Service difficulty reports · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR F3LA2009122900274Cover · out of positionDURING CLIMB OUT, THE FLIGHT CREW RECEIVED SPURIOUS ECAM INDICATIONS RT DOOR EMERGENCY EXIT. MX REINSTALLED RT OVERWING EXIT HANDLE COVER FLAP AND ECAM INDICATION CHECKED NORMAL IAW AMM 25-23-47-420-127.SDR F3LA2009021600027Cable · lack of lubeDURING C3 C-CHECK, INSPECTION NOTED THAT THE RIGHT OVERWING EMERGENCY SLIDE CABLE FAILED THE FUNCTIONAL TEST OF THE SLIDE RELEASE SIGNAL AND OPERATIONAL TEST OF THE UNLOCKING AND OPENING FROM THE OUTER SIDE IN THE ARMED MODE. MAINTENANCE INSPECTED AND LUBED CSDR F3LA2009021600026Sill · corrodedDURING C3 C-CHECK, INSPECTION NOTED CORROSION AT THE FASTENER HOLE OF THE AFT GIRT BAR FITTING, L2 DOOR THRESHOLD. MAINTENANCE REMOVED THE CORROSION. FABRICATED REPAIR DOUBLER AND FILLER AND COMPLETED THE REPAIR PER ENGINEERING AUTHORIZATION A8-53R-30930.SDR F3LA2009021300025Floorbeam · corrodedREFERENCE NON-ROUTINE C057562. DURING C3 C-CHECK, INSPECTION NOTED CORROSION ON FLOORBEAM -Y1292 BETWEEN FRAME 66 AND FRAME 68. MAINTENANCE REMOVED AND REPLACED FLOORBEAM -Y1292 BETWEEN FRAME 66 AND FRAME 68 IN REFERENCE TO SRM 51-42-11 PARAGRAPHS 5 AND 7.SDR F3LA2008121600726Isolation Valve · crackedENROUTE AT FL330, PILOT REPORTED INDICATION OF HYDRAULIC RESERVOIR LOW LEVEL FOLLOWED BY ENGINE NR 2 PUMP LOW LEVEL AND NOTED THE YELLOW SYSTEM FLUID QUANTITY DEPLETED. MAINTENANCE INSPECTED THE NR 2 ENGINE AND FOUND THE THRUST REVERSER ISOLATION VALVE HYDRAUSDR F3LA200800507Floor Panel · puncturedLINE MAINTENANCE NOTED THE AFT CARGO PIT TRANSITION PANEL 151FG HAS PUNCTURE DAMAGE IN THREE PLACES ON UPPER SKIN. MAINTENANCE REPAIRED DAMAGE IN ACCORDANCE WITH A318 SRM 53-02-00, FIGURE 205.SDR F3LA200800506Floor Panel · puncturedLINE MAINTENANCE NOTED THE AFT CARGO PIT TRANSITION PANEL 151FH HAD PUNCTURE DAMAGE IN THREE PLACES ON THE UPPER SKIN. MAINTENANCE REPAIRED DAMAGE IN ACCORDANCE WITH A318 SRM 53-02-00, FIGURE 205.SDR F3LA200800077Cooling Fan · bindingDURING CRUISE, AT 35000, FLT CREW REPORTED LOUD NOISE AND VIBRATION FOLLOWED BY ACRID ODOR AND SMOKE IN COCKPIT. ECAM DISPLAYED BLOWER AND EXTRACTOR FAN FAULT. FLIGHT CREW DECLARED AN EMERGENCY, DIVERTED TO OKC AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANSDR F3LA200700195Line · leakingFLIGHT CREW REPORTED GREEN HYD QTY LOW IN CRUISE. PERFORMED LANDING GRAVITY EXTENSION PER FOM VOL II. REPLACED NR 1 ENGINE T/R ISOLATION VALVE PRESSURE HYDRAULIC LINE. PERFORMED OPS AND LEAK CHECK IAW 8-37-51-PB-401. CHECKED GOOD. RESET FREE FALL EXTENSIOSDR F3LA200700177Floor Panel · puncturedDURING C-2 CHECK, INSPECTION REPORTED PUNCTURE ON TOPSIDE OF AFT CARGO COMPARTMENT FLOOR PANEL 161QF. REPAIRED AFT CARGO COMPARTMENT FLOOR PANEL 161QF IAW SRM 53-02-00, FIG 204.SDR F3LA200700176Floor Panel · damagedDURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR PANEL 161QF DAMAGED. REPAIRED FLOOR PANEL 161QF IAW A318 SRM 53-02-00, FIG 204.SDR F3LA200700175Panel · puncturedDURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT TRANSITION PANELS 151FH, 151HH, AND 162SF DAMAGED. REPAIRED PUNCTURES IN PANELS IAW A318 SRM 53-20-00, PB 201, PARA 8C, FIG 204.SDR F3LA200700174Panel · damagedDURING C-2 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT TRANSITION PANEL 131BF DAMAGED. REPAIRED PUNCTURE IAW A318 SRM 53-20-00, PB 201, PARA 8.C., FIG. 204.SDR F3LA200700031Windshield · crackedAIR TURN BACK, CAPTAIN'S FWD WINDSHIELD SHATTERED. REPLACED CAPTAINS FWD WINDSHIELD IAW 56-11-11, PB401.SDR F3LA200600088Flap System · malfunctionedON APPROACH ECAM FLAPS LOCKED. FLAPS WOULD NOT EXTEND BEYOND F2, SLATS EXTEND NORMALLY. MAINTENANCE PERFORMED TROUBLESHOOTING PER TSM 27-51-00-810-818, OPERATIONAL TEST OK. FLAP ALIGNMENT OK. NO ALIGNMENT OR FLAP FAULT NOTED DURING TEST. PER TSM 27-51-00-