N802FR

Part: LINE — WORN (HYDRAULIC SYS) · airframe 23,989 hrs · 12,565 cycles

REFERENCE LOG PAGE, NR 535350, ITEM 1. ECAM HYD YELLOW LOW LEVEL INDICATION. FOUND DAMAGED HYD LINE IN NR 2 ENG PYLON. REPLACED LINE REF AMM 29-13-49-000-049 AND 29-13-49-400-049.

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 23,476 hrs · 12,295 cycles

DURING CLIMB THE FLIGHT CREW NOTED THE GREEN HYD SYS FLUID LEVEL WAS LOW. MX R & R THE RT MLG DOOR ACTUATOR AFT HYD HOSE AND SERVICED THE GREEN HYD SYS AMM IAW 32-31-38 PB 401 AND AMM 29-00-00-870-003.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 23,189 hrs · 12,139 cycles

DURING HEAVY SERVICE CHECK MX NOTED ROW 19 ABC SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. MX DEFERRED SEAT MOUNTED EMERGENCY LIGHT AT 19 ABC IAW MEL 33-50-03B, CNTRL NR 1073010. FINAL C/A TO BE ACCOMPLISHED AT A CLASS 1 OR CLASS 2 STATION.

Part: TRANSMITTER — INOPERATIVE (OIL PRESSURE) · airframe 20,299 hrs · 10,553 cycles

AIR TURN BACK, PILOT REPORTED THAT AFTER TAKEOFF, ENGINE NR 2 OIL PRESSURE GAUGE INDICATED ZERO PRESSURE. INDICATION ALTERNATED BETWEEN RED 0 AND AMBER XX. ALL OTHER INDICATIONS WERE NORMAL, NO ELECTRONIC CENTRALIZED AIRCRAFT MONITORING WARNING. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE OIL PRESSURE TRANSMITTER AND PERFORMED OPERATION AND LEAK CHECK IAW AMM 79-33-15 PB 401.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,834 hrs · 10,303 cycles

EMERGENCY PATH LIGHT PARTIALLY BURNED OUT AT SEAT ROWS 9 AND 13. MAINTENANCE REMOVED AND REPLACED EMERGENCY PATH LIGHT ASSEMBLY AND PERFORMED OPERATIONAL CHECK, REFERENCE AMM 33-51-19 PB401.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 19,331 hrs · 10,027 cycles

DURING C4 C-CHECK, INSPECTION NOTED THE EMERGENCY PATH LIGHTING AT SEAT 7 ABC INOPERATIVE. MAINTENANCE FOUND PUSHED BACK PIN ON ROW 7 SEAT CONNECTOR, LOCKED PIN IN PLACE AND PERFORMED OPERATIONAL CHECK IN ACCORDANCE WITH AMM 33-51-00-710-009.

Part: SUPPORT — CRACKED (LANDING GEAR) · airframe 18,026 hrs · 9,295 cycles

DURING SCHEDULED MAINT TASK CARD TC32711-02, INSP NOTED A CRACK ON THE FWD ANTI-ROTATION LUG. MAINT REMOVED AND REPLACED THE UPPER SUPPORT ASSEMBLY IAW THE REQUIREMENTS OF ENGINEERING AUTHORIZATION A8-32R-30496. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: EPSU — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,516 hrs · 7,480 cycles

FLIGHT CREW REPORTED EMERGENCY EXIT LIGHT OVER AFT GALLEY ENTRY INOP. REPLACED EPSU 13WL IAW AMM 33-51-35.

Part: DOOR — INOPERATIVE (LAV OXY MASK) · airframe 13,757 hrs · 7,079 cycles

DURING C-3 CHECK, INSPECTION REPORTED O2 MASK DOOR DID NOT OPEN IN LAV E DURING MANUAL MASK DROP TEST. REPLACED EMERGENCY OXYGEN CONTAINER FOR AFT LAV IAW AMM 35-21-41-400-001 AND CHECKED GOOD.

Part: EPSU — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,757 hrs · 7,079 cycles

DURING C-3 CHECK, INSPECTION REPORTED ROW A EMERGENCY EXIT SEAT LIGHTING INOP. REPLACED EPSU IN FWD GALLEY. OPS CHECKED GOOD IAW AMM 33-51-38-PB 401.

Part: GIRT BAR — CORRODED (L2 DOOR) · corrosion level 2 · airframe 13,757 hrs · 7,079 cycles

DURING C-3 CHECK, INSPECTION REPORTED L2 FWD GIRT BAR FITTING AND HARDWARE CORRODED. REPLACED GIRT BAR BLANKING PLATE IAW 52-13-31-400-007.

Part: GIRT BAR — CORRODED (R2 DOOR) · corrosion level 2 · airframe 13,757 hrs · 7,079 cycles

DURING C-3 CHECK, INSPECTION REPORTED R2 FWD GIRT BAR FITTING AND HARDWARE CORRODED. REPLACED GIRT BAR BLANKING PLATE IAW AMM 52-13-31-400-007.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,757 hrs · 7,079 cycles

DURING C-3 CHECK, INSPECTION REPORTED FLOOR PANEL 221FF CORRODED. REPLACED FLOOR PANEL 221FF IAW AMM 53-12-12-400-001.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,757 hrs · 7,079 cycles

DURING C-3 CHECK, INSPECTION REPORTED FLOORBOARD THRESHOLD STRIP 222FF CORRODED AROUND FASTENER HOLES. REPLACED FLOORBOARD THRESHOLD STRIP IAW AMM 53-12-12-400-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,757 hrs · 7,079 cycles

DURING C-3 CHECK, INSPECTION REPORTED SURFACE CORROSION ON CABIN FLOOR FR20 AT -Y765 (RT I/B SEAT TRACK). REPLACED SEAT TRACK IAW SRM 51-42-11 AND 51-72-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,757 hrs · 7,079 cycles

DURING C-3 CHECK, INSPECTION REPORTED FLOOR PANEL 262FF CORRODED. REPLACED PANEL 262FF IAW 53-42-12, PB 401.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,757 hrs · 7,079 cycles

DURING C-3 CHECK, INSPECTION REPORTED FLOOR PANEL 261FF CORRODED. REPLACED PANEL 261FF IAW AMM 53-42-12, PB 401.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,757 hrs · 7,079 cycles

DURING C-3 CHECK, INSPECTION REPORTED AFT LT LONGITUDINAL BEAM Y1292 HAD SURFACE CORROSION IN FASTENER HOLES AND ON TOP SURFACE. REPLACED CORRODED FLOORBEAMS (P/N D5347217220400 AND D5347218820400) AND COUPLING JUST FWD OF FR67 THRU FR 69 IAW A318 SRM 53-41-14, 51-44-21 AND 51-42-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,757 hrs · 7,079 cycles

DURING C-3 CHECK, INSPECTION REPORTED AFT RT SHEAR PLATE HAD SMALL AMOUNT OF CORROSION BETWEEN FR 69 AND FR 70. REPLACED AFT RT SHEAR PLATE IAW SRM 51-42-11 AND 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,757 hrs · 7,079 cycles

DURING C-3 CHECK, INSPECTION REPORTED AFT LT SHEAR PLATE CORRODED BETWEEN FR 69 AND FR70. REPLACED AFT LT SHEAR PLATE IAW SRM 51-42-11.

Part: CONNECTOR — CONTAMINATED (R1 DOOR SLIDE) · airframe 10,699 hrs · 5,483 cycles

R1 DOOR SLIDE ARMED INDICATION INOP ON ECAM AND CIDS PANEL. REMOVED R1 DOOR LINING. DISCONNECTED R1 SLIDE PROX SWITCH CONNECTOR AND FOUND GREASE CONTAMINATION. CLEANED AND RECONNECTED CONNECTOR. REINSTALLED R1 DOOR LINER. OPS CHECKED GOOD.

Part: TRANSMITTER — UNSERVICEABLE (ELEVATORS) · airframe 6,738 hrs · 3,299 cycles

AIR TURNBACK DUE TO FAULT, FLT/CTL ALTN LAW L&R AIL FAULT. REPLACED CAPTAIN'S SSTU 4CE1 PER AMM 27-92-41, PB 401. PERFORMED OPERATIONAL TEST PER AMM 27-92-41-710-001. REPLACED ELEV SERVO 34CE3 PER AMM 27-34-56-400-001. PERFORMED OPERATIONAL TEST, OPS CHECK GOOD. REPLACED NR 1 & NR 2 FCDC, PERFORMED OPS CHECK. PERFORMED FLIGHT CONTROL CHECKS PER GMM 50-13 FUNCTIONAL CARDS C271001-1 THRU C271001-6. PERFORMED AFS TEST PER AMM 22-96-00-710-001. NR 2 ELAC NOT REPLACED. PERFORMED LAND CAT III TEST, TEST OKAY. ACFT RETAINS CAT III STATUS. PERFORMED OPERATIONAL TEST FLIGHT. TEST FLIGHT SATISFACTORY. PERFORMED POST FLIGHT WALKAROUND AND FOUND AIRCRAFT SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE.

Part: COMPUTER — UNSERVICEABLE (ELAC 1) · airframe 6,738 hrs · 3,298 cycles

AIR TURNBACK DUE TO FAULT: FLT/CTL ALTN LAW PROT LOST ECAM. PERFORMED EFCS GROUND SCAN PER AMM 27-96-00-740-001. FOUND ELAC NR 1 FAULT. REPLACED ELAC NR 1 PER AMM 27-93-34, PB401. PERFORMED OPS TEST OF ELAC NR 1 PER AMM 27-93-00-710-001 AND TESTED OKAY. NO FAULTS NOTED. PERFORMED LAND CAT III OPERATIONAL TEST PER AMM 22-97-00-710-001 AND TESTED OKAY. AIRCRAFT CAT IIIB STATUS RETAINED.

Part: FILTER — MALFUNCTIONED (VALVE BLOCK) · airframe 1,215 hrs · 599 cycles

BLOCK TURNBACK. FLIGHT CREW REPORTED F/CTL SLAT SYS 1 FAULT. COMPLETED CONTINUITY CHECK BETWEEN SFCC NR 1 AND SLAT FFPU IAW ASM 27-81-00 SCH06 AND CHECKED GOOD. REPLACED FILTER IAW TSM ON FLAP/SLAT VALVE BLOCK NR 1 IAW MM 27-84-53-400-03.