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-38-112
Year
1978
Serial number
38-78A0527
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
2
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
A51938
Engine
Make and model
Lycoming 0-235 Series
Type
4 Cycle
Power
115 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records
1987 – 2014Individual ownerTwentynine Palms, CA
1952 – 1955Individual ownerMonroe Center, IL · different airframe: 1947 Aeronca 11cc S/N 11cc-150
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
Jan 20, 1995 · Joshua Tree, CA
the operator's inadequate annual inspection by failing to find that the flight control's horizontal section of the 'T' bar was rubbing against the vacuum hoses behind the instrument panel. The jammed 'T' bar and the rough terrain were factors in this accident.
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 Corporation Model PA-38-112 Airplanes
Mar 16, 1998
Airframe (PA-38-112)Certain serial numbers: PA-38-112 38-80A0166–38-82A0122
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.
Flight controls · control · bindingJan 30, 1995
INVESTIGATION OF OFF AIRPORT LANDING FOUND EVIDENCE OF VACUUM FILTER LINES BEING CHAFED. IT WAS REPORTED ELEVATOR CONTROL FAILED TO RESPOND DURING TAKEOFF. SUBMITTER SUSPECTS CHAFE ON HOSE LINES IS INDICATIVE OF BINDING OR A CONTRIBUTING FACTOR TO LOSS OF ELEVATOR CONTROL. RECOMMENDS MORE…
From FAA Service Difficulty Reports; matched by N-number and serial number.