N672AW

Part: DAMPER — LOW PRESSURE (L1 DOOR) · airframe 45,927 hrs · 16,821 cycles

L1 DOOR DAMPER INDICATES BELOW THE LIMIT. SERVICED THE DOOR DAMPER IAW AMM 52-40-00.

Part: GASKET — LEAKING (RT SPOILER) · airframe 45,896 hrs · 16,810 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED A LOSS OF GREEN HYDRAULIC SYSTEM PRESSURE AND DIVERTED TO ORD WHERE THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT SPOILER SERVO VALVE GASKET SEAL PER AMM 27-64-51.

Part: PROXIMITY SENSOR — FAULTY (MLG) · airframe 45,780 hrs · 16,757 cycles

AFTER TAKEOFF, NOSE GEAR DID NOT RETRACT, ECAM LANDING GEAR NOT UPLATCHED AND LANDING GEAR DOORS NOT CLOSED. AFTER ONE MINUTE THE GEAR RETRACTED AND ECAM CLEARED. AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND FAULTING PROXIMITY SENSOR (24GA) AND REPLACED SENSOR PER AMM 32-31-73.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 45,489 hrs · 16,630 cycles

MISSING LENS COVER ON FLOOR EMERGENCY LIGHT AT SEAT 13C. REPLACED LENS COVER.

Part: COVER — DAMAGED (R2 DOOR) · airframe 45,481 hrs · 16,626 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY EXIT COVER LIGHT DAMAGED AT DOOR 2R. REPLACED DOOR 2R EXIT LIGHT ASSEMBLY PER AMM 33-51-13 AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 44,614 hrs · 16,221 cycles

EMERGENCY LIGHT LENS MISSING AT SEAT ROW 9 LEFT. INSTALLED A NEW LENS.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 43,727 hrs · 15,860 cycles

AIRCRAFT WAS NOT GNDED. L1 DOOR ASSIST BOTTLE LOW PSI. SERVICED L1 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001.

Part: SHADE — INOPERATIVE (CABIN) · airframe 43,504 hrs · 15,771 cycles

AIRCRAFT WAS NOT GNDED. ROW 1 ACFT LT EMER EXIT ROW WINDOW SHADE INOPERATIVE. REPLACED WINDOW SHADE & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 25-23-47.

Part: LIGHT — BROKEN (CABIN) · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. BROKEN EMER EXIT LIGHT DOOR FRAME, LT SIDE AT AFT GALLEY AREA, ONE EACH. REPLACED EMER EXIT LIGHT IAW AMM 33-51-13-0401.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. RT BOX BEAM FLANGE 1.3" FWD OF FRAME 43 & -Y1650 HAS CRACK INDICATION. REPAIRED IAW EO 5315Y066.

Part: PLATE — CRACKED (FUSELAGE) · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT WAS IN BASE MX. CRACK INDICATION ON PRESS PLATE OF BOX BEAM FLANGE 1.300" FWD OF FRAME 43 AT Y-1650. REPAIRED FLANGE IAW SRM 51-72-11.

Part: HINGE FITTING — WORN (RT WING) · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT WAS IN BASE MX. RT WING SPOILER NR 2 HINGE CTR FITTING HAS AN AREA OF WEAR. REPAIRED FITTING IAW SRM 57-70-00 PARAGRAPH 4C FIG 201 SHEET 2.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. CABIN FLOOR PANEL 251RF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. CABIN FLOOR PANEL 241CF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. CABIN FLOOR PANEL 231KF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT WAS IN BASE MX. LT WING FUEL ACCESS PANEL 540KB HAS CORRODED COUNTERSINKS. R & R ACCESS PANEL IAW SRM 51-72-11.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT WAS IN BASE MX. LT ELEVATOR UPPER SKIN HAS 3 AREAS OF TRAPPED WATER FROM STATIONS 3416 - 4035, BETWEEN RIBS 9 & 10. REPAIRED SKIN IAW SRM 55-21-11-201-2.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. LT SIDE BOX BEAM FLANGE HAS CRACK INDICATION AT 2.5" FWD OF FRAME 43 & +Y1650. REPAIRED IAW EO 5315Y066.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. LT SIDE BOX BEAM FLANGE HAS CRACK INDICATION AT 1.3" FWD OF FRAME 43 & +Y1650. REPAIRED IAW EO 5315Y066.

Part: ACCESS DOOR — CORRODED (ZONE 800) · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. CORROSION ON ACCESS DOOR 312AR, INTERNAL STRUCTURE. REPLACED ACCESS DOOR IAW SRM 51-72-11.

Part: BOLT — CORRODED (LE SLAT) · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT WAS IN BASE MX. CORROSION ON RT WING SLAT TRACK 3 ECCENTRIC BOLT. R & R BOLT IAW AMM 27-84-63-400-001-A.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. CORROSION ON WEB, BETWEEN FRAME 69 & 70, AT STRINGER 23R. REPLACED WEB IAW SRM 51-72-11.

Part: HINGE PIN — CORRODED (LT AILERON) · corrosion level 2 · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. CORROSION ON LT WING AILERON HINGE NR 2 PIN. REPLACED HINGE PIN IAW AMM 27-14-41.

Part: HINGE PIN — CORRODED (LT AILERON) · corrosion level 2 · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. CORROSION IN LT WING AILERON NR 1 HINGE PIN. REPLACED HINGE PIN IAW AMM 27-14-41.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. CORROSION ON R1 DOOR CUT OUT LOWER SILL, BETWEEN FRAME 16 & 20 AT STRINGER 23R. REPLACED SILL IAW SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. CORROSION ON SEAT TRACK, BETWEEN FRAME 12 & 24 AT +Y765. REPLACED SEAT TRACK IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. CORROSION ON FLOORBEAM, BETWEEN FRAME 67 + 15" & 69 AT +Y1162. REPLACED FLOORBEAM IAW SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT WAS IN BASE MX. CABIN FLOOR SHEAR PLATE IS CORRODED, BETWEEN FRAME 69 & 70 AT S23L. R & R SHEAR PLATE IAW SRM 51-72-11 & DWG D53474180.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. CORROSION ON WEB AT FRAME 16 & STRINGER 23L. REPLACED WEB IAW SRM 51-72-11.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. CORROSION ON DUMMY RAIL BEAM, BETWEEN FRAME 12 & 16 AT +Y503.2. REPLACED DUMMY RAIL BEAM IAW SRM 51-72-11.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. CORROSION ON R2 DOOR CUT OUT LOWER SILL, BETWEEN FRAME 66 & 68 AT STRINGER 23R. REPLACED SILL IAW SRM 51-72-11.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. CORROSION ON L2 DOOR CUT OUT LOWER SILL, BETWEEN FRAME 66 & 68 AT STRINGER 23L. REPLACED SILL IAW SRM 51-72-11.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. CORROSION ON L1 DOOR CUT OUT LOWER SILL, BETWEEN FRAME 16 & 20 AT STRINGER 23L. REPLACED SILL IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. AFT GALLEY FLOOR PANEL 261PF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. CORROSION ON FLOORBEAM, BETWEEN FRAME 66 + 5" & 667 + 15" AT -Y1225. REPLACED FLOORBEAM IAW SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. CORROSION ON SHEAR PLATE, BETWEEN FRAME 69 & 70, AT STRINGER 23R. REPLACED SHEAR PLATE IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. AFT CARGO FLOOR PANEL 152BF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. FWD CARGO FLOOR PANEL 132JF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. AFT CARGO FLOOR PANEL 151BF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. FWD CARGO FLOOR PANEL 131AF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. AFT CARGO FLOOR PANEL 151RF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. FWD CARGO FLOOR PANEL 132KF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. AFT CARGO FLOOR PANEL 152EF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. FWD CARGO FLOOR PANEL 151LF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. FWD CARGO COMPARTMENT, FLOOR PANEL 131EF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,787 hrs · 15,480 cycles

AIRCRAFT IN BASE MX. FWD CARGO FLOOR PANEL 131HF DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.

Part: DOOR — WORN (NLG) · airframe 41,375 hrs · 14,872 cycles

AIRCRAFT HAS NOTICEABLE AIRFRAME VIBRATION INFLIGHT AT CRUISE. HIGHEST ENG VIBRATION WAS 0.8 N1 ON NR 1 ENG, ALL OTHERS 0.0. REPLACED THE NLG LT AFT DOOR IAW AMM 32-22-13-400-001A. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: SERVO — FAULTY (NLG STEERING) · airframe 40,927 hrs · 14,701 cycles

EMERGENCY LANDING, NOSE WHEEL STEERING FAULT OCCURRED AT CRUISE. UPON GEAR EXTENSION THE FAULT CLEARED & NO INCIDENTS WERE REPORTED UPON LANDING. REPLACED THE NOSE WHEEL STEERING SERVO 6GC. ACCOMPLISHED A LEAK OPERATIONAL CHECK WITH NO DEFECTS NOTED IAW AMM 32-51-51.

Part: PRESSURE SWITCH — LEAKING (APU GEN) · airframe 40,575 hrs · 14,564 cycles

NOTICED A DIRTY SOCK SMELL IN COCKPIT & AFT CABIN, TAKEOFF POWER & CLIMB. FLIGHT ATTENDANTS NOTICED IT FOR LAST 5 MIN OF FLIGHT IN ENTIRE CABIN. INSPECTED ACFT IAW 26L00021001 & 26L00021003. NO EXTERNAL LEAKAGE SOURCES NOTED FROM ENGS OR EXTERNAL FUSELAGE AREAS. FOUND APU GEN DIFF PRESSURE SWITCH LEAKING ONTO INLET PLENUM. RESEALED IAW 49-91-14-400-001. CLEANED AREAS & LEAK CHECKED. COMPLETED DECONTAMINATION CARD 26L00021004. NO UNUSUAL ODORS NOTED AFTER COMPLETION..

Part: SHADE — INOPERATIVE (CABIN) · airframe 40,185 hrs · 14,421 cycles

EXIT ROW 11A WINDOW SHADE IS INOPERATIVE. REPLACED WINDOW SHADE AT ROW 11A IAW AMM 25-23-43-000-002A.

Part: SLIDE — UNSERVICEABLE (ZONE 800) · airframe 39,389 hrs · 14,130 cycles

RON VISIT DURING A SCHEDULED PARTS CHANGE OF THE R1 DOOR SLIDE, FOUND REPLACEMENT SLIDE FROM STOCK HAD BROKEN SAFETY WIRE ON RELEASE. ORDERED & REPLACED WITH NEW SLIDE.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 39,043 hrs · 14,002 cycles

ENGINE NR 2 COMP STALL. 1ST STALL AT 600FT AGL, ENG QUICKLY RECOVERED ENG STALLED 2ND TIME AT 2500FT WHILE CLIMBING, ALSO RECOVERED QUICKLY. ENG WAS AT TOGA THRUST FOR THE 1ST COMP STALL, WAS AT CLIMB THRUST WHEN 2ND COMP STALL OCCURRED. ENG FAILED BORESCOPE. REPLACED NR 2 ENG IAW JOB CARD 26L40071004. OPERATION & LEAK CHECKED IAW JOB CARD 26L00071015 REF LOG PAGE 8694301.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 38,041 hrs · 13,632 cycles

FORWARD FLIGHT ATTENDANT STATION EMER FLASHLIGHT SHOWING NOT CHARGED. REPLACED FWD EMER FLASHLIGHT BATTERY.

Part: SHADE — DEFECTIVE (CABIN) · airframe 37,496 hrs · 13,423 cycles

WINDOW SHADE AT EMERGENCY EXIT ROW 10A WILL NOT RETRACT. REPLACED WINDOW SHADE AT EMERGENCY EXIT ROW 10A.

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 36,054 hrs · 12,932 cycles

CREW REPORTED THE CAPTAIN'S WINDSHIELD IS ARCING. R & R CAPTAIN'S WINDSHIELD IAW AMM 56-11-11-400-001-A. R & R WINDOW HEAT COMPUTER NR 1 IAW AMM 30-42-34 PB401. OPERATIONS CHECKED GOOD IAW AMM 30-42-00-710-001A.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 35,578 hrs · 12,765 cycles

EMERGENCY EXIT LIGHT LENS MISSING AT SEATS 3C,24C. REPLACED MISSING LIGHT LENS.

Part: SLIDE — UNSERVICEABLE (DOOR) · airframe 33,112 hrs · 11,954 cycles

UNABLE TO READ PRESSURE GAUGE AT FORWARD LEFT DOOR SLIDE. REPLACED FORWARD LEFT DOOR SLIDE PER JOB CARD 26L00025010.

Part: LENS — MISSING (CABIN) · airframe 32,428 hrs · 11,719 cycles

EMERGENCY EXIT SEAT ROW 9R FLOOR LEVEL RED LENS IS MISSING. INSTALLED NEW RED LENS AT SEAT ROW 9R AS REQUIRED.

Part: LENS — MISSING (CABIN) · airframe 32,428 hrs · 11,719 cycles

ROW 11A EMERGENCY EXIT ROW LIGHT COVER MISSING. REPLACED MISSING EMERGENCY LIGHT LENS COVER ROW 11A.

Part: LENS — MISSING (CABIN) · airframe 31,793 hrs · 11,482 cycles

EMERGENCY FLOOR LIGHTING MISSING AT 26C. REPLACED LENS.

Part: LENS — MISSING (CABIN) · airframe 30,025 hrs · 10,916 cycles

EMERGENCY LIGHT LENS MISSING AT L2 DOOR. INSTALLED LENS AT L2 DOOR.

Part: LENS — LOOSE (CABIN) · airframe 28,212 hrs · 10,299 cycles

EMERGENCY LIGHT COVER AT L-1 DOOR COMING LOOSE. SECURED L-1 DOOR COVER.

Part: LENS — MISSING (CABIN) · airframe 28,192 hrs · 10,292 cycles

EMERGENCY EXIT LIGHT ROW 9 LEFT MISSING LENS. INSTALLED LENS ON EMERGENCY EXIT LIGHT ROW 9 LEFT.

Part: LENS — MISSING (CABIN) · airframe 28,171 hrs · 10,285 cycles

FORWARD GALLEY LEFT BULKHEAD WALL EMERGENCY LIGHT LENS MISSING. INSTALLED MISSING LENS AS REQUIRED.

Part: LENS — MISSING (CABIN) · airframe 27,687 hrs · 10,124 cycles

OVERWING EMERGENCY EXIT ROW 11 RIGHT IS MISSING LOWER EXIT LIGHT LENS. MAINTENANCE INSTALLED EMERGENCY EXIT LIGHT LENS AT ROW 11 RIGHT AS REQUIRED.

Part: SLIDE — DEFECTIVE (L1 DOOR) · airframe 27,380 hrs · 10,029 cycles

DOOR SLIDE PACK ON L1 DOOR SHIFTED AND COVERING SLIDE PACK PRESSURE GAUGE MAKING SLIDE PRESSURE UNREADABLE. MAINTENANCE REMOVED AND REPLACED L1 DOOR ESCAPE SLIDE.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 25,771 hrs · 9,465 cycles

FLT 454 - PHX - EE - AFT MEGAPHONE WIIL NOT TEST. MAINTENANCE REMOVED & REPLACED AFT MEGAPHONE.

Part: SIGN — DEFECTIVE (CABIN) · airframe 23,884 hrs · 8,764 cycles

FLT 373 - DFW - EEL - OVERWING EMERGENCY EXIT LIGHTS A/C LEFT, RIGHT & CEILING INOPERATIVE. AIRCRAFT WAS MAINTENANCE FERRIED TO PHX FOR REPAIR. FOUND LIGHT ASSEMBLY 53WL TO BE SHORTED AND TAKING OUT POWER SUPPLY UNITS 11WL & 12WL. REPLACED EMERGENCY EXIT SIGN 53WL ALONG WITH EMERGENCY POWER SUPPLY UNITS 11WL & 12WL (2X) IAW AIRBUS MAINTENANCE MANUAL 33-51-38.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 23,884 hrs · 8,764 cycles

FLT 373 - DFW - EEL - OVERWING EMERGENCY EXIT LIGHTS A/C LEFT, RIGHT & CEILING INOPERATIVE. AIRCRAFT WAS MAINTENANCE FERRIED TO PHX FOR REPAIR. FOUND LIGHT ASSEMBLY 53WL TO BE SHORTED AND TAKING OUT POWER SUPPLY UNITS 11WL & 12WL. REPLACED EMERGENCY EXIT SIGN 53WL ALONG WITH EMERGENCY POWER SUPPLY UNITS 11WL & 12WL (2X) IAW AIRBUS MAINTENANCE MANUAL 33-51-38.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 23,884 hrs · 8,764 cycles

FLT 373 - DFW - EEL - OVERWING EMERGENCY EXIT LIGHTS A/C LEFT, RIGHT & CEILING INOPERATIVE. AIRCRAFT WAS MAINTENANCE FERRIED TO PHX FOR REPAIR. FOUND LIGHT ASSEMBLY 53WL TO BE SHORTED AND TAKING OUT POWER SUPPLY UNITS 11WL & 12WL. REPLACED EMERGENCY EXIT SIGN 53WL ALONG WITH EMERGENCY POWER SUPPLY UNITS 11WL & 12WL (2X) IAW AIRBUS MAINTENANCE MANUAL 33-51-38.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 23,884 hrs · 8,764 cycles

FLT 373 - DFW - EEL - OVERWING EMERGENCY EXIT LIGHTS A/C LEFT, RIGHT & CEILING INOPERATIVE. AIRCRAFT WAS MAINTENANCE FERRIED TO PHX FOR REPAIR. FOUND LIGHT ASSEMBLY 53WL TO BE SHORTED AND TAKING OUT POWER SUPPLY UNITS 11WL & 12WL. REPLACED EMERGENCY EXIT SIGN 53WL ALONG WITH EMERGENCY POWER SUPPLY UNITS 11WL & 12WL (2X) IAW AIRBUS MAINTENANCE MANUAL 33-51-38.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 23,884 hrs · 8,764 cycles

FLT 378 - CLT - OVERWING EMERGENCY EXIT LIGHTS A/C LEFT INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY 11WL IAW AIRBUS MAINTENANCE MANUAL 33-51-38.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 23,859 hrs · 8,758 cycles

FLT 70 - PHL - EEL - EMERGENCY EXIT LIGHT OVERWING A/C LEFT NOT ILLUMINATED. MAINTENANCE REPLACED THE POWER SUPPLY.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,721 hrs · 8,718 cycles

FLT 82 - PHX-SEA - EMERGENCY LIGHTS - OVERWING CEILING AND AIRCRAFT LEFT EMERGENCY EXIT SIGNS LIGHT ARE OUT. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (EPSU) AND BATTERY PER AMM 33-51-38, OPERATIONAL CHECK WAS GOOD.

Part: EPSU — INOPERATIVE (CABIN) · airframe 23,721 hrs · 8,718 cycles

FLT 82 - PHL-SEA - EMERGENCY LIGHTS - RIGHT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38. OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 23,398 hrs · 8,628 cycles

FLT 78 - PHL - EEL - FLIGHT ATTENDANT REPORTED EN ROUTE THAT EMERGENCY EXIT LIGHTS AT MID CABIN AND A/C LEFT OVERWING WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY UNIT AND BATTERY.

Part: RELEASE MECH — OUT OF ADJUST (L2 DOOR) · airframe 22,860 hrs · 8,450 cycles

FLT 77 - PHX - EES - L2 DOOR DOES NOT STAY ARMED ON ECAM DOOR PAGE. ON GROUND, DOOR ARMING HANDLE SITS IN RECESS NORM, BUT IN FLIGHT L2 SLIDE HANDLE MOVES OUT OF RECESS AND SLIDE DISARMS. MAINTENANCE ADJUSTED L2 DOOR EMERGENCY ESCAPE SLIDE RELEASE MECHANISM PER TASK 52-13-15-700-802-A01.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 22,848 hrs · 8,447 cycles

SAL - S1 - MAJOR REPAIR - CORROSION ON FLOOR PANEL 222FF BETWEEN FR16 TO FR20 & BETWEEN -Y1292 TO -Y765. REPLACED FLOOR PANEL 222FF IAW JOB CARD 26C2265002.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 22,848 hrs · 8,447 cycles

SAL - S1 - MAJOR REPAIR - CORROSION ON FLOOR PANEL 221FF BETWEEN FR16 TO FR20 & BETWEEN Y1292 TO Y765. REPLACED FLOOR PANEL 221FF IAW JOB CARD 26C22053002.

Part: STRIKER — OUT OF ADJUST (R1 DOOR) · airframe 22,848 hrs · 8,442 cycles

SAL - S1 - EES - R-1 DOOR DIMENSION "A" BETWEEN FINGER & STRIKER LEVER IS OUT OF ADJUSTMENT. PERFORMED ADJUSTMENT OF DIMENSION "A" BETWEEN FINGER & STRIKER LEVER AT L-1 DOOR IAW A320 AMM 52-11-14-820-002.

Part: WEB — CRACKED (FUSELAGE) · airframe 22,848 hrs · 8,447 cycles

SAL - S1 - MAJOR REPAIR - CRACK ON LATERAL WEB BETWEEN FR68 TO FR69, S23R. REPLACED LATERAL WEB BETWEEN FR68 TO FR69, S23R IAW AIRBUS DRAWING D53480020.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 22,848 hrs · 8,447 cycles

SAL - S1 - MAJOR REPAIR - CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23R. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23R IAW EA 132949.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,848 hrs · 8,447 cycles

SAL - S1 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM SUPPORT BETWEEN FR12 TO FR24, Y254. REPLACED FLOORBEAM SUPPORT BETWEEN FR12 TO FR24, Y254 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,848 hrs · 8,447 cycles

SAL - S1 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, Y1292. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112812.

Part: SILL — CORRODED (FUSELAGE) · airframe 22,848 hrs · 8,447 cycles

SAL - S1 - MAJOR REPAIR - CORROSION ON LOWER SILL AREA OF L-2 DOOR AT FR66, S23L, Y1732. REPAIRED LOWER SILL AREA OF L-2 DOOR AT FR66, S23L, Y1732 IAW AIRBUS A320 SRM 53-41-14.

Part: SILL — CORRODED (FUSELAGE) · airframe 22,848 hrs · 8,447 cycles

SAL - S1 - MAJOR REPAIR - CORROSION ON LOWER SILL AREA OF AFT SERVICE DOOR AT FR68, S23R. REPAIRED LOWER SILL AREA OF AFT SERVICE DOOR AT FR68, S23R IAW EA 132923.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,844 hrs · 8,447 cycles

SAL - S1 - MAJOR REPAIR - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, -Y259. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, -Y259 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,848 hrs · 8,447 cycles

SAL - S1 - MAJOR REPAIR - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, -Y1292. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, -Y1292 IAW A320 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 22,848 hrs · 8,447 cycles

SAL - S1 - MAJOR REPAIR - CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23L. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23L IAW EA 132949.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,848 hrs · 8,447 cycles

SAL - S1 - MAJOR REPAIR - CORROSION ON FLOORBEAM AT FR68, Y1292. REPLACED FLOORBEAM AT FR68, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING 53472000.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,848 hrs · 8,447 cycles

SAL - S1 - MAJOR REPAIR - CORROSION ON FLOORBEAM AT FR68, -Y1292. REPLACED FLOORBEAM AT FR68, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING 53472000.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,898 hrs · 8,447 cycles

SAL - S1 - MAJOR REPAIR - CORROSION ON FLOORBEAM BETWEEN FR66 + 10 INCHES TO FR67, Y1292. REPLACED FLOORBEAM BETWEEN FR66 + 10 INCHES TO FR67, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D5347217220400.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,848 hrs · 8,447 cycles

SAL - S1 - MAJOR REPAIR - CORROSION ON FLOORBEAM BETWEEN FR66 + 10 INCHES TO FR67 + 8 INCHES, -Y1292. REPLACED FLOORBEAM BETWEEN FR66 + 10 INCHES TO FR67 + 8 INCHES, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING 53472000.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,840 hrs · 8,445 cycles

FLT 9205 - CLT-PHX - EMERGENCY LIGHTS - ROW 4A EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-19. OPERATIONAL CHECK WAS GOOD.

Part: O-RING — LEAKING (APU) · airframe 22,508 hrs · 8,321 cycles

FLT 117 - PHX - CABIN ODOR - STRONG ACRID DIRTY SOCK SMELL PERMEATING ENTIRE AIRCRAFT. SMELL ON GROUND IS LESS STRONG WITH PACK 2 TURNED OFF. MAINTENANCE FOUND LEAK AT APU TURBINE BEARING CAVITY VENT AND LUBE. REPLACED O-RINGS & GASKET IAW AIRBUS MAINTENANCE MANUAL 49-91-53.

Part: GASKET — LEAKING (APU) · airframe 22,508 hrs · 8,321 cycles

FLT 117 - PHX - CABIN ODOR - STRONG ACRID DIRTY SOCK SMELL PERMEATING ENTIRE AIRCRAFT. SMELL ON GROUND IS LESS STRONG WITH PACK 2 TURNED OFF. MAINTENANCE FOUND LEAK AT APU TURBINE BEARING CAVITY VENT AND LUBE. REPLACED O-RINGS AND GASKET IAW AIRBUS MAINTENANCE MANUAL 49-91-53.

Part: LENS — BROKEN (CABIN) · airframe 22,432 hrs · 8,290 cycles

FLT 578 - RNO - EEL - FORWARD EMERGENCY EXIT LENS COVER BY DOOR 1L IS DETACHED WITH A BROKEN TAB. MAINTENANCE INSTALLED NEW LENS COVER AT FORWARD ENTRY DOOR EMERGENCY LIGHT.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 21,329 hrs · 7,880 cycles

FLT 81 - PHX - EEL - AFT LEFT INBOARD FLASHLIGHT NOT FLASHING. MAINTENANCE REPLACED AFT LEFT FLASHLIGHT BATTERY.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 20,785 hrs · 7,672 cycles

FLT 232 - PHX - EEL - EMERGENCY EXIT LIGHT AT ROW 9 LEFT INOPERATIVE. MAINTENANCE REPLACED THE SEAT HARNESS AT ROW 9 LEFT. OPERATIONAL CHECK WAS GOOD.

Part: OIL COOLER — LEAKING (APU) · airframe 20,031 hrs · 7,415 cycles

EWR - FUMES - PILOT REPORTED MIST AND FOUL SMELL OR FUMES FROM APU OR AIR PACKS. DETECTED LEAK AT APU OIL COOLER. REMOVED & REPLACED OIL COOLER.

Part: SEAL — BROKEN (FLASHLIGHT) · airframe 19,723 hrs · 7,312 cycles

LOG PAGE 4395168 - FLT 614-ATL - EMERGENCY EQUIPMENT - EMERGENCY FLASHLIGHT SEAL BROKEN AT CENTER FLIGHT ATTENDANT SEAT. MAINTENANCE REPLACED EMERGENCY FLASHLIGHT SEAL AT CENTER FLIGHT ATTENDANT SEAT AS REQUIRED.

Part: SEAL — BROKEN (FLASHLIGHT) · airframe 19,723 hrs · 7,312 cycles

LOG PAGE 4395167 - FLT 614-ATL - EMERGENCY EQUIPMENT - EMERGENCY FLASHLIGHT SEAL BROKEN AT AFT LEFT FLIGHT ATTENDANT SEAT. MAINTENANCE REPLACED SEAL ON EMERGENCY FLASHLIGHT AT AFT LEFT FLIGHT ATTENDANT SEAT AS REQUIRED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 18,235 hrs · 6,793 cycles

LOGPAGE: 8316389 - FLT 323 - GDL-PHX - EEL - AFT GALLEY FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED AFT GALLEY FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 18,199 hrs · 6,781 cycles

LOGPAGE: 8316380 - FLT 672 - PHL-PHX - EEL - EMERGENCY FLASHLIGHT ON AIRCRAFT AFT LEFT INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY ON AIRCRAFT AFT LEFT. OPERATIONAL CHECK WAS GOOD.

Part: TRANSFORMER — DEFECTIVE (NR 2) · airframe 15,363 hrs · 5,800 cycles

FLT NR 188 - TPA-PHX - EMERGENCY LANDING, AIRCRAFT EXPERIENCED A DC BUS 2 FAULT. AFTER ONE RESET, THE FAULT REOCCURRED. DUE TO SLOW SLATS AND FLAPS, THE LOSS OF ONE REVERSER AND THE AUTOBRAKE SYSTEM, CREW DECLARED AN EMERGENCY ON APPROACH TO PHX RUNWAY 08. A NORMAL LANDING WAS REPORTED. MAINTENANCE REMOVED AND REPLACED CONTACTOR 3PX, RELAY 6XX, DIODE 2420 VD, NO HELP. REPLACED THE NR 2 TRANSFORMER RECTIFIER AND OPERATIONAL CHECK WAS GOOD.

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 11,243 hrs · 4,270 cycles

SAL - FOUND CORROSION ON L2 DOOR WAY FLOOR PANEL 261 FF, FR 66 - FR 68, +Y1550. REPLACED L2 DOOR WAY FLOOR PANEL 261 FF, FR 66 - FR 68, +Y1550 IAW AWA TASK CARD C1C53303.

Part: CIRCUIT BREAKER — TRIPPED · airframe 57,063 hrs · 25,545 cycles

LAS - AT FL 350, SEC 2 FAULTED, THEN SEC 3, C/B BD POPPED CAUSING NUMEROUS FAULTS. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO DEN. THE LANDING WAS UNEVENTFUL AND THE A/C TAXIED TO THE GATE. MX FOUND C/B BD ON THE 124VU TRIPPED, MX RESET AND RAN ENG NR 2, LOADED ENG NR 2 GEN FOR SEVERAL MINUTES. NO FAULTS NOTED. MX INSPECTED C/B BD 6PP, DC SERVICE FOUND IN GOOD CONDITION. NO FAULTS, T/S PER ASM 24-61-00 AND AWM 24-61-02. THE A/C WAS RETURNED TO SERVICE. AS A PRECAUTIONARY MEASURE, MX GENERATED A FUP TO REPLACE C/B'S 7PN AND 3PN2.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 10,477 hrs · 3,970 cycles

LOG NR 3949667 - EMERGENCY TEST ON CIDS FAILS IAW T/C I8M05333. MX REMOVED AND REPLACED EPSU AND BATTERY ON AFT LT CABIN IAW A1C3302 OPS CHECK WAS GOOD.

Part: RELAY — FAULTY (ZONE 120) · airframe 873 hrs · 319 cycles

ABORTED TAKEOFF AT BEGINNING OF TAKEOFF ENROUTE FOR LAS WHILE MOVING THRUST LEVERS FORWARD RECEIVED ECAM MESSAGE (HYDRAULIC YELLOW SYSTEM LOW PRESSURE; BRAKE ACCUMULATOR PRESSURE MONITOR), REJECTED TAKEOFF AT 50 KTS. MAINTENANCE PREFORMED GROUND SCAN AUTOMATIC FLIGHT SYSTEM AND OPERATIONAL TEST OF YELLOW HYDRAULIC SYSTEM, FOUND YELLOW SYSTEM ELECTRIC HYDRAULIC PUMP IN CONTINUOUS OPERATION AND POWER TRANSFER UNIT WITH AMBER INDICATION ON ECAM. REMOVED AND REPLACED RELAYS 3816GX AND 6MJ IAW TASK 29-13-00-810-816, OPERATIONAL CHECK WAS GOOD. PART NAME (6MJ); RELAY, MFG; AIRBUS, P/N; E0218UUU010A, LOC; ZONE 120