Safety record in brief:1 NTSB accident (substantial damage, Mar 2026)9 ADs may apply
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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.
Maintenance personnel’s failure to ensure that the throttle cable was properly secured to the carburetor, which resulted an inflight separation of the throttle cable and the pilots’ inability to control the engine.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA26LA151)
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 |
|---|---|---|---|
| 2026-17-10 | Reciprocating Engine Cylinder Section | Sep 14, 2026 | Engine (O-540-E4B5)Serial numbers per Table 2 or Table 3 of Lycoming Mandatory Service Bulletin No. 667A, dated March 12, 2026. Only with: Installed piston pin P/N LW-13445 with an OEM FAA Form 8130-3 production dated between January 7, 2021 and December 15, 2025, or where the production date cannot be determined or the form is unavailable. |
| 2013-02-13 | Stabilizer Control System | Mar 11, 2013 | Airframe (PA-32-260) |
| 2010-15-10 | Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series Airplanes | Aug 31, 2010 | Airframe (PA-32-260)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; … |
| 2006-10-21 | Engine Components Incorporated (ECi) Reciprocating Engine Connecting Rods | Jun 22, 2006 | Engine (O-540-E4B5)Only with: ECi connecting rods P/N AEL11750 (forging P/N AEL11488) installed, rod serial numbers 54/6 and below, produced between January 2002 and January 2004. |
| 2005-19-11 | Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, LO-360… | Oct 21, 2005 | Engine (O-540-E4B5)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 (O-540-E4B5)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. |
| 99-05-09 | The New Piper Aircraft, Inc. PA-23, PA- 24, PA-28, PA-32, and PA-34 Series Airplanes | Mar 19, 1999 | Airframe (PA-32-260)Certain serial numbers: PA-23-235 27-505–27-622; PA-23-250 27-01–27-2504; PA-24-180 24-103–24-3687; PA-24-250 24-103–24-3687; PA-24-260 24-3642; PA-24-260 24-4000–24-5028; …. Only with: Equipped with Purolator air filter P/N 638873, Model CA161PL, or Piper P/N 460-632 (PS60007-2). |
| 99-04-04 | Textron Lycoming Reciprocating Engines IO-540 and O-540 Engines Equipped With Slick… | Feb 25, 1999 | Engine (O-540-E4B5)Only with: Equipped with Slick Aircraft Products magneto model numbers 6251, 6252, 6255, 6351 or 6355. |
| 95-26-13 | The New Piper Aircraft, Inc. (Formerly Piper Aircraft Corporation) PA28 and PA32 Series… | Feb 5, 1996 | Airframe (PA-32-260)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.
No Service Difficulty Reports found for this airframe since 1995.