Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Mar 2013)2 ADs may apply
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A loss of preload to the crankshaft gear attachment bolt, resulting in rotation of the crankshaft gear and a subsequent total loss of engine power. The root cause for the loss of preload could not be determined during a postaccident examination of the components.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA13LA174)
The failure of the pilot-in-command to maintain airspeed following a reported loss of engine power, resulting in a stall/mush, uncontrolled descent, and in-flight collision with terrain. Factors in the accident were the pilot's intentional operation of the airplane with known deficiencies (inoperative No. 3 banner release), and inadequate installation of the banner tow-release hook assembly by…
From NTSB records; matched by serial number.Read NTSB report (search CAROL for MIA06LA033)
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 |
|---|---|---|---|
| 99-26-05 | The New Piper Aircraft, Inc. Models PA- 25, PA-25-235, PA-25-260, PA-28S-160… | Jan 13, 2000 | Airframe (PA-25-235)Only with: Equipped with Purolator air filter P/N 638873, Model CA161PL, or Piper P/N 460-632 (PS60007-2); PA-28-151/161 only when STC SA2946SO is incorporated. |
| 95-12-01 | Piper Aircraft Corporation PA-25 Series Airplanes | Jul 7, 1995 | Airframe (PA-25-235) |
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.