N640AW

Part: BATTERY — DISCHARGED (CABIN) · airframe 78,144 hrs · 30,259 cycles

AIRCRAFT WAS NOT GNDED. OPERATION TEST OF EMER LIGHT TEST FAILED. LIGHTS INOPERATIVE AT SEATS 9L, 9R, 11L, 11R & OVERHEAD 14R. REF JC 26L00005005 STEP 14. REPLACED LT EPSU & BATTERY IAW AMM 33-51-38-400-002-A & 33-51-38-400-001-A. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED. SEE AALA201512039002 FOR ADDITIONAL INFORMATION.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 78,144 hrs · 30,259 cycles

AIRCRAFT WAS NOT GNDED. OPERATION TEST OF EMER LIGHT TEST FAILED. LIGHTS INOPERATIVE AT SEATS 9L, 9R, 11L, 11R & OVERHEAD 14R. REF JC 26L00005005 STEP 14. REPLACED LT EPSU & BATTERY IAW AMM 33-51-38-400-002-A & 33-51-38-400-001-A. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED. SEE AALA201512039005 FOR ADDITIONAL INFORMATION.

Part: PRESSURE SWITCH — CRACKED (HYDRAULIC SYS) · airframe 76,994 hrs · 29,749 cycles

FLIGHT 498 EN-ROUTE, LOSS OF FLUID ON Y HYD SYS. THE FLIGHT DECLARED AN EMER & DIVERTED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. FOUND NR 2 ENG HYD PRESS SWITCH CRACKED. R & R NR 2 ENG HYD PRESS SWITCH IAW AMM 29-13-17. SERVICED Y HYD SYS IAW AMM 12-12-29. OPERATIONS & LEAK CHECKED GOOD.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 76,866 hrs · 29,701 cycles

BC2 CHECK, EMER POWER SUPPLY 12WL FAILED BITE CHECK. REPLACED POWER SUPPLY. ACCOMPLISHED A SUCCESSFUL OPERATIONAL CHECK IAW AMM 33-51-38.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 76,540 hrs · 29,588 cycles

L2 DOOR ASSIST BOTTLE LOW PSI, 1400 PSI. SERVICED THE L2 DOOR ASSIST BOTTLE.

Part: LANYARD — MISROUTED (R1 DOOR) · airframe 76,422 hrs · 29,549 cycles

THE YELLOW RELEASE STRAP & WHITE SURVIVAL KIT LANYARD AT R1 DOOR IS NOT ROUTED CORRECTLY. ROUTED THE YELLOW RELEASE STRAP & WHITE SURVIVAL KIT LANYARD FOR THE R1 DOOR ESCAPE SLIDE CORRECTLY.

Part: POWER SUPPLY — FAULTY (GALLEY) · airframe 76,108 hrs · 29,434 cycles

ELECTRICAL SMELL COMING FROM SOMEWHERE IN FWD GALLEY. REPLACED EPSU IN THE FWD GALLEY.

Part: PRESSURE SWITCH — LEAKING (HYDRAULIC SYS) · airframe 75,817 hrs · 29,325 cycles

HYDRAULIC LEAK ON RT ENG. REPLACED RT ENG HYD PUMP PRESS SWITCH IAW AMM 29-13-17. LEAK CHECKED GOOD.

Part: PRESSURE SWITCH — LEAKING (HYDRAULIC SYS) · airframe 75,817 hrs · 29,325 cycles

HYDRAULIC YELLOW SYS INDICATED LOW QTY. FOUND NR 2 ENG HYD PUMP PRESS SWITCH LEAKING. REPLACED PRESS SWITCH & O RING IAW AMM 29-13-17-400-010-A. GOOD LEAK & OPERATIONAL CHECK.

Part: LENS — DETACHED (CABIN) · airframe 75,571 hrs · 29,239 cycles

ROW 11 RED LIGHT COVER ON THE SEAT BOTTOM BECAME DETACHED. REINSTALLED LENS.

Part: LENS — DETACHED (CABIN) · airframe 75,456 hrs · 29,189 cycles

ROW 1 LT EXIT LIGHT LENS CAME OFF. REINSTALLED EMER EXIT LIGHT LENS AT ROW 1 LT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 75,456 hrs · 29,189 cycles

NUMEROUS CABIN EMER LIGHTS INOPERATIVE. REPLACED AFT EMER LIGHT BATTERY UNIT IAW AMM 33-51-38-400-002-A.

Part: TACHOMETER — INOPERATIVE (LANDING GEAR) · airframe 75,080 hrs · 29,032 cycles

AFTER TAKEOFF, ECAM MSG, BRAKES AUTO BRAKE FAULT & BRAKE RELEASED PRIOR TO LANDING, BRAKE TEMPS 95/95/80/55. AFTER LANDING & TAXING TO GATE, BRAKE TEMPS 415/55/395/295. BRAKE NR 2 APPEARS INOPERATIVE. REPLACED NR 2 TACHOMETER IAW AMM 32-42-57-000-01A. OPERATIONS CHECKED GOOD.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 74,843 hrs · 28,936 cycles

SOFT SPOT IN AISLE AT ROW 23. REPLACED FLOOR PANEL AT ROW 23 IAW AMM 53-42-12.

Part: LENS — MISSING (CABIN) · airframe 74,064 hrs · 28,630 cycles

EMER LIGHT LENS MISSING AT SEAT 13C. INSTALLED EMER LIGHT LENS AT SEAT 13C.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 73,796 hrs · 28,530 cycles

CABIN EMER LIGHT SYS FAILED OPERATIONS CHECK. REPLACED POWER SUPPLY UNIT 12WL IAW AMM 33-51-00.

Part: PANEL — CRACKED (INDICATION) · airframe 73,675 hrs · 28,483 cycles

SPEED BREAK SURFACE PANEL CRACKED. R & R SPEED BREAK SURFACE PANEL, OPEN. PN, SN & LOCATION INFORMATION TO FOLLOW.

Part: BATTERY — FAILED (CABIN) · airframe 72,887 hrs · 28,205 cycles

AT L2 DOOR EMERGENCY LIGHT BATTERY FAILS CHECK. REPLACED EMERGENCY LIGHT BATTERY AT DOOR L2.

Part: ACCUMULATOR — LOW PRESSURE (L2 DOOR) · airframe 72,879 hrs · 28,201 cycles

L2 DOOR EMERGENCY DOOR ACCUMULATOR LOW. SERVICED L2 DOOR EMERGENCY DOOR ACCUMULATOR.

Part: SIGN — CRACKED (CABIN) · airframe 72,639 hrs · 28,128 cycles

R1 DOOR EXIT SIGN LIGHT CRACKED. R & R R1 DOOR EXIT SIGN LIGHT IAW AMM 33-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 71,966 hrs · 27,914 cycles

C1 CHECK DELAMINATION ON FLOOR PANEL 261EF AFT OF FRAME 66, Z 500 & Y 1292. REPLACED FLOOR PANEL 261EF IAW IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 71,966 hrs · 27,914 cycles

C1 CHECK DELAMINATION ON FLOOR PANEL 261NF AFT OF FRAME 64, Z 500 & Y 254. REPLACED FLOOR PANEL 261NF IAW IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 71,966 hrs · 27,914 cycles

C1 CHECK DELAMINATION ON FLOOR PANEL 242KF BETWEEN FRAME 42 TO FRAME 47, Z 500 & BETWEEN Y 254 TO Y 765. REPLACED FLOOR PANEL 242KF IAW A320 SRM 53-02-00, PAGES 201-207, FIGURE 201.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 71,966 hrs · 27,914 cycles

C1 CHECK DELAMINATION ON FLOOR PANEL 261DF AFT OF FRAME 66, Z 500 & Y 254. REPLACED FLOOR PANEL 261DF IAW IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 71,966 hrs · 27,914 cycles

C1 CHECK, DELAMINATION ON FLOOR PANEL NR 241KF BETWEEN FR 42 TO FR 47, Z 500 & BETWEEN Y 254 TO Y 765. REPLACED FLOOR PANEL 241KF IAW IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 71,966 hrs · 27,914 cycles

C1 CHECK, DELAMINATION ON FLOOR PANEL 241JF BETWEEN FR 42 TO FR 47, Z 500 & BETWEEN Y 254 TO Y 254. REPLACED FLOOR PANEL NR 241JF IAW IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 71,966 hrs · 27,914 cycles

C1 CHECK, DELAMINATION ON FLOOR PANEL 242LF BETWEEN FR 42 TO FR 47, Z 500 & BETWEEN Y 765 TO Y 1292. REPLACED FLOOR PANEL 242LF IAW IRM 9701, REV G.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 71,966 hrs · 27,914 cycles

C1 CHECK, CRACK IN FWD RT SHEAR PLATE AT FR 68, Z 500, Y 1500. REPLACED FWD RT SHEAR PLATE AT FR 68, Z 500, Y 1500 IAW A320 SRM 51-42-11 & DRAWING D53480020.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 71,966 hrs · 27,914 cycles

C1 CHECK, CRACK IN FWD LT SHEAR PLATE BETWEEN FR 68 TO FR 69, Z 500 & BETWEEN Y 1270 TO Y 1450. REPLACED FWD LT SHEAR PLATE BETWEEN FR 68 TO FR 69, Z 500 & BETWEEN Y 1270 TO Y 1450 IAW A320 SRM 51-42-11 & DRAWING D53480020.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,966 hrs · 27,914 cycles

C1 CHECK, LEVEL 2 INTERGRANULAR CORROSION ON L2 DOOR AFT CORNER SHAPE SILL AT FR 68, Z 500, Y 1600. REPLACED L2 DOOR AFT CORNER SHAPE SILL AT FR 68, Z 500, Y 1600 IAW A320 SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 71,966 hrs · 27,914 cycles

C1 CHECK, CABIN CREASE BEAM SHEAR PLATE CRACKED AT FR 69 & Y 1160, STRINGER 23R. R & R SHEAR PLATE IAW A320 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,966 hrs · 27,914 cycles

C1 CHECK, L2 DOOR SILL CTR SECTION CORRODED AT FR 67 & Y 1589. R & R SILL SECTION IAW 1320 SRM 51-21-11 & DRAWING D5340020.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,966 hrs · 27,914 cycles

C1 CHECK, CABIN FLOOR BEAM CORRODED AT FR 68 & W 1160. R & R FLOOR BEAM IAW A320 SRM 51-72-11 & DRAWING D53472040.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,966 hrs · 27,914 cycles

C1 CHECK, CABIN FLOOR BEAM CORRODED AT FR 66 & Y 465. R & R FLOOR BEAM IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,966 hrs · 27,914 cycles

C1 CHECK, CABIN FLOOR BEAM CORRODED AT FR 66 & Y 308. R & R FLOOR BEAM IAW A320 SRM 51-72-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,966 hrs · 27,914 cycles

C1 CHECK, CABIN FLOOR BEAM CORRODED AT FR 20 AT Y -765. R & R FLOOR BEAM IAW A320 SRM 51-72-11 & DRAWING D53112812.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,966 hrs · 27,914 cycles

C1 CHECK, CABIN SEAT TRACK CORRODED BETWEEN FR 20 & FR 24 AT Y 1292. R & R TRACK IAW A320 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,966 hrs · 27,914 cycles

C1 CHECK, LEVEL 2 INTERGRANULAR CORROSION ON FLOOR BEAM BETWEEN FR 66 TO FR 68, Y 765. REPLACED FLOOR BEAM BETWEEN FR 66 TO FR 68, Y 765 IAW A320 SRM 51-72-11 & DRAWING 18D53472040.

Part: SUPPORT FITTING — INOPERATIVE (L1 DOOR) · airframe 71,610 hrs · 27,783 cycles

L1 DOOR HARD TO OPEN. R & R L1 DOOR LOWER SUPPORT ARM FITTING IAW AMM 52-11-31-400-002-A, STEP 4.

Part: DOUBLER — CORRODED (ZONE 100) · airframe 71,598 hrs · 27,777 cycles

CORROSION ON FUSELAGE SKIN AT LAVATORY EXHAUST PORT BETWEEN FRAMES 69 TO 70 & BETWEEN S31-32R. R & R LAVATORY EXHAUST PORT DOUBLER AT IAW SRM 51-42-11. NO DAMAGE TO FUSELAGE SKIN.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 70,962 hrs · 27,569 cycles

EMERGENCY LIGHT LENS AT ROW 1 AND ROW 5 MISSING. REPLACED MISSING LENS.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 70,780 hrs · 27,516 cycles

EMERGENCY LIGHT LENS COVER MISSING AT ROW 17L. REPLACED LENS COVER AT ROW 17L.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 70,584 hrs · 27,459 cycles

LOWER EMERGENCY EXIT LIGHT COVER AT L1 DOOR BROKEN OFF. REPLACED EMERGENCY LIGHT COVER.

Part: ACCUMULATOR — LOW PRESSURE (L2 DOOR) · airframe 70,298 hrs · 27,382 cycles

PAX DOOR 2L DOOR ASSIST ACCUMULATOR PRESSURE IS LOW. SERVICED 2L DOOR ASSIST ACCUMULATOR IAW AMM 52-10-00-010-001-A.

Part: ACCUMULATOR — LOW PRESSURE (R2 DOOR) · airframe 70,298 hrs · 27,382 cycles

PAX DOOR R2 ASSIST ACCUMULATOR PRESSURE IS LOW. SERVICED R2 DOOR ASSIST ACCUMULATOR IAW AMM 52-10-00-010-001-A.

Part: COVER — MISSING (CABIN) · airframe 70,226 hrs · 27,367 cycles

EMERGENCY EXIT LIGHT COVER AT DOOR 2R MISSING. REPLACED EMERGENCY EXIT LIGHT COVER AT DOOR 2R.

Part: SLIDE RAFT — LOW PRESSURE (L2 DOOR) · airframe 70,113 hrs · 27,321 cycles

AFT LT BOTTLE SHOWS LOW PRESSURE ON SLIDE RAFT (L2) DOOR. R & R AFT LT (L2) SLIDE RAFT.

Part: GENERATOR — FAILED · airframe 69,897 hrs · 27,254 cycles

CONSTANT SPEED MOTOR GENERATOR FAILS EMERGENCY GENERATOR TEST. DURING OPERATIONAL CHECK STEP 4, NO OUTPUT FROM CSM/G AT 2XE TERMINALS. R & R CONSTANT SPEED MOTOR GENERATOR IAW MM 24-24-51-000-001-A.

Part: WIRE — BROKEN (CABIN) · airframe 69,541 hrs · 27,160 cycles

ROW 11 DEF EMERGENCY EXIT LIGHT ON AISLE, WILL NOT ILLUMINATE, HAS BROKEN WIRE AT SPLICE BELOW SEAT D. SPLICED EMERGENCY LIGHT ROW 11 RIGHT AISLE BELOW SEAT D.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 68,779 hrs · 26,905 cycles

FLIGHT ATTENDANT REPORTED AFT LEFT FLASHLIGHT INOPERATIVE. REPLACED AFT LEFT FLASHLIGHT BATTERY.

Part: DAMPER — WEAK (L1 DOOR) · airframe 68,767 hrs · 26,900 cycles

C6 CHECK - L1 DOOR DAMPER WEAK. REPLACED L1 DOOR DAMPER IAW A320 AMM 52-11-14-400.

Part: ESCAPE ROPE — MISSING (CABIN) · airframe 68,515 hrs · 26,803 cycles

ESCAPE ROPE OVERWING AIRCRAFT RIGHT IS MISSING. INSTALLED ESCAPE ROPE AT AIRCRAFT RIGHT OVERWING.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 68,483 hrs · 26,790 cycles

AFT FLIGHT ATTENDANT SEAT FLASHLIGHT NOT BLINKING. REMOVED AND REPLACED BATTERY. OPS CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 68,448 hrs · 26,780 cycles

LENS COVER MISSING ON FLOOR PATH LIGHT AT DOOR L2. REPLACED LENS, EMERGENCY LIGHT CHECKS GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 67,259 hrs · 26,390 cycles

FORWARD FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FORWARD FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 66,989 hrs · 26,296 cycles

AFT EMERGENCY EXIT LIGHT BLINKING. REMOVED AND REPLACED THE BATTERY OF THE EMERGENCY POWER SUPPLY UNIT (EPSU) PER AMM 33-51-38-400-002-A. OPS CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 66,661 hrs · 26,197 cycles

EMERGENCY EXIT ROW 11C SEAT SIDE LIGHT AIRCRAFT LEFT LENS MISSING. REPLACED EMERGENCY EXIT LIGHT LENS AT ROW 11 AIRCRAFT LEFT.

Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 66,565 hrs · 26,171 cycles

EMERGENCY EXIT LIGHT TEST FAILS - FAULTS ALL LOCATIONS. RESET CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS) AND PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AIRBUS MAINTENANCE MANUAL 33-51-00-710-001-A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,880 hrs · 25,941 cycles

L1 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED L1 DOOR EMERGENCY LIGHT ASSEMBLY, OPERATIONAL CHECK GOOD.

Part: POWER SUPPLY — MALFUNCTIONED (CABIN) · airframe 65,778 hrs · 25,903 cycles

EMERGENCY LIGHT CHECK FAULTS AT FORWARD LEFT AND MID CABIN LEFT AND RIGHT. MAINTENANCE RESET POWER SUPPLY UNITS - OPERATIONAL CHECKS NORMAL.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 65,237 hrs · 25,712 cycles

L-1 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED L-1 DOOR ASSIST BOTTLE PER AIBUS MAINTENANCE MANUAL 52-10-00-614-001.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 65,237 hrs · 25,712 cycles

L-2 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED L-2 DOOR ASSIST BOTTLE PER AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.

Part: O-RING — BLOWN (HYDRAULIC SYS) · airframe 63,797 hrs · 25,179 cycles

EN ROUTE TO PHX, CREW REPORTED 'HYD G RSVR LO LVL' ECAM MESSAGE. CREW SHUT OFF ENGINE NR 1 PUMP AND DIVERTED TO CLT DECLARING AN EMERGENCY. FLIGHT LANDED WITHOUT INCIDENT BUT AIRCRAFT WAS OVERWEIGHT AT 155.000. MAINTENANCE FOUND A BLOWN OUT O-RING ON NR 1 ENGINE PUMP LOW PRESSURE SWITCH. REPLACED O-RING IAW AIRBUS MAINTENANCE MANUAL 29-11-17.

Part: ACCUMULATOR — LOW PRESSURE (L2 DOOR) · airframe 63,614 hrs · 25,111 cycles

L-2 DOOR ASSIST ACCUMULATOR PRESSURE REQUIRES SERVICING. MAINTENANCE SERVICED L-2 DOOR ASSIST ACCUMULATOR IAW AIRBUS MAINTENANCE MANUAL 52-10-00-614.

Part: LENS — BROKEN (CABIN) · airframe 63,614 hrs · 25,111 cycles

R1 DOOR EMERGENCY LIGHT LENS BROKEN. MAINTENANCE REMOVED AND REPLACED LENS AS REQUIRED.

Part: SLIDE — CRACKED (CABIN) · airframe 62,857 hrs · 24,876 cycles

LEFT OVERWING SLIDE BOX HAS A CRACK AROUND ATTACH FASTENER. REPLACE SLIDE ASSY PER AMM 25-62-42-400-001-0.

Part: CABLE — BROKEN (EVAC SLIDE) · airframe 62,857 hrs · 24,876 cycles

LEFT OVERWING INFLATION BOTTLE CABLE FOUND BROKEN AT RELEASE CABLE DISASSEMBLE POINT. REPLACED LEFT OFFWING ESCAPE SLIDE INFLATION RESERVOIR IAW A320 AMM 25-62-46.

Part: RESERVOIR — BROKEN (EVAC SLIDE) · airframe 62,857 hrs · 24,876 cycles

PIT - EES - LEFT OVERWING INFLATION BOTTLE CABLE FOUND BROKEN AT RELEASE CABLE DISASSEMBLE POINT. MAINTENANCE REPLACED LEFT OFFWING ESCAPE SLIDE INFLATION RESERVOIR IAW AIRBUS MAINTENANCE MANUAL 25-62-46.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 62,531 hrs · 24,751 cycles

CRACKS IN LEFT AFT EMERGENCY EXIT FORWARD SEGMENT ANGLE. REPLACED LEFT AFT EMERGENCY EXIT FORWARD SEGMENT ANGLE IAW EO EO5210Y228.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 62,531 hrs · 24,751 cycles

CRACKS IN AFT SEGMENT ANGLE OF LEFT AFT EMERGENCY EXIT DOOR. REPLACED AFT SEGMENT ANGLE OF LEFT AFT EMERGENCY EXIT DOOR IAW EO 5210Y228 & EA117931.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 62,531 hrs · 24,751 cycles

CRACK IN LEFT FORWARD EMERGENCY EXIT SEGMENT ANGLE. REPLACED LEFT FORWARD EMERGENCY EXIT SEGMENT ANGLE IAW EO 5210Y228.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 62,531 hrs · 24,751 cycles

CRACKS ON RIGHT AFT EMERGENCY EXIT DOOR FORWARD SEGMENT ANGLE. REPLACED RIGHT AFT EMERGENCY EXIT DOOR FORWARD SEGMENT ANGLE IAW EO5210Y228.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 62,531 hrs · 24,751 cycles

CRACK IN LEFT AFT EMERGENCY EXIT DOOR AFT SEGMENT ANGLE. REPLACED LEFT AFT EMERGENCY EXIT DOOR AFT SEGMENT ANGLE IAW EO5210Y228.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 62,531 hrs · 24,751 cycles

CRACKS ON RIGHT AFT EMERGENCY EXIT DOOR AFT SEGMENT ANGLE. REPLACED RIGHT AFT EMERGENCY EXIT DOOR AFT SEGMENT ANGLE IAW EO5210Y228.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 62,531 hrs · 24,751 cycles

CRACKS IN LEFT FORWARD EMERGENCY EXIT DOOR FORWARD SEGMENT ANGLE. REPLACED LEFT FORWARD EMERGENCY EXIT DOOR FORWARD SEGMENT ANGLE IAW EO5210Y228.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 62,531 hrs · 24,751 cycles

CRACK IN RIGHT FORWARD EMERGENCY EXIT DOOR AFT SEGMENT ANGLE. REPLACED RIGHT FORWARD EMERGENCY EXIT DOOR AFT SEGMENT ANGLE IAW EO5210Y228.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 62,531 hrs · 24,751 cycles

CRACKS ON RIGHT FORWARD EMERGENCY EXIT DOOR FORWARD SEGMENT ANGLES. REPLACED RIGHT FORWARD EMERGENCY EXIT DOOR FORWARD SEGMENT ANGLES IAW EO5210Y228.

Part: SLIDE RAFT — DEFECTIVE (L2 DOOR) · airframe 62,220 hrs · 24,630 cycles

FLT 439 - LAS - EES - L-2 DOOR SLIDE FAILS "EXTERNAL LOADS" EMERGENCY LIGHT TEST. MAINTENANCE REPLACED L-2 DOOR SLIDE / RAFT.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 62,147 hrs · 24,607 cycles

FLT 339 - PHX - EES - R-2 DOOR ASSIST BOTTLE LOW PRESSURE. MAINTENANCE SERVICED DOOR ASSSIT BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 62,147 hrs · 24,607 cycles

FLT 339 - PHX - EES - L-2 DOOR ASSIST BOTTLE LOW PRESSURE. SERVICED DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 61,085 hrs · 24,225 cycles

FLT 191-SAN - EES - L-2 DOOR ASSIST BOTTLE REQUIRES SERVICING. MAINTENANCE SERVICED L-2 DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 61,085 hrs · 24,225 cycles

FLT 191-SAN - EES - R-2 DOOR ASSIST BOTTLE REQUIRES SERVICING. MAINTENANCE SERVICED R-2 DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.

Part: LIGHT — BURNED (COCKPIT) · airframe 59,848 hrs · 23,790 cycles

FLT 239 PHX-DTW - SMOKE - FLIGHT DIVERTED TO DEN DUE TO SMOKE IN THE COCKPIT. MAINTENANCE FOUND EVIDENCE OF ELECTRICAL ARCING ON PILOT'S MAP LIGHT 25LE ALONG WITH BURNT ELECTRICAL SMELL INTERNALLY. REPLACED MAP LIGHT ASSEMBLY IAW AIRBUS MAINTENANCE MANUAL 33-12-12.

Part: SLIDE — FAILED (L2 DOOR) · airframe 59,721 hrs · 23,746 cycles

FLT 439 - LAS - EES - L2 DOOR SLIDE FAILS EMERGENCY LIGHT TEST. MAINTENANCE REMOVED AND REPLACED L2 DOOR SLIDE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 59,200 hrs · 23,586 cycles

FLT 220 - PHX - EEL - AFT CABIN FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED BATTERY FOR AFT CABIN F/A FLASHLIGHT. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 58,218 hrs · 23,238 cycles

FLT 574 - TPA - EEL - EMERGENCY LIGHT BATTERY A/C LEFT OVERWING INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY A/C LEFT OVERWING. OPERATIONAL CHECK GOOD.

Part: LENS — BROKEN (CABIN) · airframe 58,165 hrs · 23,214 cycles

FLT 90-PHX - EEL - EMERGENCY EXIT ROW AISLE LIGHT LENS 9 LEFT BROKEN. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT LENS AT ROW 9 LEFT.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,647 hrs · 23,034 cycles

SAL - MAJOR REPAIR - BC4 CHECK - CORROSION ON FUSELAGE SKIN AT FR 62 - FR 63, S43L - S44L. REPAIRED FUSELAGE SKIN AT FR 62 - FR 63, S43L - S44L IAW EA 132712.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,647 hrs · 23,034 cycles

SAL - S2 - MAJOR REPAIR - LEVEL 2 INTERGRANULAR CORROSION ON AFT CORNER FITTING AT FR67 + 19 INCHES, S23R AT R-2 DOOR CUTOUT. REPLACED AFT CORNER FITTING AT FR67 + 19 INCHES, S23R AT R-2 DOOR CUTOUT IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53480505.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,647 hrs · 23,034 cycles

SAL - S2 - MAJOR REPAIR - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR16 + 3 INCHES, Y1292. REPLACED FLOORBEAM AT FR16 + 3 INCHES, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112813.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,647 hrs · 23,034 cycles

SAL - BC4 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR41 TO FR47, - Y765. REPLACED SEAT TRACK BETWEEN FR41 TO FR47, -Y765 IAW A320 SRM 51-72-11 AND DRAWING D53370500.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,647 hrs · 23,034 cycles

SAL - BC4 - MAJOR REPAIR - LEVEL 2 CORROSION ON WEB BETWEEN FR20 TO FR24, -Y1650. REPLACED WEB BETWEEN FR20 TO FR24, -Y1650 IAW A320 SRM 51-72-11 AND DRAWING D531-12783, D531-12261.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,647 hrs · 23,034 cycles

SAL - BC4 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM BETWEEN FR66 TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR70, -Y765 PAX CABIN IAW A320 SRM 51-72-11 & DRAWING D5347200.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,647 hrs · 23,034 cycles

SAL - BC 4 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR46 TO FR64, Y+765. REPLACED SEAT TRACK BETWEEN FR46 TO FR64, Y+765 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,647 hrs · 23,034 cycles

SAL - BC4 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM AT FR65+21 INCHES, +Y765. REPLACED FLOORBEAM AT FR65+21 INCHES, +Y765 IAW A320 SRM 51-72-11 AND DRAWING D53472000.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,647 hrs · 23,034 cycles

SAL - BC4 - MAJOR REPAIR - LEVEL 2 CORROSION ON ANGLE SUPPORT FITTING AT FR20, -Y1615. REPLACED ANGLE SUPPORT FITTING AT FR20, -Y1615 IAW A320 SRM 51-72-77 AND DRAWING D533112786.

Part: WEB — CORRODED (CARGO BAY) · corrosion level 2 · airframe 57,647 hrs · 23,034 cycles

SAL - BC4 - MAJOR REPAIR - LEVEL 2 CORROSION ON WEB BETWEEN FR 50 TO FR 51, S38R AFT CARGO COMPARTMENT. REPLACED WEB BETWEEN FR50 TO FR 51, S38R AFT CARGO COMPARTMENT IAW SRM 51-72-11 AND DRAWING D53470320.

Part: WEB — CORRODED (CARGO BAY) · corrosion level 2 · airframe 54,647 hrs · 23,034 cycles

SAL - BC4 - MAJOR REPAIR - LEVEL 2 CORROSION ON WEB LOCATED BETWEEN FR50 TO FR51 STR 38L AFT CARGO COMPARTMENT. REPLACED WEB LOCATED BETWEEN FR50 TO FR51 STR 38L AFT CARGO COMPARTMENT IAW SRM A320 51-72-11 DWG D53470490.

Part: PLATE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 57,647 hrs · 23,034 cycles

SAL - BC4 - MAJOR REPAIR - LEVEL 2 CORROSION ON PROFILE PLATE AT FR58, STR 44 OF AFT CARGO COMPARTMENT. REPLACED PROFILE PLATE AT FR58, STR 44 OF AFT CARGO COMPARTMENT IAW A320 SRM 51-72-11 AND DRAWING D53974870.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,647 hrs · 23,034 cycles

SAL - BC4 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR35 TO FR36, -Y1292. REPLACED SEAT TRACK BETWEEN FR35 TO FR36, -Y1292 IAW A320 SRM 51-72-11 AND DRAWING D53371034.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,647 hrs · 23,034 cycles

SAL - MAJOR REPAIR - BC4 CHECK - CRACKED SEAT TRACK AT FR 48 - FR 49, +Y1292. REPAIRED SEAT TRACK AT FR 48 - FR 49, +Y1292 IAW A320 SRM 53-41-15.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 57,647 hrs · 23,034 cycles

SAL - BC4 - MAJOR REPAIR - CORROSION ON GUSSET SUPPORT AT FR65 + 22 INCHES BETWEEN S17L TO S18L. REPLACED GUSSET SUPPORT AT FR65 + 22 INCHES BETWEEN S17L TO S18L IAW SRM A320 51-72-11 DRAWING D53480505.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,647 hrs · 23,034 cycles

SAL - BC4 - MAJOR REPAIR - LEVEL 2 INTERGRANULAR CORROSION ON SHEAR PLATE WEB BETWEEN FR56 TO FR57, S38L. REPLACED SHEAR PLATE WEB BETWEEN FR56 TO FR57, S38L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53470320.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,647 hrs · 23,034 cycles

SAL - MAJOR REPAIR - BC4 CHECK - LEVEL 2 CORROSION ON SHEAR PLATE AT FR 48 - FR 49, S38L. REPLACED SHEAR PLATE AT FR 48 - FR 49, S38L IAW A320 SRM 51-72-11 AND EA 132728.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,647 hrs · 23,034 cycles

SAL - S2 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE WEB ASSEMBLY BETWEEN FR58 TO FR59, S38L. REPLACED SHEAR PLATE WEB ASSEMBLY BETWEEN FR58 TO FR59, S38L IAW A320 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,647 hrs · 23,034 cycles

SAL - BC4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE ASSEMBLY WEB BETWEEN FR51 TO FR52, S38R. REPLACED SHEAR PLATE ASSEMBLY WEB BETWEEN FR51 TO FR52, S38R IAW A320 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,647 hrs · 23,034 cycles

SAL - BC4 - MAJOR REPAIR - LEVEL 2 INTERGRANULAR CORROSION ON SHEAR PLATE WEB BETWEEN FR58 TO FR59, S38R. REPLACED SHEAR PLATE WEB BETWEEN FR58 TO FR59, S38R IAW A320 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,647 hrs · 23,034 cycles

SAL - MAJOR REPAIR - BC4 CHECK - LEVEL 2 CORROSION ON SHEAR PLATE AT FR 52-FR 53, S38L. REPLACED SHEAR PLATE AT FR 52-FR 53, S38L IAW A320 SRM 51-72-11.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 57,647 hrs · 23,034 cycles

SAL - S2 - MAJOR REPAIR - EXCESSIVE PLAY ON RUDDER HINGE ARM NR 5. REPLACED RUDDER HINGE ARM NR 5 IAW A320 AMM 55-36-91 & 27-21-00.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,647 hrs · 23,034 cycles

SAL - MAJOR REPAIR - BC4 CHECK - LEVEL 2 CORROSION ON PLATE ASSEMBLY AT FR 67 + 18 INCHES, S23R. REPLACED PLATE ASSEMBLY AT FR 67 + 18 INCHES, S23R IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,647 hrs · 23,034 cycles

SAL - S2 - MAJOR REPAIR - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR65 + 21 INCHES, Y1292. REPLACED FLOORBEAM AT FR65 + 21 INCHES, Y1292 IAW A320 SRM 51-72-11.

Part: DAMPER — FAILED (PAX DOOR) · airframe 57,647 hrs · 23,034 cycles

SAL - BC4 - EES - DURING OPERATIONAL TEST OF DAMPING FUNCTION & EMERGENCY OPERATIONAL CYLINDER HARD IMPACT OF BUFFER ON A/C STRUCTURE WAS FOUND DURING OPENING & CLOSING AT AFT PASSENGER/CREW DOOR 832. REPLACED DOOR DAMPER EMERGENCY OPERATIONAL CYLINDER AT AFT PASSENGER/CREW DOOR 832 IAW A320 AMM 52-13-14.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,647 hrs · 23,034 cycles

SAL - MAJOR REPAIR - BC4 - LEVEL 2 INTERGRANULAR CORROSION ON THE R2 DOOR CUTOUT LOWER SILL AT FR 67 - FR 68, S23R, -Y1732. REPAIRED THE R2 DOOR CUTOUT LOWER SILL AT FR 67 - FR 68, S23R, -Y1732 IAW EA 132700.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,647 hrs · 23,034 cycles

SAL - S2 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON WEB OF FLOOR STRUCTURE BETWEEN FR12 TO FR16, Y1650. REPLACED WEB OF FLOOR STRUCTURE BETWEEN FR12 TO FR16, Y1650 IAW A320 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,647 hrs · 23,034 cycles

SAL - S2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR41 TO FR46 + 17, INCHES, -Y1292. REPLACED SEAT TRACK BETWEEN FR41 TO FR46 + 17, INCHES, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING 53370500.

Part: DAMPER — FAILED (PAX DOOR) · airframe 57,647 hrs · 23,034 cycles

SAL - BC4 - EES - DURING OPERATIONAL TEST OF DAMPING FUNCTION & EMERGENCY OPERATIONAL CYLINDER HARD IMPACT OF BUFFER ON A/C STRUCTURE WAS FOUND DURING OPENING & CLOSING AT AFT PASSENGER/CREW DOOR 842. REPLACED DOOR DAMPER EMERGENCY OPERATIONAL CYLINDER AT AFT PASSENGER/CREW DOOR 842 IAW A320 AMM 52-13-14.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · airframe 57,647 hrs · 23,034 cycles

SAL - BC4 - MAJOR REPAIR - CORROSION ON DUMMY RAIL BETWEEN FR12 TO FR16, Y503. REPLACED DUMMY RAIL BETWEEN FR12 TO FR16, Y503 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112826.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,647 hrs · 23,034 cycles

SAL - MAJOR REPAIR - BC4 CHECK - LEVEL 2 CORROSION ON SEAT TRACK AT FR 12 FR 24, -Y1292. REPLACED SEAT TRACK AT FR 12 FR 24, -Y1292 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,647 hrs · 23,032 cycles

SAL - BC4 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, Y1292. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53370500.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,647 hrs · 23,034 cycles

SAL - BC4 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR49 TO FR64, Y1292. REPLACED SEAT TRACK AT FR49 TO FR64, Y1292 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,647 hrs · 23,034 cycles

SAL - BC4 - MAJOR REPAIR - CORROSION ON SEAT RAIL AT FR46 + 17 INCHES TO FR64. REPLACED SEAT RAIL AT FR46 + 17 INCHES TO FR64 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000 & D53370500.

Part: DAMPER — FAILED (PAX DOOR) · airframe 57,647 hrs · 23,034 cycles

SAL - BC4 - EES - DURING OPERATIONAL TEST OF DAMPING FUNCTION & EMERGENCY OPERATIONAL CYLINDER HARD IMPACT OF BUFFER ON A/C STRUCTURE WAS FOUND DURING OPENING & CLOSING AT FORWARD PASSENGER/CREW DOOR 831. REPLACED DOOR DAMPER EMERGENCY OPERATIONAL CYLINDER AT FORWARD PASSENGER / CREW DOOR 831 IAW A320 AMM 52-11-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,647 hrs · 23,034 cycles

SAL - BC4 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR41 TO FR46 + 17 INCHES, Y1292. REPLACED SEAT TRACK BETWEEN FR41 TO FR46 + 17 INCHES, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53370500.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 276,947 hrs · 23,034 cycles

SAL - BC4 - MAJOR REPAIR - CORROSION ON SEAT TRACK RAIL BETWEEN FR46 TO FR64, -Y765. REPLACED SEAT TRACK RAIL BETWEEN FR46 TO FR64, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,647 hrs · 23,034 cycles

SAL - BC4 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR35 TO FR36, Y1292. REPLACED SEAT TRACK BETWEEN FR35 TO FR36, Y1292 IAW A320 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,647 hrs · 23,034 cycles

SAL - BC4 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, Y1292. REPLACED SEAT TRACK BETWEEN FR24 TO FR35, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D532317412000.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,647 hrs · 23,034 cycles

SAL - BC4 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, Y765. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, Y765 IAW A320 SRM 51-42-11.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,647 hrs · 23,034 cycles

SAL - MAJOR REPAIR - BC4 CHECK - CORROSION ON FUSELAGE SKIN AT FR 60 - FR 61, S43L - S44L. REPAIRED FUSELAGE SKIN AT FR 60 - FR 61, S43L - S44L IAW EA 132711.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,647 hrs · 23,034 cycles

SAL - S2 - MAJOR REPAIR - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR66 TO FR67, Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR67, Y1292 IAW A320 SRM 51-72-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 57,647 hrs · 23,034 cycles

SAL - S2 - MAJOR REPAIR - CORROSION ON FLOOR PANEL 221FF BETWEEN FR16 TO FR20 & BETWEEN Y1292 TO Y1732. REPLACED FLOOR PANEL 221FF BETWEEN FR16 TO FR20 & BETWEEN Y1292 TO Y1732 IAW JOB CARD 26C22053002.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,647 hrs · 23,034 cycles

SAL - BC4 - MAJOR REPAIR - CORROSION ON SEAT TRACKS BETWEEN FR36 TO FR41, -Y765. REPLACED SEAT TRACK AND FASTENER BETWEEN FR36 TO FR41, -Y765 IAW A320 SRM 51-72-11 AND DRAWING D53370500.

Part: COFFEEMAKER — DEFECTIVE (AFT GALLEY) · airframe 57,169 hrs · 22,868 cycles

FLT 27 - PHX - BURNING SMELL - AFT GALLEY COFFEEMAKER NR 1 ELECTRICAL SMELL. FLIGHT ATTENDANT PULLED CIRCUIT BREAKER. MAINTENANCE REMOVED AND REPLACED NR 1 AFT COFFEEMAKER.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 56,653 hrs · 22,695 cycles

FLT 614 - PHX - EEL - EMERGENCY LIGHTS OPERATIONAL TEST ON CIDS PTP PANEL FAILED WITH FAULT MESSAGES 'INT LOADS EMER R' AND 'EXT LOADS EMER R'. MAINTENANCE REPLACED RT EMERGENCY POWER SUPPLY UNIT 12WL AND BATTERY PACK IAW AIRBUS MAINTENANCE MANUAL 33-51-38-401.

Part: LENS — MISSING (FUSELAGE) · airframe 56,630 hrs · 22,685 cycles

FLT 680 - CLT - EEL - DOOR 2L EMERGENCY EXIT LIGHT LENS MISSING. MAINTENANCE INSTALLED NEW LENS.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 55,578 hrs · 22,344 cycles

FLT 306 - CLT-LAS - EMERGENCY LIGHT - EMERGENCY LIGHT TEST FAILED. AFT LEFT BATTERY PACK FAULT. MAINTENANCE REMOVED AND REPLACED AFT L2 EMERGENCY POWER SUPPLY UNIT. SYSTEM OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 53,974 hrs · 21,769 cycles

FLT NR 182 - PHX - FLASHLIGHT AT FWD FLT ATTENDANT JUMPSEAT INOPERATIVE. MX REMOVED AND REPLACED THE FWD FLT ATTENDANT FLASHLIGHT BATTERY. OPS CHECK GOOD.

Part: HINGE FITTING — WORN (RUDDER)

C3-CHECK, NR 6105675, NR 3 RUDDER HINGE FITTING HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 2279/ RIB 5. REPLACED NR 3 RUDDER HINGE FITTING, VERTICAL STABILIZER STATION 2279/ RIB 5 IAW AMM 55-36-41.

Part: HINGE FITTING — WORN (RUDDER)

MAJOR REPAIR: C3 CHECK- NR 6105676, NR 5 RUDDER HINGE FITTING HAS EXCESSIVE PLAY. VERTICAL STABILIZER STATION 2985/ RIB 7. REPLACED NR 5 RUDDER HINGE FITTING, VERTICAL STABILIZER STATION 2985 / RIB 7 IAW AMM 55-36-41. (K)

Part: HINGE FITTING — WORN (RUDDER) · airframe 55,889 hrs · 21,361 cycles

SAL - MAJOR REPAIR - C3 CHECK - NR 2 RUDDER HINGE FITTING HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 1926 RIB 4. REPLACED NR 2 RUDDER HINGE FITTING, VERTICAL STABILIZER STATION 1926 RIB 5 IAW AMM 55-36-41. (S)

Part: HINGE FITTING — WORN (RUDDER)

C3 CHECK, NR6105677, NR 4 RUDDER HINGE FITTING HAS EXCESSIVE PLAY. VERTICAL STABILIZER STATION 2632 / RIB 6. REPLACED NR 4 RUDDER HINGE FITTING, VERTICAL STABILIZER STATION 2632/ RIB 6 IAW AMM 55-36-41. (K)

Part: WIRE — DISCONNECTED (CABIN) · airframe 51,750 hrs · 20,930 cycles

FLT 710 - FLL-PHX - EEL - R1 SERVICE / EMERGENCY DOOR EXIT ESCAPE PATH LIGHT ABOVE DOOR IS INOP. MAINTENANCE REMOVED PANEL AND RECONNECTED WIRING TO LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 49,279 hrs · 19,980 cycles

PHX - AFT PASSENGER COMPARTMENT FLOORBOARD 251RF, BS 2670 - BS 2936, -Z240, +Y254 TO -Y254 IS DELAMINATED. REPLACED AFT PASSENGER COMPARTMENT FLOORBOARD 251RF, BS 2670 - BS 2936, -Z240, +Y254 TO -Y254 IAW AWA TASK CARD R1C25306.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 48,739 hrs · 19,794 cycles

LAS - EEL - LT AFT EPSU BATTERY PACK FAILED TEST. MX REMOVED AND REPLACED BATTERY PACK PER TASK CARD A1C33302. OPERATIONAL CHECK WAS GOOD.

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 48,488 hrs · 19,712 cycles

SAL - CORROSION ON AFT GALLEY FLOORBOARD 261 FF, FR 66 - FR 68, +Y1292 TO +Y1732. REPLACED AFT GALLEY FLOORBOARD 261 FF, FR 66 - FR 68, +Y1292 TO +Y1732 IAW AWA TASK CARD C1C53303.

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 48,488 hrs · 19,712 cycles

SAL - CORROSION ON FORWARD GALLEY FLOORBOARD 222 FF, FR 16 - FR 20, -Y1292 TO -Y1732. REPLACED FORWARD GALLEY FLOORBOARD 222 FF, FR 16 - FR 20, -Y1292 TO -Y1732 IAW AWA TASK CARD C1C53302.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 48,488 hrs · 19,712 cycles

SAL - CORROSION ON CABIN FLOORBEAM, -Y1292, FR 66 + 8" - FR 68. REPLACED CABIN FLOORBEAM, -Y1292, FR 66 - FR 68 IAW A320 SRM 51-72-11.

Part: SHEAR WEB — CRACKED (ZONE 200) · airframe 48,488 hrs · 19,712 cycles

SAL - CRACKED CABIN FLOOR PLATE/SHEAR WEB TRAY, FR 68 - FR 68 + 12", +Y1250. REPLACED CABIN FLOOR PLATE/SHEAR WEB TRAY, FR 68 - FR 68 + 12", +Y1250 IAW A320 SRM 51-72-11.

Part: SHEAR WEB — CRACKED (ZONE 200) · airframe 48,488 hrs · 19,712 cycles

MCN - CRACKED CABIN FLOOR PLATE/SHEAR WEB TRAY, FR 68 - FR 68 + 12", -Y1250. REPLACED CABIN FLOOR PLATE/SHEAR WEB TRAY, FR 68 - FR 68 + 12", -Y1250 IAW A320 SRM 51-72-11.

Part: FITTING — CORRODED (ZONE 200) · airframe 48,488 hrs · 19,712 cycles

MCN - FOUND CORROSION ON L1 DOOR CUT OUT LOWER SILL CENTER FITTING, FR 16 + 5" - FR 19 + 4". REPLACED L1 DOOR CUT OUT LOWER SILL CENTER FITTING, FR 16 + 5" - FR 19 + 4" IAW A320 SRM 51-72-11.

Part: FITTING — CORRODED (ZONE 200) · airframe 48,488 hrs · 19,712 cycles

FOUND CORROSION ON R1 DOOR CUT OUT LOWER SILL CENTER FITTING, -Y1860, FR 16 + 5" - FR 19 + 4". REPLACED R1 DOOR CUT OUT LOWER SILL CENTER FITTING, -Y1860, FR 16 + 5" - FR 19 + 4" IAW A320 SRM 51-42-11.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 47,850 hrs · 19,466 cycles

LAS - EEL - RT MID EMERGENCY LIGHT BATTERY NEEDS REPLACEMENT. MX REPLACED BATTERY PER TASK CARD A1C33302.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 47,850 hrs · 19,460 cycles

LAS - EEL - LEFT OVERWING EXIT LIGHT POWER SUPPLY FAULTS BATTERY PACK. REMOVED AND REPLACED BATTERY PACK PER T/C AIC33302. OP'S CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,190 hrs · 19,205 cycles

LAS - EEL - OPERATION TEST OF EMERGENCY LIGHTS ON PTP PANEL FAILED WITH BATTERY FWD LEFT MESSAGE. MAINTENANCE REPLACED FWD LEFT EPSU BATTERY PACK. OPS CHECK GOOD.

Part: HYDRAULIC SYSTEM — LEAKING (GREEN SYS) · airframe 45,937 hrs · 18,716 cycles

WHILE EN ROUTE TO PHX, LOST GREEN HYDRAULIC SYSTEM. PILOT DECLARED AN EMERGENCY LANDING, THE PASSENGERS DID NOT BRACE. THE LANDING WAS UNEVENTFUL AND THE AIRCRAFT WAS ABLE TO TAXI TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT ON A WALK AROUND AND FOUND NO EVIDENCE OF A HYDRAULIC LEAK. MAINTENANCE SERVICED THE GREEN HYDRAULIC SYSTEM AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PRESSURE VALVE — FAULTED (LT AC PACK) · airframe 45,516 hrs · 18,559 cycles

FLT 776 - EN ROUTE TO BWI FROM LAS, UNABLE TO CONTROL CABIN PRESS AT FL 310. CABIN ALT CLIMBED TO 9500'. CREW DESCENDED TO LWR ALT AND EVENTUALLY STABILIZED CABIN. REPORTED BLEED PRESS AT 12 PSI. NR 2 PACK WAS DEFFERED WITH NR 1 PACK INTERMITTENT, FLUXING. DIVERTED TO PHX AND LANDED. MX REPLACED NUMEROUS SEALS IN LT PACK FROM ACM TO HEAT EXCHANGERS, HEAT EXCHANGERS TO RE-HEATER AND RE-HEATER TO CONDENSER. ALSO, FOUND POST FLT REPORT WAS FAULTING NR 1 ENG PRV (PRESS REG-V 4001HA1 OR SOL 10HA1 OR SENSE LINE). R&R NR 1 ENG PRV IAW AMM 36-11-52, LEAK AND OP TESTS NORMAL. ALSO, FOUND LT PACK ACM LEAKING AT MATING SURFACE. R&R NR 1 PACK ACM DUCT SEAL IAW AMM 21-52-21-400-002. LEAK CHECKS WERE GOOD.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 43,100 hrs · 17,644 cycles

SAL - DURING C1 CHECK DISCOVERED CRACK, 5 INCHES IN LENGTH, LOCATED ON STIFFENING SECTION AT FS 41+19" AND Y1292. MAINTENANCE REMOVED CRACKED STIFFENING SECTION AND INSTALLED NEW STIFFENING SECTION AT FS 41+19" AND Y1292 IAW AIRBUS SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,100 hrs · 17,644 cycles

SAL - DURING C1 CHECK DISCOVERED CORROSION ON LT INBOARD SEAT TRACK AT Y765 AND FS 36+16". MAINTENANCE REMOVED SEAT TRACK FROM FS 36 TO FS 41 IAW AIRBUS 320 SRM 53-31-15. INSTALLED NEW SEAT TRACK FROM FS 36 TO FS 41 AT Y765 IAW AIRBUS 320 SRM 53-31-15 AND 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,100 hrs · 17,644 cycles

SAL - DURING C1 CHECK DISCOVERED CORROSION ON RT INBOARD SEAT TRACK AT Y-765 AND FS 42+18". MAINTENANCE REMOVED SEAT TRACK FROM FS 41 TO FS 47 IAW AIRBUS 320 SRM 51-42-11. INSTALLED NEW SEAT TRACK FROM FS 41 TO FS 47 AT Y-765 IAW AIRBUS 320 SRM 51-42-11 AND DRAWING D53371110.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,100 hrs · 17,644 cycles

SAL - MAJOR REPAIR - DURING C1 CHECK DISCOVERED CORROSION ON LT OUTBOARD SET TRACK AT FR37 AND Y1292. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. REMOVED SEAT TRACK FROM FS 36 TO FS 41 AT Y1292 IAW AIRBUS 320 SRM 51-42-11 AND INSTALLED NEW SEAT TRACK FROM FS 36 TO FS 41 AT Y1292 IAW AIRBUS 320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,100 hrs · 17,644 cycles

SAL - DURING C1 CHECK DISCOVERED CORROSION ON RT INBOARD SEAT TRACK AT Y-765 AND FR 40+15". MAINTENANCE REMOVED SEAT TRACK FROM FS 36 TO FS 41 IAW AIRBUS 320 SRM 53-31-15. INSTALLED NEW SEAT TRACK FROM FS 36 TO FS 42 AT Y-765 IAW AIRBUS 320 SRM 51-42-11 AND DRAWING NR D53371110.

Part: TERMINAL — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,278 hrs · 17,308 cycles

ONT - EEL - CREW REPORTED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING, AT 10D, INOPERATIVE. MAINTENANCE REPLACED TERMINAL IAW STANDARD PRACTICES. OPERATIONAL CHECKS GOOD.

Part: EPSU — FAULTY (EMEGENCY LIGHT) · airframe 40,447 hrs · 16,588 cycles

DURING 8 DAY CHECK THE EMERGENCY PATH LIGHTS DID NOT ILLUMNATE IN THE FWD ENTRY AREA. MX REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT INCLUDING THE BATTERY PACK IAW 33-51-38-740-050. OPERATIONAL CHECK GOOD.

Part: TIRE — FAILED (MLG) · airframe 39,067 hrs · 16,054 cycles

EMERGENCY LANDING, ON TAKEOFF, EN ROUTE, THE NR 2 TIRE BLEW OUT CAUSING DAMAGE IN WHEEL WELL, LT WING, AND LT FLAPS, AIRCRAFT OUT OF SERVICE. EXAMINATION OF CASING FOUND TREAD MISSING 360º AROUND TIRE FROM SERIAL SIDE UPPER SIDEWALL TO OPPOSITE SERIAL SIDE SHOULDER. IN CROWN OF TIRE UNDER TREAD FABRIC WAS EXPOSED AND ABRADED WITH VERY LITTLE RUBBER & TEAR LINE EVIDENCE. THE OPPOSITE SERIAL SIDE SHOULDER IS TIGHT MOST OF THE WAY AROUND TIRE WITH A LOOSE SECTION AT 120º TO 215º. AT 200º THERE IS DAMAGE TO EDGE OF SHOULDER RIB WITH TEAR LINES IN UNDER TREAD RUBBER, THESE TEAR LINES INDICATE POSSIBLE INITIATION SITE. THERE WERE NO POLISHED AREAS ON EXPOSED SURFACES THAT INDICATE THIS WAS A WORKING SEPARATION.

Part: EPSU — FAULTY (ZONE 242)

DURING E-06 CHECK THE RT FORWARD RED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED RT OVER WING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-08 CHECK A 6 INCH CRACK WAS FOUND IN CABIN FLOOR PANEL 261DF BETWEEN FR 66 AND FR 68, Y765 LT AND Y765 RT. MAINTENANCE REMOVED CRACKED FLOOR PANEL BETWEEN FR 66 AND FR 68, Y765 LT AND Y765 RT; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG D536-70048, AND A320 SRM 53-02-00, FIG 209.

Part: FLOORBOARD — CRACKED (FUSELAGE) · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-8 CHECK A 4 INCH CRACK WAS FOUND IN CABIN FLOORBOARD (261NF). MAINTENANCE REMOVED CRACKED FLOORBOARD BETWEEN FR 64 TO FR 66; FABRICATED AND INSTALLED A NEW REPLACEMENT FLOORBOARD IAW A320 SRM 53-02-00 FIG 209.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-8 CHECK FRETTING CORROSION WAS FOUND ON CABIN SEAT TRACK Y1292 RT BETWEEN FR 24 AND FR 35. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y1292 RT FROM FR 24 TO FR 35; RECEIVED AND INSTALLED A NEW REPLACEMENT SECTION OF SEAT TRACK IAW A320 SRM 51-42-11 FIG 9-12 & 18.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN SEAT TRACK Y765 RT BETWEEN FR 47 AND FR 66. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y765 RT FROM FR 47 TO FR 66; FABRICATED A NEW REPLACEMENT SECTION OF TRACK AND 4 EACH SPLICE ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 51-42-11 FIG 9-13 & 18.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-8 CHECK FRETTING CORROSION WAS FOUND ON CABIN SEAT TRACK Y765 RT BETWEEN FR 24 AND FR 35. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y765 RT FROM FR 24 TO FR 35; RECEIVED AND INSTALLED A NEW REPLACEMENT SECTION OF SEAT TRACK IAW A320 SRM 51-42-11 FIG 9-12, & 18.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN SEAT TRACK Y1292 RT BETWEEN FR 47 AND FR 66. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y1292 RT FROM FR 47 TO FR 66; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK AND 4 EACH SPLICE ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 51-42-11 FIG 9-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-8 CHECK FRETTING CORROSION WAS FOUND ON CABIN SEAT TRACK Y1292 LT BETWEEN FR 24 AND FR 35. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y1292 LT FROM FR 24 TO FR 35; RECEIVED AND INSTALLED A NEW REPLACEMENT SECTION OF SEAT TRACK IAW A320 SRM 51-42-11 FIG 9 & 18.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-8 CHECK FRETTING CORROSION WAS FOUND ON CABIN SEAT TRACK Y1292 LT BETWEEN FR 41 AND FR 47. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y1292 LT FROM FR 41 TO FR 47; RECEIVED AND INSTALLED A NEW REPLACEMENT SECTION OF SEAT TRACK IAW A320 SRM 51-42-11 FIG 9 & 18.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-8 CHECK FRETTING CORROSION WAS FOUND ON CABIN SEAT TRACK Y765 LT BETWEEN FR 24 AND FR 35. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y765 LT FROM FR 24 TO FR 35; RECEIVED AND INSTALLED A NEW REPLACEMENT SECTION OF SEAT TRACK IAW A320 SRM 51-42-11 FIG 12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y1292 LT, BETWEEN FR 47 AND FR 66. MAINTENANCE REMOVED CORRODED SEAT TRACK Y1292 LT, FROM FR 47 TO FR 64; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK AND 4 EACH SPLICE ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 51-42-11, FIG. 9-13, & 18.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-8 CHECK FRETTING CORROSION WAS FOUND ON CABIN SEAT TRACK Y1292 RT BETWEEN FR 41 AND FR 47. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y1292 RT FROM FR 41 TO FR 47; RECEIVED AND INSTALLED A NEW REPLACEMENT SECTION OF SEAT TRACK IAW A320 SRM 51-42-11 FIG 9-12 & 18.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-8 CHECK FRETTING CORROSION WAS FOUND ON CABIN SEAT TRACK Y765 LT BETWEEN FR 41 AND FR 47. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y765 LT FROM FR 41 TO FR 47; RECEIVED AND INSTALLED A NEW REPLACEMENT SECTION OF SEAT TRACK IAW A320 SRM 51-42-11, FIG 12 & 18.

Part: SUPPORT — CORRODED (FRAME) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON FRAME SUPPORT, FORWARD OF FR 70 AT STR 23 LT. MAINTENANCE REMOVED CORRODED FRAME SUPPORT, FORWARD OF FR 70 AT STR 23 LT; FABRICATED A NEW REPLACEMENT FRAME SUPPORT; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 2, 3, & 8.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

DURING C-8 CHECK STRESS CORROSION WAS FOUND ON FLOORBEAM Y765 LT AT FR 16. MAINTENANCE REMOVED CORRODED FLOORBEAM Y765 LT, FROM FR 12 TO FR 24, INSTALLED NEW REPLACEMENT FLOORBEAM IAW A320 SRM 51-42-11, FIG. 12 & 18.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y1292 RT AT FR 20. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y1292 RT, FROM FR 20 TO FR 24; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK AND 4 EACH SPLICE ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 51-42-11, FIG. 12.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-08 CHECK FOUND A 1 INCH CRACK IN CABIN FLOOR PANEL 251AF. MAINTENANCE REMOVED CRACKED FLOOR PANEL 251AF; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 10D5367022; INSTALLED NEW PANEL IAW A320 SRM 53-02-00 FIG 209 PG 233-236.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y765 R/H, FR 20. MAINTENANCE REMOVED CORRODED SEAT TRACK Y765 R/H, FROM FR 12 TO FR 24, INSTALLED NEW REPLACEMENT SEAT TRACK IAW A320 SRM 51-42-11, FIG. 18.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-8 CHECK GALVANIC CORROSION WAS FOUND ON L-2 DOOR THRESHOLD DRAIN PAN SILL AT FR 68, Y1732 LT. MAINTENANCE REMOVED CORRODED L-2 DOOR THRESHOLD DRAIN PAN SILL AT FR 68, Y1732 LT; FABRICATED A NEW REPLACEMENT SILL; INSTALLED REPAIR PART IAW A320 SRM 53-41-14 FIG 101.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1292 RT BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 R/H FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 9.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1292 RIGHT, FORWARD OF FR 68. MAINTENANCE REMOVED CORRODED BEAM Y1292 RIGHT FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 9, PG 6-7 & 25.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON THE RT OUTBOARD SHEAR PLATE, OUTBOARD OF Y1292, BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED AND REPLACED RT OUTBOARD SHEAR PLATE IAW AIRBUS A320 SRM 51-42-11.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF SUPPORT FRAME BETWEEN FR 69 AND FR 70, STR 24 RT. MAINTENANCE REMOVED CORRODED SUPPORT FRAME BETWEEN FR 69 AND FR 70, STR 24 RT; FABRICATED A NEW REPLACEMENT SUPPORT FRAME; INSTALLED REPAIR PART IAW AIRBUS A320 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y765 LT BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM Y765 L/H FROM FR 66 AND FR 70; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 53-41-14, FIG. 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1292 L/H, FORWARD OF FR 68. MAINTENANCE CUTOUT CORRODED SECTION OF L-2 DOOR SILL FLOORBEAM Y1292 LT FROM FR 67 TO FR 69; PERFORMED HFEC INSPECTION OF CUTOUT; FABRICATED AN ANGLE AND SHIM; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14, FIG. 201.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON SHEAR PLATE, FORWARD SIDE OF FR 70, STR 23 LT. MAINTENANCE REMOVED CORRODED SHEAR PLATE AT FR 70, STR 23 LT; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 53-41-17, FIG. 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y254 RT BETWEEN FR 68 AND FR 70. MAINTENANCE REMOVED CORRODED FLOORBEAM Y254 RT FROM FR 68 TO FR 70; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 12 & 18.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y765 RT AT FR 66. MAINTENANCE REMOVED CORRODED BEAM Y765 RT FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG D53472-190; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 12.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON INBOARD AFT R-2 DOOR SILL BETWEEN FR 66 AND FR 68, Y1800 R/H. MAINTENANCE CUTOUT CORRODED SECTION OF R-2 DOOR SILL FROM FR 66 TO FR 68 AT Y1800 R/H; PERFORMED HFEC INSPECTION OF CUTOUT; FABRICATED AN ANGLE AND SHIM; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14, FIG. 201

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y765 RT BETWEEN FR 66 AND FR 70. MAINTENANCE REMOVED CORRODED FLOORBEAM Y765 RT FROM FR 66 TO FR 70; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 8, 12, & 18.

Part: SPLICE — CORRODED (STRINGER) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER SPLICE BETWEEN FR 66 AND FR 67, STR 26 R/H. MAINTENANCE REMOVED CORRODED STRINGER SPLICE SECTION BETWEEN FR 66 AND FR 67, STR 26 R/H; FABRICATED A NEW REPLACEMENT SPLICE SECTION; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 8 & 12.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-08 CHECK A 2 INCH CRACK WAS FOUND IN SHEAR WEB (TRAY) AFT SIDE OF R-2 DOORWAY, OUTBOARD OF Y1732 RT, BETWEEN FR 68 & FR 69. MAINTENANCE REMOVED CRACKED TRAY FROM Y1732 RT TO Y1800 RT, FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT TRAY PER DWG D53480020; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 2 & 3 PG 7-10 & 12.

Part: WEB — CRACKED (FUSELAGE) · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-08 CHECK A 2 INCH CRACK WAS FOUND IN SHEAR WEB (TRAY) ON AFT SIDE OF L-2 DOOR WAY, OUTBOARD OF Y1732, BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CRACKED SHEAR WEB AFT OF L-2 DOORWAY Y1732, BETWEEN FR 68 AND FR 69; FABRICATED A NEW REPLACEMENT SHEAR WEB; INSTALLED REPAIR PART IAW A320 SRM 51-42-11.

Part: CONNECTOR — BROKEN (CABIN) · airframe 37,573 hrs · 15,484 cycles

MCN - EEL - DURING C-08 CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT HARNESS DAMAGED AT SEAT ROW 24 LT. MAINTENANCE REMOVED AND REPLACED THE CONNECTOR AT EMERGENCY ESCAPE PATH LIGHT HARNESS SEAT ROW 24 LT, OPERATIONAL CHECK WAS GOOD.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,573 hrs · 15,484 cycles

DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 31 RT, AFT OF FR 65 BELOW OUTFLOW VALVE. MAINTENANCE REMOVED CORRODED SECTION OF STRINGER 31 RT AT FR 65+10; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 12 & 18.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-08 CHECK FOUND 3 EACH CRACKS IN CABIN FLOOR PANEL 261EF. MAINTENANCE REMOVED CRACKED FLOOR PANEL 261EF; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 10D5367049; INSTALLED NEW PANEL IAW A320 SRM 53-02-00 FIG 209 PG 233-236.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-08 CHECK A 1 INCH CRACK WAS FOUND IN TWO PLACES ON CABIN FLOOR PANEL 241KF. MAINTENANCE REMOVED CRACKED FLOOR PANEL 241KF; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 10D5367034; INSTALLED NEW PANEL IAW A320 SRM 53-02-00 FIG 209 PG 233-236.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 37,573 hrs · 15,484 cycles

MCN - MAJOR REPAIR - DURING C-08 CHECK FOUND CABIN FLOOR PANEL 241JF DELAMINATED. MAINTENANCE REMOVED DELAMINATED FLOOR PANEL 241JF; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 10D5367033; INSTALLED NEW PANEL IAW A320 SRM 53-02-00 FIG 209 PG 233-236.

Part: LATCH — LACK OF LUBE (CARGO DOOR) · airframe 36,620 hrs · 15,111 cycles

ABORTED TAKEOFF, SHORTLY AFTER TAKEOFF ROLL, EN ROUTE, THE AFT CARGO DOOR INDICATED OPEN, REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE FOUND DOOR SECURED, APPLIED MEL 52-70-01, COND. 8, AND VISUALLY VERIFIED DOOR SECURE. UPON ARRIVAL, MAINTENANCE CLEANED AND LUBRICATED DOOR LATCH MECHANISM, CYCLED DOOR A DOZEN TIMES, DOOR INDICATION WAS GOOD.

Part: TERMINAL BLOCK — ARCED (ZONE 900 - LAVAT) · airframe 33,607 hrs · 1,394 cycles

CRACKLING SOUND AND SPARKS WERE SEEN COMING FROM BEHIND AFT GALLEY OVEN ALONG WITH A SMALL AMOUNT OF SMOKE. AFT GALLEY FEEDER "A" CIRCUIT BREAKER WAS FOUND POPPED IN COCKPIT. MAINTENANCE FOUND TERMINALS LOOSE AT BLOCK TERMINAL (7200VT), TERMINALS 2, 3, & 4, WERE FOUND BURNED. REPLACED TERMINALS 2, 3, & 4 IAW AMM 20-48-11, OPERATIONAL CHECK OF AFT GALLEY OVENS WAS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,199 hrs · 13,793 cycles

MCN - EEL - DURING C-07 CHECK THE EMERGENCY LIGHTS FAIL TEST ON CIDS AS REQUIRED ON TASK CARD R1A25301 STEP 7. MAINTENANCE REMOVED AND REPLACED BATTERIES AT EMERGENCY POWER SUPPLY UNITS (11WL) AND (12WL) IAW AMM 33-51-38-04, SUBTASK 33-51-38-020-053, AND REPLACED EMERGENCY POWER SUPPLY UNIT (10WL) IAW AMM 33-51-38-04, TASK 33-51-38-000-001; OPERATIONAL TEST GOOD IAW AMM 33-51-38-04, TASK 33-51-38-04, AND TASK 33-51-358-000-001.

Part: FITTING — CRACKED · corrosion level 0 · airframe 33,199 hrs · 13,793 cycles

MCN - MAJOR REPAIR - DURING C-07 CHECK HFEC INSPECTION INDICATED 2 EACH CRACKS ON THE L/H MAIN LANDING GEAR DOOR ACTUATOR FITTING, AFT 6TH FASTENER HOLE FROM THE TOP IN KEEL BEAM, 12 AND 6 O'CLOCK POSITION. MAINTENANCE ENLARGED THE AFT 6TH L/H MAIN LANDING GEAR DOOR ACTUATOR FITTING FASTENER HOLE PER E.O. 53-15-17. HFEC INSPECTION VERIFIED NO CRACKS EXIST.

Part: SKIN — CRACKED · corrosion level 0 · airframe 33,199 hrs · 13,793 cycles

MCN - MAJOR REPAIR - DURING C-07 CHECK A 1/4" CRACK WAS FOUND BELOW THE NO. 3 SLAT STOP PAD AT L/H WING LEADING EDGE. MAINTENANCE REPAIRED L/H WING LEADING EDGE IAW A320 SRM 51-42-11, PG. 2, 4, FIG. 204, PG. 212, 214-217, SRM 57-41-18, PG. 202-203, AND DWG D57443557.

Part: SKIN — CRACKED · corrosion level 0 · airframe 33,199 hrs · 13,793 cycles

MCN - MAJOR REPAIR - DURING C-07 CHECK A 1/4" CRACK WAS FOUND BELOW THE NO. 3 SLAT STOP PAD AT R/H WING LEADING EDGE. MAINTENANCE CUTOUT DAMAGED SECTION OF R/H WING LEADING EDGE SKIN AND 2 EACH SECTIONS OF LEADING EDGE SPAR; FABRICATED 2 EACH REPAIR ANGLES, PACKINGS, SKIN INSERTS, AND REINFORCEMENT STRIPS; INSTALLED REPAIR PARTS IAW A320 SRM 51-41-11, PG. 215-217.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 31,815 hrs · 13,241 cycles

PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED DAMAGED CONNECTOR AT LOWER BULKHEAD SEAT ROW 26 LT, OPERATIONAL CHECK WAS GOOD IAW T/C F1C33301.

Part: SWITCH — ERRATIC (COCKPIT) · airframe 31,223 hrs · 13,019 cycles

PHX - EMERGENCY LANDING - FLT 0612 - ON DESCENT INTO PHX EN ROUTE FROM YVR ECAM INDICATED GREEN HYDRAULIC SYSTEM RESERVOIR LOW QUANTITY INDICATION. MAINTENANCE TROUBLESHOT AND FOUND FLUID LEVEL NORMAL, INDICATION PROBLEM ONLY. REPLACED GREEN HYDRAULIC LOW LEVEL SWITCH, OPERATIONAL CHECK WAS GOOD IAW AMM 29-31-00-51. **SUPP** VENDOR TEARDOWN OF LOW LEVEL SWITCH S/N 986 CONFIRMED FAILURE OF UNIT, SWITCH WAS SCRAPPED NO OTHER INFORMATION AVAILABLE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 31,149 hrs · 12,991 cycles

SEA - EMERGENCY EQUIPMENT - DURING INSPECTION THE EMERGENCY FLASHLIGHT AT THE AFT FLIGHT ATTENDANT JUMP SEAT WAS FOUND TO HAVE A LOW BATTERY. MAINTENANCE REPLACED THE BATTERIES IN EMERGENCY FLASHLIGHT AT THE AFT FLIGHT ATTENDANTS JUMP SEAT.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 28,977 hrs · 12,137 cycles

YWG - C6 CK - "C" - CORROSION FOUND ON #4 SEAT TRACK AT FR 20R, Y-1292. AFTER CORROSION REMOVAL FOUND TO BE BEYOND SRM LIMITS. MAINTENANCE REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED REPAIR SECTION AND SPLICES AND INSTALLED IAW A320 SRM 53-11-15, FIG 203, PG 217 - 218.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 28,977 hrs · 12,137 cycles

YWG - C6 CK - "C" - CORROSION FOUND ON #3 SEAT TRACK AT FR 20R, Y765. AFTER CORROSION REMOVAL, FOUND TO BE BEYOND SRM LIMITS. MAINTENANCE REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED REPAIR SECTION AND SPLICEDS AND INSTALLED IAW SRM 53-00-15, FIG 201, PG 202 - 206

Part: PILOT VALVE — LEAKING (HYDRAULIC SYS) · airframe 27,808 hrs · 11,680 cycles

PHX - AIR TURNBACK - 6/5/01 - FLT 253 - EN ROUTE TO PHL ECAM MSG DISPLAYED HYD YELLOW SYS LOW LEVEL; YELLOW HYD QUANTITY INDICATED IN THE AMBER BAND; CREW COMPLIED W/ THE ECAM ACTIONS & RETURNED TO PHX MAKING AN UNEVENTFUL LANDING. MX INSPECTED THE A/C AND FOUND THE YELLOW HYD SYS LEAK MEASUREMENT VALVE, PILOT VALVE LEAKING; THE PILOT VALVE WAS REPLACED, THE YELLOW SYS WAS SERVICED AND LEAK CHECKS AND FUNCTIONAL CHECKS WERE GOOD IAW AMM 29-19-51-401.

Part: VOR SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 27,801 hrs · 11,674 cycles

PHX - AIR TURNBACK - 6/2/01 - FLT 73 - ON DEPARTURE CLIMBOUT OF PHX THE AIRCRAFT LOST VOR NR 1, VOR NR 2, ILS NR 1 & ILS NR 2; THE AIRCRAFT RETURNED TO PHX. IN PHX MAINTENANCE RESET NR 1 & NR 2 RMP NAV SWITCHES AND CIRCUIT BREAKERS; CYCLED NR 1 & NR 2 FMGC CIRCUIT BREAKERS AND PERFORMED ADIRU REALIGNMENT. PERFORMED AFS TEST 22-96-00-501 W/ NO FAULTS NOTED. PERFORMED NR 1 & NR 2 VOR, ILS AND ADIRU'S BITE TEST W/ NO FAULTS NOTED AND NR 1 & NR 2 RMP BITE TEST W/ NO FAULTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE AND NO FURTHER DISCREPANCIES HAVE BEEN REPORTED.

Part: LINE — CLOGGED (LAVATORY) · airframe 26,809 hrs · 11,258 cycles

LAS - AIR TURNBACK - 2/22/01 - ALL LAVS WOULD NOT FLUSH (CIDS PANEL RED LIGHT WAS ON, WASTE AT 0 PERCENT FULL, WATER AT 40 PERCENT FULL); AIRCRAFT DESTINATION WAS JFK SO THE FLIGHT RETURNED TO LAS. THE LAV SYSTEM HAD PREVIOUSLY BEEN PLACED ON MEL 38-30-01 FOR THE VAC GENERATOR INOP. HOWEVER THE SYSTEM FAILED TO FLUSH USING DIFFERENT DIFFERENTIAL PRESSURE AT ALTITUDE. IN LAS MAINTENANCE FOUND THE WASTE LINE CLOGGED AT THE LAV WASTE TANK; THE LINE WAS DISCONNECTED AND CLEANED OUT; AFTER CLEANING THE SYSTEM FUNCTIONALLY CHECKED GOOD.

Part: FITTING — LEAKING (AIR DISTRIBUTION)

DURING CLIMBOUT NOTICED VERY STRONG DIRTY SOCKS ODOR IN COCKPIT. REMOVED AND REPLACED LEAKING SERVICE OVERFLOW FITTING, WASHED OIL FROM APU INLET AND AIRCRAFT INLET.

Part: BATTERY PACK — DISCHARGED (GALLEY)

EMERGENCY EXIT LIGHTS BLINK ON AND OFF DURING CRUISE. REMOVED AND REPLACED AFT GALLEY EMER LIGHT BATT PACK, SYSTEM TEST OK.

Part: WINDSHIELD — CRACKED (LT COCKPIT)

EMERGENCY DESCENT, PILOTS FWD WINDSHIELD CRACKED. REPLACED CAPTAINS FWD WINDSHIELD.

Part: RAIL — CORRODED (BS 189)

IN MAINTENANCE, FOUND CORROSION DUMMY RAIL Y189 RT CORRODED AT FR 21. FABRICATED NEW RAIL Y189 AS PER SRM 51-72-11. TREATED, PRIMED AND PAINTED PER SRM 51-75-00. INSTALLED RAIL PER DWG D5312836. NRC 5159872, ZONE 1D SEQ 023.

Part: RAIL — CORRODED (BS 1292)

IN MAINTENANCE, FOUND CORROSION ON FLOOR RAIL Y1292 RT CORRODED FROM FR 16 TO TRACK SPLICE AT C-20. FABRICATED NEW RAIL PER DWG D53112781202. TREATED, PRIMED AND PAINTED PER 51-75-00. INSTALLED RAIL PER SRM 51-72-11. NRC 5159876, ZONE 1D SEQ 026.

Part: RAIL — CORRODED (BS 254)

IN MAINTENANCE, FOUND CORROSION ON FLOOR RAIL Y254 LT, FR 16-23 CORROSION AROUND MOUNT SCREW HOLES, CORROSION ON UPPER AND LOWER SURFACES. CORROSION REMOVAL BEYOND LIMITS. FABRICATED NEW RAIL PER DWG D5311281200. TREATED, PRIMED AND PAINTED AS PER SRM 51-75-00. INSTALLED RAIL PER SRM 51-72-11, NRC5159866, ZONE 1D SEQ 017.

Part: FLOOR TRACK — CORRODED (BS 765)

IN MAINTENANCE, FOUND CORROSION SEAT TRACK Y765 LEFT CORRODED FR 20. REPAIRED PER SRM 53-00-15, NRC 5159871, ZONE 1D SEQ 022.

Part: RAIL — CORRODED (BS 254)

IN MAINTENANCE, FOUND CORROSION ON FLOOR RAIL Y254 CORRODED FROM FR 16 TO FR 20. FABRICATED NEW TRACK AS PER DWG D53112782200. TREATED, PRIMED AND PAINTED PER SRM 51-75-00. INSTALLED RAIL PER SRM 53-11-14. NRC 5159873, ZONE 1D SEQ 024.

Part: FLOOR TRACK — CORRODED (BS 808)

NR 2 AND 3 FLOOR TRACK STN 808 FR 20 REPLACED DUE CORROSION BEYOND SRM LIMITS. SPLICED IN FLOOR TRACK AS PER SRM 53-00-15 PAGE 201.

Part: FLOOR TRACK — CORRODED (BS 808)

DURING SCHEDULED C-3 INSPECTION, REPLACED NR 2 AND NR 3 FLOOR TRACK STN 808 FR 20 DUE TO CORROSION BEYOND SRM LIMITS. SPLICED IN FLOOR TRACK PER SRM 53-00-15, PAGE 201.

Part: SEAT TRACK — CORRODED (BS 808)

DURING SCHEDULED C-3 INSPECTION, NR 4 SEAT TRACK REPLACED FROM STN 808 FR 20 TO STN 950 FR 24 DUE TO CORROSION BEYOND SRM LIMITS. SPLICED IN FLOOR TRACK PER ER 32-53-12-17.

Part: SEAT TRACK — CORRODED (BS 808)

NR 4 SEAT TRACK REPLACED FROM STN 808 FRO 20 TO STN 950 FRA 24 DUE CORRODED BEYOND SRM LIMITS. SPLICED IN FLOOR TRACK AS PER ER 32-53:12-17.

Part: BATTERY — DISCHARGED (CABIN)

FWD LT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY ASSY, OPS CHECK NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS AT RT MID-CABIN EXITS INOP. REMOVED AND REPLACED POWER SUPPLY UNIT. OPS CHECK OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INTERMITTENT IN AFT CABIN. REMOVED AND REPLACED AFT POWER SUPPLY, NO HELP. ORIGINAL AFT POWER SUPPLY INSTALLED AND RESET, SYSTEM OPS TEST GOOD.

Part: CONNECTOR — BROKEN (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT WIRE BROKEN AT CANNON PLUG. REMOVED AND REPLACED CANNON PLUG. SYSTEM OPS CHECKS GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND LT OVERWING EMERGENCY POWER SUPPLY FAULTS ON BITE. REMOVED AND REPLACED POWER SUPPLY, BITE TEST NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

PHX - FLT 2249 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT FORWARD INOPERATIVE. FORWARD BATTERY DEAD. REMOVED AND REPLACED BATTERY PACK. OPERATES GOOD. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

PHX - FLT 2249 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT INTERMITTENTLY INOPERATIVE THROUGHOUT CABIN. MID-RIGHT BATTERY DEAD. REMOVED AND REPLACED BATTERY PACK. OPERATIONS CHECK GOOD. (X)

Part: BATTERY — DISCHARGED (CABIN)

PYX - FLT 2249 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT INTERMITTENT, INOPERATIVE THROUGHOUT CABIN. FORWARD AND MID-RIGHT BATTERIES DEAD. REMOVED AND REPLACED BATTERY PACKS. OPS CHECK GOOD. REF: OPERATOR CONTROL NR AWXA960405.

Part: BATTERY — DISCHARGED (CABIN)

PYX - FLT 2249 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT INTERMITTENT, INOPERATIVE THROUGHOUT CABIN. FORWARD AND MID-RIGHT BATTERIES DEAD. REMOVED AND REPLACED BATTERY PACKS. OPS CHECK GOOD. REF: OPERATOR CONTROL NR 96ZZZX5182. (X)