N806FR

Part: WARNING LIGHT — FAILED (OVERWING SLIDE) · airframe 16,334 hrs · 8,454 cycles

PILOT REPORTED THAT THE LEFT OVERWING EXIT SLIDE ARMED LIGHT IS ILLUMINATED WHEN ON MAINTENANCE BUS. EMERGENCY EXIT OPEN ECAM INDICATION. MAINTENANCE REMOVED AND REPLACED LEFT OVERWING SLIDE ARMED INDICATOR LIGHT AND PERFORMED OPERATIONAL TEST IN ACCORDANCE WITH A318 AMM 52-73-21-000-003.

Part: CONTROL PANEL — FAILED (EMERGENCY LIGHT) · airframe 16,321 hrs · 8,447 cycles

PILOT REPORTED THE LEFT OVERWING EXIT SHOWS OPEN ON LOWER ECAM. MAINTENANCE PERFORMED TROUBLESHOOTING AND FOUND LEFT OVERWING LIGHT TO BE AT FAULT. THE WARNING LIGHT PANEL WAS REMOVED, REPLACED AND CHECKED IN ACCORDANCE WITH A318 AMM 52-73-21 PB 401.

Part: BLANKING PLATE — CORRODED (GIRT BAR) · corrosion level 2 · airframe 15,487 hrs · 7,973 cycles

DURING C-CHECK, INSP NOTED L2 FWD GIRT BAR BLANKING PLATE HAS CORROSION. MAINT REMOVED AND REPLACED BLANKING PLATE WITH NEW ONE FROM STOCK AND INSTALLED ON TASK CARD C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: BLANKING PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,487 hrs · 7,973 cycles

DURING C-CHECK, INSP NOTED L2 AFT GIRT BAR BLANKING PLATE HAS CORROSION. MAINT REMOVED AND REPLACED BLANKING PLATE WITH NEW ONE FROM STOCK AND INSTALLED ON TASK CARD C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,487 hrs · 7,973 cycles

DURING C3 C-CHECK, INSP NOTED FLOOR PANEL 261FF HAS CORROSION ON LOWER SURFACE. MAINT REMOVED AND REPLACED FLOOR PANEL 261FF WITH A NEW PANEL AND INSTALLED ON TASK CARD C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,487 hrs · 7,973 cycles

DURING C-CHECK INSP, NOTED CORROSION AROUND NUT CLIP HOLE APPROX 4.25 INCHES AFT OF FWD END ON RT SIDE FLOORBEAM ALONG Y1292 BETWEEN FR68 AND FR69. MAINTENANCE BLENDED AREA, FABRICATED FLANGE BUSHING AND INSTALLED IAW THE REQUIREMENTS OF ENGINEERING AUTHORIZATION A8-53R-30558. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: BLANKING PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,487 hrs · 7,973 cycles

DURING C-CHECK INSP, NOTED R2 FWD GIRT BAR BLANKING PLATE HAS CORROSION. MAINT REMOVED AND REPLACED BLANKING PLATE WITH NEW ONE FROM STOCK AND INSTALLED ON TASK CARD C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: BLANKING PLATE — CORRODED (GIRT BAR) · corrosion level 2 · airframe 15,487 hrs · 7,973 cycles

DURING C-CHECK, INSP NOTED R2 AFT GIRT BAR BLANKING PLATE HAS CORROSION. MAINT REMOVED AND REPLACED BLANKING PLATE WITH NEW ONE FROM STOCK AND INSTALLED ON TASK CARD C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,487 hrs · 7,973 cycles

DURING C3 C-CHECK, INSPECTION NOTED THE VERY AFT NUT PLATE HOLE ON L-2 DOOR SILL AT FRAME 68, JUST AFT OF GIRT BAR FITTING ASSEMBLY, WAS CORRODED. MAINTENANCE CUTOUT DAMAGE, MANUFACTURED REPAIR DOUBLER AND INSTALLED IAW THE REQUIREMENTS OF ENGINEERING AUTHORIZATION A8-53R-30556. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,487 hrs · 7,973 cycles

DURING C-CHECK, INSP NOTED 3 OB NUT CLIP HOLES CORRODED ON FLOORBEAM Y1292 (L-2) AT FR 67. MAINT REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11, PARAGRAPH 5. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,487 hrs · 7,973 cycles

DURING C3 C-CHECK, INSPECTION NOTED THE FORWARD CARGO PIT FORWARD FLOOR PANEL 131CG HAS SEVERAL HOLES. MAINTENANCE REPAIRED DAMAGED PANEL 131CG IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 15,487 hrs · 7,973 cycles

DURING C3 C-CHECK, INSPECTION NOTED THE AFT CARGO PIT LT TRANSITION PANEL 151HH WAS DAMAGED. MAINTENANCE REPAIRED DAMAGED PANEL 151HH IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPSH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,487 hrs · 7,973 cycles

DURING C3 C-CHECK, INSPECTION NOTED THE FORWARD CARGO PIT FORWARD FLOOR PANEL 131AF HAS SEVERAL HOLES. MAINTENANCE REPAIRED DAMAGED PANEL 131AF IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 15,487 hrs · 7,973 cycles

DURING C3 C-CHECK, INSPECTION NOTED THE FORWARD CARGO PIT LT TRANSITION PANEL 161CF WAS DAMAGED. MAINTENANCE REPAIRED DAMAGED PANEL 161CF IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,487 hrs · 7,973 cycles

DURING C3 C-CHECK, INSPECTION NOTED THE AFT CARGO PIT RT TRANSITION PANEL 162BF WAS DAMAGED. MAINTENANCE REPAIRED DAMAGED PANEL 162BF IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — GOUGED (CARGO BAY) · airframe 15,487 hrs · 7,973 cycles

DURING C3 C-CHECK, INSPECTION NOTED THE FORWARD CARGO PIT RT AFT UPPER TRANSITION PANEL 132EG HAD A GOUGE. MAINTENANCE REPAIRED DAMAGED PANEL 132EG IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: SERVO CONTROL — INOPERATIVE (NLG STEERIN) · airframe 15,010 hrs · 7,715 cycles

DURING TAXI OUT, THE FLIGHT CREW RECEIVED A NOSE WHEEL STEERING FAULT AND LOSS OF STEERING. MAINT REMOVED AND REPLACED NLG STEERING SERVO CONTROL VALVE IAW AMM 32-51-51 PAGE BREAK 401. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE AND OPERATIONAL CHECKED GOOD. (A)

Part: TUBE — DAMAGED (HYD SYSTEM) · airframe 12,905 hrs · 6,661 cycles

FLIGHT CREW REPORTED YELLOW HYDRAULIC RESERVOIR LOW LEVEL INDICATION IN COCKPIT. REF TSM 52-36-00-810-805, FOUND YELLOW SYSTEM LOW PRESSURE SWITCH TUBE DAMAGED. REMOVED AND REPLACED LOW PRESSURE SWITCH TUBE IAW AMM 29-13-49-000-005 AND 29-13-49-400-005. PERFORMED LEAK CHECK. NO LEAKS NOTED.

Part: LINE — WORN (HYD SYSTEM) · airframe 11,208 hrs · 5,767 cycles

FLIGHT CREW REPORTED YELLOW HYDRAULIC QUANTITY LOW. FOLLOWED HYD QTY LOW ECAM: PTU-OFF; ENG DRIVEN PUMP-OFF. YELLOW HYDRAULIC PUMP NEVER CAVITATED OR OVERHEATED. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT AND WAS TOWED TO THE GATE. PERFORMED CHECK OF YELLOW HYD SYS FOR POSSIBLE CAVITATION IAW AMM 29-00-00-280-006, STEP 4A. REPLACED PRESSURE LINE FOR TRANSDUCER IAW AMM 20-23-11-911-001. REPLACED NR 2 ENG CASE DRAIN FILTER IAW AMM 29-13-93-610-041. REPLACED HP FILTER IAW AMM 29-13-45-610-001. REPLACED LP FILTER IAW AMM 29-13-44, PB 401. NO CONTAMINATION FOUND IN THE FILTERS REPLACED. NO CAVITATION WAS REPORTED IAW 29-00-00-280-006, STEP 4A, STEP 1. CHECKED FOR EXTERNAL LEAKING OF HY

Part: COOLING FAN — INOPERATIVE (E/E BAY) · airframe 3,696 hrs · 1,700 cycles

FLIGHT CREW REPORTED LIVE TV SMOKE WARNING LIGHT DURING FLIGHT. INSPECTED LIVE TV RACK, FOUND COOLING FAN INOP (NO SMOKE PRESENT). REPLACED LTV COOLING FAN ASSY PER LTV AMM 44-25-00. OPS CHECK NORMAL.