Safety record in brief:1 NTSB accident (substantial damage, May 2007)2 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.
Collapse of the landing gear during landing for undetermined reasons.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX07LA158)
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 |
|---|---|---|---|
| 2012-17-06 | Flight Controls | Oct 22, 2012 | Airframe (PA-24)Certain serial numbers: PA-24 24-1–24-3687; PA-24-250 24-1; PA-24-250 24-103–24-3687; PA-24-260 24-3642; PA-24-260 24-4000–24-5034. Only with: Horn P/N 20397-00 (assembly P/N 20399) installed. |
| 97-01-01 R1 | The New Piper Aircraft, Inc. PA-24, PA- 28R, PA-30, PA-32R, PA-34, and PA-39 Series… | Dec 8, 1998 | Airframe (PA-24)Certain serial numbers: PA-28R-180 28R-30002–28R-31135; PA-28R-180 28R-7130001–28R-7130013; PA-28R-200 28R-35001–28R-35820; PA-28R-200 28R-7135001–28R-7635539; PA-28R-201 28R-7737002–28R-7737096; PA-28R-201T 28R-7703001–28R-7703239; …. Only with: All serials of PA-24, PA-24-250, PA-24-260, PA-24-400, PA-30, PA-39; PA-28R, PA-32R, PA-34 models (all serials of PA-34-200) only if not equipped with Piper P/N 78717-02 (or FAA-approved equivalent) main gear sidebrace stud in both main gear sidebrace bracket assemblies. |
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.
LANDING GEAR STUD IS TO BE INSPECTED EVERY 1,000 HOURS PER AD 97-01-01. CRACKED STUD IN QUESTION HAD ONLY 453 HOURS SINCE LAST MAGNAFLUX INSPECTION. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number.