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-46-310P
Year
1986
Serial number
4608026
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
6
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
AC99E9
Engine
Make and model
Cont Motor Tsio-520 Ser
Type
Reciprocating
Power
300 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records
until 2013Individual ownerGriffin, GA
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 10, 2001 · Milwaukee, WI
the rich fuel mixture and the unsuitable landing area encountered by the pilot. Contributing factors were the high output of the fuel pump and the low altitude.
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.
Piper Aircraft, Inc. (Type Certificate Previously Held by The New Piper Aircraft, Inc.)…
May 6, 2011
Airframe (PA-46-310P)Serial numbers per Table 3 of this AD. Only with: Equipped with a turbine inlet temperature (T.I.T.) system (Lewis T.I.T. indicators/probes or Avidyne Entegra/EFIS with probe P/N 686-216) identified in table 3; relief only if gauge and probe replaced through STC.
The New Piper Aircraft Corporation Models PA-46-310P and PA-46-350P Airplanes
Mar 13, 1998
Airframe (PA-46-310P)
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (2)
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.
Exhaust · tailpipe · crackedApr 27, 1995
ONE-HUNDRED HOUR INSPECTION/ANNUAL, RT TAILPIPE CRACKED AT TURBO MOUNTING FLANGE. SUSPECT CAUSE: NORMAL WEAR AND VIBRATION. RECOMMEND RETORQUING CLAMP, PN 646434, AT 50-HOUR INTERVAL.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Exhaust · tailpipe · crackedApr 27, 1995
ONE-HUNDRED HOUR INSPECTION/ANNUAL, LT TAILPIPE CRACKED AT WASTEGATE MOUNTING FLANGE. SUSPECT CAUSE NORMAL WEAR AND VIBRATION. RECOMMEND RETORQUING CLAMP, PN 646434, AT 50-HOUR INTERVALS.
From FAA Service Difficulty Reports; matched by N-number and serial number.