This N-number isn't registered right now. Below is its last known registration, canceled Sep 3, 2021.
Safety record in brief:1 NTSB accident (substantial damage, Nov 2019)6 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 pilot's hard, bounced landing and the flight instructor's delayed remedial action, which resulted in a fracture of the nose landing gear mounting structure.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN20TA025)
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 |
|---|---|---|---|
| 2022-09-13 | Nose/Tail Landing Gear | May 31, 2022 | Airframe (PA-34-200)Certain serial numbers: PA-34-200 34-7250001–34-7450220 |
| 2013-02-13 | Stabilizer Control System | Mar 11, 2013 | Airframe (PA-34-200) |
| 2010-15-10 | Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series Airplanes | Aug 31, 2010 | Airframe (PA-34-200)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; … |
| 2005-13-16 | The New Piper Aircraft, Inc. PA-34 Series Airplanes | Aug 8, 2005 | Airframe (PA-34-200) |
| 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-34-200)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. |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 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-34-200) |
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 ROUTINE ANNUAL INSPECTION, THE FRONT STRINGER, LOWER WING SKIN STIFFENER, WAS FOUND CRACKED UNDER THE LT ENGINE NACELLE USING A FLASHLIGHT & MIRROR VIA THE FRONT WING SECTION ACCESS PANEL JUST INBD OF THE INBD MAIN FUEL TANK. IN ORDER TO FACILITATE A BETTER VIEW & ACCESS, THE LT FUEL TANKS…
From FAA Service Difficulty Reports; matched by N-number and serial number.(ZB0R) DURING PREFLIGHT RUNUP, PILOT FOUND RT PROPELLER CONTROL TO BE FROZEN - WOULD NOT OPERATE. ACFT REPORTED TO MX. REPLACED RT PROPELLER CONTROL, PN 555-443. OPS CK GOOD
From FAA Service Difficulty Reports; matched by N-number and serial number.IN CRUISE, PILOT ATTEMPTED TO REDUCE POWER FOR MANEUVERS PRACTICE. LT ENGINE WAS UNRESPONSIVE. INSTRUCTOR IDENTIFIED LT ENGINE THROTTLE PROBLEM, ENGINE RPM WAS STABLE AT NEAR FULL POWER. RETURNED TO HOME BASE. PILOT FEATHERED AND SHUTDOWN LT ENGINE ON APPROACH. MAINTENANCE DISCOVERED LT ENGINE…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING GEAR MAINTENANCE, FOUND NLG ACTUATOR LEAKING. INSPECTION REVEALED WORN SEALS. REPLACED SEALS BUT STILL LEAKED. FURTHER INSPECTION WITH BORESCOPE IN BODY OF ACTUATOR REVEALED LONGITUDINAL SCORING ON INSIDE WALL OF ACTUATOR BODY. REPLACED ACTUATOR TO CORRECT DISCREPANCY.
From FAA Service Difficulty Reports; matched by N-number and serial number.ON LANDING ROLL-OUT, RIGHT MLG COLLAPSED AFT AND CAME TO REST AGAINST AFT PORTION OF WHEEL WELL.RETAINING PIN HAD SLIPPED OUT OF TRUNNION, ALLOWING GEAR TO COLLAPSE. THIS GEAR WAS PREVIOUSLY REMOVED FOR SPAR REPAIR. THE RETAINER BOLT WAS EITHER LEFT OUT OR WAS NOT INSTALLED CORRECTLY. OVER A…
From FAA Service Difficulty Reports; matched by N-number and serial number.AFT ELEVATOR TRIM/AUTOPILOT CABLE FRAYED WHERE IT GOES AROUND ELECTRIC TRIM AND AUTOPILOT SERVO PULLEYS.
From FAA Service Difficulty Reports; matched by N-number and serial number.REFER TO DOCKET NR (93-C3-61-AD). THIS PART IS THE MLG SWIVEL PIN ASSY. PART WAS DISASSEMBLED TO SEE IF IT COULD BE TIGHTENED UP. AFTER DISASSEMBLY AND CLEANING, CORROSION WAS NOTICED ON PIN SHANK AND RADIUS. SMALL CRACKS WERE FOUND WITH 10X MAGNIFYING GLASS. DYE-CHECK BOLT RT AND LT TO VERIFY THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.REFER TO DOCKET NR (93-C3-61-AD). THIS PART IS THE MLG SWIVEL PIN ASSY. PART WAS DISASSEMBLED TO SEE IF IT COULD BE TIGHTENED UP. AFTER DISASSEMBLY AND CLEANING, CORROSION WAS NOTICED ON PIN SHANK AND RADIUS. SMALL CRACKS WERE FOUND WITH 10X MAGNIFYING GLASS. DYE-CHECK BOLT RT AND LT TO VERIFY THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.