This N-number isn't registered right now. Below is its last known registration, canceled Dec 18, 2012.
Safety record in brief:1 NTSB accident (substantial damage, Apr 2002)3 ADs may apply2 service difficulty reports
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.
The pilot not maintaining aircraft control while encountering windshear during initial climbout, resulting in a stall at a low altitude.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CHI02LA109)
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-32RT-300T) |
| 2010-15-10 | Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series Airplanes | Aug 31, 2010 | Airframe (PA-32RT-300T)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; … |
| 95-26-13 | The New Piper Aircraft, Inc. (Formerly Piper Aircraft Corporation) PA28 and PA32 Series… | Feb 5, 1996 | Airframe (PA-32RT-300T)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.
INSPECTION FOUND ONE OF THE COUNTERSINK SCREWS ATTACHING MAIN GEAR TRUSS BRACKET TO WING SPAR IS LOOSE. NUT IS TIGHT ON SCREW, BUT SCREW CAN BE EASILY TURNED WITH FINGERS.
From FAA Service Difficulty Reports; matched by N-number and serial number.INSPECTION FOUND RUDDER SKIN LT SIDE AT TRAILING EDGE, APPROXIMATELY 18 INCHES FROM TOP AT AFT END OF STIFFENING DIMPLE, TO HAVE ABOUT 6 SPIDER WEB CRACKS ALL ABOUT 1 INCH IN LENGTH. PIPER SL 882A WAS INCORPORATED.
From FAA Service Difficulty Reports; matched by N-number and serial number.