N526VA

Part: UNKNOWN — ODOR (CABIN)

OPERATING FLIGHT ARRIVED IN AT DESTINATION WITH A REPORT OF AFT CABIN TRIM VALVE ERRATIC AND A FAINT ELECTRICAL BURNING ODOR REPORTED BY THE AFT CABIN CREW. THE ACFT WAS INSPECTED BY MAINTENANCE AND NO DEFECTS WERE NOTED. IFE SYSTEM WAS INSPECTED, REF TBN 4430-04 WITH NO DEFECTS NOTED. TEMP CONTROL SYSTEM WAS TESTED IAW MM 21-63-00-710-004A, NO DEFECTS NOTED. NO FURTHER PROBLEMS REPORTED ON SUBSEQUENT FLIGHTS.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 24,716 hrs · 8,459 cycles

DURING APPROACH, REPORTED LOSS OF YELLOW AND GREEN SYSTEM HYDRAULIC PRESSURE AND A LOSS OF GREEN HYDRAULIC FLUID. YELLOW SYS WAS RECOVERED SHORTLY AFTER. CREW REPORTED AN EMERGENCY BUT LANDED SAFELY. MAINTENANCE DISCOVERED A MLG DOOR ACTUATOR HOSE ON THE LT SIDE LEAKING. R & R IAW AMM 32-31-39-401, NO LEAKS NOTED AFTERWARD, ALL OPS CHECKS NORMAL AND THE ACFT WAS PLACED BACK INTO SERVICE AT 12:52Z ON 11/18/14.

Part: PROXIMITY SENSOR — OUT OF LIMITS (MLG)

DURING ATTEMPTED GEAR RETRACTION, RECEIVED A NLG SHOCK ABSORBER ECAM WARNING. THE GEAR HANDLE WOULD NOT ALLOW SELECTION TO UP POSITION DUE TO THE FAULT. IN APPROXIMATELY 30 SECONDS, THE CREW TRIED A SECOND ATTEMPT TO RETRACT LANDING GEAR WITH SAME RESULT, ACFT RETURNED TO DEPARTURE. AFTER AN UNEVENTFUL LANDING, MAINTENANCE MET ACFT AND ACCOMPLISHED A VISUAL INSPECTION OF THE LANDING GEAR, WITH NO OBVIOUS DEFECTS NOTED. MAINTENANCE ACCOMPLISHED TSM 32-31-73-200-002-A. PROXIMITY SENSORS 24GA & 25GA WERE FOUND OUT OF LIMITS. NOSE GEAR SHOCK ASORBER WAS ALSO REMOVED AND INSPECTED FOR ABNORMAL WEAR. MINOR WEAR WAS NOTED AND THE AFFECTED PARTS WERE REPLACED BY MAINTENANCE. SHOCK ABSORBER WAS REINSTALLED AND 24GA & 25GA WERE ADJUSTED IAW AMM 32-31-73-200-002-A. LANDING GEAR WAS SUCCESSFULLY CYCLED ON THE GROUND WITH NO FURTHER FINDINGS. SUCCESSFUL ACCEPTANCE FLIGHT WAS ACCOMPLISHED AND ACFT WAS RETURNED TO SERVICE.

Part: SKIN PANEL — CORRODED (LT WING)

DURING ACCOMPLISHMENT OF SB A320-57-1155, REV 3, CORROSION WAS DETECTED ON THE LOWER SURFACE OF THE LT WING TOP SKIN PANEL. AREA BLENDED IAW SRM 57-21-11. HFEC INSPECTION PERFORMED, REVEALING NO CRACK INDICATIONS. REPAIRED IAW EC 5720.000004. REPAIR CLASSIFIED AS MAJOR .

Part: SILL — CORRODED (FRAMES 16-17)

R1 DOOR SILL HAS CORROSION AROUND THE FWD TWO HOLES AT THE AFT GIRT BAR ATTACH FITTING. AREAS WERE REPAIRED IAW SRM 53-11-14, FIG 108, SPOT FACING TO REMOVE .025" MATERIAL AND INSTALLING REPAIR WASHERS FABRICATED.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-68)

FLOOR SUPPORT BETWEEN FRAMES 67-68 AT Y765 CORRODED. FLOOR SUPPORT WAS R & R IAW SRM 51-41-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66)

FLOOR SUPPORT BETWEEN FRAMES 64-66 AT Y1292 CORRODED. FLOOR SUPPORT WAS FABRICATED IAW DWG D53472209. INSTALLATION WAS PERFORMED IAW AMM 51-42-11.

Part: SHEAR PLATE — CORRODED (FRAMES 69-70)

RIGHT AFT SHEAR PLATE BETWEEN FR69-70, S23-24R CORRODED BEYOND LIMITS. SHEAR PLATE WAS REPLACED IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-68)

FLOOR SUPPORT BETWEEN FRAMES 67-68 AT Y765 CORRODED. FLOOR SUPPORT R & R IAW SRM 51-41-11.

Part: UNKNOWN — ODOR (CABIN)

THE IN FLIGHT TEAM REPORTED ELECTRICAL BURNING ODOR IN THE CABIN. THE INFLIGHT TEAM MEMBER IMMEDIATELY SHUTDOWN THE IFE SYSTEM. THE ODOR DISSIPATED AND NO OTHER ISSUES NOTED. LANDING WAS UNEVENTFUL. MX ACCOMPLISHED TSM 24-00-00-810-823A FOR ELECTRICAL BURNING ODOR OR FUMES IN THE CABIN, COCKPIT, CARGO OR AVIONICS BAY. NO ODOR NOTED, RELATED ACFT SYS. IFE SYSTEM POWER RESTORED AND OPERATED. THERE WERE NO ASSOCIATED ODORS NOTED. ACFT WAS RELEASED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN)

MX MET ACFT AND THERE WAS INBD DEFECT REPORTED IN LOGBOOK: FWD GALLEY SMOKE SMELL BY ITL ASSOCIATED WITH OVEN ON . MX INSPECTED AND PERFORMED OPS CHECK OF OVEN AND NO FAULTS OR SMELL NOTED. NO ADDITIONAL REPORTS OF THIS ON SUBSEQUENT FLIGHTS.