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Aircraft record

N155971972 Piper PA-28R-200

Registration validUnclaimedSource: FAA, updated Oct 17, 2026

Safety record in brief:No NTSB accidents or incidents since 19825 ADs may apply6 service difficulty reports

Registration
Valid
expires Apr 30, 2027
Based in
Sale Creek, TN
owner city / state
Engine
I0360 SER · 180 hp
Lycoming
Owners
1
since 2014
NTSB events
None
since 1982
ADs may apply
5
confirm with A&P
Service reports
6
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Registered owner
Co-owners
City, state
Sale Creek, TN
Certificate issued
Apr 1, 2014
Expires
Apr 30, 2027
Airworthiness
Standard · Normal
Airworthiness date
Nov 14, 1972

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-200
Year
1972
Serial number
28R-7335072
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
A0E075

Engine

Make and model
Lycoming I0360 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. 2014 – nowCo-ownersSale Creek, TN · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 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 (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-200)Serial numbers per Table 1 to paragraph (c) of this AD
2013-02-13Stabilizer Control SystemMar 11, 2013Airframe (PA-28R-200)
2010-15-10Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series AirplanesAug 31, 2010Airframe (PA-28R-200)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; …
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-200)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-28R-200)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.

  • Wings · fitting · corrodedMar 27, 1997

    DURING ANNUAL INSPECTION, FOUND AFT WING FITTINGS AND ADJACENT STRUCTURE CORRODED. PIPER SB977 ADDRESSES THIS PROBLEM. CAUSE DUE TO WINDOW SEALS FAILING AND MOISTURE REMAINING IN THE INSULATION.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · fitting · corrodedMar 27, 1997

    DURING ANNUAL INSPECTION, FOUND AFT WING FITTINGS AND ADJACENT STRUCTURE CORRODED. PIPER SB977 ADDRESSES THIS PROBLEM. CAUSE DUE TO WINDOW SEALS FAILING AND MOISTURE REMAINING IN THE INSULATION.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuel · filler neck · corrodedMar 27, 1997

    DURING ANNUAL INSPECTION, FOUND AFT WING FITTINGS AND ADJACENT STRUCTURE CORRODED. PIPER SB977 ADDRESSES THIS PROBLEM. CAUSE DUE TO WINDOW SEALS FAILING AND MOISTURE REMAINING IN THE INSULATION. FOUND THE FUEL TANK FILLER NECK CORRODED THROUGH INTO THE FUEL STORAGE AREA. THE PILOT REMARKED, 'AH! I…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 6 reports
  • Electrical power · belt · failedMar 26, 1997

    A COMMON PROBLEM THAT SUBMITTER HAS FOUND OVER THE YEARS, WITH PIPER PRODUCTS ESPECIALLY, IS THE USE OF AUTOMOTIVE OR UNAPPROVED ALTERNATOR DRIVE BELTS. IN THIS CASE, A NAPA AUTOMOTIVE BELT WAS INSTALLED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Navigation · pitot head · corrodedMar 26, 1997

    THE PITOT MAST WAS SO CORRODED THE AIR INLET HOLES WERE CLOSED APPROXIMATELY ONE-FOURTH DUE TO THE BUILD-UP OF THE CORROSION. SUBMITTER STATED THE AIRCRAFT HAD BEEN BASED IN A CORROSIVE ENVIRONMENT (FLORIDA).

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Power plant · mount · crackedMar 26, 1997

    MOST OF THE TUBES ON THIS ENGINE/LANDING GEAR MOUNT HAD TO BE REPLACED DUE TO CORROSION, CRACKS, OR CHAFING. THE CHAFING WAS FROM OLD LOOP-TYPE (ADEL) CLAMPS THAT HAD NOT BEEN REPLACED WHEN THE RUBBER CUSHIONS DRIED OUT. THE AIRCRAFT HAD BEEN IN AN ACCIDENT WHERE ONE GEAR COLLAPSED WHICH MAY…

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

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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