Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QM7R201906142502Bracket · crackedONE TIME INSPECTION FOR CRACK/BREAK OF THE RUDDER CONTROL MECHANISM BRACKET. THE INSPECTION RESULTED IN IDENTIFYING A CRACK AT BOTTOM OF RADIUS.SDR 96ZZZX2896Wire · chafedON TEST FLIGHT, AC NR 2 GENERATOR LIGHT CAME ON. DURING TROUBLESHOOTING OF SYSTEM, FOUND WIRE 2420-20001E12A-1 GROUNDED OUT. CONDUIT PASSES BETWEEN REAR SPAR AND FLAP PRIMARY CONTROL TUBE. AREA WHERE WIRES PASS THROUGH IS PRESSED AND WIRE RUBS CONDUIT. SUBSDR 95ZZZX5850Foreflap · corrodedON D-INSPECTION, NDT DEBOND CHECK OF RIGHT FOREFLAP FOUND CORROSION OF STR 14 AT STA YW257.35. SUBMITTER STATED REAR FOREFLAP PANELS NEED REMOVAL AT INSPECTION AND INSPECT FOR CORROSION OF BOTTOM SKIN AND HINGE AREA BY BORECOPE AND DEBOND INSPECTIONS.SDR 95ZZZX5849Foreflap · arm corrodedON D-INSPECTION OF FLIGHT CONTROLS, FOUND CORROSION ON INBD FORFLAP HINGE ARM UNDER PANEL COVER. PANELS ARE NOT REQUIRED TO BE REMOVED ON INSPECTION. PANELS NEED REMOVAL FOR CORROSION INSPECTION.SDR 95ZZZX5848Strut Pin · corrodedON A D-INSPECTION, REPLACED HARDWARE FOR UPPER DRAG STRUT AND WHEN STRUT PINS WERE REMOVED, THEY HAD CORROSION AND PITTING. SUBMITTER STATED WHEN HARDWARE IS SHOWING CORROSION, PINS NEED TO BE INSPECTED FOR CORROSION.SDR 95ZZZX5847Strut Pin · corrodedON A D-INSPECTION, REPLACED HARDWARE FOR UPPER DRAG STRUT AND WHEN STRUT PINS WERE REMOVED, THEY HAD CORROSION AND PITTING. SUBMITTER STATED WHEN HARDWARE IS SHOWING CORROSION, PINS NEED TO BE INSPECTED FOR CORROSION.SDR 95ZZZX5846Foreflap · corrodedON D-INSPECTION OF FLIGHT CONTROLS, FOUND A HINGE ARM WITH CORROSION AND, WITH THE OTHER FLAP PANELS OPEN, FOUND CORROSION AROUND PANEL NUTPLATES, STA YW367.90 TO STA YW423.30. SUBMITTER STATES PANELS NEED REMOVAL AT INSPECTION OF FOREFLAP.SDR 95ZZZX5845Foreflap · corrodedON D-INSPECTION OF FLIGHT CONTROLS OF LEFT FOREFLAP, FOUND CORROSION ON BOTTOM STR 12 AND STR 14 WITH BORESCOPE, STA YW242.17 TO YW257.35. FOREFLAP PANELS ARE NOT REQUIRED TO BE REMOVED ON INSPECTION. SUBMITTER STATED THEY NEED REMOVAL FOR INSPECTION OF CORRSDR 95ZZZX5868Pin · corrodedDURING D-INSPECTION, RIGHT MLG UPPER DRAG STRUT PINS WERE REMOVED AND FOUND TO HAVE CORROSION AND PITTING. SUBMITTER STATED NEED TO INSPECT BY REMOVING PINS. PINS ARE NOT NORMALLY INSPECTED.SDR 95ZZZX5867Pin · corrodedDURING D-INSPECTION, RIGHT MLG UPPER DRAG STRUT PINS WERE REMOVED AND FOUND TO HAVE CORROSION AND PITTING. SUBMITTER STATED NEED TO INSPECT BY REMOVING PINS. PINS ARE NOT NORMALLY INSPECTED.
Other aircraft with N89068 · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N89068 now.