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Aircraft record

N401SL1978 Piper PA-32RT-300T

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19823 ADs may apply4 service difficulty reports

Registration
Valid
expires Apr 30, 2029
Based in
Armuchee, GA
owner city / state
Engine
TI0-540 SER · 310 hp
Lycoming
Owners
1
since 2013
NTSB events
None
since 1982
ADs may apply
3
confirm with A&P
Service reports
4
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Catalina Air Harbor INC
Owner type
Corporation
City, state
Armuchee, GA
Certificate issued
Apr 12, 2013
Expires
Apr 30, 2029
Airworthiness
Standard

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-32RT-300T
Year
1978
Serial number
32R-7887148
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
7
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
A4B1F3

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. 2013 – nowCatalina Air Harbor INCArmuchee, GA · current

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 (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
2013-02-13Stabilizer Control SystemMar 11, 2013Airframe (PA-32RT-300T)
2010-15-10Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series AirplanesAug 31, 2010Airframe (PA-32RT-300T)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; …
95-26-13The New Piper Aircraft, Inc. (Formerly Piper Aircraft Corporation) PA28 and PA32 Series…Feb 5, 1996Airframe (PA-32RT-300T)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 (4)

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 · camshaft · galledApr 23, 2019

    CAMSHAFT LOBES 1 AND 2 GALLING AND ERODED. REDUCED LOBE LIFT OF VALVES RESULTED IN LOSS OF PERFORMANCE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Turbochargers · turbocharger · failedApr 23, 2019

    TURBOCHARGER FAILURE DUE TO MAIN BEARING FAILURE. TURBOCHARGER LOCKED UP (FROZE) AND BLOCKED AIR TO THE INDUCTION SYSTEM. PIC DID NOT EXECUTE PROCEDURES IN THE POH (MANUAL SELECTION OF ALTERNATE AIR SOURCE) RESULTING IN OFF AIRPORT LANDING AND INCIDENT REPORT. LAS VEGAS FSDO

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Exhaust · clamp · failedJul 2, 2014

    FAILURE OF THE CLAMP AND OR EXHAUST GASKET WHICH CAUSED EXCESSIVE HEAT DAMAGE TO THE UPPER COWLING AND ASSOCIATED WIRING LOCATED IN THE VICINITY OF THE EXHAUST LEAK. THE OCCURANCE HAPPEDED DURING THE TAKEOFF AT FULL POWER SETTING OF 2700 RPM AND 35" MAP. GASKETS, 78084, WERE FOUND MISSING IN 2…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 4 reports
  • Power plant · cowling · damagedJun 20, 2014

    FAILURE OF THE CLAMP AND OR EXHAUST GASKET WHICH CAUSED EXCESSIVE HEAT DAMAGE TO UPPER COWLING AND ASSOCIATED WIRING LOCATED IN THE VICINITY OF THE EXHAUST LEAK. THE OCCURRENCE HAPPENED DURING TAKEOFF AT FULL POWER SETTING OF 2700 RPM AT 36" MAP. INSPECTION OF THE CLAMP AND GASKET SHOULD BE MADE…

    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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