Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR I5HA041108001Volt Regulator · out of adjustAFTER CLIMB OUT, THE CREW LOST THE NR1 DC GENERATOR. AS A PRECAUTIONARY MEASURE THEY RETURNED TO DEPARTURE FOR MAINT TO CORRECT THE PROBLEM. MAINT RERACKED THE NR1 DC GEN CONTROL PANEL AND PARALLEL THE DC GENERATORS IAW THE MM. THE AC WAS RETURNED TO SERVICE ASDR I5HA0758012Pump · crackedDURING DEPARTURE, ENROUTE, THE CREW LOST HYDRAULIC PRESSURE AND RETURNED TO DEPARTURE. THE AIRCRAFT LANDED UNEVENTFULLY AND WAS TOWED TO A PARKING SPACE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE ENGINE DRIVEN HYDRAULIC PUMP HAD FAILED AND PUMPED ALL THSDR I5HA058005Regulator · fluctuatesDURING TAKEOFF ROLL, CREW OBSERVED WHAT THEY BELIEVED TO BE A LOSS OF POWER FROM THE LT ENGINE. TAKEOFF WAS ABORTED AND AC RETURNED FOR MAINT. AFTER PERFORMING INSP FOR FOD, WATER IN THE FUEL FILTERS, BLEED AIR LEAKS AND A HIGH POWER PENALTY RUN, THE AC WAS SDR I5HA058004Uplock · out of rigCREW OBSERVED LANDING GEAR UNSAFE LIGHT AND FELT THE NOSE LANDING GEAR EXTEND DURING THE CLIMB OUT, AFTER THE HYDRAULIC BYPASS WAS SELECTED TO BYPASS. CREW SHIFTED THE HYDRAULIC BYPASS HANDLE BACK TO THE PRESSURE POSITION AD THE LANDING GEAR CAME UP AND LOCKESDR I5HA0558002Tie · crackedDURING A ROUTINE INSP, A CRACK WAS DISCOVERED AT THE POWER SECTION END ON THE IB TIE STRUT ON THE RT ENGINE. CRACK WAS LOCATED IN THE WELD AREA ON THE END CLOSEST TO THE POWER SECTION. A THROUGH INSPECTION WAS DONE ON THE REST OF THE ENGINE FOR EVIDENCE OF OSDR 15HA03580005Lever · crackedAFTER TAKEOFF FROM PIT, EN ROUTE TO MIDDLETOWN, THE PILOT OBSERVED A LANDING GEAR 'UNSAFE' LIGHT AFTER GEAR RETRACTION. THE PILOT LOWERED THE GEAR AND PROCEEDED, GEAR DOWN, TO THE COLUMBUS MAINTENANCE FACILITY. THE LANDING GEAR 'UNSAFE' LIGHT WAS EXTINGUISHE