N229MM2008 Piper PA46R-350T
Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply1 service difficulty report
Registration
FAA Aircraft Registry · Oct 17, 2026- Registered owner
- Fair Winds Aviation LLC
- Owner type
- LLC
- City, state
- Cheyenne, WY
- Certificate issued
- Apr 11, 2026
- Expires
- Apr 30, 2033
- Airworthiness
- Standard · Normal
- Airworthiness date
- Apr 22, 2008
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 dataAirframe
- Manufacturer
- Piper
- Model
- PA46R-350T
- Year
- 2008
- Serial number
- 4692029
- Aircraft type
- Fixed wing single engine
- Category
- Land
- Certification
- Not Type Certificated
- Seats
- 6
- Engines
- 1
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A2038F
Engine
- Make and model
- Lycoming Tio-540-Ae2a
- Type
- Reciprocating
- Power
- 350 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2026 – nowFair Winds Aviation LLCCheyenne, WY · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (6)
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. |
Show all 6 ADsShow fewer ADs
| 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.
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.
- Turbochargers · turbine wheel · wornMar 22, 2011
TURBOCHARGER WOULD NOT OBTAIN MANIFOLD PRESSURE AT CRITICAL ALTITUDE. TURBOCHARGER EXHIBITS NOTICEABLE RADIAL PLAY AND DRAGGING. THE COMPRESSOR OIL SEAL APPEARS TO BE DEFECTIVE. OIL IS BYPASSING THE SEAL BEING FORCED INTO ENGINE INDUCTION SYS. TURBINE WHEEL SHOWS CONSIDERABLE WEAR AND EROSION.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026