N634VA

Part: WIRE — DAMAGED (EMERGENCY LIGHTS)

DURING PRE DEPARTURE THE SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 22L AND 23L WERE FOUND INOPERATIVE. R & R THE BASE CONNECTOR 7260 VC9 IAW ESPM 20-44-00 AND REPAIRED A DAMAGED WIRE. OPS CHECKED GOOD. OK FOR SERVICE.

Part: SKIN — CORRODED (RT WING)

CORROSION FOUND ON THE RIGHT WING LOWER SURFACE SKIN BETWEEN RIBS 11 AND 12, NR 2 SPOILER ACTUATOR FITTING AREA. THE CORROSION WAS REMOVED AND FOUND TO BE WITHIN LIMITS IAW SRM 67-21-11.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 31,845 hrs · 9,432 cycles

EXPERIENCED A F/O WINDSHIELD OUTER PANE FAILURE DURING CRUISE FLIGHT. THE ACFT DIVERTED AND THE WINDSHIELD WAS REPLACED, THE WINDSHIELD HAD NO HISTORY OF HEAT FAULTS OR PREVIOUS DELAMINATION’S NOTED. THERE WAS NO LOSS OF CABIN PRESSURE OR STRUCTURAL INTEGRITY OF THE INNER PANE.

Part: SHEAR PLATE — CORRODED (FUSELAGE)

RT AFT SHEAR PLATE BETWEEN FR 69-70, S23-24R CORRODED BEYOND LIMITS. SHEAR PLATE WAS REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN)

CABIN AFT FLOOR SEAT TRACK BETWEEN FRAMES 64-65, AT Y765 HAS AN AREA OF CORROSION. SEAT TRACK WAS R & R IAW SRM 51-42-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE)

RT AFT SHEAR PLATE SUPPORT BETWEEN FR 69-70, S23R CORRODED BEYOND LIMITS. SHEAR PLATE SUPPORT WAS REPLACE IAW SRM 51-42-11.

Part: BEAM — CORRODED (FUSLEAGE)

LEFT AFT DOOR SILL BEAM HAS TWO AREAS OF CORROSION BETWEEN FR 66-68, S23-24L, AT Y1725. THE AREAS WERE REPAIRED IAW SRM 53-41-14, FIG 201K, PRINCIPLE 5.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70)

CABIN AFT FLOOR SUPPORT BETWEEN FRAMES 66-70, Y765 HAS AN AREA OF CORROSION. FLOOR SUPPORT R & R IAW SRM 51-42-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE)

LT AFT SHEAR PLATE, BETWEEN FR 69-70, S23-24L CORRODED BEYOND LIMITS. SHEAR PLATE WAS REPLACED IAW SRM 51-42-11.

Part: UNKNOWN — ODOR (CABIN) · airframe 21,459 hrs · 6,450 cycles

REPORTED AN ELECTRICAL BURNING ODOR IN AFT GALLEY AND CABIN AREA. CREW TURNED OFF THE IN SEAT POWER SUPPLY MASTER SWITCH AS WELL AS THE AFT GALLEY COFFEEMAKER, THE ODOR DISSIPATED. ARRIVED WITH NO FURTHER REPORTS. MX ACCOMPLISHED TSM PROCEDURE 24-00-810-023A WITH NO FINDINGS. ACFT RETURNED TO SERVICE WITH NO FURTHER REPORTS.

Part: LINE — DAMAGED (HYD SYSTEM)

ON INITIAL CLIMB, IT WAS REPORTED OF POSSIBLE SMOKE FROM AROUND LEFT WHEELWELL. ALL SYS WERE NORMAL AND INDICATING NORMAL TEMPERATURE RANGES, ACCORDING TO FLIGHT CREW. CONTINUED TO DESTINATION. CREW CHECK SYS PAGES AND NOTICED A SLOW DECLINE OF HYDRAULIC FLUID IN GREEN SYS. DECIDED TO DIVERT. ON ARRIVAL AND GEAR DOWN, ECAM TRIGGERED ON FINAL FOR GREEN HYD SYS. ACFT LANDED WITHOUT INCIDENT. ON INSPECTION, FOUND LT MLG DOOR ACTUATOR HYD LINE LEAKING FLUID. LINE R & R IAW AMM 20-23-11-9-17-002-A AND LEAK AND OPS CHECKED GOOD.

Part: PLATE — CRACKED (LT PYLON) · airframe 19,776 hrs · 5,956 cycles

ACFT WAS BEING INSPECTED BY COMPANY PERSONNEL IAW TC 5454.000001LH. DURING THIS INSPECTION, CRACKING WAS FOUND ON THE INBD SIDE OF THE LT PYLON AFT FIXED FAIRING UPPER SPAR. SPECIFICALLY, THE INBD FLANGE OF THE AFT FIXED FAIRING UPPER SPAR PLATE WAS FOUND CRACKED BETWEEN RIBS 14 AND 15. THE UPPER SPAR PLATE WAS CRACKED AREA 1 AND HAS PROPAGATED INTO AREA 2. ACCOMPLISHED THE REPAIR OF THE LT PYLON AFT FIXED FAIRING UPPER SPAR PLATE BETWEEN RIBS 14 AND 15 IAW TECH DISPOSITION TD-J2-S2-0310-2013 ISSUE A.

Part: BEARING — DAMAGED (L1 DOOR)

CREW REPORTED TO MX THAT THE L1 DOOR WAS DIFFICULT TO OPEN. DURING TROUBLESHOOTING, MX VERIFIED THE 1 LT DOOR UPPER SUPPORT BUSHING AND BOLT GALLED. 1 LT DOOR DAMPER/ EMERGENCY OPERATION CYLINDER DISARMED TO FACILITATE MAINTENANCE. 1 LT DOOR ESCAPE SLIDE PACK ASSY REMOVED TO FACILITATE MX IAW AMM 25-62-44-04. R & R 1 LT DOOR SUPPORT ARM UPPER BUSHINGS AND BOLT IAW SRM 51-72-12. 1 LT DOOR ESCAPE SLIDE PACK ASSY REINSTALLED IAW AMM 25-62-44-04. 1 LT DOOR DAMPER/EMERGENCY OPERATION CYLINDER RE-ACTIVATED IAW AMM 52-10-00. ALL DOOR OPS CHECK NORMAL. ACFT RELEASED TO SERVOCE ON 5/24/2012.