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Aircraft record

N6166H1977 Piper PA-28R-201T

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:1 NTSB accident (substantial damage, Aug 1985)5 ADs may apply1 service difficulty report

Registration
Valid
expires Jul 31, 2027
Based in
Glendale, AZ
owner city / state
Engine
TSIO-360 SER · 225 hp
Cont Motor
Owners
1
since 2002
NTSB events
1
substantial, 1985
ADs may apply
5
confirm with A&P
Service reports
1
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Individual owner
City, state
Glendale, AZ
Certificate issued
Jun 25, 2002
Expires
Jul 31, 2027
Airworthiness
Standard · Normal
Airworthiness date
Nov 17, 1977

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-28R-201T
Year
1977
Serial number
28R-7803093
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
A8083A

Engine

Make and model
Cont Motor Tsio-360 Ser
Type
Reciprocating
Power
225 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. 2002 – nowIndividual ownerGlendale, AZ · 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 (1)

Accident · substantial damage

Aug 6, 1985 · Hesperia, CA

UPON COMPLETING A X-C FLT, THE PLT PLACED THE LANDING GEAR SELECTOR IN THE DOWN POSITION, & THEREAFTER OBSERVED 'THREE IN THE GREEN.' THE PLT REPORTED THAT THE ACFT TOUCHED DOWN NORMALLY, & AS WEIGHT PLACED ONTO THE GEAR THE RIGHT MAIN GEAR RETRACTED. THE ACFT VEERED OFF TH RWY & SLID TO A STOP. THE LANDING GEAR & GEAR RETARACT SYSTEM WERE SUBSEQUENTLY EXAMINED. THEY WERE FOUND TO OPERATE…

Damage
Substantial
Injuries
None
Report
LAX85LA341

From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX85LA341)

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-28R-201T)Serial numbers per Table 1 to paragraph (c) of this AD
2013-02-13Stabilizer Control SystemMar 11, 2013Airframe (PA-28R-201T)
2010-15-10Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series AirplanesAug 31, 2010Airframe (PA-28R-201T)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-28R-201T)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-28R-201T)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.

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.

  • Nacelles and pylons · firewall · corrodedSep 17, 1997

    HOLE IN FIREWALL OBSERVED DURING ANNUAL INSPECTION. UPON REMOVAL, FOUND INTERIOR CORROSION MUCH MORE ADVANCED THAN EXTERIOR. HOLE SEEMED TO BE CAUSED BY CONSTANT EXPOSURE TO TURBOCHARGER OPERATING TEMPERATURES. PLASTIC ON AFT SIDE OF FIREWALL EXHIBITED SIGNS OF THERMAL BREAKDOWN AND CHARRING.

    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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