N732US

Part: MONITOR — INOPERATIVE (ENG VIBRATION) · airframe 66,940 hrs · 40,373 cycles

AIRCRAFT WAS GROUNDED: ENGINE #2 VIBRATION HIGH ON DEPARTURE. WITNESSED AS HIGH AS 9.9.PULLED #2 ENGINE BACK AND IT LOWERED WITHIN PARAMETERS. WHEN THRUST LEVEL PUT BACK IN, ENGINE VIBRATION REINTRODUCED. WENT REMAINDER OF FLIGHT WITH THRUST REDUCED AND REMAINED WITHIN PARAMETERS. RTB AS A PRECAUTION. DECESION MADE TO RETURN TO MIA. EMERGENCY DECLARED, AIRCRAFT WAS OVERWEIGHT FOR LANDING AND MET BY ARFF AND TAXIED TO GATE. MAINTENANCE REPLACE ENGINE VIBRATION MONITIORING UNIT IAW AMM 77-32-34.

Part: WEB — CRACKED (ZONE 100) · airframe 66,672 hrs · 40,195 cycles

AIRCRAFT IN BASE MAINTENANCE: 1.5" CRACK AT FRAME 68, STRINGER 22R. MAINTENANCE CUT OUT WEB AND INSTALLED NESTED FITTING IAW EA 369221 & DRAWING R3534222.

Part: BULB — INOPERATIVE (ZONE 200) · airframe 65,803 hrs · 39,643 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY LIGHT INOP AT FWD LH CLOSET. MAINTENANCE RELAMPED LIGHT IAW AMM 33-51-18.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 65,803 hrs · 39,643 cycles

AIRCRAFT WAS GROUNDED: L2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER REQ SERVICING PER PS CHK. MAINTENANCE SERVICED L2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDERTO PROPER LEVEL IAW AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 65,803 hrs · 39,643 cycles

AIRCRAFT WAS GROUNDED: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER REQ SERVICING PER PS CHK. MAINTENANCE SERVICED L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER TO PROPER LEVEL IAW AMM 52-10-00.

Part: LIGHT — NO TEST (ZONE 200) · airframe 65,600 hrs · 39,520 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY PATHWAY LIGHT AT SEAT 19 ABC INOP. MAINTENANCE REPLACED PATHWAY LIGHT AT SEAT 19 ABC IAW AMM 33-50-21.

Part: LIGHT — NO TEST (ZONE 200) · airframe 65,600 hrs · 39,520 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY PATHWAY LIGHT AT SEAT 18 ABC INOP. MAINTENANCE REPLACED PATHWAY LIGHT AT SEAT 18 ABC IAW AMM 33-51-21.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 65,600 hrs · 39,520 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT TEST FAILS L FWD EPSU BAT AND LIGHTS OUT AT SEAT 18 AND 19. MAINTENANCE REPLACED EPSU (10WL) BATTERY IAW AMM 33-51-38.

Part: LIGHT — NO TEST (ZONE 200) · airframe 65,291 hrs · 39,316 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR EMERGENCY LTS INOP. MAINTENANCE REPLACED CABIN EMERGENCY LIGHT, OPS. TEST GOOD IAW AMM 33-51-11. OK FOR SERVICE.

Part: DOOR LATCH — OUT OF ADJUST (ZONE 800) · airframe 65,105 hrs · 39,207 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY DOOR STUCK IN LOCKED POSITION. MAINTENANCE ADJUSTED LAVATORY DOOR KNOB / LATCH PER AMM 25-45-19. A SATISFACTORY OPERATIONAL CHECK WAS NOT ACCOMPLISHED.

Part: LANDING — SHEARED (ZONE 700) · airframe 64,865 hrs · 39,052 cycles

AIRCRAFT IN BASE MAINTENANCE: SHEARED HEAD SIDE OF HILOCK FASTENER (ANOMALY SHOWN WITH HFEC OF HOLE). MAINTENANCE REPLACED LH MLG DOOR.

Part: BOTTLE — LOW PRESSURE (L4 DOOR SLIDE) · airframe 63,599 hrs · 38,249 cycles

AIRCRAFT WAS GROUNDED: L4 DOOR SLIDE BOTTLE PRESSURE OUT OF SERVICEABLE LIMITS. REPLACED L4 DOOR ESCAPE SLIDE PER JOB CARD 2600025011.

Part: FAN — ODOR (RECIRCULATION) · airframe 63,397 hrs · 38,130 cycles

AIRCRAFT WAS NOT GROUNDED: ELECTRICAL BURNING SMELL ON DECENT. "COND" PAGE SHOWS FAN IN AMBER OVER COCKPIT. REMOVED AND REPLACED #1 CABIN RECIRCULATION FAN (15HG) PER AMM 21-21-51.

Part: LATCH — FAULTY (COCKPIT DOOR) · airframe 63,333 hrs · 38,090 cycles

AIRCRAFT WAS GROUNDED: PARKED AT THE GATE. UNABLE TO OPEN COCKPIT DOOR. REPLACED FLIGHT DECK DOOR CENTER LATCH MECHANISM PER AMM REF 52-51-21-400-001-A.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 63,316 hrs · 38,081 cycles

AIRCRAFT WAS NOT GROUNDED: DURING PS CHECK FOUND L2 PASSENGER DOOR EMERGENCY OPERATION CYLINDER PRESSURES LOW. SERVICED L2 PASSENGER DOOR EMERGENCY OPERATION CYLINDER PRESSURE PER AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 63,316 hrs · 38,081 cycles

AIRCRAFT WAS GROUNDED: DURING PS CHECK FOUND L1 PASSENGER DOOR EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED L1 PASSENGER DOOR EMERGENCY OPERATION CYLINDER PRESSURE PER AMM 52-10-00.

Part: DOOR — STUCK (COCKPIT) · airframe 63,046 hrs · 37,902 cycles

AIRCRAFT WAS NOT GROUNDED: COCKPIT DOOR WOULD NOT OPEN AFTER SHUT DOWN. ADJUSTED COCKPIT DOOR LATCH MECHANISM.

Part: PROXIMITY SENSOR — FAULTED (MLG) · airframe 62,802 hrs · 37,747 cycles

AIRCRAFT WAS GROUNDED: AFTER TAKEOFF LANDING GEAR DID NOT RETRACT. FLIGHT CREW REPORTED RECEIVED MULTIPLE OTHER WARNINGS. AS WE WERE WORKING THOSE WARNINGS, LANDING GEAR CAME UP. MAINTENANCE REVIEWED THE POST FLIGHT REPORT AND DETERMINED THAT THE MULTIPLE WARNINGS WERE RELATED TO A GEAR WEIGHT ON WHEELS CONFLICT OF THE PROXIMITY SENSORS ON THE MAIN GEARS AND NOTED THAT THE RIGHT MAIN LANDING GEAR PROXIMITY SENSOR 22GA HAD FAULT MESSAGES IN LGCIU #2. MAINTENANCE REPLACED PROXIMITY SENSOR 22GA ON THE RIGHT MAIN LANDING GEAR PER AMM 32-31-73-400-001.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: INOPERATIVE EMERGENCY POWER SUPPLY UNIT ASSEMBLY 13WL IN AFT GALLEY AREA. REPLACED EMERGENCY POWER SUPPLY UNIT 13WL AT GALLEY AREA PER AMM 33-51-38-000-001-A.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: INOPERATIVE EMERGENCY POWER SUPPLY UNIT ASSEMBLY 10WL AT FORWARD GALLEY AREA. REPLACED EMERGENCY POWER SUPPLY UNIT 10WL PER AMM 33-51-38-000-001-A.

Part: REGULATOR VALVE — MISALIGNED (SLIDE) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 SLIDE RAFT SAFETY PIN CAN NOT BE INSTALLED TO LOCKOUT THE SLIDE INFLATION RESERVOIR DUE TO THE LOCK PIN HOLES ON THE REGULATOR VALVE DO NOT ALIGN. MAINTENANCE INTENTIONALLY DEPLOYED THE SLIDE AND REMOVED THE SLIDE ASSEMBLY. **SUPPLEMENTAL REPORT FOR AALA202402288079: MAINTENANCE INSTALLED A SERVICEABLE SLIDE PER TASK CARD 26L00025011.** (CLOSED)

Part: REGULATOR VALVE — OUT OF POSITION (DOOR SLIDE) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 832 SLIDE RAFT SAFETY PIN CAN NOT BE INSTALLED TO LOCKOUT THE SLIDE INFLATION RESERVOIR DUE TO THE LOCK PIN HOLES ON THE REGULATOR VALVE DO NOT ALIGN. MAINTENANCE INTENTIONALLY DEPLOYED THE SLIDE AND REMOVED THE SLIDE ASSEMBLY. **SUPPLEMENTAL REPORT FOR AALA202402282813: MAINTENANCE REPLACED SLIDE RAFT ASSSMBLY PER TASK CARD 26L00025011 .** (CLOSED)

Part: REGULATOR VALVE — OUT OF POSITION (CREW DOOR SLIDE) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 SLIDE RAFT SAFETY PIN CAN NOT BE INSTALLED TO LOCKOUT THE SLIDE INFLATION RESERVOIR DUE TO THE LOCK PIN HOLES ON THE REGULATOR VALVE DO NOT ALIGN. MAINTENANCE INTENTIONALLY DEPLOYED THE SLIDE AND REMOVED THE SLIDE ASSEMBLY. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: REGULATOR VALVE — OUT OF POSITION (CREW DOOR SLIDE) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 832 SLIDE RAFT SAFETY PIN CAN NOT BE INSTALLED TO LOCKOUT THE SLIDE INFLATION RESERVOIR DUE TO THE LOCK PIN HOLES ON THE REGULATOR VALVE DO NOT ALIGN. MAINTENANCE INTENTIONALLY DEPLOYED THE SLIDE AND REMOVED THE SLIDE ASSEMBLY. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: RESERVOIR — MISALIGNED (SLIDE) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND EMERGENCY EXIT DOOR 844 OFFWING ESCAPE SLIDE SAFETY PIN CAN NOT BE INSTALLED TO LOCKOUT THE SLIDE INFLATION RESERVOIR DUE TO THE LOCK PIN HOLES ON THE REGULATOR VALVE DO NOT ALIGN. MAINTENANCE REMOVED THE INFLATION RESERVOIR. MAINTENANCE INSTALLED A SERVICEABLE INFLATION RESEVOIR.

Part: RESERVOIR — OUT OF POSITION (OVERWING SLIDE) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND EMERGENCY EXIT DOOR 844 OFFWING ESCAPE SLIDE SAFETY PIN CAN NOT BE INSTALLED TO LOCKOUT THE SLIDE INFLATION RESERVOIR DUE TO THE LOCK PIN HOLES ON THE REGULATOR VALVE DO NOT ALIGN. MAINTENANCE REMOVED THE INFLATION RESERVOIR. **SUPPLEMENTAL REPORT WILL BE SUBMITTED. ** (OPEN)

Part: DAMPER — NO TEST (ZONE 800 - DOORS) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: DO NOT PASS OPERATIONAL TEST DAMPING FUNCTION DOOR DAMPER ON PASSENGER CREW DOOR 832 AT AFT GALLEY AREA. REPLACED DOOR DAMPER ON PASSENGER CREW DOOR AT AFT GALLEY AREA.

Part: BOLT — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #12 LOWER AFT BOLT AT WS 14057 AND RIB 26. REPLACED BOLT PER TASK CARD 26C61057005.

Part: BOLT — CORRODED (NR 6 SLAT TRACK) · corrosion level 2 · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #6 UPPER FORWARD BOLT AT WES 6699 AND RIB 12. REPLACED BOLT PER TASK CARD 26C61057005.

Part: BOLT — CORRODED (NR 8 SLAT TRACK) · corrosion level 2 · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #6 LOWER FORWARD BOLT AT WES 6699 AND RIB 12. REPLACED BOLT PER TASK CARD 26C61057005.

Part: FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT JACK FITTING / BRACKET BETWEEN WS 70 AND WS 141, BETWEEN RIBS 2-3. REPAIRED JACK FITTING PER EA 114066A.

Part: ANCHOR FITTING — CORRODED (ZONE 500) · corrosion level 2 · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT BRACKET / ANCHORAGE FITTING BETWEEN WS 70 AND WS 141, BETWEEN RIBS 2 AND 3. REPAIRED ANCHORAGE FITTING PER EA 351074.

Part: SPIGOT — CORRODED (ZONE 400 - NAC/P) · corrosion level 2 · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT PYLON LOWER SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-001.

Part: FLOORBEAM — CORRODED (FRM 66) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM INBOARD UPPER SPLICE / SECTION-CONNECTING AT FR 66 AND -Y1292. REPLACED SPLICE / SECTION-CONNECTING PER SRM 51-42-11.

Part: SPIGOT — CORRODED (ZONE 400 - NAC/P) · corrosion level 2 · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT PYLON LOWER SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-001.

Part: SKIN PANEL — CORRODED (ZONE 600) · airframe 62,727 hrs · 37,680 cycles

AIRRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE BETWEEN RIB 13 AND RIB 17. REPAIRED SKIN PANEL PER EA 350498.

Part: SKIN PANEL — CORRODED (LT WING) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE BETWEEN RIBS 10 AND RIB 11 PLUS 14 INCHES. REPAIRED SKIN PANEL PER EA 350524.

Part: FITTING — CRACKED (FRM 16 S10-11R) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16, BETWEEN S10R AND S11R AT DOOR STOP #7. REPLACED INTERCOSTAL FITTING PER SRM 51-42-11.

Part: WEB — CRACKED (DOOR FRAME) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT RIGHT PASSENGER / CREW DOOR CUT OUT UPPER CORNER WEB CRACKED AT FR 68 BETWEEN S8R AND S9R. REPLACED WEB PER SRM 51-72-11.

Part: SKIN — CORRODED (RT WING TE) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE AT RIB 14 PLUS 10 INCHES. REPAIRED SKIN PANEL PER EA 350498.

Part: SKIN PANEL — CORRODED (LT WING) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE BETWEEN RIBS 14 AND 17. REPAIRED SKIN PANEL PER EA 350524.

Part: SHEAR PLATE — CRACKED (FRMS 69-70 S23R) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK ON SHEAR PLATE LOCATED AT STR 23R BETWEEN FR 69 TO FR 70 AT AFT GALLEY AREA. REPLACED SHEAR PLATE PER SRM 51-72-11-911-001.

Part: SEAT TRACK — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN BEAM-SEAT TRACK AT FR 21 AND -Y1292. REPLACED BEAM-SEAT TRACK PER SRM 51-42-11.

Part: FLOORBEAM — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM BETWEEN FR 64 AND FR 66 AT -Y765. REPLACED FLOOR BEAM PER SRM 51-42-11.

Part: SHEAR PLATE — CRACKED (FRMS 69-70 S23L) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FRM 66) · corrosion level 2 · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM-SEAT TRACK BETWEEN FR 64 AND FR 66 AT -Y1292. REPLACED FLOOR BEAM-SEAT TRACK PER SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FRM 16) · corrosion level 2 · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM-SEAT TRACK AT FR 16 AND +Y1292. REPLACED FLOOR BEAM-SEAT TRACK PER SRM 51-72-11.

Part: SKIN — CORRODED (RT WING TE) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE BETWEEN RIB 20 AND RIB 21 PLUS 8 INCHES. REPAIRED SKIN PANEL PER EA 350498.

Part: DUMMY RAIL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR DUMMY RAIL AT FR 16 AND +Y503.2. REPLACED DUMMY RAIL PER SRM 51-42-11.

Part: PLATE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN RAIL DUMMY RETAINER PLATE AT FR 14 AND -Y81. REPLACED RAIL DUMMY RETAINER PLATE PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRM 21) · corrosion level 2 · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM-SEAT TRACK AT FR 21 AND -Y765. REPLACED FLOOR BEAM-SEAT TRACK PER SRM 51-72-11.

Part: FITTING — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUTOUT LOWER CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23L. REPLACED CENTER SHAPE FITTING PER SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRMS 64-66) · corrosion level 2 · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM BETWEEN FR 64 AND FR 66 AT +Y765. REPLACED FLOOR BEAM PER SRM 51-72-11.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: LAVATORY "D" RIGHT HAND FLIGHT ATTENDANT SEAT FLASHLIGHT BATTERY INOPERATIVE. REPLACED FLASHLIGHT BATTERY.

Part: FLAP — CRACKED (RT WING) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING TRAILING EDGE OUTBOARD FLAP CRACKED BETWEEN RIBS 9 AND 10. REPAIRED FLAP PER SRM 57-53-00-300-029.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: LAVATORY "D" LEFT HAND FLIGHT ATTENDANT SEAT FLASHLIGHT BATTERY INOPERATIVE. REPLACED FLASHLIGHT BATTERY.

Part: PRESSURE DECK — CRACKED (ZONE 100) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR STRUCTURE PRESSURE DECK MEMBRANE HAS 6 FASTENER HOLES CRACKED AT FR 36 BETWEEN +Y1294 AND -Y1295. REPAIRED PRESSURE DECK MEMEBRANE PER EA 350303.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: LAVATORY "A" RIGHT HAND FLIGHT ATTENDANT SEAT FLASHLIGHT BATTERY INOPERATIVE. REPLACED FLASHLIGHT BATTERY.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: LAVATORY "A" LEFT HAND FLIGHT ATTENDANT SEAT FLASHLIGHT BATTERY INOPERATIVE. REPLACED FLASHLIGHT BATTERY.

Part: FLOORBEAM — CRACKED (FRM 36) · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR BEAM HAS 2 CRACKED FASTENER HOLES AT THE CENTER WING BOX FRONT SPAR COMMON TO VERTICAL STRINGER 4 AT FR 36 AND -Y254. REPAIRED FLOOR BEAM PER EA 350424.

Part: SKIN PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE BETWEEN RIB 7 AND RIB 8. REPAIRED SKIN PANEL PER EA 350498.

Part: SKIN PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE AT RIB 7 PLUS 5.5 INCHES. REPAIRED SKIN PANEL PER EA 350524.

Part: SKIN PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE AT RIB 11. REPAIRED SKIN PANEL PER EA 350498.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING UPPER SURFACE TRAILING EDGE TOP SKIN PANEL AT RIB 5 PLUS 26 INCHES. REPAIRED SKIN PANEL PER SRM 57-21-11-283-026.

Part: SKIN PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 62,727 hrs · 37,680 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE AT RIB 8. REPAIRED SKIN PANEL PER EA 350498.

Part: POWER SUPPLY — NO TEST (ZONE 200 - FUSE) · airframe 62,623 hrs · 37,610 cycles

DURING ACCOMPLISHMENT OF PERIODIC SERVICE CHECK MAINTENANCE FOUND CABIN EMERGENCY LIGHTS AT ZONE 1L INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY UNIT 10WL PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: HANDLE — STICKING (ZONE 900 - LAV/G) · airframe 62,236 hrs · 37,358 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR STICKS DURING FLIGHT AND DIFFICULT TO OPEN OR CLOSE, NO ISSUE ON GROUND. MAINTENANCE CLEANED AND LUBRICATED DOOR MECHANISM (AALA202310046862) AND DOOR HANDLE. (AALA202310049912) A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: MECHANISM — STICKING (ZONE 900 - LAV/G) · airframe 62,236 hrs · 37,358 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR STICKS DURING FLIGHT AND DIFFICULT TO OPEN OR CLOSE, NO ISSUE ON GROUND. MAINTENANCE CLEANED AND LUBRICATED DOOR MECHANISM (AALA202310046862) AND DOOR HANDLE. (AALA202310049912) A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BATTERY — INOPERATIVE (ZONE 200 - FUSE) · airframe 61,901 hrs · 37,140 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT 1R FLASHLIGHT DOES NOT WORK. MAINTENANCE REPLACED FLASHLIGHT BATTERY AT DOOR 1R AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — NO TEST (ZONE 200 - FUSE) · airframe 61,407 hrs · 36,808 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT OWERWING EXIT EMERGENCY POWER SUPPLY UNIT FAILED TEST. REMOVED AND REPLACED LEFT OWERWING EXIT EMERGENCY POWER SUPPLY UNIT BATTERY PER AMM 33-51-38. OPERATIONAL CHECKS GOOD.

Part: POWER SUPPLY — NO TEST (ZONE 200 - FUSE) · airframe 61,398 hrs · 36,803 cycles

AIRCRAFT WAS NOT GROUNDED: AFT EMERGENCY POWER SUPPLY UNIT FAILED TEST. REPLACED EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: SMOKE DETECTOR — FALSE ACTIVATION (ZONE 900 - LAV/G) · airframe 61,271 hrs · 36,739 cycles

AIRCRAFT WAS NOT GROUNDED: AFT STARBOARD SMOKE DETECTOR LAVATORY WENT OFF MOMENTARILY IN FLIGHT. MAINTENANCE INSPECTED LAVATORY AND PERFORMED A BITE TEST OF THE LAVATORY SMOKE DETECTION SYSTEM PER AMM 26-17-00 AND NO FAULTS WERE NOTED.

Part: LIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 60,869 hrs · 36,459 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT ROW 23 ABC EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT PER AMM 33-51-19 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 60,869 hrs · 36,459 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT ROW 22 ABC EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT PER AMM 33-51-19 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 60,725 hrs · 36,379 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR HARD TO OPEN AND CLOSE INFLIGHT. MAINTENANCE LUBRICATED AND ADJUSTED FORWARD LAVATORY DOOR PER AMM 25-41-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: TRIM PANEL — LOOSE (ZONE 800 - DOORS) · airframe 60,716 hrs · 36,375 cycles

AIRCRAFT WAS NOT GROUNDED: MAIN ENTRY DOOR (1L) HANDLE GETS CAUGHT ON PLASTIC ,MOULDING WHICH IS LOOSE CAUSING IT TO BE TOUGH TO OPEN DOOR. MAINTENANCE TIGHTENED AND SECIRED PLASTIC MOLDING AT L1 DOOR. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BATTERY — NO TEST (ZONE 200 - FUSE) · airframe 60,502 hrs · 36,244 cycles

AIRCRAFT WAS GROUNDED: LEFT HAND MID CABIN EMERGENCY POWER SUPPLY UNIT HAS BATTERY FAULT. MAINTENANCE REPLACED THE BATTERY PER AMM 33-51-04 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: SLIDE — NO TEST (ZONE 800 - DOORS) · airframe 60,502 hrs · 36,244 cycles

AIRCRAFT WAS GROUNDED: AFT EMERGENCY POWER SUPPLY UNIT FAILS SYSTEM TEST DUE TO INTERNAL AND EXTERNAL FAULTS. MAINTENANCE ISOLATED ISSUE TO THE L2 DOOR SLIDE AND REPLACED IT PER TASK CARD 26L00025011. A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WAS ACCOMPLISHED.

Part: DOOR — STICKING (ZONE 900 - LAV/G) · airframe 59,865 hrs · 35,828 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY 1L DOOR DIFFICULT TO OPEN AND CLOSE IN FLIGHT. MAINTENANCE LUBRICATED THE LAVATORY DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: RELAY — DEFECTIVE (ZONE 100 - FUSE) · airframe 59,821 hrs · 35,798 cycles

AIRCRAFT WAS GROUNDED: ALL CABIN EMERGENCY EXIT SIGNS CAME ON IN FLGHT. MAINTENANCE REPLACED RELAY 8WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: PANEL — NONE (ZONE 200 - FUSE) · airframe 59,411 hrs · 35,564 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY LIGHTS FAILED TO TEST. MAINTENANCE REPLACED FORWARD EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38 (AALA202209027842) AND THE PROGRAMMING AND TEST PANEL PER AMM 23-73-18. (AALA202209023352). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: POWER SUPPLY — NONE (ZONE 200 - FUSE) · airframe 59,411 hrs · 35,564 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY LIGHTS FAILED TO TEST. MAINTENANCE REPLACED FORWARD EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38 (AALA202209027842) AND THE PROGRAMMING AND TEST PANEL PER AMM 23-73-18. (AALA202209023352). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: NONE — CORRODED (ZONE 300 - STABS) · airframe 59,412 hrs · 35,564 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RUDDER RIGHT HAND SIDE TRAILING EDGE LOWER APEX STRIP APPROXIMATELY 20 INCHES UP FROM THE BOTTOM OF THE RUDDER. REPLACED RUDDER APEX STRIP PER SRM 55-41-19-300-006.

Part: SPRING — LACK OF LUBE (ZONE 900 - LAV/G) · airframe 59,327 hrs · 35,492 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY DOOR SPRING NOT WORKING DOOR DIFFICULT TO OPEN AND CLOSE. MAINTENANCE LUBRICATED LEFT LAVATORY DOOR SPRING AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: POWER SUPPLY — DEFECTIVE (ZONE 200 - FUSE) · airframe 58,962 hrs · 35,272 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY EXIT SIGN LIGHTS WON'T SHUT OFF. **SUPPLEMENTAL REPORT FOR AALA202206293598: REPLACED EMERGENCY POWER SUPPLY UNIT 10WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.** (CLOSED)

Part: SIGN — INOPERATIVE · airframe 58,962 hrs · 35,272 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY EXIT SIGN LIGHTS WON'T SHUT OFF. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: NONE — NONE (ZONE 100 - FUSE) · airframe 58,780 hrs · 35,177 cycles

AIRCRAFT WAS NOT GROUNDED: FUEL AUTO FEED FAULT IN FLIGHT, FOLLOWED ECAM PROCEDURES. MAINTENANCE REPLACED REPLACED THE FUEL LEVEL SENSING CONTROL UNIT #1 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 28-46-34.

Part: LINE — LEAKING (ZONE 400 - NAC/P) · airframe 58,634 hrs · 35,075 cycles

AIRCRAFT WAS GROUNDED: UPON SETTING TAKE OFF FLEX # 2 ENGINE TARGET IS 2 % LOWER THAN # 1 ENGINE ALL OTHER PARAMETERS NORMAL. MAINTENANCE FOUND #1 ENGINE PS12 LINE LOOSE / LEAKING AND REPLACED IT PER AMM 72-23-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: PIPE — CRACKED (ZONE 400 - NAC/P) · airframe 58,625 hrs · 35,069 cycles

AIRCRAFT WAS GROUNDED: FOUND #2 ENGINE PYLON FIRE EXTINGUISHING PIPE WITH LOWER "Y" OF PIPE MISSING/CRACKED AND SEPARATION. REPLACED FIRE EXTINGUISHING PIPE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 26-21-49

Part: SUPPORT — WORN (ZONE 400 - NAC/P) · airframe 58,625 hrs · 35,069 cycles

AIRCRAFT WAS GROUNDED: RIGHT HAND PYLON SUPPORT HAS WEAR MARK FROM SAFETY WIRE AT STATION 647 AND RIB 3. REPLACED SUPPORT PER SRM 54-51-18.

Part: LATCH — DIRTY (ZONE 900 - LAV/G) · airframe 58,373 hrs · 34,905 cycles

AIRCRAFT WAS NOT GROUNDED: L2 LAVATORY DOOR LOCK DIFFICULT TO WORK FROM INSIDE THE LAVATORY. CLEARED DEBRIS FROM DOOR LATCH AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LOCK — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 58,163 hrs · 34,789 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY ENTRY DOOR DIFFICULT TO OPEN AND CLOSE. ADJUSTED DOOR LOCK AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-50-00.

Part: PIN — INOPERATIVE (ZONE 800 - DOORS) · airframe 57,308 hrs · 34,294 cycles

AIRCRAFT WAS GROUNDED: AFTER SHUTDOWN 2L OVERWING SLIDE IS NOT ARMED ON THE ELECTRONIC CENTRALIZED AIRCRAFT MONITOR DOOR P AFTER SHUTDOWN 2L OVERWING SLIDE IS NOT ARMED ON THE ELECTRONIC CENTRALIZED AIRCRAFT MONITOR DOOR PAGE. RESET LEFT WING ESCAPE SLIDE LATCH PIN AMM 52-70-00.

Part: NONE — NONE · airframe 57,036 hrs · 34,131 cycles

AIRCRAFT WAS NOT GROUNDED: R2 DOOR INDICATED DISARMED DURING DESCENT WITH DOOR HANDLE IN ARMED POSITION. **SUPPLEMENTAL REPORT FOR AALA202110121672: OPERATIONAL CHECK ACCOMPLISHED PER TSM 52-13-00 WITH NO FAULTS NOTED, MAINTENANCE COULD NOT DUPLICATE FAULT. ** (CLOSED)

Part: NONE — NONE · airframe 57,036 hrs · 34,131 cycles

AIRCRAFT WAS NOT GROUNDED: R2 DOOR INDICATED DISARMED DURING DESCENT WITH DOOR HANDLE IN ARMED POSITION. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: CIDS — DEFECTIVE (ZONE 200) · airframe 56,772 hrs · 33,990 cycles

AIRCRAFT WAS GROUNDED: AURAL WARNING IN COCKPIT WITH PED SWITCH OFF. *SUPPLEMENTAL REPORT FOR AALA202109024543: REPLACED CIDS DIRECTOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 23-73-34** (CLOSED)

Part: WARNING HORN — ACTIVATED · airframe 56,772 hrs · 33,990 cycles

AIRCRAFT WAS GROUNDED: AURAL WARNING IN COCKPIT WITH PED SWITCH OFF. *SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: CONTROL UNIT — FALSE ACTIVATION (SMOKE DETECTION) · airframe 56,759 hrs · 33,984 cycles

AIRCRAFT WAS NOT GROUNDED: UPON TAKEOFF THE COCKPIT AURAL SMOKE ALERT SOUNDED CONTINUOUSLY. NO SMOKE OR ANY EVIDENCE IN THE CABIN PUT THE NO PORTABLE ELECTRONIC DEVICES SWITCH IN THE ON POSITION ALERT WENT OFF. RESEATED SMOKE DETECTOR CONTROL UNIT (SDCU) AND PERFORMED BITE CHECK PER AMM 26-17-00 WITH NO FAULTS NOTED, SYSTEM OPERATIONAL CHECKS GOOD. NO FAULTS WERE FOUND ON THE LAST LEG REPORT.

Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 56,749 hrs · 33,980 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY SMOKE AURAL ALERT IN COCKPIT. NO ECAM MESSAGE. NO CABIN INDICATIONS AURAL OR VISUAL. FLIGHT ATTENDANT CONFIRMED NO SMOKE. NO SMOKING ECAM APPEARS INTERMITTENT, COCKPIT AURAL ALERT REMAINED ON AFTER LANDING. MAINTENANCE PERFORMED LAV SMOKE DETECTOR TEST. NO FAULTS NOTED PER AMM 26-12-00.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 56,430 hrs · 33,814 cycles

AIRCRAFT WAS GROUNDED: FOUND L1 DOOR GIRT BAR/SLIDE ASSEMBLY LACING LOOSE AND HANGING. REMOVED AND REPLACED THE L1 ESCAPE SLIDE ASSEMBLY IAW WORKCARD 26L00025011.

Part: PRESSURE SWITCH — FAULTED (HYD SYSTEM) · airframe 56,180 hrs · 33,686 cycles

AIRCRAFT WAS GROUNDED: HYDRAULIC GREEN RESERVOIR LOW LEVEL ECAM 30 MINUTES AFTER TAKE OFF. COMPLIED WITH ECAM PROCEDURES, DECLARED AN EMERGENCY AND RETURNED TO PHX WHERE THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. MCDU SHOWED FAILURE MESSAGE FOR SYSTEM PRESSURE SWITCH, REPLACED SWITCH AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER AMM 29-32-12 AND 29-11-00.

Part: DECODER — FAULTY (ZONE 100) · airframe 55,586 hrs · 33,360 cycles

AIRCRAFT WAS GROUNDED: ACCOUNT REPEATS ON UNCOMMANDED EVAC WARNING. REPLACED FAULTY DEUB IAW AMM 23-73-47.

Part: DECODER — FAULTY (ZONE 100) · airframe 55,586 hrs · 33,360 cycles

AIRCRAFT WAS GROUNDED:EVAC COMMAND TRIGGERED IN FLIGHT. REPLACED FAULTY DEUB ( 300RH1) IAW AMM 23-73-47.

Part: FIRE LOOP — FALSE INDICATION (NR 1 ENGINE) · airframe 56,445 hrs · 33,821 cycles

AIRCRAFT WAS NOT GROUNDED: AT SHUTDOWN ELECTRONIC CENTRALIZED AIRCRAFT MONITOR ENGINE 1 FIRE LOOP A FAULT. ACCOMPLISHED TEST OF ENGINE 1 FIRE LOOP PER AMM 26-12-00 OPERATIONS CHECK NORMAL.

Part: APU — ODOR · airframe 55,307 hrs · 33,216 cycles

AIRCRAFT WAS GROUNDED. AFTER TAKEOFF F/A COMPLAINED OF UNIDENTIFIED ODOR, PASSENGERS ALSO COMPLAINED. ODOR HAD A FAINT ELECTRICAL SMELL. AIRCRAFT RETURNED TO DFW WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. SUPPLEMENTAL: ACCOMPLISHED APU SMOKE ODOR TROUBLESHOOTING TASK CARD 26L00021002, APU COMPRESOR CLEANING, AS PER AMM 49-20-100-004-A AND PACK DECONTAMINATION PER TASK CARD 26L00021004 WITH NO ODORS NOTE. AIRCRAFT RETURNED TO SERVICE. (SUPPLEMENTAL CLOSED)

Part: HOSE — BROKEN (HYD SYSTEM) · airframe 55,154 hrs · 33,132 cycles

AIRCRAFT WAS GROUNDED. CHEMICAL OR OILY SMELL IN DESCENT, APU WAS OFF. MAINTENANCE FOUND PUDDLES OF SKYDROL IN THE KEEL BEAM AREA AND FOUND HOSE GOING FROM RIGHT HAND MAIN LANDING GEAR NORMAL BRAKE MAINFIOLD COLLECTOR TANK BROKEN AND DRAINING INTO THE KEEL BEAM AREA. REPAIRED HOSE, PER AMM 29-17-11.

Part: PRESSURE SWITCH — DEFECTIVE (HYDRAULIC SYS) · airframe 545,340 hrs · 32,699 cycles

AIRCRAFT WAS GROUNDED: RECIEVED NR 1 ENGINE GREEN HYDRAULIC PUMP LOW PRESSURE AND GREEN SYSTEM LOW PRESSURE FAULT. DUE TO THE LOSS OF THE GREEN HYDRAULIC SYSTEM AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO DFW WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. REPLACED NR 1 ENGINE PUMP PRESSURE SWITCH AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER AMM 29-11-17 AND 29-11-00.

Part: HINGE FITTING — WORN (LG DOOR) · airframe 53,999 hrs · 32,353 cycles

AIRCRAFT WAS GROUNDED: RIGHT HAND FORWARD GEAR DOOR-FUSELAGE- FITTING DAMAGED ON INBOARD AREA OF REAR LUG ASSOCIATED WITH BEARING PLAY. **SUPPLEMENTAL REPORT: REPLACED LOWER GEAR DOOR HINGE FITTING PER SRM 51-42-11 (SEE ASSOCIATED REPORTS AALA202003069015, AALA202003089013 & AALA202003089014) ** (CLOSED)

Part: HINGE FITTING — WORN (RT MLG DOOR) · airframe 53,999 hrs · 32,353 cycles

AIRCRAFT WAS GROUNDED: RIGHT HAND MAIN LANDING GEAR DOOR FORWARD HINGE FITTING BEARING HAS FREE PLAY MOVEMENT OF APPROXIMATELY.030 INCHES. **SUPPLEMENTAL REPORT: REPLACED HINGE FITTING PER CMM 52-81-14. (SEE ASSOCIATED REPORTS AALA202003089013, AALA202003089014 & AALA202003119014) ** (CLOSED)

Part: HINGE FITTING — WORN (LG DOOR) · airframe 53,999 hrs · 32,353 cycles

AIRCRAFT WAS GROUNDED: RIGHT HAND FORWARD GEAR DOOR-FUSELAGE- FITTING DAMAGED ON INBOARD AREA OF REAR LUG ASSOCIATED WITH BEARING PLAY. **SUPPLEMENTAL REPORT: REPLACED LOWER GEAR DOOR HINGE FITTING PER SRM 51-42-11 (SEE ASSOCIATED REPORTS AALA202003069015, AALA202003089014 & AALA202003119014) ** (CLOSED)

Part: HINGE FITTING — WORN (LG DOOR) · airframe 53,999 hrs · 32,353 cycles

AIRCRAFT WAS GROUNDED: RIGHT HAND MAIN LANDING GEAR DOOR FORWARD FITTING ON DOOR IS DAMAGED AT UPPER END NEAR HINGE PLATE ASSOCIATED WITH BEARING PLAY. **SUPPLEMENTAL REPORT: REPLACED LANDING GEAR DOOR (SEE ASSOCIATED REPORTS AALA202003069015, AALA202003089013 & AALA202003119014)** (CLOSED)

Part: DAMPER — LOW PRESSURE (L1 DOOR) · airframe 53,717 hrs · 32,201 cycles

AIRCRAFT WAS NOT GROUNDED: L1 ENTRY DOOR DAMPER REQUIRED SERVICE. MAINTENANCE SERVICED DOOR DAMPER TO PROPER PRESSURE IAW AMM 52-10-00.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 53,717 hrs · 32,201 cycles

AIRCRAFT WAS GROUNDED: WHEN DOOR WAS OPENED SLIDE CAME OUT OF BUSSLE...DOOR WAS DISARMED PRIOR TO OPENING. REPLACED L1 DOOR SLIDE IAW JPC 26L00025011.

Part: PINTLE PIN — CORRODED (RT MLG) · airframe 53,218 hrs · 31,876 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING MAIN LANDING GEAR REAR PINTLE PIN CORRODED AT FLANGE EDGE. REPLACED PINTLE PIN PER TASK CARD 26T00032001.

Part: COMPUTER — INTERMITTENT (COCKPIT) · airframe 53,153 hrs · 31,830 cycles

AIRCRAFT NOT GROUNDED: AFTER TAKEOFF BOTH CAPTAINS DISPLAY UNITS AND UPPER ECAM DISPLAYWENT BLANK, CAME BACK ON A MIN LATER. HAPPENED A FEW TIMES DURING FLIGHT. REPLACED DMC1 IAW AMM 31-63-34. C/W LAND CAT III CAP TEST IAW AMM 22-97-00. SUPPLEMENTAL ACTION: SECT 4, AIRCRAFT NOT GROUNDED.

Part: LINE — RUPTURED (HYDRAULIC SYS) · airframe 53,053 hrs · 31,766 cycles

AIRCRAFT WAS GROUNDED: MAINTENANCE FOUND HYD FLUID IN FUEL RT WING TANKS WHILE TROUBLESHOOTING GREEN HYD LOW QYT WITH 4 SERVICES IN TWO DAYS, FOUND NO EXTERNAL HYD LEAKS. PERFORMED LEAK CHECK OF GREEN SYSTEM HYDRAULIC LINES IN R/H WING SURGE TANK. NO LEAKS FOUND. RT WING FUEL SAMPLE PRODUCED TRACE AMOUNTS OF WATER ONLY. MAINTENANCE FOUND NOSE GEAR CLOSURE LINE LEAKING. REMOVED AND REPLACED CONTAMINATED INSULATION AND REPLACED HYD LINE AND RE-INSTALLED ALL FWD CARGO PANELS AND FLOORING OPS LEAK CHECKS GOOD IAW AMM'S 25-54-11, 32-31-00 AARD 21-21-00, EA 299349.

Part: FCU — FAILED (ZONE 200) · airframe 52,892 hrs · 31,659 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS THAT DURING TAXI OUT SMELLED AN ODOR (ELECTRIC) AND F/O OBSERVED FUMES COMING OUT OF HIS SIDESTICK PRIORITY PANEL. RETURNED TO THE GATE AND DEPLANED ALL PAXS. MAINTENANCE REPORTS PROBLEM CAUSED BY MCP. REMOVED AND REPLACED MCP (FCU) IAW AMM 22-81-12-401-001-A, PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 22-10-00-710-001-A. SYSTEM CHECKED NORMAL.

Part: SPEED BRAKE — MALFUNCTIONED · airframe 52,705 hrs · 31,529 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS ON DESCENT OUT OF 8000' DURING FULL SPEED BRAKE EXTENSION, LEFT OUT BOARD PANEL WOULD NOT DEPLOY AND AIRCRAFT ROLLED LEFT. SPOILER DEPLOYMENT OKAY ON LANDING, ALL PANELS FUNCTIONED. MAINTENANCE PERFORMED TROUBLESHOOTING IAW TSM 27-60-00-810-840A. NO FAULTS NOTED. OPS TEST NORMAL. COULD NOT DUPLICATE FAULT.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,167 hrs · 31,228 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS OPS TEST OF EMERGENCY LIGHT SYS. FAILED EPSU UNIT EMER R. REMOVED AND REPLACED EPSU (12WL)IAW AMM 33-51-38-000-001/400-001.

Part: BATTERY PACK — FAULTED (CABIN) · airframe 51,960 hrs · 31,107 cycles

AIRCRAFT WAS NOT GROUNDED: EPSU BATTERY FORWARD LEFT FAULT. MAINTENANCE REPLACED FORWARD LEFT EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-38.

Part: POWER SUPPLY — FAULTED (CABIN) · airframe 51,960 hrs · 31,107 cycles

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

Part: UNKNOWN — UNKNOWN (THRUST) · airframe 51,345 hrs · 30,727 cycles

UNCOMMANDED AUTO-THRUST DISCONNECT ON ARRIVAL. PERFORMED AMM 22-30-00-040-004-A, PASSED, NO FAULTS NOTED.

Part: COVER — LOOSE (R2 DOOR SLIDE) · airframe 50,721 hrs · 30,293 cycles

L2 DOOR SLIDE COVER CAME OFF. SECURED THE DOOR SLIDE COVER. OK FOR SERVICE.

Part: COVER — DAMAGED (R2 DOOR SLIDE) · airframe 50,711 hrs · 30,288 cycles

R2 DOOR SLIDE PLASTIC COVER WAS DAMAGED. INSTALLED THE COVER IAW AMM 25-62-50. OK FOR SERVICE.

Part: PANEL — INOPERATIVE (CABIN) · airframe 50,443 hrs · 30,111 cycles

AIRCRAFT WAS NOT GROUNDED. CEILING EMERGENCY LIGHTS AT OVERWING EXITS INOPERATIVE. REPLACED CEILING PANEL ASSEMBLY AT OVERWING EXITS PER AMM 25-23-41. OPERATIONS CHECK ON EMERGENCY LIGHTS NORMAL.

Part: COOLING FAN — ODOR (ZONE 200) · airframe 49,760 hrs · 29,655 cycles

DURING DESENT AT 10000 - 8000FT MSL OILY ODOR IN COCKPIT. NO NOTICEABLE ODOR WAS DETECTED AT ANY CABIN LOCATION. THE AIRCRAFT WAS GROUNDED. REPLACED APU ACCESSORY COOLING FAN IAW AMM 49-52-00. APU DUCTS AND INLETS CLEANED. NO FURTHER ODOR NOTED AND AIRCRAFT IS OK FOR SERVICE.

Part: APU — ODOR (ZONE 400) · airframe 49,373 hrs · 29,419 cycles

THE AIRCRAFT WAS GROUNDED. SMELLED OIL FUMES WITH APU BLEED ON / STARTED ENGINES AND FUME SMELL CONTINUED. ACCOMPLISHED J/C 26L00021001, FOUND SOURCE OF CABIN ODOR TO BE APU. ACCOMPLISHED PACK BURN WITH ENGINES, NO ODORS NOTED AND AIRCRAFT IS OK FOR SERVICE.

Part: SENSOR — FAULTY (LT MLG) · airframe 49,268 hrs · 29,349 cycles

AIRCRAFT WAS GROUNDED. SHORTLY AFTER TAKE OFF WE RECEIVED ECAM LANDING GEAR DOOR NOT CLOSED. RECYCLED GEAR HANDLE AS PER ECAM TO NORMAL GEAR UP. REPLACED SENSOR (LMLG) 23GA PER MM 32-31-73-400, ADJ. PER MM 32-31-73-820, ACCOMPLISHED FUNCTIONAL TEST OF EXTENSION & RETRACTION PER 32-31-00-720. (NO FAULTS NOTED).

Part: FITTING — WORN (LT MLG DOOR) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. LEFT HAND MAIN LANDING GEAR DOOR FWD FITTING WAS FOUND TO BE WORN DURING A PREVIOUS MAINTENANCE VISIT AND WAS REPAIRED PER EA 261518. THIS FITTING WAS REPLACED DURING THE CURRENT MAINTENANCE VISIT PER EA 276186 AND SRM 51-72-11.

Part: FITTING — WORN (LT MLG DOOR) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. LEFT HAND MAIN LANDING GEAR DOOR AFT FITTING WAS FOUND TO BE WORN DURING A PREVIOUS MAINTENANCE VISIT AND WAS REPAIRED PER EA 261513. THIS FITTING WAS REPLACED DURING THE CURRENT MAINTENANCE VISIT PER EA 276186 AND SRM 51-72-11.

Part: SKIN PANEL — SATURATED (LT HORIZ STAB) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE. TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS LOCATED AT 47.3 IN. INBOARD FROM RIB 10 AND 3.5 IN. FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER. REPAIRED UPPER SKIN PANEL HONEYCOMB CORE ON LT HORIZONTAL STABILIZER PER ARM 51-21-11-300-005.

Part: FLOOR PANEL — DELAMINATED (FWD CARGO BAY) · airframe 48,505 hrs · 28,926 cycles

DELAMINATED FLOOR PANEL 131AF IN THE FWD CARGO COMPARTMENT. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-01.

Part: CYLINDER — INOPERATIVE (PAX DOOR) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE. PASSENGER CREW DOOR 842 AT AFT GALLEY AREA DAMPING FUNCTION DID NOT OPERATE CORRECTLY, BUFFER HIT FUSELAGE. REPLACED DOOR DAMPER CYLINDER PER AMM 52-13-14-400-001-B.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL ON 242FF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-013 PARA 2.

Part: STOWAGE BOX — CRACKED (COCKPIT) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CRACK STOWAGE CRASH AXE IN COCKPIT. REPLACED STOWAGE CRASH AXE IN COCKPIT PER AMM 51-42-11-001.

Part: SLIDE — DETERIORATED (LT OVERWING) · airframe 48,505 hrs · 28,926 cycles

DETERIORATED ENCLOSURE OF THE LEFT OVERWING ESCAPE SLIDE SURFACE COMPOUND ON LEFT WING. REPLACED ENCLOSURE OF THE SLIDE IAW AMM 25-62-42-400-001-A.

Part: SLIDE — DEFORMED (DOOR) · airframe 48,505 hrs · 28,926 cycles

OVER INFLATED DOOR SLIDE RAFT AT PASSENGER CREW DOOR 832 AT AFT GALLEY AREA. REPLACED SLIDE RAFT AT PASSENGER CREW DOOR 832 AT AFT GALLEY AREA IAW JOB CARD 26C83252008.

Part: LIFE RAFT — DEFORMED (CREW DOOR) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE. DEFORMATION ON PASSENGER CREW DOOR 842 SLIDE RAFT AT FORWARD GALLEY AREA. (WHEN DOOR IS FULLY OPEN SLIDE RAFT TOUCHES FUSELAGE). REPLACED AFT SLIDE RAFT PER JOB CARD 26C84252006.

Part: BOLT — CORRODED (SLAT TRACK) · corrosion level 2 · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION TO LOWER MID BOLT SLAT TRACK 8 BETWEEN STA 8744 AND STA 9235 AT RIGHT RIB 16 TO RIGHT RIB 17. REPLACED LOWER MID BOLT SLAT TRACK 8 BETWEEN STA 8744 AND STA 9235 AT RIGHT RIB 16 TO RIGHT RIB 17 PER AMM 27-84-65.

Part: BOLT — CORRODED (SLAT TRACK) · corrosion level 2 · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION TO LOWER BOLT SLAT TRACK 7 BETWEEN STA 7316 AND STA 7792 AT RIGHT RIB 13 TO RIGHT RIB 14. REPLACED LOWER BOLT SLAT TRACK 7 BETWEEN STA 7316 AND STA 7792 AT RIGHT RIB 13 TO RIGHT RIB 14 PER AMM 27-84-65.

Part: BOLT — CORRODED (SLAT TRACK) · corrosion level 2 · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION TO FORWARD BOLT SLAT TRACK 9 BETWEEN STA 9704 AND STA 10204 BETWEEN RIGHT RIB 18 AND RIGHT RIB 19. REPLACED FORWARD BOLT SLAT TRACK 9 BETWEEN STA 9704 AND STA 10204 BETWEEN RIGHT RIB 18 AND RIGHT RIB 19 PER AMM 27-84-66.

Part: ATTACH FITTING — CORRODED (GIRT BAR) · airframe 48,505 hrs · 28,926 cycles

CORROSION WAS FOUND AT THE FORWARD AND AFT GIRT BAR FITTING ATTACHMENT ON THE L1 DOOR SILL. REPLACED LOWER SILL AND FASTENERS LOCATED BETWEEN FRAMES 16 TO 20 IAW SRM 51-72-11, AND DRAWING D53110339.

Part: BELLCRANK — OUT OF ADJUST (PAX DOOR) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE: OUT OF ADJUSTMENT PASSENGER CREW DOOR 831 RIGGING POINT TORSION BAR BELLCRANK AT FOWARD GALLEY AREA. MAINTENANCE ADJUSTED MISSING POINT TORSION BAR BELLCRANK PER AMM 52-11-21-400-001-A.

Part: CYLINDER — INOPERATIVE (PAX DOOR)

AIRCRAFT WAS IN BASE MAINTENANCE. PASSENGER CREW DOOR 832 (L2) DAMPIING FUNCTION DID NOT OPERATE CORRECTLY, BUFFER HIT FUSELAGE. REMOVED AND REPLACED DOOR DAMPER CYLINDER PER AMM 52-13-14-400-001-B. OPERATIONAL CHECK GOOD.

Part: WINDOW FRAME — CRACKED (FRAMES 4-8) · airframe 48,505 hrs · 28,926 cycles

CRACK INDICATION ON WINDOW LATERAL FRAME LEFT SIDE UPPER CUT OUT BETWEEN FRAMES 4 - 8, Y1292. REPLACED THE WINDOW FRAME IAW EA 275851.

Part: WINDOW FRAME — CRACKED (FRAMES 4-8) · airframe 48,505 hrs · 28,926 cycles

CRACKED LATERAL RIGHT WINDOW FRAME BETWEEN FRAMES 4 TO 8 AT -Y1292. MODIFIED THE RIGHT WINDOW FRAME IAW EA 275851.

Part: RECEPTACLE — BROKEN (ZONE 600) · airframe 48,506 hrs · 28,926 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. BROKEN OFFWING ESCAPE SLIDE RECEPTACLES, AREA STOWAGE RIGHT WING AND LEFT WING. REPLACED FOUR RIGHT WING RECEPTACLES AND FOUR LEFT WING RECEPTACLES (AALA201711289020) PER SRM A319 51-42-11 AND DRAWING D53371604.

Part: RECEPTACLE — BROKEN (ZONE 500) · airframe 48,506 hrs · 28,926 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. BROKEN OFFWING ESCAPE SLIDE RECEPTACLES, AREA STOWAGE RIGHT WING AND LEFT WING. REPLACED FOUR RIGHT WING RECEPTACLES (AALA201711279046) AND FOUR LEFT WING RECEPTACLES PER SRM 51-42-11 AND DRAWING D53371604.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 48,505 hrs · 28,926 cycles

LEFT CENTER WINDOW POST FOUND TO BE CRACKED. REPLACED CONTINUITY FITTINGS IAW EA 275578.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 48,505 hrs · 28,926 cycles

LEFT CENTER WINDOW POST FOUND TO BE CRACKED. REPLACE CONTINUITY FITTINGS IAW EA 275578.

Part: DOOR SILL — CORRODED (FRAMES 16-20) · airframe 48,505 hrs · 28,926 cycles

DURING THE PREVIOUS 2S CHECK, CORROSION WAS FOUND ON L1 DOOR SILL AT FRAMES 16 - 20. REPAIRED IAW EA 201884. THE L1 DOOR SILL WAS REPLACED DURING THE CURERNT 3S CHECK IAW SRM 51-72-11 AND DRAWING D53110339.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LOWER SILL AT LEVEL STR 23L AND BETWEEN FR 66 & FR 68 AT AFT GALLEY AREA. REPLACED LOWER SILL PER SRM 51-72-11.

Part: SKIN — DAMAGED (RUDDER) · airframe 48,505 hrs · 28,926 cycles

TRAPPED WATER INDICATION ON THE RUDDER RIGHT SIDE PANEL, AROUND UPPER HOIST POINT AT TRAILING EDGE FASTENER NR 20, BETWEEN RIBS 6 AND 7. REPAIREDTHE RUDDER PANEL IAW EA 275614.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL 212EF BETWEEN FR 6 TO FR 9 AT RIGHT BUTTLINE -Y765 TO RIGHT BUTTLINE -Y254. REPLACED FLOOR PANEL 212EF BETWEEN FR 6 TO FR 9 AT RIGHT BUTTLINE -Y765 TO RIGHT BUTTLINE -Y254 PER A319 SRM 53-12-00-300-006 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION FLOOR PANEL 214EF BETWEEN FR 36 TO FR 42 AT RIGHT BUTTLINE -Y254 TO LEFT BUTTLINE Y254. REPLACED FLOOR PANEL 214EF BETWEEN FR 36 TO FR 42 AT RIGHT BUTTLINE -Y254 TO LEFT BUTTLINE Y254 PER A319 SRM 53-02-00-300-011 FIGURE 20109 AND IRM 9701 REVISION G.

Part: COUPLING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION FOUND ON FLOORBEAM COUPLING Y765 AT LEVEL FR 66 AT AFT GALLEY AREA. REPLACED COUPLING PER SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL 241HF BETWEEN FR 36 TO FR 42 AT RIGHT BUTTLINE Y-1292 TO LEFT BUTTLINE Y1332. REPLACED FLOOR PANEL 241HF BETWEEN FR 36 TO FR 42 AT RIGHT BUTTLINE Y-1292 TO LEFT BUTTLINE Y1332 PER A319 SRM 53-02-00-300-011 AND IRM 9701 REVISION G.

Part: SKIN — CONTAMINATED (LT ELEVATOR) · airframe 48,505 hrs · 28,926 cycles

TRAPPED WATER INDICATION IN THE LEFT ELEVATOR AT 16.45 INCHES FROM TRAILING EDGE AND 3.76 INCHES FROM ELEVATOR RIB 3. REPAIRED THE ELEVATOR SKIN PANEL IAW SRM 55-21-11-300-005.

Part: SKIN PANEL — SATURATED (LT HORIZ STAB) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS INBOARD FROM RIB 10, FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER. REPAIRED UPPER SKIN PANEL HONEYCOMB CORE PER SRM 55-21-11-300-005.

Part: SKIN PANEL — SATURATED (LT HORIZ STAB) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE. TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 6.2 IN. OUTBOARD FROM RIB 5 AND 3.3 IN. FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER. REPAIRED UPPER SKIN PANEL HONEYCOMB CORE PER SRM 55-21-11-300-004.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,505 hrs · 28,926 cycles

DELAMINATED FLOOR PANEL 242KF BETWEEN FRAMES 42 TO 47, -Y765 TO -Y254. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, FIGURE 20109, AND IRM 9701 REVISION G.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY FLOORBEAM AT -Y1162.5 AND FR 68. REPLACED FLOORBEAM PER SRM 51-72-11 AND DRAWING 53472780.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY LOWER SILL AT STRINGER 23R, BETWEEN FR 66 AND FR 68. REPAIRED LOWER SILL PER SRM 53-42-14-300-001.

Part: SKIN PANEL — SATURATED (LT HORIZ STAB) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 1.5 IN. INBOARD FROM RIB 4 AND 12.5 IN. FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER. REPAIRED UPPER SKIN PANEL HONEYCOMB CORE PER SRM 55-21-11-300-005.

Part: FRAME — CRACKED (FRM 68) · airframe 48,505 hrs · 28,926 cycles

CRACK INDICATION ON FRAME 68, STRINGER 8. REPAIRED THE FRAME IAW EA 275412.

Part: SKIN — CONTAMINATED (LT ELEVATOR) · airframe 48,505 hrs · 28,926 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB, CORE CELLS. LOCATED AT 20.5 IN. OUTBOARD FROM RIB 1 AND 7.5 IN. FROM TRAILING EDGE. REPAIRED UPPER SKIN PANEL HONEYCOMB CORE IAW SRM 55-21-11-300-005.

Part: FLOORBEAM — CORRODED (FRAME 66) · corrosion level 2 · airframe 48,505 hrs · 28,926 cycles

ARICRAFT IN BASE MAINTENANCE. CORRSION FOUND ON FLOOR BEAM AT FR66, AT Y765, IN THE AFT GALLEY AREA. REPLACE FLOOR BEAM PER SRM A319 51-72-11 AND DWG D53472190

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. EXCESSIVE PLAY ON RUDDER NR 6 HINGE ARM BEARING ON VERTICAL STABILIZER. REPLACED HINGE ARM FITTING PER SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL 241LF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION FOUND ON WEB FRAME 20 AT LEVEL OF STRINGER 23R AT FWD GALLEY AREA. REPLACED WEB AND FASTENER SRM 51-72-11.

Part: SKIN PANEL — SATURATED (LT HORIZ STAB) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE. TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS LOCATED AT 47.5 IN. OUTBOARD FROM RIB 5 AND 3.5 IN. FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER. REPAIRED UPPER SKIN PANEL HONEYCOMB CORE PER SRM 55-21-11-300-005.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION FLOOR PANEL 232FF BETWEEN FR 20 TO FR 24 AT RIGHT BUTTLINE Y-1732 TO RIGHT BUTTLINE Y-1292. REPLACED FLOOR PANEL 232FF BETWEEN FR 20 TO FR 24 AT RIGHT BUTTLINE Y-1732 TO RIGHT BUTTLINE Y-1292 PER SRM 53-12-00-300-006 FIGURE 20106 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,505 hrs · 28,926 cycles

DELAMINATED FLOOR PANEL 221PF BETWEEN FRAMES 12 TO 16, Y254 TO 1732. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, FIGURE 20106, AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL 222EF BETWEEN FR 16 TO FR 20 AT RIGHT BUTTLINE -Y1292 TO RIGHT BUTTLINE -Y254. REPLACED FLOOR PANEL 222EF BETWEEN FR 16 TO FR 20 AT RIGHT BUTTLINE -Y1292 TO RIGHT BUTTLINE -Y254 PER A319 SRM 53-12-00-300-006 FIGURE 20106 AND IRM 9701 REVISION G.

Part: FITTING — CRACKED (DOOR FRAME) · airframe 48,505 hrs · 28,926 cycles

A CRACK INDICATION ON FRAME 16 LEFT AT DOOR STOP FITTING 7 FROM UPPER INBOARD AND LOWER INBOARD HOLES AT FORWARD GALLEY AREA. REPLACED THE FITTING IAW SRM 51-72-11.

Part: FITTING — CRACKED (DOOR FRAME) · airframe 48,505 hrs · 28,926 cycles

A CRACK INDICATION ON FRAME 16 RIGHT SIDE AT DOOR STOP FITTING 7 FROM UPPER INBOARD AND LOWER INBOARD HOLES AT FORWARD GALLEY AREA. REPLACED THE FITTING IAW SRM 51-72-11, AND DRAWING D53110339.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL 231CF AT FWD GALLEY AREA. REPLACED FLOOR PANEL PER SRM 53-12-00-300-006.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION FLOOR PANEL 221DF BETWEEN FR 16 TO FR 21 AT RIGHT BUTTLINE -Y254 TO LEFT BUTTLINE Y254. REPLACED FLOOR PANEL 221DF BETWEEN FR 16 TO FR 21 AT RIGHT BUTTLINE -Y254 TO LEFT BUTTLINE Y254 PER A319 SRM 53-12-00-300-006 FIGURE 20106 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION FLOOR PANEL 221EF BETWEEN FR 16 TO FR 20 AT LEFT BUTTLINE Y254 TO LEFT BUTTLINE +Y1292. REPLACED FLOOR PANEL 221EF BETWEEN FR 16 TO FR 20 AT LEFT BUTTLINE Y254 TO LEFT BUTTLINE +Y1292 PER A319 SRM 53-12-00-300-006 FIGURE 20106 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 48,505 hrs · 28,926 cycles

DELAMINATION ON FLOOR PANEL 261AG BETWEEN FRAMES 64 TO 66, Y-765 TO Y765. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, FIGURE 20109 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION FLOOR PANEL 262EF BETWEEN FR 20 TO FR 24 AT RIGHT BUTTLINE -1292 TO RIGHT BUTTLINE -Y765. REPLACED FLOOR PANEL 262EF BETWEEN FR 20 TO FR 24 AT RIGHT BUTTLINE -1292 TO RIGHT BUTTLINE -Y765 PER A319 SRM 53-12-00-300-006 FIGURE 20106 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL 261PF BETWEEN FR 68 TO FR 70 AT RIGHT BUTTLINE -Y1292 TO LEFT BUTTLINE Y1292. REPLACED FLOOR PANEL 261PF BETWEEN FR 68 TO FR 70 AT RIGHT BUTTLINE -Y1292 TO LEFT BUTTLINE Y1292 PER A319 SRM 53-12-00-300-006 FIGURE 20106 AND IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 48,505 hrs · 28,926 cycles

DELAMINATED FLOOR PANEL 231BF BETWEEN FRAMES 23 TO 24, Y-254 TO 254. REPLACED THE FLOOR PANEL 231BF IAW SRM 53-12-00-300-006, FIGURE 20106, AND IRM 9701 REVISION G.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 48,505 hrs · 28,926 cycles

CRACK INDICATION ON WINDSHIELD FRAME CENTER POST, LOWER ATTACH AREA RIGHT SIDE IN COCKPIT BETWEEN FRAMES 2 & 6, Y1292 TO -Y1292. REPLACED THE WINDOW FRAME CENTER POST IAW EA 275578.

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 48,505 hrs · 28,926 cycles

DELAMINATED FLOOR PANEL 261BG AT AFT GALLEY AREA. REPLACED FLOOR PANEL IAW SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL 151CE IN AFT CARGO COMPARTMENT. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 48,505 hrs · 28,926 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL 151ZG IN AFT CARGO COMPARTMENT. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: POWER UNIT — LEAKING · airframe 48,409 hrs · 28,843 cycles

FLIGHT ATTENDANT NOTED ODOR IN CABIN DURING FLIGHT AND GROUND OPERATIONS. FOUND A LEAKING POWER TRANSFER UNIT. REMOVED AND REPLACED GREEN/YELLOW POWER TRANSFER UNIT IAW AMM.

Part: OVEN — ODOR (GALLEY) · airframe 48,055 hrs · 28,585 cycles

FOWARD GALLEY OVEN EMITTED PLASTIC ODOR. TURN OFF OVEN AND ODOR WENT AWAY. REPLACED FOWARD GALLEY OVEN.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 47,718 hrs · 28,392 cycles

EMERGENCY LENS MISSING . INSTALLED A NEW LENS IAW AMM

Part: PRINTER — ODOR (COCKPIT) · airframe 47,224 hrs · 28,109 cycles

PRINTER HAS AN ELECTRIC BURNING ODOR. PRINTER LATCH APPEARS TO BE DAMAGED AND MAY BE CAUSING PROBLEM. REPLACED THE PRINTER IAW MM 31-35-22. OPS NORMAL.

Part: WARNING LIGHT — FALSE ACTIVATION (FUEL AUTOFEED) · airframe 46,938 hrs · 27,933 cycles

FUEL AUTOFEED FAULT IN CLIMB AND CRUISE WHILE IN AUTO MODE. ACCOMPLISHED ECAM NOW NORMAL ACTIONS AND REQUIRED FOLLOW UP. NO SIGNIFICANT OF FUEL IMBALANCE. MAINTENANCE COULD NOT DUPLICATE, NO FAULTS FOUND, ACCOMPLISHED TS IAW TSM 28-21-00-810-816-A AND TSM 28-21-00-810-823-A, ACCOMPLISHED SUCCESSFUL OPS TEST OF THE MAIN FUEL PUMP SYS WITH FUEL FLOW BY TRANSFER IAW AMM 28-21-00-710-007-A, ACCOMPLISHED SUCCESSFUL FUNCTIONAL TEST OF THE CENTER TANK FUEL CONTROL IAW AMM 28-21-00-720-001, ACCOMPLISHED SUCCESSFUL BITE TEST OF FQIC IAW AMM 28-42-00-740-001-A, NO FAULTS FOUND.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 46,918 hrs · 27,925 cycles

L2 DOOR EMERGENCY LIGHT LENS MISSING. REPLACED THE LENS.

Part: PUMP — INOPERATIVE (FUEL SYSTEM) · airframe 46,450 hrs · 27,598 cycles

AIRCRAFT WAS NOT GROUNDED. CENTER TANK FUEL PUMP NR 2 INOPERABLE. MAINTENANCE REPLACED CENTER TANK FUEL PUMP NR 2 PER AMM 28-21-51-400-002-A.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 45,533 hrs · 26,971 cycles

FORWARD LEFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT AND FLASHLIGHT BATTERY.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 45,533 hrs · 26,971 cycles

FORWARD LEFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT AND FLASHLIGHT BATTERY.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 45,503 hrs · 26,945 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY FLASHLIGHT INOPERATIVE AT 2L DOOR. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT 2L DOOR. OPS CHECKS GOOD.

Part: SKIN — CORRODED (FRAME 42) · airframe 45,461 hrs · 26,915 cycles

CORROSION ON THE AFT TOP SKIN PANEL OF THE CENTER WING FORWARD OF FRAME 42 AT CRUCIFORM. REPAIRED THE SKIN IAW EA 263252.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 45,461 hrs · 26,915 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT SIDE BOX BEAM UPPER FLANGE AFT 2 FASTENER HOLES CRACKED AT FRAME 43 AND Y1622. REPAIRED BOX BEAM IAW EO 5315Y066.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 45,461 hrs · 26,915 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT SIDE BOX BEAM UPPER FLANGE AFT 2 FASTENER HOLES CRACKED AT FRAME 43 AND -Y1622. REPAIRED BOX BEAM IAW EO 5315Y066.

Part: CONTROL UNIT — MALFUNCTIONED (EFCS) · airframe 45,408 hrs · 26,894 cycles

FLIGHT CREW REPORTED RECIEVING A BLUE SYSTEM LOW PRESSURE FAULT WARNING AND A FLIGHT CONTROL ELAC 1 PITCH FAULT AT CRUISE. THE FLIGHT CREW DECLARED AN EMERGENCY, DIVERTED, AND LANDED SAFELY. AIRCRAFT GROUNDED. MAINTENANCE REPLACED THE BLUE SYSTEM ELECTRIC PUMP AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 29-12-51, 29-00-00-870-008A, & 29-00-00-870-009A. MAINTENANCE ALSO ACCOMPLISHED A BITE TEST OF THE EFCS (GROUND SCANNING) WITH NO FAULTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 45,408 hrs · 26,894 cycles

FLIGHT CREW REPORTED RECIEVING A BLUE SYSTEM LOW PRESSURE FAULT WARNING AND A FLIGHT CONTROL ELAC 1 PITCH FAULT AT CRUISE. THE FLIGHT CREW DECLARED AN EMERGENCY, DIVERTED, AND LANDED SAFELY. AIRCRAFT GROUNDED. MAINTENANCE REPLACED THE BLUE SYSTEM ELECTRIC PUMP AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 29-12-51, 29-00-00-870-008A, & 29-00-00-870-009A. MAINTENANCE ALSO ACCOMPLISHED A BITE TEST OF THE EFCS (GROUND SCANNING) WITH NO FAULTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: APU — SMOKE · airframe 45,167 hrs · 26,749 cycles

REPORT OF SMOKE ON APU SHUTDOWN. AIRCRAFT GROUNDED. MAINTENANCE REPLACED THE APU PER TASK CARD 26L31049003.

Part: O-RING — MISSING (APU) · airframe 45,125 hrs · 26,722 cycles

SMOKE COMING FROM APU TAILPIPE ON SHUTDOWN. MAINTENANCE FOUND APU OIL LEVEL LOW AND OIL IN TAIL PIPE. MAINTENANCE FOUND THE OIL LEAK FROM STARTER PAD DUE TO A MISSING O-RING ON THE STARTER WHICH RESULTED IN THE REPLACEMENT OF THE STARTER IAW AMM 49-42-51. A SATISFACTORY OPS CHECK WAS ACCOMPLISHED. IAW AALA 201607119004 WHICH REPLACED THE APU.

Part: UNKNOWN — ODOR (CABIN) · airframe 44,334 hrs · 26,246 cycles

AIRCRAFT WAS GNDED. FLIGHT ATTENDANTS REPORTED A MUSTY & MOLDY BUT SWEET ANTI-FREEZE TYPE CABIN ODOR, THAT CAUSED THEM TO BE ILL & RECEIVED MEDICAL ATTENTION. ACCOMPLISHED JC 26L000021001 & JC 26L00021002. TROUBLESHOOT CABIN AIR QUALITY & APU SMELL IN CABIN. APU HOURS 16283 & OIL LEVEL OK. APU OIL FOUND AT FULL MARK, NO LEAKS NOTED & MUSTY SMELL NO LONGER.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 44,123 hrs · 26,118 cycles

AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,988 hrs · 26,025 cycles

AIRCRAFT WAS GNDED. EMER EXIT LIGHTS WON'T TEST PROPERLY. REPLACED BATTERY PACK ON LT OVERWING EXIT EPSU 11WL. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,540 hrs · 25,066 cycles

AFT CARGO FLOOR PANEL 151VG DELAMINATED. REPLACED FLOOR PANEL IAW AMM 53-42-14-000-001A.

Part: NUT — MISSING (THRUST REVERSER) · airframe 41,651 hrs · 24,550 cycles

ECAM MSG FOR NR 2 ENG REVERSER UNLOCKED, OCCURRED THREE TIMES DURING CLIMB OUT. CREW RETURNED TO FIELD. FOUND NUTS MISSING FROM LOWER RT STOW LATCH. REINSTALLED & TORQUED IAW AMM 78-31-19-400-001-A. PERFORMED OPERATIONAL CHECK IAW AMM 78-31-00-710-042-A WITH NO FAULTS NOTED.

Part: GIRT BAR — DIRTY (ZONE 800) · airframe 41,651 hrs · 24,550 cycles

L1 DOOR ARMING LEVER STIFF WHEN ARMING DOOR. CLEANED FWD & AFT GIRT BAR FITTINGS IAW AMM 52-11-31, GIRT BAR FITTINGS OK, DOOR L1 ARMED AS REQUIRED.

Part: HOOK AND LOOP — WORN (L1 DOOR)

VELCRO TOO SHORT & WORN TO HOLD SLIDE LANYARDS IN PLACE ON DOOR L1. REPLACED EMER EXIT RAFT SLIDE ASST DOOR L1 IAW AMM 52-73-00-710-004-A.

Part: COVER — UNSERVICEABLE (CABIN) · airframe 40,594 hrs · 23,905 cycles

SEAT 8D EMER LIGHT COVER NEEDS REPLACED. REPLACED EMER EXIT LIGHT COVER AT SEAT 8D. OK FOR SERVICE.

Part: BATTERY — DISCHARGED (MEGAPHONE) · airframe 40,451 hrs · 23,802 cycles

THE AFT MEGA PHONE IS OUT OF DATE & BATTERIES LOW. REPLACED MEGA PHONE BATTERIES & INSPECTION PLACARD FROM AFT MEGA PHONE IAW MPPM 52-01-05. OPERATIONS CHECKED GOOD.

Part: COVER — DEFECTIVE (L1 DOOR) · airframe 39,788 hrs · 23,424 cycles

THE L1 DOOR DECORATIVE SLIDE COVER MAKING CONTACT WITH ACFT SKIN. ONLY LIGHT ABRASION TO THE FUSELAGE SKIN PAINT AT DECORATIVE COVER CONTACT POINT.

Part: LENS — MISSING (CABIN) · airframe 39,622 hrs · 23,329 cycles

SEAT MOUNTED EMERGENCY LIGHT LENS MISSING ON SEATS 1C & 22C. REPLACED THE LENS IAW AMM 33-51-19 PB 401.

Part: LENS — MISSING (CABIN) · airframe 38,897 hrs · 22,863 cycles

CREW REPORTED THE EXIT LIGHT COVER MISSING ON AISLE SEAT 10D. MX REPLACED LENS, OK FOR SERVICE.

Part: FILTER — DIRTY (SMOKE DETECTOR) · airframe 38,418 hrs · 22,522 cycles

CREW RECEIVED A SMOKE LAVATORY DETECTION FAULT. REPLACED FILTERS IN ALL THREE LAVATORY SMOKE DETECTORS. PERFORMED TASK 26-17-00-710-001-A, ALL SYS RESET, OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 37,387 hrs · 21,801 cycles

THE "A" F/A REPORTED A CHEMICAL SMELL IN FIRST CLASS CABIN AND FWD COACH CABIN (ROW 5) WHILE AT 35,000' AND 1 HOUR OF CRUISE FLIGHT. NO ODOR NOTED IN COCKPIT. MX ACCOMPLISHED JC 26L00021001, "TROUBLESHOOT CABIN AIR QUALITY". APU OIL IS SERVICED CORRECTLY. RAN NR 1 AND NR 2 ENGINES, PLUS ACFT PACKS, IN ALL CONFIGURATIONS. NO CABIN ODORS NOTED AT ANY TIME. ACFT OK FOR SERVICE.

Part: LENS — MISSING (CABIN) · airframe 37,343 hrs · 21,774 cycles

MX REPORTED THE EMERGENCY LIGHT LENS MISSING AT SEAT 3AC. MX REPLACED EMERGENCY LIGHT LENS AT SEAT 3AC. ACFT OK FOR SERVICE.

Part: SLIDE — UNSERVICEABLE (OVERWING EXIT) · airframe 37,144 hrs · 21,641 cycles

MX REPORTED THE RT OVERWING SLIDE ENCLOSURE AFT EDGE DELAMINATED. MX R & R THE RT OVERWING SLIDE ASSY IAW AMM 25-62-42.

Part: FASTENER — LOOSE (EVAC SLIDE) · airframe 35,952 hrs · 20,863 cycles

MAINTENANCE REPORTED THE RIGHT OVERWING SLIDE HAS ONE FASTENER LOOSE. MAINTENANCE TIGHTENED FASTENER ON RIGHT OVERWING SLIDE AS REQUIRED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 34,030 hrs · 19,659 cycles

LENS MISSING FROM OVERHEAD EMERGENCY LIGHT AT ROW 14. REPLACED LENS ON OVERHEAD EMERGENCY LIGHT ROW 14.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 33,843 hrs · 19,537 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION IN 17 COUNTERSINK HOLES ON LOWER LEFT WING FUEL ACCESS PANEL 540MB BETWEEN S8L TO S11L & BETWEEN RIB 17 TO RIB 18. REPLACED LOWER LEFT WING FUEL ACCESS PANEL 540MB IAW A319 SRM 51-72-11 & SRM 57-27-11 PARAGRAPH 4, PAGE 103.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 33,843 hrs · 19,537 cycles

S2 CHECK - LEVEL 2 INTERGRANULAR CORROSION IN 16 COUNTERSINK HOLES ON LOWER LEFT WING FUEL ACCESS PANEL 540NB BETWEEN S8L TO S11L & BETWEEN RIB 18 TO RIB 19. REPLACED LOWER LEFT WING FUEL ACCESS PANEL 540NB IAW A319 SRM 51-72-11 & SRM 57-27-11 PARAGRAPH 4, PAGE 103.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 33,843 hrs · 19,537 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION IN 12 COUNTERSINK HOLES ON LOWER LEFT WING FUEL ACCESS PANEL 540PB BETWEEN S8L TO S11L & BETWEEN RIB 19 TO RIB 20. REPLACED LOWER LEFT WING FUEL ACCESS PANEL 540PB IAW A319 SRM 51-72-11 & 57-27-11 PARAGRAPH 4, PAGE 103.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,843 hrs · 19,537 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SILL BEAM BETWEEN FR66 TO FR68, -Y1589. REPLACED SILL BEAM BETWEEN FR66 TO FR68, -Y1589 IAW A319 SRM 51-72-11 & AIRBUS DRAWING # 18D53480505.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 32,609 hrs · 18,663 cycles

FORWARD EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FORWARD EMERGENCY FLASHLIGHT. OPERATIONAL CHECK GOOD.

Part: SLIDE — BROKEN (PAX DOOR) · airframe 32,590 hrs · 18,653 cycles

C11 CHECK - RIGHT AFT PAS/CREW DOOR RETAINING PINS/SHAFT ASSEMBLY SAFETY WIRE BROKEN ON PAWL. REPLACED R2 SLIDE ASSEMBLY WITH SERVICEABLE SLIDE IAW JOB CARD 26C84252002.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - DELAMINATION ON UPPER SURFACE OF FLOOR PANEL 261QF AT FR64, Y=0. REPLACED FLOOR PANEL 261QF AT FR64, Y=0 IAW MCGILL IRM 9701 REV G.

Part: AILERON — DELAMINATED (LEFT) · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - DELAMINATION ON LEFT AILERON TRAILING EDGE AT WS1406 & WING RIB 26. REPAIRED LEFT AILERON TRAILING EDGE AT WS 1406 & WING RIB 26 IAW A319 SRM 57-61-21.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - DELAMINATION ON UPPER SURFACE OF FLOOR PANEL AT FR24, Y=0. REPLACED FLOOR PANEL AT FR24, Y=0 IAW MCGILL I IRM 9701 REV G.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR16, -Y81. REPLACED FLOORBEAM AT FR16, -Y81 IAW A319 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR23, Y503.2. REPLACED FLOORBEAM AT FR23, Y503.2 IAW A319 SRM 53-11-14.

Part: SKIN — SATURATED (ELEVATOR) · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - WATER SATURATION IN HONEYCOMB ON LEFT ELEVATOR UPPER SURFACE APPROX 9 FEET 7 INCHES FROM INBOARD END NEAR TRAILING EDGE. REPAIRED LEFT ELEVATOR UPPER SURFACE IAW A319 SRM 55-21-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR20 TO FR21, -Y1292. REPLACED FLOORBEAM BETWEEN FR20 TO FR21, -Y1292 IAW A319 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR65, Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR65, Y765 IAW A319 SRM 51-72-11.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON ANGLE BETWEEN FR66 TO FR68, S23L. REPLACED ANGLE BETWEEN FR66 TO FR68, S23L IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR66, -Y464.8. REPLACED FLOORBEAM AT FR66, -Y464.8 IAW A319 SRM 51-42-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR66, -Y765. REPLACED FLOORBEAM AT FR66, -Y765 IAW A319 SRM 53-41-14.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR TIE SUPPORT BETWEEN FR69 TO FR70, -Y1160. REPLACED SHEAR TIE SUPPORT BETWEEN FR69 TO FR70, -Y1160 IAW A319 SRM 51-42-11 & SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR64 + 9 INCHES, -Y765. REPLACED FLOORBEAM AT FR64 + 9 INCHES, -Y765 IAW A319 SRM 53-42-11.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - CRACK IN SHEAR PLATE AT FR68 + 8 INCHES, -Y1162. REPLACED SHEAR PLATE AT FR68 + 8 INCHES, -Y1162 IAW A319 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68 & BETWEEN -Y1162 TO -Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68 & BETWEEN -Y1162 TO -Y1292 IAW A319 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, -Y1162.5. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, -Y1162.5 IAW A319 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR68 TO FR70 OUTBOARD OF Y1162. REPLACED SHEAR PLATE BETWEEN FR68 TO FR70 OUTBOARD OF Y1162 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, -Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, -Y1292 IAW A319 SRM 51-42-11.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - CRACK ON SHEAR WEB PLATE AT FR68+8 INCHES, Y1162.5. REPLACED SHEAR WEB PLATE AT FR68+8 INCHES, Y1162.5 IAW A319 SRM 51-72-11 & AIRBUS DRAWING 18D53480019.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, Y1162.5. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, Y1162.5 IAW A319 SRM 51-72-11, AIRBUS DRAWING D53472780.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR67 TO FR68, -Y765. REPLACED FLOORBEAM BETWEEN FR67 TO FR68, -Y765 IAW A319 SRM 53-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR66, Y1292. REPLACED FLOORBEAM AT FR66, Y1292 IAW A319 SRM 51-72-11 & EA 200483.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR70, Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR70, Y765 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68 & BETWEEN Y1162.5 TO Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68 & BETWEEN Y1162.5 TO Y1292 IAW A319 SRM 51-72-11, AIRBUS DRAWING D53472780.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FORWARD END OF L2 DOOR SILL PLATE AT FR66, Y1589. REPLACED L2 DOOR SILL PLATE AT FR66, Y1589 IAW A319 SRM 53-41-14.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR68 TO FR70, -Y1162.5. REPLACED SHEAR PLATE BETWEEN FR68 TO FR70, -Y1162.5 IAW A319 SRM 51-72-11 & TYPICAL REPAIR 320-2528-10-0011.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR16, -Y1292. REPLACED FLOORBEAM AT FR16, -Y1292 IAW A319 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR20, -Y254. REPLACED FLOORBEAM AT FR20, -Y254 IAW A319 SRM 51-42-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR16, Y503.2. REPLACED FLOORBEAM AT FR16, Y503.2 IAW A319 SRM 53-11-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,294 hrs · 18,447 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR16 TO FR23, Y254. REPLACED FLOORBEAM BETWEEN FR16 TO FR23, Y254 IAW A319 SRM 51-42-00.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 31,143 hrs · 17,740 cycles

FLT 1967 - ABE-CLT - EMERGENCY LIGHTS - 2 BATTERIES REQUIRED FOR FORWARD HANDHELD FLASHLIGHT. REMOVED AND REPLACED BATTERIES ON FORWARD HANDHELD FLASHLIGHT.

Part: CONNECTOR — LOOSE (CABIN) · airframe 28,537 hrs · 16,132 cycles

FLT 1620 - MBJ-PHX - EMERGENCY LIGHTS - EMERGENCY LIGHT 12L INOPERATIVE. FOUND LOOSE CONNECTOR AT 12L SEAT, RECONNECTED. OPERATIONAL CHECK WAS GOOD.

Part: CONNECTOR — FAULTY (CABIN) · airframe 28,431 hrs · 16,084 cycles

FLT 2048 - DCA - BOS - EMERGENCY LIGHTS - RIGHT EMERGENCY EXIT LIGHT FORWARD OF OVERWING EXIT INOPERATIVE. REMOVED AND REPLACED ELECTRICAL CONNECTOR PER ESM 20-44-19. OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 27,272 hrs · 15,409 cycles

FLT 1907 - BUF-PHL - EMERGENCY LIGHTS - FLASHLIGHT AFT RIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD.

Part: LENS — MISSING (CABIN) · airframe 27,118 hrs · 15,331 cycles

FLT 1907 - PHL - DFW - EMERGENCY LIGHTS - EMERGENCY LIGHT LENS MISSING AT SEAT 4C. INSTALLED MISSING LIGHT LENS. OPERATIONAL CHECK WAS GOOD.

Part: ODOR — DETECTED (CABIN)

CLT FLT 1109 EN-ROUTE LGA TO CLT - A HOT ODOR WAS NOTED IN CABIN IN BOTH TAKEOFF AND DESCENT. THE ODOR WAS NOTED TO BE PARTICULARLY PRESENT DESCENT AT IDLE. FLIGHT COMPLETED WITHOUT FURTHER INCIDENT. MAINTENANCE RAN BOTH ENGINES AND BLEED SYSTEMS. NO ODORS NOTED.

Part: FLOORBEAM — CORRODED (BS 66) · corrosion level 1 · airframe 16,336 hrs · 16,336 cycles

FOUND CORROSION RT BEAM Y-1292 STA 66 AT ATTACH HOLE AFT END. REPLACED WITH IDENTICAL PART PER SRM 51-42-00, DEFECT SIZE: 1" X 2".

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 1 · airframe 16,336 hrs · 16,336 cycles

FOUND CORROSION FLOOR SUPPORT Y-1162, DEFECTIVE PART REPLACED WITH IDENT PART NUMBER, DEFECT SIZE: 6 SQ IN IN SEVERAL SPOTS.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 16,336 hrs · 16,336 cycles

FOUND Y-765 FLOORBEAM CORROSION (RT) 7" AFT OF STA 66 AROUND ATTACH HOLES. REMOVED AND REPLACED BEAM WITH IDENTICAL PART NUMBER PER SRM 51-72-11, DEFECT SIZE: 1 X 1".

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 16,336 hrs · 16,336 cycles

FOUND CORROSION RT BEAM STA 66-68 INB OF RT DOOR SEAL AT ATTACH HOLES. REPLACED WITH IDENTICAL PART NUMBER PER SRM 51-42-0, DEFECT SIZE: 1" X 2".

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 16,336 hrs · 16,336 cycles

FOUND CORROSION FR 16 AND BETWEEN FR 19 AND 20 CENTER BEAM. INSTALLED DOUBLERS PER SRM 53-00-14 FIG 206, DEFECT SIZE: 2" X 2" AND 1" X 1".

Part: FLOORBEAM — CORRODED (BS 66-68) · corrosion level 1 · airframe 16,336 hrs · 16,336 cycles

FOUND CORROSION LT BS 66 TO 68 INB OF DOOR SILL -Y1162. REPLACED WITH IDENTICAL PART PER SRM 51-42-00, DEFECT SIZE: 1" X 2".

Part: FLOORBEAM — CORRODED (BS 68) · corrosion level 1 · airframe 16,336 hrs · 16,336 cycles

FOUND CORROSION LT BEAM Y1162 STA 68 AROUND NUT PLATES AT ATTACH HOLES. REPLACED WITH IDENTICAL PART PER SRM 51-42-00, DEFECT SIZE: 1" BY 2".

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 16,336 hrs · 16,336 cycles

FOUND CORROSION BETWEEN FR 13 AND 15. REPLACED BEAM PER SRM 51-72-11, DEFECT SIZE: 1" X 2".

Part: FLOORBEAM — CORRODED (STA 66) · corrosion level 1 · airframe 16,336 hrs · 16,336 cycles

FOUND CORROSION LT STA 66 AFT END OF FLOORBEAM AT ATTACH HOLES FOR FLOORBOARD. REPLACED WITH IDENTICAL PART PER SRM 51-42-00, DEFECT SIZE: 1" X 2".

Part: SHEAR TIE — CORRODED (FR 69-70) · corrosion level 1 · airframe 16,336 hrs · 16,336 cycles

RT SIDE SHEAR TIE CORRODED BETWEEN FRAMES 69 AND 70. DEFECTIVE PART REPLACED WITH IDENT PART NR, DEFECT SIZE: 2 SQ IN.

Part: EPSU — FAULTY (EMERGENCY LIGHT)

THE AFT LT EMERGENCY POWER SUPPLY UNIT FAULTED DURING TEST. MAINTENANCE REPLACED THE AFT LT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.

Part: RELEASE CABLE — INCORRECT (EVAC SLIDE)

CLT - THE AFT ENTRY DOOR EMERGENCY ESCAPE SLIDE WAS FOUND TO HAVE AN INCORRECT RELEASE CABLE INSTALLED DURING INSPECTION. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. OK FOR SERVICE. THE REPAIR SHOP INSTALLED THE PROPER RELEASE CABLE ON THE SLIDE AND RETURNED THE SLIDE TO SERVICE. (M)