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-44-180
Year
1978
Serial number
44-7995099
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
4
Engines
2
Max takeoff weight
Up to 12,499 lb
Mode S code
A1CED8
Engine
Make and model
Lycoming O&Vo-360 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
2002 – 2018Golden Eagle Enterprises INCFresno, CA
1958 – 1967Individual ownerPontiac 16, MI · different airframe: 1949 Luscombe 8a S/N 6580
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
May 21, 1998 · Fresno, CA
The dual's student improper flare that led to the right main landing gear collapsing. A related factor in the accident was the instructor pilot's inadequate supervision.
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-34-200T, PA-34-220T, PA-44-180, and PA-44-180T…
Aug 26, 2005
Airframe (PA-44-180)Certain serial numbers: PA-34-200T 34-7570002–34-8170092; PA-34-220T 34-8133002–3449278; PA-44-180 44-7995001–4496168; PA-44-180T 44-8107001–44-8207020; PA-34-220T 3449279–3449309; PA-44-180 4496169–4496190. Only with: Equipped with a model 91E92-1 or 91E93-1 aircraft heater fuel pump.
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.
Fuselage · spar · crackedAug 22, 1996
DURING 100-HOUR INSPECTION, BOTH SPARS WERE DETERMINED TO HAVE CRACKS IN THE 'S' ANGLE REINFORCEMENT AT LOWER AFT BOLT HOLE FOR DRAG LINK MOUNTING BRACKET. CRACKS RAN LENTGHWISE AND EXTENDED PAST BOLT HOLE IN BOTH DIRECTIONS APPROXIMATELY ONE INCH. THIS IS THE SECOND SEMINOLE FOUND WITH THIS ON…
From FAA Service Difficulty Reports; matched by N-number and serial number.