This N-number isn't registered right now. Below is its last known registration, canceled Jul 2, 2008.
Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Apr 2008)6 ADs may apply7 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's VFR flight into adverse weather conditions that resulted in a collision with snow-covered terrain during a turn to reverse direction. Factors contributing to the accident were low ceilings, flat lighting conditions, and the snow-covered terrain.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC08LA046)
THE FAILURE OF THE NUMBER 3 CYLINDER INTAKE VALVE STEM. A FACTOR IN THE DEGREE OF DAMAGE THE AIRCRAFT SUSTAINED IN THE MISHAP WAS ATTRIBUTABLE TO THE OFF AIRPORT EMERGENCY LANDING ON SHOW COVERED TUNDRA.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC93LA029)
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-32-301) |
| 2010-15-10 | Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series Airplanes | Aug 31, 2010 | Airframe (PA-32-301)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; … |
| 2005-19-11 | Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, LO-360… | Oct 21, 2005 | Engine (IO-540 SER)Only with: Engines rated at 300 HP or lower, manufactured new, rebuilt, or overhauled after March 1, 1999, or that had a crankshaft installed after March 1, 1999. |
| 2004-05-24 | Lycoming Engines (Formerly Textron Lycoming) AEIO-540, IO-540, LTIO-540, O-540, and… | Mar 30, 2004 | Engine (IO-540 SER)Only with: Engines with crankshaft gear retaining bolts P/N STD-2209 installed; excludes O-540-F series engines subject to AD 99-03-05 with bolt not since replaced, engines with bolt installed at original assembly or replaced by Lycoming per SB 554 after November 10, 1998, engines with bolt from replacement kits 05K19987, 05K23325, 05K23326, 05K23327, 05K23335 or 05K23336, and engines with single-drive dual magnetos. |
| 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-32-301)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). |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 95-26-13 | The New Piper Aircraft, Inc. (Formerly Piper Aircraft Corporation) PA28 and PA32 Series… | Feb 5, 1996 | Airframe (PA-32-301)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.
EN ROUTE TO AKN FROM PDB AIRCRAFT HAD AN ALTERNATOR FAILURE AND LOSS RADIOS. PILOT TRIED TO GET LIGHT SIGNAL FROM AKN TOWER WITH NO SUCCESS AND DIVERTED TO 5NK AND CONTACTED AKN MAINTENACE. MAINTENANCE CHANGED OUT THE FAILED ALTERNATOR AND BATTERY. FLIGHT CONTINUED TO AKN.
From FAA Service Difficulty Reports; matched by N-number and serial number.DEPARTED DLG AT APPROX 250 AGL ENGINE BEGAN RUNNING ROUGH AND LOST PARTIAL POWER. AIRCRAFT MADE UNEVENTFUL LANDING AT AIRPORT. MAINT FOUND RIGHT MAGNETO CAUSED PROBLEM. MAGNETO REPLACED AIRCRAFT RETURNED TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOTS SIDE WINDOW DURING MODERATE TURBULENCE HAD PREVIOUS REPAIR COME LOOSE. AIRCRAFT REPAIRED BY AKN MAINTENANCE PER AC 43.13 PLEXIGLASS REPAIR PROCEDURE.
From FAA Service Difficulty Reports; matched by N-number and serial number.ENGINE WAS RUNNING A LITTLE ROUGH DURING CRUISE. AFTER LANDING AT DESTINATION ENGINE RPM WENT TO IDLE AFTER ADVANCING THROTTLE. RETURNED TO BLOCK. REPLACED FUEL SERVO. OPERATIONAL CHECK OK.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING TAKEOFF, ENGINE STARTED TO CUT OUT. RETURNED TO BASE. ENGINE, FUEL SYSTEM AND IGNITION SYSTEM WERE INSPECTED AND FOUND SERVICEABLE NO FAULT FOUND. AIRCRAFT RETURNED TO SERVICE. NO FURTHER PROBLEMS HAVE BEEN NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number.ON SHORT FINAL, ENGINE APPEARED TO SURGE. LANDING WAS UNEVENTFUL. NO FAULT FOUND. PURGED FUEL FLOW SENSE LINE.
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT REPORTED ENGINE NO START, REPLACED BATTERY, NO OTHER FAULT FOUND.
From FAA Service Difficulty Reports; matched by N-number and serial number.