This N-number isn't registered right now. Below is its last known registration, canceled May 21, 2014.
Safety record in brief:1 NTSB accident (destroyed damage, Aug 2013)8 ADs may apply8 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 student pilot's failure to maintain control and climb the airplane during a go-around maneuver. Contributing to the accident was the flight instructor's failure to provide adequate oversight of the student pilot by ensuring that the cockpit was free of distractions.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA13FA385)
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.
REMOVED CARBURETOR, WAS UNABLE TO PROPERLY LEAN. NO RISE AT ANY RPM. ROUGH AND STUMBLED WHEN REDUCING POWER AND WHEN ADVANCING POWER. HAD CARBURETOR O/H RS NR V1RR580Y. INSTALLED AFTER O/H AND WAS STILL UNABLE TO LEAN AT ANY RPM WITH IDLE MIXTURE SCREW 4 TURNS OUT. STILL ROUGH AND STUMBLED. THIS…
From FAA Service Difficulty Reports; matched by N-number and serial number.INSTALLED SUPPLIED O/H CARBURETOR ON 7-19-2010. AFTER 80 HOUR OF TIME ON REPLACEMENT CARBURETOR, ENGINE BECAME HARD STARTING AND WAS UNABLE TO ACHEIVE PROPER LEANING AT ANY RPM. ALSO, NOTICED A POWER DROP OR STUMBLE, WHEN REDUCING POWER FROM FULL THROTTLE BACK TO CRUISE. REMOVED AND FOUND LEAK…
From FAA Service Difficulty Reports; matched by N-number and serial number.INSTALLED A NEW CARBURETOR ON 9-3-2010. AFTER 21 HOURS TIME IN SERVICE WE WERE UNABLE TO ACHEIVE PROPER LEANING AT ANY RPM AND HAD A POWER LOSS OR STUMBLE WHEN REDUCING POWER BACK TO CRUISE RPM. WITH THE ASSISTANCE OF A MFG REPRESENTATIVE, THE ACFT WAS INSPECTED AND WE WERE INSTUCTED TO RETURN…
From FAA Service Difficulty Reports; matched by N-number and serial number.(V1RR) INSTALLED, SUPPLIED OVERHAULED CARBURETOR ON 7-7-2010. AFTER 33 HOURS ON CARBURETOR IT BECAME HARD STARTING AND UNABLE TO ACHIEVE PROPER LEANING AT ANY RPM. REMOVED AND FOUND HEAVY FUEL LEAK AROUND TOP OF VENTURI. REPLACED IAW WITH ANOTHER CARBURETOR SUPPLIED BY REPAIR STATION.
From FAA Service Difficulty Reports; matched by N-number and serial number.(V1RR) INSTALLED FACTORY O/H ENGINE ON 2-25-2010. AFTER 178 HOURS ENGINE BECAME VERY HARD STARTING. SEEMED TO BE FLOODING. REMOVED CARBURETOR AND FOUND LEAK AROUND LOWER PART OF ACCELERATOR PUMP AND FUEL LEAK INTERNAL AROUND TOP OF VENTURI. REPLACED IAW MFG WITH ANOTHER CARBURETOR SUPPLIED BY…
From FAA Service Difficulty Reports; matched by N-number and serial number.WHEN STARTING AIRCRAFT, MADE LOUD NOISE AT STARTER. INSPECTED AND FOUND BENDIX SHATTERED. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.WING WALK STIFFENER PANEL CRACKED UNDER UPPER WING SKIN, YEARS OF WALKING ON PANEL. STIFFENER PANEL SHOULD BE HEAVER GAUGE METAL. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.REPORT BY PILOT THAT OVERHEAD LIGHT INOP. REPAIR/SIGN OFF - BY MECHANIC STATED 'DID NOT HAVE SWITCH TURNED ON. WORKS FINE'. AFTER SEEING THIS AND BEING FAMILIAR WITH CESSNA SEB 92-33, REV 2, TOOK ANOTHER LOOK AT OVERHEAD PANEL AND FOUND THAT YOU HAD TO HIT THE PANEL TO GET THE LIGHT TO COME ON AND…
From FAA Service Difficulty Reports; matched by N-number and serial number.