N627AW

Part: FCU — FAILED (APU) · airframe 74,601 hrs · 33,526 cycles

STRONG SMELL OF FUEL IN AIRCRAFT PHX TOWER REPORTED FIRE ON APU EXHAUST. APU FIRE BOTTLE DISCHARGED. REMOVED AND REPLACED FUEL CONTROL UNIT (FCU) DUE TO INTERNAL FAILURE. ALSO REPLACED APU FIRE BOTTLE. RAN APU AND OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 73,445 hrs · 32,963 cycles

AFT FLIGHT ATTENDANT SEAT FLASHLIGHT INOP. REMOVED AND REPLACED AFT F/A FLASHLIGHT.

Part: LENS — MISSING (CABIN) · airframe 73,218 hrs · 32,850 cycles

DOOR 2L RED COVER MISSING. REPLACED 2L RED COVER LENS.

Part: SEAL — BROKEN (CABIN) · airframe 73,096 hrs · 32,790 cycles

AFT FIRE EXTINGUISHER SEAL BROKEN. REPLACED H2O FIRE BOTTLE AS REQUIRED.

Part: BATTERY PACK — OUT OF ADJUST (MEGAPHONE) · airframe 73,047 hrs · 32,762 cycles

FORWARD MEGAPHONE WILL NOT TEST. MAINTENANCE ADJUSTED BATTERY PACK - OPERATIONAL CHECK GOOD.

Part: LENS — BROKEN (CABIN) · airframe 73,013 hrs · 32,743 cycles

ROW 9 AIRCRAFT LEFT EMERGENCY LIGHT LENS COVER BROKEN. REMOVED AND REPLACED LENS COVER AT ROW 9.

Part: LENS — MISSING (ZONE 200) · airframe 72,364 hrs · 32,410 cycles

ROW 11 RT SIDE EMERGENCY LIGHT LENS COVER MISSING. REPLACED ROW 11 RT EMERGENCY LIGHT LENS.

Part: EXTINGUISHER — UNSERVICEABLE (AFT GALLEY) · airframe 72,221 hrs · 32,339 cycles

H2O FIRE EXTINGUISHER IN AFT GALLEY IS MISSING THE SECURITY SEAL. REMOVED AND REPLACED AFT GALLEY FIRE EXTINGUISHER WITH SERVICEABLE UNIT.

Part: CHECK VALVE — FAILED (YELLOW SYS) · airframe 71,928 hrs · 32,210 cycles

FLIGHT 660 EN ROUTE FROM PHX TO SNA EXPERIENCED A YELLOW SYSTEM HYDRAULIC FAILURE. AIRCRAFT RETURNED TO PHX, LANDED WITHOUT INCIDENT AND TAXIED TO GATE UNDER ITS OWN POWER. MAINTENANCE REPLACED A CRACKED CHECK VALVE 3093GM IAW AIRBUS MAINTENANCE MANUAL 29-13-00.

Part: LENS — MISSING (CABIN) · airframe 71,827 hrs · 32,164 cycles

SEAT MOUNTED EMERGENCY PATHWAY LIGHT LENS IS MISSING AT 26L. INSTALLED LENS AT 26L FOR SEAT MOUNTED EMERGENCY PATHWAY LIGHT.

Part: BEARING — CORRODED (RT PYLON) · airframe 70,416 hrs · 31,535 cycles

S4 CHECK - CORROSION ON RIGHT PYLON SPIGOT BEARING BETWEEN PYLON RIB 7 & 8. REPLACED RIGHT PYLON SPIGOT BEARING IAW JOB CARD 26C40054035.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 70,404 hrs · 31,529 cycles

S4 CHECK - CORROSION ON SEAT TRACK RAIL AT FR20, -Y1292. REPLACED SEAT TRACK RAIL AT FR20, -Y1292 IAW A320 SRM 53-00-15 FIG 101, 51-42-11 & 51-75-12.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 69,902 hrs · 31,296 cycles

FLT 409 - SFO-PHX - EMERGENCY EQUIPMENT - AFT FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY AT AFT FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT. OPERATIONAL CHECK WAS GOOD.

Part: APU — LEAKING (APU BAY) · airframe 69,681 hrs · 31,196 cycles

FLT 504 SAN-PHX - FUMES/CABIN ODOR - FLIGHT ATTENDANTS REPORTED A DIRTY SOCK SMELL DURING CLIMB AND DESCENT THROUGHOUT THE AIRCRAFT, BUT NO SMELL WAS NOTED IN THE COCKPIT. MAINTENANCE FOUND THE APU LEAKING OIL AT THE CASE SPLIT LINE FORWARD OF THE APU INTAKE. REMOVED AND REPLACED APU.

Part: COMPRESSOR BLADE — DAMAGED (NR 2 ENGINE) · airframe 69,593 hrs · 31,160 cycles

FLT 51 - PHX - RTO - ON TAKEOFF ROLL AT ABOUT 110 KNOTS, CREW REPORTED A LOUD BANG AND THE AIRCRAFT VEERED SHARPLY TO THE RIGHT - TAKEOFF WAS REJECTED. PASSENGERS REPORTED SEEING FLAMES COMING OUT OF THE RIGHT ENGINE. MAINTENANCE FOUND NR 2 ENGINE HIGH PRESSURE COMPRESSOR STAGE 6 HAS BLADES WITH MISSING MATERIAL AND TEARS. REPLACED NR 2 ENGINE.

Part: STRAP — OUT OF POSITION (EVAC SLIDE) · airframe 69,416 hrs · 31,082 cycles

FLT 94 - PHX - EES - STRAP HANGING OUT OF BOTTOM OF THE 2R DOOR SLIDE. MAINTENANCE RE-ROUTED STRAP ON BOTTOM OF SLIDE IAW AIRBUS MAINTENANCE MANUAL 25-62-44.

Part: BATTERY — DISCHARGED (MEGAPHONE) · airframe 68,123 hrs · 30,498 cycles

FLT 271-LAS - EMERG EQUIP - FIRST CLASS FLIGHT ATTENDANT MEGAPHONE BATTERIES REQUIRE REPLACEMENT. MAINTENANCE REMOVED AND REPLACED FIRST CLASS MEGAPHONE BATTERIES.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 67,702 hrs · 30,308 cycles

FLT 196 - ATL-PHX - EMERGENCY LIGHTS - CABIN OVERHEAD EMERGENCY LIGHTS INTERMITTENTLY INOPERATIVE. REMOVED AND REPLACED FORWARD EMERGENCY POWER SUPPLY UNIT & BATTERY IAW AMM 33-51-38-400-001 & 33-51-38-400-002. OPERATIONAL CHECK WAS GOOD.

Part: SLIDE — DEFECTIVE (R1 DOOR) · airframe 67,586 hrs · 30,257 cycles

FLT 355 - LAS - EES - R1 DOOR SLIDE FAILED EMERGENCY LIGHT TEST. MAINTENANCE REMOVED AND REPLACED THE R1 DOOR SLIDE.

Part: ENGINE — LEAKING (APU) · airframe 67,123 hrs · 30,059 cycles

FLT 544 PDX-PHX - CABIN ODOR - CABIN HAS VERY BAD DIRTY SOCK SMELL COMING FROM PACKS, FIRST ON TAKEOFF, THEN AGAIN ON DESCENT INTO PHX. SMELL IS WORSE WITH THE ENGINE HP VALVES OPEN. APU WAS DETERMINED TO BE THE SOURCE. MAINTENANCE REMOVED AND REPLACED THE APU. VENDOR REPORT INDICATES WHITE STREAK RESIDUE FOUND IN BLEED DUCT, POSSIBLY FROM ON-WING WASH - OIL FILM RESIDUE FOUND IN INLET PLENUM DOES FLUORESCE LIKE APU OIL - SUSPECT FOREIGN OBJECT INGESTION.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 65,840 hrs · 29,502 cycles

NR 6161717- INOPERATIVE ESPU IN FWD GALLEY AREA, LT SIDE. REPLACED ESPU IN FWD GALLEY AREA. LT SIDE IAW AMM 33-51-38. OPS TEST GOOD. (K)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 65,840 hrs · 29,502 cycles

MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SHEAR TIE AT FR33 BETWEEN S40L TO S41L. REPLACED SHEAR TIE AT FR 33 BETWEEN S40L TO S41L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231212.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 65,840 hrs · 29,502 cycles

MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SUPPORT FRAME BETWEEN FR69 TO FR70. REPLACED SUPPORT FRAME BETWEEN FR69 TO FR70 IAW A320 SRM 51-72-11 & DRAWING D53470100.

Part: RIB — CRACKED (RT PYLON) · airframe 65,840 hrs · 29,502 cycles

SAL - BC7 - MAJOR REPAIR - CRACK ON RIB 12 OF AFT FIXED FAIRING OF RIGHT PYLON ENGINE NR 2. REPLACED RIB 12 OF AFT FIXED FAIRING OF RIGHT PYLON ENGINE NR 2 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D54510054.

Part: WEB — CORRODED (FUSELAGE) · airframe 65,840 hrs · 29,502 cycles

SAL - BC7 - MAJOR REPAIR - CORROSION ON WEB BETWEEN FR51 TO FR52, S38R. REPLACED WEB BETWEEN FR51 TO FR52, S38R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D5340320.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 65,840 hrs · 29,502 cycles

SAL - BC7 - MAJOR REPAIR - CORROSION ON SUPPORT ANGLE BETWEEN FR56 TO FR57, S43L. REPLACED SUPPORT ANGLE BETWEEN FR56 TO FR57, S43L IAW A320 SRM 51-72-11.

Part: BOLT — CORRODED (SLAT TRACK) · airframe 65,840 hrs · 29,502 cycles

SAL - BC7 - MAJOR REPAIR - CORROSION ON BOLT OF SLAT TRACK NR 8 FROM SLAT NR 3 RIGHT WING. REPLACED BOLT OF SLAT TRACK NR 8 FROM SLAT NR 3 RIGHT WING IAW A320 AMM 27-84-65.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 65,840 hrs · 29,502 cycles

SAL - BC7 - MAJOR REPAIR - CRACK IN ANGLE SEGMENT BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO 4 OF AFT RIGHT EMERGENCY EXIT HATCH. REPLACED ANGLE SEGMENT BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO 4 OF AFT RIGHT EMERGENCY EXIT HATCH IAW A320 SRM 51-72-11 & AIRBUS DRAWING D52279010.

Part: BOLT — CORRODED (SLAT TRACK) · airframe 65,840 hrs · 29,502 cycles

SAL - BC7 - MAJOR REPAIR - CORROSION ON BOLT OF SLAT TRACK NR 7 FROM SLAT NR 3 RIGHT WING (BOLT NR 1). REPLACED BOLT OF SLAT TRACK NR 7 FROM SLAT NR 3 RIGHT WING (BOLT NR 1) IAW A320 AMM 27-84-65.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 65,840 hrs · 29,502 cycles

SAL - BC7 - MAJOR REPAIR - CRACK IN ANGLE SEGMENT BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO 4 OF AFT LEFT EMERGENCY EXIT HATCH. REPLACED ANGLE SEGMENT BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO 4 OF AFT LEFT EMERGENCY EXIT HATCH IAW A320 SRM 51-72-11 & AIRBUS DRAWING D52279010.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 65,840 hrs · 29,502 cycles

SAL - BC7 - MAJOR REPAIR - CRACK IN ANGLE SEGMENT BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO 3 OF FORWARD RIGHT EMERGENCY EXIT HATCH. REPLACED ANGLE SEGMENT BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO 3 OF FORWARD RIGHT EMERGENCY EXIT HATCH IAW A320 SRM 51-72-11 & AIRBUS DRAWING D52279020.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 65,840 hrs · 29,502 cycles

SAL - BC7 - MAJOR REPAIR - CRACK IN ANGLE SEGMENT BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO 4 OF FORWARD RIGHT OVERWING EXIT HATCH. REPLACED ANGLE SEGMENT BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO 4 OF FORWARD RIGHT OVERWING EXIT HATCH IAW A320 SRM 51-72-11 & AIRBUS DRAWING D52279010.

Part: BOLT — CORRODED (SLAT TRACK) · airframe 65,840 hrs · 29,502 cycles

SAL - BC7 - MAJOR REPAIR - CORROSION ON BOLT OF SLAT TRACK NR 7 FROM SLAT NR 3 RIGHT WING (BOLT NR 2). REPLACED BOLT OF SLAT TRACK NR 7 FROM SLAT NR 3 RIGHT WING (BOLT NR 2) IAW A320 AMM 27-84-65.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 65,840 hrs · 29,502 cycles

SAL - BC7 - MAJOR REPAIR - CRACK IN ANGLE SEGMENT BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO 4 OF AFT RIGHT EMERGENCY EXIT HATCH. REPLACED ANGLE SEGMENT BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO 4 OF AFT RIGHT EMERGENCY EXIT HATCH IAW A320 SRM 51-72-11 & AIRBUS DRAWING D52279010.

Part: BOLT — CORRODED (SLAT TRACK) · airframe 65,840 hrs · 29,502 cycles

SAL - BC7 - MAJOR REPAIR - CORROSION ON BOLTS (4 EA) OF SLAT TRACK NR 6 FROM SLAT NR 2 RIGHT WING. REPLACED BOLTS (4 EA) OF SLAT TRACK NR 6 FROM SLAT NR 2 RIGHT WING IAW A320 AMM 27-84-64.

Part: FITTING — CORRODED (FUSELAGE) · airframe 65,840 hrs · 29,502 cycles

SAL - BC7 - MAJOR REPAIR - CORROSION ON SHEAR PLATE ASSEMBLY BETWEEN FR 50 TO FR 51, S38R. REPLACED WEB BETWEEN FR 50 TO FR 51, S38R IAW A320 SRM 51-72-11.

Part: WEB — CORRODED (ZONE 100)

MAJOR REPAIR- NR 6154487 - CORROSION ON WEB BETWEEN FR20 TO FR21, Y1584. REPLACED WEB BETWEEN FR20 TO 21, Y1584 IAW SRM 51-72-11. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 65,840 hrs · 29,502 cycles

SAL - BC7 - MAJOR REPAIR - CORROSION ON CABIN FLOOR SUPPORT BETWEEN FR20 TO FR21, -Y1584. REPLACED WEB BETWEEN FR 20 TO FR 21, -Y1584 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112088.

Part: FITTING — CORRODED (FUSELAGE) · airframe 65,840 hrs · 29,502 cycles

SAL - BC7 - MAJOR REPAIR - CORROSION ON SHEAR PLATE ASSEMBLY BETWEEN FR 52 TO FR 53, S38L. REPLACED WEB BETWEEN FR 52 TO FR 53, S38L IAW A320 SRM 51-72-11.

Part: BOLT — CORRODED (SLAT TRACK) · airframe 65,840 hrs · 29,502 cycles

SAL - BC7 - MAJOR REPAIR - CORROSION ON BOLT OF SLAT TRACK NR 2 FROM SLAT NR 1 RIGHT WING. REPLACED BOLT OF SLAT TRACK NR 2 FROM SLAT NR 1 RIGHT WING IAW A320 AMM 27-84-63.

Part: SKIN — CORRODED (ZONE 100)

MAJOR REPAIR - NR 6156114- CORROSION ON INTERNAL FUSELAGE SKIN AT FR65 BETWEEN S44R TO S43R. REPAIRED INTERNAL FUSELAGE SKIN AT FR 65 BETWEEN S44R TO S43R IAW SRM 53-41-11. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,840 hrs · 29,502 cycles

SAL - BC7 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON CABIN FLOORBEAM BETWEEN FR 68 TO FR 69, -Y1292. REPLACED CABIN FLOORBEAM BETWEEN FR 68 TO FR 69, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2

MAJOR REPAIR - NR 6154385 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR 64 +4 INCHES. Y1292. REPLACED FLOORBEAM BETWEEN FR 64 + 4 INCHES TO FR 67 + 16 INCHES, Y1292 IAW A320 SRM 51-72-11 & DWG D53472000. (K)

Part: FLOOR PANEL — CORRODED (ZONE 200)

MAJOR REPAIR - NR 6161703 - CORROSION ON FLOOR PANEL 222FF BETWEEN FR16 TO FR20 & BETWEEN - Y1752 TO Y1292. REPLACED FLOOR PANEL 222FF BETWEEN FR16 TO FR20 & BETWEEN Y1752 TO Y1792 IAW AMM 53-12-12. (K)

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2

MAJOR REPAIR - NR 6154383 - LEVEL 2 CORROSION ON FLOORBEAM AT FR 64 +9 INCHES, Y 765. REPLACED FLOORBEAM BETWEEN FR 64 TO FR 66, Y765 IAW SRM 51-72-11 DWG D53472000. (K)

Part: FLOOR PANEL — CORRODED (ZONE 200)

MAJOR REPAIR - NR 6161704 - CORRODION ON FLOOR PANEL 262FF BETWEEN FR66 TO FR68 AND BETWEEN Y1300 TO Y1560. REPLACED FLOOR PANEL 262FF BETWEEN FR66 TO FR68 AND BETWEEN Y1300 TO Y1560 IAW AMM53-12-12. (K)

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 65,145 hrs · 29,201 cycles

FLT 656 - PHX - EMERGENCY EGRESS SYSTEM - R2 DOOR ASSIST BOTTLE PRESSURE READS 1700 PSI AT 26 C. MAINTENANCE SERVICED R2 DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 64,966 hrs · 29,115 cycles

FLT 614 - ATL - EMERGENCY EGRESS SYSTEM - R-1 DOOR ASSIST BOTTLE PRESSURE LOW. MAINTENANCE SERVICED R-1 DOOR ASSIST BOTTLE AS REQUIRED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 64,640 hrs · 28,975 cycles

FLT 544 - FLASHLIGHT UNDER FLIGHT ATTENDANT JUMPSEAT FORWARD SEAT NOT CHARGING. REMOVED AND REPLACED FLASHLIGHT AT FORWARD JUMPSEAT. OPERATIONAL CHECK WAS GOOD.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 64,501 hrs · 28,916 cycles

FLT 350 LAS - EMERGENCY EGRESS SYSTEM - R1 DOOR ASSIST BOTTLE PRESSURE LOW. MAINTENANCE SERVICED R1 DOOR ASSIST BOTTLE PER AIRBUS MAINTENANCE MANUAL 52-10-00-614-050.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 64,329 hrs · 28,840 cycles

LOG PAGE 4501170 - FLT 9-ORD - EMERGENCY EGRESS SYSTEM - R1 DOOR EMERGENCY CYLINDER PRESSURE AT 900 PSI. MAINTENANCE RECHARGED R1 DOOR EMERGENCY CYLINDER TO 1900 PSI IAW AIRBUS MAINTENANCE MANUAL 52-10-00.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 64,267 hrs · 28,815 cycles

LOG PAGE 4395129 - FLT 612-ATL - EMERGENCY EQUIPMENT - R1 ENTRY DOOR EMERGENCY OPERATION CYLINDER PRESSURE LOW. MAINTENANCE SERVICED R1 ENTRY DOOR EMERGENCY OPERATION CYLINDER PER AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.

Part: LANYARD — MISROUTED (EVAC SLIDE) · airframe 64,123 hrs · 28,753 cycles

FLT 645 - PHX - EMERGENCY EQUIPMENT - R2 DOOR SLIDE SURVIVAL KIT LANYARDS NOT PROPERLY ROUTED THROUGH GIRT BAR TRIGGER. MAINTENANCE PROPERLY ROUTED R2 DOOR SLIDE SURVIVAL KIT LANYARD AND RELEASE LANYARD.

Part: LANYARD — MISROUTED (EVAC SLIDE) · airframe 64,123 hrs · 28,753 cycles

FLT 645 -PHX - EMERGENCY EQUIPMENT - L1 DOOR SLIDE SURVIVAL KIT LANYARD NOT PROPERLY ROUTED THROUGH GIRT BAR RELEASE TRIGGER. MAINTENANCE ADJUSTED SLIDE LANYARD PROPERLY.

Part: LANYARD — MISROUTED (EVAC SLIDE) · airframe 63,773 hrs · 28,590 cycles

CAMPAIGN EO - PHX - EMERGENCY EGRESS SYSTEM - PRECAUTIONARY INSPECTION OF SLIDE RAFTS FOR PROPER HARNESS/ CABLE/ LANYARD ROUTING AND CONNECTION FOUND AFT RIGHTHAND SLIDE RAFT RELEASE STRAP AND SURVIVAL KIT LANYARD ROUTED INCORRECTLY. MAINTENANCE RETURNED TO SERVICEABLE CONDITION PER EO INSTRUCTIONS.

Part: LANYARD — MISROUTED (EVAC SLIDE) · airframe 63,773 hrs · 28,590 cycles

CAMPAIGN EO - PHX - EMERGENCY EGRESS SYSTEM - PRECAUTIONARY INSPECTION OF SLIDE RAFTS FOR PROPER HARNESS/ CABLE/ LANYARD ROUTING AND CONNECTION FOUND FORWARD RIGHTHAND SLIDE RAFT RELEASE STRAP AND SURVIVAL KIT LANYARD ROUTED INCORRECTLY. MAINTENANCE RETURNED TO SERVICEABLE CONDITION PER EO INSTRUCTIONS.

Part: LANYARD — MISROUTED (EVAC SLIDE) · airframe 63,773 hrs · 28,590 cycles

CAMPAIGN EO - PHX - EMERGENCY EGRESS SYSTEM - PRECAUTIONARY INSPECTION OF SLIDE RAFTS FOR PROPER HARNESS/ CABLE/ LANYARD ROUTING AND CONNECTION FOUND FORWARD LEFTHAND SLIDE RAFT RELEASE STRAP AND SURVIVAL KIT LANYARD ROUTED INCORRECTLY. MAINTENANCE RETURNED TO SERVICEABLE CONDITION PER EO INSTRUCTIONS.

Part: LANYARD — MISROUTED (EVAC SLIDE) · airframe 63,773 hrs · 28,590 cycles

CAMPAIGN EO - PHX - EMERGENCY EGRESS SYSTEM - PRECAUTIONARY INSPECTION OF SLIDE RAFTS FOR PROPER HARNESS/ CABLE/ LANYARD ROUTING AND CONNECTION FOUND AFT LEFTHAND SLIDE RAFT RELEASE STRAP AND SURVIVAL KIT LANYARD ROUTED INCORRECTLY. MAINTENANCE RETURNED TO SERVICEABLE CONDITION PER EO INSTRUCTIONS.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 63,622 hrs · 28,508 cycles

FLT 343 - ORD - EMERGENCY EQUIPMENT - AFT FLASHLIGHT AT L2 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLASHLIGHT BATTERY.

Part: HINGE FITTING — LOOSE (RUDDER) · airframe 61,837 hrs · 27,686 cycles

SAL-C6-MAJOR REPAIR - EXCESSIVE PLAY ON RUDDER HINGE BEARING NR 4 AT VERTICAL STABILIZER STA 2632 RIB NR 6. REPLACED RUDDER HINGE FITTING NR 4 AT VERTICAL STABILIZER STA 2632 RIB NR6 IAW A320 AMM 55-36-41. (S)

Part: HINGE FITTING — LOOSE (RUDDER) · airframe 61,837 hrs · 27,686 cycles

SAL-C6-MAJOR REPAIR - PLAY ON RUDDER HINGE FITTING NR 7 AT VERTICAL STABILIZER STA 5605 RIB NR 11. REPLACED RUDDER HINGE FITTING NR 7 AT VERTICAL STABILIZER STA5605 RIB NR 11 IAW A320 AMM 55-36-41. (S)

Part: ANCHOR FITTING — CORRODED (RT WING) · airframe 61,837 hrs · 34,841 cycles

SAL-C6- MAJOR REPAIR- CORROSION ON ANCHORAGE FITTING RT WING. REPAIRED ANCHORAGE FITTING RT WING IAW US AIRWAYS EA 132038. (A)

Part: ANCHOR FITTING — CORRODED (LT WING) · airframe 61,837 hrs · 27,686 cycles

SAL-C6- MAJOR REPAIR - CORROSION ON ANCHORAGE FITTING LT WING. REPAIRED ANCHORAGE FITTING LT WING IAW US AIRWAYS EA 132038. (A)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,837 hrs · 27,686 cycles

SAL-C6- EEL - EMERGENCY EXIT LIGHT AT R1 DOOR IS INOP. REPAIRED EMERGENCY EXIT LIGHT AT R1 DOOR IAW AIRBUS AMM 33-51-00. (A)

Part: BOLT — CORRODED (SLAT TRACK) · airframe 61,837 hrs · 27,686 cycles

SAL-C6 MAJOR REPAIR - CORRODED ON BOLT THREADS ON LT WING NR 9 SLAT TRACK. REPLACED BOLT ON LT WING NR 9 SLAT TRACK IAW A320 AMM 27-84-62. (A)

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 61,349 hrs · 27,455 cycles

FLT 570 PHX-MSP - EE - FLASHLIGHT AT 1L INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY. OPERATIONAL CHECK WAS GOOD.

Part: CONTROL UNIT — FAILED (LANDING GEAR) · airframe 60,407 hrs · 27,030 cycles

FLT 18 - SNA-PHX - EL - ON CLIMBOUT FROM SNA AND ON APPROACH INTO PHX, BSCU 1 FAILED RESULTING IN "BRAKES ANTISKID NOSEWHEEL STEERING" FAULT. BSCU 2 WAS ALREADY ON MEL. AN EMERGENCY WAS DECLARED AND THE PASSENGERS WERE BRACED. THE FLIGHT LANDED WITHOUT INCIDENT AND THE AIRCRAFT WAS TOWED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE BRAKING / STEERING CONTROL UNIT. BITE CHECK WAS GOOD. BSCU WAS A CONFIRMED FAILURE. UNIT FAILED OUTPUT TEST SYSTEM 2 DUE TO DEFECTIVE RELAYS AND TRANSISTORS ON INTERCONNECT 2 BOARD. IC 37,38 ON PROCESS BOARD HAD BROKEN PINS. RELAY MFG PN EFD2C26, IC MFG PN MK7726BQ.

Part: POWER UNIT — FAILED (EMERGENCY LIGHTS) · airframe 59,034 hrs · 26,439 cycles

LAS - EEL - NR 4138710 - MX REPORTED AFT EPSU FAILS EMERG LIGHT TEST AND SELF-TEST. MX REPLACED THE AFT EPSU AND BATTERY. OPERATIONAL CHECK WAS GOOD.

Part: SKIN — DEBONDED (ZONE 600) · airframe 58,768 hrs · 26,313 cycles

LAS -NR 4165277, RIGHT WING INBOARD FLAP TRAILING EDGE HAS A 10" AREA DEBONDED, WS 0 /RIB 1 TO WS 406 / RIB 8. TEMPORARILY REPAIRED RIGHT WING INBOARD FLAP TRAILING EDGE, WS 0 /RIB 1 TO WS 406/RIB 8 IAW A320 SRM 57-52-00 AND PLACED ON MONITOR TO HAVE THE PERMANENT REPAIR ACCOMPLISHED WITHIN 3 MONTHS I/A/W A320 SRM 57-52-00.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 58,701 hrs · 26,284 cycles

LAS - EEL - LOG NR 4123399 - CREW REPORTED FWD LEFT EMERGENCY LIGHT BATTERY PACK FAILED TEST. MX REPLACED THE BATTERY PACK PER AMM 33-51-38. OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — FAILED (EMEGENCY LIGHTS) · airframe 57,698 hrs · 25,821 cycles

PHX - EEL - MX REPORTED EMERGENCY EXIT LIGHTS IN ROWS 19 AND 24 INOP. MX REPLACED THE POWER SUPPLY UNIT AND RETERMINATED THE CONNECTOR. OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 57,659 hrs · 25,805 cycles

PHX - EEL - MX REPORTED EMERGENCY LIGHTS ROW 13, 17, 19 INOP. MX REPLACED THE AFT POWER SUPPLY AND BATTERY. OPERATIONAL CHECK WAS GOOD.

Part: STRUT — CORRODED (ZONE 600) · airframe 57,506 hrs · 25,735 cycles

SAL - FOUND CORROSION ON RIGHT WING INBOARD FLAP, INTERCONNECTION STRUT FITTING HOLE, WS 3758/RIB 7. REPLACED RIGHT WING INBOARD FLAP, INTERCONNECTION STRUT FITTING, WS 3758/RIB 7 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 57,506 hrs · 25,735 cycles

SAL - FOUND CORROSION ON MAIN CABIN SEAT TRACK, FR 21 + 12" AND FR 20 + 1", -Y765 . REPLACED MAIN CABIN SEAT TRACK, FR 20 - FR 24, -Y765 IAW A320 SRM 51-72-11.

Part: SKIN — DEBONDED (ZONE 300) · airframe 57,506 hrs · 25,735 cycles

SAL - FOUND RIGHT ELEVATOR UPPER SKIN PANEL HAS EVIDENCE OF TRAPPED WATER AND IS DEBONDED, BETWEEN RIB 1 AND RIB 4. REPAIRED RIGHT ELEVATOR UPPER SKIN PANEL BETWEEN RIB 1 AND RIB 4 IAW A320 SRM 51-77-13 PARAGRAPH 2A(2), FIGURE 2.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 57,506 hrs · 25,735 cycles

SAL - FOUND CORROSION ON MAIN CABIN SEAT TRACK, +Y765, FR 36, FR 36 + 17", FR 37 + 2", FR 38 + 9", FR 39 + 2" AND FR 40 + 16". REPLACED MAIN CABIN SEAT TRACK , +Y765, FR 36 - FR 41 IAW A320 SRM 51-72-11.

Part: ANGLE — CORRODED (ZONE 500) · airframe 57,506 hrs · 25,735 cycles

SAL - FOUND CORROSION ON LEFT WING INBOARD FLAP, INTERCONNECTION STRUT FITTING HOLE, WS 4067/RIB 8. REPLACED LEFT WING INBOARD FLAP, INTERCONNECTION STRUT FITTING, WS 4067/RIB 8 IAW A320 SRM 51-72-11.

Part: SKIN — WORN (ZONE 600) · airframe 57,506 hrs · 25,735 cycles

SAL - WORN AREA ON RIGHT WING NR 2 SLAT, LOWER SURFACE TRAILING EDGE, WS 4862. REPAIRED RIGHT WING NR 2 SLAT, LOWER SURFACE TRAILING EDGE, WS 4862 IAW AWA ER 26-5743-07072-SS1.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 54,865 hrs · 24,590 cycles

LAS - EEL - CENTER LEFT (11WL) EPSU AND BATTERY FAILED TESTS REQUIRED BY TASK CARD I8M05334. MX REPLACED THE POWER SUPPLY UNIT. OPS CHECK WAS GOOD.

Part: OVEN — MALFUNCTIONED (GALLEY) · airframe 56,136 hrs · 25,131 cycles

LAS - BS - FLIGHT ATTENDANT REPORTED BURNING ODOR NR 1 OVEN NO VISIBLE RESIDUE. MAINTENANCE INSERTED DIFFERENT OVEN IN NR 1 OVEN RACK, OPS CK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,588 hrs · 24,901 cycles

PHX - EEL - MAINTENANCE TECHNICIAN NOTICED THE LEFT SIDE EMERGENCY EXIT LIGHTS IN THE MAIN CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 55,145 hrs · 24,708 cycles

ORD - FLT 654 - LG 7245620 - FLIGHT ATTENDANT REPORTS THAT EMERGENCY FLASHLIGHT AT FWD F/A JUMPSEAT NR 2 IS INOP. MAINTENANCE REMOVED AND REPLACED FLASHLIGHT BATTERY AT FWD F/A JUMPSEAT NR 2. OPS NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 54,999 hrs · 24,644 cycles

ORD - EEL - NR 3984394 - DURING OVERNIGHT MAINTENANCE DISCOVERED THE FLOOR PROXIMITY EMERGENCY LIGHT WAS INOPERATIVE AT ROW 26. MAINTENANCE FOUND A BROKEN WIRE ON HARNESS CONNECTOR. REMOVED AND REPLACED CONNECTOR IAW STANDARD PRACTICES. OPERATIONAL CHECKS WERE GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 54,706 hrs · 24,512 cycles

PHX - EEL - DURING 4 DAY CHECK, THE EMERGENCY LIGHT SYSTEM FAIL STEP 5 OF 4-DAY INSPECTION. MAINTENANCE REMOVED AND REPLACED THE RT MIDDLE EMERGENCY POWER SUPPLY UNIT AND BATTERY PACK. OPERATIONAL CHECKS WERE GOOD.

Part: HANDLE — UNSECURE (CARGO DOOR) · airframe 52,764 hrs · 23,687 cycles

FLT 287 - CREW REPORTED AFT CARGO DOOR OPEN ON T/O ROLL PRIOR TO 60 KNOTS. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND HANDLE NOT COMPLETELY CLOSED. CLOSED HANDLE OPS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,189 hrs · 23,450 cycles

PHX - EEL - DURING 8-DAY CHECK DISCOVERED, THE LT OVERWING ESCAPE PATH LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING EMERGENCY LIGHT POWER SUPPLY IAW AIRBUS 319/320 MM 33-51-38-04. OPERATIONAL CHECKS GOOD.

Part: STRINGER — CORRODED · corrosion level 2 · airframe 51,911 hrs · 23,325 cycles

MCN - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION IN SEVERAL LOCATION ON STRINGER 42R, FROM FR 54 + 16" TO FR 58 + 6". MAINTENANCE REMOVED CORROSION ON STRINGER 42R, FROM FR 54 + 16" TO FR 58 + 6", IAW AIRBUS 320 SRM 51-74-00. NO ALLOWABLE DAMAGE LIMITS ARE AVAILABLE IN THE AIRBUS A320 SRM. MAINTENANCE REMOVED DAMAGED SECTION FROM STRINGER 42R IAW AMERICA WEST AIRLINES ENGINEERING REPAIR 26-5341-05215-SS1. FABRICATED ANGLE IAW AWA ER 26-5341-05215-SS1. PREPARED ANGLE, STRINGER, CLIPS FOR INSTALLATION IAW AWA ER 26-5341-05215-SS1. INSTALLED REPAIR PART ON STRINGER 42R. FROM FR 54 + 16" TO FR 58 + 6" IAW AWA ER 26-5341-05215-SS1.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,911 hrs · 23,325 cycles

SAL - DURING C4 CHECK DISCOVERED CORROSION AT STRINGER 31R, FS 65, INTERNAL STRUCTURE UNDER FLOOR COMPARTMENT. MAINTENANCE REMOVED CORROSION AND NO ALLOWABLE DAMAGE WAS FOUND IN SRM. MAINTENANCE REMOVED STRINGER 31R FROM FS 64 TO FS 67 IAW AIRBUS SRM 51-42-11. INSTALLED NEW STRINGER AND FASTENERS FROM FS 64 TO FS 67 IAW AIRBUS 320 SRM 51-42-11.

Part: FLAP — DETERIORATED (ZONE 500 - LEFT) · airframe 51,911 hrs · 23,325 cycles

DURING C4 CHECK DISCOVERED COMPOSITE DETERIORATED AT TRAILING EDGE OF THE INBOARD FLAP ON THE LT WING. MAINTENANCE GROUND DOWN AND CLEANED THE SURFACE OF THE INBOARD FLAP, TRAILING EDGE, L/H WING IAW AIRBUS A320 SRM 57-52-00. APPLIED GLASS FABRIC AND LAMINATING RESIN TO TRAILING EDGE INBOARD FLAP, LT WING, IAW AIRBUS A320 SRM 57-52-00 AND AMERICA WEST AIRLINES ENGINEERING REPAIR NR 26-5752-05213-RC2.

Part: WEB — CORRODED · corrosion level 2 · airframe 51,911 hrs · 23,325 cycles

DURING C4 CHECK DISCOVERED CORROSION ON WEB LOCATED IN THE AFT CARGO COMPARTMENT BETWEEN FS 58 AND FS 59, Y700. WEB WAS REMOVED FROM AFT CARGO COMPARTMENT, BETWEEN FS 58 AND FS 59, Y700 IAW AIRBUS 320 SRM 51-72-11. INSTALLED REPAIR PARTS IAW AIRBUS 320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,911 hrs · 23,325 cycles

DURING C4 CHECK, DISCOVERED CORROSION ON THE RT OUTBOARD SEAT TRACK FS 41+10, -Y1292. MAINTENANCE REMOVED CORROSION IAW A320 SRM 51-75-00 AND FOUND REWORK TO BE OUT OF LIMITS IAW A320 SRM 53-31-15. RT OUTBOARD SEAT TRACK, AT FR 41+10, -Y1292, WAS REMOVED IAW A320 SRM 51-47-11 AND NEW SEAT TRACK WAS PREPARED FOR INSTALLATION IAW A320 SRM 51-44-11. INSTALLED REPAIR PARTS, AT FR 41+10, -Y1292, IAW A320 SRM 51-42-11 AND DRAWING NR D53370500.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,911 hrs · 23,325 cycles

DURING C4 CHECK DISCOVERED CORROSION ON LOWER SILL OF L1 DOOR, FROM FS 16 TO FS 20, Y 1584. NO ALLOWABLE LIMITS FOUND. MAINTENANCE REMOVED AND REPLACED THE FITTINGS ON L1 DOOR, LOWER SILL, FROM FS 16 TO FS 20, Y 1584, IAW AIRBUS 320 SRM 51-72-11.

Part: FITTING — CORRODED (DOOR SILL) · corrosion level 2 · airframe 51,911 hrs · 23,325 cycles

DURING C4 CHECK, DISCOVERED CORROSION AROUND HOLES ON R1 DOOR LOWER SILL FROM FS 16 TO FS 20. NO ALLOWABLE LIMITS EXIST. MAINTENANCE REMOVED AND REPLACED THE FITTINGS ON R1 DOOR LOWER SILL IAW AIRBUS 320 SRM 51-72-11.

Part: WEB — CORRODED · corrosion level 2 · airframe 51,911 hrs · 23,325 cycles

DURING C4 CHECK DISCOVERED CORROSION ON FLANGE OF WEB LOCATED IN THE AFT CARGO COMPARTMENT BETWEEN FS 56 AND FS 57, Y700. NO ALLOWABLE DAMAGE LIMITS FOUND IN THE AIRBUS SRM. MAINTENANCE REMOVED WEB IN THE AFT CARGO COMPARTMENT BETWEEN FS 56 AND FS 57, Y700 IAW SRM. INSTALLED NEW WEB AND FASTENERS IN THE AFT CARGO COMPARTMENT BETWEEN FR56 AND FR57, Y700 IAW AIRBUS 320 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,911 hrs · 23,325 cycles

SAL - DURING C4 CHECK DISCOVERED CORROSION ON SEVERAL SECTION OF SEAT TRACK LOCATED BETWEEN FS 36 AND FS 47, BUTT LINE Y765 AND Y-1292. MAINTENANCE REMOVED ALL CORROSION FROM SEAT TRACKS BETWEEN FS 36 AND FS 47, BL Y765 AND Y-1292 IAW AIRBUS 320 SRM 51-74-00. FOUND RE-WORK ON SEAT TRACKS TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK SECTIONS FROM VARIOUS LOCATION BETWEEN FS 36 TO FS 47 AND BETWEEN BUTT LINE Y765 TO Y-1292 IAW AIRBUS 320 SRM 51-42-11. INSTALLED NEW SEAT TRACK SECTIONS FROM FS 36 TO FS 47, BUTT LINE Y765 TO Y-1292 AND APPLIED PROTECTIVE TREATMENT IAW AIRBUS 320 SRM 51-42-11 AND A320 SRM 51-21-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,911 hrs · 23,325 cycles

DURING C4 CHECK, DISCOVERED CORROSION ON LONGITUDINAL BEAM BETWEEN FS 68 TO FS 69, BL +Y1170. REMOVED CORROSION IAW A320 SRM 51-74-00 AND WAS FOUND TO BE OUT OF LIMITS. REMOVED BEAM BETWEEN FS 68 TO FS 69 IAW AIRBUS 320 SRM 51-42-11. NEW BEAM WAS PREPARED FOR INSTALLATION IAW A320 SRM 51-44-11. INSTALLED REPAIR PARTS BETWEEN FS 68 TO FS 69, BL +Y1170 IAW A320 SRM 51-42-11 AND 51-21-11.

Part: SHEAR WEB — CRACKED · airframe 51,911 hrs · 23,325 cycles

SAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CRACK IN SHEAR WEB BETWEEN FR 68 AND FR 68+13", AND BETWEEN -Y1190 AND -Y1432. MAINTENANCE REMOVED CRACKED SHEAR WEB BETWEEN FR 68 AND FR 68+13", AND BETWEEN -Y1190 AND -Y1432 IAW AIRBUS 320 SRM 51-42-11. INSTALLED NEW SHEAR WEB BETWEEN FR 68 AND FR 68+13", AND BETWEEN -Y1190 AND -Y1432 IAW AIRBUS 320 SRM 51-42-11 IAW AIRBUS 320 SRM 51-72-11 PAGE 1. CRACK LENGTH NOT LISTED.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,911 hrs · 23,325 cycles

DURING C4 CHECK, DISCOVERED CORROSION ON WEB NEXT TO R1 DOOR, FRAME 20, -Y1584. NO ALLOWABLE DAMAGE LIMITS FOUND IN AIRBUS SRM 53-11-14. MAINTENANCE REMOVED CORRODED NEXT TO R1 DOOR, FS 20 IAW AIRBUS SRM 51-72-11. PREPARED NEW WEB FOR INSTALLATION IAW AIRBUS SRM 51-25-00. INSTALLED REPAIR PARTS NEXT TO R1 DOOR, FR 20 IAW AIRBUS SRM 51-72-11.

Part: STRUCTURE — CORRODED (R2 DOOR WAY) · corrosion level 2 · airframe 51,911 hrs · 23,325 cycles

DURING C4 CHECK, DISCOVERED CORROSION ON EXTRUSION AT R2 DOOR CUTOUT, BETWEEN FS 66 +5, AND FS 68 -5, BL -Y1465. MAINTENANCE REMOVED CORRODED EXTRUSION AT R2 DOOR CUTOUT BETWEEN FS 66 +5 AND FS 68 -5 IAW AIRBUS 320 SRM 51-42-11. INSTALLED NEW EXTRUSION AT R2 DOOR CUTOUT BETWEEN FR 66 +5 AND FR 68 -5 IAW SRM 51-42-11.

Part: SUPPORT — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 51,911 hrs · 23,325 cycles

DURING C4 CHECK, DISCOVERED CORROSION ON SUPPORT, LOCATED AT FR 70 - 4, -Y 1180, UNDER STRINGER 23R. MAINTENANCE REMOVED CORRODED SUPPORT AT FR 70 - 4, -Y1180, UNDER STRINGER 23R. PREPARED NEW SUPPORT FOR INSTALLATION IAW AIRBUS MM 51-25-00. INSTALLED REPAIR PARTS AT FR 70 - 4" AND -Y 1180, UNDER STRINGER 23R IAW AIRBUS MM 51-72-11 PAGES 1 AND 2.

Part: COVER — CORRODED · corrosion level 2 · airframe 51,911 hrs · 23,325 cycles

DURING C4 CHECK DISCOVERED CORROSION ALONG LOWER SILL COVER SHEET, UPPER SURFACE, FROM FS 52A TO FS 56 IN THE AFT CARGO COMPARTMENT. MAINTENANCE MECHANICALLY REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-41-49. REMOVED COVER SHEET AND INSTALLED NEW COVER SHEET FROM FS 52A TO FS 56 IN THE AFT CARGO COMPARTMENT IAW AIRBUS 320 SRM 51-42-11.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,911 hrs · 23,325 cycles

DURING C4 CHECK DISCOVERED EXFOLIATION CORROSION ON WEB, LOCATED AT -Y1180, FROM FS 69 TO FS 70. MAINTENANCE REMOVED CORRODED WEB FROM FS 69 TO FS 70, -Y1180 IAW AIRBUS SRM 51-72-11 PAGE 1 AND 2. INSTALLED NEW WEB IAW AIRBUS SRM 51-72-11 PAGES 1 AND 2.

Part: WEB — CORRODED · corrosion level 2 · airframe 51,911 hrs · 23,325 cycles

DURING C4 CHECK DISCOVERED CORROSION ON WEB NEXT TO FORWARD FRAME OF THE R1 DOOR, FS 16 TO FS 14, -Y1379.5. MAINTENANCE REMOVED CORROSION IAW AIRBUS 320 SRM 51-74-00. NO ALLOWABLE DAMAGE LIMITS AVAILABLE. MAINTENANCE FABRICATED DOUBLER IAW AMERICA WEST ENGINEERING REPAIR NR 26-5312-05204-ES1. INSTALLED FABRICATED REPAIR PARTS FROM FS 14 TO FS 16, -Y1379.5 IAW AWA ER NR 26-5312-05204-ES1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,911 hrs · 23,325 cycles

DURING C4 CHECK, DISCOVERED CORROSION ON LONGITUDINAL BEAM BETWEEN FS 65-5 TO FS 69+4, -Y1170. REMOVED CORROSION IAW A320 SRM 51-74-00 AND WAS FOUND TO BE OUT OF LIMITS. REMOVED BEAM BETWEEN FS 65-5 TO FS 69+4 IAW AIRBUS 320 SRM 51-42-11. NEW BEAM WAS PREPARED FOR INSTALLATION IAW A320 SRM 51-44-11. INSTALLED REPAIR PARTS BETWEEN FS 65-5 TO FS 69+4 IAW A320 SRM 51-42-11 AND 51-21-11.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,911 hrs · 23,325 cycles

DURING C4 CHECK DISCOVERED CORROSION ALONG LOWER SILL THRESHOLD SHEET IN THE AFT CARGO COMPARTMENT FROM FS 52+9.5 TO FS 56. MAINTENANCE REMOVED LOWER SILL THRESHOLD SHEET IN THE AFT CARGO COMPARTMENT IAW AIRBUS SRM 51-42-11 PAGE 2. FABRICATED NEW THRESHOLD SHEET IAW AIRBUS DRAWING NR D53475575. INSTALLED FABRICATED REPAIR PARTS AT LOWER SILL IN THE AFT CARGO COMPARTMENT FROM FS 52+9.5 TO FS 56 IAW AIRBUS SRM 51-42-11.

Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 51,911 hrs · 23,325 cycles

SAL - DURING C4 CHECK DISCOVERED SILL SHAPE LOCATED AT FS 68-8" ON CABIN FLOOR STRUCTURE. MAINTENANCE REMOVED SILL SHAPE LOCATED AT FR 68-8" ON CABIN FLOOR STRUCTURE IAW AIRBUS 320 SRM 51-42-11. INSTALLED NEW FASTENERS AND SILL SHAPE AT FS 68-8", CABIN FLOOR STRUCTURE, IAW AIRBUS 320 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,911 hrs · 23,325 cycles

DURING C4 CHECK, DISCOVERED CORROSION ON SEAT RAIL BETWEEN FS 64 AND FS 66+5, -Y1292. MAINTENANCE REMOVED CORROSION FROM SEAT RAIL AND FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-15. REMOVED CORRODED SEAT RAIL FROM FS 64 TO FS 66+5 IAW AIRBUS 320 SRM 51-42-11. INSTALLED NEW SEAT RAIL AND FASTENERS FROM FS 64 TO FS 66+5, -Y1292 IAW AIRBUS 320 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,911 hrs · 23,325 cycles

DURING C4 CHECK, DISCOVERED CORROSION AT LONGITUDINAL FLOOR SUPPORT, LOCATED AT -Y81, FR 14. NO ALLOWABLE LIMITS FOUND. MAINTENANCE REMOVED FLOOR SUPPORT AT -Y81, FR 14 IAW AIRBUS SRM 51-42-11. INSTALLED NEW FLOOR AT -Y81, FS 14 BEAM IAW AIRBUS SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,911 hrs · 23,325 cycles

SAL - DURING C4 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT +Y1180 AND BETWEEN FR 66+4" AND FR 68-5". MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14 FIG 102. MAINTENANCE REMOVED FLOORBEAM AT +Y1180 AND BETWEEN FR 66+4" AND FR 68-5" AND INSTALLED NEW FLOORBEAM IAW AIRBUS 320 SRM 51-42-11.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,911 hrs · 23,325 cycles

DURING C4 CHECK DISCOVERED GALVANIC CORROSION ON DUMMY RAIL FROM FS 66+5 TO FS 68-5, FROM -Y1170 TO -Y1292. REMOVED CORROSION FROM DUMMY RAIL, FROM FS 66+5 TO FS 68-5, FROM -Y1170 TO -Y1292 IAW AIRBUS 320 SRM 51-74-00. REWORK FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14. REMOVED DUMMY RAIL FROM FS 66+5 TO FS 68-5, FROM -Y1170 TO -Y1292 IAW AIRBUS 320 SRM 51-42-11. PREPARED NEW DUMMY RAIL FOR INSTALLATION IAW AIRBUS 320 SRM 51-49-11. REPAIR PARTS INSTALLED FROM FS 66+5 TO FS 68-5, FROM -Y1170 TO -Y1292 IAW AIRBUS 320 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,911 hrs · 23,325 cycles

DURING C4 CHECK, DISCOVERED CORROSION ON FLOORBEAM Y-254, FROM FS 16 TO FS 19. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM AT Y -254, FROM FS 16 TO FS 19 IAW AIRBUS SRM 53-11-14 FIG 202. PREPARED NEW FLOORBEAM FOR INSTALLATION IAW AIRBUS SRM 53-11-14 AND 51-47-00. INSTALLED FABRICATED REPAIR PARTS AT Y -254, FS 16 TO FS 19 IAW AIRBUS SRM 51-42-11.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,911 hrs · 23,325 cycles

SAL - DURING C4 CHECK DISCOVERED CORROSION ON WEB IN CABIN LOCATED AT FS 69+16", STRINGER 23L, Y1200. NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE AIRBUS 320 SRM. MAINTENANCE REMOVED AND REPLACED THE WEB LOCATED AT FR 69+16", STRINGER 23L, Y1200 IAW AIRBUS 320 SRM 51-44-11. ALSO, APPLIED SEALANT TO NEW WEB IAW AIRBUS 320 SRM 51-76-11.

Part: CABLE — LOOSE (R2 DOOR SLIDE) · airframe 51,753 hrs · 23,245 cycles

DURING 8-DAY CHECK, FOUND R2 DOOR SLIDE CABLE LOOSE. MAINTENANCE REMOVED AND REPLACED R2 DOOR SLIDE IAW AMERICA WEST AIRLINES TASK CARD R1C25304.

Part: GENERATOR — DAMAGED (NR 1 ENGINE) · airframe 50,918 hrs · 22,883 cycles

ON TAKEOFF AT LAS EN ROUTE TO MSP RECEIVED CLASS I ECAM MESSAGE ELECT IDG OIL LOW PRESSURE, REJECTED TAKEOFF AT 50 KTS. ISSUED MEL 24-20-01, COND 2 NR 1 IDG INOP. MAINTENANCE TROUBLESHOT THE NR 1 IDG PER TSM TASK 24-20-00-810 AND FOUND METALIC PARTICLES IN THE FILTER AND HOUSING ASSEMBLIES. REMOVED AND REPLACED NR 1 IDG IAW T/C R5M24301, OPERATIONAL CHECK WAS GOOD. FAILURE ANALYSIS OF IDG S/N 1593 CONFIRMED REASON FOR REMOVAL FINDING SMALL METAL PARTICLES IN SCAVENGE FILTER CAUSING IT TO CLOG. FURTHER INVESTIGATION REVEALED FIXED SPINE SHAFT INBOARD BEARING INNER RACE WAS END LOADING CAUSE BEARING FAILURE. VENDOR RECOMMENDS THIS UNIT TO BE OVERHAULED.

Part: ODOR — DETECTED (COCKPIT) · airframe 48,738 hrs · 21,950 cycles

ON CLIMB OUT, AN ELECTRICAL BURNING ODOR NOTICED IN COCKPIT FOLLOWED BY SMOKE COMING FROM AIR CON VENTS IN COCKPIT & CABIN, DONNED O2 MASKS & TURNED BACK, WHEN EXITING RUNWAY RECEIVED PACK 1 OVRHT IND. A/C OUT OF SERVICE. MX FOUND ACM FROZEN, R & R ACM IAW AMM, OPS CK GOOD, NO SMOKE NOTED. NR 1 PACK STILL HAS LOW FLOW PROBLEM, REPLACED NR 1 PACK FLOW CONTROL VALVE IAW AMM, ANTI-ICE VALVE, BYPASS VALVE, AND NR 1 & 2 PACK SENSORS, SYS OPS NORM. INSP OF ACM FOUND TURBINE OUTLET LINED WITH CARBON RESIDUE THAT HAD A NOTICEABLE ODOR, UNIT NOT SEIZED, BUT HAD A HIGH TORQUE OF 56 IN. LBS. DISASSY FOUND TURBINE BEARING DAMAGED WITH A SEVERE RUB & OVRHT COND THAT RESULTED IN A SCORED BEARING JOURNAL ON SHAFT ASSY.

Part: PACKING — BURST (HYD SYSTEM) · airframe 47,216 hrs · 21,343 cycles

PHL - EMERGENCY LANDING - FLT 0256 - EN ROUTE FROM PHX TO PHL AT CRUISE RECEIVED CLASS 1 MESSAGE FOR GREEN HYDRAULIC SYSTEM RESERVOIR LOW LEVEL, MANUALLY EXTENDED LANDING GEAR AND DECLARED AN EMERGENCY. MAINTENANCE FOUND HYDRAULIC LEAK IN LEFT WHEEL WELL WHERE PRESSURE SWITCH (10CE1) IS INSTALLED IN MANIFOLD. REMOVED AND REPLACED O-RING PACKINGS ON FLIGHT CONTROL PRESSURE SWITCH (10CE1), LEAK AND OPERATIONAL CHECKS WERE GOOD.

Part: CONNECTOR — LOOSE (SEAT ROW 11 LT) · airframe 46,518 hrs · 21,073 cycles

MCN - EEL - DURING C-03 CHECK THE EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT SEAT ROW 11 LT WILL NOT LOCK ONTO THE RECEPTACLE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT SEAT ROW 11 LT; OPERATIONAL CHECK WAS GOOD.

Part: PROXIMITY SWITCH — FAULTY (L-2 DOOR) · airframe 46,518 hrs · 21,073 cycles

MCN - EES - DURING C-03 CHECK THE L-2 DOOR SLIDE ARMED LIGHT DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR SLIDE ARM LIGHT PROXIMITY SWITCH, OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 46,250 hrs · 20,962 cycles

DURING INSPECTION FOUND EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE AT SEAT ROWS 13, 17, 19, & 24. MAINTENANCE REMOVED AND REPLACED AFT LT EMERGENCY POWER SUPPLY UNIT (13WL), ALSO FOUND SHORT TO GROUND AT SEAT ROW 19 AT 6690VN DCI; REPAIRED BROKEN WIRES AT SEAT ROW 19 LT, OPERATIONAL CHECK WAS GOOD. PART NAME: CABLE, MFG; AIRBUS, P/N; ABS0374A24, REASON; SHORTED, LOC; SEAT ROW 19 LT.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 45,912 hrs · 20,820 cycles

PHX - EEL - DURING INSPECTION THE LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL) FAILED SELF TEST (INTERNAL LOAD FAULT). MAINTENANCE REMOVED AND REPLACED LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 45,912 hrs · 20,820 cycles

PHX - EEL - DURING INSPECTION FOUND A WIRE BROKEN ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26. MAINTENANCE REPAIRED BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 26 LT, OPERATIONAL CHECK WAS GOOD.

Part: BRAKE — MALFUNCTIONED (MLG) · airframe 43,796 hrs · 19,976 cycles

ON TAKEOFF ROLL AT PHX EN ROUTE FOR ONT FLIGHT CREW THOUGHT THEY MAY HAVE EXPERIENCED A POSSIBLE BRAKE LOCKUP. AS A PRECAUTION, DECLARED AN EMERGENCY AT ONT.

Part: TERMINAL — BROKEN (CABIN) · airframe 39,908 hrs · 18,435 cycles

EWR - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT WAS INOPERATIVE AT SEAT ROW 19 LT. MAINTENANCE REPAIRED BROKEN TERMINAL AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 19 LT, OPERATIONAL CHECK GOOD.

Part: CABLE — BROKEN (SEAT ROW 22 L/H) · corrosion level 0 · airframe 42,729 hrs · 19,562 cycles

LAS - EEL - DURING INSPECTION BROKEN WIRES WERE FOUND ON THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 22 L/H. MAINTENANCE REPAIRED EMERGENCY ESCAPE PATH LIGHT WIRES AT SEAT ROW 22 L/H, OPERATIONAL CHECK GOOD.

Part: CONNECTOR — IMPROPER PART (R/H OVERWING) · corrosion level 0 · airframe 42,487 hrs · 19,468 cycles

PHX - EMERGENCY EVACUATION - DURING INSPECTION THE SLIDE DISARM LIGHTS WOULD NOT EXTINGUISH WHEN DISARMING THE L/H AND R/H OVERWING SLIDES. MAINTENANCE DISCOVERED PIN "B" ON THE L/H OVERWING SLIDE CONNECTOR 5WN1 WAS RECESSED, RESEATED PIN "B" ON L/H OVERWING SLIDE CONNECTOR 5WN1. ON THE R/H OVERWING SLIDE MAINTENANCE FOUND PIN "F" RECESSED, AND PIN "U" WAS THE TYPE ON CONNECTOR 2WN2. REMOVED AND REPLACED R/H OVERWING SLIDE CONNECTOR 2WN2, OPERATIONAL CHECK OF SLIDE DISARM LIGHTS WAS GOOD.

Part: SPLICE — LOOSE (SEAT ROW 11 L/H) · corrosion level 0 · airframe 42,482 hrs · 19,466 cycles

MCN - EEL - DURING C-02 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 L/H WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BAD SPLICE ON ESCAPE PATH LIGHT AT SEAT ROW 11 L/H PER ESPM 20-53-29, PG.4, FUNCTIONAL CHECK WAS GOOD IAW AWA T/C F1C33301.

Part: SPLICE — LOOSE (SEAT ROW 5 L/H) · corrosion level 0 · airframe 42,482 hrs · 19,466 cycles

MCN - EEL - DURING C-02 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 L/H WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BAD SPLICE ON ESCAPE PATH LIGHT AT SEAT ROW 5 L/H PER ESPM 20-53-29, PG.4, FUNCTIONAL CHECK WAS GOOD IAW AWA T/C F1C33301.

Part: FRAME — CRACKED · corrosion level 0 · airframe 42,482 hrs · 19,466 cycles

MCN - MAJOR REPAIR - DURING C-02 CHECK A 1/8" CRACK WAS FOUND AT FASTENER HOLE ON FRAME 39 AT BS 1725, BELOW STR 14 R/H. MAINTENANCE CUTOUT CRACK ON FRAME 39 AT BS 1725; FABRICATED A FILLER AND REPAIR ANGLE; AND INSTALLED REPAIR PARTS IAW AWA E.O. 53-14-20.

Part: FRAME — CRACKED · corrosion level 0 · airframe 42,482 hrs · 19,466 cycles

MCN - MAJOR REPAIR - DURING C-02 CHECK A 1/8" CRACK WAS FOUND AT FASTENER HOLE ON FRAME 38 AT BS 1669, BELOW STR 14 R/H. MAINTENANCE CUTOUT CRACK ON FRAME 38 AT BS 1669; FABRICATED A FILLER AND REPAIR ANGLE; AND INSTALLED REPAIR PARTS IAW AWA E.O. 53-14-20.

Part: FRAME — CRACKED · corrosion level 0 · airframe 42,482 hrs · 19,466 cycles

MCN - MAJOR REPAIR - DURING C-02 CHECK A 1/8" CRACK WAS FOUND AT FASTENER HOLE ON FRAME 41 AT BS 1810, BELOW STR 14 R/H. MAINTENANCE CUTOUT CRACK ON FRAME 41 AT BS 1810; FABRICATED A FILLER AND REPAIR ANGLE; AND INSTALLED REPAIR PARTS IAW AWA E.O. 53-14-20.

Part: FRAME — CRACKED · corrosion level 0 · airframe 42,482 hrs · 19,466 cycles

MCN - MAJOR REPAIR - DURING C-02 CHECK A 1/8" CRACK WAS FOUND AT FASTENER HOLE ON FRAME 38 AT BS 1669, BELOW STR 14 L/H. MAINTENANCE CUTOUT CRACK ON FRAME 38 AT BS 1669; FABRICATED A FILLER AND REPAIR ANGLE; AND INSTALLED REPAIR PARTS IAW AWA E.O. 53-14-20.

Part: FRAME — CRACKED · corrosion level 0 · airframe 42,482 hrs · 19,466 cycles

MCN - MAJOR REPAIR - DURING C-02 CHECK A 1/8" CRACK WAS FOUND AT FASTENER HOLE ON FRAME BS 1810, BELOW STR 14 L/H. MAINTENANCE CUTOUT CRACK ON FRAME AT BS 1810; FABRICATED A FILLER AND REPAIR ANGLE; AND INSTALLED REPAIR PARTS IAW AWA E.O. 53-14-20.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 42,033 hrs · 19,283 cycles

LAS - EMERGENCY EQUIPMENT - DURING INSPECTION THE AFT CABIN EMERGENCY FLASHLIGHT WAS FOUND TO NEED NEW BATTERIES. MAINTENANCE REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,847 hrs · 19,199 cycles

PHX - EEL - FLIGHT CREW REPORTED OVERWING EXIT LIGHTS ILLUMINATED AND THE RT OVERWING EXIT SLIDE LIGHT DOES NOT INDICATES ARMED. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING BATTERY PACK AT POWER SUPPLY (11WL), AND RESEATED THE RT OVERWING DOOR WARNING PLUNGER, OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 41,284 hrs · 18,986 cycles

CMH- EEL - DURING CHECKS OF THE EMERGENCY LIGHTING SYSTEM, MAINTENANCE FOUND LT OVERWING SLIDE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY PER MM 33-51-32-401. LIGHTS CHECKED OK.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 41,218 hrs · 18,961 cycles

PHX - EEL - PROGRAMMING AND TEST PANEL FAILED TEST OF EMERGENCY LIGHT SYSTEM. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 10WL (LT FWD), AND 11WL (LT MIDDLE) IAW AMM 33-51-00-710-001, EMERGENCY LIGHT TEST CHECKED GOOD.

Part: FILTER — CLOGGED (BLEED AIR SYS) · airframe 41,132 hrs · 18,929 cycles

ON CLIMBOUT, CREW RECEIVED ECAM MESSAGE FOR NR 1 ENG BLEED FAULT; BLEED TEMP REACHED 280 DEGREES & CROSSFEED VALVE OPENED; ACFT TURNED BACK TO PHX. MX REPLACED THE FAN AIR THERMOSTAT AND OPERATIONALLY CHECKED OUT SYS BY RUNNING ENG FOR AN EXTENDED PERIOD OF TIME AT POWER, CHECK GOOD. SYS WAS PREVIOUSLY PLACED ON MEL 36-11-04 COND. NR 1 FAN AIR VALVE INOPERATIVE FOR SIMILAR EVENT OCCURRED 04/28/2002. NR 1 ENG FAN AIR VALVE REPLACED. VENDOR BENCH TEST REPORT FOR FAN AIR VALVE, NO FAULT FOUND. VENDOR TEAR DOWN OF TEMP CONTROL THERMOSTAT CONFIRMED FAILURE. PROBLEM IDENTIFIED AS FILTER CLOGGED BY POLLUTION. FILTER CLEANED, A PRESSURE REDUCING CLAPPER GUIDE & PACKING SEAL WERE REPLACED.

Part: CONNECTOR — BROKEN (SEAT ROW 19 L/H) · corrosion level 0 · airframe 40,991 hrs · 18,867 cycles

ATL - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 L/H WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CANNON PLUG AT THE WALL PLUG IN, SEAT ROW 19 L/H, OPERATIONAL CHECK WAS GOOD IAW AMM 33-51-00-710-001.

Part: FIRE LOOP — CHAFED (NR 1 ENGINE) · airframe 40,035 hrs · 18,484 cycles

PHX - ABORTED T/O - FLT 0317 - C - WHILE PREPARING TO TAKEOFF FROM PHX EN ROUTE TO CMH WHEN THROTTLE WERE ADVANCED FLIGHT CREW RECEIVED A NR 1 ENGINE FIRE LOOP-A FAULT. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE TROUBLESHOT AND FOUND CORE LOOP-A HARNESS CHAFED ALMOST ALL THE WAY THROUGH IN TWO PLACES APPROXIMATELY 6 INCHES FROM HIGH PRESSURE BLEED VALVE. REMOVED AND REPLACED CORE LOOP-A HARNESS IAW AMM 26-12-17-401, OPERATIONAL TEST WAS GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 39,752 hrs · 18,376 cycles

PHX - EEL - C - EMERGENCY ESCAPE LIGHTS INOPERATIVE ON THE LEFT SIDE OF THE AIRCRAFT. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 11WL, OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 39,577 hrs · 18,305 cycles

CMH - EEL - "C" - SEVERAL EMERGENCY LIGHTS INOPERATIVE MID CABIN LT SIDE. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT AT 11WL, ZONE 241 IAW AMM 33-51-38-000-001.

Part: O-RING — LEAKING (HYDRAULIC SYS)

CLE - EMERGENCY LANDING - FLT 534 - C - EN ROUTE FROM PHX TO CLE RECEIVED YELLOW HYDRAULIC SYSTEM RESERVOIR LOW LEVEL QUANTITY INDICATION WITH PRESSURE INDICATING NORMAL, 1 HR 30 MIN LATER SYSTEM LOST ALL PRESSURE. DECLARED EMERGENCY LANDING INTO CLE, LANDING WAS UNEVENTFUL. MAINTENANCE TROUBLESHOT AND REPLACED DEFECTIVE O-RING ON QUICK DISCONNECT COUPLING AE99116K ON YELLOW SYSTEM HYDRAULIC MANIFOLD. MAINTENANCE ALSO DISCOVERED NR 2 ENGINE HYDRAULIC PUMP CASE DRAIN FILTER DIFFERENTIAL BUTTON POPPED, AS PRECAUTION REPLACED CASE DRAIN FILTER AND NR 2 ENGINE HYDRAULIC PUMP IAW AMM 29-13-51-401.

Part: PACKING — BROKEN (ZONE 198) · airframe 38,962 hrs · 18,055 cycles

LAX - ABORTED APPROACH - FLT 37 - "C" - ON FINAL APPROACH ECAM INDICATED YELLOW HYDRAULIC SYSTEM LOW PRESSURE, SYSTEM FLUID DEPLETED AND THE CREW PERFORMED A GO AROUND. THE SUBSEQUENT APPROACH AND LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A PACKING FROM THE QUICK DISCONNECT FITTING FROM THE PTU BROKEN AND THE FITTING LEAKING FLUID. MAINTENANCE REPLACED THE PACKING, SERVICED THE HYD SYSTEM AND PERFORMED LEAK CHECKS, ALL CHECKS WERE GOOD.

Part: TRANSFORMER — FAILED (NR 1) · airframe 38,541 hrs · 17,866 cycles

BOS- AIR TURNBACK - FLT 442 - AFTER TAKEOFF FROM BOS EN ROUTE TO PHX THE CREW GOT A TRANSFORMER RECTIFIER 1 (TR1) FAILURE INDICATION AND RETURNED TO BOS. IN BOS MAINTENANCE TROUBLESHOT AND REPLACED TR1 PER AMM 24-32-51-401. THE SYSTEM OPERATIONALLY CHECKED NORMAL PER AMM 24-23-00-501. NO FURTHER DISCREPANCIES HAVE BEEN REPORTED.

Part: HYDRAULIC SYSTEM — LOW (FUSELAGE) · airframe 36,840 hrs · 17,203 cycles

SEA - EMERGENCY LANDING - 2/10/01 - ON DESCENT INTO SEA THE GREEN HYDRAULIC SYSTEM WENT TO LOW LEVEL. IN SEA THE AIRCRAFT WAS INSPECTED AND NO LEAKS FOUND. THE GREEN SYSTEM HYDRAULIC SYSTEM WAS SERVICED TO FULL AND NO FURTHER PROBLEMS REPORTED. THIS WAS THE FIRST FLIGHT AFTER NR 1 ENGINE CHANGE AND PROBABLY HAD AIR TRAPPED IN THE SYSTEM AFTER THE ENGINE CHANGE.

Part: LANDING GEAR — MALFUNCTIONED (MAIN) · airframe 36,477 hrs · 17,052 cycles

ON LANDING GEAR EXTENSION THE NOSE GEAR SHOWED NOT DOWN/LOCKED; THE PILOT JIGGLED THE HANDLE AND ABOUT 10 SEC LATER THE GEAR THEN SHOWED DOWN AND LOCKED; CREW MADE AN EMERGENCY LANDING. THE PROBLEM WAS TROUBLESHOT IAW TSM 32-31-00 PG.A212 & A213; NO FAULTS WERE FOUND AND NO ASSOCIATED FAULTS WERE NOTICED ON PREVIOUS FLIGHT REPORTS; THE AIRCRAFT WAS RELEASED IAW TSM 00-INTRO: PG 28 (2)(B)2

Part: LIGHT — INOPERATIVE (CABIN)

RIGHT FWD OVERWING ERMERGENCY ESCAPE SLIDE LIGHT INOP. REMOVED AND REPLACED RIGHT OVERWING ESCAPE LIGHT ASSEMBLY

Part: WIRE — BROKEN (CABIN)

DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT AT SEAT 24 LEFT WAS FOUND INOP. A NEW TERMINAL END WAS INSTALLED ON THE WIRE, OPS CHECKED GOOD

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 33,222 hrs · 15,779 cycles

C-CHECK, AFT CABIN FLOOR SUPPORT Y1292 RT CORRODED FS 66 TO FS 69. REPLACED AFT CABIN FLOOR SUPPORT IAW A320 SRM 53-41-14 FIG 8 PG 33. PRIMED IAW A320 SRM 51-75-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 33,222 hrs · 15,779 cycles

C-CHECK, CABIN FLOOR SUPPORT Y1292 LT BETWEEN FS 16 & 20 SUPPORT CORRODED ON TOP SURFACE. REMOVED FLOOR SUPPORT, FABRICATED REPAIR PARTS AND INSTALLED PARTS IAW A320 SRM 53-11-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,222 hrs · 15,779 cycles

C-CHECK, AFT CABIN SUPPORT BEAM Y765 RT CORRODED AT FS 68. CORROSION REMOVED IAW A320 SRM 51-74-00, FLOOR SUPPORT BEAM Y 765 RT REPAIRED IAW ER 26-5341-00045-JL1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 33,222 hrs · 15,779 cycles

C-CHECK, AFT CABIN FLOOR SUPPORT Y1292 LT UPPER AND LOWER SURFACES CORRODED AT FS 66 TO FS 69. REPLACED FLOOR SUPPORT IAW A320 SRM 53-41-14 FIG 8 PG 33. PRIMED IAW A320 SRM 51-75-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 33,222 hrs · 15,779 cycles

C-CHECK, AFT CABIN FLOOR SUPPORT Y160 RT CORRODED AT FS 70. CORROSION REMOVED FOUND BEYOND LIMITS. REPLACED FLOOR SUPPORT IAW A320 SRM 53-41-14. PRIMED AND PAINTED IAW A320 SRM 51-75-00.

Part: BRACKET — CORRODED (LATCH MOUNT) · airframe 332,221 hrs · 15,779 cycles

C-CHECK, LT AFT OVERWING HATCH, LOWER AFT LATCH MOUNT BRACKET CORRODED. INSTALLED NEW T-SECTION IAW A320 SRM 52-21-00.

Part: PITOT — MALFUNCTIONED (FUSELAGE)

CONDITION: ABORTED TAKE-OFF NO F/O AIRSPEED INDICATION LP 7552885DISCREPANCY: TAKE-OFF REJECTED @90KTS DUE TO NO AIRSPEED INDICATION ON FO SIDECORRECTIVE ACTION: R+R F/O PITOT PROBE PER AMM 13-11-15-109--PITOT STATIC LK CHECK NML AND PRBES R+R'D AIR DATA MODULE AS A PRECAUTION--CHECKED PITOT LINES FROM ADM AND PROBE--NO FAULT FOUNDCURRENT HISTORY: ATA 341 ONE UN-RELATED WRITE-UP IN 90 DAY LOOK BACKRECOMMENDATION: REMAIN OPEN PENDING TEARDOWN REPORT

Part: BSCU — FAILED (NLG STEERING)

ABORTED TAKEOFF, UNCOMMANDED VEERING TO THE RIGHT THEN TO THE LEFT, BSCU CHANNEL 2 FAULT ON UPPER ECAM NO ASSOCIATED DATA. REMOVED AND REPLACED BSCU, OPS CK NML IAW MM 32-42-000-001.

Part: SEAT TRACK — CORRODED (BS 254)

DURING ROUTINE MAINTENANCE CHECK, FOUND LT AND RT FLOOR TRACK DUMMY RAILS AT STATION Y254, FRAMES FR16 TO FR20 WERE CORRODED BEYOND SRM LIMITS. DUMMY RAILS REPLACED PER SRM 51-54-00.

Part: FAN — FAILED (E/E COMPT)

DURING CLIMBOUT, EXPERIENCED A VIBRATION THAT SEEMED TO ORIGINATE IN THE AREA BELOW THE FLIGHT DECK, FOLLOWED BY AN ELECTRICAL SMOKE SMELL. SHUT DOWN OF VENTILATION BLOWER FAN, STOPPED ALL NOISES, VIBRATIONS AND SMELLS. REPLACED AVIONICS COOLING FAN, SYSTEM OPS NORMAL.

Part: O-RING — FAILED (GREEN HYD SYST)

EMERGENCY DECLARED, GREEN SYSTEM RSVR LO LEVEL EN ROUTE. DIVERT TO LAS. REPLACED O-RING ON PRESSURE SWITCH ON GREEN MAIN HYDRAULIC POWER MANIFIOLD, SERVICED ALL THREE MANIFOLDS, RESET EMERGENCY GEAR HANDLE.

Part: LENS — MISSING (CABIN)

L3/D EMERGENCY LIGHT LENS MISSING. REINSTALLED LENS.

Part: ANTI-ICE DUCT — FAILED (NR 2 ENGINE)

AIR TURNBACK, NR 2 ENGINE NACELLE TEMP AND HIGH EGT FOUND ANTI-ICE ELBOW THAT CONNECTS ENG TO VENTURI MISSING HALF OF FLANGE AND HOLDING CLAMP WAS BLOWN OUT. REMOVED AND REPLACED BOTH PARTS.

Part: WIRE — LOOSE (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 15 LT EMERGENCY EXIT LIGHT INOP. RECONNECTED LOOSE CONNECTION, OPS CHECK GOOD.

Part: CONNECTOR — DISCONNECTED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT MOUNTED EMERGENCY LIGHT INOP AT ROW 15 AND ROW 26. RESECURED CONNECTOR AND INSTALLED NEW LENS AT ROW 15. RESECURED CONNECTOR AT ROW 2, SYSTEM OPS CHECK GOOD.

Part: SLIDE — BLOWN (CABIN)

CAPTAIN CALLED AT PUSH TIME WITH OVERWING SLIDE NOT SHOWING ARMED ON ECAM. REMOVED HANDLE ACCESS PANEL AND SLIDE ARMED LIGHT DID NOT COME ON. FOUND THE PIN THAT ARMS SLIDE JAMMED. PINNED DOOR SLIDE BOTTLE IN AFT PIT FOR LEFT WING SLIDE. WENT TO INSTALL PIN AND SLIDE POPPED THE COVER OFF ON THE OUTSIDE. SLIDE DID NOT FULLY INFLATE. FOUND A BENT ROLL PIN ON ARMING PIN AT AFT DOOR. REMOVED AND REPLACED SLIDE.

Part: WIRE — BROKEN (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 26 A, B, C SEAT MOUNTED EMERGENCY LIGHT INOP. REPAIRED WIRING AS NEEDED, OPS CHECK GOOD.

Part: EEL BATTERY — DISCHARGED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, RT MID CABIN BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY, OPS CHECK GOOD. (W)

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, LEFT AFT EMERGENCY LIGHT BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M)

Part: IDG COOLER — CONTAMINATED (NR 2 ENGINE)

LAS-MKE - ON CLIMBOUT, LOST NR 2 ENG IDG. ACFT RETURNED TO LAS WITHOUT FURTHER PROBLEMS, NO OVERWEIGHT LANDING. MX REMOVED AND REPLACED THE NR 2 ENG IDG PER AWA TASK CARD R3M24301. REMOVED AND REPLACED NR 1 ENG TEMP CONTROL THERMOSTAT PER AMM. REMOVED AND REPLACED THE NR 2 ENG IDG OIL COOLER PER AMM, LEAK CHECK GOOD. NR 2 ENG IDG LEAK CHECK GOOD AND PARAMETERS WITHIN LIMITS OF AWA TASK CARD R3M24301. NR 1 ENG TCT OPS CHECK NORMAL. BLEED PRESSURE AND TEMP NORMAL. ACFT RETURNED TO SERVICE. REF 95ZZZZ244, 95ZZZZ245.

Part: IDG THERMOSTAT — FAILED (NR 1 ENGINE)

LAS-MKE - ON CLIMBOUT, LOST NR 2 ENG IDG. ACFT RETURNED TO LAS WITHOUT FURTHER PROBLEMS, NO OVERWEIGHT LANDING. MX REMOVED AND REPLACED THE NR 2 ENG IDG PER AWA TASK CARD R3M24301. REMOVED AND REPLACED NR 1 ENG TEMP CONTROL THERMOSTAT PER AMM. REMOVED AND REPLACED THE NR 2 ENG IDG OIL COOLER PER AMM, LEAK CHECK GOOD. NR 2 ENG IDG LEAK CHECK GOOD AND PARAMETERS WITHIN LIMITS OF AWA TASK CARD R3M24301. NR 1 ENG TCT OPS CHECK NORMAL. BLEED PRESSURE AND TEMP NORMAL. ACFT RETURNED TO SERVICE. REF 95ZZZZ245, AWXA9500291.

Part: GENERATOR — FAILED (NR 2 ENGINE)

LAS-MKE - ON CLIMBOUT, LOST NR 2 ENG IDG. ACFT RETURNED TO LAS WITHOUT FURTHER PROBLEMS, NO OVERWEIGHT LANDING. MX REMOVED AND REPLACED THE NR 2 ENG IDG PER AWA TASK CARD R3M24301. REMOVED AND REPLACED NR 1 ENG TEMP CONTROL THERMOSTAT PER AMM. REMOVED AND REPLACED THE NR 2 ENG IDG OIL COOLER PER AMM, LEAK CHECK GOOD. NR 2 ENG IDG LEAK CHECK GOOD AND PARAMETERS WITHIN LIMITS OF AWA TASK CARD R3M24301. NR 1 ENG TCT OPS CHECK NORMAL. BLEED PRESSURE AND TEMP NORMAL. ACFT RETURNED TO SERVICE. REF 95ZZZZ244, AWXA9500291.

Part: B-NUT — LOOSE (YELLOW HYD SYST)

CMH-LAS - FLT 255 - IN CRUISE, LOST YELLOW HYDRAULIC QUANTITY. AC RETURNED TO CMH WITHOUT FURTHER PROBLEMS. MX TIGHTENED B-NUT AT YELLOW SYSTEM VALVES, HYDRAULIC PRESS MANIFOLD. SYSTEM SERVICED AND LEAK CHECKS OK. AC RETURNED TO SERVICE. (Z)

Part: RAIL — CORRODED (BS 1292)

PHX - DURING SCHEDULED C4 INSPECTION, FOUND RAIL MINUS 1292 BETWEEN FRAME 16 AND FRAME 20 CORRODED. FABRICATED AND INSTALLED RAIL PER SRM 51-42-11. (M)

Part: RAIL — CORRODED (BS 254)

PHX - DURING SCHEDULED C4 INSPECTION, FOUND RAIL AT MINUS 254 BETWEEN FRAME 16 AND FRAME 18 CORRODED AT SCREW HOLES. REPAIRED PER SRM 53-11-14. (M)