N644AW

Part: ACTUATOR — FAULTY (NLG) · airframe 70,119 hrs · 30,960 cycles

AFTER LG RETRACTION, NOSE GEAR DOORS WOULD NOT CLOSE. INDICATION ON WHEEL PAGE CONFIRMED WITH ACFT BUFFETING. RECYCLED GEAR, SAME RESULT. NOSE GEAR DOORS CLOSED 3 MINUTES LATER & STAYED CLOSED. REPLACED THE NLG ACTUATING CYLINDER IAW AMM 32-31-16-400-001-A. OPERATIONS CHECKED GOOD.

Part: SLIDE — FAILED (L1 DOOR) · airframe 69,912 hrs · 30,806 cycles

L1 DOOR SLIDE RAFT INSPECTION FAILED IAW EO 2514A109, FOUND CONTACT WITH THE SLIDE COVER & FUSELAGE, NO DAMAGE FOUND. L1 DOOR SLIDE RAFT INSPECTION FAILED IAW EO 2514A109. FOUND CONTACT WITH THE SLIDE COVER & FUSELAGE, NO DAMAGE FOUND. REPLACED L1 DOOR EMERGENCY SLIDE.

Part: SLIDE — FAILED (L2 DOOR) · airframe 69,912 hrs · 30,806 cycles

L2 DOOR SLIDE RAFT INSPECTION FAILED IAW EO 2514A109. FOUND CONTACT WITH THE SLIDE COVER & FUSELAGE, NO DAMAGE FOUND. L2 DOOR SLIDE RAFT INSPECTION FAILED IAW EO 2514A1. FOUND CONTACT WITH THE SLIDE COVER & FUSELAGE, NO DAMAGE FOUND. REPLACED DOOR L2 EMER SLIDE IAW JOB CARD 26L00025011.

Part: PACKING — LEAKING (MANIFOLD) · airframe 69,351 hrs · 30,425 cycles

LOSS OF YELLOW HYD SYS. REPLACED PACKING ON MANIFOLD ASSEMBLY IAW IPC 32-44-03-06 ITEM 50, PACKING NAS 1612-10, SERVICED YELLOW HYD TO SPECIFICATIONS, PRESS CHECKED OK.

Part: CONNECTOR — DISCONNECTED (ELECTRICAL SYS) · airframe 69,289 hrs · 30,380 cycles

ON CLIMB OUT CREW REPORTED AN ELEC DC ESS FAULT ON ROTATION. DECLARED AN EMER & RETURNED TO FIELD. FLIGHT LANDED WITHOUT FURTHER INCIDENT. FOUND CONNECTOR OFF OF ESSENTIAL TR CONTACTOR 3PE. REINSTALLED CONNECTOR IAW AMM 24-34-55-400-001-A. ACCOMPLISHED OPERATIONS TEST OF EMER GENERATOR SYS IAW AMM 24-24-00-710-001-A. ALL OPERATIONS NORMAL.

Part: DOOR — LOOSE (NR 1 ENGINE) · airframe 69,098 hrs · 30,273 cycles

ON REACHING LEVEL OFF AT 35000 FT, NR 1 ENGINE VIBRATION EXCEEDED 5.0 N1, IT REACHED A MAXIMUM OF 6.2. REDUCED POWER TO KEEP VIBRATION BELOW 5.0 IAW TSM 77-30-00-810-826A. FOUND NR 1 ENG OIL SERVICE DOOR LOOSE & HAS PLAY. REPLACED ENGINE OIL SERVICE DOOR & HINGE ASSEMBLY IAW SRM 51-42-11.

Part: CONTAINER — FAULTY (CABIN) · airframe 69,019 hrs · 30,229 cycles

FORWARD FLIGHT ATTENDANT O2 COMPARTMENT FAILED MANUAL DROP TEST. REPLACED FWD FLIGHT ATTENDANT EMER OXYGEN CONTAINER IAW AMM 35-21-41-401.

Part: LENS — BROKEN (CABIN) · airframe 68,986 hrs · 30,213 cycles

EMERGENCY LIGHT LENS AT SEAT 9C IS BROKEN. REPLACED EMER LIGHT LENS AT SEAT 9C.

Part: BUTTON — STUCK (CABIN SEAT) · airframe 68,896 hrs · 30,163 cycles

EMERGENCY EXIT ROW SEAT 11C RECLINE BUTTON STUCK IN. FREED STUCK RECLINE BUTTON 11C. OPERATIONS CHECKED NORMAL. OK FOR SERVICE.

Part: LENS — MISSING (CABIN) · airframe 67,881 hrs · 29,683 cycles

EMERGENCY EXIT LENS NEAR FLOOR LEVEL AT DOOR 1L MISSING. REPLACED EMERGENCY EXIT LENS NEAR FLOOR LEVEL AT DOOR 1L.

Part: BLANKING PLATE — UNKNOWN (FUSELAGE) · airframe 67,734 hrs · 29,620 cycles

MOD LINE VISIT, R & R IFPC ANTENNA BLANKING PLATE ON FUSELAGE SKIN BETWEEN FRAME 62 TO FRAME 63 & BETWEEN STRINGER 43L TO STRINGER 44 IAW EA 206696A.

Part: BLANKING PLATE — UNKNOWN (FUSELAGE) · airframe 67,734 hrs · 29,620 cycles

MOD LINE VISIT, R & R IFPC ANTENNA BLANKING PLATE ON FUSELAGE SKIN BETWEEN FRAME 60 TO FRAME 61 & BETWEEN STRINGER 43L TO STRINGER 44 IAW EA 206696A.

Part: ESCAPE ROPE — MISSING (CABIN) · airframe 67,345 hrs · 29,430 cycles

OVERWING EMERGENCY EXIT ESCAPE ROPE MISSING. INSTALLED OVERWING EMERGENCY EXIT ESCAPE ROPE IN OVERHEAD BIN IAW DRAWING 2560012.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 67,340 hrs · 29,428 cycles

4S CHECK, CABIN FLOOR PANEL 221DF DELAMINATED. FABRICATED & INSTALLED NEW FLOOR PANEL IAW IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 67,340 hrs · 29,428 cycles

4S CHECK, CABIN FLOOR PANEL 261EF DELAMINATED. FABRICATED & INSTALLED NEW FLOOR PANEL IAW IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 67,340 hrs · 29,428 cycles

4S CHECK, CABIN FLOOR PANEL 261NF DELAMINATED. FABRICATED & INSTALLED NEW FLOOR PANEL IAW IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 67,340 hrs · 29,428 cycles

4S CHECK, CABIN FLOOR PANEL 261DF DELAMINATED. FABRICATED & INSTALLED NEW FLOOR PANEL IAW IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 67,340 hrs · 29,428 cycles

4S CHECK, CABIN FLOOR PANEL 262EF DELAMINATED. FABRICATED & INSTALLED NEW FLOOR PANEL IAW IRM 9701 REV G.

Part: CYLINDER — LEAKING (R1 DOOR) · airframe 67,340 hrs · 29,248 cycles

R1 SEAL MISSING FROM PRESS GAUGE OF DOOR DAMPER. REPLACED R1 DOOR DAMPER CYLINDER IAW A320 AMM 52-11-14.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 67,340 hrs · 29,428 cycles

S4 CHECK, CORROSION ON STRINGER 13R BETWEEN FR 64 TO FR 67. REPLACED STRINGER 13R BETWEEN FR 64 TO FR 67 IAW A320 SRM 51-72-11, 51-42-11 & DRAWING 53480020.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 67,340 hrs · 29,428 cycles

S4 CHECK LEVEL 2 CORROSION ON LT WING LOWER FUEL DOOR PANEL 540QB BETWEEN WING RIBS 20L TO RIB 21L & BETWEEN STRINGER 8L TO STRINGER 11L. REPLACED LT WING LOWER FUEL DOOR PANEL 540QB IAW A320 SRM 51-75-12.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 67,340 hrs · 29,428 cycles

S4 CHECK LEVEL 2 CORROSION ON LT WING LOWER FUEL DOOR PANEL 540MB BETWEEN WING RIBS 17L TO RIB 18L & BETWEEN STRINGER 8L TO STRINGER 11L. REPLACED LT WING LOWER FUEL DOOR PANEL 540MB IAW A320 SRM 51-75-12.

Part: SILL — CORRODED (FUSELAGE) · airframe 67,340 hrs · 29,428 cycles

4S CHECK, L2 DOOR SILL CORRODED BETWEEN FR 67 & FR 69 AT Y 1292. REPAIRED DOOR SILL IAW EA 206275.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,340 hrs · 29,428 cycles

S4 CHECK, LEVEL 2 INTERGRANULAR CORROSION ON FLOOR BEAM BETWEEN FR 66 TO FR 68, Z 500, Y 1292. REPLACED FLOOR BEAM BETWEEN FR 66 TO FR 68, Z 500, Y 1292 IAW A320 SRM 51-72-11.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 67,253 hrs · 29,389 cycles

RED LENS MISSING FROM EMERGENCY LIGHT AT SEAT 11C. INSTALLED RED LENS ON EMERGENCY LIGHT AT SEAT 11C.

Part: LIGHT — BROKEN (ZONE 200) · airframe 67,121 hrs · 29,326 cycles

MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT THAT MOUNTS TO SEAT ROW 15, ACFT LT, IS BROKEN. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT . OPS CHECKED GOOD.

Part: LENS — MISSING (EXIT SIGN) · airframe 66,036 hrs · 28,798 cycles

EMERGENCY EXIT SIGN COVER IS MISSING AT DOOR 1L. INSTALLED NEW EMERGENCY EXIT SIGN COVER AT DOOR 1L.

Part: SLIDE — CRACKED (CABIN) · airframe 65,997 hrs · 28,774 cycles

RIGHT OVERWING SLIDE HAS VERTICAL CRACK APPROX. 8" LONG. REPLACED SLIDE.

Part: LENS — MISSING (CABIN) · airframe 65,978 hrs · 28,767 cycles

L2 DOOR MISSING EMERGENCY LIGHT LENS. REPLACED L2 DOOR EMERGENCY LIGHT LENS.

Part: LIGHT — LOOSE (CABIN) · airframe 65,969 hrs · 28,761 cycles

EMERGENCY EXIT LIGHT UNDER SEAT 11D LOOSE. REINSTALLED LIGHT ASSY, OPS CHECK GOOD IAW MM 33-51-00-710-001-A.

Part: LENS — BROKEN (EXIT SIGN) · airframe 65,958 hrs · 28,754 cycles

DOOR 1L EXIT SIGN LENS BROKEN. REPLACED L1 DOOR EMERGENCY LIGHT COVER.

Part: LIGHT — LOOSE (CABIN) · airframe 65,765 hrs · 28,663 cycles

SEAT MOUNTED EMERGENCY LIGHT AT 17L, LOOSE. RESECURED EMERGENCY PATH LIGHT AT 17L.

Part: LIGHT — LOOSE (CABIN) · airframe 65,765 hrs · 28,663 cycles

SEAT MOUNTED EMERGENCY LIGHT IS LOOSE AT 13L. RESECURED EMERGENCY PATH LIGHT AT 13L.

Part: FLOORBOARD — CRACKED (FUSELAGE) · airframe 65,760 hrs · 28,659 cycles

ATG 4 MOD VISIT -CRACK AND DISBONDING ON FLOORBOARD 251LF BETWEEN FR57 & FR58 AND BETWEEN Y254 TO Y254. REPLACED FLOORBOARD 251LF IAW AMM 53-42-12-401.

Part: DIAPHRAGM — UNSERVICEABLE (L2 DOOR) · airframe 65,634 hrs · 28,600 cycles

L-2 DOOR EMERGENCY OPERATION CYLINDER PRESSURE DEPLETED. REPLACED DIAPHRAM IN L-2 DOOR EMERGENCY OPERATION CYLINDER.

Part: SLIDE — FAILED (CABIN) · airframe 65,634 hrs · 28,600 cycles

EMERGENCY ESCAPE SLIDE AFT LEFT DEPLOYED BY GROUND SECURITY PERSONNEL FROM INSIDE AIRCRAFT. FAILED TO FULLY DEPLOY.

Part: LENS — MISSING (CABIN) · airframe 65,369 hrs · 28,474 cycles

EMERGENCY AISLE LIGHT LENS IS MISSING AT ROW 11R. INSTALLED EMERGENCY AISLE LIGHT LENS AT ROW 11R.

Part: LENS — MISSING (FUSELAGE) · airframe 65,353 hrs · 28,465 cycles

FOUND SEAT 1L EMERGENCY LIGHT LENS COVER MISSING. REPLACED SEAT 1L LIGHT COVER.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 65,324 hrs · 28,451 cycles

L1 DOOR DIFFICULT TO CLOSE. LUBRICATED L1 DOOR PER AIRBUS AMM 12-22-52-03.

Part: WIRE — DAMAGED (CABIN) · airframe 65,153 hrs · 28,375 cycles

ROW 7L SEAT MOUNTED EMERGENCY EXIT LIGHT-INOPERATIVE. RE-TERMINATED WIRE IN ACCORDANCE WITH ELECTRICAL STANDARD PRACTICES MANUAL CHAPTER 20. LIGHT OPERATES NORMALLY.

Part: LENS — MISSING (CABIN) · airframe 64,998 hrs · 28,303 cycles

EMERGENCY LIGHT LENS COVER MISSING FROM SEATS 17L, 16L. INSTALLED EMERGENCY EXIT LENS COVER ON SEATS 17L AND 16L.

Part: WIRE — DISCONNECTED (CABIN) · airframe 64,845 hrs · 28,229 cycles

MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY AISLE LIGHT IS INOP AT ROW 7L. MAINTENANCE FOUND WIRE TO BE DISCONNECTED FROM LIGHT ASSEMBLY. RECONNECTED WIRE. OPS CHECK NORMAL.

Part: LENS — BROKEN (CABIN) · airframe 64,509 hrs · 28,071 cycles

DOOR L1 EMERGENCY EXIT LIGHT COVER BROKEN. INSTALLED NEW EMERGENCY EXIT LIGHT LENS COVER. OPS CHECKED GOOD.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 64,443 hrs · 28,036 cycles

RON CHECK - DELAMINATION ON FORWARD GALLEY FLOOR PANEL AT FR18, RBL 20. REPLACED FORWARD GALLEY FLOOR PANEL AT FR18, RBL 20 IAW A320 AMM 53-12-12-400.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,351 hrs · 27,994 cycles

ROW 5 LEFT EMERGENCY LIGHT INOPERATIVE. RE-TERMINATED LIGHT AT 4 LEFT LIGHT. OPS CHECKED GOOD.

Part: LENS — DETACHED (CABIN) · airframe 64,286 hrs · 27,960 cycles

AFT RIGHT DOOR EXIT LIGHT COVER FELL OFF. REPLACED EMERGENCY EXIT DOOR (AFT RIGHT) LENS.

Part: LENS — MISSING (CABIN) · airframe 63,571 hrs · 27,614 cycles

ROW 9R EXIT ROW LIGHT LENS MISSING. REPLACED MISSING LENS AT ROW 9R.

Part: LIGHT — LOOSE (CABIN) · airframe 63,259 hrs · 27,457 cycles

EMERGENCY EXIT LIGHTS ROW 5 AND 17 AIRCRAFT LEFT ARE LOOSE AND ROW 19 IS BROKEN. RE-SECURED EMERGENCY LIGHTS AT ROWS 5, 17 AND 19. EMERGENCY EXIT LIGHT SYSTEM OPS CHECKED NORMAL IAW AIRBUS MAINTENANCE MANUAL 33-51-00-710-001A.

Part: LIGHT — BROKEN (CABIN) · airframe 62,749 hrs · 27,197 cycles

SEAT 17C EMERGENCY LIGHT IS DISCONNECTED FROM SEAT. MAINTENANCE SECURED LIGHT AND PLACED ON DEFERRAL. REMOVED AND REPLACED EMERGENCY LIGHT AT SEAT 17C.

Part: WIRE — DAMAGED (GENERATOR) · airframe 62,526 hrs · 27,084 cycles

BC7 CHECK - OPERATIONAL TEST OF EMERGENCY GENERATING SYSTEM FAILED. REPAIRED DAMAGED WIRES FOR THE CONSTANT SPEED MOTOR GENERATOR, PERFORMED OPERATIONAL TEST OF THE EMERGENCY GENERATING SYSTEM IAW A320 WD 24-24-01, 24-24-02, 20-53-21 AND A320 AMM 24-24-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,522 hrs · 27,083 cycles

BC7 CHECK - AFT LEFT LAV EMERGENCY EXIT LIGHT INOPERATIVE. SECURED BULB AT AFT LEFT LAV EMERGENCY EXIT LIGHT IAW MPPM 54-03-20 AND OPS CHECKED GOOD IAW AMM 33-51-00.

Part: TERMINAL — LOOSE (EMERGENCY LIGHT) · airframe 62,522 hrs · 27,083 cycles

C7 CHECK - MAIN CABIN INTERIOR EMERGENCY LIGHT BETWEEN LEFT EMERGENCY EXITS IS INOPERATIVE. TIGHTENED LOOSE TERMINAL AT MAIN CABIN INTERIOR EMERGENCY LIGHT LEFT IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,521 hrs · 27,082 cycles

BC7 CHECK - 15 CRACKS IN FORWARD FRAME SEGMENT ON RIGHT FORWARD EMERGENCY EXIT DOOR 843. REPLACED FRAME SEGMENT ON RIGHT FORWARD EMERGENCY EXIT DOOR 843 IAW EO 5210Y228.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,521 hrs · 27,082 cycles

BC7 CHECK - 13 CRACKS IN FORWARD FRAME SEGMENT ON LEFT FORWARD EMERGENCY EXIT DOOR 833. REPLACED FRAME SEGMENT ON LEFT FORWARD EMERGENCY EXIT DOOR 833 IAW AIRWAYS EO 5210Y228.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,521 hrs · 27,082 cycles

BC7 CHECK - 12 CRACKS IN AFT FRAME SEGMENT ON RIGHT AFT EMERGENCY EXIT DOOR 844. REPLACED FRAME SEGMENT ON RIGHT AFT EMERGENCY EXIT DOOR 844 IAW EO 5210Y228.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,521 hrs · 27,082 cycles

BC7 CHECK - 12 CRACKS IN AFT FRAME SEGMENT ON LEFT AFT EMERGENCY EXIT DOOR 834. REPLACED FRAME SEGMENT ON LEFT AFT EMERGENCY EXIT DOOR 834 IAW EO 5210Y228.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,521 hrs · 27,082 cycles

BC7 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR16, Y520. REPAIRED SEAT TRACK BETWEEN FR13 TO FR16, Y520 IAW SRM 51-42-11.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,521 hrs · 27,082 cycles

BC7 CHECK - 11 CRACKS IN FORWARD FRAME SEGMENT ON RIGHT AFT EMERGENCY EXIT DOOR 844. REPLACED FRAME SEGMENT ON RIGHT AFT EMERGENCY EXIT DOOR 844 IAW EO 5210Y228.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,521 hrs · 27,082 cycles

BC7 CHECK - 1 CRACK IN FORWARD FRAME SEGMENT ON LEFT AFT EMERGENCY EXIT DOOR 834. REPLACED FRAME SEGMENT ON LEFT AFT EMERGENCY EXIT DOOR 834 IAW EO 5210Y228.

Part: LIGHT — WRONG PART (ZONE 200) · airframe 62,521 hrs · 27,082 cycles

BC7 CHECK - FORWARD EXIT LIGHT OUTSIDE LAVATORY D IS THE WRONG COLOR, IT SHOULD BE WHITE (IS RED). REMOVED THE FORWARD EXIT LIGHT OUTSIDE LAVATORY D AND REPLACED IT WITH A WHITE COLOR LIGHT IAW AMM 33-51-19.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,521 hrs · 27,082 cycles

BC7 CHECK - 8 CRACKS IN AFT FRAME SEGMENT ON LEFT FORWARD EMERGENCY EXIT DOOR 833. REPLACED FRAME SEGMENT ON LEFT FORWARD EMERGENCY EXIT DOOR 833 IAW EO 5210Y228.

Part: PLATE — CORRODED (RT PYLON) · airframe 62,521 hrs · 27,082 cycles

BC7 CHECK CORROSION ON SPIGOT PIN RT PYLON UPPER PANEL INNER RACE. REPLACED RT PYLON UPPER PANEL INNER RACE IAW A320 AMM 54-51-12 & REPLACED RT PYLON UPPER SPIGOT PLATE IAW A320 SRM 54-51-12 FIG 201.

Part: STRUCTURE — CORRODED (LT PYLON) · airframe 62,521 hrs · 27,082 cycles

BC7 CHECK, LT PYLON SPIGOT PIN OUTER RACE APPROXIMATELY 75% DAMAGED DUE TO CORROSION, EXCEEDS THE .002 LIMIT. REPLACED LT PYLON SPIGOT PIN OUTER RACE IAW A320 SRM 54-51-12, FIG 201.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 62,521 hrs · 27,082 cycles

BC7 CHECK - CRACK ON SHEAR PLATE AT FR70, Y1292. REPLACED SHEAR PLATE AT FR70, Y1292 IAW SERVICE BULLETIN A320-53-1207.

Part: LENS — BROKEN (CABIN) · airframe 62,521 hrs · 27,082 cycles

BC7 CHECK - MAIN CABIN WALL MOUNTED EXIT LENS ARE BROKEN. REPLACED MAIN CABIN WALL MOUNTED EXIT LENS IAW A320 / AMM 33-51-13.

Part: WEB — CRACKED (ZONE 100) · airframe 62,521 hrs · 27,082 cycles

CRACK ON FLOOR WEB AT FR68, -Y1162.5. REPAIRED FLOOR WEB AT FR68, -Y1162.5 IAW A320 SRM 51-42-11.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 62,521 hrs · 27,082 cycles

BC7 CHECK - FLOOR PANEL 231KF AT BS 2885, BL 0 IS SOFT AND SPONGY. REPLACED FLOOR PANEL 231KF IAW A320 AMM 53-42-12.

Part: BRACKET — BROKEN (CABIN) · airframe 62,309 hrs · 26,983 cycles

THE 9C EMERGENCY LIGHT BROKEN. MAINTENANCE REPLACED EMERGENCY LIGHT BRACKET.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 62,241 hrs · 26,954 cycles

RON - SOFT FLOOR PANEL 251AF BETWEEN FR47 TO FR51. REPAIRED FLOOR PANEL 251AF BETWEEN FR47 TO FR51 IAW A320 SRM 53-02-00 FIGURE 208.

Part: GIRT BAR — OUT OF ADJUST (L2 DOOR) · airframe 62,126 hrs · 26,908 cycles

DOOR 2L UNABLE TO ARM / CLOSE. MAINTENANCE ADJUSTED GIRT BAR STRAP.

Part: LENS — BROKEN (CABIN) · airframe 61,906 hrs · 26,806 cycles

RED LENS COVER OFF EMERGENCY LIGHT IN FORWARD ENTRY BROKE AND WILL NOT STAY ON. REMOVED AND REPLACED EMERGENCY LIGHT RED COVER ON FORWARD PARTITION WALL. OPS CHECK GOOD.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 61,666 hrs · 26,702 cycles

FLIGHT ATTENDANT REPORTED AN ELECTRICAL SMELL IN MID CABIN. MAINTENANCE PERFORMED INSPECTION AND FOUND BURNED OUT LAMP AND BALLAST AT ROW 22/23 LT. REPLACED SAME WITH NO FURTHER SMELL NOTED.

Part: FAN — FAULTY (E&E BAY) · airframe 61,253 hrs · 26,511 cycles

AVIONIC BLOWER FAN MAKING GRINDING SOUND AND CREW REPORTED SMELLING ELECTRICAL SMOKE IN COCKPIT. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED BLOWER FAN 20HQ IAW AIRBUS MAINTENANCE MANUAL 21-26-51-401.

Part: SPLICE — BROKEN (CABIN) · airframe 61,238 hrs · 26,503 cycles

EMERGENCY LIGHTING AT ROW 9ABC INOPERATIVE. MAINTENANCE REPLACED BROKEN SPLICE AT 9ABC.

Part: BUMPER — BROKEN (CABIN) · airframe 61,166 hrs · 26,470 cycles

ROW 15 AIRCRAFT LEFT EMERGENCY LIGHT BROKEN. REMOVED AND REPLACED AISLE BUMPER AT ROW 15 AIRCRAFT LEFT THAT HOLDS EMERGENCY LIGHT.

Part: LIGHT — LOOSE (CABIN) · airframe 61,122 hrs · 26,454 cycles

EMERGENCY EXIT LIGHT LOOSE. MAINTENANCE SECURED EMERGENCY LIGHT AT ROW 15L.

Part: COFFEEMAKER — DEFECTIVE (GALLEY) · airframe 60,997 hrs · 26,397 cycles

CABIN CREW NOTICED ELECTRICAL SMELL WHEN AFT COFFEEMAKER WAS TURNED ON IN FLIGHT. TURNED BOTH COFFEEMAKERS OFF AND SMELL DISSIPATED. MAINTENANCE REMOVED AND REPLACED AFT GALLEY NR 3 COFFEEMAKER.

Part: DIFFUSER — BROKEN (CABIN) · airframe 60,931 hrs · 26,363 cycles

R2 DOOR EMERGENCY EXIT SIGN HAS BROKEN DIFFUSER PANEL. MAINTENANCE REPLACED EXIT SIGN DIFFUSER PANEL WITH NEW LAMPS.

Part: LENS — MISSING (CABIN) · airframe 60,513 hrs · 26,154 cycles

PHX-LAS - EEL - EMERGENCY EXIT LIGHT LENS AT L1 DOOR MISSING. INSTALLED EMERGENCY EXIT LIGHT LENS AT L1 DOOR.

Part: PIN — PULLED (EMERGENCY LIGHT) · airframe 60,513 hrs · 26,154 cycles

PHX-LAX - EEL - EMERGENCY EXIT LIGHT AT 13L INOPERATIVE. FOUND PIN PULLED FROM RECEPTACLE 726OVC5. REPINNED PINS C & B PER ELECTRICAL STANDARD PRACTICES MANUAL (ESPM) CHAPTER 20, OPERATIONAL CHECK GOOD.

Part: SLIDE — DELAMINATED (OVERWING EXIT) · airframe 60,370 hrs · 26,086 cycles

PHX - EES - LT OVERWING SLIDE DELAMINATED AT THE LOWER CORNER. REMOVED AND REPLACED LT OVERWING SLIDE IAW AIRBUS MAINTENANCE MANUAL 25-62-42-0401.

Part: LENS — MISSING (CABIN) · airframe 60,221 hrs · 26,022 cycles

PDX - EEL - EMERGENCY EXIT SIGN AND LIGHT MISSING DOOR 2-R. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT LENS AT DOOR 2-R.

Part: LIGHT — DETACHED (CABIN) · airframe 59,476 hrs · 25,694 cycles

FLT 504 - PHX - EEL - EMERGENCY LIGHT UNDER SEAT 5C IS DETACHED FROM SEAT ASSEMBLY. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 5C.

Part: BRACKET — LOOSE (CABIN) · airframe 59,376 hrs · 25,650 cycles

FLT 612 - PHX - EEL - EMERGENCY EXIT LIGHT AT 19C BROKEN (BRACKET LOOSE). MAINTENANCE ADJUSTED AND RE-SECURED EMERGENCY EXIT LIGHT BRACKET AT SEAT 19C.

Part: LINE — MISSING (CABIN) · airframe 59,239 hrs · 25,590 cycles

FLT 460 - IND - EMERGENCY EQUIPMENT - RIGHT OVERWING ESCAPE LIFE LINE MISSING. MAINTENANCE REPLACED MISSING OVERWING LIFE LINE.

Part: SLIDE — UNSERVICEABLE (R1 DOOR) · airframe 59,227 hrs · 25,587 cycles

MCN - BC6 - EES - R-1 DOOR EVACUATION SLIDE PACK RETAINING STRAP BUCKLE BROKEN. REPLACED R-1 DOOR EVACUATION SLIDE PACK IAW A320 AMM 25-62-44.

Part: LANYARD — MISINSTALLED (SLIDE RAFT) · airframe 59,227 hrs · 25,587 cycles

MCN - BC6 - EES - R-2 DOOR SURVIVAL KIT LANYARD CONNECTED TO WRONG END OF GIRT BAR. PROPERLY R-2 DOOR SURVIVAL KIT LANYARD TO GIRT BAR IAW A320 AMM 25-62-44.

Part: LANYARD — MISINSTALLED (SLIDE RAFT) · airframe 59,227 hrs · 25,587 cycles

MCN - BC6 - EES - R-1 DOOR SURVIVAL KIT LANYARD CONNECTED TO WRONG END OF GIRT BAR. PROPERLY R-2 DOOR SURVIVAL KIT LANYARD TO GIRT BAR IAW A320 AMM 25-62-44.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 59,227 hrs · 25,587 cycles

MCN - BC6 - MAJOR REPAIR - CRACK IN AFT CARGO DOOR FORWARD ACTUATOR ATTACH FRAME AT CENTER LUG HOLE AT FR55, S21R. REPAIRED AFT CARGO DOOR FORWARD ACTUATOR ATTACH FRAME AT CENTER LUG HOLE AT FR55, S21R IAW EA 102083 & EO 52-30-14.

Part: SPLICE — DAMAGED (CABIN) · airframe 59,227 hrs · 25,587 cycles

MCN - BC6 - EEL - EMERGENCY EXIT LIGHT INOP AT ROW 9ABC. REPLACED SPLICE UNDER SEAT AT ROW 9 ABC, EMERGENCY LIGHT OPS CHECKS GOOD IAW AIRBUS ESPM 20-43-11 & A320 AMM 33-51-00.

Part: LENS — MISSING (CABIN) · airframe 59,088 hrs · 25,524 cycles

FLT 614 - ATL - EEL - EMERGENCY LIGHT LENS MISSING ON SEAT 9-L. MAINTENANCE INSTALLED LENS ON SEAT 9-L.

Part: ROLL PIN — DEFECTIVE (SLIDE RELEASE) · airframe 58,473 hrs · 25,249 cycles

FLT 488 - SFO - EES - LEFT OVERWING EXIT SLIDE INDICATION IS INOPERATIVE. SLIDES HAVE BEEN DISARMED AND ARE UNUSABLE. MAINTENANCE REPLACED LT AFT OVERWING HATCH SLIDE RELEASE MECHANISM ROLL PIN.

Part: BRACKET — BROKEN (CABIN) · airframe 56,566 hrs · 24,420 cycles

FLT 371 - MKE - EEL - FLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHT ROW 15C BROKEN. MAINTENANCE REPLACED LIGHT BRACKET AS REQUIRED. REFERENCE ILLUSTRATED PARTS CATALOG 33-51-09 & ENGINEERING AUTHORIZATION 114738.

Part: ADIRU — DEFECTIVE (NR 1 & NR 2) · airframe 56,377 hrs · 24,340 cycles

FLT 9205 SEA-PHX - EMERGENCY LANDING - ADIRU 1 & 2 FAULT AT CRUISE RESULTING IN LOSS OF AUTO THRUST, AUTO PILOT AND ALL OF THE FIRST OFFICER'S INSTRUMENTS. CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 1 & NR 2 AIR DATA INERTIAL REFERENCE UNITS.

Part: ADIRU — DEFECTIVE (NR 1 & NR 2) · airframe 56,377 hrs · 24,340 cycles

FLT 9205 SEA-PHX - EMERGENCY LANDING - ADIRU 1 & 2 FAULT AT CRUISE RESULTING IN LOSS OF AUTO THRUST, AUTO PILOT AND ALL OF THE FIRST OFFICER'S INSTRUMENTS. CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 1 & NR 2 AIR DATA INERTIAL REFERENCE UNITS.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 56,288 hrs · 24,299 cycles

FLT 339 - PHX - EEL - THE FLASHLIGHT AT THE DIRECT VIEW JUMPSEAT IS INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT ASSEMBLY.

Part: LENS — MISSING (CABIN) · airframe 55,935 hrs · 24,145 cycles

FLT 005 - LAX-PHX - EMERGENCY LIGHTS - EMERGENCY EXIT LIGHT LENS AT 11C IS MISSING. REPLACED LENS ON EMERGENCY LIGHT SEAT 11C.

Part: LENS — BROKEN (CABIN) · airframe 55,912 hrs · 24,134 cycles

FLT 342 - LAS - EEL - DOOR 2R EMERGENCY EXIT LENS COVER BROKEN. MAINTENANCE REMOVED AND REPLACED THE 2R EMERGENCY EXIT LENS COVER.

Part: LENS — MISSING (CABIN) · airframe 55,912 hrs · 24,134 cycles

FLT 342 - LAS - EEL - EMERGENCY EXIT LENS COVER ROW 11L MISSING. MAINTENANCE REPLACED EMERGENCY EXIT LENS COVER ROW 11L.

Part: COVER — BROKEN (CABIN) · airframe 55,434 hrs · 23,924 cycles

FLT 371 - PHX - EEL - EMERGENCY EXIT LIGHT COVER AT AFT LEFT OVERWING EXIT BY SEAT 11A BROKEN & DETACHED. MAINTENANCE INSTALLED EMERGENCY EXIT LIGHT COVER ROW 11ABC.

Part: LENS — MISSING (CABIN) · airframe 55,352 hrs · 23,887 cycles

FLT 599 - PHX - EEL - RED LENS COVER ON THE EMERGENCY EXIT AT 11C IS MISSING. MAINTENANCE REPLACED LIGHT LENS.

Part: BRACKET — BROKEN (CABIN) · airframe 55,080 hrs · 23,767 cycles

FLT 500 - LAX-PHX - EMERGENCY LIGHTS - 13C EMERGENCY AISLE FLOOR LIGHT BROKEN BRACKET. REPLACED BRACKET AND SEAT MOUNTED EMERGENCY LIGHT AT SEAT 13C. OPERATIONAL CHECK WAS GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 55,020 hrs · 23,734 cycles

FLT 5 - PHX - EEL - EMERGENCY EXIT LIGHT HANGING LOOSE AT ROW 24 A/C LEFT. MAINTENANCE REPLACED EMERGENCY LIGHT ASSEMBLY AT ROW 24 LEFT IAW COMPONENT MAINTENANCE MANUAL 25-26-93.

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 54,941 hrs · 23,700 cycles

FLT 407 PHX-ATL - DIVERSION / BURNING SMELL - DIVERTED INTO MEMPHIS DUE TO STRONG BURNING PLASTIC SMELL IN CABIN THROUGHOUT CLIMB AND INTO CRUISE. MAINTENANCE FOUND EVIDENCE OF BIRD INGESTION IN NR 1 ENGINE ON STAGE 3 HIGH PRESSURE COMPRESSOR. PERFORMED COMPRESSOR WASH IAW AIRBUS MAINTENANCE MANUAL 72-00-00-100-010.

Part: LENS — DAMAGED (EMERGENCY LIGHTS) · airframe 54,574 hrs · 23,543 cycles

FLT 457 - ESCAPE PATH LIGHT AT 17C DAMAGED. REMOVED AND REPLACED 17C ESCAPE PATH LIGHT LENS CAP.

Part: LENS — BROKEN (EMERGENCY LIGHTS) · airframe 54,533 hrs · 23,525 cycles

FLT 9 -YVR-PHX - EMERGENCY LIGHTS - EMERGENCY EXIT LIGHT ROW 9 BROKEN. REMOVED AND REPLACED LENS ON ROW 9 EMERGENCY LIGHT. OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 69,752 hrs · 23,627 cycles

SAL - C5 - EEL - EMERGENCY POWER SUPPLY UNIT DOESN'T PASS TEST. REPLACED EMERGENCY POWER SUPPLY UNIT IAW A320 AMM 33-51-38.

Part: SKIN — DELAMINATED (ELEVATOR) · airframe 54,414 hrs · 23,474 cycles

SAL - C5 - MAJOR REPAIR - DELAMINATION DUE TO TRAPPED WATER IN LEFT ELEVATOR UPPER SKIN SURFACE AT ELEVATOR STATION 4655 TO 5274. REPAIRED LEFT ELEVATOR UPPER SKIN SURFACE AT ELEVATOR STATION 4655 TO 5274 IAW A320 SRM 51-77-13.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 54,414 hrs · 23,474 cycles

SAL - C5 - MAJOR REPAIR - DELAMINATION ON RIGHT ELEVATOR UPPER SURFACE AT ELEVATOR STATION 2707 TO 2973. REPLACED RIGHT ELEVATOR IAW A320 AMM 27-34-41.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 54,414 hrs · 23,474 cycles

SAL - C5 - MAJOR REPAIR - EXCESSIVE PLAY AT NR 4 RUDDER HINGE FITTING. REPLACED NR 4 RUDDER HINGE FITTING IAW A320 SRM 55-36-41.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 54,414 hrs · 23,474 cycles

SAL - C5 - MAJOR REPAIR - EXCESSIVE PLAY AT NR 1 RUDDER HINGE FITTING. REPLACED NR 1 RUDDER HINGE FITTING IAW A320 SRM 55-36-41.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 54,414 hrs · 23,474 cycles

SAL - C5 - MAJOR REPAIR - EXCESSIVE PLAY AT NR 3 RUDDER HINGE FITTING. REPLACED NR 3 RUDDER HINGE FITTING IAW A320 SRM 55-36-41.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 54,414 hrs · 23,474 cycles

SAL - C5 - MAJOR REPAIR - EXCESSIVE PLAY AT NR 2 RUDDER HINGE FITTING. REPLACED NR 2 RUDDER HINGE FITTING IAW A320 SRM 55-36-41.

Part: LENS — MISSING (CABIN) · airframe 54,302 hrs · 23,424 cycles

LOG PAGE 4431319 - FLT 350-LAS - EMERGENCY EQUIPMENT - SEAT ROW 11L MISSING EMERGENCY LIGHT LENS. MAINTENANCE REPLACED LENS AS REQUIRED.

Part: BLADE — SEPARATED (COMPRESSOR) · airframe 54,049 hrs · 23,317 cycles

FLT 500 YYC-PHX - COMPRESSOR STALLS - NR 2 ENGINE EXPERIENCED TWO RAPID COMPRESSOR STALLS CLIMBING THROUGH FL340 IN SMOOTH AIR, VCM. TEMPORARILY LOST POWER. ENGINE QUICKLY SELF RECOVERED. NO LIMITS EXCEEDED. ENGINE CONTINUED NORMAL POWER THEREAFTER. RAN 30-60 DEGREES C HOTTER THAN NR 1 ENGINE FOR ENTIRE FLIGHT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE. VENDOR REPORTED (3) STAGE-5 COMPRESSOR BLADE LOCKS BECAME FREE DAMAGING THE COMPRESSOR.

Part: BLADE — FAILED (COMPRESSOR) · airframe 53,650 hrs · 23,140 cycles

FLT 180 - WHILE CLIMBING THROUGH 23,000 FT THE FLIGHT CREW FELT 6 TO 12 STRONG JOLTS AND RECEIVED ECAM MESSAGES "NUMBER 1 ENGINE FAIL" THEN "NUMBER ONE ENGINE STALL". THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO MCI FOR MAINTENANCE. COMPLIED WITH (DFDR) DIGITAL FLIGHT DATA RECORDER DOWNLOAD PER A6A31301. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE. VENDOR REPORTED STAGE 6 COMPRESSOR BLADE FAILURE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 52,505 hrs · 22,589 cycles

FLT 290 PHX-LAX EMERGENCY EQUIPMENT. FORWARD FLIGHT ATTENDANT FLASHLIGHT WAS NOT CHARGED, WAS NOT STOWED CORRECTLY IN CHARGER. MX R&R THE FORWARD FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT BATTERY. OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (NR 2) · airframe 50,663 hrs · 21,744 cycles

FLT 363 - PHX-SMF - UNSCHEDULED LANDING - CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE COCKPIT JUST AFTER AN ELAC-2 FAULT. CREW WERE UNABLE TO RESET AND SUSPECTED THE BURNING SMELL WAS FROM THE ELAC (ELEVATOR AILERON COMPUTER). THE AIRCRAFT WAS DIVERTED TO LAS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ELEVATOR AILERON COMPUTER. SYSTEM TEST PASSED AND NO ELECTRICAL SMELL NOTED.

Part: POWER SUPPLY — INTERMITTENT (EMERGENCY LIGHTS) · airframe 50,348 hrs · 21,616 cycles

FLT NR 322 - LAS-ORD - EEL - EMERGENCY LIGHTS AT DOORS L2, R2 AND ONE LOCATED IN CEILING BETWEEN AFT LAVS FLICKER ON AND OFF. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY UNIT. OPERATIONAL CHECK WAS NORMAL.

Part: SKIN — CORRODED (ZONE 100) · airframe 49,270 hrs · 21,138 cycles

SAL - MAJOR REPAIR - NR 5979790 - CORROSION ON EXTERNAL FUSELAGE SKIN BETWEEN BS 3310 / FR 69 TO BS 3366 / FR 70 AND S31R TO S32R. REPAIRED FUSELAGE SKIN BETWEEN BS 3310 / FR 69 TO BS 3366 / FR 70 AND S31R TO S32R IAW A320 SRM 53-41-11, PAGE 239-244, FIG 205.

Part: HINGE FITTING — WORN (ZONE 300) · airframe 49,270 hrs · 21,138 cycles

SAL - MAJOR REPAIR - C-04 CHECK - NR 5975509, RUDDER HINGE FITTING NR 3 HAS EXCESSIVE PLAY, VERTICAL STABILIZER STA 2279 / RIB 5. REPLACED RUDDER HINGE FITTING 3, VERTICAL STABILIZER STA 2279 RIB 5 IAW A320 AMM 55-36-41.

Part: HINGE FITTING — WORN (RUDDER) · airframe 49,270 hrs · 21,138 cycles

SAL - MAJOR REPAIR - C-04 CHECK - NR 5975508, RUDDER HINGE FITTING NR 2 HAS EXCESSIVE PLAY, VERTICAL STABILIZER STA 1926 / RIB 4. REPLACED RUDDER HINGE FITTING NR 2, VERTICAL STABILIZER STA 1926 / RIB 4 IAW A320 AMM 55-36-41.

Part: HINGE FITTING — WORN (ZONE 300) · airframe 49,270 hrs · 21,138 cycles

SAL - MAJOR REPAIR - C-04 CHECK - NR 5975507, RUDDER HINGE FITTING NR 4 HAS EXCESSIVE PLAY, VERTICAL STABILIZER STA 2632 RIB 6. REPLACED RUDDER HINGE FITTING NR 4, VERTICAL STABILIZER STA 2632 RIB 6 IAW A320 AMM 55-36-41.

Part: SILL — CORRODED (ZONE 200) · airframe 49,270 hrs · 21,138 cycles

SAL - MAJOR REPAIR - C-04 CHECK - NR 5976234, CORROSION FOUND ON L2 DOOR SILL, BS 3158/FR 66 TO BS 3257/FR 68, S23L. REPAIRED L2 DOOR SILL, BS 3158/FR 66 TO BS 3257/FR 68, S23L IAW A320 SRM 53-41-14.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 49,270 hrs · 21,138 cycles

SAL - MAJOR REPAIR - C-4 CHECK - NR 5975013, CORROSION ON CABIN FLOOR SUPPORT ANGLE (JOINT COVER), BS 657/FR 14, -Y35. REPLACED CABIN FLOOR SUPPORT ANGLE (JOINT COVER), BS 657/FR 14, -Y35 IAW A320 SRM 51-72-11.

Part: SILL — CORRODED (ZONE 200) · airframe 49,270 hrs · 21,138 cycles

SAL - MAJOR REPAIR - C-4 CHECK - NR 5975813, CORROSION ON THE R2 DOOR CUT OUT SHAPE SILL, BS 3158/FR 66 - BS 3257/FR 68, 23R. REPLACED THE R2 DOOR CUT OUT SHAPE SILL, BS 3158/FR 66 - BS 3257/FR 68, 23R IAW A320 SRM 51-72-11.

Part: SKIN — CRACKED (ZONE 300) · airframe 49,270 hrs · 21,138 cycles

SAL - MAJOR REPAIR - C-04 CHECK - NR 5975503, LEFT ELEVATOR LEADING EDGE CRACKED, ELEVATOR RIB STATION 2 - ELEVATOR RIB STATION 3. REPAIRED LEFT ELEVATOR LEADING EDGE ELEVATOR RIB STATION 2 - ELEVATOR RIB STATION 3 IAW A320 SRM 55-21-11.

Part: SILL — CORRODED (ZONE 200) · airframe 49,270 hrs · 21,138 cycles

SAL - MAJOR REPAIR - C-4 CHECK - NR 5976233, CORROSION ON THE R2 DOOR CUTOUT LOWER SILL, BS 2786 / FR 66 - BS 2884 / FR 68. REPAIRED THE R2 DOOR CUTOUT LOWER SILL, BS 2786 / FR 66 - BS 2884 / FR 68 IAW A320 SRM 53-41-14.

Part: FITTING — CORRODED (ZONE 200) · airframe 49,270 hrs · 21,138 cycles

SAL - MAJOR REPAIR - C-4 CHECK - NR 5975761, CORROSION ON R1 DOOR THRESHOLD CENTER FITTING, BS 709/FR 16 - BS 783/FR 19, S23R. REPLACED R1 DOOR THRESHOLD CENTER FITTING, BS 709/FR 16 - BS 783/FR 19, S23R IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (ZONE 200 - FUSEL) · airframe 49,270 hrs · 21,138 cycles

SAL - MAJOR REPAIR - C-4 CHECK - NR 5975709, CORROSION ON CABIN FLOORBEAM, BS 3207/FR 67, -Y1180. REPLACED CABIN FLOORBEAM, BS 3207/FR 67, -Y1180 IAW A320 SRM 51-72-11.

Part: SILL — CORRODED (ZONE 200) · airframe 49,270 hrs · 21,138 cycles

SAL - MAJOR REPAIR - C-04 CHECK - NR 5975814, CORROSION ON THE R2 DOOR CUT OUT LOWER SILL, BS 2786 / FR 66. REPAIRED THE R2 DOOR CUTOUT LOWER SILL, BS 2786 / FR 66 IAW A320 SRM 53-41-14.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 49,270 hrs · 21,138 cycles

SAL - MAJOR REPAIR - C-4 CHECK - NR 5975707, CORROSION ON CABIN FLOORBEAM, BS 3043/FR 64, +Y765. REPLACED CABIN FLOORBEAM, BS 3043/FR 64 - BS 3158/FR 66, +Y765 IAW A320 SRM 51-72-11.

Part: SILL — CORRODED (ZONE 200) · airframe 49,270 hrs · 21,138 cycles

SAL - MAJOR REPAIR - C-4 CHECK - NR 5975817, CORROSION ON THE L2 DOOR CUT OUT SHAPE SILL, BS 3158/FR 66 - BS 3257/FR 68, 23L. REPLACED THE L2 DOOR CUT OUT SHAPE SILL, BS 3158/FR 66 - BS 3257/FR 68, 23L IAW A320 SRM 51-72-11.

Part: FITTING — CORRODED (ZONE 200) · airframe 49,270 hrs · 21,138 cycles

SAL - MAJOR REPAIR - C-4 CHECK - NR 5975764, CORROSION ON L1 DOOR THRESHOLD CENTER FITTING, BS 709/FR 16 - BS 783/FR 19, S23L. REPLACED L1 DOOR THRESHOLD CENTER FITTING, BS 709/FR 16 - BS 783/FR 19, S23L IAW A320 SRM 51-72-11.

Part: DUMMY RAIL — CORRODED (ZONE 200) · airframe 49,270 hrs · 21,138 cycles

SAL - MAJOR REPAIR - C-4 CHECK - NR 5975014, CORROSION ON CABIN DUMMY RAIL, BS 709/FR 16, BS 732/FR 17, BS 808/FR 20, +Y254. REPLACED CABIN DUMMY RAIL, BS 605/FR 12 - BS 950/FR 20, +Y254 IAW A320 SRM 51-72-11.

Part: DAMPER — MALFUNCTIONED (ZONE 800) · airframe 49,270 hrs · 21,138 cycles

SAL - EES - C-04 CHECK - NR 5975045, THE L1 DOOR ASSIST DAMPER CYLINDER DOES NOT FUNCTION PROPERLY. REPLACED AND OPERATIONAL CHECKED THE L1 DOOR ASSIST DAMPER CYLINDER IAW A320 AMM 52-11-14.

Part: DUMMY RAIL — CORRODED (ZONE 200) · airframe 49,270 hrs · 21,138 cycles

SAL - MAJOR REPAIR - C-4 CHECK - CORROSION ON CABIN DUMMY RAIL, BS 709/FR 16, -Y1379.5. REPLACED CABIN DUMMY RAIL, BS 709/FR 16, -Y1379.5 IAW A320 SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 49,270 hrs · 21,138 cycles

SAL - MAJOR REPAIR - C-4 CHECK - NR 5975016, CORROSION ON CABIN FLOORBEAM, BS 808/FR 20, -Y189. REPLACED CABIN FLOORBEAM, BS 808/FR 20 - BS 897/FR 23, -Y189 IAW A320 SRM 51-72-11.

Part: DUMMY RAIL — CORRODED (ZONE 200) · airframe 49,270 hrs · 21,138 cycles

SAL - MAJOR REPAIR - C-04 CHECK - NR 5975012, CORROSION ON CABIN DUMMY RAIL, BS 683/FR 15, -Y81. REPLACED CABIN DUMMY RAIL, BS 683/FR 15, -Y81 IAW A320 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (ZONE 200) · airframe 49,270 hrs · 21,138 cycles

SAL - MAJOR REPAIR - C-4 CHECK - NR 5975702, CORROSION ON CABIN SHEAR PLATE, BS 3257/FR 68 - BS 3310/FR 69, S23L. REPLACED CABIN SHEAR PLATE, BS 3257/FR 68 - BS 3310/FR 69, S23L IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 49,270 hrs · 21,138 cycles

SAL - MAJOR REPAIR - C-4 CHECK - NR 5975579, CORROSION ON CABIN SEAT TRACK, BS 808/FR 20, BS 843/FR 21 AND BS 897/FR 23, -Y765. REPLACED CABIN SEAT TRACK, BS 808/FR 20 - BS 897/FR 23, -Y1292 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 49,270 hrs · 21,138 cycles

SAL - MAJOR REPAIR - C-4 CHECK - NR 5975580, CORROSION ON CABIN SEAT TRACK, BS 808/FR 20, BS 843/FR 21 AND BS 897/FR 23, -Y1292. REPLACED CABIN SEAT TRACK, BS 605/FR 12 - BS 950/FR 24, -Y1292 IAW A320 SRM 51-72-11.

Part: SENSOR — FAILED (RT GENERATOR) · airframe 48,915 hrs · 20,969 cycles

SEA - LAS - EL - LOG 7757269 - AT CRUISE, THE CREW REPORTED THE RT ENGINE GENERATOR HAD DROPPED OFF LINE. THE APU WAS ON MEL. THE CREW DECLARED AN EMERGENCY. THE LANDING WAS UNEVENTFUL. MX REPLACED SENSOR 50XU2 PER MM 24-22-18. OPERATIONAL CHECK WAS GOOD DURING ENGINE RUN-UP. THE A/C WAS RETURNED TO SERVICE.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 47,753 hrs · 20,458 cycles

LAS - EEL - MID LEFT EMERGENCY LIGHT BATTERY FAULT. MX REPLACED THE LEFT MID EMERGENCY LIGHTING BATTERY. OPERATIONAL CHECK WAS GOOD.

Part: LINE — LEAKING (RT MLG) · airframe 45,061 hrs · 19,283 cycles

DURING INITIAL CLIMB RECEIVED A MOMENTARY ECAM MESSAGE FOR THE GREEN HYDRAULIC SYSTEM ON ENGINE NR 1 PUMP LOW PRESSURE LIGHT. AFTER THE LIGHT FLICKERED A FEW TIMES IT CAME ON STEADY AND DISPLAYED A GREEN SYSTEM DEPLETED MESSAGE. MAINTENANCE REPLACED THE RIGHT GEAR DOWNLOCK RETURN LINE DUE TO IT LEAKING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,615 hrs · 19,078 cycles

MCN - DURING C3 CHECK DISCOVERED CORROSION ON SEAT TRACK AT FS 44 TO FS 46+16", LT INBOARD SIDE AT 4 PLACES. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-31-15 FIG 103. MAINTENANCE REMOVED AND INSTALLED NEW LT INBOARD SEAT TRACK FROM FS 41 TO FS 47 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,615 hrs · 19,078 cycles

MCN - DURING C3 CHECK DISCOVERED CORROSION ON THE RT OUTBOARD SEAT TRACK FROM FS 36 TO FS 41. CORROSION WAS REMOVED AND FOUND OUT OF LIMITS IAW A320 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW RT OUTBOARD SEAT TRACK FROM FS 36 TO FS 42 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,615 hrs · 19,078 cycles

MCN - DURING C3 CHECK DISCOVERED CORROSION ON THE LT INBOARD SEAT TRACK FROM FS 36 TO FS 41. CORROSION WAS REMOVED AND FOUND OUT OF LIMITS IAW A320 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW LT INBOARD SEAT TRACK FROM FS 36 TO FS 41 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,615 hrs · 19,078 cycles

MCN - DURING C3 CHECK DISCOVERED CORROSION ON THE RT OUTBOARD SEAT TRACK FROM FS 42 TO FS 46+16". CORROSION WAS REMOVED AND FOUND OUT OF LIMITS IAW A320 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW RT OUTBOARD SEAT TRACK FROM FS 41 TO FS 47 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,615 hrs · 19,078 cycles

MCN - DURING C3 CHECK DISCOVERED CORROSION ON THE LT OUTBOARD SEAT TRACK FROM FS 44 TO FS 46+16". CORROSION WAS REMOVED AND FOUND OUT OF LIMITS IAW A320 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW LT OUTBOARD SEAT TRACK FROM FS 41 TO FS 47 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,615 hrs · 19,078 cycles

MCN - DURING C3 CHECK DISCOVERED CORROSION ON THE LT OUTBOARD SEAT TRACK AT FS 41 TO FS 44. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 103. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK FROM FS 41 TO FS 47 IAW AIRBUS 320 SRM 51-72-11 AND AIRBUS 320 AMM 20-21-11 FIG 203.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,615 hrs · 19,078 cycles

MCN - DURING C3 CHECK DISCOVERED CORROSION ON SEAT TRACK AT FS 41 TO FS 44, LT INBOARD SIDE AT 4 PLACES. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-31-15 FIG 103. MAINTENANCE REMOVED AND INSTALLED NEW LT INBOARD SEAT TRACK FROM FS 41 TO FS 47 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,615 hrs · 19,078 cycles

MCN - DURING C3 CHECK DISCOVERED CORROSION ON SEAT TRACK AT FS 44 TO FS 46+16", RT INBOARD SIDE AT 4 PLACES. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-31-15 FIG 103. MAINTENANCE REMOVED AND INSTALLED NEW RT INBOARD SEAT TRACK FROM FS 41 TO FS 47 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,615 hrs · 19,078 cycles

MCN - DURING C3 CHECK DISCOVERED CORROSION ON THE LT OUTBOARD SEAT TRACK FROM FS 36 TO FS 41. CORROSION WAS REMOVED AND FOUND OUT OF LIMITS IAW A320 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW LT OUTBOARD SEAT TRACK FROM FS 36 TO FS 41 IAW A320 SRM 51-72-11.

Part: NONE — NONE · airframe 44,134 hrs · 18,880 cycles

DURING FLIGHT CREW REPORTED, FWD CARGO DOOR OPEN ECAM MESSAGE. CREW RETURNED TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE PLACED THE FORWARD CARGO DOOR INDICATION ON DEFERRAL. DEFERRAL WAS CLEARED ON 03/12/06, PILOT REPORTED THAT AT PUSHBACK RAMPERS PUSHED CARGO DOOR HANDLE ALL THE WAY IN AND UNLOCK INDICATION WENT TO LOCKED. PILOT REPORTED NO OPEN INDICATION AFTER HANDLE WAS STOWED CORRECTLY. OPERATIONALLY CHECKED GOOD ON GROUND AND THERE WAS NO HISTORY IN THE PAST 90 DAYS. DEFERRAL WAS CLEARED.

Part: BATTERY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 24,626 hrs · 9,392 cycles

PHX - EEL - DURING OVERNIGHT MAINTENANCE THE EMERGENCY LIGHT SYSTEM TEST "OK" LIGHT WOULD NOT ILLUMINATE AND RECEIVED MESSAGES "COMM EMER R" AND "BATTERY EMER R". MAINTENANCE REMOVED AND REPLACED THE RT OVERWING EMERGENCY POWER SUPPLY BATTERY. OPERATIONAL CHECKS WERE GOOD.

Part: POWER SUPPLY — FAILED (LT AFT) · airframe 43,112 hrs · 18,457 cycles

OVERNIGHT MAINTENANCE DISCOVERED EMERGENCY LIGHT TEST FAILING, FAULT (115 VAC AFT L) PRESENT. MAINTENANCE REMOVED AND REPLACED THE LT AFT POWER SUPPLY IAW MM 33-51-38-04. VENDOR CONFIRMED FAULT. UNIT WAS REPAIRED AND TESTED IAW CMM 33-51-09 REV.2

Part: LANDING GEAR — MALFUNCTIONED (MAINS)

AFTER TAKEOFF MLG HANDLE UP, ECAM CAUTION: L/G GEAR NOT UPLOCKED. CYCLED MLG PER ECAM ALL GEAR UP & LOCKED OK. MX CYCLED MLG, OPS CHK GOOD. ACFT RETURNED TO SERVICE. WITHIN 8 CYCLES DISCREPANCY RETURNED. ACFT MX FERRIED BACK TO PHX. SEVERAL SENSORS INSPECTED, ADJUSTED & REPLACED IAW AIRBUS MM. NLG RESTRICTORS 2535GM, 2536GM & 2691GM REPLACED. MLG SELECTOR VALVE 40GA CHANGED, NLG DOOR BYPASS VALVE REPLACED. R & R RELAYS 48GA AND 53GA. TEAR DOWN REPORT CONFIRMS REPLACEMENT OF MLGCU. FOUND S1 SWITCH FAULTY. SWITCH REPLACED & UNIT TESTED OK. ALL WORK PERFORMED IAW CMM 32-31-13 REV 9.

Part: MODULE — FAILED (LANDING GEAR) · airframe 41,749 hrs · 17,876 cycles

AFTER TAKEOFF, TRIED TO RAISE MLG, GEAR UNLOCKED ILLUMINATED FOR NLG. CYCLED GEAR PER ECAM, GEAR CAME UP & LOCKED. LANDED IN SEA WITHOUT FURTHER INCIDENT. A/C FERRIED BACK TO PHX. MX R & R MLG CONTROL MODULE IAW AIRBUS MM 32-30-00. TEAR DOWN REPORT CONFIRMS FAILURE. DURING PRE-TEST "DOWN-UP SWITCHING BY S1" TEST FAILED. SEVERAL CONTACTS OVER VOLTAGE DROPS STATED IN CMM. UNIT REPAIRED & RETESTED IAW CMM 32-31-13. OPS TESTS GOOD.

Part: COMPRESSOR — DIRTY (NR 1 ENGINE) · airframe 41,686 hrs · 17,852 cycles

ODOR DETECTED. DURING FLIGHT, PACKS CREATING GYM SOCK ODOR WITH PASSENGERS COMPLAINING. MAINTENANCE OPERATED PACKS WITH APU BLEED AIR AND ENGINE BLEED AIR. DISCOVERED ODOR COMING FROM NR 1 ENGINE BLEED AIR SOURCE, ABOVE IDLE. INSPECTED NR 1 ENG AND UNABLE TO FIND OIL LEAK. FOUND BLACK SUBSTANCE PRESENT AT STAGE 3 HPC. SUSPECT VSV LUBRICANT. PERFORMED COMPRESSOR WASH OF NR 1 ENG IAW AMERICA WEST AIRLINES (AWA) TASK CARD S5M72303. ALSO, REPLACED NR 1 AND NR 2 OZONE FILTERS DUE TO CONTAMINATION FROM NR 1 ENG BLEED AIR, IAW AWA TASK CARD S2C21301. OPERATIONAL CHECKS GOOD, NO ODOR PRESENT WHEN PACKS RUNNING OFF OF NR 1 ENG BLEED AIR SOURCE.

Part: UPLOCK — MALFUNCTIONED (NLG)

DURING GEAR RETRACTION AFTER TAKEOFF, NOSE GEAR STAYED DOWN & ALL GEAR DOORS STAYED DOWN. MX R & R THE NLG DOOR UPLOCK ASSY IAW AWXA TASK CARD F4N32301. OPS CHECKS GOOD. TEAR DOWN REPORT CONFIRMS REASON FOR REMOVAL OF NLG DOOR UPLOCK ASSEMBLY. FOUND BINDING BETWEEN STOPS ON UNIT. BOTH STOPS WERE FOUND WORN. STOPS WERE REPLACED AND UNIT WAS TESTED IAW CMM 32-37-09 REV. 7

Part: ACTUATOR — FAULTY (UPLOCK) · airframe 41,349 hrs · 17,705 cycles

DURING CLIMB SELECTING GEAR UP & NLG FAILED TO RETRACT & RECEIVED A RED UNLOCK LIGHT. SELECTED GEAR DOWN & GEAR FAILED TO EXTEND (MAINS, NOSE SHOWED GREEN/RED UNLK.) SELECTED GEAR UP & GEAR RETRACTED WITH NORMAL INDICATIONS. SELECTED GEAR DOWN WITH NORMAL EXTENSION & INDICATIONS. MX R & R LGCIU NR 1 & 2 AS A PRECAUTIONARY MEASURE IAW AMM. OPS CK GOOD. MX ADDITIONALLY R & R NLG PROX SENSORS 19GA, 24GA, 25GA, 30GA, & 31GA PER AMM & R & R NLG DOWNLOCK SENSOR 18GA IAW MM. OPS CK GOOD. MX R & R NLG UPLOCK ACTUATOR 2530GM IAW AWA TASKCARD NR R4N32307 OPS & FUNCTIONAL CKS GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 39,904 hrs · 17,103 cycles

PHX - EEL - FLIGHT CREW REPORTED THE RT CENTER EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 39,579 hrs · 16,982 cycles

SAL - MAJOR REPAIR - DURING C-02 CHECK A 16 INCH CRACK WAS FOUND IN CABIN FLOOR PANEL 251RF BETWEEN FR 58 AND FR 62. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 251RF IAW A320 SRM 53-02-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,579 hrs · 16,982 cycles

SAL - MAJOR REPAIR - DURING C-02 CHECK CORROSION WAS FOUND ON SEAT TRACK -Y765 AT FR 20. MAINTENANCE REMOVED CORRODED SEAT TRACK -Y765 FROM FR 20 TO FR 24; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 53-00-15 FIG 202.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 39,579 hrs · 16,982 cycles

SAL - MAJOR REPAIR - DURING C-02 CHECK, CABIN FLOOR PANEL 241EF WAS FOUND DELAMINATED BETWEEN FS 30 AND FS 42. MAINTENANCE PERFORMED BOND REPAIR ON FLOOR PANEL 241EF IAW A320 SRM 53-02-00, FIG 201 AND 202.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 39,579 hrs · 16,982 cycles

SAL - MAJOR REPAIR - DURING C-02 CHECK A 16 INCH CRACK WAS FOUND IN CABIN FLOOR PANEL 231QF BETWEEN FR 28 AND FR 32. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 231QF IAW A320 SRM 53-02-00.

Part: FLOOR PANEL — TORN (FUSLEAGE) · airframe 39,579 hrs · 16,982 cycles

SAL - MAJOR REPAIR - DURING C-02 CHECK FOUND AFT CARGO COMPARTMENT ALUMINUM FLOOR PANEL PLATE TORN BETWEEN FR 49 AND FR 50. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT FLOOR PANEL PLATE; FABRICATED A NEW REPLACEMENT PLATE FROM 2024T3.071; AND INSTALLED REPAIR PART IAW EO 5326-01007.

Part: FAIRING — CRACKED (NR 1 PYLON) · airframe 34,925 hrs · 15,139 cycles

MCN - MINOR REPAIR - DURING C-01 CHECK A 8.5 INCH CRACK WAS FOUND AT THE AFT END OF THE NR 1 PYLON INBOARD UPPER FAIRING WELDED ASSEMBLY, NAC STA 5369-6077, BETWEEN RIBS 7 & 8. MAINTENANCE REMOVED AND REPLACED WELDED ASSEMBLY INBOARD SIDE OF NR 1 PYLON IAW AMM SUBTASK 54-57-22-020-050-0A2.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 34,925 hrs · 15,139 cycles

MCN - EMERGENCY EQUIPMENT - DURING C-01 CHECK ALL 4 EMERGENCY FLASHLIGHTS UNDER FLIGHT ATTENDANTS SEATS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED ALL 4 EMERGENCY FLASHLIGHT BATTERY PACKS, OPERATIONAL CHECKS WERE GOOD.

Part: TERMINAL — BROKEN (SEAT ROW 26) · airframe 33,724 hrs · 14,646 cycles

FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT WAS INOPERATIVE. MAINTENANCE REPAIRED WALL PLUG CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT SEAT ROW 26 LT, OPERATIONAL CHECK WAS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,946 hrs · 14,359 cycles

DURING INSPECTION THE LEFT FORWARD EMERGENCY LIGHT POWER PACK FAILED TEST. MAINTENANCE REMOVED AND REPLACED THE LEFT FORWARD EMERGENCY POWER SUPPLY UNIT BATTERY PACK, OPERATIONAL TEST WAS GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 32,097 hrs · 14,030 cycles

PHX - EEL - DURING TEST OF EMERGENCY LIGHTING SYSTEM THE TEST FAILED. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (12WL) IAW AMM 33-51-38, OPERATIONAL CHECK WAS GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,407 hrs · 13,376 cycles

MAJOR REPAIR - DURING C-8 CHECK CORROSION WAS FOUND ON OUTBOARD UPPER LIP OF SEAT TRACK NR2, 2 INCH AFT OF FR 20, Y 765. MAINTENANCE REMOVED CORROSION AND CUTOUT DAMAGED SECTION OF SEAT TRACK, FABRICATED A REPAIR DOUBLER AND PLUG, AND INSTALLED REPAIR PARTS.

Part: DAMPER — FAILED (R1 DOOR) · airframe 30,407 hrs · 13,376 cycles

YWG - EMERGENCY EVACUATION - DURING C-08 CHECK THE R1 DOOR DAMPER WOULD NOT SNUB. MAINTENANCE REMOVED AND REPLACED THE R1 DOOR DAMPER IAW AMM 52-11-14-401, PRESSURE CHECKED IAW AMM 52-11-14-210-056.

Part: DAMPER — FAILED (L1 DOOR) · airframe 30,407 hrs · 13,376 cycles

YWG - EMERGENCY EVACUATION - DURING C-08 CHECK THE L1 DOOR DAMPER WOULD NOT SNUB. MAINTENANCE REMOVED AND REPLACED THE L1 DOOR DAMPER IAW AMM 52-11-14-401, PRESSURE CHECKED IAW AMM 52-11-14-210-056.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,407 hrs · 13,376 cycles

YWG - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON NUTPLATES AND FLOOR SUPPORT AT Y254L, BETWEEN FR 20 AND FR 21. MAINTENANCE REMOVED FLOOR SUPPORT BETWEEN FR 12 TO FR 24. FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-72-11, PG. 1 & 2.

Part: RIB — CRACKED (LT WING) · airframe 30,407 hrs · 13,376 cycles

YWG - MAJOR REPAIR - DURING C-08 CHECK A CRACK WAS FOUND ON LT WING GEAR SUPPORT RIB 5, HOLE NR 82. MAINTENANCE OVERSIZED HOLE TO AND INSTALLED NEW FASTENER IAW AWA ER 26-5721-02093-TB2.

Part: SILL — CORRODED (FUSELAGE) · airframe 30,407 hrs · 13,376 cycles

YWG - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON THE R2 DOOR SILL AT FR 68. MAINTENANCE FABRICATED AND INSTALLED REPAIR IAW SRM.

Part: SILL — CORRODED (FUSELAGE) · airframe 30,407 hrs · 13,376 cycles

YWG - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON THE L2 DOOR SILL AT FR 68. MAINTENANCE FABRICATED AND INSTALLED REPAIR IAW SRM.

Part: PLATE — CRACKED (FUSELAGE) · airframe 30,407 hrs · 13,376 cycles

YWG - MAJOR REPAIR - DURING C-08 CHECK A 2 INCH CRACK WAS FOUND ON THE LT AFT L2 DOOR SHEAR PLATE. MAINTENANCE REMOVED SHEAR PLATE, FABRICATED A NEW SHEAR PLATE AND INSTALLED REPAIR IAW SRM 51-42-11 PG 1 AND SRM 51-72-11 PG 1 & 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,407 hrs · 13,376 cycles

YWG - MAJOR REPAIR - DURING C-8 CHECK CORROSION WAS FOUND IN 7 PLACES ON FLOOR SUPPORT RAIL AT Y254, FR 16 TO FR 20, INCLUDING THE SPLICE REPAIR. MAINTENANCE FABRICATED AND INSTALLED REPAIR IAW SRM 51-72-11 PG 1 & 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,407 hrs · 13,376 cycles

YWG - MAJOR REPAIR - DURING C-8 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BEAM AT Y1292 RT, FR 68 TO FR 69. MAINTENANCE FABRICATED AND INSTALLED REPAIR IAW SRM 51-42-11 PG 1, PARA 5.

Part: PLATE — CRACKED (FUSELAGE) · airframe 30,407 hrs · 13,376 cycles

YWG - MAJOR REPAIR - DURING C-08 CHECK A 6 INCH CRACK WAS FOUND ON THE RT AFT SIDE OF THE R2 DOOR SHEAR PLATE. MAINTENANCE REMOVED SHEAR PLATE, FABRICATED A NEW SHEAR PLATE AND INSTALLED REPAIR IAW SRM 51-42-11 PG 1, SRM 51-72-11 PG 1 & 2.

Part: FLANGE — CRACKED (HORIZ STAB) · airframe 30,407 hrs · 13,376 cycles

YWG - MAJOR REPAIR - DURING C-08 CHECK A CRACK WAS FOUND ON THE RT HORIZONTAL STABILIZER L/E 3 FROM OUTBOARD END ON LOWER L/E PANEL MATING SURFACE. MAINTENANCE REMOVED DAMAGED AREA AT STAB STA 6009, RIB 14, FABRICATED AND INSTALLED REPAIR PARTS IAW AWA ER 26-5513-02095-ES4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,407 hrs · 13,376 cycles

YWG - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON RECESSED NUT HOLE OF SEAT RAIL AT FR 64, Y765. MAINTENANCE REMOVED SEAT RAIL AT FR 64, Y765 RT, FABRICATED A NEW SEAT RAIL, AND INSTALLED REPAIR IAW SRM 51-72-11 PG 1 & 2 AND SRM 51-42-11 PG 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,407 hrs · 13,376 cycles

YWG - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND AT RECESSED NUT HOLES ON SEAT RAIL Y1292 RT, FR 64 TO FR 66. MAINTENANCE REMOVED SEAT RAIL Y1292 RT BETWEEN FR 64 AND FR 66, FABRICATED A NEW SEAT RAIL AND INSTALLED REPAIR IAW SRM 51-72-11 PG 1 & 2, AND SRM 51-42-11, PG 1.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 30,332 hrs · 13,349 cycles

PHX - EEL - C - FLIGHT ATTENDANT PANEL INDICATED EMERGENCY LIGHT POWER SUPPLY FAULT LT FWD (10WL). MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY 10WL IAW AMM 33-51-38-000-001, OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 30,280 hrs · 13,327 cycles

SAN - EEL - "C" - RT OVERWING EXIT SIGN 42WL INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY UNIT 12WL AT ZONE 242 IAW AMM 33-51-38-000-001, OPERATIONAL CHECK WAS GOOD.

Part: HANDLE — MISALIGNED (CARGO DOOR) · airframe 27,923 hrs · 12,399 cycles

C1 DOOR UPPER LOCKING SHAFT AFT SUPPORT FITTING BORE FOUND IN MISALIGNMENT TO SHAFT. REPAIRED IAW AWA ER 26-5231-01087-5-S51.

Part: ENGINE — VIBRATION (NR 2) · airframe 24,333 hrs · 10,963 cycles

NR 2 ENGINE VIBRATION WAS 5.3 ON T/O. PERFORMED FAN TRIM BALANCE IAW CARD F5M71303 AND GROUND CARD F5M71306. VIBRATION LEVELS LESS THAN 1 UNIT. CURRENT HISTORY: A/C HAD VIBRATION 2.6-2.9 MILS ON 14 MAR 00 WITHIN LIMITS. RECOMMENDATION: MONITOR.

Part: BRACKET — BROKEN (LT MLG)

EMERGENCY LANDING, ON SHORT FINAL GOT ECAM MSG INDICATING DOOR PROXIMITY. NOSE AND RT MLG INDICATED GREEN, LT MLG INDICATED RED. FOUND LT MLG DOWNLOCK TARGET AND BRACKET MISSING. INSTALLED TARGET AND BRACKET PER AAM 32-31-73 401. ADJUSTED PER AMM 32-31-73.

Part: OIL SYS — LEAKING (APU)

UPON ACCEPTING A/C IN LAS, SMELLED THE DIRTY SOCK SMELL FAIRLY STRONG. CLEANED AND REMOVED RESIDUAL OIL FROM APU INLET, SMELL CLEARED. APU OPS CK GOOD. SUSPECT SLOW EXTERNAL OIL SEEP CAUSING APU INLET.

Part: APU — DIRTY (APU)

STRONG ODOR IN CABIN WHILE RUNNING PACK ON APU. WASHED APU PER CARD Z6D49301 MEL CLEARED.

Part: OIL COOLER — CRACKED (NR 1 ENGINE)

NR 1 ENGINE OIL PRESSURE DROPPED AFTER TAKEOFF. ENGINE WAS SHUTDOWN, OIL QUANTITY DROPPED TO ZERO. LEAK FOUND AT LOWER SECTION OF NR 1 ENGINE AIR/OIL COOLER. REPLACED AIR/OIL COOLER AND SERVICED OIL TANK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT AT 17 C INOP. REPAIRED BROKEN WIRE AT WALL DISCONNECT. REMOVED CAP REPLACED POWER SUPPLY, OPS CHECK GOOD.

Part: PROX SENSOR — INOPERATIVE (NLG)

ON GEAR RETRACTION, NOSE GEAR UNLOCKED LIGHTS REMAINED ON AND NOISE INDICATED THAT NOSE GEAR DID NOT RETRACT. CYCLED GEAR SWITCH AND GEAR RETRACTED OK. REMOVED AND REPLACED NLG DOOR OPEN PROXIMITY SENSORS ON LEFT DOOR, BITE TEST GOOD.

Part: UPLOCK ASSY — INOPERATIVE (LT MLG)

AFTER TAKEOFF WHEN LANDING GEAR RETRACTED, RECEIVED ECAM MESSAGE THAT LEFT MAIN GEAR DOOR WAS NOT CLOSED. CYCLED LANDING GEAR. FLIGHT DIVERTED TO CMH. REMOVED AND REPLACED LEFT DOOR UPLOCK ASSEMBLY. OPS CHECK GOOD.

Part: PROX SENSOR — MALFUNCTIONED (LT MLG)

AFTER TAKEOFF, LEFT MAIN GEAR DOOR DID NOT INDICATE CLOSED WHEN GEAR HANDLE WAS SELECTED UP (CLASS 1 ECAM, LEVEL 2). CYCLED GEAR PER ECAM AND DOOR CLOSED. FOUND LGCIU NR 1 ON ECAM. SWAPPED LGCIU NR 1 S/N 209 WITH LGCIU NR 2 S/N 230. CFDS BITE CHECKS GOOD ON BOTH LGCIUS. REMOVED AND REPLACED PROX SENSOR 9GA AND 11GA ON LT GEAR UPLOCK ACTUATOR.

Part: PROX SENSOR — INOPERATIVE (NLG)

ON APPROACH, RECEIVED A CLASS 1 LEVEL 3 RED WARNING THAT LANDING GEAR WAS NOT SAFE. ONE RED AND ONE GREEN NOSE GEAR INDICATION ON ECAM. RECYCLED LANDING GEAR, NO HELP. LOST NOSE WHEEL STEERING ON ROLLOUT. EMERGENCY WAS DECLARED. REPLACED NLG PROX SENSOR 19GA, CHECKS OK REM MM 32-31-73, PG 430. ALSO, CLEANED NLG CONNECTOR 6GA AND OP CHECKED BSCUS REF MM 32-46-00, PG 502. REMOVED AND RETURNED 3 GEAR PINS TO COCKPIT.

Part: SPOILER ACTUATOR — MALFUNCTIONED (NR 3 SPOILER)

PHX - FLT 2050 - ON LANDING, LOST BLUE HYDRAULIC SYSTEM. NR 3 SPOILER FAULTED UP. BLUE RESERVOIR LOW LEVEL. REMOVED AND REPLACED NR 3 SPOILER ACTUATOR. OPS CHECK NORMAL. PART TOTAL CYCLES 5060. (X)