Service difficulty reports · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR IXXA0300014OComputer · failedAFTER DEPARTURE FROM MCO DURING CLIMBOUT DESTINED FOR TOL AIRCRAFT EXPERIENCED YAW ABNOMALY. CREW ELECTED TO RETURN TO MCO. AFTER UNEVENTFUL LANDING IN MCO MAINTINANCE INSPECTED SYSTEM AND TRANSFERRED THE YAW DAMPNER TO MEL. ALL WORK COMPLETED PER APPLICABLSDR IXXA0200090ODuct · damagedAFTER TAKE OFF FROM ANC, THE FIRE WARNING LIGHT ILLUMINATED AND THE AUDIO WARNING SOUNDED FOR THE NUMBER THREE ENGINE. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND SECURED THE ENGINE. THE FLIGHT RETURNED TO ANC FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPESDR IXXA0100022Sensing Element · shortedEN ROUTE FROM TOL TO LAX, THE NUMBER TWO ENGINE FIRE WARNING SHORT CIRCUIT LIGHT ILLUMINATED INTERMITTENTLY. THE FLIGHT CREW SECURED THE ENGINE FOLLOWING COMPANY PROCEDURES AND RETURNED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE FIRE SDR IXXA0100012Starter · defectiveEN ROUTE FROM TOL TO LAX, THE FLIGHT CREW NOTICED A DECLINE IN THE NUMBER TWO ENGINE OIL QUANTITY SYSTEM. THE FLIGHT CREW SECURED THE ENGINE FOLLOWING COMPANY PROCEDURES FOR PRECAUTIONARY MEASURES. THE FLIGHT CONTINUED TO LAX FOR AN UNEVENTFUL LANDING. MAINSDR IXXA0100011OEngine · leakingEN ROUTE FROM LAX TO SAN, THE FLIGHT CREW NOTICE A DECLINE OF OIL QUANTITY ON THE NR 2 ENGINE. THE FLT CREW SECURED THE ENGINE FOLLOWING COMPANY PRECEDURES FOR PRECAUTIONARY MEASURES. THE FLIGHT CONTINUED TO SAN FOR AN UNEVENTFUL LANDING. MAINTENANCE SERVICSDR IXXA0100015Skin · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON LEFT WING OUTER WING SKIN PANEL AT STATION XRS 533.3, STRINGER 62 END FITTING. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA. FABRICATION AND INSTALLATION AN REPAIR FILLER, DOUBLER AND TRIPLER IN ACCORSDR IXXA0100014Stringer · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED AT THE RIGHT WING STRINGER 54 AT WING STATION 510. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA. FABRICATION AND INSTALLATION OF A CHANNEL FILLER AND TWO REPAIR ANGLES IN ACCORDANCE WITH FAA DER APPRSDR IXXA199571Attach Fitting · crackedDURING C-CHECK, THE LEFT MLG ATTACH FITTING WAS FOUND TO BE CRACKED. A CRACK IN EXCESS OF 2.5 INCHES WAS LOCATED IN THE BOTTOM OF LUG 'D' OF THE ATTACH FITTING. (SEE SB 57-94, VIEW JJ). THE ATTACH FITTING WAS REPLACED IAW THE DC-8 SRM, MM, AND DOUG INSTALLASDR IXXA199543Downlock Switch · out of adjustTOL - ON APPROACH, NO NOSE LANDING GEAR DOWN INDICATION WAS OBTAINED WHEN THE LANDING GEAR WAS EXTENDED, AND THE LANDING GEAR UNSAFE LIGHT WAS ILLUMINATED. THE LANDING GEAR WAS CYCLED FOUR TIMES, AND A SAFE INDICATION WAS OBTAINED AND VISUALLY VERIFIED. ON T