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Aircraft record

N8127K1979 Piper PA-32-300

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply7 service difficulty reports

Registration
Valid
expires Oct 31, 2029
Based in
Wasilla, AK
owner city / state
Engine
IO-540 SER · 300 hp
Lycoming
Owners
1
since 2016
NTSB events
None
since 1982
ADs may apply
6
confirm with A&P
Service reports
7
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Antler Aviation And Wildlife Service LLC
Owner type
LLC
City, state
Wasilla, AK
Certificate issued
Oct 20, 2016
Expires
Oct 31, 2029
Airworthiness
Standard · Normal
Airworthiness date
Oct 23, 1979

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-32-300
Year
1979
Serial number
32-7940268
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
6
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
AB1421

Engine

Make and model
Lycoming Io-540 Ser
Type
Reciprocating
Power
300 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 – nowAntler Aviation And Wildlife Service LLCWasilla, AK · 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 (6)

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-32-300)
2010-15-10Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series AirplanesAug 31, 2010Airframe (PA-32-300)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; …
2005-19-11Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, LO-360…Oct 21, 2005Engine (IO-540 SER)Only with: Engines rated at 300 HP or lower, manufactured new, rebuilt, or overhauled after March 1, 1999, or that had a crankshaft installed after March 1, 1999.
2004-05-24Lycoming Engines (Formerly Textron Lycoming) AEIO-540, IO-540, LTIO-540, O-540, and…Mar 30, 2004Engine (IO-540 SER)Only with: Engines with crankshaft gear retaining bolts P/N STD-2209 installed; excludes O-540-F series engines subject to AD 99-03-05 with bolt not since replaced, engines with bolt installed at original assembly or replaced by Lycoming per SB 554 after November 10, 1998, engines with bolt from replacement kits 05K19987, 05K23325, 05K23326, 05K23327, 05K23335 or 05K23336, and engines with single-drive dual magnetos.
99-05-09The New Piper Aircraft, Inc. PA-23, PA- 24, PA-28, PA-32, and PA-34 Series AirplanesMar 19, 1999Airframe (PA-32-300)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).
Show all 6 ADs
ADSubjectEffectiveApplies to
95-26-13The New Piper Aircraft, Inc. (Formerly Piper Aircraft Corporation) PA28 and PA32 Series…Feb 5, 1996Airframe (PA-32-300)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 (7)

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.

  • Ignition · breaker points · brokenMay 17, 2004

    SLICK MAG MODEL NUMBER M3637 CONTACT POINTS BROKE. 10 HOURS SINCE NEW.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Ignition · points · failedMay 17, 2004

    INVESTIGATION OF MAGNETO FAILURE FOUND THAT THE CONTACT ARM OF THE PRIMARY POINT SET HAD SNAPPED OFF. THE BREAK OCCURED AT THE AREA WHERE THE STIFFENER FLANGES FLATEN OUT. JUST AT THE EDGE OF THE NYLON BLOCK. UNABLE TO DETERMINE CAUSE OF FAILURE. (AL05200402443)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Navigation · receiver · malfunctionedMar 29, 2004

    THIS RECEIVER WAS INSTALLED AS PART OF THE EFIS-SV SYSTEM. AFTER APPROXIMATELY 30 HOURS OF OPERATION FOLLOWING THE INSTALLATION, AN LOI MESSAGE DISPLAYED ON THE INTEGRATED DISPLAY UNIT (IDU). THE RECEIVER WAS REPLACED, AND THE ERROR MESSAGE WAS NO LONGER DISPLAYED, AND THE SYSTEM FUNCTIONED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 7 reports
  • Propellers · blade · snappedSep 1, 1998

    WHILE AT CRUISE RPM, PILOT HEARD LOUD BANG FOLLOWED BY A SEVERE VIBRATION. REDUCING RPM MADE VIBRATION WORSE. A HIGHER RPM SETTING WAS USED AND AIRCRAFT RETURNED TO LAND SAFELY. UPON EXAMINATION, FOUND APPROXIMATELY 8 INCHES OF ONE PROPELLER BLADE SEPARATED FROM BLADE. SUBMITTER STATED THE BREAK…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Ignition · impulse coupling · looseAug 10, 1998

    SUBMITTER FOUND IMPULSE COUPLING RETAINER NUT LOOSE ON SHAFT WITH COTTER PIN STILL IN PLACE. THE IMPULSE ASSY COULD BE PULLED FROM TAPERED SHAFT WITH ONLY SLIGHT PRESSURE. A BLUEING COMPOUND WAS APPLIED TO THE TAPERED SHAFT AND THE IMPULSE ASSY WAS RESEATED. IT WAS FOUND THE SHAFT HAD A HIGH AREA…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Ignition · impulse coupling · looseJul 17, 1998

    REMOVED MAGNETO FOR 400-HOUR IMPULSE INSPECTION. FOUND BOTH PAWL PINS HAD BECOME LOOSE ON IMPULSE BODY WITH ONE PIN NEARLY READY TO COME OUT OF ITS MOUNT HOLE. THIS WAS A NEW MAGNETO ASSY INSTALLED ON ENGINE AS A UNIT.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Ignition · impulse coupling · defectiveNov 1, 1997

    MAGNETO REMOVED AT 500 HOURS TIS DUE TO IMPULSE COUPLING DEFECT.

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

Related aircraft

Show all 8 related aircraft
All 992 registered Piper PA-32-300 aircraft

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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