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Aircraft record

N4352F1976 Piper PA-32R-300

Registration validUnclaimedSource: FAA, updated Oct 19, 2026

Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Nov 2016)5 ADs may apply6 service difficulty reports

Registration
Valid
expires Apr 30, 2028
Based in
Dillingham, AK
owner city / state
Owners
1
since 2004
NTSB events
2
substantial, 2016
ADs may apply
5
confirm with A&P
Service reports
6
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Registered owner
Bidzy Ta Hot Aana Corp
Owner type
Corporation
City, state
Dillingham, AK
Certificate issued
Sep 30, 2004
Expires
Apr 30, 2028
Airworthiness
Standard · Normal
Airworthiness date
Aug 18, 1976

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-32R-300
Year
1976
Serial number
32R-7680441
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
A53855

Engine

Type
Reciprocating

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2004 – nowBidzy Ta Hot Aana CorpDillingham, AK · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 2026 · SDRs · Oct 16, 2026

NTSB events (2)

Accident · minor damage

Nov 21, 2016 · Mcgrath, AK

The failure of the nose landing gear to extend and lock due to the failure of the alternator and reduced battery power due to the cold ambient temperature, which prohibited the electrically-driven hydraulic pump from supplying adequate hydraulic pressure to extend the nose landing gear. The cause of the left main landing gear collapse could not be determined, as there were no postaccident…

Damage
Minor
Injuries
Serious
Report
ANC17LA014

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC17LA014)

Accident · substantial damage

Sep 22, 2001 · Tanana, AK

An unlocked landing gear mechanism during landing roll. A factor associated with the accident was an electrical system failure.

Damage
Substantial
Injuries
None
Report
ANC01LA145

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC01LA145)

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
2013-02-13Stabilizer Control SystemMar 11, 2013Airframe (PA-32R-300)
2010-15-10Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series AirplanesAug 31, 2010Airframe (PA-32R-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; …
99-05-09The New Piper Aircraft, Inc. PA-23, PA- 24, PA-28, PA-32, and PA-34 Series AirplanesMar 19, 1999Airframe (PA-32R-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).
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-32R-300)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.
95-26-13The New Piper Aircraft, Inc. (Formerly Piper Aircraft Corporation) PA28 and PA32 Series…Feb 5, 1996Airframe (PA-32R-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 (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.

  • Electrical power · terminal · corrodedDec 10, 2001

    AIRPLANE LANDED, LEFT GEAR UNLOCKED AFTER ELECTRICAL POWER FAILURE ON APPROACH TO LAND. INSPECTION OF ELECTRICAL SYSTEM, FOUND BATTERY POST CORRODED ON POSITIVE TERMINAL.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · brace · brokenNov 16, 2001

    INSPECTION FOUND RIGHT NOSE GEAR DOOR BRACE BROKEN AT REAR ATTACH POINT. ALSO CRACKED OUT FROM RIVETS AT AFT END OF BRACE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · brace · brokenNov 16, 2001

    INSPECTION FOUND RIGHT NOSE GEAR DOOR BRACE BROKEN AT REAR ATTACH POINT. ALSO CRACKED OUT FROM RIVETS AT AFT END OF BRACE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 6 reports
  • Doors · brace · brokenNov 16, 2001

    INSPECTION FOUND RIGHT NOSE GEAR DOOR BRACE BROKEN AT REAR ATTACH POINT. ALSO CRACKED OUT FROM RIVETS AT AFT END OF BRACE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Reciprocating engine · arm · wornApr 9, 2001

    DURING VALVE CLEARANCE INSPECTION, FOUND NR 6 INTAKE ROCKER ARM FACE WHERE IT CONTACTS ROTATER CAP, WORN SEVERELY .1250 AND BADLY PITTED. ENGINE HAS BEEN ON OIL ANALYSIS SINCE OVERHAUL WITH NO PROBLEMS NOTED. ALL OTHER ROCKER ARMS FOUND NORMAL. PROBABLE CAUSE IS THAT A WORN UNAIRWORTHY PART WAS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Reciprocating engine · crankcase · crackedOct 6, 1995

    DURING ANNUAL INSPECTION, FOUND CRANKCASE CRACKED FROM EDGE OF NR 2 CYLINDER FLANGE TO FORWARD CORNER AT CYLINDER BASE STUD. EDDY CURRENT INSPECTION VERIFIED CRACK TO BE SUBSURFACE. VISUAL INSPECTION SHOWED NO CRACKING ON INSIDE OF CASE. THE CRACK WAS APPROXIMATELY 1.50 INCHES LONG. ENGINE…

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

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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