This N-number isn't registered right now. Below is its last known registration, canceled Feb 3, 2012.
Safety record in brief:1 NTSB accident (substantial damage, Jun 2006)5 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.
Improper installation of the fuel line by maintenance personnel which resulted in the fuel line disconnecting and a loss of engine power during approach.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ATL06LA090)
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 |
|---|---|---|---|
| 2018-07-03 | Placard and Markings | Apr 20, 2018 | Airframe (PA-28-140)Serial numbers per Table 1 to paragraph (c) of this AD |
| 2013-02-13 | Stabilizer Control System | Mar 11, 2013 | Airframe (PA-28-140) |
| 2010-15-10 | Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series Airplanes | Aug 31, 2010 | Airframe (PA-28-140)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; … |
| 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-28-140)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). |
| 95-26-13 | The New Piper Aircraft, Inc. (Formerly Piper Aircraft Corporation) PA28 and PA32 Series… | Feb 5, 1996 | Airframe (PA-28-140)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.
DURING ANNUAL INSPECTION, FOUND PILOT'S OUTBOARD SEAT RAIL HAD SEVERE EXFOLIATION CORROSION SEVEN INCHES FORWARD OF SPAR CARRY-THROUGH STRUCTURE. UPON PROBING CORROSION WITH A PICK, THE RAIL DISINTEGRATED. SUBMITTER STATED THERE WAS EVIDENCE OF WATER PREVIOUSLY STANDING IN CABIN AREA.
From FAA Service Difficulty Reports; matched by N-number and serial number.CORROSION FOUND ON BOTH WING REAR ATTACH FITTINGS. THIS PROBLEM IS ADDRESSED BY PIPER SB 977. IT APPEARS THERE IS SURFACE CORROSION ON THE STEEL FITTING AND DISSIMILAR METAL CORROSION ON THE SPAR CARRY-THROUGH STRUCTURE. SUBMITTER RECOMMENDED THIS SB BE MADE INTO AN AD TO ELIMINATE THIS UNSAFE…
From FAA Service Difficulty Reports; matched by N-number and serial number.