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-28-151
Year
1974
Serial number
28-7415504
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
A53563
Engine
Make and model
Lycoming 0-320 Series
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
1995 – 2015Individual ownerMiami, TX
1946 – 1949Individual ownerNorfolk, VA · different airframe: Taylorcraft Bc12-D S/N 7132
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 8, 2002 · Masterson, TX
The loss of engine power due to fuel starvation as a result of a blockage of the carburetor. A contributing factor was the lack of suitable terrain for the emergency landing.
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.
The New Piper Aircraft, Inc. Models PA- 25, PA-25-235, PA-25-260, PA-28S-160…
Jan 13, 2000
Airframe (PA-28-151)Only with: Equipped with Purolator air filter P/N 638873, Model CA161PL, or Piper P/N 460-632 (PS60007-2); PA-28-151/161 only when STC SA2946SO is incorporated.
The New Piper Aircraft, Inc. (Formerly Piper Aircraft Corporation) PA28 and PA32 Series…
Feb 5, 1996
Airframe (PA-28-151)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 (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.
Engine fuel and control · carburetor · inoperativeSep 9, 2002
(CARBURETOR) AN ALUMINUM SLIVER, .188 LONG, .018 THICK, .023 WIDE WAS FOUND BETWEEN THE NEEDLE VALVE AND SEAT. PREVENTING OPERATION OF NEEDLE VALVE. THE SLIVER APPEARS OF THE THROTTLE BODY ASSEMBLY, WHERE THE FUEL INLET AND STRAINER ASSEMBLY IS INSTALLED.
From FAA Service Difficulty Reports; matched by N-number and serial number.