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-301
Serial number
32R-8013048
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
AB1B87
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
2012 – nowOK3 Wire Aviation LLCVirginia Beach, VA · current
until 1957Cessna Aircraft CoWichita, KS · different airframe: Cessna 172 S/N 29947
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 2026 · SDRs · Oct 16, 2026
NTSB events (1)
Accident · substantial damage
Aug 17, 1997 · Jefferson City, MO
the pilot's incomplete preflight of the airplane's stabilizer and rudder trim settings for takeoff, his failure to correct for the high pitch during the initial climb, his failure to recover from the bounced landing, and the inadvertent stall. Factors relating to this accident were the improper stabilizer and rudder trim settings.
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. (Formerly Piper Aircraft Corporation) PA28 and PA32 Series…
Feb 5, 1996
Airframe (PA-32R-301)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.
Stabilizers · skin · crackedAug 29, 1996
THREE CRACKS WERE NOTICED IN SKIN OF RUDDER POSSIBLY DUE TO FATIGUE OVER TIME. REMOVED SKIN, NO INTERNAL DAMAGE FOUND. NEW SKIN INSTALLED. CRACK LENGTHS APPROXIMATELY 1 INCH.
From FAA Service Difficulty Reports; matched by N-number and serial number.