This N-number isn't registered right now. Below is its last known registration, canceled May 2, 2012.
Safety record in brief:1 NTSB accident (substantial damage, Sep 1983)8 ADs may apply3 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.
DURING ARRIVAL, THE PLT ELECTED TO LAND ON AN UNLIGHTED ARPT. AFTER LANDING & WHILE SLOWING, THE ACFT DRIFTED TO THE LEFT SIDE OF THE RWY. SUBSEQUENTLY, THE ACFT WENT OVER A CONCRETE CURB & THE LEFT MAIN GEAR FAILED.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for FTW83LA434)
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-28-161)Serial numbers per Table 1 to paragraph (c) of this AD |
| 2016-07-21 | Wing Ribs/Bulkhead | Apr 26, 2016 | Airframe (PA-28-161)Certain serial numbers: PA-28-161 2842393–2842395; PA-28-181 2843769–2843775; PA-28-181 2843779–2843791; PA-28R-201 2844152; PA-28-161 2842010–2842392; PA-28-181 2843021–2843768; … |
| 2013-02-13 | Stabilizer Control System | Mar 11, 2013 | Airframe (PA-28-161) |
| 2010-26-04 | Piper Aircraft, Inc. Model PA-28-161 Airplanes | Feb 1, 2011 | Airframe (PA-28-161)Only with: Equipped with Thielert TAE-125-01 engine installed per STC No. SA03303AT. |
| 2010-15-10 | Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series Airplanes | Aug 31, 2010 | Airframe (PA-28-161)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; … |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2004-14-12 | The New Piper Aircraft, Inc., Models PA-28-161, PA-28-181, PA-28R-201, PA-32R-301 (HP)… | Aug 10, 2004 | Airframe (PA-28-161)Certain serial numbers: PA-28-161 2842026–2842180; PA-28-181 2843112–2843565; PA-28R-201 2844014–2844099; PA-32R-301 3246098–3246214; PA-32R-301T 3257028–3257327; PA-34-220T 3449042–3449292; … |
| 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-28-161)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. |
| 95-26-13 | The New Piper Aircraft, Inc. (Formerly Piper Aircraft Corporation) PA28 and PA32 Series… | Feb 5, 1996 | Airframe (PA-28-161)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 FLIGHT ENGINE STARTED RUNNING ROUGH AND WOULD ONLY DEVELOP 1800 RPM. PILOT LANDED WITHOUT INCIDENT. UPON INSPECTION FOUND NR 3 CYLINER ROCKER SHAFT BOSS BROKEN AND SHAFT AND ROCKERS LAYING LOOSE IN THE ROCKER BOX COVER. THE PUSH RODS WERE STRAIGHT AND THE VALVES WERE NOT STUCK. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.THE SKIN RIVETED TO THE UNDERSIDE OF THE WING WALK PANELS FOR RE-ENFORCEMENT WERE FOUND CRACKED. THE CRACKS RAN FORE AND AFT. THE CRACKS WERE DISCOVERED AT 100-HOUR INSPECTION AFTER NOTING WEAKNESS IN THE WING WALK AREA WITH WEIGHT ON THIS AREA. THE AIRCRAFT IS USED FOR FLIGHT TRAINING. SUSPECT…
From FAA Service Difficulty Reports; matched by N-number and serial number.THE SKIN RIVETED TO THE UNDERSIDE OF THE WING WALK PANELS FOR RE-ENFORCEMENT WERE FOUND CRACKED. THE CRACKS RAN FORE AND AFT. THE CRACKS WERE DISCOVERED AT 100-HOUR INSPECTION AFTER NOTING WEAKNESS IN THE WING WALK AREA WITH WEIGHT ON THIS AREA. THE AIRCRAFT IS USED FOR FLIGHT TRAINING. SUSPECT…
From FAA Service Difficulty Reports; matched by N-number and serial number.