This N-number isn't registered right now. Below is its last known registration, canceled Aug 16, 2017.
Safety record in brief:1 NTSB accident (substantial damage, Aug 2012)9 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 loss of directional control during landing roll, which resulted in a runway excursion. The reason for the loss of directional control could not be determined because postaccident examination did not reveal any malfunctions or anomalies that would have precluded normal operation.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN12LA516)
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 |
|---|---|---|---|
| 2024-10-04 | Wing, Attach Fittings | Jun 6, 2024 | Airframe (PA-44-180)Serial numbers per Piper Service Bulletin No. 1413, dated April 9, 2024 |
| 2015-26-08 | Rudder Control System | Jan 20, 2016 | Airframe (PA-44-180)Certain serial numbers: PA-44-180 44-7995001–44-8195026; PA-44-180 4495001–4496377; PA-44-180 4496379; PA-44-180 4496380; PA-44-180 4496384–4496386; PA-44-180T 44-8107001–44-8207020 |
| 2013-02-13 | Stabilizer Control System | Mar 11, 2013 | Airframe (PA-44-180) |
| 2010-15-10 | Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series Airplanes | Aug 31, 2010 | Airframe (PA-44-180)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; … |
| 2006-10-21 | Engine Components Incorporated (ECi) Reciprocating Engine Connecting Rods | Jun 22, 2006 | Engine (O-360-A1H6)Only with: ECi connecting rods P/N AEL11750 (forging P/N AEL11488) installed, rod serial numbers 54/6 and below, produced between January 2002 and January 2004. |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2006-06-16 | Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, and… | Apr 27, 2006 | Engine (O-360-A1H6)Only with: Engines manufactured new or rebuilt, overhauled, or that had a crankshaft installed after March 1, 1999. |
| 2005-19-11 | Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, LO-360… | Oct 21, 2005 | Engine (O-360-A1H6)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. |
| 2005-15-10 | The New Piper Aircraft, Inc. Models PA-34-200T, PA-34-220T, PA-44-180, and PA-44-180T… | Aug 26, 2005 | Airframe (PA-44-180)Certain serial numbers: PA-34-200T 34-7570002–34-8170092; PA-34-220T 34-8133002–3449278; PA-44-180 44-7995001–4496168; PA-44-180T 44-8107001–44-8207020; PA-34-220T 3449279–3449309; PA-44-180 4496169–4496190. Only with: Equipped with a model 91E92-1 or 91E93-1 aircraft heater fuel pump. |
| 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-44-180)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; … |
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 PHASE INSPECTION MECHANIC NOTED BOTH MLG STRUTS LEAKING FLUID. UPON DISASSEMBLY TO REPACK STRUTS MECHANIC FOUND APPROXIMATELY .5 CUP OF ALUMINUM SHAVINGS IN INNER STRUT. FURTHER INSPECTION FOUND OUTER STRUT INNER BORE GROOVED AND GOUGED IN THE AREA OF UPPER BEARING TRAVEL. UPPER BEARING ON…
From FAA Service Difficulty Reports; matched by N-number and serial number.AT RUN-UP, FOUND EXCESSIVE MAGNETO DROP ON LT ENGINE, RT MAGNETO. REMOVED MAGNETO AND FOUND DISTRIBUTOR FINGER LOOSE ON DISTRIBUTOR GEAR. THIS IS A COMMON FAILURE. REPLACED MAGNETO WITH SERVICEABLE MAGNETO.
From FAA Service Difficulty Reports; matched by N-number and serial number.RIGHT MAGNETO, RT ENGINE OPERATED INTERMITTENTLY. REMOVED AND DISASSEMBLED. FOUND DISTRIBUTOR FINGER LOOSE ON DISTRIBUTOR GEAR. THIS IS A COMMON PROBLEM. INSTALLED SERVICEABLE MAGNETO.
From FAA Service Difficulty Reports; matched by N-number and serial number.AFTER LEVELING OFF AT 5,500 MSL THE CREW BEGAN LEANING MIXTURES AND THE RT ENGINE RPM BEGAN TO DROP AT A STEADY RATE. NO ENGINE ANNUNCIATORS APPEARED AND ALL ENGINE INSTRUMENTS READ NORMAL AFTER 15 SECONDS THE RT PROP WENT FULL FEATHER AND THE ENGINE WAS SHUTDOWN BY THE CREW. THEY RETURNED TO THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.