This N-number isn't registered right now. Below is its last known registration, canceled Feb 23, 2018.
Safety record in brief:2 NTSB accidents (destroyed damage at worst, latest Aug 2012)6 ADs may apply4 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 failure to maintain clearance from trees and terrain while in cruise flight in marginal visual meteorological conditions.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC12FA083)
THE PILOT STATED THAT THE AIRPORT REGULATIONS WERE SUCH THAT HE HAD TO MAKE A DOWNWIND TAKEOFF ON RUNWAY 17. THE WIND WAS FROM 350 DEGREES AT 10 KNOTS. HE STATED THAT JUST AFTER LIFTOFF, THE AIRCRAFT STALLED. FORWARD ELEVATOR WAS APPLIED TO BREAK THE STALL AND THE AIRCRAFT SETTLED BACK TO THE GROUND. THE AIRCRAFT HIT SOFT DIRT AND A DITCH CAUSING THE LANDING GEAR TO COLLAPSE.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for FTW82DA366)
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.
NR 2 CYL CRACKED FROM UPPER SPARK PLUG HOLE TO THE EXHAUST VALVE SEAT. CRACK IN HEAD LED TO FAILURE OF EXHAUST PUSHROD HOUSING, AND DEFORMATION OF THE EXHAUST PUSHROD. AC LANDED WITHOUT INCIDENT. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.FOUND BOLT BROKEN AT NR 1 CYLINDER BASE. NUT AND SPACER FROM OPPOSITE SIDE MISSING AT TIME OF INSPECTION. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.ADC REPORTING TO IDU VARIED ALTITUDE OF +800 FEET. CROSSWIND COMPONENT ERRONEOUS AT TIMES. UNIT INSTALLED AS PART OF EFIS-SV SYSTEM.
From FAA Service Difficulty Reports; matched by N-number and serial number.AHRS REPORTING TO IDU WANDERING HEADING AND ERRONEOUS ACCELL/DECELERATION. UNIT INSTALLED AS PART OF FLIGHT SYSTEMS, INC EFIS-SV SYSTEM. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.