Incident
Aug 1, 2010 · Mount Pleasant, TXThe failure of an aileron control cable due to a seized idler pulley bearing.
- Injuries
- None
- Report
- CEN10IA453
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN10IA453)
Safety record in brief:1 NTSB incident (Aug 2010)5 ADs may apply1 service difficulty report
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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 an aileron control cable due to a seized idler pulley bearing.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN10IA453)
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 |
|---|---|---|---|
| 2013-02-13 | Stabilizer Control System | Mar 11, 2013 | Airframe (PA-32R-301T) |
| 2010-15-10 | Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series Airplanes | Aug 31, 2010 | Airframe (PA-32R-301T)Certain serial numbers: PA-28-140 28-20001–28-26946; PA-28-140 28-7125001–28-7725290; PA-28-150 28-03; PA-28-150 28-1–28-4377; PA-28-150 28-1760A; PA-28-160 28-03; … |
| 2010-13-07 | Piper Aircraft, Inc. Models PA-32R-301T and PA-46-350P Airplanes | Jul 28, 2010 | Airframe (PA-32R-301T)Certain serial numbers: PA-32R-301T 3257001–3257311; PA-46-350P 4622001–4622200; PA-46-350P 4636001–4636341 |
| 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-32R-301T)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; … |
| 95-26-13 | The New Piper Aircraft, Inc. (Formerly Piper Aircraft Corporation) PA28 and PA32 Series… | Feb 5, 1996 | Airframe (PA-32R-301T)Only with: Equipped with oil cooler hose assemblies that do not meet TSO-C53a, Type D requirements. |
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.
THE HARDWARE ATTACHING THE TURBOCHARGER SCAVANGE SUMP TO THE TURBOCHARGER BECAME LOOSE ALLOWING LARGE QUANITY OF OIL TO LEAK FROM THE ENGINE OIL SYSTEM. ONE BOLT WAS MISSING. A FORCED LANDING WAS NECESSARY. THIS ENGINE HAD BEEN DISASSEMBLED, REPAIRED AND REASSEMBLED BY MFG FOR COMPLIANCE WITH AD…
From FAA Service Difficulty Reports; matched by N-number and serial number.