N814AW

Part: POWER SUPPLY — FAULTY (ZONE 200) · airframe 75,217 hrs · 35,954 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN EMERGENCY LIGHTING SYSTEM, CIDS FAULT EPSU FWD LEFT BATTERY POWER SUPPLY. MAINTENANCE REPLACED FORWARD LEFT EPSU IAW AMM 33-51-38.

Part: POWER SUPPLY — FAULTED (ZONE 200) · airframe 75,217 hrs · 35,954 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN EMERGENCY LIGHTING SYSTEM, CIDS FAULT EPSU AFT LEFT BATTERY POWER SUPPLY. MAINTENANCE REPLACED FORWARD LEFT EPSU IAW AMM 33-51-38.

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 75,136 hrs · 35,896 cycles

AIRCRAFT WAS NOT GROUNDED: DURING ACCOMPLISHMENT OF PS CHECK, FOUND LH WALL OVERWING EMERGENCY EXIT SIGN WITH 2 LED LIGHTS INOP. MAINTENANCE REPLACED LH EXIT SIGN LED PANEL AT LH WALL OVERWING EMERGENCY DOOR, IAW AMM 33-51-16.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 75,136 hrs · 35,896 cycles

AIRCRAFT WAS NOT GROUNDED: DURING ACCOMPLISHMENT OF PS CHECK, FOUND R/H WALL OVERWING EMERGENCY EXIT LIGHT WITH 5 LEDS INOP. MAINTENANCE REPLACED LED PANEL ASSEMBLY IAW AMM 33-51-16.

Part: BULB — BURNED OUT (ZONE 200) · airframe 73,590 hrs · 34,885 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT SIGN AT R/H OVERWING DOOR HAS 7 BULBS BURNED OUT. MAINTENANCE REPLACED BURNED OUT BULBS IAW AMM 33-51-16.

Part: BULB — BURNED OUT (ZONE 200) · airframe 73,590 hrs · 34,885 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT SIGN BEHIND ROW 27 ON THE CEILING HAS 5 BULBS INOP. MAINTENANCE REPLACED BURNED OUT BULBS IAW AMM 33-51-16.

Part: BULB — BURNED OUT (ZONE 200) · airframe 73,590 hrs · 34,885 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT SIGN ABOVE R2 DOOR HAS A BULB BURNED OUT. MAINTENANCE REPLACED BURNED OUT BULB IAW AMM 33-51-16.

Part: BOTTLE — INOPERATIVE (DOOR ASSIST) · airframe 73,484 hrs · 34,805 cycles

AIRCRAFT WAS GROUNDED: L2 DOOR DOES NOT OPEN FULLY. GUST LOCK CANNOT ENGAGE BECAUSE THE DOOR WON'T FULLY OPEN. MAINTENANCE REPLACED EMERGENCY OPERATION CYLINDER IAW AMM 52-13-14-400-001B.

Part: BATTERY — DISCHARGED (ZONE 200) · airframe 73,469 hrs · 34,797 cycles

AIRCRAFT WAS NOT GROUNDED: FA REPORT FLASHLIGHT INBOARD JUMPSEAT NOT FLASHING RED LIGHT. MAINTENANCE REPLACED FWD JUMPSEAT I/B FLASH LIGHT BATTERY.

Part: ENGINE — FAILED (NR 2) · airframe 72,985 hrs · 34,481 cycles

AIRCRAFT WAS GROUNDED: - DIVERTED TO IAD DUE TO ENG 2 STALL AND ENG 2 FAIL (ENG SHUTDOWN). A/C DIVERTED TO IAD AND LANDED UNEVENTFULLY. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: ENGINE — STALLED (NR 2) · airframe 72,985 hrs · 34,481 cycles

AIRCRAFT WAS GROUNDED: - DIVERTED TO IAD DUE TO ENG 2 STALL AND ENG 2 FAIL (ENG SHUTDOWN). A/C DIVERTED TO IAD AND LANDED UNEVENTFULLY. **SUPPLEMENTAL REPORT FOR SDR AALA202411043100** (CLOSED) MAINTENANCE REPLACED #2 ENGINE.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 72,562 hrs · 34,196 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR ACCUMULATOR REQUIRES SERVICING. SERVICED THE L1 DOOR ACCUMULATOR.

Part: CONNECTOR — UNSECURE (ZONE 200) · airframe 72,556 hrs · 34,191 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY PATH LIGHTING AT SEAT ROW 22ABC IS INOPERATIVE. SECURED CONNECTOR.

Part: CONNECTOR — DISCONNECTED (ZONE 200) · airframe 72,287 hrs · 34,016 cycles

AIRCRAFT WAS NOT GROUNDED: 1L EXIT SIGN NOT ILLUMINATED. RECONNECTED 1L DOOR LIGHT.

Part: BOTTLE — LOW PRESSURE (PAX DOOR) · airframe 72,147 hrs · 33,929 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: LOW PRESSURE SPRING PERCUSSION MECHANISM ON DOOR DAMPER OPERATION CYLINDER PASSENGER CREW DOOR 831 AT FORWARD GALLEY AREA(1EA). REPLACED DOOR DAMPER OPERATION CYLINDER PASSENGER CREW DOOR 831 AT FORWARD GALLEY AREA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 72,147 hrs · 33,929 cycles

AIRCRAFT IN BASE MAINTENANCE: 2 EACH EXTERIOR EMERGENCY LIGHTS ON WTB FAIRING 192DT INOPERATIVE. REPLACED EMERGENCY LIGHTS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-15.

Part: FITTING — CRACKED (FRM 16) · airframe 72,147 hrs · 33,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 RIGHT AND DOOR STOP #7. REPLACED INTERCOSTAL FITTING PER SRM 51-42-11.

Part: HINGE ARM — EXCESS PLAY (RT ELEVATOR) · airframe 72,147 hrs · 33,929 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 5 ON RIGHTHAND HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM 5 ON RIGHTHAND HORIZONTAL STABILIZER.

Part: HINGE ARM — EXCESS PLAY (RT ELEVATOR) · airframe 72,147 hrs · 33,929 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 3 ON RIGHTHAND HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM 3 ON RIGHTHAND HORIZONTAL STABILIZER.

Part: HINGE ARM — EXCESS PLAY (RT ELEVATOR) · airframe 72,147 hrs · 33,929 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 1 ON RIGHTHAND HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM 1 ON RIGHTHAND HORIZONTAL STABILIZER

Part: SHEAR PLATE — CRACKED (FR 69-70 S23L) · airframe 72,147 hrs · 33,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.

Part: SHEAR PLATE — CRACKED (FRS 69-70 S23R) · airframe 72,147 hrs · 33,929 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT GALLEY AREA CRACKED SHEAR PLATE LOCATED FROM FR 69 TO FR 70 AND S23R. REPLACED SHEAR PLATE PER SRM 51-42-11-801.

Part: FITTING — CRACKED (WINDOW FRAME) · airframe 72,147 hrs · 33,929 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING CRACKED BETWEEN FR 1 AND FR 2 AT Y0. REPLACED CONTINUITY FITTING PER EA 353956.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 72,147 hrs · 33,929 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING CRACKED AT RIGHT HAND WINDSHIELD CENTER POST LOWER ATTACHMENT AREA UPPER RADIUS BETWEEN FR 1 AND FR 2 AT Y0. REPAIRED FRAME PER EA 353956.

Part: FITTING — CRACKED (WINDOW FRAME) · airframe 72,147 hrs · 33,929 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING CRACKED BETWEEN FR 1 AND FR 2 AT Y0. REPLACED CONTINUITY FITTING PER EA 353956.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 72,147 hrs · 33,929 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING CRACKED AT LEFT HAND WINDSHIELD CENTER POST LOWER ATTACHMENT AREA UPPER RADIUS BETWEEN FR 1 AND FR 2 AT Y0. REPAIRED FRAME PER EA 353956.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 72,093 hrs · 33,898 cycles

AIRCRAFT WAS NOT GROUNDED: CIDS OPERATIONAL TEST OF EMERGENCY LIGHTS FAIL ON EMERGENCY LEFT AND FORWARD LEFT POSITION. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (AALA202404150256) AND BATTERY ON FORWARD LEFT POSITION 10WL AND BATTERY ON EMERGENCY LEFT POSITION 11WL (AALA202404154166).

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 72,093 hrs · 33,898 cycles

AIRCRAFT WAS NOT GROUNDED: CIDS OPERATIONAL TEST OF EMERGENCY LIGHTS FAIL ON EMERGENCY LEFT AND FORWARD LEFT POSITION. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT AND BATTERY ON FORWARD LEFT POSITION 10WL (AALA202404156358) AND BATTERY ON EMERGENCY LEFT POSITION 11WL (AALA202404154166).

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 72,093 hrs · 33,898 cycles

AIRCRAFT WAS NOT GROUNDED: CIDS OPERATIONAL TEST OF EMERGENCY LIGHTS FAIL ON EMERGENCY LEFT AND FORWARD LEFT POSITION. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (AALA202404150256) AND BATTERY ON FORWARD LEFT POSITION 10WL (AALA202404156358) AND BATTERY ON EMERGENCY LEFT POSITION (11WL).

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 71,962 hrs · 33,812 cycles

AIRCRAFT WAS GROUNDED: OVERHEAD MID-CABIN EXIT SIGN HAS SEVERAL BULBS BURNED OUT. REPLACED MID-CABIN EXIT SIGN BULBS PER AMM 33-51-17.

Part: LEVER — LACK OF LUBE (L2 DOOR) · airframe 71,710 hrs · 33,674 cycles

AIRCRAFT WAS NOT GROUNDED: GRINDING NOISE AT DOOR WHEN ARMING AND DISARMING 2L. MAINTENANCE LUBRICATED 2L DOOR ARMING LEVER.

Part: LIGHT — INOPERATIVE (SEAT 19C) · airframe 71,504 hrs · 33,549 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY ESCAPE PATH LIGHT AT SEAT 19C HAS BECOME DETACHED FROM THE ARM REST. MAINTENANCE CONFIRMED THE LIGHT WAS DAMAGED AND INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BULB — BURNED OUT (ZONE 200 - FUSE) · airframe 71,252 hrs · 33,401 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT SIGNS ABOVE AFT CABIN DOORS LIGHT BULBS BURNED OUT. RELAMPED EXIT SIGNS ABOVE AFT CABIN DOORS PER AMM 33-51-16.

Part: BULB — BURNED OUT (ZONE 200 - FUSE) · airframe 71,252 hrs · 33,401 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT SIGNS ABOVE AFT CABIN DOORS LIGHT BULBS BURNED OUT. RELAMPED EXIT SIGNS ABOVE AFT CABIN DOORS PER AMM 33-51-16.

Part: RELAY — MALFUNCTIONED (ZONE 200 - FUSE) · airframe 71,225 hrs · 33,384 cycles

AIRCRAFT WAS NOT GROUND ED: EMERGENCY LIGHTS ABOVE DOORS AND OVER WING EXITS ARE STUCK ON. WILL NOT TURN OFF. REPLACED RELAY 8WL.

Part: PROXIMITY SENSOR — DEFECTIVE (ZONE 700 - GEARS) · airframe 70,938 hrs · 33,179 cycles

AIRCRAFT WAS GROUNDED: AN EMERGECNY WAS DECLARED AND THE AIRCRAFT RETURNED TO PIT DUE TO AN ECAM WARNING FOR A LANDING GEAR SHOCK ABSORBER FAULT RESULTING IN THE GEAR FAILING TO RETRACT AFTER TAKEOFF. THE AIRCRAFT LANDED SAFELY AT PIT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED PROXIMITY SENSORS 24GA (AALA202311063894) AND 25GA (AALA202311061238) PER AMM 32-31-73. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: PROXIMITY SENSOR — DEFECTIVE (ZONE 700 - GEARS) · airframe 70,938 hrs · 33,179 cycles

AIRCRAFT WAS GROUNDED: AN EMERGECNY WAS DECLARED AND THE AIRCRAFT RETURNED TO PIT DUE TO AN ECAM WARNING FOR A LANDING GEAR SHOCK ABSORBER FAULT RESULTING IN THE GEAR FAILING TO RETRACT AFTER TAKEOFF. THE AIRCRAFT LANDED SAFELY AT PIT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED PROXIMITY SENSORS 24GA (AALA202311063894) AND 25GA (AALA202311061238) PER AMM 32-31-73. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: LAMP — INOPERATIVE (ZONE 200 - FUSE) · airframe 70,769 hrs · 33,080 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT HAND OVERWING CABIN EXIT SIGN HAS LIGHTS OUT. RELAMP OVERWING CABIN EXIT SIGN.

Part: SLIDE — NO TEST (ZONE 800 - DOORS) · airframe 70,685 hrs · 33,022 cycles

AIRCRAFT WAS GROUNDED: DURING THE ACCOMPLISHMENT OF THE OPERATIONAL TEST OF EMERGENCY LIGHTING SYSTEM MULITPLE FAULTS OCCURRED. REPLACED THE R1 DOOR ESCAPE SLIDE PER TASK CARD 26L00025010 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BULB — INOPERATIVE (ZONE 200 - FUSE) · airframe 69,659 hrs · 32,395 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY EXIT SIGN ON CEILING OVER WING BURNT OUT. REPLACED BULB IN EMERGENCY EXIT LIGHT.

Part: BATTERY — FAULT MESSAGE (ZONE 200 - FUSE) · airframe 69,421 hrs · 32,234 cycles

AIRCRAFT WAS NOT GROUNDED: ON TAKEOFF AND SHORT FINAL EMERGENCY LIGHTS FLASHED ON AND OFF. MAINTENANCE PERFORMED TSM 33-51-00-810-802-A AND FOUND A FORWARD EMERGENCY POWER SUPPLY UNIT BATTERY FAULT MESSAGE. MAINTENANCE REPLACED THE BATTERY FOR THE FORWARD EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38 AND ACCOMPLISHED A A SATISFACTORY OPERATIONAL CHECK

Part: RELAY — FAULT MESSAGE (ZONE 100 - FUSE) · airframe 69,365 hrs · 32,200 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT FUEL TANK TRANSFER VALVE SHOW IN TRANSIT. MAINTENANCE REPLACED LEFT FUEL TANK TRANSFER VALVE RELAY PER TSM 28-15-00-810-804-A.

Part: RELAY — FAULT MESSAGE (ZONE 100 - FUSE) · airframe 69,359 hrs · 32,195 cycles

AIRCRAFT WAS NOT GROUNDED: ECAM FUEL RIGHT TANK PUMP 1 LOW PRESSURE. MAINTENANCE REPLACED FUEL LOW PRESSURE RELAY 18QA PER TSM 28-21-00-810-802-A AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: ACTUATOR — DEFECTIVE (RUDDER TRIM) · airframe 68,527 hrs · 31,688 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHL DUE TO RUDDER TRIM AND AILERON OUT OF TRIM IN FLIGHT AUTOPILOT 2 WAS ON REQUIRED 3 UNITS LEFT RUDDER TRIM TO FLY LEVEL. THE AIRCRAFT LANDED SAFELY AT PHL WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND RUDDER TRIM ACTUATOR RIG INCORRECT WITH RUDDER TRIM INDICATOR ON PEDESTAL AT ZERO, RUDDER IS DEFLECTED 2-3 INCHES TO THE RIGHT. REPLACED RUDDER TRIM ACTUATOR PER AMM 27-22-51-401. VERIFIED WITH RUDDER TRIM INDICATION AT ZERO, RUDDER TRAILING EDGE IS ALIGNEDWITH RIG INDEX (TRIANGLE ON TRAILING CONE).

Part: BRAKE SYS — ABNORMAL (MLG) · airframe 68,518 hrs · 31,681 cycles

AIRCRAFT WAS GROUNDED: BOTH LEFT AND RIGHT BRAKES GRAB AND PULSE WHEN BRAKING. MAINTENANCE ACCOMPLISHED TSM 32-42-00-810-912-A AND BLED ALL 4 BRAKES AT BRAKE UNITS PER AMM 32-42-00-870-001-A. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO BRAKE PULSATING, PULLING OR ABNORMAL CONDITIONS NOTED WHILE TAXING THE AIRCRAFT.

Part: APU — ODOR (ZONE 100 - FUSE) · airframe 67,202 hrs · 30,854 cycles

AIRCRAFT WAS GROUNDED: CREW REPORTED DIRTY SOCK SMELL ON TAXI OUT, TAKE OFF, DESCENT AND APPROACH. MAINTENANCE HAS ISOLATED THE SOURCE OF THE ODOR TO THE APU. **SUPPLEMENTAL REPORT FOR AALA202205234652: MAINTENANCE FOUND OIL COMING FROM THE LOAD COMPRESSOR SEAL WITNESS DRAIN PORT. REPLACED APU PER TASK CARD 26L31049005. ** (CLOSED)

Part: APU — ODOR (ZONE 100 - FUSE) · airframe 67,202 hrs · 30,854 cycles

AIRCRAFT WAS GROUNDED: CREW REPORTED DIRTY SOCK SMELL ON TAXI OUT, TAKE OFF, DESCENT AND APPROACH. MAINTENANCE HAS ISOLATED THE SOURCE OF THE ODOR TO THE APU. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: ACTUATOR — FAULT MESSAGE (ZONE 400 - NAC/P) · airframe 66,697 hrs · 30,557 cycles

AIRCRAFT WAS GROUNDED: ABORTED TAKE OFF AT 63 KNOTS, ECAM ENGINE #2 COMPRESSOR VANE FAULT. RETURNED TO GATE. REPLACED ENGINE #2 VSV ACTUATOR PER JOB CARD 26T4007500. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECKS.

Part: BATTERY — INOPERATIVE (ZONE 200 - FUSE) · airframe 66,216 hrs · 30,262 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT TEST STEP 2(10) OF JOB CARD 26C20033001 FAILS TO BRING ON ALL EMERGENCY LIGHTS ON. JUST HALF ILLUMINATE. REMOVED AND REPLACED AFT EMERGENCY POWER SUPPLY UNIT BATTERY PER AMM 33-51-38.

Part: LENS — DAMAGED (EMERGENCY LGIHT) · airframe 65,530 hrs · 29,889 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT OVERWING EMERGENCY LIGHT BURNED OUT. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY LIGHT LENS ASSEMBLY PER AMM 33-50-00.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 65,178 hrs · 29,711 cycles

AIRCRAFT WAS GROUNDED: LEFT ELEVATOR HINGE #6 HINGE ARM END FITTING BEARINGS FAILED BEARING FREE PLAY CHECK ON TASK CARD 26L3027002 AND AMM 55-26-00-200-802. TO CLARIFY, THIS IS THE BEARING AT THE ELEVATOR HINGE STABILIZER SIDE.. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 65,178 hrs · 29,711 cycles

AIRCRAFT WAS GROUNDED: LEFT ELEVATOR HINGE #4 HINGE ARM END FITTING BEARINGS FAILED BEARING FREE PLAY CHECK ON TASK CARD 26L3027002 AND AMM 55-26-00-200-802. TO CLARIFY, THIS IS THE BEARING AT THE ELEVATOR HINGE STABILIZER SIDE.. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 65,178 hrs · 29,711 cycles

AIRCRAFT WAS GROUNDED: LEFT ELEVATOR HINGE #1 HINGE ARM END FITTING BEARINGS FAILED BEARING FREE PLAY CHECK ON TASK CARD 26L3027002 AND AMM 55-26-00-200-802. TO CLARIFY, THIS IS THE BEARING AT THE ELEVATOR HINGE STABILIZER SIDE.. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 65,178 hrs · 29,711 cycles

AIRCRAFT WAS GROUNDED: RIGHT ELEVATOR HINGE #6 HINGE ARM END FITTING BEARINGS FAILED BEARING FREE PLAY CHECK ON TASK CARD 26L3027002 AND AMM 55-26-00-200-802. TO CLARIFY, THIS IS THE BEARING AT THE ELEVATOR HINGE STABILIZER SIDE.. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 65,178 hrs · 29,711 cycles

AIRCRAFT WAS GROUNDED: RIGHT ELEVATOR HINGE #3 HINGE ARM END FITTING BEARINGS FAILED BEARING FREE PLAY CHECK ON TASK CARD 26L3027002 AND AMM 55-26-00-200-802. TO CLARIFY, THIS IS THE BEARING AT THE ELEVATOR HINGE STABILIZER SIDE.. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 65,178 hrs · 29,711 cycles

AIRCRAFT WAS GROUNDED: RIGHT ELEVATOR HINGE #1 HINGE ARM END FITTING BEARINGS FAILED BEARING FREE PLAY CHECK ON TASK CARD 26L3027002 AND AMM 55-26-00-200-802. TO CLARIFY, THIS IS THE BEARING AT THE ELEVATOR HINGE STABILIZER SIDE.. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 65,178 hrs · 29,711 cycles

AIRCRAFT WAS GROUNDED: LEFT ELEVATOR HINGE #3 HINGE ARM END FITTING BEARINGS FAILED BEARING FREE PLAY CHECK ON TASK CARD 26L3027002 AND AMM 55-26-00-200-802. TO CLARIFY, THIS IS THE BEARING AT THE ELEVATOR HINGE STABILIZER SIDE.. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 65,178 hrs · 29,711 cycles

AIRCRAFT WAS GROUNDED: RIGHT ELEVATOR HINGE #5 HINGE ARM END FITTING BEARINGS FAILED BEARING FREE PLAY CHECK ON TASK CARD 26L3027002 AND AMM 55-26-00-200-802. TO CLARIFY, THIS IS THE BEARING AT THE ELEVATOR HINGE STABILIZER SIDE.. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 65,178 hrs · 29,711 cycles

AIRCRAFT WAS GROUNDED: RIGHT ELEVATOR HINGE #2 HINGE ARM END FITTING BEARINGS FAILED BEARING FREE PLAY CHECK ON TASK CARD 26L3027002 AND AMM 55-26-00-200-802. TO CLARIFY, THIS IS THE BEARING AT THE ELEVATOR HINGE STABILIZER SIDE.. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 65,178 hrs · 29,711 cycles

AIRCRAFT WAS GROUNDED: LEFT ELEVATOR HINGE #5 HINGE ARM END FITTING BEARINGS FAILED BEARING FREE PLAY CHECK ON TASK CARD 26L3027002 AND AMM 55-26-00-200-802. TO CLARIFY, THIS IS THE BEARING AT THE ELEVATOR HINGE STABILIZER SIDE.. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE ARM — WORN (LT ELEVATOR) · airframe 65,178 hrs · 29,711 cycles

AIRCRAFT WAS GROUNDED: LEFT ELEVATOR HINGE #2 HINGE ARM END FITTING BEARINGS FAILED BEARING FREE PLAY CHECK ON TASK CARD 26L3027002 AND AMM 55-26-00-200-802. TO CLARIFY, THIS IS THE BEARING AT THE ELEVATOR HINGE STABILIZER SIDE.. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 65,178 hrs · 29,711 cycles

AIRCRAFT WAS GROUNDED: RIGHT ELEVATOR HINGE #4 HINGE ARM END FITTING BEARINGS FAILED BEARING FREE PLAY CHECK ON TASK CARD 26L3027002 AND AMM 55-26-00-200-802. TO CLARIFY, THIS IS THE BEARING AT THE ELEVATOR HINGE STABILIZER SIDE.. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 63,678 hrs · 28,896 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY POWER SUPPLY UNIT EMERGENCY LIGHT FAULT FOUND ON EMERGENCY POWER SUPPLY UNIT BUILT IN TEST EQUIPMENT CHECK FOR R1 SLIDE CHANGE. REMOVED AND REPLACED MID LEFT EMERGENCY POWER SUPPLY UNIT (11WL), PER AMM 33-51-13-840.

Part: RELAY — DEFECTIVE (RT WING PUMP) · airframe 63,664 hrs · 28,889 cycles

AIRCRAFT WAS GROUNDED. RIGHT WING TANK PUMP NR 1 LOW PRESSURE. FOUND NO POWER AT 103VU AND REPLACED 64QA BUS RELAY, PER AMM 28-21-00.

Part: INDICATOR — UNCALIBRATED (AIRSPEED) · airframe 63,390 hrs · 28,752 cycles

AIRCRAFT WAS GROUNDED: STANDBY AIRSPEED INDICATOR 60 KNOTS FAST ON TAKEOFF. AT ALTITUDE 20 KNOTS OFF. INSTALLED NEW STANDBY AIRSPEED INDICATOR. OPERATIONS NORMAL PER AMM 34-21-26.

Part: SDAC — FAULTY (ZONE 100) · airframe 62,990 hrs · 28,523 cycles

AIRCRAFT WAS GROUNDED: DECLARED EMERGENCY INTO PHX ACCOUNT CREW RECEIVED MULTIPLE ECAM MESSAGES. REMOVED AND REPLACED ANTI SKID N/W STEERING CONTROL SWITCH IAW AMM 32-46-00 AND SDAC NO.1 AMM31-55-34.

Part: MODULE — FAULTY (CABIN) · airframe 62,563 hrs · 28,261 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT WAS INOPERABLE AT R1 DOOR. MAINTENANCE REPLACED EXIT LIGHT MODULE PER AMM 33-51-13.

Part: LUBRICATION UNIT — CRACKED (APU) · airframe 61,810 hrs · 27,852 cycles

AIRCRAFT WAS GROUNDED: F/A REPORTED ADVERSE PHYSIOLOGICAL SYMPTOMS DUE TO FUMES IN THE AFT PART OF CABIN. MAINTENANCE FOUND APU TO BE SOURCE OF THE ODOR. MAINTENANCE FOUND LUBE JET ASSEMBLY CAST FITTING CRACKED AND LEAKING. REMOVED AND REPLACED JET ASSY IAW CMM 49-25-65. LEAK AND OPS CHECK GOOD.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 59,375 hrs · 26,461 cycles

PILOT REPORTED SOF EVENT. THE AIRCRAFT WAS GROUNDED.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 59,009 hrs · 26,258 cycles

AIRCRAFT WAS GROUNDED. IN ALL POSITIONS EMERGENCY EXIT LIGHTS IN CABIN ON, WILL NOT TURN OFF. RESET CIDS PER AMM 23-73-34. OPERATIONS CHECK GOOD.

Part: LENS — CRAZED (EMERGENCY LIGHT) · airframe 58,695 hrs · 26,098 cycles

THE L2 DOOR OVERHEAD EXIT LENS CRAZED. REPLACED THE LENS IAW AMM 25-23-45-400-008-A.

Part: HINGE ARM — CRACKED (RT ELEVATOR) · airframe 58,690 hrs · 26,096 cycles

RIGHT ELEVATOR HAD THREE CRACKED HINGE ARMS. REPLACED THE HINGE ARMS IAW SRM 51-42-11 AND DRAWING D55181526.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 58,690 hrs · 26,096 cycles

DELAMINATION FOUND ON FLOOR PANEL 222FF IN THE FORWARD GALLEY. REPLACED THE FLOOR PANEL IAW AMM 53-00-00-400-801-A.

Part: HINGE ARM — CRACKED (LT ELEVATOR) · airframe 58,690 hrs · 26,096 cycles

LEFT ELEVATOR HAD FOUR CRACKED HINGE ARMS. REPLACED THE HINGE ARMS IAW SRM 51-42-11 AND DRAWING D55181526.

Part: SPAR — DAMAGED (LT PYLON) · airframe 58,690 hrs · 26,096 cycles

LEFT PYLON LOWER SPAR HAS ELONGATED HOLE. REPLACED THE SPAR IAW SRM 51-72-11, 51-42-111, AND DRAWING D54510054.

Part: FLOOR PANEL — DELAMINATED (GALLEY) · airframe 58,690 hrs · 26,096 cycles

DELAMINATION FOUND ON FLOOR PANEL 232DF AT FORWARD GALLEY. REPLACED THE FLOOR PANEL IAW JC 26C22053014.

Part: FLOOR PANEL — DELAMINATED (GALLEY) · airframe 58,690 hrs · 26,096 cycles

DELAMINATED FLOOR PANEL 261DF IN THE AFT GALLEY. REPLACED THE FLOOR PANEL IAW AMM 53-00-00-400-801-A.

Part: FLOOR PANEL — DELAMINATED (GALLEY) · airframe 58,690 hrs · 26,096 cycles

DELAMINATION FOUND ON FLOOR PANEL 222CF IN THE FORWARD GALLEY. REPLACED THE FLOOR PANEL IAW AMM 53-00-00-400-801-A, STEP 1A, ITEM 4.

Part: SLIDE — DEFORMED (PAX DOOR) · airframe 58,690 hrs · 26,096 cycles

DEFORMATION ON ESCAPE SLIDE PASSENGER DOOR AT FORWARD GALLEY AREA. REPLACED THE SLIDE IAW J/C 26C83152008.

Part: DAMPER — OUT OF ADJUST (PAX DOOR) · airframe 58,690 hrs · 26,096 cycles

PASSENGER DOOR DAMPER OUT OF ADJUSTMENT. ADJUSTED THE DOOR DAMPER IAW AMM 52-13-14-820-002-A, STEP 4A(1).

Part: DAMPER — OUT OF ADJUST (PAX DOOR) · airframe 58,690 hrs · 26,096 cycles

PASSENGER DOOR DAMPER WAS OUT OF ADJUSTMENT. PERFORMED AN ADJUSTMENT IAW AMM 52-11-14-820-002-A, STEP 4A(1).

Part: FLOOR PANEL — DELAMINATED (GALLEY) · airframe 58,690 hrs · 26,096 cycles

DELAMINATED FLOOR PANEL 231AF IN THE FORWARD GALLEY. REPLACED THE FLOOR PANEL IAW AMM 53-00-00-400-801-A.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 58,690 hrs · 26,096 cycles

CORROSION FOUND ON FLOOR PANEL 262LG. REPLACED THE FLOOR PANEL IAW AMM 53-00-00-400-801-A.

Part: FLOOR PANEL — CORRODED (GALLEY) · airframe 58,690 hrs · 26,096 cycles

CORROSION ON FLOOR PANEL 261LG IN THE AFT GALLEY. REPLACED THE FLOOR PANEL IAW AMM 53-00-00-400-801-A.

Part: RECEPTACLE — CRACKED (ESCAPE SLIDE) · airframe 58,690 hrs · 26,096 cycles

CRACKED OVERWING ESCAPE SLIDE RECEPTACLE, RT SIDE, ON THE LOWER FUSELAGE. REPLACED ESCAPE SLIDE RECEPTACLE IAW SRM 51-42-11.

Part: FITTING — WORN (RT WING TE FLAP) · airframe 58,690 hrs · 26,096 cycles

RIGHT WING INBOARD FLAP INTERCONNECTING STRUT ATTACH FITTING HAS EXCESSIVE PLAY. REPLACED FITTING IAW SRM 51-72-11 AND AIRBUS DRAWING D57570280.

Part: WINDOW — GLAZED (PAX DOOR) · airframe 58,690 hrs · 26,096 cycles

GLAZED OUTER PANE ON THE PASSENGER DOOR WINDOW. REPLACED THE WINDOW OUTER PANE IAW AMM 56-31-11-400-002-A.

Part: CYLINDER — OUT OF ADJUST (DOOR) · airframe 58,690 hrs · 26,096 cycles

DURING OPERATIONAL TEST OF PASSENGER CREW DOOR DAMPING FUNCTION, HAD HARD IMPACT BETWEEN BUFFER DOOR AND FUSELAGE AT FORWARD GALLEY AREA (1EA). REPLACED DOOR DAMPER CYLINDER AT PASSENGER/CREW DOOR 841 PER AMM 52-11-14-400-001-B.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-69) · airframe 58,690 hrs · 26,096 cycles

CORROSION FOUND ON THE FLOOR SUPPORT BETWEEN FRAMES 66 TO 69, -Y1732. REPLACED THE FLOOR SUPPORT IAW SRM 51-75-11, AND DWG D53472750.

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 58,690 hrs · 26,096 cycles

EXCESSIVE PLAY ON THE HINGE ARM FITTING RT ELEVATOR. REPLACED THE HINGE ARM FITTING IAW AMM 55-16-42.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 58,690 hrs · 26,096 cycles

CORROSION ON THE FLOOR SUPPORT, FRAMES 66 TO 68, -Y1225. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-141, AND DRAWING D53472780.

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 58,690 hrs · 26,096 cycles

EXCESSIVE PLAY ON THE HINGE ARM FITTING, RT ELEVATOR. REPLACED THE HINGE ARM FITTING IAW AMM 55-16-42.

Part: SUPPORT — DAMAGED (FRAMES 16-20) · airframe 58,690 hrs · 26,096 cycles

DAMAGE ON THE LOWER SILL AROUND GIRT BAR FITTING BETWEEN FRAMES 16 TO 20, STRINGER 23R. REPAIRED THE SILL IAW SRM 51-72-11, AND DRAWING D53110339.

Part: DOOR SILL — CORRODED (FRAMES 16-20) · airframe 58,690 hrs · 26,096 cycles

DURING A PREVIOUS MAINTENANCE VISIT, CORROSION WAS DISCOVERED ON THE L2 DOOR CUTOUT LOWER SILL AROUND THE GIRT BAR FITTING AT FR 19 AND S23L WHICH WAS REPAIRED BY BLENDING PER EA 133964 (MINOR REPAIR). DURING THIS CURRENT MAINTENANCE VISIT THE SILL WAS REPALCED PER SRM 51-72-11 AND AIRBUS DRAWING D53110339.

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 58,690 hrs · 26,096 cycles

EXCESSIVE PLAY ON THE HINGE ARM FITTING, RT ELEVATOR. REPLACED THE HINGE ARM FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 58,690 hrs · 26,096 cycles

EXCESSIVE PLAY ON THE HINGE ARM FITTING 4, ON THE RT ELEVATOR. REPLACED THE HINGE ARM FITTING IAW AMM 55-16-42.

Part: WEB — CORRODED (FRAMES 55A-59) · corrosion level 2 · airframe 58,690 hrs · 26,096 cycles

AFT CARGO COMPARTMENT, CORROSION WAS FOUND ON COVER SHEET LOCATED AT FRAME 55A TO 59, STRINGERS 34R TO 41R. REPLACED THE COVER SHEET IAW SRM 51-42-11, DWG D53477000, AND SRM 51-72-11.

Part: FRAME — CRACKED (FRM 35) · airframe 58,690 hrs · 26,096 cycles

FORWARD CARGO FRAME CRACKED, FRM 35, STRINGER 30L. REPAIRED THE FRAME IAW EA 283091.

Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 58,690 hrs · 26,096 cycles

CORROSION FOUND ON THE FLOORBEAM, FRAME 68, -Y1162. REPLACED THE FLOORBEAM IAW SRM 51-72-11, AND DRAWING D53472780

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 58,690 hrs · 26,096 cycles

CORRODED FLOOR SUPPORT BETWEEN FRAME 64 TO 66, Y765. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DRAWINGS D53472815, AND D53472090.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 58,690 hrs · 26,096 cycles

CORROSION FOUND ON THE FLOOR SUPPORT, -Y1292, FRAMES 64 - 66. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53472780.

Part: PROFILE — CRACKED (FRAMES 34-41) · airframe 58,690 hrs · 26,096 cycles

CRACKED EMERGENCY DOOR RIGHT LOAD TRANSMITTING PROFILE AT FRAMES 34 TO 41, STRINGER 14R TO STRINGER 21R. REPAIRED THE PROFILE PER EO 5210Y228.

Part: FLOOR SUPPORT — CORRODED (FRAMES 65-67) · corrosion level 2 · airframe 58,690 hrs · 26,096 cycles

CORRODED FLOOR SUPPORT BETWEEN FRAMES 65 TO 67, -Y318. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472819.

Part: FITTING — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 58,690 hrs · 26,096 cycles

CORROSION FOUND ON CENTER FITTING, BETWEEN FRAMES 66 TO 68, STRINGER 23L. REPLACED THE FITTING IAW SRM 51-72-11, AND DRAWING D53480505.

Part: FITTING — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 58,690 hrs · 26,096 cycles

CORROSION FOUND ON THE CENTER FITTING LOCATED BETWEEN FRAMES 66 - 68, RT SIDE IN THE AFT GALLEY AREA. REPLACED THE FITTING IAW SRM 51-72-11, 51-42-11, AND DRAWING D53480019.

Part: PROFILE — CRACKED (FRAMES 31-41) · airframe 58,690 hrs · 26,096 cycles

CRACKED EMERGENCY DOOR, LEFT LOAD TRANSMITTING PROFILE AT FR 31 TO FR 41, STRINGER 14L TO 21L. REPAIRED THE PROFILE PER EO # 5210Y228.

Part: SEAT TRACK — CORRODED (FRAMES 36-41) · airframe 58,690 hrs · 26,096 cycles

CORROSION FOUND ON THE SEAT TRACK, FRAMES 36 TO 41, Y765. REPLACED THE SEAT TRACK IAW SRM 51-72-11, DRAWING D57130147, AND D5337050.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · corrosion level 2 · airframe 58,690 hrs · 26,096 cycles

CORROSION FLOOR SUPPORT +Y765 BETWEEN FRAMES 66 TO 70. REPLACED THE FLOOR SUPPORT SRM A319 51-72-11 AND DRAWING D53472780.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · corrosion level 2 · airframe 58,690 hrs · 26,096 cycles

CORRODED FLOOR SUPPORT, -Y765 BETWEEN FRAMES 66 AND 70 OF FORWARD GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53472780.

Part: SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 58,690 hrs · 26,096 cycles

CORROSION ON SILL LOCATED AT STA FR66 TO FR68, STR 23R. REPLACED SILL PER SRM A319 51-72-11 DWG D53480019 AND D53480505.

Part: SUPPORT — CORRODED (FRAME 68) · corrosion level 2 · airframe 58,690 hrs · 26,096 cycles

CORROSION FOUND ON LOWER SILL AT FRAME 68. REPAIRED THE SILL AIW SRM 53-41-14-300-001, FIGURE 20101 (SHEET 1)(SHEET 3).

Part: SEAT TRACK — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 58,690 hrs · 26,096 cycles

CORROSION ON SEAT TRACK, FRAMES 12 TO 24, -Y1292. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING D53112812.

Part: SHEAR PLATE — CORRODED (AFT GALLEY) · corrosion level 2 · airframe 58,690 hrs · 26,096 cycles

CORROSION FOUND ON SHEAR PLATE AT STRINGER 23R IN THE AFT GALLEY. REPLACED THE SHEAR PLATE IAW SRM 51-72-11, AND DRAWING D53474180.

Part: SEAT TRACK — CORRODED (FRAMES 12-16) · corrosion level 2 · airframe 58,690 hrs · 26,096 cycles

CORRODED SEAT TRACK BETWEEN FRAMES 12 TO 16, +Y503.2. REPAIRED THE SEAT TRACK IAW SRM 53-11-14-283-004.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 58,690 hrs · 26,096 cycles

CORROSION ON THE FLOOR SUPPORT, FRAMES 12 TO 24, -Y765. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DRAWINGS D53918123, D53110920, AND D53110984.

Part: WEB — CRACKED (FRAMES 69-70) · airframe 58,690 hrs · 26,096 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. AFT GALLEY AREA WEB (SHEAR PLATE) IS CRACKED AT STA FR 69 TO FR 70 AND STR 23L. REPLACED WEB (SHEAR PLATE) PER A319 SRM 51-72-11 AND DWG # D53474180.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 58,690 hrs · 26,096 cycles

CORROSION FOUND ON THE FLOOR SUPPORT, FRAMES 12 TO 24, Y1292. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53112812.

Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 58,690 hrs · 26,096 cycles

CORROSION FOUND ON THE FLOORBEAM, FRAME 68, -Y160. REPLACED THE FLOORBEAM IAW SRM 51-72-11, AND DRAWING D53472780.

Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 58,690 hrs · 26,096 cycles

CORROSION FOUND ON FLOORBEAM, FRAME 68, Y512.5. REPLACED THE FLOORBEAM IAW SRM 51-72-11, AND DRAWING D53472780.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 58,690 hrs · 26,096 cycles

DELAMINATION ON FLOOR PANEL 231LF, PASSENGER CABIN, BETWEEN FRAMES 24 TO 28, Y254 TO Y765. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, PARAGRAPH 2, FIGURE 20109, AND IRM 9701, REVISION H .

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 58,690 hrs · 26,096 cycles

DELAMINATION ON FLOOR PANEL 241EF, FRAMES 36 TO 42, Y254 TO -Y254. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701, REVISION H.

Part: HINGE FITTING — DAMAGED (NLG DOOR) · airframe 58,690 hrs · 26,096 cycles

AFT DOOR HINGE FITTING LT NOSE LANDING GEAR BETWEEN FRAMES 19A TO 20, STRINGER 41L. REPLACED HINGE FITTING IAW CMM 52-82-32.

Part: HINGE FITTING — DAMAGED (NLG) · airframe 58,690 hrs · 26,096 cycles

LEFT FORWARD DOOR HINGE FITTING, FOR THE NOSE LANDING GEAR BETWEEN FRAMES 19A TO 20, STRINGER 41L DAMAGED. REPLACED HINGE FITTING IAW CMM 52-82-32.

Part: HINGE FITTING — DAMAGED (NLG) · airframe 58,690 hrs · 26,096 cycles

LEFT FORWARD DOOR HINGE FITTING FOR THE NOSE LANDING GEAR BETWEEN FRAMES 19A TO 20, STRINGER 41L DAMAGED. REPLACED THE HINGE FITTING IAW CM 52-82-32.

Part: HINGE FITTING — DAMAGED (NLG DOOR) · airframe 58,690 hrs · 26,096 cycles

LEFT AFT DOOR HINGE FITTING, FOR THE NOSE LANDING GEAR BETWEEN FRAMES 19A TO 20, STRINGER 41L DAMAGED. REPLACED THE HINGE FITTING IAW CMM 52-82-32.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 58,690 hrs · 26,096 cycles

DELAMINATION FOUND ON FLOOR PANEL 221DF, BETWEEN FRAMES 16 TO 20, Y-254 TO Y254. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, PARA 2, FIG 20106, AND IRM 9701, REV H.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 58,690 hrs · 26,096 cycles

DELAMINATED FLOOR PANEL 241KF, FRAMES 42 TO 47 AND Y254 TO Y765. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701 REV H.

Part: FLOOR PANEL — DELAMINATED (COCKPIT) · airframe 58,690 hrs · 26,096 cycles

DELAMINATION ON FLOOR PANEL 212EF, FRAMES 6 TO 11, Y-765 TO Y-254 IN THE COCKPIT. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, FIGURE 20106, AND IRM 9701, REVISION H.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 58,690 hrs · 26,096 cycles

DELAMINATION FOUND ON FLOOR PANEL 232LF, BETWEEN FRAMES 24 TO 28, Y-765 TO Y-254. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, PARA 2, FIG 20109, AND IRM.

Part: HINGE FITTING — DAMAGED (NLG DOOR) · airframe 58,690 hrs · 26,096 cycles

LEFT, AFT DOOR HINGE FITTING FOR THE NOSE LANDING GEAR BETWEEN FRAMES 19A TO 20, STRINGER 41L. REPLACED THE HINGE FITTING IAW CMM 52-82-32.

Part: FLOOR PANEL — DELAMINATED (COCKPIT) · airframe 58,690 hrs · 26,096 cycles

DELAMINATION ON FLOOR PANEL 211EF IN THE COCKPIT, BETWEEN FRAMES 6 TO 11, FROM -Y254 TO Y254 . REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, PARAGRAPH 2, FIGURE 20106, AND IRM 9701, REVISION H.

Part: HINGE FITTING — DAMAGED (LT NLG DOOR) · airframe 58,690 hrs · 26,096 cycles

DAMAGED AFT DOOR HINGE FITTING, LT NOSE LANDING GEAR DOOR, BETWEEN FRAMES 19A & 20, STRINGER 41L. REPLACED THE HINGE FITTING IAW CMM 52-82-32.

Part: HINGE FITTING — DAMAGED (LT NLG DOOR) · airframe 58,690 hrs · 26,096 cycles

FORWARD HINGE FITTING ON THE LT NOSE LANDING GEAR DOOR DAMAGED, BETWEEN FRAMES 19A & 20, STRINGER 41L. REPLACED THE HINGE FITTING IAW CMM 52-82-32.

Part: FLOOR PANEL — DELAMINATED · airframe 58,690 hrs · 26,096 cycles

DELAMINATION FOUND ON FLOOR PANEL 251GF. FRAMES 51 TO 54, Y254 TO Y765. REPLACED THE FLOOR PANEL SRM 53-02-00-300-011, PARA 2, FIG 20109, AND IRM 9701, REV.H.

Part: HINGE FITTING — DAMAGED (LT NLG DOOR) · airframe 58,690 hrs · 26,096 cycles

FORWARD HINGE FITTING, LT NOSE LANDING GEAR DOOR, BETWEEN FRAMES 19A & 20, STRINGER 41L. REPLACED THE HINGE FITTING IAW CMM 52-82-32.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 58,690 hrs · 26,096 cycles

DELAMINATION ON FLOOR PANEL 232EF, FRAMES 20 TO 24, Y-1292 TO Y-765. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, FIGURE 20106, AND IRM 9701.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 58,690 hrs · 26,096 cycles

DELAMINATED FLOOR PANEL 262BG, BETWEEN FRAMES 64 - 66 AND BETWEEN -Y1732 TO -Y512. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011 AND IRM 9701 REV.H.

Part: FLOOR PANEL — DELAMINATED (GALLEY) · airframe 58,690 hrs · 26,096 cycles

DELAMINATION ON FLOOR PANEL 231CF IN THE FORWARD GALLEY, BETWEEN FRAMES 20 TO 24, Y765 TO Y254. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, PARAGRAPH 2, FIGURE 20106, AND IRM 9701 REVISION H.

Part: FLOOR PANEL — DELAMINATED (GALLEY) · airframe 58,690 hrs · 26,096 cycles

DELAMINATION OF FLOOR PANEL 261CG. FRAMES 64 TO 66 , -Y765 TO Y765. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, PARAGRAPH 2, FIGURE 20109, AND IRM 9701, REVISION H.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 58,690 hrs · 26,096 cycles

TRAPPED WATER INDICATION ON THE RT ELEVATOR HONEYCOMB CORE STRUCTURE UPPER SKIN PANEL LOCATED NEXT TO OUTBOARD SIDE OF LIGHTENING STRIP NR 4 AND 12 INCHES FROM TRAILING EDGE, THE RIGHT STABILIZER. WAS REPAIRED ELEVATOR IAW SRM 55-21-11-300-005.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 58,690 hrs · 26,096 cycles

DELAMINATION FOUND ON FLOOR PANEL 221PF, FRAMES 16 TO 20, Y254 TO Y1292. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, AND IRM 9701 REVISION H.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 58,690 hrs · 26,096 cycles

DELAMINATION FOUND ON FLOOR PANEL 261PF, FRAMES 68 TO 70, -Y1292 TO Y1292. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, PARA 2, FIG 20109, AND IRM 9701, REV H.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 58,690 hrs · 26,096 cycles

DELAMINATION FOUND ON FLOOR PANEL 251WF BETWEEN FRAMES 62 TO 64, -Y765 TO Y765. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, PARA 2, FIGURE 20109, AND IRM 9701, REV.H.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 58,690 hrs · 26,096 cycles

DELAMINATION ON FLOOR PANEL 252JG, FRAMES 62 TO 64, -Y1292 TO -Y1732. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701, REVISION H.

Part: FITTING — CRACKED (FRAME 16) · airframe 58,690 hrs · 26,096 cycles

CRACK INDICATION ON INTERCOSTAL FITTING FRAME 16, LT SIDE DOOR STOP NR 7 IN INBOARD UPPER HOLE OF FORWARD GALLEY AREA. REPLACED THE INTERCOSTAL FITTING IAW SRM 51-72-11, AND DWG D53112300.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 58,690 hrs · 26,096 cycles

DELAMINATED FLOOR PANEL 222EF, FRAMES 16 TO 20,-Y1292 TO -Y254. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, AND IRM 9701 REV H.

Part: FITTING — CRACKED (FRAME 20) · airframe 58,690 hrs · 26,096 cycles

CRACK INDICATION, FRAME 20 ON DOOR STOP FITTING NR 7 LT. REPLACED THE FITTING IAW SRM 51-72-11, AND DRAWING D53112331.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 58,690 hrs · 26,096 cycles

DELAMINATION ON FLOOR PANEL 221EF, FRAMES 16 TO 20, Y254 TO Y1292. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-600-006, AND IRM 9701, REVISION H.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 58,690 hrs · 26,096 cycles

DELAMINATION FOUND ON FLOOR PANEL 261BG, FRAMES 64 TO 66, Y512 TO Y1732. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701 REVISION H.

Part: FLOOR PANEL — DELAMINATED (GALLEY) · airframe 58,690 hrs · 26,096 cycles

DELAMINATION ON FLOOR PANEL 232FF, FRAMES 20 TO 24, Y-1732 TO Y-1292. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, PARAGRAPH 2, FIGURE 20106, AND IRM 9701, REVISION H.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 58,690 hrs · 26,096 cycles

THE AIRCRAFT WAS IN BASE MAINTENANCE. CRACK INDICATION FOUND ON PANEL (SKIN) ON FRAME 35, LEFT HAND LOWER HOLE AT LEVEL OF STRINGER 30. REPAIRED PANEL (SKIN) PER EA 283091.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 58,662 hrs · 26,081 cycles

LEFT WINDSHIELD OUTER PANE WAS CRACKED. THE AIRCRAFT WAS GROUNDED. REPLACED THE WINDSHIELD IAW JC 26L21056001.

Part: COVER — MISSING (L2 DOOR SLIDE) · airframe 58,520 hrs · 25,995 cycles

L2 DOOR SLIDE ARM COVER MISSING. REPLACED THE COVER IAW AMM 52-73-21. OK FOR SERVICE.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 58,363 hrs · 25,890 cycles

AIRCRAFT WAS NOT GROUNDED. FORWARD EMERGENCY LIGHT ON IN ARMED POSITION. REPLACED FORWARD EMERGENCY LIGHT POWER SUPPLY PER AMM 33-51-38.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,457 hrs · 25,306 cycles

LAVATORY D EMERGENCY LIGHT FOUND INOPERATIVE. REPLACED THE LAMPS.

Part: PIN — BENT (MLG TORQUE LINK) · airframe 56,784 hrs · 24,905 cycles

AFTER TAKE-OFF, WHEN GEAR EXTENDED, MAJOR VIBRATION WAS EXPERIENCED FROM NOSE WHEEL AREA. VIBRATION WENT AWAY WHEN GEAR RETRACTED, ALSO FELT IN FORWARD GALLEY AND MID CABIN. MAINTENANCE TROUBLESHOT IAW TSM 32-20-00810-802-S, FOUND TORQUE LINK PIN ASSEMBLY BENT. REPLACED THE CENTER LINK PIN ASSEMBLY IAW MM 32-21-27-400-002-A. AIRCRAFT WAS GROUNDED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,339 hrs · 24,633 cycles

LIGHTS INOPERATIVE ON CENTER EXIT SIGN ABOVE L1 AND JUST AFT OF FA ANNUNCIATOR PANEL. REPLACED EMERGENCY EXIT LIGHT IAW AMM 33-51-11.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,308 hrs · 24,610 cycles

EXIT MARKING SIGN AT DOOR 2 LEFT NEEDS FIVE BULBS RELPACED. MAINTENANCE REPLACED EXIT MARKING SIGN IAW MM 33-51-16-0401. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS GROUNDED.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,308 hrs · 24,610 cycles

EXIT LOCATION SIGN ON MAIN AISLE FORWARD CABIN AFT FACING FIRST CLASS NEEDS FIVE BULBS REPLACED. MAINTENANCE REPLACED EXIT MARKING SIGN IAW MM 33-51-16-0401. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS GROUNDED.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,308 hrs · 24,610 cycles

EXIT MARKING SIGN AT DOOR 1 RIGHT NEEDS FOUR BULBS REPLACED. MAINTENANCE REPLACED EXIT MARKING SIGN IAW MM 33-51-16-0401. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS GROUNDED.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,308 hrs · 24,610 cycles

EXIT MARKING SIGN AT DOOR 2 RIGHT NEEDS FOUR BULBS REPLACED. MAINTENANCE REPLACED EXIT MARKING SIGN IAW MM 33-51-16-0401. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS GROUNDED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,308 hrs · 24,610 cycles

LEFT FORWARD ENTRY DOOR EXIT SIGN NEEDS TWO BULBS. REPLACED THE BULBS. MAINTENANCE REPLACED EXIT MARKING SIGN IAW MM 33-51-16-0410. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS GROUNDED.

Part: PRESSURE SWITCH — FAULTY (APU) · airframe 56,108 hrs · 24,500 cycles

AIRCRAFT WAS GROUNDED. CABIN ODOR IN THE FLIGHT DECK AND AFT CABIN DURING DESCENT. AUXILIARY POWER UNIT OFF. ODOR STOPPED UPON LANDING. REMOVED AND REPLACED APU OIL PUMP DIFFERENTIAL PRESSURE SWITCH IAW AMM 49-91-15. OPERATIONAL CHECK GOOD.

Part: DUCT — DIRTY (A/C PACK) · airframe 55,596 hrs · 24,193 cycles

MUSTY ODOR FROM THE PACKS WHEN FLYING THRU HEAVY RAIN. CLEANED APU INLET PLENUM AND RAN PACKS AND BLEED FOR OVER AN HOUR NO ODOR.

Part: NOZZLE — DAMAGED (NR 2 ENGINE) · airframe 55,192 hrs · 23,963 cycles

FLIGHT CREW REPORTED THAT THE AIRCRAFT ENCOUNTERED SEVERE TURBULENCE AND OVERSPEED WHILE AT FL. 370. OVERSPEED WAS APPROXIMATELY 10 KTS FOR ABOUT 5 SECONDS. THE FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED INSPECTION AFTER INFLIGHT EXCESSIVE LOAD FACTOR DUE TO TURBULANCE IAW AMM 05-51-17-200-001-A. SEVERAL RIVETS WERE FOUND TO BE PULLING THRU THE NR 2 ENGINE TAIL PIPE EXHAUST AT 4 & 5 O'CLOCK POSITIONS RESULTING IN THE REPLACEMENT OF THE COMMON NOZZLE ASSEMBLY. THE NR 2 ENGINE RIGHT THRUST REVERSER AFT HINGE ACCESS DOOR LATCH WAS FOUND TO BE DAMAGED AND WAS REPLACED. AIRCRAFT WAS GROUNDED

Part: PROXIMITY SENSOR — FAULTY (R1 DOOR) · airframe 55,175 hrs · 23,956 cycles

R1 DOOR INDICATES OPEN IN FLIGHT AND DISPLAYS INTERMITTENT CABIN PRESSURE NORMAL. REPLACED PROXIMENTY DETECTOR.

Part: PROXIMITY SWITCH — DIRTY (R1 DOOR) · airframe 55,145 hrs · 23,945 cycles

R1 DOOR SHOWS OPEN INDICATION WHEN DOOR IS CLOSED. CLEANED THE R1 DOOR PROXIMITY SWITCH AND PERFORM DOOR WARNING OPERATIONAL TEST IAW AMM 52-71-00-710-001-A. INDICATION AND OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (R1 DOOR) · airframe 55,122 hrs · 23,935 cycles

R1 DOOR SHOWS OPEN ON ECAM WHEN DOOR IS CLOSED. TROUBLESHOT IAW TSM 52-11-00-810-803-A. NO FAULTS NOTED. OPS NORMAL.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 54,768 hrs · 23,756 cycles

AIRCRAFT WAS NOT GROUNDED. BACK FLIGHT ATTENDANT JUMP SEAT FLASHLIGHT NOT WORKING. MAINTENANCE REPLACED BATTERY AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: SDAC — FAULTED (ZONE 100) · airframe 54,265 hrs · 23,492 cycles

CIDS 1 FAULT INFLIGHT WITH CABIN ELECTRICAL SMELL. MAINTENANCE ISOLATED SMELL TO FAILED SDAC 1. WHICH WAS REPLACED AMM 31-55-34-400-001-A. MAINTENANCE PERFORMED JOB CARD 26L00021001. NO ODORS NOTED. NO CIDS FAULTS AFTER SDAC 1 REPLACEMENT.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 52,292 hrs · 22,304 cycles

AIRCRAFT IN BASE MX. LT SIDE BOX BEAM FLANGE, FOURTH HOLE HAS CRACK INDICATION, FRAME 43 & Y1622. REPAIRED BOX BEAM IAW EO 5315Y066.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 52,292 hrs · 22,304 cycles

AIRCRAFT IN BASE MX. RT SIDE BOX BEAM FLANGE, FOURTH HOLE HAS CRACK INDICATION, FRAME 43 & -Y1622. REPAIRED BOX BEAM IAW EO 5315Y066.

Part: APU — ODOR (APU BAY) · airframe 50,360 hrs · 21,126 cycles

FLIGHT 489, EN-ROUTE CREW NOTICED ODOR IN COCKPIT & FWD CABIN DURING IDLE DESCENT. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. DETERMINED THE SOURCE OF ODOR TO BE THE APU. R & R APU IAW 26L31049003, OPERATIONS GOOD.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 49,862 hrs · 20,864 cycles

EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT ROW 22L. REPAIRED BROKEN WIRES AT SEAT ROW 22L.

Part: WINDOW — CRACKED (COCKPIT) · airframe 49,843 hrs · 20,855 cycles

AFT LT SIDE FIXED WINDOW FLAKING & CRACKING 1.4 INCH. R & R AFT LT FIXED WINDOW IAW AMM 56-11-12-401. GOOD OPERATIONAL CHECK.

Part: TRUNNION — WORN (TE FLAP) · airframe 49,363 hrs · 20,600 cycles

RON VISIT LT WING INBD FLAP DRIVE STRUT TRUNNION WORN BEYOND ALLOWABLE LIMITS IAW JOB CARD 26T50057066. REPLACED LT WING INBD FLAP DRIVE STRUT TRUNNION IAW JOB CARD 26L00027003.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 49,160 hrs · 20,484 cycles

GDAFR VISIT, EMER LIGHTS ABOVE L2 & R2 DOORS ARE INOPERATIVE. RECONNECTED EMER LIGHTS AT L2 & R2 DOORS. OPERATIONS CHECKED GOOD.

Part: LENS — DAMAGED (CABIN) · airframe 49,160 hrs · 20,484 cycles

GDAFR VISIT, R2 DOOR JAMB TRIM EMER EXIT LIGHT, LENS COVER DAMAGED. REPLACED EMER LIGHT LENS AT R2 DOOR JAMB. .

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 47,086 hrs · 19,336 cycles

RESET SMOKE DETECTORS ON GND IN DTW, RESET GOOD. ABOUT A HALF HOUR FROM PHX, GOT A FIRE BELL & LAVATORY SMOKE ECAM THAT LASTED FOR 5 OR 6 SECONDS THEN CLEARED ITSELF. NO SMOKE IN ANY LAVATORY`S, DID NOT REPEAT. PERFORMED TROUBLESHOOTING IAW 26-17-00-810-801A, NO FAULTS NOTED. PERFORMED OPERATIONAL CHECK OF ALL LAVATORY`S IAW AMM 26-17-00-710-001-A, NO FAULTS NOTED.

Part: SEAL — LEAKING (ENGINE) · airframe 46,741 hrs · 19,197 cycles

CREW REPORTED A STRONG ODOR OF FUEL NOTICED IN FWD & AFT GALLEYS. SINGLE ENG TAXI - ODOR COMING FROM ENG NR 1. FLIGHT RETURNED TO THE GATE. MX COMPLIED WITH JOB CARDS 26L00021001, 26L00021003 & 26L00021004. FOUND OIL COMING OUT OF NR 1 & NR 2 ENG BREATHER AFTER ENG SHUTDOWN. R & R NR 1 & NR 2 ENG DE-OILER SEAL ASSEMBLIES IAW AMM 72-60-31-400-010-A. R & R LT & RT CONDENSERS & RE-HEATERS. OPERATIONS & LEAK CHECKED GOOD. ACCOMPLISHED SATISFACTORY MX TEST FLIGHT.

Part: APU — CONTAMINATED (APU BAY) · airframe 46,741 hrs · 19,197 cycles

DURING BOARDING, THE FLIGHT ATTENDANT`S REPORTED THE CABIN AIR HAS A DIRTY SOCK ODOR. FLIGHT PROCEEDED EN ROUTE FROM OAK TO PHX WITHOUT INCIDENT. FOUND SOURCE OF ODOR TO BE FROM THE APU, PLACED APU ON MEL. SUBSEQUENTLY, ON NEXT FLIGHT DURING TAXI-OUT, THE ODOR RETURNED & THE ACFT RETURNED TO THE GATE. REPORTED AN EXTERNAL VAPOR & EXHAUST INGESTION BY APU SUSPECTED. APU GOOD FOR SERVICE. CLEANED THE ACTUATOR AREA OF DE-ICING FLUID. COMPLIED WITH JOB CARDS 26L00021001, 26L00021002 & 26L00021004 DECONTAMINATION. NO REOCCURRENCE OF ANY ODOR FROM ANY BLEED SOURCE. CLEARED APU MEL.

Part: FEEL UNIT — INOPERATIVE (RUDDER SYS) · airframe 45,677 hrs · 18,762 cycles

DURING LANDING, AT APPROXIMATELY 50 FT, RUDDER PEDALS AND RUDDER LOCKED AND WERE FROZEN IN PLACE. AUTOPILOT WAS OFF AND LANDING IN CROSSWIND. WITH A LOUD SNAP RUDDER AND PEDALS WERE FREED. IT WAS ALSO NOTED THAT THE F/O PEDAL ADJUST WAS BEYOND THE MAX 12 AND RETURNED TO NORMAL AFTER THE SNAP. TROUBLESHOT, REPLACED ARTIFICIAL FEEL UNIT IAW AMM 27-23-41-400-001A. OPS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (RUDDER SYS) · airframe 44,511 hrs · 18,241 cycles

ON APPROACH WITH A/P OFF, RUDDER PEDALS WERE DIFFICULT TO MOVE IN EITHER DIRECTION, FELT A JOLT AND RUDDER PEDAL MOVEMENT RESUMED NORMALLY. PERFORMED OPS TEST OF THE RUDDER SERVO CONTROLS WITH HYD SYS, OPS CHECK GOOD IAW AMM 27-24-00-710-002-A.

Part: COVER — MISSING (CABIN) · airframe 44,109 hrs · 18,049 cycles

MAINTENANCE REPORTED THE EMERGENCY LIGHT LENS COVER MISSING AT ROW 12 LEFT. MAINTENANCE REPLACED EMERGENCY LIGHT LENS COVER AT ROW 12 LEFT PER AMM 33-51-19.

Part: LENS — MISSING (CABIN) · airframe 43,134 hrs · 17,621 cycles

MAINTENANCE REPORTED THE EMERGENCY LIGHT LENS AT 16L MISSING. MAINTENANCE REPLACED LENS AT 16L. OPS CHECK GOOD.

Part: PLATE — CRACKED (LT WING) · airframe 42,154 hrs · 17,155 cycles

2S CHECK - CRACK ON LEFT WING PYLON MOUNTING PLATE AFT OF WING REAR SPAR BETWEEN RIB 7 AND RIB 8. REPLACED LEFT WING PYLON MOUNTING PLATE IAW A319 SRM 57-21-11, FIGURE 204 AND SRM 51-75-12.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,154 hrs · 17,155 cycles

2S CHECK - GALVANIC CORROSION ON SILL PLATE 9 INCHES AFT OF FR54, S38L, Y273.9. REPLACED SILL PLATE 9 INCHES AFT OF FR54, S38L, Y273.9 IAW A319 SRM 51-72-11 AND SRM 51-75-12.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,154 hrs · 17,155 cycles

2S CHECK - GALVANIC CORROSION ON SILL PLATE 4 INCHES FORWARD OF FR58, AT S38L, Y723.9. REPLACED SILL PLATE 4 INCHES FORWARD OF FR58, AT S38L, Y723.9 IAW A319 SRM 51-72-11 AND SRM 51-75-12.

Part: HOOK — GOUGED (EMERGENCY EXIT) · airframe 42,154 hrs · 17,155 cycles

2S CHECK - RIGHT EMERGENCY EXIT HATCH LOWER HOOKS FORWARD & AFT HAD GOUGES. REPLACED RIGHT EMERGENCY EXIT HATCH FORWARD & AFT LOWER HOOKS IAW A319 AMM 52-21-00.

Part: HOOK — GOUGED (EMERGENCY EXIT) · airframe 42,154 hrs · 17,155 cycles

2S CHECK - LEFT EMERGENCY EXIT HATCH LOWER HOOKS FORWARD & AFT HAD GOUGES. REPLACED LEFT EMERGENCY EXIT HATCH FORWARD & AFT LOWER HOOKS IAW A319 AMM 52-21-00.

Part: FLOOR PANEL — PEELING (FUSELAGE) · airframe 42,154 hrs · 17,155 cycles

2S CHECK - FLOOR PANEL 222EF COVERING PEELING, LOCATED BETWEEN FR16 TO FR20, -Y762. REPLACED FLOOR PANEL 222EF IAW A319 SRM 53-02-00, FIG 209.

Part: DOOR — OUT OF ADJUST (L2) · airframe 40,348 hrs · 16,339 cycles

C11, SY6 CHECK - OUT OF ADJUSTMENT DIM A BETWEEN FINGER AND STRIKER LEVER AT DOOR 832. ADJUSTED DIM A BETWEEN FINGER AND STRIKER LEVER AT DOOR 832 IAW A319 AMM 52-13-14-820-002 & 52-10-00-710-003.

Part: DOOR — OUT OF ADJUST (R2) · airframe 40,348 hrs · 16,339 cycles

C11, SY6 CHECK - OUT OF ADJUSTMENT DIM A BETWEEN FINGER AND STRIKER LEVER AT DOOR 842. ADJUSTED DIM A BETWEEN FINGER AND STRIKER LEVER AT DOOR 842 IAW A319 AMM 52-13-14-820-002 & 52-10-00-710-003.

Part: DOOR — OUT OF ADJUST (R2) · airframe 40,348 hrs · 16,339 cycles

C11, SY6 CHECK - OUT OF ADJUSTMENT DIM B BETWEEN FINGER AND STRIKER LEVER AT DOOR 842. ADJUSTED DIM B BETWEEN FINGER AND STRIKER LEVER AT DOOR 842 IAW A319 AMM 52-13-14-820-002 & 52-10-00-710-003.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 40,348 hrs · 16,339 cycles

C11 CHECK - DELAMINATION ON FLOOR PANEL 261PF BETWEEN FR68 TO FR70, BETWEEN -Y1292 TO Y1292. REPLACED FLOOR PANEL 261PF IAW A319 SRM 53-02-00 AND IRM 9701, REV G.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,348 hrs · 16,339 cycles

C11 CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT SHEAR PLATE BETWEEN FR69 TO FR70, S23R. REPLACED RIGHT SHEAR PLATE BETWEEN FR69 TO FR70, S23R IAW A319 SRM 55-72-11, 51-42-11 & AIRBUS DRAWING D53474180.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,348 hrs · 16,339 cycles

C11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, Y1162. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, Y1162 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,348 hrs · 16,339 cycles

C11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, -Y1162. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, -Y1162 IAW A319 SRM 51-72-11 & DRAWING D53472780.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,348 hrs · 16,339 cycles

C11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, -Y1292. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, -Y1292 IAW A319 SRM 51-72-11, AIRBUS DRAWING D53110984.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,348 hrs · 16,339 cycles

C11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, -Y1185. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, -Y1185 IAW A319 SRM 51-72-11 & DRAWING D53472420.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,348 hrs · 16,339 cycles

C11 CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY BETWEEN FR12 TO FR16, Y1162. REPLACED RAIL DUMMY BETWEEN FR12 TO FR16, Y1162 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112831.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,348 hrs · 16,339 cycles

C11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67 TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR67 TO FR70, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,348 hrs · 16,339 cycles

C11 CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, STR23L. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, STR 23L IAW A319 SRM 51-72-11, AIRBUS DRAWING D53474180 AND TYPICAL REPAIR 320-2528-10-0011.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,348 hrs · 16,339 cycles

C11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, -Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472420.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,348 hrs · 16,339 cycles

C11 CHECK - LEVEL 2 GALVANIC CORROSION AT R2 DOOR LOWER SILL AT FR66, -Y1732. REPAIRED R2 DOOR LOWER SILL AT FR66, -Y1732 IAW EA 133973 & A319 SRM 53-41-14 PB201.

Part: SKIN — SATURATED (ELEVATOR) · airframe 40,348 hrs · 16,339 cycles

C11 CHECK - WATER INGRESS ON RIGHT ELEVATOR BETWEEN THSS589 TO THSS601, BETWEEN RIB 13 TO RIB 14. REPAIRED RIGHT ELEVATOR BETWEEN THSS589 TO THSS601, BETWEEN RIB 13 TO RIB 14 IAW A319 SRM 55-21-11 PARAGRAPH 5, E.

Part: SKIN — SATURATED (ELEVATOR) · airframe 40,348 hrs · 16,339 cycles

C11 CHECK - WATER INGRESS ON RIGHT ELEVATOR BETWEEN THSS181 TO THSS227, BETWEEN RIB 5 TO RIB 6. REPAIRED RIGHT ELEVATOR BETWEEN THSS181 TO THSS227, BETWEEN RIB 5 TO RIB 6 IAW A319 SRM 55-21-11 PARAGRAPH 5, E.

Part: SKIN — SATURATED (ELEVATOR) · airframe 40,348 hrs · 16,339 cycles

C11 CHECK - WATER INGRESS ON RIGHT ELEVATOR BETWEEN THSS527 TO THSS589, BETWEEN RIB 12 TO RIB 13. REPAIRED RIGHT ELEVATOR BETWEEN THSS527 TO THSS589, BETWEEN RIB 12 TO RIB 13 IAW A319 SRM 55-21-11 PARAGRAPH 5, E.

Part: SKIN — SATURATED (ELEVATOR) · airframe 40,348 hrs · 16,339 cycles

C11 CHECK - WATER INGRESS ON LEFT ELEVATOR BETWEEN THSS342 TO THSS404, BETWEEN RIB 9 TO RIB 10. REPAIRED LEFT ELEVATOR BETWEEN THSS342 TO THSS404, BETWEEN RIB 9 TO RIB 10 IAW A319 SRM 55-21-11 PARAGRAPH 5, E.

Part: SKIN — SATURATED (ELEVATOR) · airframe 40,348 hrs · 16,339 cycles

C11 CHECK - WATER INGRESS ON LEFT ELEVATOR BETWEEN THSS227 TO THSS271, BETWEEN RIB 6 TO RIB 7. REPAIRED LEFT ELEVATOR BETWEEN THSS227 TO THSS271, BETWEEN RIB 6 TO RIB 7 IAW A319 SRM 55-21-11 PARAGRAPH 5, D.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 40,024 hrs · 16,197 cycles

LEFT CABIN EMERGENCY POWER SUPPLY UNIT INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38-000-001.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 38,665 hrs · 15,576 cycles

PHX-SNA - EEL - EMERGENCY LIGHTS OVERWING AND CEILING INOPERATIVE. REMOVED AND REPLACED OVERWING EMERGENCY LIGHTS POWER SUPPLY PER AIRBUS MAINTENANCE MANUAL 33-51-38.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 38,499 hrs · 15,501 cycles

SMF-PHX - EMERGENCY LIGHTS - EMERGENCY POWER SUPPLY UNIT FORWARD LEFT INOPERATIVE (FIN #10WL). REMOVED AND REPLACED (EPSU) EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-38. OPERATIONAL CHECK GOOD.

Part: APU — ODOR (APU BAY) · airframe 35,740 hrs · 14,263 cycles

FLT 623 - CABIN HAS DIRTY SOCK ODOR FROM TOP OF DESCENT TILL ARRIVING AT GATE. REMOVED AND REPLACED APU. OPERATIONAL AND LEAK CHECKED GOOD. VENDOR REPORTED SIGNS OF INGESTION AT APU INLET AND NEAR COOLING AIR DISTRIBUTION DUCT. AFTER DISASSEMBLY, UNIT ALSO SHOWED SIGNS OF INGESTION AT L/C INLET BELLMOUTH.

Part: FAN — FAULTY (APU) · airframe 35,712 hrs · 14,252 cycles

FLT 209 - SLC-PHX - ODOR - EXTRA DIRTY SOCK SMELL THROUGHOUT CABIN & GALLEYS. REMOVED AND REPLACED APU OIL COOLER FAN IAW AMM 49-52-05.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 34,771 hrs · 13,851 cycles

FLT 622 - PHX-LAS - EMERGENCY LIGHTS - AFT GALLEY CABIN EMERGENCY POWER SUPPLY UNIT FAILED TEST. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT IN AFT GALLEY PER AMM 33-51-38 PB 401.

Part: FILTER — DIRTY (CABIN) · airframe 34,748 hrs · 13,837 cycles

FLT 42 - PHX-DCA - ODOR - DIRTY SOCK-OILY SMELL THAT MADE EYES BURN ON DESCENT TO DCA. REMOVED AND REPLACED RECIRCULATION FILTERS AND OZONE FILTERS AS PART OF DECONTAMINATION PROCESS. ACCOMPLISHED BURNOUT. NO SMOKE/ODOR IN COCKPIT/CABIN AFTER ENGINE RUN. NO FURTHER DIRTY SOCK SMELL INCIDENTS FOLLOWED.

Part: WIRE — DAMAGED (CABIN) · airframe 34,605 hrs · 13,770 cycles

FLT 115 - LAS-LAX - EMERGENCY LIGHTS - SEAT MOUNTED EMERGENCY LIGHT LAST LEFT SEAT INOPERATIVE. REPAIRED WIRE TO LIGHT ASSEMBLY. REFER ESPM.

Part: LENS — MISSING (EVAC SLIDE) · airframe 33,435 hrs · 13,249 cycles

FLT 407 - DTW - EMERGENCY EGRESS SYSTEM - L2 DOOR SLIDE ARMED LIGHT MISSING LENS. MAINTENANCE REPLACED MISSING L2 DOOR SLIDE ARMED LIGHT LENS IAW AIRBUS MAINTENANCE MANUAL 52-73-21.

Part: LENS — MISSING (CABIN) · airframe 33,204 hrs · 13,157 cycles

FLT 296 - LAS-DTW - EMERGENCY LIGHTS - EMERGENCY LIGHT LENS MISSING AT ROW 4. INSTALLED NEW EMERGENCY LIGHT LENS AT ROW 4.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 33,137 hrs · 13,134 cycles

FLT 62 - BOS-LAX - EMERGENCY LIGHTS - 2 FLASHLIGHTS INOPERATIVE IN CABIN. REMOVED AND REPLACED BATTERIES IN FLASHLIGHTS. OPERATIONAL CHECK WAS GOOD.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 32,864 hrs · 13,022 cycles

FLT 525 - RNO-PHX- EMERGENCY EQUIPMENT - L1 AND L2 DOOR ASSIST BOTTLES NEED SERVICE. SERVICED L1 AND L2 DOOR ASSIST BOTTLES TO PROPER PRESSURE.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 32,864 hrs · 13,022 cycles

FLT 525 - RNO-PHX - EMERGENCY EQUIPMENT - L1 AND L2 DOOR ASSIST BOTTLES NEED SERVICE. SERVICE L1 AND L2 DOOR ASSIST BOTTLES TO PROPER PRESSURE.

Part: CONNECTOR — LOOSE (EVAC SLIDE) · airframe 32,222 hrs · 12,690 cycles

FLT 528 - IAD-PHX - EMERGENCY EQUIPMENT - CIDS CAUTION EMERGENCY LEFT SLIDE BOTTLE INDICATION. SECURED ELECTRICAL PRESSURE SENSOR CONNECTOR. MESSAGE WENT AWAY. BOTTLE FULL AT LEFT EMERGENCY OVERWING SLIDE BOTTLE.

Part: PLUNGER — MALFUNCTIONED (EVAC SLIDE) · airframe 31,917 hrs · 12,547 cycles

LOGPAGE:8226314 - FLT 77 - EWR-PHX - EMERGENCY EQUIPMENT - NO ECAM SLIDE ARMED INDICATION OVERWING AIRCRAFT RIGHT. RESET RIGHT OVERWING EMERGENCY DISARMED PLUNGER.

Part: STRIKER — OUT OF ADJUST (R2 DOOR) · airframe 31,640 hrs · 12,419 cycles

SAL - BC6 - EES - DIMENSION "A" OUT OF LIMITS IN STRIKER MECHANISM OF DOOR DAMPER & EMERGENCY OPERATION CYLINDER AT R-2 DOOR. PERFORMED ADJUSTMENT OF DIMENSION "A" IN STRIKER MECHANISM OF DOOR DAMPER & EMERGENCY OPERATION CYLINDER AT R-2 DOOR IAW A319 AMM 52-13-14-820-002.

Part: STRIKER — OUT OF TOLERANCE (R2 DOOR) · airframe 31,640 hrs · 12,419 cycles

SAL - BC6 - EES - DIMENSION "B" OUT OF LIMITS IN STRIKER MECHANISM OF DOOR DAMPER & EMERGENCY OPERATION CYLINDER AT R-2 DOOR. PERFORMED ADJUSTMENT OF DIMENSION "B" IN STRIKER MECHANISM OF DOOR DAMPER & EMERGENCY OPERATION CYLINDER AT R-2 DOOR IAW A319 AMM 52-13-14-820-002.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 31,640 hrs · 12,419 cycles

SAL - BC6 - MAJOR REPAIR - EXCESSIVE PLAY AT NR 2 RUDDER HINGE FITTING. REPLACED RUDDER HINGE ARM FITTING NR 2 IAW A319 AMM 55-36-41.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 31,640 hrs · 12,419 cycles

SAL - BC6 - MAJOR REPAIR - EXCESSIVE PLAY AT NR 3 RUDDER HINGE FITTING. REPLACED RUDDER HINGE ARM FITTING NR 3 IAW A319 AMM 55-36-41.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 31,640 hrs · 12,419 cycles

SAL - BC6 - MAJOR REPAIR - EXCESSIVE PLAY AT NR 4 RUDDER HINGE FITTING. REPLACED RUDDER HINGE ARM FITTING NR 4 IAW A319 AMM 55-36-41.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 31,640 hrs · 12,419 cycles

SAL - BC6 - MAJOR REPAIR - EXCESSIVE PLAY AT NR 1 RUDDER HINGE FITTING. REPLACED RUDDER HINGE ARM FITTING NR 1 IAW A319 AMM 55-36-41.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 31,640 hrs · 12,419 cycles

SAL - BC6 - MAJOR REPAIR - EXCESSIVE PLAY AT NR 5 RUDDER HINGE FITTING. REPLACED RUDDER HINGE ARM FITTING NR 5 IAW A319 AMM 55-36-41.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 31,686 hrs · 12,442 cycles

FLT 471 - SFO-LAS - EMERGENCY EQUIPMENT - R2 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED R2 DOOR ASSIST BOTTLE AS REQUIRED.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 31,060 hrs · 12,144 cycles

FLT 319 ORD-LAS - EE - L-2 DOOR ASSIST BOTTLE CHARGE LOW. SERVICED L-2 DOOR ASSIST BOTTLE PER CHART. LEAK CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 30,722 hrs · 11,988 cycles

LOGPAGE: 8371748 FLT NR 162 LAS-SJC. FLASHLIGHT UNDER FORWARD GALLEY JUMPSEAT IS INOPERATIVE. R&R FORWARD FLASHLIGHT BATTERY. OPS CHECK WAS GOOD.

Part: PIN — DEFECTIVE (ZONE 800) · airframe 30,098 hrs · 11,703 cycles

FLT 72 SEA-PHX EMERGENCY EGRESS SYSTEM RT OVERWING ESCAPE DOOR LATCH PIN WILL NOT LOCK IN EXTENDED POSITION. MX R&R THE RELEASE PIN AND SPRING. IAW AIRBUS MX MANUAL 52-21-11-000-003 AND 52-21-11-400-003. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

FLT 0526 - GDL-PHX- EMERGENCY EQUIPMENT- FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD FLIGHT ATTENDANT FLASHLIGHT BATTERY. FLASHLIGHT OPERATES NORMALLY AND STOWS PROPERLY. (S)

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 25,686 hrs · 9,866 cycles

LAS - EEL - LOG# 7779890 - EMERGENCY EXIT LIGHTS RAN DOWN THEIR BATTERIES. EMERGENCY LIGHT SWITCH WAS LEFT ON AND A/C POWER WAS LOST WHEN JET BRIDGE WAS MOVED. MX REMOVED AND REPLACED ALL FOUR EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW T/C A1C33302.

Part: PIN — CRACKED (NLG) · airframe 25,282 hrs · 9,697 cycles

DTW - NOSE LANDING GEAR UPPER AND LOWER TORQUE LINK CONNECTING HINGE PIN CRACKED. REPLACED NOSE LANDING GEAR UPPER AND LOWER TORQUE LINK CONNECTING HINGE PIN IAW A320 AMM 32-21-11.

Part: SMOKE DETECTOR — FAILED (LAVATORY) · airframe 23,747 hrs · 9,059 cycles

LAS LOG NR 7485109. MX REPORTED LAV AND CARGO SMOKE DETECTORS FAULT, SDCU INOP. MX TROUBLESHOT SYSTEM AND FOUND FWD CARGO 2WH INOP. MX REMOVED AND REPLACED FWD CARGO 2WH SMOKE DETECTOR. OPS CHECK WAS GOOD.

Part: CONTROL UNIT — FAULTY (CARGO BAY) · airframe 22,489 hrs · 8,505 cycles

PHX - SMOKE - DURING MAINTENANCE CHECK, ECAM SMOKE LAV AND CARGO DET FAULT. REMOVED AND REPLACCED SDCU, CARGO TEST OK. ROTATABLE PARTS CHANGE WAS INDICATED.

Part: DOOR ACTUATOR — OUT OF ADJUST (FUSELAGE) · airframe 20,154 hrs · 7,490 cycles

DURING BC4 CHECK DISCOVERED THE R2 DOOR EMERGENCY ASSIST MECH DIMENSION A WAS .4125 INCH, WHICH IS OUT OF LIMITS IAW TASK CARD I1C52307. MAINTENANCE ADJUSTED THE R2 DOOR EMERGENCY ASSIST MECH TO A NEW DIMENSION OF .291 INCHES, WHICH IS IN LIMITS IAW MM 52-13-14.

Part: COVER — CRACKED (FUSELAGE) · airframe 20,154 hrs · 7,490 cycles

SAL - DURING BC4 CHECK DISCOVERED CRACK ON JOINT COVER, FLOOR STRUCTURE SUPPORT, LOCATED AT FR 14 AND Y0.04. MAINTENANCE REMOVED AND INSTALLED NEW JOINT COVER AT FR 14 AND Y-0.040 IAW AIRBUS 319 SRM 51-42-11 AND DRAWING D53112829.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,154 hrs · 7,490 cycles

SAL - DURING BC4 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT FR 66 AND Y1292. RE-WORK AREA WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 319 SRM 53-00-14. MAINTENANCE REMOVED AND INSTALLED NEW FLOORBEAM FROM FR 64 TO FR 66 AND Y1292 IAW AIRBUS 319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,154 hrs · 7,490 cycles

SAL - DURING BC4 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT FR 66+8" AND Y-1292. RE-WORK AREA WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 319 SRM 53-00-14. MAINTENANCE REMOVED AND INSTALLED NEW FLOORBEAM FROM FR 67 TO FS 68 AND Y-1292 IAW AIRBUS 319 SRM 51-42-11 AND DRAWING 53472040.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,154 hrs · 7,490 cycles

SAL - DURING BC4 CHECK DISCOVERED CORROSION ON LOWER SILL OF THE R2 DOOR AT FR 66 AND Y-1732. MAINTENANCE CUT OUT THE DAMAGED AREA IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 25-5341-05365-ES2. FABRICATED REPAIR ANGLES AND FILLER IAW AWA ER NO. 25-5341-05365-ES2 AND AIRBUS 319 SRM 53-41-14 REPAIR 6. INSTALLED FABRICATED REPAIR PARTS AT FS 66 TO FS 68 AND Y-1732 IAW AWA ER NR 25-5341-05365-ES2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,154 hrs · 7,490 cycles

MCN - DURING BC-4 CHECK DISCOVERED CORROSION ON FLOORBEAM SEAT RAIL AT FR 66 AND Y-1292. CORROSION WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND INSTALLED NEW FLOORBEAM FROM FR 64 TO FR 66 AND Y-1292 IAW AIRBUS 319 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · airframe 20,154 hrs · 7,490 cycles

DURING BC4 CHECK DISCOVERED CORROSION ON THE LOWER SILL AT FR 68-3 AND Y 1732. MAINTENANCE CUT OUT DAMAGED AREA IAW AIRBUS 319 SRM 53-41-14 FIG 201. FABRICATED REPAIR ANGLE AND REPAIR FILLER IAW AIRBUS 319 SRM 53-41-14 FIG 201. INSTALLED FABRICATED REPAIR PARTS FROM FR 66 TO FR 68 AND Y 1732 IAW AIRBUS 319 SRM 53-41-14 PAGE 201 TO 212, FIG 201, SHEET 3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,154 hrs · 7,490 cycles

SAL - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK FROM FR36 TO FR 41 AND Y765. RE-WORK AREA WAS FOUND TO BE OUT OF LIMITS IAW 51-31-15 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK FROM FR36 TO FR41 AND Y765 IAW AIRBUS 319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,154 hrs · 7,490 cycles

SAL - DURING BC4 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT FR 68 AND Y-1162. RE-WORK AREA WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 319 SRM 53-00-14. MAINTENANCE REMOVED AND INSTALLED NEW FLOORBEAM FROM FR 68 TO FR 69 AND Y-1162 IAW AIRBUS 319 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 20,154 hrs · 7,490 cycles

SAL - DURING BC4 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT FR 16 AND Y503.2. RE-WORK AREA WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 319 SRM 53-11-14. MAINTENANCE REMOVED AND INSTALLED NEW FLOORBEAM FROM FR 12 TO FR 16 AND Y503.2 IAW AIRBUS 319 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,154 hrs · 7,490 cycles

SAL - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK FROM FR 37+1 TO FR 40+2 AND Y1292. RE-WORK AREA WAS FOUND TO BE OUT OF LIMITS IAW 53-31-15 FIG 103. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK FROM FR36 TO FR41 AND Y1292 IAW AIRBUS 319 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,154 hrs · 7,490 cycles

SAL - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK AT FR 42+7" AND Y-765. RE-WORK AREA WAS FOUND TO BE OUT OF LIMITS IAW 53-31-15 FIG 103. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK FROM FR42 TO FR51 AND Y-765 IAW AIRBUS 319 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,154 hrs · 7,490 cycles

SAL - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK FROM FR 38 TO FR 40 AND Y-1292. RE-WORK AREA WAS FOUND TO BE OUT OF LIMITS IAW 51-31-15 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK FROM FR36 TO FR41 AND Y-1292 IAW AIRBUS 319 SRM 51-72-11.

Part: IRU — MALFUNCTIONED (NR 2) · airframe 17,720 hrs · 6,551 cycles

EN ROUTE, AFTER REACHING CRUISE ALTITUDE RECEIVED ECAM MESSAGE ADR 1 FAULT FOLLOWED BY NR 1 IR FAILURE. APPROXIMATELY 2 HRS 45 MINUTES LATER AUTOPILOT, AUTO THROTTLES, AND FLIGHT DIRECTORS DISCONNECTED AND WOULD NOT RE-ENGAGE, NR 2 IR FAULT INDICATED ON ADIRU STATUS AND CENTRALIZED FAULT DISPLAY SYSTEM. DIVERTED INTO PHX FOR REPAIR. MAINTENANCE REMOVED AND REPLACED THE NR 1 AND NR 2 ADIRU'S IAW T/C R2A34304, OPERATIONAL CHECK WAS GOOD. VENDOR CONFIRMED REASON FOR REMOVAL ON THE NO. 1 ADIRU, SN 3138, FAULT WAS ISOLATED TO SENSOR ELECTRONICS ASSEMBLY AS PRIMARY ROOT CAUSE AND WAS A CONFIRMED FAILURE. GYROS WERE A SECONDARY FAULT ON UNIT. UNIT WAS REPAIRED IAW AT261847-01 CMM TP1011 REV 24.

Part: SEAT — LEAKING (NR 1 ENGINE) · airframe 14,902 hrs · 5,569 cycles

AFTER TAKEOFF AT JFK EN ROUTE TO PHX, RECEIVED ECAM MESSAGE "AIR ENG 1 BLEED ABNORMAL PRESSURE", NR 1 ENGINE BLEED VALVE WOULD NOT OPEN, DIVERTED TO BWI FOR REPAIR. MX T/S PER TSM 36-11-00-810-809A, BLEED PRESSURE REGULATOR VALVE FAILED 20 PSI TEST PER STEP 2, REMOVED AND REPLACED BLEED PRESSURE REGULATOR IAW AMM 36-11-52-04. ALSO, REPLACED NR 1 ENGINE HIGH PRESSURE VALVE (HPV) IAW AMM 36-11-51-04, AND AS A PRECAUTION REPLACED TEMPERATURE LIMITATION SOLENOID THERMOSTAT IAW AMM 36-11-55-000-001. OPERATIONAL AND LEAK CHECK WAS GOOD. SUPP - VENDORS INCOMING TEST OF PRESSURE REGULATOR VALVE S/N 00513 CONFIRMED REASON FOR REMOVAL, UNIT FAILED INTERNAL LEAKAGE TEST.

Part: FUEL CONTROL — MALFUNCTIONED (NR 1 ENGINE) · airframe 12,719 hrs · 4,888 cycles

PHX - ABORTED TAKEOFF - FLT 0820 - ON TAKEOFF AT PHX EN ROUTE FOR BOS THE NR 1 ENGINE FAILED TO ACCELERATE, REJECTED TAKEOFF AT 60 KTS. TAXIED CLEAR OF RUNWAY AND RAN UP NR 1 ENGINE, ENGINE AGAIN FAILED TO ACCELERATE ABOVE 1.1 EPR, RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE ELECTRONIC ENGINE CONTROL IAW T/C R5M73302, OPERATIONAL CHECK WAS GOOD. FUNCTIONAL TEST OF ELECTRONIC ENGINE CONTROL CONFIRMED FAILURE OF UNIT FOR SENSOR FAILURE. REPLACED P2 SENSOR, P5 SENSOR, PAMB SENSOR, AND PB PORT SCREEN IAW CMM 73-28-02, REV. 0. UNIT TESTED AND RETURNED TO SERVICE IAW HS14743.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 11,984 hrs · 4,625 cycles

NR 1 GENERATOR INOPERATIVE AND ON (MEL), APU AUTO SHUTDOWN AT 330 FT, ATTEMPTED 1 RESTART, NO LUCK, DIVERTED & LANDED WITHOUT FURTHER EVENT. MAINT R & R NR 1 IDG, OPS CHK GOOD. MAINT FOUND APU BEARINGS GRINDING & DAMAGE TO BLADES, R & R APU, OPS CHECK GOOD. INCOMING TEST & VISUAL INSPECT OF IDG COULD NOT VERIFY REASON FOR REMOVAL, UNIT DISASSEMBLED & INSPECTED, NO DISCREP NOTED, REPLACED SPEED SENSOR. CONFIRMED FAILURE OF APU TURBINE SECTION DAMAGE. PRIMARY CAUSE OF DAMAGE DUE TO TURBINE WHEEL SHAFT SEPARATION; THIS CAUSED SECONDARY DAMAGE TO LOAD COMP & COMP IMPELLERS. INLET GUIDE VANES, COMP DIFFUSERS, & TURBINE NOZZLE DAMAGED BY CONTACT WITH CENTER SHAFT. UNIT REPAIRED, TESTED, & RETURNED TO SERVICE.

Part: ACTUATOR — MALFUNCTIONED (NR 2 ENGINE) · airframe 11,181 hrs · 4,335 cycles

ON TAKEOFF ROLL AT SMF EN ROUTE FOR PHX RECEIVED NR 2 ENGINE COMPRESSOR VANE FAULT, REJECTED TAKEOFF AT 60 KTS. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75306, OPERATIONAL AND LEAK CHECK WERE GOOD PER T/C F5M71312. FUEL LACQUER BUILDUP DEGRADED UNIT PERFORMANCE SUFFICIENTLY ENOUGH TO PLAY AN INSTRUMENTAL PART IN REPORTED FAILURE MESSAGE.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 11,176 hrs · 4,332 cycles

ON TAKEOFF ROLL AT ORD EN ROUTE FOR PHX RECEIVED NR 2 ENGINE COMPRESSOR VANE FAULT, REJECTED TAKEOFF AT 60 KTS. MAINTENANCE INSPECTED ENGINE INLET AREA, NO DAMAGE NOTED. PERFORMED FULL AUTHORITY DIGITAL ENGINE CONTROL TEST ON THE NR 2 ENGINE PER TSM 75-30-00-810-846, ALL TESTS WERE GOOD. PERFORMED HIGH POWER ASSURANCE TEST IAW AMM 71-00-00-710-013-A, ALL ENGINE PARAMETERS ARE WITHIN LIMITS, NO FAULTS OR WANINGS ON PFR OR ECAM. COULD NOT DUPLICATE PROBLEM.

Part: BLEED ACTUATOR — FAULTY (ENGINE) · airframe 10,677 hrs · 4,139 cycles

ON TAKE OFF ROLL AT PHX EN ROUTE TO YYC, EGT LIMIT EXCEEDED (645) DEGREES. ABORTED TAKEOFF AND RETURNED TO GATE. MECHANIC REMOVED AND REPLACED THE 2.5 BLEED (LPC MASTER) ACTUATOR IAW AWA T/C R5M75307 AND PERFORMED POWER ASSURANCE TESTS IAW AWA T/C F5M71312 AS REQUIRED. VENDOR TEARDOWN OF LPC BLEED MASTER ACTUATOR S/N 1777839 CONFIRMED FAILURE OF UNIT. DURING RIG INVESTIGATION THE PISTON WOULD NOT EXTEND, ERRATIC MOVEMENT WAS ALSO FOUND DURING VELOCITY CHECKS, AND HIGH INTERNAL LEAKAGE WAS NOTED. REPLACED TORQUE MOTOR FOR ERRATIC MOVEMENT, AND REPLACED SEAL (P/N STD949-77) FOR INTERNAL LEAKAGE. UNIT TESTED IAW CMM 75-38-02, REV. 1.

Part: PRESSURE SENSOR — FAULTY (NR 1 ENGINE) · airframe 10,147 hrs · 3,935 cycles

CMH - DIVERSION - FLT 0045 - AFTER CLIMBOUT OF DCA EN ROUTE FOR PHX NOTICED HYDRAULIC POWER TRANSFER UNIT ON ECAM AFTER THRUST REDUCTION. ALSO DISPLAYED ECAM MESSAGE NR 1 ENGINE HYDRAULIC PUMP. DIVERTED TO CMH AS PRECAUTION. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP PRESSURE SWITCH (1074GK) IAW AMM TASK 29-11-17-000-010, OPERATIONAL AND LEAK CHECK WAS GOOD.

Part: SEAL — TORN (ZONE 210) · corrosion level 0 · airframe 9,371 hrs · 365 cycles

PHX - DIVERSION - FLT 0251 - ON CLIMB OUT FROM LAS EN ROUTE FOR PHL A NOISE WAS HEARD COMING FROM THE LEFT LOWER CORNER OF THE CAPTAINS WINDSHIELD. NOISE WAS INTERMITTENT AT FIRST, BUT AS DIFFERENTIAL INCREASED THE NOISE INCREASED AND THEN BECAME STEADY. DIVERTED TO PHOENIX WITHOUT FURTHER EVENT. MAINTENANCE REMOVED THE L/H WINDSHIELD AND PERFORMED VISUAL INSPECTION, NO DEFECTS WERE NOTED, REINSTALLED L/H WINDSHIELD IAW AMM 56-11-11-401. INSPECTED THE CAPTAINS L/H SLIDING WINDOW AND FOUND THE FORWARD LOWER CORNER SEAL TORN. REPLACED SEAL ON CAPTAINS L/H SLIDING WINDOW IAW 56-12-11. PRESSURIZATION CHECK WAS GOOD, NO LEAKS NOTED ON FLIGHT DECK WINDOWS.

Part: SLAT — CRACKED · corrosion level 0 · airframe 8,537 hrs · 3,367 cycles

MCN - MAJOR REPAIR - DURING B-02 CHECK A 1/2" CRACK AND 1/2" X 1/2" SECTION OF #2 SLAT WAS FOUND MISSING AT THE UPPER TRAILING EDGE 8" FROM THE INBOARD END. MAINTENANCE BLENDED OUT DAMAGED AREA ON #2 SLAT AT UPPER TRAILING EDGE INBOARD END; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; AND INSTALLED REPAIR PART IAW AWA E.R. 25-5740-02365-JS1.

Part: COMPUTER — FAILED (INERT GUIDANCE) · airframe 7,894 hrs · 3,126 cycles

FLT 0843 DURING CRUISE RECEIVED ECAM WARNING AP AUTOTHRUST YAW DAMPER 2 FAULT A/C "ALT LAW", DIVERTED TO ABQ. MAINTENANCE DOWNLOADED PREFLIGHT REPORT AND FOUND BOTH THE NR 2 AND 3 AIR DATA INERTIAL REFERENCE UNITS (ADIRU) FAILED. REMOVED AND REPLACED THE NR 3 ADIRU AND PLACED THE NR 2 ADIRU, COND. 4, NR 2 IR INOP. BITE TEST OF NR 3 ADIRU GOOD. MAINTENANCE REPLACED THE NR 2 ADIRU, SYSTEM OPS TEST WAS GOOD. VENDOR BENCH TEST OF ADIRU CONFIRMED FAILURE OF UNIT; IDENTIFIED REASON FOR FAILURE AS SLOW IGNITION GYRO. REPLACED SENSOR ASSEMBLY AND PERFORMED THERMAL CALIBRATION; FUNCTIONAL TEST WAS GOOD. VENDOR BENCH TEST OF ADIRU WAS NO FAULT FOUND; UNIT WAS THERMAL CALIBRATED, TESTED, AND RETURNED TO SERVICE.

Part: POWER SUPPLY — MALFUNCTIONED (CABIN) · airframe 7,825 hrs · 3,096 cycles

LAS - EEL - EMERGENCY POWER SUPPLY UNIT INDICATED LOAD MESSAGE ON FORWARD FLIGHT ATTENDANT PANEL AFTER EMERGENCY LIGHT TEST. MAINTENANCE REMOVED AND REPLACED FORWARD LT EMERGENCY POWER SUPPLY UNIT (11WL) IAW AMM 33-51-38-401, OPERATIONAL CHECK WAS GOOD.

Part: SIGN — BROKEN (CABIN) · airframe 5,043 hrs · 2,013 cycles

PHX - EEL - C - EMERGENCY EXIT SIGN HOUSING AND LENS BROKEN AT L1 DOOR. MAINTENANCE REMOVED AND REPLACED L1 EMERGENCY EXIT SIGN HOUSING AND LENS IAW AMM 33-51-16-401A.

Part: CYLINDER — FAILED (R1 DOOR) · airframe 4,800 hrs · 1,917 cycles

MAF - EMERGENCY EVACUATION - FLT 786 -O- REFERENCE SDR AWXA200100565, DURING EMERGENCY EVACUATION THE R-1 DOOR DAMPER CYLINDER (POWER ASSIST) FAILED TO FULLY OPEN THE R-1 DOOR AND THE ESCAPE SLIDE FAILED TO DEPLOY. THE L-1 & L-2 DOORS WERE USED FOR EVACUATION AND FUNCTIONED NORMALLY. LATER THE CAPTAIN MOVED THE R-1 DOOR FULLY OPEN BY HAND AND THE ESCAPED SLIDE DEPLOYED AND INFLATED NORMALLY. THE R-1 DOOR DAMPER CYLINDER WAS REMOVED AND TURNED OVER TO THE NTSB ON SITE AT MAF. SERVICEABLE SLIDES AND DOOR DAMPER CYLINDER ASSEMBLIES WERE INSTALLED ON THE L-1, L-2 & R-1 POSITIONS.

Part: BEARING — FRACTURED (NR 1 ENGINE) · airframe 4,800 hrs · 1,917 cycles

EN ROUTE ECAM MESSAGE FOR NR 1 ENG OIL FILTER CLOG APPEARED, FOLLOWED BY NR 1 ENG OIL PRESSURE RISE INTO THE RED AREA, NR 1 ENG HIGH VIBRATION & SMOKE IN THE CABIN. EXECUTED EMERGENCY DESCENT & LANDED AT MAF. MX REMOVED MAIN OIL FILTER & CHIP DETECTORS AND FOUND THEM CONTAMINATED WITH METALIC DEBRIS, ENG WAS REMOVED. TEAR DOWN OF NR 1 ENGINE REVEALED NR 3 BEARING FRACTURE AS CAUSE OF INCIDENT. NR 3 BEARING OUTER RING WAS FRACTURED AND EXHIBITED SIGNS OF RACEWAY SPALLING WITH OUTSIDE DIAMETER OF OUTER RING DISPLAYING SIGNS OF LOCALIZED FRETTING, FRACTURE INITIATED FROM OUTSIDE DIAMETER FRETTING AREA.

Part: CIRCUIT BOARD — FAULTY (COCKPIT) · airframe 4,449 hrs · 1,778 cycles

PHX - AIR TURNBACK - FLT 803 - C - DURING CLIMBOUT OF PHX TO SFO, THE NR 1 ENG FIRE LIGHT AT THE START SWITCH AND OVERHEAD INDICATION CAME ON TWICE, (NO ECAM INDICATION OR CRC). THE AIRCRAFT WAS RETURNED TO PHX MAKING AN UNEVENTFUL LANDING. MAINTENANCE TROUBLESHOT PER TSM 26-12-00-810 AND REPLACED ANNUNCIATOR LIGHT INTERFACE BOARDS 5LP & 18LP PER AMM 33-14-33. INDICATIONS AND OPERATIONAL TESTS WERE NORMAL. (NOTE: 2 BOARDS WERE REPLACED, SAME P/N).