Safety record in brief:1 NTSB accident (substantial damage, Mar 2003)5 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.
The inadequate fuel consumption calculations by the pilot and the fuel exhaustion. The inadequate traffic pattern distance from the runway, which precluded his reaching the runway.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CHI03LA090)
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-28-151)Serial numbers per Table 1 to paragraph (c) of this AD |
| 2013-02-13 | Stabilizer Control System | Mar 11, 2013 | Airframe (PA-28-151) |
| 2010-15-10 | Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series Airplanes | Aug 31, 2010 | Airframe (PA-28-151)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; … |
| 99-26-05 | The New Piper Aircraft, Inc. Models PA- 25, PA-25-235, PA-25-260, PA-28S-160… | Jan 13, 2000 | Airframe (PA-28-151)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-28-151)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 FRONT SPINNER BULKHEAD CRACKED. A CRACK HAD PREVIOUSLY BEEN STOP DRILLED.
From FAA Service Difficulty Reports; matched by N-number and serial number.WHILE CHANGING LANDING LIGHT, FOUND LAMP RETAINER CRACKED AROUND UPPER STUD AND AROUND SCREW HOLE. THIS CONDITION CAUSED LANDING LIGHT TO VIBRATE EXCESSIVELY, PREMATURELY BURNING OUT BULB. SUBMITTER STATED THIS RETAINER SHOULD BE CHECKED AT EVERY INSPECTION, INCLUDING PRE-FLIGHT. IF RETAINER BROKE…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING 100-HOUR INSPECTION, FOUND WING-WALK DOUBLER RIBS CRACKED. FIVE OF THE RIBS WERE CRACKED AT OUTBOARD EDGE. SUBMITTER SUSPECTS CAUSE WAS TOTAL TIME AND POSSIBLY STRESS INDUCED DURING FORMING OF RIBS.
From FAA Service Difficulty Reports; matched by N-number and serial number.