N803AW

Part: LIGHT — FAULTY (ZONE 200) · airframe 79,842 hrs · 38,244 cycles

AIRCRAFT WAS NOT GROUNDED: DURING EMERGENCY LIGHT TEST FOUND MESSAGES ESPU INT LOAD AFT L,AND ESPU EXT AFT L. MAINTENANCE REPLACED ENTRANCE EMERGENCY LIGHT IAW AMM 35-51-11.

Part: ACCUMULATOR — LOW PRESSURE (ZONE 800) · airframe 79,842 hrs · 38,244 cycles

AIRCRAFT WAS NOT GROUNDED: R2 DOOR EMERGENCY ACCUMULATOR PRESSURE LOW 1100 PSI AT 37F. MAINTENANCE SERVICED R2 DOOR ACCUMULATOR IAW AMM 52-13-00.

Part: TRANS RECTIFIER — FAULTED (ZONE 100)

AIRCRAFT WAS GROUNDED: DCA-ORD AIR INTERRUPTED BACK TO DCA ACCOUNT DC ESSENTIAL BUS FAULT. FLIGHT DID NOT DECLARE AN EMERGENCY. AIRCRAFT WAS NOT OVERWEIGHT FOR LANDING. MAINTENANCE REPLACED #2 TANSFORMER RECTEFIER ( 1PU2 ) IAW AMM 24-32-51.

Part: ACTUATOR — LEAKING (ZONE 700) · airframe 79,607 hrs · 38,114 cycles

AIRCRAFT WAS GROUNDED: AFTER TAKEOFF AT APPROXIMATELY 1000-1200FT MSL, NOTICED CONTINUED LOUDER THAN NORMAL AIRFLOW NOISE, QUICKLY FOLLOWED BY HYD G RSVR LO LVL ECAM WITH ASSOCIATED L/G DOORS NOT LOCKED AND L/G OTUPLOCKED ECAMS. HYD SD SHOWED ALL HYD G PRESSURE AND FLUID COMPLETELY GONE. COMPLETED ECAM PROCEDURES. ACHIEVED GEAR DOWN AND LOCKED WITHOUT EMERGENCY EXTENSION SHOWING "DOWN 3 GREEN" WITH NORMAL CYCLE OF GEAR HANDLE TO DOWN POSITION. LANDED FLAPS FULL ATAPPROXIMATELY 127,000LBS. DECESION TO RETURN TO FILED, EMERGENACY DECLARED AND NORMAL TOUCHDOWN. TOWED TO GATE DUE TONWS INOP. MAINTENANCE REPLACED RH MLG LOCK STAY ACTUATOR CYLINDER IAW AMM 32-11-21.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 77,996 hrs · 37,069 cycles

AIRCRAFT WAS GROUNDED: EXIT SIGN CEILING IN BACK GALLEY. NOT ILLUMINATED. MAINTENANCE REPLACED AFT GALLEY EMERGENCY EXIT LIGHT IAW AMM 33-51-16.

Part: APU — ODOR (ZONE 100) · airframe 77,662 hrs · 36,850 cycles

AIRCRAFT WAS GROUNDED: DESCENDING BELOW 15000FT A LIGHT "DIRTY SOCK SMELL" BEGAN TO BENOTICED IN THE FLIGHT DECK AND ONE F/A ALSO NOTICED IT IN THE CABIN AROUND THE SAME TIME. AT THE GATE WITH THE APU RUNNING FOR AT LEAST 10 MIN THE SMELL BRIEFLY TURNED TO A STRONG WAXY SMELL FOR A FEW MINUTES BEFORE DISSIPATING TO THE PREVIOUS LIGHT SMELL. MAINTENANCE REPLACED APU IAW J/C 26L31049003.

Part: UNKNOWN — ODOR (CABIN) · airframe 77,662 hrs · 36,850 cycles

AIRCRAFT WAS GROUNDED: DESCENDING BELOW 15000FT A LIGHT "DIRTY SOCK SMELL" BEGAN TO BENOTICED IN THE FLIGHT DECK AND ONE F/A ALSO NOTICED IT IN THE CABIN AROUND THE SAME TIME. AT THE GATE WITH THE APU RUNNING FOR AT LEAST 10 MIN THE SMELL BRIEFLY TURNED TO A STRONG WAXY SMELL FOR A FEW MINUTES BEFORE DISSIPATING TO THE PREVIOUS LIGHT SMELL. (OPEN)

Part: BATTERY — DISCHARGED (ZONE 200) · airframe 77,395 hrs · 36,685 cycles

AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT ON AFT F/A CLEAR VIEW JUMP SEAT IS NOT FLASHING (REDLIGHT). MAINTENANCE REPLACED AFT FWD FACING F/A JUMP SEAT FLASH LIGHT BATTERY PER AMM 25-65-00, OP CHECK GOOD.

Part: BULB — BURNED OUT (ZONE 200) · airframe 76,789 hrs · 36,266 cycles

AIRCRAFT WAS GROUNDED: EXIT SIGN ABOVE 1L DOOR HAS LIGHT BULBS BURNED OUT. REMOVED AND REPLACED EXIT LIGHT ABOVE DOOR 1L PER AMM 33-51-17.

Part: BULB — BURNED OUT (ZONE 200) · airframe 76,789 hrs · 36,266 cycles

AIRCRAFT WAS GROUNDED: RIGHT OVER-WING EXIT SIGN HAS BURNED OUT BULBS. REMOVED AND REPLACED OVER-WING EXIT LIGHT PER AMM 33-51-18.

Part: FRAME — CRACKED (FRM 68 S22L) · airframe 75,346 hrs · 35,321 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME WEB HORIZONTAL FLANGE RADIUS ABOVE THE LOWER INBOARD DOOR STOP FITTING FASTENER AT FR 68 AND S22L. REPAIRED FRAME PER EA 351414.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 75,260 hrs · 35,270 cycles

AIRCRAFT WAS NOT GROUNDED: CREW REPORTED FLIGHT ATTENDANT FLASHLIGHT AT INBOARD JUMPSEAT IS MOUNTED BACKWARDS AND THEY CAN NOT SEE THE BLINKING RED LIGHT. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY PER AMM 25-65-00 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — INOPERATIVE (FWD FLASHLIGHT) · airframe 75,187 hrs · 35,230 cycles

AIRCRAFT WAS GROUNDED: FORWARD EMERGENCY FLASHLIGHTS NEED NEW BATTERIES WILL NOT FLASH. REMOVED AND REPLACED FORWARD FLASHLIGHT BATTERIES.

Part: LAMP — NO TEST (ZONE 200 - FUSE) · airframe 74,569 hrs · 34,821 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY EXIT LIGHT ON DOOR 4R INOPERATIVE. REPLAMPED EMERGENCY EXIT SIGN PER AMM 33-51-16 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LAMP — NO TEST (ZONE 200 - FUSE) · airframe 74,569 hrs · 34,821 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY EXIT LIGHTS AT SEAT ROW 14 ABC INOPERATIVE. MAINTENANCE RELAMPED EMERGENCY EXIT LIGHT SIGN AT SEAT ROW 14 ABC PER AMM 33-51-16 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — NO TEST (ZONE 200 - FUSE) · airframe 7,916 hrs · 2,122 cycles

AIRCRAFT WAS GROUNDED: LEFT EMERGENCY POWER SUPPLY UNIT BATTERY FAULT. MAINTENANCE REPLACED BATTERY PER AMM 33-51-38.

Part: POWER SUPPLY — NO TEST (ZONE 200 - FUSE) · airframe 73,069 hrs · 33,873 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT 10WL FAULTING DURING SYSTEM TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 10WL (AALA202303095357) AND BATTERY (AALA202303091079) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BATTERY — NO TEST (ZONE 200 - FUSE) · airframe 73,069 hrs · 33,873 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT 10WL FAULTING DURING SYSTEM TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 10WL (AALA202303095357) AND BATTERY (AALA202303091079) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: WARNING MESSAGE — ILLUMINATED (NR 2 BLEED SYS) · airframe 72,556 hrs · 33,542 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHX DUE TO AN AIR ENGINE #2 BLEED ABNORMAL PRESSURE MESSAGE DURING CLIMB OUT. FLIGHT CREW ACCOMPLISHED ECAM PROCEDURES WHICH RENDERED BLEED 2 INOPERATIVE. THE AIRCRAFT LANDED SAFELY AT PHX WITHOUT FURTHER INCIDENT. (OPEN)

Part: SENSE LINE — LOOSE (NR 2 BLEED) · airframe 72,556 hrs · 33,542 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHX DUE TO AN AIR ENGINE #2 BLEED ABNORMAL PRESSURE MESSAGE DURING CLIMB OUT. FLIGHT CREW ACCOMPLISHED ECAM PROCEDURES WHICH RENDERED BLEED 2 INOPERATIVE. THE AIRCRAFT LANDED SAFELY AT PHX WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE #2 ENGINE BLEED PRESSURE REGULATOR VALVE AND FOUND SENSE LINES LOOSE ALONG WITH THE CANNON PLUG BACKSHELL LOOSE (AALA202212204082). THE SENSE LINES AND THE CANNON PLUG BACK SHELL WERE TIGHTENED PER AMM 36-11-52. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.

Part: CONNECTOR — LOOSE (REGULATOR VALVE) · airframe 72,556 hrs · 33,542 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHX DUE TO AN AIR ENGINE #2 BLEED ABNORMAL PRESSURE MESSAGE DURING CLIMB OUT. FLIGHT CREW ACCOMPLISHED ECAM PROCEDURES WHICH RENDERED BLEED 2 INOPERATIVE. THE AIRCRAFT LANDED SAFELY AT PHX WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE #2 ENGINE BLEED PRESSURE REGULATOR VALVE AND FOUND SENSE LINES LOOSE ALONG WITH THE CONNECTOR PLUG BACKSHELL LOOSE (AALA202212204082). THE SENSE LINES AND THE CANNON PLUG BACK SHELL WERE TIGHTENED PER AMM 36-11-52. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.

Part: NONE — DEFECTIVE (ZONE 100 - FUSE) · airframe 71,432 hrs · 32,860 cycles

AIRCRAFT WAS GROUNDED: WITH AUTO PILOT OFF, CONTINUOUS NOSE DOWN PRESSURE REQUIRED TO MAINTAIN LEVEL FLIGHT OR CORRECT CLIMB ANGLE. WITHOUT PRESSURE THE AIRCRAFT PITCHES NOSE UP CONTINUOUSLY. MAINTENANCE REPLACED #2 ELEVATOR AILERON COMPUTER (ELAC) PER AMM 27-93-24. (AALA202207130949) ALSO REPLACED ACCELEROMETER (12CE4) PER AMM 27-92-16. (AALA202207135088) SATISFACTORY OPERATIONAL CHECKS WERE ACCOMPLISHED.

Part: ACCELEROMETER — DEFECTIVE (ZONE 100 - FUSE) · airframe 71,432 hrs · 32,860 cycles

AIRCRAFT WAS GROUNDED: WITH AUTO PILOT OFF, CONTINUOUS NOSE DOWN PRESSURE REQUIRED TO MAINTAIN LEVEL FLIGHT OR CORRECT CLIMB ANGLE. WITHOUT PRESSURE THE AIRCRAFT PITCHES NOSE UP CONTINUOUSLY. MAINTENANCE REPLACED #2 ELEVATOR AILERON COMPUTER (ELAC) PER AMM 27-93-24. (AALA202207130949) ALSO REPLACED ACCELEROMETER (12CE4) PER AMM 27-92-16. (AALA202207135088) SATISFACTORY OPERATIONAL CHECKS WERE ACCOMPLISHED.

Part: COMPUTER — NONE (ZONE 100 - FUSE) · airframe 71,428 hrs · 32,858 cycles

AIRCRAFT WAS GROUNDED: ECAM AUTO FLIGHT YAW DAMPER ILLUMINATION DURING TAKEOFF (APPROXIMATELY 70 KNOTS) REJECTED TAKEOFF. REPLACED #1 FLIGHT AUGMENTATION COMPUTER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 22-66-34.

Part: ACTUATOR — FAULTED (ZONE 400 - NAC/P) · airframe 70,697 hrs · 32,443 cycles

AIRCRAFT WAS GROUNDED: REJECTED TAKEOFF AT 60 KNOTS DUE TO ENGINE #2 COMPRESSOR VANE ECAM ALERT. RETURNED TO GATE. REPLACED ENGINE #2 VSV ACTUATOR PER JOB CARD 26T40075005. PERFORMED HIGH POWER ASSURANCE RUN PER JOB CARD 26L0071014. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — INOPERATIVE (ZONE 200 - FUSE) · airframe 69,936 hrs · 31,998 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY EXIT LIGHT INOPERATIVE OVER 2L AND 2R. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (AALA202112079070) AND BATTERY PER AMM 33-51-00.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200 - FUSE) · airframe 69,936 hrs · 31,998 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY EXIT LIGHT INOPERATIVE OVER 2L AND 2R. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT AND BATTERY (AALA202112072397) PER AMM 33-51-00.

Part: SIGN — INOPERATIVE (ZONE 200 - FUSE) · airframe 69,768 hrs · 31,892 cycles

AIRCRAFT WAS NOT GROUNDED: R2 ENTRY DOOR WALL MOUNTED EXIT SIGN HAS 7 EA ADJACENT LEDS INOPERATIVE EXCEEDS MEL LIMIT. REPLACED EXIT MARKER SIGN PER AMM 33-51-17.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200 - FUSE) · airframe 69,751 hrs · 31,878 cycles

AIRCRAFT WAS GROUNDED: BOTH AFT EXIT SIGNS BLINKING RAPIDLY, ALSO BOTH SLIDE ARMING SIGNS BLINKING ON DOOR/OXYGEN ELECTRONIC CENTRALIZED AIRCRAFT MONITOR. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (13WL) OPERATIONS CHECKS OK PER AMM 33-51-38-400-001-A.

Part: DIODE — INOPERATIVE (ZONE 200 - FUSE) · airframe 69,745 hrs · 31,874 cycles

AIRCRAFT WAS GROUNDED: THE AFT OVERHEAD AND BOTH AFT DOOR EXIT SIGNS ARE BLINKING RAPIDLY. ALSO BOTH AFT SLIDE ARMING SIGNS ARE BLINKING ON THE DOOR/OXYGEN ELECTRONIC CENTRALIZED AIRCRAFT MONITOR. ACCOMPLISHED TSM 33-51-00-810-819-A, FOUND DIODE PACK 1158VD BAD. REMOVED AND REPLACED DIODE PACK 1158VD IAW ASM 33-51-00.

Part: BATTERY — FAULTY (ZONE 200 - FUSE) · airframe 69,718 hrs · 31,865 cycles

AIRCRAFT WAS GROUNDED: THREE EXIT LIGHTS IN AFT GALLEY ARE FLICKERING. REPLACED EMERGENCY POWER SUPPLY UNIT 13WL BATTERY PER AMM 33-51-58.

Part: POWER SUPPLY — FAULTY (ZONE 200 - FUSE) · airframe 69,623 hrs · 31,814 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT EMERGENCY POWER SUPPLY UNIT FAILS BYTE TEST. REPLACED POWER SUPPLY PER AMM 33-51-38.

Part: DIAPHRAGM — LEAKING (ZONE 800 - DOORS) · airframe 69,622 hrs · 31,813 cycles

AIRCRAFT IN BASE MAINTENANCE: R2 DOOR DAMPER EMERGENCY OPERATION CYLINDER PRESSURE IS BLEEDING OFF. REPLACED DIAPHRAGM IN MECHANISM OF R2 DOOR DAMPER EMERGENCY OPERATION CYLINDER AND ACCOMPLISHED A SATISFACTORY LEAK CHECK PER AMM 52-10-00.

Part: INTERCOSTAL — CRACKED (ZONE 200 - FUSE) · airframe 69,592 hrs · 31,790 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND FORWARD PASSENGER / CREW DOOR CUT OUT INTERCOSTAL UPPER INBOARD FASTENER HOLE CRACKED AT FR 16 BETWEEN S8L AND S9L. REPLACED INTERCOSTAL PER SRM 51-72-11.

Part: FITTING — CORRODED (ZONE 400 - NAC/P) · corrosion level 2 · airframe 69,592 hrs · 31,790 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION OF LOWER SPIGOT FITTING ON RH ENGINE PYLON BETWEEN RIB 4 AND RIB 5 AT UPPER SPAR, MEASURING L=13.0 IN, W=1.312 IN, D=0.009 IN. REPLACED FITTING WITH NEW IAW SRM 54-51-12-300-002 AND DRAWINGS R54612042 AND R54612043.

Part: SPIGOT — CORRODED (ZONE 400 - NAC/P) · corrosion level 2 · airframe 69,592 hrs · 31,790 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION MEASURING L=13.00 IN, W=1.3125 IN, D=0.010 IN, ON LEFT ENGINE PYLON LOWER SPIGOT FITTING LOCATED BETWEEN PYLON RIB 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-002.

Part: ACCESS PANEL — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 69,592 hrs · 31,790 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND IN 17 COUNTER SINK HOLES ON FUEL PLATE ACCESS PANEL 640LB LOCATED ON THE RIGHT WING LOWER SURFACE, STR 8-11 AND RIB 16 - 17. REPLACED FUEL PLATE ACCESS PANEL 640LB PER WORK CARD 26C64057007.

Part: FITTING — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 69,592 hrs · 31,790 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION OF AFT CORNER SHAPE OF 2R DOOR SILL AT FR68, WL -500, AND BL Y-1410, MEASURING L=0.9 IN, W=0.5 IN, D=0.03 IN. REPLACED CORNER SHAPE WITH NEW IAW SRM 53-72-11.

Part: FLOORBEAM — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 69,592 hrs · 31,790 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION OF FLOOR BEAM ON UPPER SURFACE AT FR66, WL -500, AND BL 1162.5, MEASURING L=0.5 IN, W=0.5 IN, D=0.02 IN. REPLACED FLOOR BEAM WITH NEW IAW SRM 51-72-11 AND DRAWING D53472815.

Part: FLOORBEAM — CORRODED (FRM 66) · corrosion level 2 · airframe 69,592 hrs · 31,790 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON FLOOR BEAM LOCATED AT FR 66, WATERLINE Z-500, AND BUTT LINE Y765. 1.250 INCHES LONG BY 0.500 INCHES WIDE BY 0.035 INCHES DEEP. REMOVED AND REPLACED FLOOR BEAM PER SRM 51-72-11.

Part: FLOORBEAM — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 69,592 hrs · 31,790 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION OF FLOOR BEAM AT FR70-5 IN, WL -500, AND BL -765, MEASURING L=0.5 IN, W=0.5 IN, D=0.025 IN. REPLACED FLOOR BEAM WITH NEW IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FRM 70) · corrosion level 2 · airframe 69,592 hrs · 31,790 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON FLOOR BEAM LOCATED AT STA FR 70, WATERLINE Z-500, BUTT LINE Y 160.5. REMOVED AND REPLACED FLOOR BEAM PER SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FRM 70) · corrosion level 2 · airframe 69,592 hrs · 31,790 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON FLOOR BEAM LOCATED AT FR70 - 5", WATERLINE Z-500 AND BUTT LINE Y765 0.750 INCHES LONG BY 0.750 INCHES WIDE BY 0.040 INCHES DEEP. REMOVED AND REPLACED FLOOR BEAM PER SRM 51-72-11.

Part: FLOORBEAM — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 69,592 hrs · 31,790 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION OF FLOOR BEAM AT FR66, WL -500, AND BL Y-515, MEASURING L=1.0 IN, W=1.0 IN, D=0.025 IN. REPLACED FLOOR BEAM WITH NEW IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 69,592 hrs · 31,790 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION OF FLOOR BEAM AT FR64+10 IN, WL -500, AND BL Y-765, MEASURING L=1.5 IN, W=1.0 IN, D=0.015 IN. REPLACED FLOOR BEAM WITH NEW IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 69,592 hrs · 31,790 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION OF FLOOR BEAM AT FR66, WL -500, AND BL Y-512.5, MEASURING L=0.5 IN, W=0.5 IN, D=0.025 IN. REPLACED FLOOR BEAM WITH NEW IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FRM 70) · airframe 69,592 hrs · 31,790 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM AT FR 70 AND -Y150.5. REPLACED FLOOR BEAM PER SRM 51-42-11.

Part: THROTTLE — STUCK (COCKPIT) · airframe 69,248 hrs · 31,621 cycles

AIRCRAFT WAS GROUNDED: ON LANDING, BOTH THRUST LEVERS STUCK IN REV. AFTER CLEARING THE RUNWAY THEY WENT TO FORWARD THRUST WITH EFFORT. PREVIOUS LANDING WAS NORMAL OPERATION. REPLACED LEFT THROTTLE CONTROL UNIT (AALA202107132957) AND THE RIGHT THROTTLE CONTROL UNIT (AALA202107139367) AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 76-11-00-710-010-A13, AMM 76-11-19 AND AMM 78-31-00.

Part: THROTTLE — STUCK (COCKPIT) · airframe 69,248 hrs · 31,621 cycles

AIRCRAFT WAS GROUNDED: ON LANDING, BOTH THRUST LEVERS STUCK IN REV. AFTER CLEARING THE RUNWAY THEY WENT TO FORWARD THRUST WITH EFFORT. PREVIOUS LANDING WAS NORMAL OPERATION. REPLACED LEFT THROTTLE CONTROL UNIT (AALA202107132957) AND THE RIGHT THROTTLE CONTROL UNIT (AALA202107139367) AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 76-11-00-710-010-A13, AMM 76-11-19 AND AMM 78-31-00.

Part: BOLT — MISINSTALLED (THRUST REVERSER) · airframe 69,230 hrs · 31,610 cycles

AIRCRAFT WAS GROUNDED: THRUST LEVERS WOULD NOT MOVE BEYOND IDLE REVERSE ON LANDING. UPON FURTHER INVESTIGATION FOUND ROD END TO THROTTLE CONTROL UNIT BOLTS TO BE INCORRECTLY INSTALLED AND FOUND THROTTLES TO BE OUT OF RIG. INSTALLED BOLTS CORRECTLY (AALA202107123780) AND RIGGED THROTTLE LEVERS (AALA202107120629) IAW AMM 76-11-19.

Part: LEVER — OUT OF RIG (THRUST) · airframe 69,230 hrs · 31,610 cycles

AIRCRAFT WAS GROUNDED: THRUST LEVERS WOULD NOT MOVE BEYOND IDLE REVERSE ON LANDING. UPON FURTHER INVESTIGATION FOUND ROD END TO THROTTLE CONTROL UNIT BOLTS TO BE INCORRECTLY INSTALLED AND FOUND THROTTLES TO BE OUT OF RIG. INSTALLED BOLTS CORRECTLY (AALA202107123780) AND RIGGED THROTTLE LEVERS (AALA202107120629) IAW AMM 76-11-19.

Part: TRANSDUCER — FAULTED (NR 1 ENG BLEED) · airframe 68,666 hrs · 31,295 cycles

AIRCRAFT WAS GROUNDED: AFTER TAKEOFF ECAM MESSAGE FOR ENGINE 1 BLEED. CREW ATTEMPTED RESET BUT FAILED A SECOND TIME. EMERGENCY WAS DELARED. TESTED THE OVER PRESSURE VALVE PER AMM 36-11-53-720-001-A. ALSO CHANGED THE PRESSURE TRANSDUCER PER AMM 36-11-16.

Part: CONNECTOR — UNSECURE (POWER SUPPLY) · airframe 68,655 hrs · 31,287 cycles

AIRCRAFT WAS GROUNDED (SHORT TERM STORAGE): EMERGENCY POWER SUPPLY UNIT AT 10WL FAILS TEST. RESECURED CANON PLUG.

Part: MODULE — INOPERATIVE (EXIT SIGN) · airframe 68,466 hrs · 31,190 cycles

AIRCRAFT NOT GROUNDED. 1L EXIT LIGHT-HALF IS BURNED OUT. REPLACED EXIT SIGN LIGHTING MODULE PER AMM 33-51-17.

Part: WINDOW — MALFUNCTIONED (COCKPIT) · airframe 68,055 hrs · 30,979 cycles

AIRCRAFT NOT GROUNDED: FO WINDOW CAME OPEN ON T/O ROLL WILL NOT CLOSE. INSPECTED AND CLOSED COCKPIT WINDOW IAW AMM 56-12-11. OPS CHECK GOOD.

Part: APU — LEAKING · airframe 66,270 hrs · 29,915 cycles

AIRCRAFT WAS GROUNDED: F/A REPORTED ODOR AFT OF CABIN 10 MINUTES PRIOR TO LANDING, PAX WERE COUGHING AND REPORTED BURNING EYES. MAINTENANCE DETERMINED APU TO BE THE SOURCE. MAINTENANCE REMOVED AND REPLACED THE APU IAW CARD 26L31049005. OPS CHECKED GOOD.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 65,761 hrs · 29,632 cycles

AIRCRAFT WAS GROUNDED. PILOT REPORTED AT AROUND 6000 FEET, THE SAFETY VALVE WENT TO FULL OPEN, DEPESSURIZATION ENSUED. THE CABIN RATE OF DESCENT GOT TO 1400 FPM. MAINTENANCE RESET FCU IAW TSM 24-00-00-817-818-C1. NO FAULTS, OK FOR SERVICE.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 65,701 hrs · 29,592 cycles

CRACK INDICATION FOUND ON THE RIGHT WINDSHIELD POST FRAME 4 VERTICAL WEB OF THE SIDE POST BELOW 1ST OFFICERS SLIDING WINDOW. REPLACED WINDOW FRAME IAW EA 291511.

Part: CYLINDER — LEAKING (R2 DOOR ASSIST) · airframe 65,714 hrs · 29,601 cycles

MAINTENANCE REPORTED THAT THE R2 DOOR ASSIST CYLINDER WAS LEAKING AT THE ACTUATOR PISTON SHAFT BODY HOUSING, WHEN THE DOOR IS OPENED AND CLOSED. REMOVED AND REPLACED THE R2 DOOR ASSIST ACTUATOR IAW AMM 52-13-14-400-001-B.

Part: LOCK — BROKEN (R1 DOOR SLIDE) · airframe 65,714 hrs · 29,601 cycles

MAINTENANCE FOUND THE R1 ESCAPE SLIDE COVER RELEASE BALLS AND PIN LOCK BROKEN. REPLACED THE R1 SLIDE.

Part: INTERCOSTAL — CRACKED (FRAME 16) · airframe 65,701 hrs · 29,592 cycles

CRACKED INTERCOSTAL AT FRAME 16, STRINGER 9R. REPLACED THE INTERCOSTAL IAW SRM 51-72-11.

Part: FAN — ODOR (CABIN) · airframe 65,110 hrs · 29,194 cycles

FUMES THROUGH OUT CABIN, DIRTY SOCK, MELTED WAX ODOR CONTINUED UNTIL TOUCHDOWN. ACCOMPLISHED J/C 26L00021001, 26L00021002,& 26L0004, FOUND SOURCE OF ODOR. AC DIVERTED INTO IAD ON ACCOUNT OF ODOR REPORTED IN CABIN. CREW DECLARED EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. ARFF MET FLIGHT AND C TAXIED TO GATE ON IT'S OWN POWER. REPLACED EXTRACT FAN 18HQ PER AMM 21-26-51. OPERATIONS CHECK GOOD.

Part: CONTROL UNIT — INOPERATIVE (FUEL SYSTEM) · airframe 65,110 hrs · 29,194 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT WING FUEL TANK PUMP VALVE INOPERABLE. MAINTENANCE REPLACED FUEL LEVEL SENSING CONTROL UNIT 2 PER AMM 28-46-34-0401 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LAMP — INOPERATIVE (EXIT SIGN) · airframe 65,007 hrs · 29,130 cycles

EXIT SIGNS LAMP INOPERATIVE, FORWARD AND AFT GALLEYS. REPLACED THE LAMPS . OPS CHECKED GOOD.

Part: DOOR — MISSING (ZONE 100) · airframe 64,223 hrs · 28,697 cycles

ON ARRIVAL AT THE GATE, THE DOOR WAS FOUND MISSING. AIRCRAFT WAS GROUNDED. INSTALLED A NEW FUEL SERVICE DOOR IAW AMM 52-42-18.

Part: LEVER — BINDING (L1 DOOR) · airframe 63,498 hrs · 28,265 cycles

ARMING LEVER ON THE L1 DOOR STICKING. INSPECTED THE L1 DOOR ARMING LEVER FUNCTION, CHECKED OK. INSPECTED THE GIRT BAR AND GIRT BAR FLOOR FITTING BRACKET, NO DEFECTS NOTED. OPERATED THE L1 DOOR ARMING LEVER SEVRAL TIMES. OPS CHECKED OK IAW AMM 52-11-00.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 63,454 hrs · 28,241 cycles

R2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER INDICATING 200 PSI. SERVICED THE CYLINDER TO 1800 PSI, IAW AMM 52-10-00. NO LEAKS NOTED.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 63,231 hrs · 28,120 cycles

AFT INBOARD FLASHLIGHT UNDER FLIGHT ATTENDANT JUMPSEAT NEEDS A NEW BATTERY PACK. REPLACED THE BATTERY PACK.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 63,224 hrs · 28,114 cycles

MULTIPLE BULBS BURNED OUT OF THE CENTER AISLE OVERHEAD EMERGENCY EXIT SIGN. REPLACED THE LAMPS IN THE EXIT SIGN. OPS CHECKED GOOD IAW AMM 33-51-11.

Part: RESERVOIR — LOW PRESSURE (R2 DOOR) · airframe 63,123 hrs · 28,043 cycles

AIRCRAFT WAS NOT GROUNDED. R2 PASSENGER DOOR DAMPER CYLINDER RESERVIOR PRESSURE LOW. SERVICED R-2 DOOR DAMPER EMERGENCY OPERATION CYLINDER RESERVIOR PER A319 AMM 52-10-00-614-001-A.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 63,036 hrs · 27,993 cycles

EXTERIOR CRACK ACROSS CAPTAINS WINDSHIELD, LEFT WINDSHIELD HEAT INOPERATIVE. AIRCRAFT WAS GROUNDED. COMPLETED WINDSHIELD, CAPTAIN SIDE REPLACEMENT IAW JOB CARD 26L210.

Part: LENS — CRACKED (CABIN) · airframe 62,139 hrs · 27,415 cycles

EMERGENCY EXIT LIGHT LENS CRACKED AND FELL OFF LIGHT NEAR DOOR L1. REPLACED EMERGENCY EXIT LIGHT LENS L1 DOOR.

Part: LIGHT — INOPERATIVE (SEAT 15) · airframe 61,993 hrs · 27,345 cycles

EMERGENCEY LIGHT AT SEATS 15 LEFT INOPERATIVE. REPLAED EMERGENCEY LIGHT

Part: LIGHT — BROKEN (SEAT 11C) · airframe 61,993 hrs · 27,345 cycles

EMERGENCY LIGHT IS BROKEN AT SEAT 11C. REPLACED EMERGENCY LIGHT ASSEMBLY.

Part: O-RING — LEAKING (APU) · airframe 61,238 hrs · 26,877 cycles

AIRCRAFT WAS GROUNDED. AIRCRAFT HAS STRONG DIRTY SOCK SMELL. F/A'S FROM INBD FLIGHT REPORTED STRONG ODOR ON DESCENT. FOUND O-RINGS ON VALVE ASSY ON OIL PUMP LEAKING. REMOVED AND REPLACED O-RINGS PER CMM 49-91-41.

Part: GENERATOR — LEAKING (APU) · airframe 61,144 hrs · 26,809 cycles

ODOR DURING CLIMB OUT, A DIRTY SOCK ODOR IN CABIN, BETTER IN CRUISE ALSO ON DESCENT. REMOVED AND REPLACED APU GENERATOR IAW AMM 24-23-51, OPS AND LEAK CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: ACCUMULATOR — LEAKING (HYD SYSTEM) · airframe 61,121 hrs · 26,794 cycles

AN EMERGENCY WAS DECLARED, DUE TO A LOW YELLOW HYDRAULIC SYSTEM. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE YELLOW ACCUMULATOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS GROUNDED

Part: SHADE — STUCK (CABIN) · airframe 60,870 hrs · 26,652 cycles

AIRCRAFT WAS NOT GROUNDED. LEFT HAND OVERWING EXIT DOOR WINDOW SHADE WILL NOT OPEN. REPLACED LEFT OVERWING EMERGENCY DOOR WINDOW SHADE PER AMM 25-23-47.

Part: BATTERY — DISCHARGED (AFT CABIN) · airframe 60,601 hrs · 26,497 cycles

EMERGENCY FLASHLIGHT INOPERATIVE AT AFT FLIGHT ATTENDANT STATION. REPLACED THE FLASHLIGHT BATTERY.

Part: OIL CAP — UNSECURE (APU) · airframe 60,477 hrs · 26,430 cycles

WHEN LANDING GEAR SELECTED DOWN NOTICEABLE ODOR IN FLT DECK. ODOR GOT STRONGER WHEN APU BLEED SELECTED ON GROUND AND WAS THEN NOTED IN AFT GALLEY. SECURED LOOSE APU OIL CAP AND CLEANED APU.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 58,643 hrs · 25,408 cycles

LOWER EMERGENCY EXIT LIGHT LENS COVER MISSING AT SEAT 14A. INSTALLED EMERGENCY EXIT LIGHT LENS COVER AT SEAT 14A.

Part: MECHANISM — DIRTY (GIRT BAR) · airframe 58,583 hrs · 25,366 cycles

AIRCRAFT WAS NOT GNDED. LT AFT DOOR WILL NOT STAY ARMED. INSPECTED DOOR ARMING SYS IAW AMM 52-10-00 & FOUND DEBRIS IN GIRT BAR MECHANISM. CLEARED DEBRIS. OPERATIONAL CHECKED NORMAL.

Part: ENGINE — SLOW (NR 2) · airframe 58,521 hrs · 25,325 cycles

ABORTED TAKEOFF. ACFT WAS GNDED. NR 2 ENG SLOW TO SPOOL ON TAKEOFF ROLL, FLIGHT CREW ABORTED TAKEOFF, BETWEEN 25 & 30 KNOTS & RETURNED TO THE GATE. ACCOMPLISHED TSM TASK 73-00-00-810-881-A, NR 2 ENG ACCELERATION TESTED NORMAL, FADEC TESTED NORMAL, NO FAULTS FOUND.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 57,093 hrs · 24,593 cycles

3S CHECK, RT FWD PAX DOOR ROTO SCAN REVEALS CRACK INDICATION AT FRAME 20 FLOOR CROSSBEAM SPLICE, ON UPPER FASTENER ROW 10TH INBD FROM FRAME. REPAIRED IAW EA 255503.

Part: SLIDE — DEFECTIVE (R2 DOOR) · airframe 57,093 hrs · 24,593 cycles

1S CHECK, UNABLE TO PROPERLY SECURE R2 SLIDE COVER TO SLIDE. INTERFERENCE FIT ISSUE. REPLACED R2 DOOR SLIDE IAW 26C84252006.

Part: FLOORBOARD — DELAMINATED (ZONE 100) · airframe 57,093 hrs · 24,593 cycles

3S CHECK, FLOOR PANEL BETWEEN FRAME 51 & 54, Y-254 & Y-765 DELAMINATED. REPLACED FLOOR PANEL IAW IRM 9701 REV G.

Part: BEAM — CRACKED (FUSELAGE) · airframe 57,093 hrs · 24,593 cycles

3S CHECK, LT SIDE BOX BEAM, UPPER FLANGE AFT HOLE CRACKED AT FRAME 43 & +Y1622. REPAIRED IAW EO 5315Y066.

Part: HINGE FITTING — WORN (RT MLG DOOR) · airframe 57,093 hrs · 24,593 cycles

3S CHECK, RT MLG DOOR FWD HINGE FITTING, WORN AROUND BOLT HOLE. REPLACED HINGE FITTING IAW SRM 53-36-11, 51-23-11 & DWG D5337060000.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,093 hrs · 24,593 cycles

3S CHECK, CORROSION ON FLOORBEAM, BETWEEN FRAME 64 & 68 AT +Y765. REPLACED FLOORBEAM IAW SRM 51-42-11 & 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,093 hrs · 24,593 cycles

3S CHECK, CORROSION ON FLOORBEAM, BETWEEN FRAME 64 & 68, AT -Y765. REPLACED FLOORBEAM IAW SRM 51-42-11 & 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,093 hrs · 24,593 cycles

3S CHECK, CORROSION ON FLOORBEAM, BETWEEN FRAME 65 & 66 AT +Y765. REPLACED FLOORBEAM IAW SRM 51-42-11.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,093 hrs · 24,593 cycles

3S CHECK, CORROSION ON THE L2 DOOR CUT OUT LOWER SILL PLATE, BETWEEN FRAME 66 & 68 AT +Y1589. REPLACED DOOR SILL PLATE IAW SRM 51-42-11 & 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,093 hrs · 24,593 cycles

3S CHECK, CORROSION ON FLOORBEAM, BETWEEN FRAME 64 & 66 AT Y-1292. REPLACED FLOORBEAM IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,093 hrs · 24,593 cycles

3S CHECK, CORROSION ON FLOORBEAM, BETWEEN FRAME 66 & 69 AT 1292. REPLACED FLOORBEAM IAW SRM 51-42-11 & 51-72-11.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 57,093 hrs · 24,593 cycles

3S CHECK, FLOOR PANEL 251UF, HAS DELAMINATION. REPLACED FLOOR PANEL IAW IRM 9701 REV G.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,093 hrs · 24,593 cycles

3S CHECK, CORROSION ON R2 DOOR CUT OUT LOWER SILL, BETWEEN FRAME 66 & 68 AT -Y1589. REPLACED DOOR SILL IAW SRM 53-41-14, SRM 51-42-11 & DWG D53480009.

Part: FITTING — CORRODED (TE FLAP) · airframe 57,093 hrs · 24,593 cycles

3S CHECK, CORROSION ON RT WING TE OTBD FLAP, NR 4 FLAP TRACK FITTING INSIDE FLAP AT RIB 15. REPLACED FLAP ASSEMBLY IAW AMM 7-54-62.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,093 hrs · 24,593 cycles

3S CHECK, CORROSION ON LT SHEAR PLATE, BETWEEN FRAME 69 & 70 AT +Y1162.5. REPLACED SHEAR PLATE IAW SRM 51-42-11.

Part: BEAM — CRACKED (FUSELAGE) · airframe 57,093 hrs · 24,593 cycles

3S CHECK, RT SIDE BOX BEAM HOLES 1, 3 & 4 ARE CRACKED AT FRAME 43 & -Y1622. REPAIRED IAW EO 5315Y066.

Part: IDG — DEFECTIVE (NR 1 ENGINE) · airframe 56,639 hrs · 24,320 cycles

EMERGENCY LANDING, CREW CALLED EN-ROUTE ASKING TO TALK TO MTC REGARDING AN IDG 1 OIL LOW PRESS WARNING & THE EXISTING MEL 49-1B ON THE ACFT. GIVEN THAT THE FLIGHT WAS ALREADY EN-ROUTE & ABOUT TO DESCEND. THEY CONTINUED AS PLANNED TO THE ORIGINAL DESTINATION BUT DID DECLARE AN EMER. REPLACED THE NR 1 ENG IDG IAW AMM 24-25-51. ACCOMPLISHED A SATISFACTORY LEAK & OPERATIONAL CHECK.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 56,326 hrs · 24,138 cycles

AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED BATTERY FOR AFT INBD LT FLASHLIGHT. OPERATIONS CHECKED GOOD.

Part: ACCUMULATOR — LOW PRESSURE (BRAKE) · airframe 55,827 hrs · 23,850 cycles

PARKING BRAKE FAILED TO HOLD ACFT IN PLACE AT THE GATE. PARK BRAKE ACCUMULATOR HANDLE IN ON POSITION, BRAKE PRESSURE ZERO ON TRIPLE INDICATOR. SERVICED YELLOW HYD SYS BRAKE ACCUMULATOR IAW AMM 12-14-32-616-002A. TRIPLE INDICATOR SHOWS 2000 PSI WITH PARKING BRAKE IN ON POSITION.

Part: LENS — MISSING (CABIN) · airframe 54,447 hrs · 23,019 cycles

CLEAR LENS MISSING SEAT 1C. REPLACED LENS ASSEMBLY. CHECKED OK.

Part: PLATE — OUT OF POSITION (EVAC SLIDE) · airframe 53,134 hrs · 22,266 cycles

THE RT OVERWING SLIDE STAINLESS PLATE OUT OF POSITION. REPOSITIONED PLATE IAW AMM 25-62-42-0401.

Part: WIRE HARNESS — FAULTY (CABIN) · airframe 52,560 hrs · 22,041 cycles

EMERGENCY LIGHT 8L INOPERATIVE. REPLACED EMERGENCY LIGHT SEAT HARNESS 8L, SYS OPERATIONS CHECKED GOOD IAW AMM 33-51-19.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 52,408 hrs · 21,981 cycles

CREW REPORTED A STANDING ODOR IN FLIGHT DECK DURING CRUISE & ON ENG SHUTDOWN. WE DID DE-ICE BUT APU BLEED WAS OFF FOR 2 MINUTES & PACKS WERE OFF FOR 5 MINUTES AFTER DE-ICE. R & R APU IAW JOB CARD 26L31049005. COMPLIED WITH TROUBLESHOOTING REPAIR & ECS DECONTAMINATION IAW JOB CARDS 26L00021001, 26L00021002, 26L31049009 & 26L00021004. FOUND NR 1 ENG BEARING DRAIN LEAKING OIL, INBD COWL. R & R GEARBOX BREATHER SEAL. RAN NR 1 ENG. LEAK CHECKED GOOD IAW AMM 72-60-31-000-010-A13.

Part: COMPUTER — FAULTY (NR 2 ELAC) · airframe 52,318 hrs · 21,940 cycles

AFTER TAKEOFF FROM PHX CREW RECEIVED AN ECAM FOR FLIGHT CONTROL ELAC2 PITCH FAULT. FLIGHT RETURNED TO FIELD AT PHX & LANDED WITHOUT INCIDENT. R & R THE NR 2 ELAC IAW 27-93-34-401 & 27-93-00-710-001.

Part: PACKING — LEAKING (APU) · airframe 52,142 hrs · 21,874 cycles

FLIGHT ATTENDANT'S COMPLAINED OF ACRID DIRTY SOCK CABIN ODOR AFTER APU START & APU BLEED ON WHILE ACFT WAS PARKED AT GATE. ACCOMPLISHED JOB CARD 26L00021001 & DETERMINED APU TO BE THE SOURCE OF THE ODOR. FOUND THE APU NR 4 CAVITY VENT TUBES LEAKING. R & R APU NR 4 CAVITY TUBE PACKING IAW MM 49-91-53. OPERATIONS CHECKED GOOD. FOUND THE APU INTAKE DIRTY, CLEANED APU INTAKE IAW MM 49-16-00-100-001, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,132 hrs · 21,871 cycles

SEVERAL BULBS INOPERATIVE ON EMERGENCY EXIT LIGHT ON DOOR L2. R1, R2 & L1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY IAW AMM 33-51-11, PB401. RELAMPED R2, L1 & R1 EMERGENCY EXIT LIGHTS. OPERATIONS CHECKED OK IAW AMM 33-51-11.

Part: ACTUATOR — FAULTY (NR 1 ENGINE) · airframe 51,707 hrs · 21,687 cycles

CREW REPORTED AN ENGINE NR 1 COMPRESSOR STALL AFTER APPLYING TAKEOFF POWER. SPEED WAS NO MORE THAN 20 KNOTS. FLIGHT RETURNED TO THE GATE. POST FLIGHT REPORT SHOWS "ENGINE 1 COMPRESSOR VANE" FAULT. MAINTENANCE ACCOMPLISHED BOROSCOPE INSPECTION OF ENGINE NR 1 STAGE 3 AND STAGE 6 IAW AMM 72-00-00-200-016-B-01. NO DAMAGE NOTED. R & R ENGINE NR 1 FUEL PUMP AND FMU WITH NO HELP. R & R ENGINE NR 1 2.5 BLEED ACTUATOR IAW AMM. ALSO, R & R ENGINE NR 1 VSV ACTUATOR IAW AMM. LEAK AND OPS CHECK GOOD.

Part: O-RING — LEAKING (APU OIL CAP) · airframe 51,040 hrs · 21,396 cycles

CREW REPORTED A DIRTY SOCKS ODOR COMING FROM PACKS ON DESCENT. MX R & R THE APU OIL SERVICE CAP O-RING. ALSO, FOUND APU OIL QUANTITY OVER FULL. DE-SERVICED APU TO CORRECT OIL LEVEL IAW AMM 49-90-00-600-001-A. DRAINED APPROXIMATELY .5 QUART FROM APU. COMPLIED WITH JC 26L00021001, 26L00021002 AND 26L00021004.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 50,862 hrs · 21,316 cycles

CREW REPORTED THE F/O FIXED SIDE WINDOW DEVELOPED A LARGE BUBBLE WHICH VISUALLY CHANGED DIMENSIONS ALONG WITH A LARGE OPTICAL DISTORTION SURROUNDING BUBBLE. WINDOW WAS TOO HOT TO TOUCH AT BUBBLE. REST OF WINDOW COLD TO TOUCH. SOON AFTER, GOT ECAM ANTI-ICE RT WINDOW. MX R & R F/O FIXED SIDE WINDOW IAW AMM 56-11-12. ALSO, R & R RT WINDOW HEAT COMPUTER IAW AMM 30-42-34.

Part: SKIN PANEL — SATURATED (LT ELEVATOR) · airframe 50,383 hrs · 21,111 cycles

C11 CHECK - FOUND WATER INDICATIONS (6) ON LT ELEVATOR UPPER SKIN PANEL, ALL AREAS ARE MARKED SN CG1100, PN D35055280001000. REPLACED LT ELEVATOR IAW AMM 27-34-41.

Part: FRAME — CRACKED (EMERGENCY EXIT) · airframe 50,307 hrs · 21,074 cycles

C11 CHECK-CRACK ON RT EMERGENCY OVERWING DOOR AFT FRAME SEGMENT BETWEEN FR40 TO FR41. REPLACED RT EMERGENCY OVERWING DOOR AFT FRAME SEGMENT BETWEEN FR40 TO FR41 IAW EO 5210Y228.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 50,307 hrs · 21,074 cycles

C11 CHECK - FOUND WATER INDICATIONS (16) ON RT ELEVATOR UPPER SKIN PANEL ALL AREAS ARE MARKED SN CC2082, PN D55280001-005. REPLACED RT ELEVATOR IAW EO 5511Y295.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 50,000 hrs · 20,933 cycles

CREW REPORTED THE FORWARD PORTABLE PA INOP. MAINTENANCE REPLACED FORWARD MEGAPHONE. REFERENCE AMM CHAPTER 20.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 49,901 hrs · 20,885 cycles

CREW REPORTS THE ECAM INDICATES A SMOKE LAVATORY DETECTOR FAULT. CAUTION LIGHT ALSO ON AT FORWARD CIDS PANEL IN CABIN. MAINTENANCE REMOVED AND REPLACED THE LAVATORY A SMOKE DETECTOR BITE TEST GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 46,720 hrs · 19,428 cycles

CHEMICAL ODOR SMELL BY FLIGHT CREW WITH REPORTED NOSE IRRITATION AND HEADACHE. REMOVED AND REPLACED APU PER TASK CARD 26L31049005. SUP WILL SUBMIT APU TEARDOWN REPORT UPON RECEIPT. HONEYWELL COULD NOT CONFIRM REASON FOR REMOVAL - NO SIGNS OF INGESTION OR LEAKS FOUND DURING APU SHOP VISIT. REPLACEMENT OF HEPA FILTERS AND / OR CLEANING OF APU MAY HAVE RESULTED IN CLEARING ODOR.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 46,195 hrs · 19,180 cycles

FORWARD MEGAPHONE IS NOT WORKING. REMOVED AND REPLACED MEGAPHONE AT FORWARD ENTRY. OPERATIONAL CHECK GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 43,591 hrs · 18,025 cycles

FLT 590 - BOI-PHX - EMERGENCY LIGHTS - OVERHEAD EMERGENCY EXIT SIGN BETWEEN OVERWING EXITS ROW 9 & 10 HAS 4 BULBS NOT ILLUMINATING. REMOVED AND REPLACED THE EXIT SIGN UNIT. OPERATIONAL CHECK WAS GOOD.

Part: TRANSMITTER — FAILED (NR 2 ENGINE) · airframe 43,301 hrs · 17,911 cycles

FLT 339 - SJD - IFSD - NR 2 ENG OIL QUANTITY DROPPED TO 2.5 QUARTS THEN 2 THEN TO 1.5 THEN 1 THEN TO ZERO AT THE TOP OF CLIMB. SHUTDOWN NR 2 ENG AND RETURNED TO SJD. REMOVED AND REPLACED OIL QUANTITY TRANSMITTER. OPERATIONAL CHECK WAS GOOD.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 39,973 hrs · 16,478 cycles

EMERGENCY LIGHTS - ROW 9 LT RED AISLE EMERGENCY EXIT LIGHT LENS MISSING. REPLACED MISSING EMERGENCY LIGHT LENS.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 39,647 hrs · 16,333 cycles

EMERGENCY LIGHT HARNESS ON PASSENGER SEAT 20 LEFT DAMAGED. REMOVED AND REPLACED EMERGENCY LIGHT HARNESS IAW AMM 33-51-19. OPERATIONAL CHECK WAS GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,647 hrs · 16,333 cycles

SAL - S4 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR63 TO FR64, Y1292. REPAIRED SEAT TRACK BETWEEN FR63 TO FR64, Y1292 IAW A319 SRM 53-00-15.

Part: BOLT — CORRODED (SLAT TRACK) · corrosion level 2 · airframe 39,647 hrs · 16,333 cycles

SAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LEFT WING NR 1 SLAT NR 2 SLAT TRACK ATTACH BOLT. REPLACED LEFT WING NR 1 SLAT NR 2 SLAT TRACK ATTACH BOLT IAW A319 AMM 27-84-63.

Part: SKIN — SATURATED (ELEVATOR) · airframe 39,647 hrs · 16,333 cycles

SAL - S4 - MAJOR REPAIR - TRAPPED WATER FOUND IN LEFT ELEVATOR UPPER & LOWER SKIN HONEYCOMB STRUCTURE 7.5 INCHES FROM LEADING EDGE & 11 INCHES FROM LIGHTNING STRIP 4 BETWEEN RIBS 4 & RIB 5. REPLACED LEFT ELEVATOR IAW A319 AMM 27-34-00-820-003-A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,647 hrs · 16,333 cycles

SAL - S4 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR63 + 2 INCHES TO FR63 + 6 INCHES, -Y1292. REPAIRED SEAT TRACK BETWEEN FR63 + 2 INCHES TO FR63 + 6 INCHES, -Y1292 IAW A319 SRM 53-00-15.

Part: PANEL — CRACKED (RT WING) · airframe 39,697 hrs · 16,333 cycles

SAL - S4 - MAJOR REPAIR - CRACK ON RIGHT WING FUEL TANK CLOSING PLATE BETWEEN RIBS 5 TO RIB 6. REPLACED RIGHT WING FUEL TANK CLOSING PLATE 640CZ BETWEEN RIBS 5 TO RIB 6 IAW A319 AMM 57-27-11.

Part: PANEL — CRACKED (LT WING) · airframe 39,647 hrs · 16,333 cycles

SAL - S4 - MAJOR REPAIR - CRACK ON LEFT WING FUEL TANK CLOSING PLATE BETWEEN RIBS 6 TO RIB 6B. REPLACED LEFT WING FUEL TANK CLOSING PLATE 540DZ BETWEEN RIBS 6 TO RIB 6B IAW A319 AMM 57-27-11.

Part: PANEL — CRACKED (RT WING) · airframe 39,647 hrs · 16,333 cycles

SAL - S4 - MAJOR REPAIR - CRACK ON RIGHT WING FUEL TANK CLOSING PLATE BETWEEN RIBS 6 TO RIB 6B. REPLACED RIGHT WING FUEL TANK CLOSING PLATE 640DZ BETWEEN RIBS 6 TO RIB 6B IAW A319 AMM 57-27-11.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,647 hrs · 16,333 cycles

MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FORWARD ENTRY DOOR LOWER CORNER FITTING AT FR 16, Z-520. REPLACED LOWER CORNER FITTING AT FR 16, Z-520 AT FORWARD ENTRY DOOR IAW EA NR 132837.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,647 hrs · 16,333 cycles

SAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LOWER CORNER FITTING AT LEFT FORWARD PASSENGER / CREW DOOR CUTOUT FR20, S23L. REPLACED LOWER CORNER FITTING AT LEFT FORWARD PASSENGER / CREW DOOR CUTOUT FR20, S23L IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,647 hrs · 16,333 cycles

SAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, Y765. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112812.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,647 hrs · 16,333 cycles

SAL - S4 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR45 TO FR46, Y1292. REPLACED SEAT TRACK BETWEEN FR45 TO FR46, Y1292 IAW A319 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,697 hrs · 16,333 cycles

SAL - S4 - MAJOR REPAIR - CORROSION ON SEAT TRACKS BETWEEN FR36 TO FR41, -Y1292. REPLACED SEAT TRACKS BETWEEN FR36 TO FR41, -Y1292 IAW A319 SRM 51-72-11.

Part: LENS — MISSING (CABIN) · airframe 38,990 hrs · 16,043 cycles

FLT 590 - SNA-PHX - EMERGENCY LIGHT AT 10C INOPERATIVE. REPLACED MISSING LENS.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 38,984 hrs · 16,036 cycles

FLT 431 - SFO-LAS - EMERGENCY EQUIPMENT - FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT. OPERATIONAL TEST WAS GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 38,809 hrs · 15,950 cycles

FLT 607 - ORD-LAS - EMERGENCY EQUIPMENT - FORWARD CABIN EMERGENCY POWER SUPPLY UNIT INOPERATIVE. REMOVED AND REPLACED FORWARD EMERGENCY POWER SUPPLY UNIT PER MAINTENANCE MANUAL 33-51-38-401-001. OPERATIONAL CHECK WAS GOOD.

Part: LENS — BROKEN (CABIN) · airframe 38,582 hrs · 15,829 cycles

FLT 103 - SEA-LAS - EMERGENCY LIGHTS - EMERGENCY EXIT LIGHTING LENS COVER AT SEAT 10C BROKEN. REPLACED LENS COVER AS REQUIRED.

Part: MEGAPHONE — CORRODED (CABIN) · airframe 38,532 hrs · 15,797 cycles

FLT 607 - ORD-LAS - EMERGENCY EQUIPMENT - FORWARD MEGAPHONE HAS CORROSION IN BATTERY COMPARTMENT. REMOVED AND REPLACED FORWARD MEGAPHONE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 36,803 hrs · 15,041 cycles

FLT 356 - PHX-SJO - EEL - FLASHLIGHT UNDER SECOND JUMPSEAT - TEST LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY. OPERATIONAL CHECK WAS GOOD.

Part: MOUNT — BROKEN (CABIN) · airframe 36,239 hrs · 14,799 cycles

FLT 635 - RDU-PHX - EEL - LAST ROW AIRCRAFT LEFT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT SEAT MOUNT. OPERATIONAL CHECK WAS GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,332 hrs · 14,396 cycles

SAL-C7- MAJOR REPAIR - CORROSION ON FLOOR BEAM AT FR 66, Y512. REPLACED FLOORBEAM AT FR66, Y512 IAW A318 SRM 51-72-11. (S)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,332 hrs · 14,396 cycles

SAL-C7 -MAJOR REPAIR- CORROSION ON RAIL SEAT LOCATION AT FR66 AND Y1292. REPLACED RAIL SEAT LOCATION AT FR66 AND Y1292 IAW A319 SRM 51-72-11. (S)

Part: PIN — CORRODED (LT MLG) · airframe 35,332 hrs · 14,395 cycles

SAL-C7 -MAJOR REPAIR- CORROSION ON REAR PINTLE PIN OF LT MAIN LANDING GEAR. REPLACED REAR PINTLE PIN OF LT MAIN LANDING GEAR IAW TASK CARD R4M32311. (S)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,332 hrs · 14,395 cycles

SAL - C7 - MAJOR REPAIR - CORROSION ON FLOORBEAM AT FR66 TO FR70, Y765. REPLACED FLOORBEAM AT FR66 TO FR70, Y765 IAW SRM A319 51-72-11. (S)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,332 hrs · 14,395 cycles

SAL - C7 - MAJOR REPAIR - CORROSION ON FLOORBEAM AT FR67 TO FR70, -Y765. REPLACED FLOORBEAM AT FR67 TO FR70, -Y765 IAW SRM A319 51-72-11. (S)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,332 hrs · 14,395 cycles

SAL - C7 - MAJOR REPAIR - CORROSION ON FLOORBEAM AT FR67 TO FR69, -Y1292. REPLACED FLOORBEAM AT FR67 TO FR69, -Y1292 IAW SRM A319 51-72-11. (S)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,332 hrs · 14,395 cycles

SAL-C7- MAJOR REPAIR- CORROSION ON SEAT TRACK AT FR16, BL-Y765. REPLACED SEAT TRACK AT FR16, BL-Y765 IAW A319 SRM 51-72-11. (A)

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 35,332 hrs · 14,395 cycles

SAL-C7-MAJOR REPAIR - CRACKED TRAY PLATE AT FR68 TO FR69, -Y1738. REPLACED -TRAY PLATE AT FR68 TO FR69, -Y1738 IAW A319 SRN 51-72-11. (S)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,322 hrs · 14,395 cycles

SAL-C7- MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR 16, BL-Y1292. REPLACED SEAT TRACK AT FR 16, BL-Y1292 IAW A319 SRM 51-72-11. (A)

Part: DUMMY RAIL — CORRODED (FUSELAGE) · airframe 35,332 hrs · 14,395 cycles

SAL-C7-MAJOR REPAIR - DUMMY RAIL CORRODED AT BS FR16 BL Y503. REPLACED DUMMY RAIL AT BS FR16 BL Y503 IAW A319 SRM 57-72-11. (S)

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 35,332 hrs · 14,395 cycles

SAL-C7- MAJOR REPAIR - SHEAR PLATE CORRODED FR69 TO FR70, -Y1732, S23R. REPLACED SHEAR PLATE FR60 TO FR70, -Y1732, S23R IAW A319 SRM 51-72-11. (S)

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 35,332 hrs · 14,395 cycles

SAL-C7- MAJOR REPAIR - SHEAR PLATE CORRODED BETWEEN FR69 TO FR70, Y1738. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, Y1738 IAW A319 SRM 51-42-11 AND 51-72-11. (S)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,332 hrs · 14,395 cycles

SAL-C7- MAJOR REPAIR - BEAM RAIL CORRODED AT FR66, Y1292. REPLACED BEAM RAIL AT FR66, Y1292 IAW A319 SRM 51-72-11. (S)

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 35,332 hrs · 14,395 cycles

SAL-CY- MAJOR REPAIR - EXCESSIVE PLAY ON NR 1 HINGE OF RUDDER AT RIB 2 VERTICAL STABILIZER STA 760. REPLACED FITTING ASSEMBLY AT RIB 2 VERTICAL STABILIZER STA 760 IAW A319 AMM 55-36-41. (S)

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 35,322 hrs · 14,395 cycles

SAL-C7- MAJOR REPAIR - EXCESSIVE PLAY ON HINGE NR 4 OF RUDDER. REPLACED NR 4 HINGE FITTING NR 4 AT RIB NR 6, HORIZONTAL STABILIZER STATION 2632 IAW A319 AMM27-21-00. (S)

Part: SEAT TRACK — CORRODED (CABIN) · airframe 35,332 hrs · 14,395 cycles

SAL-C7- MAJOR REPAIR - CORROSION ON CABIN SEAT TRACK FR20, -Y1292. REPLACED CABIN SEAT TRACK FR20, -Y1292 IAW A319 SRM 51-72-11. (S)

Part: PROXIMITY SWITCH — FAULTED (MLG DOORS)

LAS - FLT 268 - YYZ TO LAS - AFTER TAKEOFF, RECEIVED ECAM MESSAGE "L/G DOORS NOT LOCKED". CREW RECYCLED THE GEAR AND RECEIVED A SATISFACTORY INDICATION. FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED PROXIMITY SENSOR FIN 23GA. OPERATIONALLY CHECKS OK.

Part: SILL — CORRODED (ZONE 200) · airframe 30,250 hrs · 12,296 cycles

SAL - FOUND CORROSION ON L2 DOOR CUT OUT LOWER SILL, FR 67 + 19", +Y1250. REPAIRED L2 DOOR CUT OUT LOWER SILL, FR 67 + 19", +Y1250 IAW A319 SRM 53-41-14.

Part: SILL — CORRODED (FUSELAGE) · airframe 30,250 hrs · 12,296 cycles

SAL - FOUND CORROSION ON L2 DOOR CUT OUT SILL BEAM SHAPE SILL, FR 60 - FR 68, S23L. REPLACED L2 DOOR CUT OUT SILL BEAM SHAPE SILL, FR 60 - FR 68, S23L IAW B737-300 SRM 51-72-11.

Part: FITTING — CORRODED (ZONE 200) · airframe 30,250 hrs · 12,296 cycles

SAL - FOUND CORROSION ON R1 DOOR SILL CENTER FITTING, FR16 + 6". REPLACED R1 DOOR SILL CENTER FITTING, FR16 - FR 20 IAW A319 SRM 51-72-11.

Part: FITTING — CORRODED (ZONE 100) · airframe 30,250 hrs · 12,296 cycles

SAL - FOUND CORROSION ON FORWARD CARGO COMPARTMENT DOOR CUT OUT THRESHOLD CORNER FITTING, FR 24A, S37R. REPLACED FORWARD CARGO COMPARTMENT DOOR CUT OUT THRESHOLD CORNER FITTING, FR 24A, S37R IAW A319 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,250 hrs · 12,296 cycles

SAL - FOUND CORROSION ON MAIN CABIN SEAT TRACK, FR 41 - FR 47, -Y1292. REPLACED MAIN CABIN SEAT TRACK, FR 41 - FR 47, -Y1292 IAW A319 SRM 51-72-11.

Part: ACTUATOR — BYPASSING (MLG) · airframe 23,776 hrs · 9,597 cycles

FLT 605 EN ROUTE TO DEN PILOT REPORTED THE NOSE LANDING GEAR WAS SLOW TO RETRACT AT APPROXIMATELY 20 SECONDS ECAM MESSAGE LANDING GEAR NOT UPLOCKED AND LANDING GEAR DOORS NOT CLOSED. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR ACTUATING CYLINDER PER AIRBUS AMM 32-31-22-04. MAINTENANCE SWUNG THE GEAR PER AWA TASKCARD F4N32301. SUBMITTED FOR INFORMATIONAL PURPOSES. TEAR DOWN REPORT SHOWS THAT THE UNIT'S OPERATIONAL TEST WAS NORMAL IN SHOP. NO FAULTS WERE FOUND. UNIT WAS OVERHAULED AND TESTED IAW MESSIER DOWTY CMM 32-37-12 REV. 2.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 19,928 hrs · 8,289 cycles

AIR TURN BACK - FLT 0051 - ON CLIMB OUT OF LAS EN ROUTE, RECEIVED AVIONICS VENT SYSTEM FAULT, AIRCRAFT PRESSURIZED NORMALLY, TURNED BACK TO LAS AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE ISSUED MEL 21-26-04 COND 1, "SKIN AIR OUTLET VALVE INOP". ON 05/31/2004 IN BOS: MAINTENANCE REMOVED AND REPLACED SKIN AIR OUTLET VALVE IAW AMM TASK 21-26-53-000-001, OPERATIONAL CHECK WAS GOOD. FUNCTIONAL TEST OF SKIN AIR OUTLET VALVE S/N 47 WAS NO FAULT FOUND. REMOVED ACTUATOR (S/N 188) AND TESTED ON ACTUATOR BENCH, NO FAULTS FOUND, REINSTALLED ACTUATOR. RETESTED UNIT AND RETURNED TO SERVICE IAW CMM 21-26-53, REV. 6.

Part: PROXIMITY SENSOR — DEFECTIVE (NLG) · airframe 18,975 hrs · 7,973 cycles

LAX - LANDING GEAR - FLT 0409 - ON DESCENT INTO LAX EN ROUTE FROM BOS WHEN LANDING GEAR WAS SELECTED DOWN, RECEIVED ECAM MESSAGE FOR LANDING GEAR NOT DOWN AND LOCKED. ALSO HAD 3 RED LIGHTS & LANDING GEAR DOOR OPEN INDICATIONS. RECYCLED LANDING GEAR HANDLE WITH SAME RESULT, THEN APPROXIMATELY 30 SECONDS LATER HAD NORMAL GEAR INDICATION. MAINTENANCE DOWNLOADED POST FLIGHT REPORT AND FOUND LGCIU NR 2 PROXIMITY SENSOR (39GA) TARGET POSITION MESSAGE. PER TSM 32-31-00-810-818, REMOVED AND REPLACED (SYSTEM 2) LT NOSE LANDING GEAR DOOR OPEN PROXIMITY SENSOR (39GA) IAW AMM 32-13-00-810-818, OPERATIONAL CHECKS WERE GOOD.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 18,346 hrs · 7,722 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON LOWER SIDE OF FLOOR PANEL 261FF FROM BS 31577 TO BS 32571, Y1600 TO Y1898, Z240. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 261FF FROM BS 31577 TO BS 32571, Y1600 TO Y1898, Z240 IAW AWA T/C C1D25310.

Part: RIB — CRACKED (NR 2 PYLON) · airframe 18,346 hrs · 772 cycles

DURING C-04 CHECK A .375 INCH CRACK WAS FOUND ON NR 2 ENGINE PYLON AFT FIXED FAIRING RIB 14 AT PYLON STATION 908. MAINTENANCE REMOVED AND REPLACED CRACKED NR 2 ENGINE PYLON AFT FIXED FAIRING RIB 14 AT PYLON STATION 908 IAW A319 SRM 51-42-11, FIG 2, 3, & 8, PG 8-10, 12, & 22, AND TABLES 1, 4, 7 5, FIG 8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,346 hrs · 7,722 cycles

DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON THE UPPER AND LOWER SURFACE OF FLOORBEAM AT FR 66, Y1292, Z240. MAINTENANCE REMOVED CORRODED FLOORBEAM FROM FR 64 TO FR 66, Y1292, Z240; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG D534-72209; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 PG 6-7, AND SRM 51-49-00 PG 5-6.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 18,346 hrs · 7,722 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON AFT LOWER SURFACE OF FLOOR PANEL 262FF. MAINTENANCE REMOVED CORROSION AND TRIMMED AWAY CORRODED AREA ON AFT LOWER SURFACE OF FLOOR PANEL 262FF; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW AWA ER 25-5302-03353-TB3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,346 hrs · 772 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM AT FR 68, Y1193, Z240. MAINTENANCE REMOVED CORRODED FLOORBEAM AT FR 68, Y1193, Z240; RECEIVED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 PG 6-7.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,346 hrs · 7,722 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK 4 AREAS OF GALVANIC CORROSION WERE FOUND ON FLOORBEAM 279MM AFT OF FR 67 AT Y1219, 431MM AFT OF FR 67 AT Y1143, 330MM AFT OF FR 67 AT Y1143, AND 220MM AFT OF FR 66 AT Y1292, Z240. MAINTENANCE REMOVED AND REPLACED FLOORBEAM FROM BS 31030 TO BS 33200, Y1143 TO Y1292, Z240 IAW A319 SRM 51-42-11 PG 6-7.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,346 hrs · 7,722 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM AT FR 68, Y1219, Z240. MAINTENANCE REMOVED CORRODED FLOORBEAM AT FR 68, Y1219, Z240; FABRICATED A NEW REPLACEMENT FLOOR BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 PG 6-7.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 18,346 hrs · 7,722 cycles

DURING C-04 CHECK A .5 INCH CRACK WAS FOUND IN LOWER RADIUS OF L- ANGLE ON LT SIDE OF FR 34 UNDER PANEL 191A, BS 14836. MAINTENANCE REMOVED CRACKED -L- ANGLE ON LT SIDE OF FR 34; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, PG 6-7, A23, & A27.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 18,346 hrs · 7,722 cycles

DURING C-04 CHECK A .5 INCH CRACK WAS FOUND IN LOWER RADIUS OF L-ANGLE ON RT AFT SIDE OF FR 34 UNDER PANEL 192AT, BS 14836. MAINTENANCE REMOVED CRACKED -L- ANGLE ON RT AFT SIDE OF FR 34; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, PG 6-7, A20-A23, & A27.

Part: DOOR — OUT OF RIG (PAX) · airframe 15,814 hrs · 6,768 cycles

EN ROUTE FROM LAS TO MIA THE FLIGHT DECK DOOR WAS EXTREMELY HARD TO OPEN. DOOR WOULD NOT CLOSE PROPERLY AND THE UPPER & CENTER LATCH WOULD NOT ENGAGE. MAINTENANCE RIGGED THE FLIGHT DECK DOOR IAW AMM 52-51-11, OPERATIONAL CHECK WAS GOOD.

Part: COVER — DELAMINATED (ESCAPE SLIDE) · airframe 13,397 hrs · 5,864 cycles

PHX - EMERGENCY ESCAPE EQUIPMENT - DURING POST FLIGHT INSPECTION THE EDGE OF THE LT OVERWING DUAL LANE SLIDE COVER WAS FOUND DELAMINATING. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING ESCAPE SLIDE PACK ASSEMBLY IAW T/C R1A25301.

Part: RESTRICTOR VALVE — OBSTRUCTED (NR 2 ENGINE) · airframe 12,722 hrs · 5,604 cycles

T/O ROLL APPROX 90 KTS, CAPT NOTICED NR 2 ENG HIGH OIL PRESSURE IND 332 PSI. AIRCRAFT RETURNED. MX REPLACED NR 2 ENG PRESSURE PUMP, NR 4 BEARING SCAVENGE VALVE & OIL FILTERS. PROBLEM PERSISTS, BUT OIL PRESSURE REDUCED TO ACCEPTABLE LIMITS FOR FERRY TO PHX. FILTERS EXAMINED & FOUND CONTAMINATED WITH CARBON. MX FLUSHED NR 2 ENG OIL SYS & DISCONNECTED. INSPECTED FOR DEBRIS & RECONNECTED OIL SYS RESTRICTORS & STRAINERS. NO DEBRIS FOUND. REPLACED NR 2 ENG INTERFACE UNIT, NR 4 BEARING PRESSURE TRANSDUCER & PROBLEM PERSISTS. REMOVED & REPLACED NR 2 ENG. DURING TEAR DOWN OF ENG OIL DISTRIBUTION SYS, A PIECE OF SAFETY WIRE FOUND UPSTREAM OF OIL DISTRIBUTOR RESTRICTOR. OIL JETS FOUND SATISFACTORY.

Part: PANEL — UNSECURE (EMERG EXIT DOOR) · airframe 9,145 hrs · 4,188 cycles

LAS - ABORTED TAKEOFF - 4/7/01 - AT APPROX 40 KIAS ECAM MESSAGE FOR THE LEFT EMERGENCY OVERWING EXIT DOOR OPEN ILLUMINATED AND THE TAKEOFF WAS ABORTED. A PAX REPORTED THE EMERGENCY DOOR HANDLE ACCESS COVER FELL OFF DURING INITIAL TAKEOFF ROLL. MAINTENANCE INSPECTED THE PANEL (FLAP ASSY HANDLE) AND DOOR; NO DISCREPANCIES NOTED. MAINTENANCE REINSTALLED PANEL AND THE AIRCRAFT WAS RETURNED TO SERVICE W/ NO FURTHER DISCREPANCIES.

Part: CONTACTOR — FAILED (BUS SWITCH) · airframe 8,020 hrs · 3,712 cycles

PHX - AIR TURNBACK - ON DEPARTURE AT APPROX 3000FT MSL THE CENTER ESSENTIAL BUS LOST POWER; CREW COMPLIED WITH ECAM ACTION AND RETURNED TO PHX; ND NR 1 WAS NOT POWERED, PFD NR 1 OPERATED NORMAL; AN OVERWEIGHT LANDING WAS MADE, SINK RATE WAS LESS THAN 200 FPM ON TOUCHDOWN. MAINTENANCE TROUBLESHOT IAW THE TSM AND REPLACED THE FOLLOWING PARTS: A.C. ESS. BUS SWITCHING CONTRACTOR P/N (MANUFACTURER ECE) 503CA02F1-02Y1, RECTIFIER P/N (MANUFACTURER ALLIED SIGNAL) NSA932901-02C, AND RELAY P/N (MANUFACTURER ALLIED SIGNAL) NSA932843AL01; ALL CHECKS GOOD; REF AMM 24-50-00.

Part: UNKNOWN — ODOR (CABIN) · airframe 7,476 hrs · 3,472 cycles

MELTING PLASTIC OR WIRING SMELL WAS NOTICED AT THE TOP OF CLIMB AND DISSIPATED AFTER TWO MINUTES. SMELL RETURNED DURING DESCENT WHILE PASSING THROUGH 140 FT, AGAIN DISSIPATING AFTER TWO MINUTES. SMELL WAS COMING FROM ROW EIGHT FORWARD. INSPECTED FWD COMPARTMENTS, BITE CHECKED ON BOARD SYSTEMS INCLUDING LIGHTING, RAN BOTH ENGINES AND PACKS FOR 15 MINUTES. ALSO RAN GALLEY EQUIPMENT, NO PROBLEMS FOUND.

Part: SLIDE — DEPLOYED (PAX DOOR) · airframe 5,335 hrs · 2,553 cycles

ON ARRIVAL AT TUS, SLIDE WAS DEPLOYED (DID NOT INFLATE). REPLACED ESCAPE SLIDE IAW CARD R1C25305. TT 0064631 RECOMMENDATION: REMAIN OPEN PENDING REVIEW OF TEARDOWN REPORT. NO HISTORY.