This N-number isn't registered right now. Below is its last known registration, canceled Sep 27, 2011.
Safety record in brief:2 NTSB events (substantial damage at worst, latest Aug 1998)7 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 inadequate landing flare, causing components of the nose wheel landing gear to fracture.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for FTW98LA369)
THE RIGHT MAIN LANDING GEAR STRUT FAILED ON LANDING ROLL. THE CAUSE FOR THE FAILURE WAS NOT DETERMINED, THE OWNER WOULD NOT MAKE THE STRUT AVAILABLE FOR TESTING.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ATL83IA208)
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-34-200T) |
| 2010-15-10 | Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series Airplanes | Aug 31, 2010 | Airframe (PA-34-200T)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; … |
| 2005-15-10 | The New Piper Aircraft, Inc. Models PA-34-200T, PA-34-220T, PA-44-180, and PA-44-180T… | Aug 26, 2005 | Airframe (PA-34-200T)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. |
| 2005-13-16 | The New Piper Aircraft, Inc. PA-34 Series Airplanes | Aug 8, 2005 | Airframe (PA-34-200T) |
| 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-34-200T)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 |
|---|---|---|---|
| 97-01-01 R1 | The New Piper Aircraft, Inc. PA-24, PA- 28R, PA-30, PA-32R, PA-34, and PA-39 Series… | Dec 8, 1998 | Airframe (PA-34-200T)Certain serial numbers: PA-28R-180 28R-30002–28R-31135; PA-28R-180 28R-7130001–28R-7130013; PA-28R-200 28R-35001–28R-35820; PA-28R-200 28R-7135001–28R-7635539; PA-28R-201 28R-7737002–28R-7737096; PA-28R-201T 28R-7703001–28R-7703239; …. Only with: All serials of PA-24, PA-24-250, PA-24-260, PA-24-400, PA-30, PA-39; PA-28R, PA-32R, PA-34 models (all serials of PA-34-200) only if not equipped with Piper P/N 78717-02 (or FAA-approved equivalent) main gear sidebrace stud in both main gear sidebrace bracket assemblies. |
| 98-04-27 | The New Piper Aircraft Corporation Models PA-23, PA-23-160, PA-23-235, PA-23-250… | Mar 13, 1998 | Airframe (PA-34-200T) |
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.
PILOT EXPERIENCED PROBLEM WITH HIS LANDING GEAR WHILE ON APPROACH. THE GEAR UNSAFE LIGHT FLICKERED ON AND OFF WHILE ENROUTE; WHEN GEAR LEVER WAS PUT DOWN, NOTHING HAPPENED. AFTER EXECUTING A CHECKLIST TO TROUBLESHOOT, HE DETERMINED THAT SOMETHING IN THE SYSTEM HAD MALFUNCTIONED. MAINTENANCE…
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT REPORTED AN OIL LEAK COMING FROM THE LEFT (NR 1) ENGINE AFTER FINISHING THEIR FLIGHT FOR THE DAY. MAINTENANCE INVESTIGATED THE OIL LEAK AND FOUND THE CRANKSHAFT CRACKED AROUND THE CIRCUMFERENCE OF THE PROPELLER FLANGE. WHEN MAINTENANCE STARTED TO REMOVE THE PROPELLER THEY FOUND AN O-RING…
From FAA Service Difficulty Reports; matched by N-number and serial number.INSTALLED A FACTORY REMANUFACTURED ENGINE FROM CONTINENTAL THAT CAME WITH A NEW FUEL PUMP. UPON DOING THE ENGINE GROUND RUNS AND INITIAL ENGINE SET UP THE FUEL PUMP WOULD NOT SHUT OFF THE FUEL AFTER THE MIXTURE HAD BEEN PULLED BACK. INSPECTED SYSTEM FOUND TO HAVE A DEFECTIVE FUEL PUMP, REPLACED…
From FAA Service Difficulty Reports; matched by N-number and serial number.WHILE PERFORMING AD 96-12-07, THE MECHANIC NOTICED THAT THE STOP PIN FOR THE IMPULSE COUPLING WAS MISSING. INSPECTED THE ACCESSORY SECTION AND FOUND THE PIN WEDGED BETWEEN THE CRANK CASE AND A GEAR. REMOVED THE PIN, NO FURTHER DAMAGE WAS FOUND.
From FAA Service Difficulty Reports; matched by N-number and serial number.