This N-number isn't registered right now. Below is its last known registration, canceled May 20, 2008.
Safety record in brief:1 NTSB accident (substantial damage, Apr 2007)11 ADs may apply1 service difficulty report
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 pilot's delayed decision to abort the takeoff. Contributing to the accident was the attempted takeoff above the airplane's maximum gross weight, and an undetermined partial power loss, as reported by the pilot.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for NYC07LA106)
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 |
|---|---|---|---|
| 2023-25-02 | Control Column Section | Dec 19, 2023 | Airframe (PA 46-350P)Certain serial numbers: PA-46-350P 4636811–4636814; PA-46-350P 4636816–4636829; PA-46-500TP 4697692–4697700; PA-46-600TP 4698224–4698240; PA-46-600TP 4698242–4698274 |
| 2015-13-09 | Cabin Pressure Control System | Jul 13, 2015 | Airframe (PA 46-350P)Certain serial numbers: PA-46-350P 4636652–4636662; PA-46-500TP 4697549; PA-46-500TP 4697569; PA-46-500TP 4697582–4697591; PA-46-500TP 4697593–4697595; PA-46-500TP 4697597; … |
| 2013-13-01 | Fuel Storage | Jul 10, 2013 | Airframe (PA 46-350P)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 46-350P)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. |
| 2010-13-07 | Piper Aircraft, Inc. Models PA-32R-301T and PA-46-350P Airplanes | Jul 28, 2010 | Airframe (PA 46-350P)Certain serial numbers: PA-32R-301T 3257001–3257311; PA-46-350P 4622001–4622200; PA-46-350P 4636001–4636341 |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2009-07-08 | Piper Aircraft, Inc. Models PA-46-350P and PA-46R-350T Airplanes | May 5, 2009 | Airframe (PA 46-350P)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 (PA 46-350P)Certain serial numbers: PA-46-350P 4622001–4622200; PA-46-350P 4636001–4636445; PA-46R-350T 4692001–4692054; PA-46-500TP 4697001–4697365 |
| 2004-14-12 | The New Piper Aircraft, Inc., Models PA-28-161, PA-28-181, PA-28R-201, PA-32R-301 (HP)… | Aug 10, 2004 | Airframe (PA 46-350P)Certain serial numbers: PA-28-161 2842026–2842180; PA-28-181 2843112–2843565; PA-28R-201 2844014–2844099; PA-32R-301 3246098–3246214; PA-32R-301T 3257028–3257327; PA-34-220T 3449042–3449292; … |
| 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 46-350P)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; … |
| 99-16-06 | The New Piper Aircraft, Inc. Model PA- 46-350P Airplanes | Sep 24, 1999 | Airframe (PA 46-350P)Certain serial numbers: PA-46-350P 4622191–4622200; PA-46-350P 4636001–4636175 |
| 98-04-26 | The New Piper Aircraft Corporation Models PA-46-310P and PA-46-350P Airplanes | Mar 13, 1998 | Airframe (PA 46-350P) |
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.
CROSSOVER PIPE BETWEEN LEFT AND RIGHT TURBOCHARGERS WAS SPLIT UNDER HEAT SHIELD. ALLOWING HOT EXHAUST TO BLOW ON FORWARD SIDE OF FIREWALL. THE FIREWALL WAS NOT DAMAGED, BUT THE HEAT MELTED THE VINYL TRIM ON THE FORWARD SIDE OF THE NOSE BAGGAGE COMPARTMENT. THE HEAT SHIELD SHOULD BE REMOVED EACH…
From FAA Service Difficulty Reports; matched by N-number and serial number.