Safety record in brief:1 NTSB accident (substantial damage, Sep 2020)6 ADs may apply1 service difficulty report
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The pilot’s inadvertent loss of aircraft control, resulting in substantial damage to the airframe during the spin recovery.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN20LA430)
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 (PA46R-350T)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 (PA46R-350T)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. |
| 2009-07-08 | Piper Aircraft, Inc. Models PA-46-350P and PA-46R-350T Airplanes | May 5, 2009 | Airframe (PA46R-350T)Certain serial numbers: PA-46-350P 4636375–4636447; PA-46R-350T 4692001–4692068 |
| 2008-26-11 | Piper Aircraft, Inc. Models PA-46-350P, PA-46R-350T, and PA-46-500TP Airplanes | Jan 28, 2009 | Airframe (PA46R-350T)Certain serial numbers: PA-46-350P 4622001–4622200; PA-46-350P 4636001–4636445; PA-46R-350T 4692001–4692054; PA-46-500TP 4697001–4697365 |
| 2005-19-11 | Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, LO-360… | Oct 21, 2005 | Engine (TIO-540-AE2A)Only with: Engines rated at 300 HP or lower, manufactured new, rebuilt, or overhauled after March 1, 1999, or that had a crankshaft installed after March 1, 1999. |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2004-05-24 | Lycoming Engines (Formerly Textron Lycoming) AEIO-540, IO-540, LTIO-540, O-540, and… | Mar 30, 2004 | Engine (TIO-540-AE2A)Only with: Engines with crankshaft gear retaining bolts P/N STD-2209 installed; excludes O-540-F series engines subject to AD 99-03-05 with bolt not since replaced, engines with bolt installed at original assembly or replaced by Lycoming per SB 554 after November 10, 1998, engines with bolt from replacement kits 05K19987, 05K23325, 05K23326, 05K23327, 05K23335 or 05K23336, and engines with single-drive dual magnetos. |
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.
WHEN SETTING UP FOR A LANDING APPROACH, THE PILOT NOTED THAT THE LG CB HAD POPPED & FURTHER NOTED THAT THERE WERE NO GREEN DOWN LIGHTS ILLUMINATED. THE PILOT PERFORMED AN EMER GEAR EXTENSION & DID A TOWER FLY BY TO VERIFY THE GEAR APPEARED TO BE DOWN. THE LANDING WAS UNEVENTFUL. TROUBLESHOOTING…
From FAA Service Difficulty Reports; matched by N-number and serial number.