Safety record in brief:1 NTSB incident (minor damage, Dec 2007)5 ADs may apply2 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
The failure of the crankshaft due to fatigue. The fatigue crack initiation was not determined.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DEN08IA044)
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.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2013-13-01 | Fuel Storage | Jul 10, 2013 | Airframe (PA-46-310P)Certain serial numbers: PA-46-310P 46-8408001–46-8408087; PA-46-310P 46-8508001–46-8508109; PA-46-310P 46-8608001–46-8608067; PA-46-310P 4608001–4608140; PA-46-350P 4622001–4622200; PA-46-350P 4636001–4636591; … |
| 2011-06-10 | 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. |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (TSIO-520 SER)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P installed. |
| 2001-12-01 | The New Piper Aircraft, Inc. Models PA-46-310P, PA-46-350P, and PA-46-500TP Airplanes | Jun 29, 2001 | Airframe (PA-46-310P)Certain serial numbers: PA-46-310P 46-8408001–46-8408087; PA-46-310P 46-8508001–46-8508109; PA-46-310P 46-8608001–46-8608067; PA-46-310P 4608001–4608140; PA-46-350P 4622001–4622200; PA-46-350P 4636001–4636313; … |
| 98-04-26 | 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.
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.
CRANKSHAFT BROKE JUST AFT OF PROPELLER MOUNTNG FLANGE. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT REPORTED FAILED RT MAGNETO. REMOVED MAGNETO FROM ENGINE AND DISASSEMBLED. FOUND ONE OF THE COIL ANCHOR WEDGES WAS DISPLACED AND HAD MIGRATED ONTO THE SECONDARY TOWER. THE TOWER WAS BURNED AND MELTED AND THERE WAS OBVIOUS SIGNS OF A DIRECT SHORT AT THE SECONDARY TERMINAL CONTACT TAB.
From FAA Service Difficulty Reports; matched by N-number and serial number.