPECTION, BOTH HAT CHANNELS IN THE RIGHT WING WERE FOUND TO BE CRACKED AT THE INBD END,

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bracket · crackedNov 23, 2016

    WHEN THE ELT WAS BEING REMOVED FOR INSPECTION, THE TECH DISCOVERED TWO 2" CRACKS NEXT TO THE NUTPLATES IN THE ELT MOUNTING BRACKET. THESE CRACKS CAN ONLY BE SEEN WHEN THE ELT TRAY IS REMOVED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 6 reports
  • Engine oil · oil cooler · leakingJun 22, 2015

    THE ACFT HAD LANDED AND WAS BEING PUT AWAY WHEN THE PILOTS NOTED THERE WAS OIL LEAKING FROM UNDER THE LT SIDE OF THE COWLING; THE LEAK TRAVELED THE LENGTH OF THE FUSELAGE AND HAD COATED THE LT WING AS WELL. THE PILOTS ALSO NOTED NO OIL WAS VISIBLE ON THE DIPSTICK; THEY HAD DEPARTED WITH 8 QUARTS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bracket · crackedDec 31, 2014

    DURING A PROGRESSIVE INSPECTION EVENT, A BRACKET WAS FOUND CRACKED BELOW WHERE THE FLAP HANDLE IS MOUNTED. THE BRACKET IN QUESTION IS LOCATED IN THE TUNNEL IN THE CENTER OF THE CABIN FLOOR AND IS USED TO MOUNT THE FLAP HANDLE ASSLY. IT CONTAINS 2 NUT PLATES TO ALLOW THE HANDLE TO BE BOLTED THROUGH…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · tube · failedJan 17, 2014

    AFTER RETURNING FROM FLIGHT, PILOT REPORTED RT MAIN TIRE FLAT. WHEEL ASSEMBLY REPLACED WITH A SERVICEABLE BUILT UP WHEEL ASSEMBLY. AFFECTED TUBE INSTALLED. REPAIR STATION HAS EXPERIENCED A NR OF TIRE TUBE FAILURES WITHIN THE PAST 6 WEEKS; THESE FAILURES OCCURRED DURING NORMAL OPERATION OR WHEN THE…

    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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