N622AW

Part: LENS — MISSING (CABIN) · airframe 75,561 hrs · 34,056 cycles

SEAT 9C MISSING EMERGENCY LIGHT LENS. INSTALLED NEW LENS ON EMERGENCY LIGHT AT 9C IAW A320 CMM 25-25-01.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 74,982 hrs · 33,787 cycles

C2 CHECK, AREA OF WATER INGRESS ON UPPER SURFACE OF RT ELEVATOR AT APPROXIMATELY 17 INCHES FWD OF TE & 1.13 INCHES FROM INBD EDGE. REPAIRED RT ELEVATOR UPPER SURFACE IAW EA 206220.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 75,083 hrs · 33,834 cycles

FLOOR PANEL SOFT AT CENTER AISLE ROW 8 AREA BETWEEN FRAMES 32 - 35 & BETWEEN S23L TO S23R, BL 0. REPLACED FLOOR PANEL IAW AMM 53-12-12.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 74,843 hrs · 33,717 cycles

RED EXIT ROW EMERGENCY LIGHT LENS IS MISSING FROM LIGHT AT 9L. INSTALLED RED LENS TO EMERGENCY LIGHT AT EXIT ROW 9L.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 74,770 hrs · 33,679 cycles

DELAMINATION ON FLOOR PANEL BETWEEN FRAMES 64 TO 66 & S21L TO S21R. REPLACED FLOOR PANEL IAW AMM 53-42-12-400-002-A.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 74,770 hrs · 33,679 cycles

FOUND DELAMINATION ON FLOOR PANEL 251WF BETWEEN FRAMES 62 TO 64 & S21L TO S21R. REPLACED FLOOR PANEL IAW AMM 53-42-12-400-001-A.

Part: SLIDE — BULGED (L1 DOOR) · airframe 74,707 hrs · 33,650 cycles

L1 DOOR GUST LOCK, HARD TO LATCH AND UNLATCH. FOUND SLIDE RAFT BULGING CAUSING GUST LOCK NOT TO ENGAGE. R & R L1 SLIDE IAW TASK CARD 26L00025011.

Part: TRU — INOPERATIVE (COCKPIT) · airframe 74,386 hrs · 33,490 cycles

THE COCKPIT CREW DETECTED SMOKE IN THE COCKPIT DURING CRUISE ALTITUDE. MX REPLACED THE NR ONE TRANSFORMER RECTIFIER.

Part: SKIN PANEL — DELAMINATED (RUDDER) · airframe 74,365 hrs · 33,480 cycles

RUDDER LT SKIN PANEL DELAMINATED 15" FROM TIP AND 8" FWD OF T/E. R & R RUDDER IAW AMM 27-21-41.

Part: SLIDE RAFT — UNSECURE (PAX DOOR) · airframe 74,329 hrs · 33,464 cycles

LEFT REAR PAX DOOR SLIDE MECHANISM CAME OFF OF DOOR. REPLACED L2 DOOR SLIDE RAFT.

Part: WIRE HARNESS — DISCONNECTED (CABIN) · airframe 73,960 hrs · 33,282 cycles

EMERGENCY LIGHT 7A INOPERATIVE. RECONNECTED LOOSE WIRE.

Part: GUST LOCK — LACK OF LUBE (L1 DOOR) · airframe 73,923 hrs · 33,265 cycles

GUST LOCK ON DOOR 1L DIFFICULT TO OPERATE. LUBRICATED L-1 GUST LOCK.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 73,482 hrs · 33,053 cycles

EMERGENCY FLASHLIGHT AT JUMP SEAT 1L DOES NOT FLASH. REPLACED FLASHLIGHT AS REQUIRED.

Part: WIRE — BROKEN (CABIN) · airframe 73,290 hrs · 32,960 cycles

EMERGENCY LIGHT ON SEAT ROW 26 LEFT INOP (WIRE BROKEN). REPAIRED WIRE PER ELECTRICAL STANDARD PRACTICE MANUAL 20-43-12, ELECTRICAL STANDARD PRACTICE MANUAL 20-43-10. TESTS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,244 hrs · 32,938 cycles

EMERGENCY EXIT LIGHT BY 2R DOOR INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT LENS COVER NEAR 2R DOOR.

Part: BRACKET — LOOSE (EMERGENCY LIGHT) · airframe 72,848 hrs · 32,746 cycles

EMERGENCY FLOOR LIGHTING SEAT 17C BROKEN. RE-SECURED EMERGENCY FLOOR LIGHT BRACKET. OPS CHECKED GOOD.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 72,702 hrs · 32,680 cycles

L2 DOOR ASSIST BOTTLE CHARGE IS LOW. SERVICED L2 DOOR ASSIST BOTTLE PER AMM 52-10-00-614-001-A.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 71,408 hrs · 32,058 cycles

L2 DOOR ASSIST NEEDS SERVICING. SERVICED L2 DOOR TO PROPER PRESSURE. OPS CHECKED GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 70,973 hrs · 31,843 cycles

C1 CHECK - BROKEN EMERGENCY EGRESS LIGHTS BROKEN AT ROW 17ABC & 11FED. RE-SECURED EMERGENCY LIGHT ASSEMBLY AT ROW 17ABC & 11FED IAW A320 AMM 33-51-19.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 70,972 hrs · 31,842 cycles

BC1 CHECK - 5 EA CRACKS ON SEGMENT ANGLE APPROX 1/8 INCH IN LENGTH ON FORWARD LEFT EMERGENCY EXIT DOOR 833. REPLACED SEGMENT ANGLE ON FORWARD LEFT EMERGENCY EXIT DOOR 833 IAW EO 5210Y228.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 70,972 hrs · 31,842 cycles

BC1 CHECK - 10 EA CRACKS ON SEGMENT ANGLE APPROX 1/8 INCH IN LENGTH ON AFT RIGHT EMERGENCY EXIT DOOR 844. REPLACED SEGMENT ANGLE ON AFT RIGHT EMERGENCY EXIT DOOR 844 IAW EO 5210Y228.

Part: DAMPER — LEAKING (L2 DOOR) · airframe 70,972 hrs · 31,842 cycles

C1 CHECK - LEFT AFT ENTRY L2 DOOR EMERGENCY ASSIST ACTUATOR BOTTLE BLEED DOWN AFTER CHARGE AND DOOR OPENS SLOWLY. REPLACED DIAPHRAGM IN THE PERCUSSION MECHANISM OF THE L2 DOOR DAMPER, SHEAR PIN WAS ALSO REPLACED IAW A320 AMM 52-10-00-610-001-A.

Part: HINGE PIN — BENT (NLG) · airframe 70,972 hrs · 31,842 cycles

BC1 CHECK - NOSE LANDING GEAR TORQUE LINKS CENTER HINGE PIN IS BENT. REPLACED NOSE LANDING GEAR TORQUE LINKS CENTER HINGE PIN IAW JOB CARD 26C71032003.

Part: LENS — MISSING (CABIN) · airframe 70,762 hrs · 31,740 cycles

EMERGENCY AISLE LIGHT LENS IS MISSING AT ROW 9R. INSTALLED EMERGENCY AISLE LIGHT LENS AT ROW 9R.

Part: COMPUTER — FAILED (E&E BAY) · airframe 70,660 hrs · 31,689 cycles

CREW RECEIVED ECAM MESSAGE FOR AVIONICS SMOKE AFTER LANDING WITH SMOKE IN GEN LINE 1 SWITCH. CAPTAIN REQUESTED PRIORITY TAXI AND FIRE TRUCK. MAINTENANCE MET AIRCRAFT AT GATE AND NO SMELL OR SIGNS OF SMOKE WERE NOTED. REMOVED AND REPLACED THE AVIONIC EQUIPMENT VENTILATION COMPUTER (AEVC) AND AVIONIC COMPARTMENT SMOKE DETECTOR. FAILURE OF THE AEVC WAS CONFIRMED DURING LOOP TESTING AT VENDOR - PART INFORMATION PROVIDED.

Part: CONNECTOR — LOOSE (CABIN) · airframe 70,534 hrs · 31,632 cycles

SEAT MOUNTED EMERGENCY LIGHT AT ROW 11 RIGHT INOPERATIVE. SECURED WALL CONNECTOR AT ROW 12 - SYSTEM OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 70,214 hrs · 31,490 cycles

RT EMERGENCY EXIT LIGHT POWER SUPPLY UNIT BATTERY FAULTS. REMOVED AND REPLACED RT EMERGENCY EXIT LIGHT POWER SUPPLY BATTERY PER AIRBUS MAINTENANCE MANUAL 33-51-39-401.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 69,762 hrs · 31,284 cycles

DOOR L2 OPEN ASSIST BOTTLE PRESSURE LOW. SERVICED DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00.

Part: PUMP — DEFECTIVE (HYDRAULIC SYS) · airframe 69,060 hrs · 30,974 cycles

CREW REPORTED LOSS OF GREEN HYDRAULIC SYSTEM ON DESCENT INTO PDX. CONDUCTED GRAVITY EXTENSION OF LANDING GEAR AND DECLARED AN EMERGENCY; PASSENGERS WERE NOT INSTRUCTED TO BRACE. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP IAW AIRBUS MAINTENANCE MANUAL 29-11-51-400 AND HYDRAULIC PRESSURE SWITCH FOR GREEN SYSTEM IAW AIRBUS MAINTENANCE MANUAL 29-11-17.

Part: PRESSURE SWITCH — DEFECTIVE (HYDRAULIC SYS) · airframe 69,060 hrs · 30,974 cycles

CREW REPORTED LOSS OF GREEN HYDRAULIC SYSTEM ON DESCENT INTO PDX. CONDUCTED GRAVITY EXTENSION OF LANDING GEAR AND DECLARED AN EMERGENCY; PASSENGERS WERE NOT INSTRUCTED TO BRACE. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP IAW AIRBUS MAINTENANCE MANUAL 29-11-51-400 AND HYDRAULIC PRESSURE SWITCH FOR GREEN SYSTEM IAW AIRBUS MAINTENANCE MANUAL 29-11-17.

Part: PUMP — LEAKING (BLUE SYSTEM) · airframe 68,830 hrs · 30,872 cycles

DURING DESCENT, PACKS STILL EMITTING DIRTY SOCK, FOUL ODOR. FOUND HYDRAULIC FLUID FROM BLUE ELECTRIC PUMP CONTAMINATING ENVIRONMENTAL SYSTEM. REMOVED AND REPLACED BLUE ELECTRIC PUMP.

Part: LIGHT — LOOSE (CABIN) · airframe 68,254 hrs · 30,600 cycles

PHX - EEL - EMERGENCY PATH LIGHT LOOSE A/C LEFT FORWARD BULKHEAD PANEL. REMOVED AND REPLACED LIGHT ASSEMBLY.

Part: ACTUATOR — STALLED (NR 1 ENGINE VSV) · airframe 67,569 hrs · 30,284 cycles

FLT 88 - CREW REPORTED NR 1 ENGINE COMPRESSOR STALL ON CLIMB WITH MAX EGT 720+ FOR ONE MINUTE. SHUT DOWN ENGINE, DECLARED AN EMERGENCY AND RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE. THE ROOT CAUSE WAS IDENTIFIED AS THE VSV ACTUATOR WHICH WAS STUCK / DIFFICULT TO MOVE.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 67,443 hrs · 30,227 cycles

FLT 77 - SEA - EES - R-2 DOOR ASSIST CYLINDER PRESSURE IS LOW. MAINTENANCE SERVICED R-2 DOOR ASSIST CYLINDER IAW AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 67,167 hrs · 30,104 cycles

FLT 77 - SEA - EES - R-2 DOOR ASSIST BOTTLE CHARGE IS LOW. MAINTENANCE SERVICED R-2 DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 67,167 hrs · 30,104 cycles

FLT 77 - SEA - EES - L-2 DOOR ASSIST BOTTLE CHARGE IS LOW. MAINTENANCE SERVICED L-2 DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 66,749 hrs · 29,916 cycles

FLT 94 - PHX - EES - R-2 DOOR ASSIST BOTTLE LOW PRESSURE. MAINTENANCE SERVICED R-2 DOOR ASSIST BOTTLE TO PROPER PRESSURE.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - CRACK ON AFT TRANSMITTING PROFILE OF AFT LEFT EMERGENCY EXIT DOOR INTERNAL STRUCTURE. REPAIRED AFT TRANSMITTING PROFILE OF AFT LEFT EMERGENCY EXIT DOOR INTERNAL STRUCTURE IAW 133087A.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - CRACKS ON FORWARD & AFT TRANSMITTING PROFILE OF FORWARD RIGHT EMERGENCY EXIT DOOR INTERNAL STRUCTURE AT BEAM 2. REPAIRED FORWARD & AFT TRANSMITTING PROFILE OF FORWARD RIGHT EMERGENCY EXIT DOOR INTERNAL STRUCTURE AT BEAM 2 IAW EA 33100A.

Part: SKIN — DEBONDED (RUDDER) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - AREA OF DEBONDING ON LEFT SIDE OF RUDDER APPROX 3.75 INCHES FROM TRAILING EDGE & 17.5 INCHES DOWN FROM TOP OF RUDDER. REPAIRED LEFT SIDE OF RUDDER IAW EA 133073.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 66,304 hrs · 29,703 cycles

SAL - C5 - EEL - FORWARD LEFT EMERGENCY POWER SUPPLY UNIT INOP. REPLACED FORWARD LEFT EMERGENCY POWER SUPPLY UNIT IAW A320 AMM 33-51-38, OPS TEST GOOD.

Part: SUPPORT ANGLE — CORRODED (E&E DOOR) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON SUPPORT ANGLE AT LOWER CURVED EDGE OF E/E DOOR AT FORWARD RIGHT SIDE INTERNAL STRUCTURE BETWEEN FR38 TO FR39. REPLACED SUPPORT ANGLE AT LOWER CURVED EDGE OF E/E DOOR AT FORWARD RIGHT SIDE INTERNAL STRUCTURE BETWEEN FR38 TO FR39 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR45, -Y765. REPLACED SEAT TRACK BETWEEN FR41 TO FR47, -Y765 IAW EA 133079.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON FUSELAGE FRAME AT FORWARD SERVICE DOOR CUTOUT AT FR16, S23R. REPAIRED FUSELAGE FRAME AT FORWARD SERVICE DOOR CUTOUT AT FR16, S23R IAW EA 133071.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON FUSELAGE FRAME AT FORWARD SERVICE DOOR CUTOUT AT FR20, S23R. REPAIRED FUSELAGE FRAME AT FORWARD SERVICE DOOR CUTOUT AT FR20, S23R IAW EA 133071.

Part: SUPPORT ANGLE — CORRODED (E&E DOOR) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON SUPPORT ANGLE AT LOWER CURVED EDGE OF E/E DOOR AT AFT LEFT SIDE INTERNAL STRUCTURE AT FR40 + 12 INCHES. REPLACED SUPPORT ANGLE AT LOWER CURVED EDGE OF E/E DOOR AT AFT LEFT SIDE INTERNAL STRUCTURE AT FR40 + 12 INCHES IAW A320 SRM 51-72-11.

Part: SUPPORT ANGLE — CORRODED (E&E DOOR) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON SUPPORT ANGLE AT LOWER CURVED EDGE OF E/E DOOR FORWARD LEFT SIDE INTERNAL STRUCTURE AT FR38 + 12 INCHES. REPLACED SUPPORT ANGLE AT LOWER CURVED EDGE OF E/E DOOR AT FORWARD LEFT SIDE INTERNAL STRUCTURE AT FR38 + 12 INCHES IAW A320 SRM 51-72-11.

Part: DAMPER — LOW PRESSURE (SERVICE DOOR) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - LOW PRESSURE AT AFT SERVICE DOOR DAMPER. REPLACED AFT SERVICE DOOR CYLINDER DOOR DAMPER IAW A320 AMM 52-13-14.

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON FITTING AT FORWARD ENTRY DOOR CUTOUT AT AFT LOWER CORNER FR20, S23L. REPLACED FITTING AT FORWARD ENTRY DOOR CUTOUT AT AFT LOWER CORNER FR20, S23L IAW A320 SRM 51-72-11.

Part: HINGE FITTING — DAMAGED (NLG DOOR) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - ELONGATED HOLE & WEAR ON AFT HINGE FITTING NR 1 AT LEFT NOSE LANDING GEAR AFT DOOR BETWEEN FR19 TO FR20, S39L. REPLACED AFT HINGE FITTING NR 1 AT LEFT NOSE LANDING GEAR AFT DOOR BETWEEN FR19 TO FR20, S39L IAW A320 CMM 52-82-32.

Part: HINGE FITTING — DAMAGED (NLG DOOR) · airframe 66,304 hrs · 26,703 cycles

SAL - S5 - MAJOR REPAIR - ELONGATED HOLE & WEAR ON AFT HINGE FITTING NR 2 AT LEFT NOSE LANDING GEAR AFT DOOR BETWEEN FR19 TO FR20, S39L. REPLACED AFT HINGE FITTING NR 2 AT LEFT NOSE LANDING GEAR AFT DOOR BETWEEN FR19 TO FR20, S39L A320 CMM 52-82-32.

Part: HINGE FITTING — DAMAGED (NLG DOOR) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - ELONGATED HOLE & WEAR ON FORWARD HINGE FITTING NR 2 AT LEFT NOSE LANDING GEAR AFT DOOR BETWEEN FR19 TO FR20, S39L. REPLACED FORWARD HINGE FITTING NR 2 AT LEFT NOSE LANDING GEAR AFT DOOR BETWEEN FR19 TO FR20, S39L IAW A320 CMM 52-82-32.

Part: HINGE FITTING — DAMAGED (NLG DOOR) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - ELONGATED HOLE & WEAR ON FORWARD HINGE FITTING NR 1 AT LEFT NOSE LANDING GEAR AFT DOOR BETWEEN FR19 TO FR20, S39L. REPLACED FORWARD HINGE FITTING NR 1 AT LEFT NOSE LANDING GEAR AFT DOOR BETWEEN FR19 TO FR20, S39L IAW A320 CMM 52-82-32.

Part: PANEL — CORRODED (LT WING) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - CORROSION IN COUNTERSUNK HOLES OF LEFT WING LOWER FUEL PANEL 540JB. REPLACED LEFT WING LOWER FUEL PANEL 540JB IAW JOB CARD 26C50057026.

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON FITTING AT FORWARD ENTRY DOOR CUTOUT AT FORWARD LOWER CORNER FR16, S23L. REPLACED FITTING AT FORWARD ENTRY DOOR CUTOUT AT FORWARD LOWER CORNER FR16, S23L IAW A320 SRM 51-72-11.

Part: DOOR FRAME — CORRODED (E&E DOOR) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON CURVED EDGE OF E/E DOOR FORWARD RIGHT SIDE OF EXTERNAL STRUCTURE BETWEEN FR38 TO FR39, BEAM 4. REPLACED CURVED EDGE OF E/E DOOR FORWARD RIGHT SIDE OF EXTERNAL STRUCTURE BETWEEN FR38 TO FR39, BEAM 4 IAW A320 SRM 51-72-11.

Part: FITTING — CORRODED (SERVICE DOOR) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON FITTING AT AFT LOWER CORNER AT FR20, S23R OF FWD SERVICE DOOR. REPLACED FITTING AT AFT LOWER CORNER AT FR20, S23R OF FWD SERVICE DOOR IAW A320 SRM 51-72-11.

Part: STRINGER — WORN (FUSELAGE) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - WEAR ON STRINGER AT FR58 + 9 INCHES, S11R. REPAIRED STRINGER AT FR58 + 9 INCHES, S11R IAW A320 SRM 53-00-13.

Part: ANGLE — CRACKED (E&E DOOR) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - CRACK IN FORWARD LEFT SIDE OF SEGMENT ANGLE AT E/E DOOR INTERNAL STRUCTURE. REPLACED FORWARD LEFT SIDE OF SEGMENT ANGLE AT E/E DOOR INTERNAL STRUCTURE IAW A320 SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON FITTING AT FORWARD SERVICE DOOR CUTOUT FORWARD LOWER CORNER AT FR16, S23R. REPLACED FITTING AT FORWARD SERVICE DOOR CUTOUT FORWARD LOWER CORNER AT FR16, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112109.

Part: HINGE FITTING — EXCESS PLAY (ELEVATOR) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - EXCESSIVE PLAY ON RIGHT ELEVATOR HINGE FITTING NR 6. REPLACED RIGHT ELEVATOR HINGE FITTING NR 6 IAW A320 AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ELEVATOR) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - EXCESSIVE PLAY ON RIGHT ELEVATOR HINGE FITTING BEARING NR 1. REPLACED RIGHT ELEVATOR HINGE FITTING NR 1 IAW A320 AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ELEVATOR) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - EXCESSIVE PLAY ON RIGHT ELEVATOR HINGE FITTING BEARING NR 5. REPLACED RIGHT ELEVATOR HINGE FITTING NR 5 IAW A320 AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ELEVATOR) · airframe 66,304 hrs · 29,703 cycles

SAL - S5 - MAJOR REPAIR - EXCESSIVE PLAY ON RIGHT ELEVATOR HINGE FITTING BEARING NR 2. REPLACED RIGHT ELEVATOR HINGE FITTING NR 2 IAW A320 AMM 55-16-42.

Part: OVEN — DEFECTIVE (GALLEY) · airframe 66,183 hrs · 29,649 cycles

FLT 9 - ORD - BURNING SMELL - NR 2 OVEN HAS AN ELECTRICAL BURNING SMELL. MAINTENANCE REMOVED AND REPLACED THE NR 2 OVEN PER AIRBUS MAINTENANCE MANUAL 25-35-19.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 65,345 hrs · 29,298 cycles

FLT 614 - ATL - EES - AFT LEFT SERVICE DOOR (L2) EMERGENCY CYLINDER / ACCUMULATOR PRESSURE LOW (100 PSI AT 26 DEG C). MAINTENANCE SERVICED AFT LEFT SERVICE DOOR EMERGENCY CYLINDER / ACCUMULATOR AS PER AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.

Part: LENS — MISSING (CABIN) · airframe 63,994 hrs · 28,693 cycles

FLT 3 - PHX - EEL - EMERGENCY EXIT LIGHT COVER MISSING AT SEAT 7C. MAINTENANCE REPLACED LENS AT 7C.

Part: O-RING — LEAKING (HYD ACCUMULATOR) · airframe 63,829 hrs · 28,622 cycles

FLT 86 - PHX-PDX - EMERGENCY LANDING - AT CRUISE ALTITUDE, ECAM CLASS 1 MESSAGE: Y HYD LOW LVL. FLUID WAS LOW. SHUT DOWN Y HYDRAULIC PUMP PER ECAM. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED HYDRAULIC ACCUMULATOR O-RING AND SERVICED ACCUMULATOR.

Part: LIGHT — MISSING (CABIN) · airframe 63,553 hrs · 28,494 cycles

FLT 342 - LAS - EEL - ROW 26L EMERGENCY EXIT LIGHT LENS MISSING. MAINTENANCE REPLACED ROW 26L EMERGENCY EXIT LAMP LENS.

Part: COVER — MISINSTALLED (EMERGENCY EXIT) · airframe 63,494 hrs · 28,469 cycles

FLT 196 - PHX - EMERGENCY EGRESS SYSTEM - DURING DESCENT AT 6000 FT AND 2.5 PSI, LEFT AFT EMERGENCY EXIT DOOR SHOWED OPEN & SLIDE IN AMBER. MAINTENANCE INSPECTED AND FOUND LEFT AFT EMERGENCY EXIT DOOR HANDLE COVER INSTALLED INCORRECTLY. RE-INSTALLED COVER AND OPS CHECKED PER AIRBUS MAINTENANCE MANUAL 52-20-00.

Part: COMPUTER — DEFECTIVE (AUTOPILOT SYS) · airframe 63,481 hrs · 28,462 cycles

FLT 71 PHX-SEA - ATO - TAKEOFF WAS ABORTED AT 80 KNOTS DUE TO THRUST SEQUENCING ECAM WARNING. MAINTENANCE REPLACED NR 1 FMGC RACK CONNECTOR AND BOTH FLIGHT MANAGEMENT GUIDANCE COMPUTERS.

Part: CONNECTOR — BROKEN (NR 1 FMGC) · airframe 63,481 hrs · 28,462 cycles

FLT 71 PHX-SEA - ATO - TAKEOFF WAS ABORTED AT 80 KNOTS DUE TO THRUST SEQUENCING ECAM WARNING. MAINTENANCE REPLACED NR 1 FMGC RACK CONNECTOR AND BOTH FLIGHT MANAGEMENT GUIDANCE COMPUTERS.

Part: CONNECTOR — DEFECTIVE (NR 1 FMGC) · airframe 63,481 hrs · 28,462 cycles

FLT 71 PHX-SEA - ATO - TAKEOFF WAS ABORTED AT 80 KNOTS DUE TO THRUST SEQUENCING ECAM WARNING. MAINTENANCE REPLACED NR 1 FMGC RACK CONNECTOR AND BOTH FLIGHT MANAGEMENT GUIDANCE COMPUTERS.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON INTERNAL STRUCTURE OF BULKHEAD FRAME AT FR70 BETWEEN S22R TO S23R. REPAIRED INTERNAL STRUCTURE OF BULKHEAD FRAME AT FR70 BETWEEN S22R TO S23R IAW US AIRWAYS EA 132598.

Part: FITTING — CRACKED (CARGO BAY) · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - CRACK ON FITTING AT FR28 BETWEEN S37R TO S39R IN FORWARD CARGO COMPARTMENT. REPLACED FITTING AT FR28 BETWEEN S37R TO S39R IN FORWARD CARGO COMPARTMENT IAW A320 SRM 51-72-11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - CRACK ON FUSELAGE FRAME AT FR40 BETWEEN S22R TO S23R. REPAIRED FUSELAGE FRAME AT FR40 BETWEEN S22R TO S23R IAW US AIRWAYS EA 132591.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - CORROSION ON FUSELAGE FRAME AT FR59 BETWEEN S33R TO S34R. REPAIRED FUSELAGE FRAME AT FR59 BETWEEN S33R TO S34R IAW EA 132619.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - CRACK ON FUSELAGE FRAME AT FR41 BETWEEN S23R TO S24R. REPAIRED FUSELAGE FRAME AT FR41 BETWEEN S23R TO S24R IAW US AIRWAYS EA 132591.

Part: LANYARD — MISINSTALLED (EVAC SLIDE) · airframe 63,232 hrs · 28,357 cycles

SAL - BC-7 - EES - SURVIVAL KIT LANYARD INSTALLED INCORRECTLY IN SLIDE RAFT AT R-1 DOOR. INSTALLED SURVIVAL KIT LANYARD CORRECTLY IN SLIDE RAFT AT R-1 DOOR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - CRACK ON FUSELAGE FRAME AT FR39 BETWEEN S22R & S23R, ALSO AT S22R. REPAIRED FUSELAGE FRAME AT FR39 BETWEEN S22R & S23R, ALSO AT S22R IAW US AIRWAYS EA 132591.

Part: LANYARD — MISINSTALLED (EVAC SLIDE) · airframe 63,232 hrs · 23,357 cycles

SAL - BC-7 - EES - SURVIVAL KIT LANYARD INSTALLED INCORRECTLY IN SLIDE RAFT AT R-2 DOOR. INSTALLED SURVIVAL KIT LANYARD CORRECTLY IN SLIDE RAFT AT R-2 DOOR.

Part: LANYARD — MISINSTALLED (EVAC SLIDE) · airframe 63,232 hrs · 28,357 cycles

SAL - BC-7 - EES - SURVIVAL KIT LANYARD INSTALLED INCORRECTLY IN SLIDE RAFT AT L-1 DOOR. INSTALLED SURVIVAL KIT LANYARD CORRECTLY IN SLIDE RAFT AT L-1 DOOR.

Part: HINGE FITTING — CORRODED (RT MLG DOOR) · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - CORROSION ON HINGE FITTING OF RIGHT MAIN LANDING GEAR DOOR FORWARD POSITION -Y206. REPLACED HINGE FITTING OF RIGHT MAIN LANDING GEAR DOOR FORWARD POSITION -Y206 IAW A320 CMM 52-81-14.

Part: HINGE FITTING — CORRODED (LT MLG DOOR) · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - CORROSION ON HINGE FITTING OF LEFT MAIN LANDING GEAR DOOR FORWARD POSITION BETWEEN FR43 TO FR44, Y300. REPLACED HINGE FITTING OF LEFT MAIN LANDING GEAR DOOR FORWARD POSITION BETWEEN FR43 TO FR44, Y300 IAW A320 CMM 52-81-14.

Part: FITTING — CORRODED (FUSELAGE) · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - CORROSION ON FITTING AT FR58, S44, BL 0. REPLACED FITTING AT FR58, S44, BL 0 IAW A320 SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON CONNECTING SECTION FITTING AT FR68, -Y1162. REPLACED CONNECTING SECTION FITTING AT FR68, -Y1162 IAW A320 SRM 51-72-11.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON INNER SKIN BETWEEN FR68 TO FR70 & BETWEEN S22L TO S25L. REPAIRED INNER SKIN BETWEEN FR68 TO FR70 & BETWEEN S22L TO S25L IAW A320 SRM 53-41-11.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SPLICE AT FR37 + 5 INCHES, S44. REPLACED SPLICE AT FR37 + 5 INCHES, S44 IAW US AIRWAYS EA 132611.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - LEVEL 2 GALVANIC CORROSION ON SHEAR TIE CLEAT AT FR33, BETWEEN S43L TO S44L. REPLACED SHEAR TIE CLEAT AT FR33, BETWEEN S43L TO S44L IAW A320 SRM 51-72-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - C7 - LEVEL 2 - GALVANIC CORROSION ON SHEAR TIE CLEAT AT FR34, BETWEEN S42L TO S43L. REPLACED SHEAR TIE CLEAT AT FR34, BETWEEN S42L TO S43L IAW A320 SRM 51-72-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - LEVEL 2 - GALVANIC CORROSION ON SHEAR TIE CLEAT AT FR33, BETWEEN S42L TO S43L. REPLACED SHEAR TIE CLEAT AT FR33, BETWEEN S42L TO S43L IAW A320 SRM 51-72-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - LEVEL 2 - GALVANIC CORROSION ON SHEAR TIE CLEAT AT FR34, BETWEEN S39L TO S40L. REPLACED SHEAR TIE CLEAT AT FR34, BETWEEN S39L TO S40L IAW A320 SRM 51-72-11.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON STRINGER BETWEEN FR31 + 18 INCHES TO FR35, S44 IN FORWARD CARGO COMPARTMENT. REPAIRED STRINGER BETWEEN FR31 + 18 INCHES TO FR35, S44 IN FORWARD CARGO COMPARTMENT IAW A320 SRM 53-00-13.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - LEVEL 2 GALVANIC CORROSION ON SHEAR TIE CLEAT AT FR33, BETWEEN S42R TO S43R. REPLACED SHEAR TIE CLEAT AT FR33, BETWEEN S42R TO S43R IAW A320 SRM 51-72-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - LEVEL 2 - GALVANIC CORROSION ON SHEAR TIE CLEAT AT FR32, BETWEEN S41R TO S42R. REPLACED SHEAR TIE CLEAT AT FR32, BETWEEN S41R TO S42R IAW A320 SRM 51-72-11.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON STRINGER BETWEEN FR30 + 4 INCHES TO FR33 + 5 INCHES, S40L IN FORWARD CARGO COMPARTMENT. REPAIRED STRINGER BETWEEN FR31 + 18 INCHES TO FR35, S44L IN FORWARD CARGO COMPARTMENT IAW A320 SRM 53-00-13.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - LEVEL 2 - GALVANIC CORROSION ON SHEAR TIE CLEAT AT FR32, BETWEEN S43L TO S44L. REPLACED SHEAR TIE CLEAT AT FR32, BETWEEN S43L TO S44L IAW A320 SRM 51-72-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - LEVEL 2 - GALVANIC CORROSION ON SHEAR TIE CLEAT AT FR32, BETWEEN S42L TO S43L. REPLACED SHEAR TIE CLEAT AT FR32, BETWEEN S42L TO S43L IAW A320 SRM 51-72-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - LEVEL 2 - GALVANIC CORROSION ON SHEAR TIE CLEAT AT FR29, BETWEEN S43L TO S44L. REPLACED SHEAR TIE CLEAT AT FR29, BETWEEN S43L TO S44L IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON BEAM BETWEEN FR66 TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR70, -Y765 IAW A320 SRM 51-72-11.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - CORROSION ON WEB BETWEEN FR51 TO FR52, S38R IN AFT CARGO COMPARTMENT. REPLACED WEB BETWEEN FR51 TO FR52, S38R IAW A320 SRM 51-72-11.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LATERAL TRAY PLATE BETWEEN FR68 TO FR69, S23R. REPLACED LATERAL TRAY PLATE BETWEEN FR68 TO FR69, S23R IAW A320 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LATERAL SHEAR PLATE BETWEEN FR69 TO FR70, S23R. REPLACED LATERAL SHEAR PLATE BETWEEN FR69 TO FR70, S23R IAW A320 SRM 51-72-11 & US AIRWAYS EA 132603.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR68 TO FR70, S23L. REPLACED SHEAR PLATE BETWEEN FR68 TO FR70, S23L IAW A320 SRM 51-72-11 & US AIRWAYS EA 132603.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM SEAT RAIL BETWEEN FR64 TO FR66 + 5 INCHES, Y1292. REPLACED FLOORBEAM SEAT RAIL BETWEEN FR64 TO FR66 + 5 INCHES, Y1292 IAW A320 SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 63,365 hrs · 28,407 cycles

SAL - BC7 - MAJOR REPAIR - CRACK ON SHEAR PLATE BETWEEN FR68 TO FR69, Y1292. REPLACED SHEAR PLATE BETWEEN FR68 TO FR69, Y1292 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON BEAM BETWEEN FR68 TO FR69, -Y1292. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, -Y1292 IAW A320 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - CORROSION ON SHEAR PLATE BETWEEN FR50 TO FR51, S38R IN AFT CARGO COMPARTMENT. REPLACED SHEAR PLATE BETWEEN FR50 TO FR51, S38R IAW A320 SRM 51-72-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - LEVEL 2 - GALVANIC CORROSION ON SHEAR TIE CLEAT AT FR27, BETWEEN S41R TO S42R. REPLACED SHEAR TIE CLEAT AT FR27, BETWEEN S41R TO S42R IAW A320 SRM 51-72-11.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON STRINGER BETWEEN FR26 TO FR34, S42L. REPAIRED STRINGER BETWEEN FR26 TO FR34, S42L IAW A320 SRM 53-00-13.

Part: DAMPER — LOW PRESSURE (L2 DOOR) · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - EES - LOW PRESSURE CYLINDER DOOR DAMPER AT DOOR L-2. CHARGED THE DAMPER AND EMERGENCY OPERATION CYLINDER AT L-2 DOOR IAW A320 AMM 52-10-00.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SUPPORT FRAME LOWER SURFACE BETWEEN FR69 TO FR70, S23L. REPLACED SUPPORT FRAME LOWER SURFACE BETWEEN FR69 TO FR70, S23L IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - MAJOR REPAIR - LEVEL 2 - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5 TO FR67+16, Y1292. REPLACED FLOORBEAM BETWEEN FR66+5 TO FR67+16, Y1292 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON BEAM BETWEEN FR68 TO FR70, Y254. REPLACED FLOORBEAM BETWEEN FR68 TO FR70, Y254 IAW A320 SRM 51-72-11.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON STRINGER BETWEEN FR27 + 7 INCHES TO FR28 + 4 INCHES, S43L. REPAIRED STRINGER BETWEEN FR27 + 7 INCHES TO FR28 + 4 INCHES IAW A320 SRM 53-00-13.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION SEAT RAIL BEAM BETWEEN FR64 TO FR66, -Y765. REPLACED SEAT RAIL BEAM BETWEEN FR64 TO FR66, -Y765 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON BEAM BETWEEN FR66+5 TO FR70, Y765. REPLACED FLOORBEAM BETWEEN FR66+5 TO FR70, Y765 IAW A320 SRM 51-72-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - MAJOR REPAIR - LEVEL 2 - GALVANIC CORROSION ON SHEAR TIE CLEAT AT FR25, BETWEEN S41L TO S42L. REPLACED SHEAR TIE CLEAT AT FR25, BETWEEN S41L TO S42L IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 25,407 cycles

SAL - BC7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR 69 TO FR 70, Y520. REPLACED FLOORBEAM BETWEEN FR 69 TO FR 70, Y520 IAW B737 SRM 51-72-11.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON STRINGER BETWEEN FR28 + 9 INCHES TO FR34, S41L. REPAIRED STRINGER BETWEEN FR28 + 9 INCHES TO FR34, S41L IAW A320 SRM 53-00-13.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - LEVEL 2 - GALVANIC CORROSION ON SHEAR TIE CLEAT AT FR29, BETWEEN S42L TO S43L. REPLACED SHEAR TIE CLEAT AT FR29, BETWEEN S42L TO S43L IAW A320 SRM 51-72-11.

Part: DAMPER — LOW PRESSURE (L1 DOOR) · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - EES - LOW PRESSURE CYLINDER DOOR DAMPER AT DOOR L-1. CHARGED THE DAMPER AND EMERGENCY OPERATION CYLINDER AT L-1 DOOR IAW A320 AMM 52-10-00.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - LEVEL 2 - GALVANIC CORROSION ON SHEAR TIE CLEAT AT FR27, BETWEEN S42L TO S43L. REPLACED SHEAR TIE CLEAT AT FR27, BETWEEN S42L TO S43L IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON BEAM BETWEEN FR66+6 TO FR67+16, -Y1292. REPLACED FLOORBEAM BETWEEN FR66+6 TO FR67+16, -Y1292 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, Y1292. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, Y1292 IAW A320 SRM 51-72-11.

Part: SUPPORT FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 25,407 cycles

SAL - BC7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SUPPORT FRAME BETWEEN FR 69 TO FR 70, S23R. REPLACED SUPPORT FRAME BETWEEN FR 69 TO FR 70, S23R IAW A320 SRM 51-72-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - LEVEL 2 - GALVANIC CORROSION ON SHEAR TIE CLEAT AT FR27, BETWEEN S43L TO S44L. REPLACED SHEAR TIE CLEAT AT FR27, BETWEEN S43L TO S44L IAW A320 SRM 51-72-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - LEVEL 2 - GALVANIC CORROSION ON SHEAR TIE CLEAT AT FR26, BETWEEN S42L TO S43L. REPLACED SHEAR TIE CLEAT AT FR26, BETWEEN S42L TO S43L IAW A320 SRM 51-72-11.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON STRINGER BETWEEN FR29 TO FR35, S43L. REPAIRED STRINGER BETWEEN FR29 TO FR35, S43L IAW A320 SRM 53-00-13.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SEAT BEAM BETWEEN FR65 TO FR66, Y765. REPLACED FLOORBEAM BETWEEN FR65 TO FR66, Y765 IAW A320 SRM 51-72-11.

Part: DAMPER — LOW PRESSURE (R2 DOOR) · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - EES - LOW PRESSURE CYLINDER DOOR DAMPER AT DOOR R-2. CHARGED THE DAMPER AND EMERGENCY OPERATION CYLINDER AT R-2 DOOR IAW A320 AMM 52-10-00.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON STAMPING STRINGER BETWEEN AT FR28 TO FR29 & BETWEEN S42L TO S44L. REPLACED STAMPING STRINGER BETWEEN AT FR28 TO FR29 & BETWEEN S42L TO S44L IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON BEAM BETWEEN FR64 TO FR66, -Y512. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, -Y512 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR16 TO FR20, Y1292. REPLACED FLOORBEAM BETWEEN FR16 TO FR20, Y1292 IAW A320 SRM 51-72-11.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON WEB AT FR20, Y1675. REPLACED WEB AT FR20, Y1675 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,353 hrs · 28,407 cycles

SAL - BC7 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, Y1292. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, Y1292 IAW A320 SRM 51-72-11.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - CRACK IN FORWARD FLOOR STRUCTURE PANEL AT FR36, -Y1292. REPAIRED PRESSURE PANEL AT FR36, -Y1292 IAW US AIRWAYS JOB CARD M2C53307.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - CRACK IN FORWARD FLOOR STRUCTURE PANEL AT FR36, Y1292. REPAIRED PRESSURE PANEL AT FR36, Y1292 IAW US AIRWAYS JOB CARD M2C53307.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 63,320 hrs · 28,395 cycles

FLT 350 - LAS - EEL - LEFT OVERWING CABIN EMERGENCY POWER SUPPLY WILL NOT TEST OR POWER LIGHTS. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY UNIT 11WL AND BATTERY PER AIRBUS MAINTENANCE MANUAL 33-51-38.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 63,296 hrs · 28,382 cycles

LOG PAGE 8509354 - FLT 504-YVR - EEL - ROW 9D LOW LEVEL EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE RESET CIDS DIRECTOR PER AIRBUS MAINTENANCE MANUAL 23-73-00-440-001. SYSTEM OPERATIONAL CHECK WAS NORMAL.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,353 hrs · 28,407 cycles

SAL - BC-7 - MAJOR REPAIR - CRACK ON FITTING AT FR28 BETWEEN S37R TO S39R. REPLACED FITTING AT FR28 BETWEEN S37R TO S39R IAW A320 SRM 51-72-11.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 62,619 hrs · 28,089 cycles

LOG PAGE 8533300 - FLT 460-PHX - EEL - RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE FOUND SPADE CONNECTOR NOT HOOKED UP ON RIGHT OVERWING EXIT. RECONNECTED - OPERATIONAL CHECK GOOD.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 62,426 hrs · 27,994 cycles

FLT 350 - LAS - EMERGENCY EQUIPMENT - L1 DOOR ASSIST BOTTLE LOW PRESSURE (350 PSI). SERVICED BOTTLE AT L1 DOOR PER AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 62,369 hrs · 27,970 cycles

FLT 461 - IND-PHX - EMERGENCY EQUIPMENT - DOOR ASSIST BOTTLE LOW AT DOOR L-1. SERVICED BOTTLE TO LIMITS PER MAINTENANCE MANUAL 52-10-00.

Part: LIGHT — DETACHED (CABIN) · airframe 62,352 hrs · 27,963 cycles

FLT 350 - PHX-LAS - EMERGENCY LIGHTS - FLOOR PROXIMITY LIGHT AT SEAT 26L HOUSING NOT ATTACHED TO SEAT. RE-ATTACHED FLOOR PROXIMITY LIGHT HOUSING AT 26L.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 62,242 hrs · 27,902 cycles

FLT 612 - ATL - EMERGENCY EQUIPMENT - L-1 DOOR ACCUMULATOR LOW. SERVICED L-1 DOOR ACCUMULATOR TO REQUIRED LIMITS.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 62,011 hrs · 27,788 cycles

FLT 612 - ATL - EMERGENCY EQUIPMENT - L1 DOOR ASSIST BOTTLE LOW. MAINTENANCE SERVICED DOOR ASSIST BOTTLE.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 62,011 hrs · 27,788 cycles

FLT 612 - ATL - EMERGENCY EQUIPMENT - L2 DOOR ASSIST BOTTLE LOW. MAINTENANCE SERVICED DOOR ASSIST BOTTLE.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 61,946 hrs · 27,764 cycles

FLT 614 ATL - EMERGENCY EQUIPMENT - L-1 DOOR ASSIST BOTTLE LOW PRESSURE. MAINTENANCE SERVICED L-1 DOOR ASSIST BOTTLE PER AIRBUS MAINTENANCE MANUAL 52-10-00-614-051.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 61,752 hrs · 27,672 cycles

FLT 311 CLT-PHX - EMERGENCY EQUIPMENT - L1 DOOR ASSIST BOTTLE LOW. MAINTENANCE REPLACED DIAPHRAGM AND SERVICED L1 DOOR ASSIST BOTTLE. LEAK CHECK GOOD.

Part: DIAPHRAGM — DEFECTIVE (L1 DOOR) · airframe 61,752 hrs · 27,672 cycles

FLT 311 CLT-PHX - EMERGENCY EQUIPMENT - L1 DOOR ASSIST BOTTLE LOW. MAINTENANCE REPLACED DIAPHRAGM AND SERVICED L1 DOOR ASSIST BOTTLE. LEAK CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 61,688 hrs · 27,641 cycles

FLT 7 PHX-ORD - EMERGENCY EQUIPMENT - L1 DOOR ASSIST BOTTLE REQUIRES SERVICING. MAINTENANCE SERVICED L1 DOOR ASSIST BOTTLE PER AIRBUS MAINTENANCE MANUAL 52-10-00.

Part: CYLINDER — LOW (L1 DOOR) · airframe 61,573 hrs · 27,586 cycles

FLT 296 LAS-SEA - EMERGENCY EQUIPMENT - L1 DOOR ASSIST BOTTLE LOW PRESSURE. MAINTENANCE SERVICED THE L1 DOOR ASSIST BOTTLE AS REQUIRED.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 61,521 hrs · 27,564 cycles

EMERGENCY EQUIPMENT - L1 DOOR ASSIST BOTTLE LOW. MX SERVICED L1 DOOR ASSIST BOTTLE TO PROPER AMOUNT.

Part: SLIDE — LOW (R1 DOOR) · airframe 60,434 hrs · 27,051 cycles

LOG PAGE 4420739 - FLT NR 352 - PHX - EES -R-1 DOOR SLIDE/RAFT PRESSURE LOW (BELOW GREEN BAND). MAINTENANCE REMOVED AND REPLACED R-1 DOOR SLIDE/RAFT.

Part: CABLE — DEFECTIVE (ESCAPE SLIDE) · airframe 60,052 hrs · 26,870 cycles

PHX-FLT 504-OPERATIONAL TEST OF THE EMERGENCY SLIDE LIGHTS FAILED. MX REPLACED AFT LT SLIDE. VENDOR REPORT INDICATES THAT A DEFECTIVE CABLE ASSEMBLY CAUSED THE LIGHTS TO GO OFF AND ON. (S)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,551 hrs · 26,194 cycles

FLT NR 570 - LAS-PHX - EEL - RIGHT EMERGENCY POWER SUPPLY UNIT WILL NOT TEST. MAINTENANCE REMOVED AND REPLACED RIGHT EMERGENCY POWER SUPPLY UNIT PER AIRBUS MAINTENANCE MANUAL. OPERATIONAL CHECK WAS GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 58,405 hrs · 26,131 cycles

SAL - MAJOR REPAIR - C6 CHECK - CORROSION ON CABIN SEAT TRACK, BS 2403 / FR 52, +Y765. REPAIRED CABIN SEAT TRACK, BS 2403 / FR 52, +Y765 IAW A320 SRM 53-00-15 FIGURE 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 58,405 hrs · 26,131 cycles

SAL - MAJOR REPAIR - C6 CHECK - CORROSION ON CABIN SEAT RAIL, BS 2510 / FR 54, +Y765. REPAIRED CABIN SEAT RAIL, BS 2510 / FR 54, +Y765 IAW A320 SRM 53-00-15.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 58,072 hrs · 25,986 cycles

ATL - EEL - MX REPORTED EMERGENCY LIGHT AT ROW 9 AND 11 LT AND RT INOP. MX REPLACED THE RIGHT BATTERY. OPERATIONAL CHECK WAS GOOD.

Part: FUEL CONTROL — FAILED (NR 1 ENGINE) · airframe 54,511 hrs · 24,374 cycles

FLIGHT 430: PHL - LAS - DURING CRUISE AT FL340, ECAM MESSAGE. ENGINE NR 1 FUEL CONTROL FAULT APPEARED ON ECAM. NR 1 ENG THRUST HAD RETARDED TO IDLE, ALL OTHER PARAMETERS NORMAL. ECAM MESSAGE ENG FAIL APPEARED AND ENGINE SHUT DOWN. ACCOMPLISHED ENG NR 1 RELIGHT AT APPROXIMATELY FL220 AND REGAINED NORMAL THRUST CONTROL. THE CREW DIVERTED TO DTW. ENGINE OPERATED NORMAL DURING LANDING. FADAC INTERROGATION SHOWED BOTH CHANNELS OF FMU HAD FAULTED. MX REPLACED THE NR 1 FUEL-METERING UNIT. MX PERFORMED A POWER ASSURANCE RUN, OPS CHECK WAS GOOD. AIRMAN HAD ISSUED A FUP FOR TROUBLESHOOTING A SINGLE CHANNEL FMU PROBLEM. THE FUP WAS STILL OPEN WHEN EVENT OCCURRED.

Part: WIRE — OPEN (EMERGENCY LIGHT) · airframe 54,433 hrs · 24,342 cycles

PHX - EEL - ROW 9 RT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT INOP. RETERMINATED CONNECTORS FOR EMERGENCY ESCAPE PATH LIGHT AT ROW 9 RT PER ESPM 20-48-14. OPS CHECK WAS GOOD.

Part: REINFORCEMENT — CORRODED (FUSELAGEG) · airframe 53,039 hrs · 23,708 cycles

SAL - DURING C5 CHECK DISCOVERED CORROSION ON INTERNAL STRUCTURE, REINFORCEMENT PLATE, LOCATED BETWEEN FS 65 TO FS 66 AND BETWEEN STR 36L TO STR 42L. CORROSION LIMITS WERE NOT FOUND IN THE SRM. MAINTENANCE REMOVED AND INSTALLED NEW REINFORCEMENT PLATE LOCATED BETWEEN FS 65 TO FS 66 AND BETWEEN STR 36L TO STR 42L IAW AIRBUS 320 SRM 51-42-11 PARAGRAPH 6.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 53,039 hrs · 23,708 cycles

DURING C5 CHECK DISCOVERED CORROSION ON ANGLE LOCATED AT FR 71 + 1" ON THE LOWER LOBE FUSELAGE TAIL SECTION CAVITY, INTERIOR CUT OUT OF ACCESS DOOR NR 312AR. CORROSION WAS FOUND TO BE OUT OF LIMITS. ANGLE WAS REMOVED AND REPLACED IAW AIRBUS 320 SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 53,039 hrs · 23,708 cycles

SAL - DURING C5 CHECK DISCOVERED FLOORBOARD 261EF IN THE AFT GALLEY AREA WAS DELAMINATED. MAINTENANCE REMOVED AND INSTALLED NEW 261EF FLOOR BOARD.

Part: PLATE — CORRODED (FUSELAGE) · airframe 53,039 hrs · 23,708 cycles

SAL - DURING C5 CHECK DISCOVERED CORROSION ON PLATE LOCATED AT THE FORWARD CARGO DOOR CUT OUT UNDER THE LOWER SILL BETWEEN FS 25 AND FS 27 AT BL Y-765. NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE SRM. MAINTENANCE REMOVED AND INSTALLED REPLACEMENT PLATE AT THE FORWARD CARGO DOOR CUTOUT UNDER THE LOWER SILL BETWEEN FS 25 AND FS 27 AT BL Y-765 IAW AIRBUS 320 SRM 51-72-11 AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 53,039 hrs · 23,708 cycles

DURING C5 CHECK DISCOVERED CORROSION ON PASSENGER SEAT TRACK AT Y-765 AT FR 37+9". CORROSION WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED SEAT TRACK FROM FR 36 TO FR 41 AT Y-765 IAW AIRBUS 320 SRM 51-72-11 AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 53,039 hrs · 23,708 cycles

SAL - DURING C5 CHECK DISCOVERED CORROSION ON PASSENGER SEAT TRACK AT Y765 AND FR 46. REWORK WAS CONSIDERED OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 PAGE 102, FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK SECTION AT Y 765 AND FROM FR 41 TO FR 47 IAW AIRBUS 320 SRM 51-72-11 PAGE 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 53,039 hrs · 23,708 cycles

DURING C5 CHECK DISCOVERED CORROSION ON PASSENGER SEAT TRACK AT Y-765 AT FR44+10". CORROSION WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED SEAT TRACK FROM FR 41 TO FR 47 AT Y-765 IAW AIRBUS 320 SRM 51-72-11 PAGE 1 AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 53,039 hrs · 23,708 cycles

DURING C5 CHECK DISCOVERED CORROSION ON PASSENGER SEAT TRACK AT Y1292 AT FR45. CORROSION WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED SEAT TRACK FROM FR 41 TO FR 47 AT Y1292 IAW AIRBUS 320 SRM 51-72-11 AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 53,039 hrs · 23,708 cycles

DURING C5 CHECK DISCOVERED CORROSION ON PASSENGER SEAT TRACK AT Y1292 AT FR45. CORROSION WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED SEAT TRACK FROM FR 41 TO FR 47 AT Y1292 IAW AIRBUS 320 SRM 51-72-11 AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 53,039 hrs · 23,708 cycles

DURING C5 CHECK DISCOVERED CORROSION ON PASSENGER SEAT TRACK AT Y-1292 AT FR 45+18". CORROSION WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED SEAT TRACK FROM FR 41 TO FR 47 AT Y-1292 IAW AIRBUS 320 SRM 51-72-11 AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 53,039 hrs · 23,708 cycles

DURING C5 CHECK DISCOVERED CORROSION ON PASSENGER SEAT TRACK AT Y765 AT FR40+19". CORROSION WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED SEAT TRACK FROM FR 36 TO FR 41 AT Y765 IAW AIRBUS 320 SRM 51-72-11 PAGE 1 AND SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 44,615 hrs · 19,078 cycles

SAL - DURING C5 CHECK DISCOVERED FLOORBOARD 221AF IN THE FWD GALLEY AREA WAS DELAMINATED. MAINTENANCE REMOVED, FABRICATED AND INSTALLED NEW 221AF FLOORBOARD IAW IRM 9701 REV F.

Part: POWER SUPPLY — UNKNOWN (RT OVERWING) · airframe 52,737 hrs · 23,577 cycles

LAS - EEL - DURING OVERNIGHT INSPECTION MAINTENANCE REPORTED THAT THE EMERGENCY POWER SUPPLY UNIT AT THE RT OVERWING EXIT REQUIRED REPLACEMENT. REASON WAS NOT SPECIFIED. MAINTENANCE REPLACED THE RT OVERWING EMERGENCY EXIT POWER SUPPLY IAW AIRBUS 320 AMM 33-51-38-401. OPERATIONAL CHECKS WERE GOOD.

Part: RIB — CRACKED (NR 1 NACELLE) · airframe 52,574 hrs · 23,512 cycles

PHX - MAJOR REPAIR - NR 1 ENGINE, NR 14 RIB FOUND CRACKED DURING MAINTENANCE INSPECTION. MAINTENANCE IS CURRENTLY REPAIRING.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 51,998 hrs · 23,268 cycles

DTW - EEL - DURING INSPECTION DISCOVERED THE FORWARD F/A JUMSEAT INBOARD EMERGENCY FLASHLIGHT BATTERY DEAD. MAINTENANCE REMOVED AND REPLACED THE FORWARD F/A FLASHLIGHT BATTERY PACK IAW AIRBUS 320 MM 25-65-52. OPERATIONAL CHECKS WERE GOOD.

Part: WIRE — SHORTED (READING LIGHT) · airframe 47,539 hrs · 21,386 cycles

ARCHING / SMOKE, FLIGHT CREW REPORTED WIRES IN CAPTAINS SLIDING WINDOW POST CONNECTED TO READING LIGHT SHORED OUT WITH VISIBLE ARCHING AND SMOKE, A SMALL HOLE BURNED THROUGH PLASTIC COVER. MAINTENANCE PULLED AND COLLARED CAPTAINS READING LIGHT CIRCUIT BREAKER, ISSUED MEL 33-10-01, COND. 1 COCKPIT/INST PANEL LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED CAPTAINS READING LIGHT ON SLIDING WINDOW, OPERATIONAL CHECK GOOD.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 47,402 hrs · 21,321 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK A .375 INCH CRACK WAS FOUND ON FR 68 TO FLOORBEAM Y1792 LT CONNECTING SECTION. MAINTENANCE REMOVED CRACKED FLOORBEAM TO FRAME CONNECTING SECTION; FABRICATED A NEW REPLACEMENT CONNECTING SECTION PER DWG 17D53471087; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 47,402 hrs · 21,321 cycles

DURING C-04 CHECK FOUND 3 EACH DELAMINATED AREAS ON AFT CARGO FLOOR PANEL 151GF. MAINTENANCE REMOVED DELAMINATED FLOOR PANEL 151GF FROM Y765 LT TO Y765 RT, FR 53 TO FR 56; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER A320 SRM 53-02-00 FIG 209.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 47,402 hrs · 21,321 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK A 10 INCH CRACK WAS FOUND IN FLOOR PANEL 261PF. MAINTENANCE REMOVED CRACKED FLOOR PANEL BETWEEN FR 68 AND FR 70, Y1700 LT TO Y1700 RT; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG D53670051; INSTALLED REPAIR PART IAW A320 SRM 53-02-00 FIG 209.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FUSELAGE SKIN AT PORTABLE WATER SERVICING CUTOUT FR 65 TO FR 66, STR 37 LT TO STR 41 LT. MAINTENANCE REMOVED CORRODED REINFORCEMENT DOUBLER; FABRICATED A NEW REPLACEMENT REINFORCEMENT DOUBLER; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. **SUPP** REGISTRATION NUMBER AND TIMES HAVE BEEN CHANGED TO REFLECT THE CORRECT AIRCRAFT.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 47,402 hrs · 21,321 cycles

DURING C-04 CHECK CORROSION WAS FOUND ON SEAT TRACK Y1292 LT BETWEEN FR 36 AND FR 41. MAINTENANCE REMOVED CORRODED SEAT TRACK FROM FR 36 TO FR 41; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FUSELAGE SKIN AROUND WASTE SERVICE COMPARTMENT CUTOUT BETWEEN FR 65 & FR 66, STRINGERS 35 & 39 RT. MAINTENANCE REMOVED CORRODED REINFORCEMENT DOUBLER FROM FR 65 TO FR 66, AND STRINGERS 35 TO 39 RT; FABRICATED A NEW REPLACEMENT DOUBLER; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON R-2 DOOR SILL AT UPPER IB END BETWEEN FR 66 AND FR 68. MAINTENANCE CUTOUT DAMAGED AREAS OF R-2 DOOR SILL AT UPPER IB END, BOTH AT FR 68; FABRICATED A REPAIR DOUBLER AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14, FIG. 201.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y1292 LT BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CORRODED BEAM Y1292 LT FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON RAIL Y254 LT BETWEEN FR 16 AND FR 22. MAINTENANCE REMOVED DAMAGED RAIL Y254 LT FROM FR 16 TO FR 22; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL Y1203 RT AFT OF FR 15. MAINTENANCE REMOVED CORRODED DUMMY RAIL Y1203 RT AFT OF FR 15; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON L-2 DOOR SILL UPPER OUTBOARD SCUFF PLATE ATTACH FITTING BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED L-2 DOOR SHAPE SILL FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT SHAPE SILL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL Y81 RT BETWEEN FR 15 AND FR 16. MAINTENANCE REMOVED CORRODED RAIL Y81 RT FROM FR 12 TO FR 16; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON R-2 DOOR SILL UPPER OUTBOARD SCUFF PLATE ATTACH FITTING AT FR 67. MAINTENANCE REMOVED CORRODED R-2 DOOR SILL UPPER OUTBOARD SCUFF PLATE ATTACH FITTING AT FR 67; FABRICATED A NEW REPLACEMENT SHAPE SILL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON RT AFT WEB SHEAR PLATE BETWEEN FR 69 AND FR 70, AFT AND OUTBOARD OF BEAM Y1292 RT. MAINTENANCE REMOVED CORRODED SHEAR PLATE FROM FR 69 TO FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: WEB — CORRODED (FUSLAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON WEB Y1546 RT AT FR 16. MAINTENANCE REMOVED AND REPLACED DAMAGED WEB Y1546 RT AT FR 16 IAW A320 SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 47,402 hrs · 21,321 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK A 1.5 INCH CRACK WAS FOUND IN LT AFT SHEAR PLATE (TRAY) ON AFT SIDE OF L-2 DOOR, OUTBOARD OF BEAM Y1292 LT. MAINTENANCE REMOVED CRACKED LT AFT SHEAR PLATE ON AFT SIDE OF L-2 DOOR, OUTBOARD OF BEAM Y1292 LT; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y1292 RT AT FR 20. MAINTENANCE REMOVED CORRODED SEAT TRACK Y1292 RT AT FR 20; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL BETWEEN FR 14 AND FR 16. MAINTENANCE REMOVED CORRODED DUMMY RAIL FROM FR 12 TO FR 16; FABRICATED A NEW REPLACEMENT SECTION OF DUMMY RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · airframe 47,402 hrs · 21,321 cycles

DURING C-04 CHECK CORROSION WAS FOUND ON L-2 DOOR SILL, AT UPPER INBOARD END BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED L-2 DOOR SILL FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT SILL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON WEB Y1292 LT BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED CORRODED WEB Y1292 LT FROM FR 69 TO FR 70; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y765 AT FR 20. MAINTENANCE REMOVED CORRODED SEAT TRACK Y765 AT FR 20; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 47,402 hrs · 21,321 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON SEAT TRACK Y765 LT BETWEEN FR 20 AND FR 24. MAINTENANCE REMOVED CORRODED SEAT TRACK Y765 LT FROM FR 20 TO FR 24; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y1292 LT AFT OF FR 66 TO FORWARD SIDE OF FR 68. MAINTENANCE REMOVED CORRODED BEAM Y1292 LT FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT RAIL Y254 RT BETWEEN FR 16 AND FR 20. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT RAIL Y254 RT FROM FR 16 TO FR 23; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL Y917 LT AFT SIDE OF FR 66. MAINTENANCE REMOVED CORRODED RAIL Y917 LT AFT SIDE OF FR 66; RECEIVED AND INSTALLED NEW REPLACEMENT RAIL IAW A320 SRM 51-72-11.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON WEB Y1546 RT AT FR 20. MAINTENANCE REMOVED CORRODED WEB Y1546 RT AT FR 20; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL WEB. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT DOOR SILL WEB AT WL -Z1500, FROM FR 53 TO FR 56; FABRICATED A NEW REPLACEMENT DOOR SILL WEB; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL Y189 BETWEEN FR 20 AND FR 23. MAINTENANCE REMOVED CORRODED RAIL Y189 FROM FR 20 TO FR 23; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT AT FORWARD END OF FR 20. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 RT AT FR 20 IAW A320 SRM 51-42-11 FIG 8, 9 & 12.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LONGITUDINAL BEAM ASSEMBLY Y460 RT AFT OF FR 66. MAINTENANCE REMOVED CORRODED LONGITUDINAL BEAM ASSEMBLY Y460 RT AFT OF FR 66; FABRICATED A NEW REPLACEMENT BEAM ASSEMBLY; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,402 hrs · 21,321 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL PLATE BETWEEN FR 53 AND FR 56. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT DOOR SILL PLATE FROM FR 53 TO FR 56; FABRICATED A NEW REPLACEMENT SILL PLATE PER DWG D53475575; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: CYLINDER — LEAKING (L-1 DOOR) · airframe 47,402 hrs · 21,321 cycles

DURING C-04 CHECK, THE L-1 DOOR DAMPER WAS FOUND LEAKING. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR DAMPER ASSEMBLY IAW AMM 52-11-14-04.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,402 hrs · 21,321 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON SKIN AT IFPC FORWARD ANTENNA CUTOUT BETWEEN FR 60 AND FR 61. MAINTENANCE BLENDED OUT CORROSION ON SKIN AT IFPC FORWARD ANTENNA CUTOUT; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW A320 SRM 53-00-11 FIG 203.

Part: FLASHLIGHT — INOPERATIVE (ZONE 900) · airframe 45,524 hrs · 20,563 cycles

SEA - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.

Part: SOLENOID VALVE — LEAKING (ZONE 140) · airframe 45,418 hrs · 20,514 cycles

ORD - ABORTED TAKEOFF - FLT 0654 - ON TAKEOFF AT ORD EN ROUTE FOR PHX RECEIVED YELLOW HYDRAULIC RESERVOIR LOW LEVEL INDICATION WITH ASSOCIATED BRAKE, ANTI-SKID, AND NOSE WHEEL STEERING FAULTS ON UPPER ECAM, REJECTED TAKEOFF BELOW 80 KTS. MAINTENANCE FOUND FLUID LEAKING FROM A CRACK IN THE POWER TRANSFER UNIT SOLENOID VALVE (1012GL) (2 WAY VALVE). REPLACED CRACKED VALVE IAW AMM 29-23-51-401. SERVICED YELLOW HYDRAULIC SYSTEM AND PERFORMED ENGINE RUN, OPERATIONAL AND LEAK CHECKS WERE GOOD. FUNCTIONAL TEST OF POWER TRANSFER UNIT SOLENOID VALVE S/N 0141 CONFIRMED FAILURE OF UNIT FOR INTERMITTENT OPENING AND CLOSING. REPLACED SEAL'S, O-RINGS, AND BACK UP RINGS, UNIT REPAIRED IAW CMM 29-10-12.

Part: ACTUATOR — FAULTY (ZONE 190) · airframe 45,090 hrs · 20,382 cycles

ON CLIMBOUT, EN ROUTE, WHEN MLG SELECTED UP, RECEIVED ECAM MESSAGE THAT MLG DOORS WERE NOT CLOSED. RECYCLED MLG & NEW ECAM MESSAGE APPEARED FOR MLG NOT UPLOCKED, LOWERED MLG & RETURNED. MAINT PULLED UP PREFLT REPORT MLG NOT UPLOCKED. FAILURE MESSAGE RT MLG DOOR OPEN PROX SENSOR 34GA TARGET POSITION, & 32GA. MAINT ADJUSTED BOTH 32GA & 34GA PROX SENSORS, R & R RT MLG DOOR ACTUATOR IAW AMM 32-31-35-401, OPS & LEAK CHECK GOOD. VENDORS FUNCTIONAL TEST OF RT MLG DOOR ACTUATOR S/N DH070399 WAS NO FAULT FOUND. VISUAL INSPECTION DID FIND 2 EACH BEARINGS MIGRATED LOOSE, R & R 2 EACH BEARINGS IAW CMM 32-31-35, REV. 12.

Part: CONNECTOR — BROKEN (SEAT ROW 15 L/H) · airframe 44,617 hrs · 20,208 cycles

PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 15 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED CANNON PLUG AT BULKHEAD SEAT ROW 15 LT, OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — FAILED (ZONE 221) · airframe 44,184 hrs · 20,042 cycles

DURING FUNCTIONAL CHECK OF EMERGENCY LIGHT SYSTEM THE FORWARD L/H EMERGENCY POWER SUPPLY UNIT FAILED TEST FOR EXTERNAL LOADS FORWARD LEFT AND COMM FORWARD LEFT MESSAGES ON CIDS PANEL. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (11WL), FUNCTIONAL CHECK OF SYSTEM WAS GOOD.

Part: SERVO VALVE — FAULTY (NLG STEERING) · airframe 43,633 hrs · 19,824 cycles

ON TAKEOFF PILOT REPORTED A NOSE WHEEL STEERING FAULT. AIRCRAFT PROCEEDED AFTER WHICH AN UNEVENTFUL LANDING OCCURED. AIRCRAFT TAXIED TO GATE UNDER ITS OWN POWER. MECHANIC PERFORMED BSCU BITE CHECKS THAT IDENTIFIED FAULT CODE 4E. REMOVED AND REPLACED THE NOSE LANDING GEAR SERVO CONTROL VALVE IAW AMM 32-51-51-04. OPERATIONAL AND LEAK CHECK WERE GOOD. VENDOR BENCH TEST OF NOSE LANDING GEAR SERVO CONTROL VALVE S/N M075 COULD NOT CONFIRM REASON FOR REMOVAL (NFF). UNIT WAS TESTED, INSPECTED, AND RETURNED TO SERVICE IAW CMM 32-57-01.

Part: TRANSMITTER — DEFECTIVE (INSTRUMENT PANEL) · airframe 43,318 hrs · 19,695 cycles

STEERING FAILURE - BSCU 1 FAULT ON TAXI AIRCRAFT COULD NOT BE STEERED WITH RUDDER PEDALS OR TILLER. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS N/W/S HAND WHEEL TRANSMITTER UNIT (1GC) IAW AMM 32-51-11-401, OPERATIONAL CHECK WAS GOOD. VENDOR TEARDOWN REPORT OF NOSE WHEEL STEERING CONTROLLER S/N 188 CONFIRMED FAILURE OF UNIT. MICRO SWITCH (P/N TS116067) WAS FOUND INTERMITTENT, AND THE PLATE DRIVE, MAIN SPRING (P/N TS116022-4), AND RINGS (P/N TS116095-3) WERE FOUND WORN BEYOND LIMITS. UNIT WAS OVERHAULED PER CMM 32-51-11.

Part: WIRE — BROKEN (ESCAPE SLIDE) · airframe 43,090 hrs · 19,603 cycles

DURING C-03 CHECK THE LT EMERGENCY ESCAPE SLIDE ARMED LIGHT WOULD NOT COME ON WITH THE FORWARD OR AFT OVER WING EXIT DOOR HANDLES OPEN AND BOTH EXITS ARMED. MAINTENANCE TROUBLESHOT SYSTEM USING A320 ASM 52-73-00 AND FOUND A WIRE BROKEN AT TERMINAL A OF LT EMERGENCY EXIT SLIDE ARMED CONNECTOR (2WN2). RE-TERMINATED WIRE IAW ESPM 20-48-21, PG. 12-22. OPERATIONAL CHECK WAS GOOD IAW AMM TASK 52-73-00-710-002.

Part: WIRE HARNESS — SHORTED (SEAT ROW 13) · airframe 43,090 hrs · 19,603 cycles

MCN - EEL - DURING C-03 CHECK THE EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 13 LT READS OPEN. MAINTENANCE REPAIRED EMERGENCY ESCAPE PATH LIGHT WIRING AT SEAT ROW 13 LT IAW ESPM 20-48-14, PG 12-13, OPERATIONAL CHECK WAS GOOD.

Part: WIRE — BROKEN (SEAT ROW 7) · airframe 43,090 hrs · 19,603 cycles

MCN - EEL - DURING C-03 CHECK THE EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 7 LT READS OPEN. MAINTENANCE SPLICED BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 7 LT IAW ESPM 20-43-11 PG 9, OPERATIONAL CHECK WAS GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,874 hrs · 19,517 cycles

MCN - MAJOR REPAIR - DURING C-03 CHECK A .0625 INCH CRACK WAS FOUND AT THE FIFTH FASTENER HOLE DOWN ON FRAME 39, STR 14 LT. MAINTENANCE CUT OUT DAMAGED SECTION OF FRAME 39 AT STR 14 LT; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW AWA EO 53-14-20 FIG 3R.

Part: FITTING — BROKEN (R1 DOOR) · airframe 43,090 hrs · 19,603 cycles

MCN - EES - DURING C-03 CHECK THE R-1 DOOR REDUCER SHAFT MECHANISM RIG PIN FITTING WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE R-1 DOOR REDUCER SHAFT MECHANISM RIG PIN FITTING PER AIRBUS INDUSTRIES CMM 52-11-15, PG. 319, 745, FIG. 308.

Part: INDICATOR — FALSE INDICATION (DOOR BOTTLE) · airframe 42,874 hrs · 19,517 cycles

MCN - EES - DURING C-03 CHECK THE L-2 DOOR ASSIST CYLINDER GAUGE READ 400 PSI WITH ZERO PRESSURE IN CYLINDER. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR DAMPER EMERGENCY OPERATION CYLINDER IAW AMM TASK 52-13-14-000-001, AND TASK 52-13-14-400-001.

Part: PANEL — CRACKED (LT PYLON) · airframe 42,874 hrs · 19,517 cycles

MCN - MAJOR REPAIR - DURING C-03 CHECK A 1.25 INCH CRACK WAS FOUND ON LT PYLON INBOARD SIDE AT FORWARD UPPER CORNER OF PANEL 414CR ATTACH POINT, STA 537. MAINTENANCE CUT OUT DAMAGED SECTION OF EXTRUSION PROFILE AT PYLON STA 537; FABRICATED A FILLER AND REPAIR SPLICE; INSTALLED REPAIR PART IAW A320 SRM 54-52-12 PG 215-220 FIG 203.

Part: PRESSURE SWITCH — FAULTY (NR 1 ENGINE) · airframe 42,670 hrs · 19,438 cycles

ON CLIMB OUT FROM PHX EN ROUTE FOR BDL THE NR 1 ENGINE DRIVEN (GREEN) HYDRAULIC PUMP FAILED. TURNED BACK TO PHX, TOUCHED DOWN AT 144,000 LBS AT LESS THAN 100 FPM. MAINTENANCE TROUBLESHOT AND FOUND GREEN HYDRAULIC SYSTEM PRESSURE SWITCH (1074GK) DEFECTIVE. REMOVED AND REPLACED PRESSURE SWITCH (1074GK) IAW AMM 29-11-17-04. OPERATIONAL CHECK OF GREEN HYDRAULIC SYSTEM WAS GOOD.

Part: O-RING — DETERIORATED (ZONE 140) · corrosion level 0 · airframe 39,853 hrs · 18,324 cycles

LAS - DIVERSION - FLT 0470 - EN ROUTE FROM PHX TO BUR ECAM INDICATED YELLOW HYDRAULIC SYSTEM LOW QUANTITY, AIRCRAFT DIVERTED TO LAS. MAINTENANCE FOUND HYDRAULIC LEAK AT QUICK DISCONNECT (3701GM) ON YELLOW HYDRAULIC SYSTEM MAIN POWER MODULE, REMOVED AND REPLACED DETERIORATED O-RING AT QUICK DISCONNECT, OPERATIONAL AND LEAK CHECK COMPLIED WITH IAW AMM 20-29-00-911-002.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 36,698 hrs · 17,081 cycles

PHX - 4/5/01 - DURING MAINTENANCE OPERATIONAL CHECK ESCAPE PATH LIGHTS AT SEAT ROW 3L, 7L & 26L AS WELL AS OVERHEAD LIGHT AT 11L FAILED TO ILLUMINATE. THE EMERGENCY LIGHT POWER SUPPLY UNIT AT POSITION NR 4 WAS REPLACED AND FUNCTIONAL CHECKS WERE GOOD.

Part: ACTUATOR — LEAKING (YAW DAMPNER) · airframe 36,666 hrs · 17,071 cycles

D: PHX - AIR TURNBACK - 3/31/01 - EN ROUTE FROM PHX TO BOS THE AIRCRAFT LOST GREEN HYDRAULIC SYSTEM QUANTITY AND RETURNED TO PHX MAKING AN UNEVENTFUL LANDING. MAINTENANCE FOUND THE LT YAW DAMP SERVO ACTUATOR LEAKING AT THE OUTPUT SHAFT; THE SERVO ACTUATOR WAS REPLACED; LEAK CHECKS AND OPERATIONAL CHECKS WERE GOOD.

Part: COMPUTER — FAILED (E/E BAY) · airframe 34,370 hrs · 16,183 cycles

AIR TURNBACK - NORTH OF ICT, AFTER NR 1 IR FAULT, CAPTAINS PFD WENT BLANK AND NR 1 AUTO PILOT DISCONNECTED WITH A THRUST LOCK. REGAINED PFD APPROX 2 - 3 SEC LATER. REMOVED AND REPLACED FLIGHT AUGMENTATION COMPUTER.

Part: TRANSMITTER — LEAKING (NR 2 HYD PUMP) · airframe 33,988 hrs · 16,052 cycles

DECLARED EMERGENCY, YELLOW HYDRAULIC RESERVOIR LOW LEVEL/PRESSURE DISPLAYED RESERVOIR LEVEL EMPTY. FOUND NR 2 ENG HYD PUMP PRESSURE TRANSMITTER CRACKED AT HYD LINE CONNECTION. REMOVED AND REPLACED TRANSMITTER, LEAK AND OPS CK GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,141 hrs · 15,720 cycles

NON-ROUTINE LINE, CORROSION. FWD RT WIND SCREEN FLOOR TRACKS BETWEEN FR 20 AND FR 24, Y 765 CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACKS IAW A320 SRM 51-72-11, DUMMY RAIL IAW A320 SRM 51-72-16. PRIMED AND PAINTED REWORK AREA IAW A320 SRM 51-70-00.

Part: ENGINE — FAILED (NR 2)

WENT TO CLIMB THRUST AND NOTICED MILD VIBRATION AT 22500 FT, NR 2 ENGINE SURGED AND COMPRESSOR STALLED. REPLACED NR 2 ENGINE. NO DIRECTLY RELATED HISTORY.

Part: ENGINE — FAILED (NR 1)

EMERGENCY LANDING, ENG SHUTDOWN IN FLT NR 1 ENGINE FAILED AT FL 310. DIVERTED TO ICT FOLLOWED ALL ECAM ACTIONS. REMOVED AND REPLACED NR 1 ENG PER CARD R5M71302 & F5M71301, OPS AND LEAK CHECK GOOD. TT 0023326.

Part: BATTERY — DISCHARGED (CABIN)

NORMAL OPS, EXIT LIGHTS NOT ILLUMINATING. EXIT LIGHT ON BOTH FORWARD DOORS NOT ILLUMINATED. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-00. SYSTEM OPS CHECKED NORMALLY ON THE GROUND. BATTERY IS EXPENDABLE; NO SERIALIZED DATA.

Part: FLOORBEAM — CORRODED (BS 189)

FWD CABIN FLOORBEAM AT Y189 RT UPPER FLANGE CORRODED BEYOND SRM LIMITS FRAME 21 TO FRAME 22. FLOORBEAM REMOVED, FABRICATED NEW DUMMY RAIL PER DWG D53112836, SPLICED NEW DUMMY RAIL TO EXISTING STRUCTURE PER SRM 53-11-14. SURROUNDING STRUCTURE TREATED AND PRIMED.

Part: FLOORBEAM — CORRODED (BS 254)

FWD CABIN FLOORBEAM AT Y254 RT SURFACE CORRODED BEYOND SRM LIMITS FRAME 12 TO FRAME 16. FLOORBEAM REMOVED, FABRICATED NEW FLOORBEAM AS PER DWG D53112836, SPLICED NEW FLOORBEAM TO EXISTING STRUCTURE AS PER SRM 53-11-14. SURROUNDING STRUCTURE TREATED AND PRIMED.

Part: FRAME — BENT (FUSELAGE)

FWD CARGO FLOOR FRAME AT FRAME 31, STR 39, LT RIVETS SHEARED AND FRAME BENT. FABRICATED NEW ANGLE PER DWG 59511600202 AND SRM 51-22-11, ANCHOR NUTS REPLACED AND STRUCTURAL AREA RIVETED PER SRM 51-72-11 & 51-73-00.

Part: SEAT TRACK — CORRODED (CABIN)

CABIN SEAT TRACK NR 3 FRAME 20 CORRODED BEYOND SRM LIMITS. TRACK REMOVED, FABRICATED NEW TRACK PER DRAWING D53112092, SPLICED NEW SEAT TRACK INTO EXISTING STRUCTURE PER SRM 53-11-14. SURROUNDING STRUCTURE TREATED AND PRIMED.

Part: SEAT TRACK — CORRODED (CABIN)

CABIN SEAT TRACK NR 4 FRAME 20 CORRODED BEYOND SRM LIMITS. SEAT TRACK REMOVED, FABRICATED NEW TRACK PER DRAWING D53112092, SPLICED NEW SEAT TRACK INTO EXISTING STRUCTURE PER SRM 53-11-14. SURROUNDING STRUCTURE TREATED AND PRIMED.

Part: CONNECTOR — BROKEN (CABIN)

INTERIOR EMERGENCY AISLE LIGHT INOP AT SEAT ROW 15. REPAIRED CONNECTOR AT ROW 15 WALL DISCONNECT, OPS OK.

Part: FUSE — BLOWN (CABIN)

OVERWING EXIT HANDLE COVER LIGHTS DO NOT WORK. A/C RT FWD AND AFT RELAMP, NO HELP. REPLACED FUSE ON EMERGENCY LIGHT PWR PACK.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED LT OVERWING BATTERY PACK, OPS CHECK GOOD.

Part: HYD SYST — REQD SERVICE (GREEN HYD SYST)

GREEN SYSTEM HYDRAULIC LOW QUANTITY. LANDING GEAR EXTENDED USING ECAM AND QRH PROCEDURES. EMERGENCY LANDING WAS DECLARED. GREEN SYSTEM FLUID QUANTITY INCREASED AND GREEN SYSTEM WAS RESTORED FOR A NORMAL LANDING. SERVICED ALL 3 HYDRAULIC SYSTEMS TO CORRRECT LEVELS. LEAK AND SYSTEM CHECKS GOOD.

Part: ENGINE — OVERTEMP (NR 1)

SHUTDOWN ENGINE NR 1 DUE TO OVERTEMP/BLEED VALVE HI AND LO OPEN. ACCOMPLISHED BORESCOPE INSPECTION PER MM 72-00-00, PAGE 258. NO ABNORMALITIES NOTED. ENGINE NR 2 FUEL FAULT ON SHUTDOWN NOTED BY MX. BITE TEST OK. REMOVED AND REPLACED NR 1 ENGINE.

Part: CONNECTOR — DISCONNECTED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND AFT SEAT EMERGENCY EXIT LIGHT INOP. REPINNED CANNON PLUG AT SIDEWALL, OPS CHECK GOOD.

Part: AIR DISTRIBUTION — ODOR (COCKPIT)

ON FINAL APPROACH TO PHOENIX, EXPERIENCED A STRONG ELECTRICAL SMELL. THERE WERE NO INDICATIONS OF A FAILURE. ODOR LOCALIZED IN THE COCKPIT. CHECKED EQUIPMENT BAYS FOR EVIDENCE OF BURNT WIRING AND ODOR. NO DISCREPANCIES NOTED. COULD NOT DUPLICATE ELECTRICAL SMELL.

Part: BATTERY — DISCHARGED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND RED EMERGENCY EXIT LIGHT, ON SEATS BY OVERWING EXITS, ARE INOP. REMOVED AND REPLACED BATTERY PACK AT POWER SUPPLY 12WL. OPS CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND RIGHT OVERWING EMERGENCY BATTERY PACK FAILS SELF TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS TEST GOOD.

Part: BATTERY — DISCHARGED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND MID-CABIN RT SIDE EMERGENCY LIGHT TEST FAILED. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY IN MID-CABIN. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND RT MID EMERGENCY BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD.

Part: LIGHTS — MALFUNCTIONED (CABIN)

PHX - FLT 583 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS IN CABIN ON WITH AC ELECT NORMAL AND SWITCH IN ARMED POSITION. CYCLED EMERGENCY LIGHT SWITCH TO ON THE BACK TO OFF. LIGHT OPERATIONS CHECK GOOD. NO FAULTS NOTED. (M)

Part: DEU — FAILED (NR 4)

CHM - FLT 0651 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTING ON WITHOUT POWER FAILURE AT SW COMMAND. RESETS OK. REMOVED AND REPLACED DEU (DECODER ENCODER UNIT) 100RH1. OPS CHECK GOOD. PART TOTAL CYCLES, 8,893. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

PHX\SNA - FLT 0657 - EMERGENCY LIGHTING ALL CAME ON IN CABIN DURING TAXI AND IN-FLIGHT. RESET WHEN EMERGENCY EXIT LIGHT SWITCH IS CYCLED ON AND OFF. REMOVED AND REPLACED LEFT AFT BATTERY PACK. OPERATIONS CHECK IS GOOD. (X)

Part: BATTERY — DISCHARGED (CABIN)

LAS - FLT NR 85 - DURING ROUTINE MAINTENANCE CHECK, FOUND MISCELLANEOUS EMERGENCY LIGHTS IN AFT INOP. REMOVED AND REPLACED EMERGENCY PACK, PACK CHECKS GOOD. REMOVED AND REPLACED BATTERY ON AFT POWER SUPPLY, CHECKS GOOD. REFERENCE AWXA960057.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

LAS - FLT NR 85 - DURING ROUTINE MAINTENANCE CHECK, FOUND MISCELLANEOUS EMERGENCY LIGHTS IN AFT INOP. REMOVED AND REPLACED EMERGENCY PACK, PACK CHECKS GOOD. REMOVED AND REPLACED BATTERY ON AFT POWER SUPPLY, CHECKS GOOD. (M)

Part: WASTE LVL TRANS — MALFUNCTIONED (LAV SYSTEM)

MCI - FLT 264 - CMH-PHX - AIRCRAFT DIVERTED TO MCI DUE TO FAILURE OF ALL LAVS TO FLUSH. MCI RAMP PERSONNEL SERVICED LAVS. AIRCRAFT DEPARTED MCI AND SYSTEM FAILED AGAIN. PHX MAINTENANCE DISCONNECTED WASTE LEVEL TRANSMITTER. SYSTEM OPS CHECK OK. TRANSMITTER PLACED ON ORDER. AIRCRAFT RETURNED TO SERVICE. (M)

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, L1 DOOR AND LEFT BATTERY PACK FAILED TEST. REMOVED AND REPLACED LEFT BATTERY PACK, OPS CHECK GOOD. (M)

Part: EEL BATT PACK — DISCHARGED (CABIN)

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

Part: ACM — SEIZED (NR 2 PACK)

PHX\CMH - FLT 266 - DURING CLIMB OUT, NR 2 PACK FAILED. PILOT STATED THAT PRIOR TO PACK FAIL A STRONG BURNING PLASTIC ODOR WAS NOTICED, BUT DISAPPEARED AFTER PACK SHUT DOWN. PILOT ELECTED TO RETURN TO PHX DUE TO ALTITUTDE RESTRICTION, LANDING WITHOUT FURTHER INCIDENT. OVERWEIGHT LANDING WAS ACCOMPLISHED PER AMM 5 51 11, PAGE 601. NO ACTION REQUIRED. MAINTENANCE FOUND ACM TO BE SEIZED. REMOVED AND REPLACED ACM PER AMM 21 52 21. OPS CHECK AND LEAK CHECK, COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE. (X)

Part: EEL BATT PACK — DISCHARGED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, LT AFT EMERGENCY BATTERY PACK FAILED TEST ON WEEKLY CHECK. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (Z)

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

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

Part: EEL BATTERY PACK — FAILED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, LT COMMON EMERGENCY EXIT LIGHT BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (W)

Part: BATTERY PACK — INOPERATIVE (CABIN EEL)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND A SECTION OF EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (X)

Part: AEVC — MALFUNCTION (CABIN)

AIR TURNBACK, ON CLIMB-OUT RECEIVED ECAM MESSAGE 'VENT SKIN VALVE FAULT'. CREW COULD NOT MAINTAIN CABIN PRESSURE. AIRCRAFT RETURNED TO LAS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND 'AVNC VENT' CNT CIRCUIT BREAKER OUT. RESET CIRCUIT BREAKER D7. SYSTEM TEST WAS OK. REPLACED AEVC AS PRECAUTIONARY PER AMM 21-26-34. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (W)

Part: SENSOR — INOPERATIVE (RT MLG DOOR)

PHX-MKE - FLT 1956 - AIR TURNBACK - RIGHT MAIN GEAR DOOR DID NOT INDICATE UP AND LOCKED. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE FOUND RT GEAR DOOR PROXIMITY SENSOR '26GA' INTERMITTENT. MAINTENANCE REMOVED AND REPLACED NR 2 RT MLG DOOR UPLOCK PROXIMITY SWITCH PER MM 32-31-73. PERFORMED NR 1 AND NR 2 LGCIU BITE TEST, BOTH SYSTEMS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (Z)