N552UW

Part: HANDLE — LOOSE (ZONE 800) · airframe 43,919 hrs · 17,397 cycles

AIRCRAFT WAS NOT GROUNDED: 3L DOOR HANDLE IS LOOSE. MAINTENANCE RESECURED 3L SLIDE ARMING LEVER HANDLE PER AMM 25-23-47.

Part: LOCK — STUCK (ZONE 800) · airframe 43,551 hrs · 17,247 cycles

AIRCRAFT WAS NOT GROUNDED: MID LAVATORY DOOR LOCK JAMMED WITH PASSENGER INSIDE. THE LAVATORY DOOR HAD TO BE REMOVED FROM PART OF THE TRACK TO GET THE PASSENGER OUT. MAINTENANCE ADJUSTED AND LUBRICATED MID LAVATORY DOOR LOCK MECHANISM PER AMM 25-40-00, A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: VENT LINE — CLOGGED (ZONE 100) · airframe 42,890 hrs · 16,966 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTED STRONG DIRTY SOCK SMELL IN THE MID CABIN ON APPROACH THRU LANDING. MAINTENANCE FOUND THE APU WAS OVERSERVICED AND DRAINED THE EXCESS OIL PER AMM 49-91-42. (AALA202505164104) MAINTENANCE ALSO FOUND THE APU GEARBOX VENT LINE HAD EVIDENCE OF COKING AND WAS CLOGGED. MAINTENANCE REPLACED THE VENT LINE PER AMM 49-26-55. (AALA202505165926) MAINTENANCE ACCOMPLISHED THE DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM PER TASK CARD 26L00021014. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO LEAKS OR ODORS NOTED.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 42,890 hrs · 16,966 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTED STRONG DIRTY SOCK SMELL IN THE MID CABIN ON APPROACH THRU LANDING. MAINTENANCE FOUND THE APU WAS OVERSERVICED AND DRAINED THE EXCESS OIL PER AMM 49-91-42. (AALA202505164104) MAINTENANCE ALSO FOUND THE APU GEARBOX VENT LINE HAD EVIDENCE OF COKING AND WAS CLOGGED. MAINTENANCE REPLACED THE VENT LINE PER AMM 49-26-55. (AALA202505165926) MAINTENANCE ACCOMPLISHED THE DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM PER TASK CARD 26L00021014. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO LEAKS OR ODORS NOTED.

Part: BATTERY — NO TEST (ZONE 200) · airframe 42,772 hrs · 16,917 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 12WL FAULT MESSAGE DISPLAYED DURING SYSTEM TEST. REPLACED BATTERY FOR EMERGENCY POWER SUPPLY UNIT 12WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.

Part: BATTERY — NO TEST (ZONE 200) · airframe 42,772 hrs · 16,917 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 10WL FAULT MESSAGE DISPLAYED DURING SYSTEM TEST. REPLACED BATTERY FOR EMERGENCY POWER SUPPLY UNIT 10WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.

Part: BATTERY — NO TEST (ZONE 200) · airframe 42,772 hrs · 16,917 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 11WL FAULT MESSAGE DISPLAYED DURING SYSTEM TEST. REPLACED BATTERY FOR EMERGENCY POWER SUPPLY UNIT 11WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.

Part: SLIDE — LOW PRESSURE (ZONE 800) · airframe 42,587 hrs · 16,833 cycles

AIRCRAFT WAS GROUNDED: DURING A SCHEDULED REPLACEMENT OF THE R4 DOOR SLIDE, THE REPLACEMENT SLIDE INDICATED LOW PRESSURE ON THE FLIGHT ATTENDANTS PANEL. MAINTENANCE DETERMINED THE REPLACEMENT SLIDE WAS BAD FROM STOCK AND REPLACED IT WITH A SERVICEABLE UNIT. THE BAD FROM STOCK SLIDE WAS ROUTED TO BE SENT OUT FOR REPAIR.

Part: HANDLE — LOOSE (ZONE 800) · airframe 41,399 hrs · 16,312 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 3L SLIDE ARMING LEVER IS LOOSE. RESECURED YELLOW HANDLE ON ARMING LEVER PER AMM 52-22-00.

Part: BUCKLE — OUT OF POSITION (ZONE 800 - DOORS) · airframe 40,142 hrs · 15,756 cycles

AIRCRAFT WAS NOT GROUNDED: STRAP HANGING FROM SLIDE BUSTLE 1R. RE-SECURED STRAP BUCKLE AT R1 DOOR PER AMM 25-62-44.

Part: STRAP — OUT OF POSITION (R2 DOOR SLIDE) · airframe 40,022 hrs · 15,710 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD GALLEY(R2) EMERGENCY SLIDE STRAP HANGING OUT FROM BOTTOM. ATTACHED FORWARD STRAP AT BOTTOM OF EMERGENCY DOOR SLIDE AT FORWARD GALLEY R1 DOOR POSITION PER AMM 25-62-44.

Part: NUT — LOOSE (L1 DOOR) · airframe 39,995 hrs · 15,698 cycles

AIRCRAFT WAS GROUNDED: CHECK DOOR PRESSURE MESSAGE FOR L1 DOOR ON FWD CIDS PANEL. RE-SERVICED AND RE-TIGHTEN NUT FOR THE L1 DOOR IAW AMM 52-10-00. OPS CHECK LEAK CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (FWD GALLEY) · airframe 39,474 hrs · 15,463 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD FLIGHT ATTENDANT FLASHLIGHT NOT WORKING. REPLACED FWD GALLEY FLASHLIGHT (AALA202404303335) AND BATTERY (AALA202404307262). OP'S CK GOOD.

Part: BATTERY — INOPERATIVE (FWD GALLEY) · airframe 39,474 hrs · 15,463 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD FLIGHT ATTENDANT FLASHLIGHT NOT WORKING. REPLACED FWD GALLEY FLASHLIGHT (AALA202404303335) AND BATTERY (AALA202404307262). OP'S CK GOOD.

Part: HANDLE — OUT OF ADJUST (L3 DOOR) · airframe 39,393 hrs · 15,410 cycles

AIRCRAFT WAS NOT GROUNDED: ARMING LEVER ON DOOR 3L LOOSE. ADJUSTED ARMING HANDLE.

Part: ARMING LEVER — LOOSE (R2 DOOR) · airframe 39,012 hrs · 15,240 cycles

AIRCRAFT WAS NOT GROUNDED: SMALL ROUND METAL PIECE CAME LOOSE FROM 2R DOOR ARMING MECHANISM, F/A REPORTS THE 2R DOOR ARMING MECHANISM IS LOOSE. PROPERLY INSTALLED SET PIECE OF L2 DOOR ARMING MECHANISM

Part: LEVER — LOOSE (R2 DOOR) · airframe 38,728 hrs · 15,109 cycles

AIRCRAFT WAS NOT GROUNDED: CABIN 2R DOOR ARMING LEVER IS LOOSE. TIGHTENED ARMING LEVER ON 2R DOOR.

Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 38,608 hrs · 15,050 cycles

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

Part: POWER SUPPLY — INOPERATIVE (ZONE 200 - FUSE) · airframe 38,608 hrs · 15,050 cycles

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

Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 38,608 hrs · 15,050 cycles

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

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 38,608 hrs · 15,050 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER #4 ELEVATOR HINGE FITTING LOCKING LUG WORN BETWEEN STABILIZER RIBS 5 AND 7. REPAIRED HINGE FITTING LOCKING LUG PER SRM 55-26-47-300-001 PROCEDURE 2.A..

Part: FITTING — WORN (ZONE 300 - STABS) · airframe 38,608 hrs · 15,050 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILZER ELEVATOR HINGE FITING #2 ACTUATOR FITTING INBOARD SIDE LOCKING LUG WORN BETWEEN STABILIZER STATION 1809 AND 2707, RIBS 5 AND 7. REPIARED FITTING PER RM 55-26-47-300-001 PROCEDURE 2.A.

Part: SEAT TRACK — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 38,608 hrs · 15,050 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM-SEAT TRACK BETWEEN FR 12 AND FR 24 AT +Y765. REPLACED BEAM-SEAT TRACK PER SRM 51-72-11.

Part: SEAT TRACK — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 38,608 hrs · 15,050 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM-SEAT TRACK BETWEEN FR 12 AND FR 24 AT +Y1292. REPLACED BEAM-SEAT TRACK PER SRM 51-72-11.

Part: HOSE — WORN (ZONE 200 - FUSE) · airframe 38,608 hrs · 15,050 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT DOOR 833 ESCAPE SLIDE ENCLOSURE INFLATION HOSE WORN. REPLACED INFLATION HOSE PER CMM 25-66-10.

Part: HOSE — WORN (ZONE 800 - DOORS) · airframe 38,608 hrs · 15,050 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT DOOR 844 ESCAPE SLIDE ENCLOSURE INFLATION HOSE WORN. REPLACED HOSE PER CMM 26-66-11.

Part: DOOR — OUT OF POSITION (ZONE 900 - LAV/G) · airframe 38,416 hrs · 14,952 cycles

AIRCRAFT WAS NOT GROUNDED: MID CABIN LAVATORY ENTRY DOOR OFF TRACK AND DIFFICULT TO OPEN AND CLOSE. PERFORMED ADJUSTMENT TO MID LAVATORY DOOR PER AMM 52-50-00.

Part: HANDLE — LOOSE (ZONE 800 - DOORS) · airframe 38,302 hrs · 14,897 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR SLIDE ARM HANDLE AT 3L LOOSE. MAINTENANCE SECURED 3L DOOR SLIDE ARM HANDLE

Part: SIGN — MISSING (ZONE 800 - DOORS) · airframe 37,273 hrs · 14,426 cycles

AIRCRAFT WAS NOT GROUNDED: L2 EMERGENCY DOOR EXIT SIGN MISSING. INSTALLED SIGN PER AMM 33-50-01.

Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 36,895 hrs · 14,280 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT AFT LAVATORY DOOR JAMMED. ADJUSTED RIGHT AFT LAVATORY DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: DOOR — DEFECTIVE (ZONE 900 - LAV/G) · airframe 36,860 hrs · 14,217 cycles

AIRCRAFT WAS NOT GROUNDED: L2 MIDDLE LAVATORY DOOR DIFICULT TO OPEN. REPLACED DOOR ASSEMBLY PER AMM 25-45-19 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: PIN — OUT OF POSITION (ZONE 200 - FUSE) · airframe 36,712 hrs · 14,151 cycles

AIRCRAFT WAS GROUNDED: SEAT ROWS 24 ABC AND 25 ABC SEAT MOUNTED EMERGENCY AISLE LIGHT INOPERATIVE. MAINTENANCE FOUND A PIN PUSHED BACK ON CONNECTOR 7261VC7 AND RE-SEATED PIN. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-51-38.

Part: DOOR — UNSECURE (L3 LAVATORY) · airframe 35,610 hrs · 13,618 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY 3L ENTRY DOOR DIFFICULT TO OPEN AND LOOSE. RESECURED LAVATORY 3L DOOR PER AMM 25-45-19.

Part: LIFE VEST — OPEN (ZONE 200 - FUSE) · airframe 35,564 hrs · 13,594 cycles

AIRCRAFT WAS NOT GROUNDED: CLEANING CREW FOUND LIFE VEST OPENED FOR FLIGHT ATTENDANT SEAT AT 4R DOOR OUTBOARD SEAT. MAINTENANCE REPLACED LIFE VEST AS REQUIRED.

Part: TRACK — LACK OF LUBE (ZONE 800 - DOORS) · airframe 34,889 hrs · 13,283 cycles

AIRCRAFT WAS NOT GROUNDED: 4L DOOR SLIDE DIFFICULT TO ARM/DISARM. MAINTENANCE REMOVED DEBRIS FROM DOOR TRACK, LUBRICATED TRACK AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-20-00.

Part: LIGHT — NOT SEATED (ZONE 200 - FUSE) · airframe 34,553 hrs · 13,131 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY LIGHT ON R4 CABIN ENTRY DOOR IS INOPERATIVE. MAINTENANCE RE-SEATED EMERGENCY LIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-11 AND AMM 33-51-00.

Part: PIN — INSTALLED (ZONE 800 - DOORS) · airframe 34,363 hrs · 13,049 cycles

AIRCRAFT WAS NOT GROUNDED: NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO BOS WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. NOTE: NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE NOSE GEAR GROUND LOCK PIN INSTALLED AND REMOVED IT PER AMM 32-00-00.

Part: WINDOW — CRACKED (ZONE 200 - FUSE) · airframe 34,196 hrs · 12,985 cycles

AIRCRAFT WAS GROUNDED: FLIGHT DECK LEFT HAND CAPTAINS SIDE WINDOW CRACKED. REPLACED WINDOW PER AMM 56-11-12.

Part: COOLING FAN — LEAKING (APU) · airframe 32,300 hrs · 12,124 cycles

AIRCRAFT WAS GROUNDED: DIRTY SOCK SMELL WITH APU BLEED ON. REPLACED APU OIL COOLING FAN AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER AMM 49-52-51.

Part: UNKNOWN — ODOR (CABIN) · airframe 32,300 hrs · 12,124 cycles

AIRCRAFT WAS GROUNDED: DIRTY SOCK SMELL WITH APU BLEED ON. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: COOLING FAN — LEAKING (APU) · airframe 32,283 hrs · 12,115 cycles

AIRCRAFT WAS GROUND: MOLD SMELL COMING FROM PACKS DURING CLIMB AND DESCENT. FOUND APU OIL COOLING FAN LEAKING, REPLACED COOLING FAN AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER AMM 49-52-51. NO ODORS NOTED.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 32,120 hrs · 12,049 cycles

AIRCRAFT WAS GROUNDED: PUNGENT SMELL IN CABIN AND COCKPIT WHEN PACKS ARE POWERED WITH APU BLEED. MAINTENANCE ACCOMPLISHED TASK CARDS 26L0021001 AND 26L00021002, FOUND OIL COKING ON APU LOWER COMPRESSOR SCREEN. RAN ENGINES 10 MINUTES EACH WITH LEFT AND RIGHT PACKS, NO ODOR SMELLED IN CABIN AND FLIGHT DECK. PLACED APU ON MEL FOR FURTHER TROUBLESHOOTING. ACCOMPLISHED GENERAL VISUAL INSPECTION OF APU, FOUND EVIDENCE OF OIL AROUND PLENUM & FAN. DETERMINED LEAK WAS CAUSED BY THE APU OIL SYSTEM BEING OVER SERVICED. CLEANED APU EXTERNAL & RAN FOR 2 HOURS. NO EXTERNAL LEAKS NOTED. DRAINED OIL TO FULL MARK. MAINTENANCE ALSO PERFORMED DECONTAMINATION OF THE APU PER TASK CARD 26L00021004 WITH NO LEAKS OR ODORS NOTED.

Part: OIL SYSTEM — LEAKING (APU) · airframe 32,120 hrs · 12,049 cycles

AIRCRAFT WAS GROUNDED: PUNGENT SMELL IN CABIN AND COCKPIT WHEN PACKS ARE POWERED WITH APU BLEED. MAINTENANCE ACCOMPLISHED TASK CARDS 26L0021001 AND 26L00021002, FOUND OIL COKING ON APU LOWER COMPRESSOR SCREEN. RAN ENGINES 10 MINUTES EACH WITH LEFT AND RIGHT PACKS, NO ODOR SMELLED IN CABIN AND FLIGHT DECK. PLACED APU ON MEL FOR FURTHER TROUBLESHOOTING. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: SLIDE — NO TEST (ZONE 800) · airframe 31,780 hrs · 11,917 cycles

AIRCRAFT WAS GROUNDED: WHILE PERFORMING EMERGENCY POWER SUPPLY UNIT BATTERY TEST PER JOB CARD 26L00005005, ESCAPE SLIDE LIGHT 13WL AT DOOR 4L FOUND FAULTED VIA CLASS 1 MESSAGE. REMOVED AND REPLACED L4 DOOR ESCAPE SLIDE PER JOB CARD 26L00025010.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 30,403 hrs · 11,351 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING C-11 CHECK PS CHECK, FOUND FIRST OFFICERS FIXED WINDOW SHOWING EVIDENCE OF DELAMINATION. REMOVED AND REPLACED THE FIRST OFFICERS FIXED WINDOW PER AMM 56-11-12.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 29,845 hrs · 11,104 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY LIGHTS FAIL TEST. REMOVED AND REPLACED MID RIGHT EMERGENCY POWER SUPPLY UNIT BATTERY, IAW AMM 33-51-38.

Part: WIRE — BROKEN (DOOR SENSOR) · airframe 29,845 hrs · 11,104 cycles

AIRCRAFT WAS GROUNDED. DOOR 3L SHOWING OPEN ON ECAM DOOR PAGE AND FAP. FOUND WIRE 3154-2452 BROKEN. REPAIRED WIRE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK, PER ESPM 20-53-29.

Part: RESERVOIR — UNSERVICEABLE (EVAC SLIDE) · airframe 29,215 hrs · 10,849 cycles

AIRCRAFT NOT GROUNDED - R3 DOOR SLIDE, LOW PRESSURE. RESERVOIR GAGE SHOWS IN GREEN, HOWEVER, DUE TO HISTORY, REPLACED R3 DOOR SLIDE RESERVOIR ASSEMBLY PER AMM TASKS 25-62-49-000-001-A AND 25-62-49-400-001-A, OPERATIONAL CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 29,193 hrs · 10,836 cycles

AIRCRAFT NOT GROUNDED, R3 SLIDE PRESSURE LOW, CIDS (CABIN INTERCOMM DATA SYSTEM) CAUTION LIGHT. SERVICED R3 DOOR ASSIST BOTTLE TO FULL PRESSURE PER AMM 52-10-00, OKAY FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 28,151 hrs · 10,422 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD EMERGENCY FLASHLIGHT WAS NOT FLASHING. MAINTENANCE REPLACED FLASHLIGHT PER STANDARD PRACTICES.

Part: BATTERY — NO TEST (L1 FLASHLIGHT) · airframe 27,614 hrs · 10,186 cycles

AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT AT 1L DOOR OUTBOARD SEAT NOT WORKING. MAINTENANCE REPLACED FLASHLIGHT BATTERY PER STANDARD PRACTICES.

Part: FLASHLIGHT — INOPERATIVE (MID CABIN) · airframe 27,614 hrs · 10,186 cycles

AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT AT 3L WAS INOPERABLE. MAINTENANCE REPLACED FLASHLIGHT PER AMM 25-60-00.

Part: SLIDE — FALSE INDICATION (L3 DOOR) · airframe 27,320 hrs · 10,072 cycles

AIRCRAFT NOT GROUNDED: SLIDE PRESSURE LOW AT 3L. ACCOMPLISHED INTERFACE AND POWER UP TEST IAW AMM 23-73-00-740-005-B. OPS TEST OK. OK FOR SERVICE. DOOR 3L BOTTLE SHOWS GREEN BAND.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 27,112 hrs · 10,003 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT EMERGENCY FLASHLIGHT 2R INOPERABLE. MAINTENANCE REPLACED BATTERY PACK PER AMM 25-65-00.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 26,460 hrs · 9,764 cycles

AIRCRAFT WAS NOT GROUNDED: AIRCRAFT WOULD NOT DESCEND IN OPEN DESCENT MODE TO 5000 FEET AND A WARNING TO 3000 FEET. VERTICAL SPEED WAS REQUIRED TO DESCEND. MAINTENANCE PERFORMED CAT III LAND CAPABILITY TEST PER AMM 22-97-00 AND AFS TEST PER AMM 22-96-00. NO FAULTS NOTED.

Part: WASHER — DEFECTIVE (PROX SENSOR) · airframe 26,367 hrs · 9,729 cycles

AIRCRAFT NOT GROUNDED: FORWARD CARGO DOOR LIGHT CAME ON AFTER PUSH BACK AND WENT OUT, CAME ON AGAIN IN FLIGHT. EMERGENCY DECLARED AND FLIGHT RETURNED FOR OVER WEIGHT LANDING. ***SUPPLEMENTAL TO UPDATE SECTION 4 AND SECTION 5. MAINTENANCE ADJUSTED PROXIMITY SENSOR AND REPLACED TAB WASHERS PER AMM 52-71-00.*** (CLOSED)

Part: CONTROL UNIT — FAULTY (AUTOPILOT SYS) · airframe 24,720 hrs · 9,054 cycles

THE AIRCRAFT WAS GROUNDED. RETURNED TO CLT DUE TO AUTO-PILOT FAULT DURING CLIMB OUT. REMOVED AND REPLACED FLIGHT CONTROL UNIT PER AMM 22-81-12. BITE AND OPERATIONS TEST SATISFACTORY.

Part: WHEEL — VIBRATION (NLG) · airframe 24,657 hrs · 9,028 cycles

THE AIRCRAFT WAS GROUNDED. 4 MIN AFTER TAKEOFF, BELOW 10000 FT, LARGE AGGRESSIVE RHYTHMIC BANGING AND VIBRATION FELT IN AREA OF NOSE GEAR - 250 KTS AT TIME OF EVENT. AFTER SLOWING TO 220 KTS, AND FOR REMAINDER OF FLT, NOTHING ELSE. FLIGHT DECLARED AN EMERGENCY AND RETURNED TO PHX WITHOUT FURTHER INCIDENT. REPLACED RIGHT NOSE WHEEL ASSY PER AMM 32-41-12. RAN ENGINES, PACKS, HYDRAULICS, GALLEY COFFEE MAKER, AND CHILLER. PERFORMED WALK-AROUND OF A/C, ALL DOORS AND FAIRINGS SECURE. (R). SEE SDR AALA201811129014 FOR LEFT WHEEL ASSY.

Part: WHEEL — VIBRATION (NLG) · airframe 24,657 hrs · 9,028 cycles

THE AIRCRAFT WAS GROUNDED. 4 MIN AFTER TAKEOFF, BELOW 10000 FT, LARGE AGGRESSIVE RHYTHMIC BANGING AND VIBRATION FELT IN AREA OF NOSE GEAR - 250 KTS AT TIME OF EVENT. AFTER SLOWING TO 220 KTS, AND FOR REMAINDER OF FLT, NOTHING ELSE. FLIGHT DECLARED AN EMERGENCY AND RETURNED TO PHX WITHOUT FURTHER INCIDENT. REPLACED LEFT NOSE WHEEL ASSY PER AMM 32-41-12. RAN ENGINES, PACKS, HYDRAULICS, GALLEY COFFEE MAKER, AND CHILLER. PERFORMED WALK-AROUND OF A/C, ALL DOORS AND FAIRINGS SECURE. (L). SEE SDR AALA201811129015 FOR RIGHT WHEEL ASSY.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 23,917 hrs · 8,757 cycles

ROW 1L EMERGENCY LIGHT MISSING THE WHITE LENS. REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-19. OPS NORMAL.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 23,917 hrs · 8,757 cycles

ROW 8R EMERGENCY LIGHT MISSING THE RED LENS. REPLACED THE LIGHT AMM 33-51-18. OPS NORMAL.

Part: HANDLE — LOOSE (R2 DOOR ARMING) · airframe 23,608 hrs · 8,645 cycles

R2 DOOR ARMING LEVER FELL OUT, MAKING SLIDE DIFFICULT TO ARM AND DISARM. TIGHTENED THE HANDLE. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BATTERY — FAULTED (CABIN) · airframe 22,885 hrs · 8,372 cycles

AIRCRAFT WAS NOT GROUNDED. PERFORMED CIDS 1 TEST, FAULTED WITH "EPSU (13WL) AFT L" MESSAGE. REPLACED BATTERY OF EPSU PER AMM 33-51-38.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 22,695 hrs · 8,309 cycles

EMERGENCY LIGHT LENS MISSING AT ROW 34C. REPLACED THE LENS IAW CMM 25-22-50. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 22,399 hrs · 8,186 cycles

EXIT LIGHT LENS AT THE L4 DOOR MISSING. REPLACED THE LENS IAW AMM 33-50-00. OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE INDICATION (FUEL TANK) · airframe 21,938 hrs · 8,013 cycles

FUEL CTR R TRANFER FAULT ECAM IN FLIGHT, TURNED OFF THE CENTER TANK RIGHT TRANSFER IAW ECAM, NO FUEL INDICATED IN CENTER TANK. RESET IAW 28-46-00. OPS NORMAL, OK FOR SERVICE.

Part: DOOR SILL — CORRODED (L1 DOORWAY) · corrosion level 2 · airframe 21,546 hrs · 7,873 cycles

CORROSION FOUND ON THE L1 DOOR SILL LOCATED AT THE GIRT BAR FITTING AROUND THE AFT FOUR LOCK FASTENERS. REPAIRED THE DOOR SILL IAW SRM 53-11-14-283-005, FIG 101108.

Part: FLOORBEAM — CORRODED (FRAME 16) · corrosion level 2 · airframe 21,546 hrs · 7,873 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON CABIN FLOOR BEAM AT FR 16 AND LEFT BUTTLINE Y254. REPLACED CABIN FLOORBEAM AT FR 16 AND LEFT BUTTLINE Y254 PER DRAWING D53111023 AND SRM 51-42-11.

Part: SHEAR PLATE — CRACKED (FRAMES 69-70) · airframe 21,546 hrs · 7,873 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK AT LEFT HAND AFT LATERAL SHEAR PLATE BETWEEN FR 69 TO FR 70 AT LEFT STRINGER 23. REPLACED LEFT HAND AFT LATERAL SHEAR PLATE BETWEEN FR 69 TO FR 70 AT LEFT STRINGER 23 PER SRM 51-42-11.

Part: DOOR SILL — CORRODED (FRAME 16) · corrosion level 2 · airframe 21,546 hrs · 7,873 cycles

CORROSION FOUND ON DOOR SILL PLATE. REPAIRED DOOR SILL IAW SRM 53-11-14-283-005, FIG 101108.

Part: DOOR SILL — CORRODED (FRAME 67) · corrosion level 2 · airframe 21,546 hrs · 7,873 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION TO DOOR SILL AT FR 67 PLUS 16 INCHES TO LEFT BUTTLINE Y1732. CUT OUT CORRODED AREA AND INSTALLED REPAIR DOUBLER PER SRM 53-41-14-300-001 REPAIR PRINCIPLE 5.

Part: DOOR SILL — CORRODED (FRAME 68) · corrosion level 2 · airframe 21,546 hrs · 7,873 cycles

CORROSION ON THE R4 DOOR CUTOUT LOWER SILL AROUND MOST INBOARD FASTENER HOLES OF AFT GIRT BAR ATTACH POINT. REPAIRED THE DOOR SILL IAW SRM 53-41-14-300-001, REPAIR PRINCIPLE 7.

Part: BEAM — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 21,546 hrs · 7,873 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION OF L4 DOOR SILL BEAM BETWEEN FR 66 TO FR 68, STA 38529 TO STA 39511 AT LEFT STRINGER 23. REPLACED DOOR SILL BEAM BETWEEN FR 66 TO FR 68, STA 38529 TO STA 39511 AT LEFT STRINGER 23 PER SRM 51-42-11.

Part: FITTING — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 21,546 hrs · 7,873 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION TO DOOR SILL SHAPE BETWEEN FR 66 TO FR 68 AT LEFT STRINGER 23. REPLACED DOOR SILL SHAPE BETWEEN FR 66 TO FR 68 AT LEFT STRINGER 23 PER SRM 51-42-11.

Part: SHEAR PLATE — CORRODED (FRAMES 69-70) · corrosion level 2 · airframe 21,546 hrs · 7,873 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND AFT LATERAL SHEAR PLATE BETWEEN FR 69 TO FR 70 AT RIGHT STRINGER 23. REPLACED LATERAL SHEAR PLATE BETWEEN FR 69 TO FR 70 AT RIGHT STRINGER 23 PER SRM 51-42-11, 53-41-00-210-835 FIGURE 2.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 20,903 hrs · 7,620 cycles

SOFT SPOT IN THE FORWARD ENTRY JUST FORWARD OF FIRST CLASS AND GALLEY FLOOR PANEL. REPAIRED FLOOR PANEL 221EF IAW EA 273498. AIRCRAFT WAS GROUNDED.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 20,903 hrs · 7,620 cycles

FLOOR PANEL HAS A SOFT SPOT IN FORWARD ENTRY, JUST FORWARD OF FIRST CLASS AND GALLEY. REPAIRED THE FLOOR PANEL 222EF IAW EA 273498. AIRCRAFT WAS GROUNDED.

Part: UNKNOWN — ODOR (CABIN) · airframe 20,452 hrs · 7,452 cycles

F/A REPORTED A FOUL ODOR IN THE AREA OF THE FIRST THREE ROWS, RIGHT SIDE, NUMEROUS 1ST CLASS PASSENGERS COMPLAINED. PREFORMED TSM 21-00-00-810-802-A. NO FOUL ODOR NOTED,

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 18,812 hrs · 6,852 cycles

LEFT EMERGENCY AISLE LIGHT INOPERATIVE. FOUND THE WIRES AT SIDE WALL CONNECTION BROKEN AT THE CONNECTOR PLUG. REPAIRED THE WIRES IAW ESPM 20-44.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 18,577 hrs · 6,767 cycles

AIRCRAFT NOT GROUNDED: MOMENTARY FALSE LAVATORY SMOKE WARNING ON ECAM. WARNING LASTED 2-3 SECONDS AND THEN CLEARED. ALSO INDICATED ON CIDS PANEL, ALL LAVS INSPECTED WITH NO EVIDENCE OF SMOKE OR ODOR. R&R ALL A/C LAV SMOKE DETECTOR FILTERS, ACCOMPLISHED LAV SMOKE DETECTOR RESET AS PER AMM 26-17-00.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 18,577 hrs · 6,767 cycles

MOMENTARY LAVATORY SMOKE INDICATION ON ECAM WITH AUDIO WARNING 3- 5 SECONDS. NO RECURRENCE, FAULT CLEARED ON ITS OWN. LAVATORIES INSPECTED, NO SMOKE OR ODOR. MAINTENANCE ACCOMPLISHED BITE TEST OF THE SDCU IAW 26-17-00-710-001-A. NO FAULTS NOTED OK FOR SERVICE.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 17,849 hrs · 6,483 cycles

COVER FOR THE EMERGENCY LIGHT AT SEAT 4C FOUND MISSING. INSTALLED THE COVER IAW AMM 33-51-19-000-003A AND 33-51-19-400-003-A.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 17,120 hrs · 6,211 cycles

AIRCRAFT WAS GROUNDED: FORWARD GALLEY FLOOR HAS SOFT SPOT ABOUT CENTER SECTION. REPLACED FLOORBOARD 222EF IAW AMM 53-32-12.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 16,612 hrs · 6,007 cycles

R4 DOOR MISSING EMERGENCY LIGHT LENS COVER. INSTALLED THE COVER.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 15,484 hrs · 5,562 cycles

AIRCRAFT WAS NOT GNDED. AFT RT FLIGHT ATTENDANT FLASHLIGHT DEAD. REPLACED FLASHLIGHT BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: ACTUATOR — DEFECTIVE (NR 1 ENGINE) · airframe 14,324 hrs · 5,078 cycles

THE CREW REJECTED TAKEOFF, BELOW 80 KTS WHEN THEY RECEIVED A COMPRESSOR VANE FAULT ON ENG 1. THEY RETURNED TO THE GATE & THE AIRPLANE WAS TAKEN OUT OF SERVICE. REPLACED THE LT ENG VSV ACTUATOR IAW AMM 75-32-41 & 26T40075005.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 13,341 hrs · 4,690 cycles

FLIGHT ATTENDANT FLASHLIGHT AT DOOR 4L DOES NOT BLINK. REPLACED BATTERY ON FLIGHT ATTENDANT FLASHLIGHT AT DOOR 4L. OPERATIONS GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 11,745 hrs · 4,064 cycles

EXIT LIGHT AT 1C BROKEN. R & R EXIT LIGHT AT 1C.

Part: RESERVOIR — LOW PRESSURE (EVAC SLIDE) · airframe 10,766 hrs · 3,708 cycles

DOOR L2 EMER SLIDE RESERVOIR IS IN RED BAND. REPLACED DOOR L2 EMER SLIDE RESERVOIR IAW AMM 25-62-49-000.

Part: ARMING LEVER — LOOSE (L2 DOOR) · airframe 10,534 hrs · 3,618 cycles

ARMING LEVER AT 2L VERY LOOSE. TIGHTENED 2L ARMING LEVER HINGE POINT IAW AMM 52-20-00.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 8,409 hrs · 2,817 cycles

DURING INITIAL DESCENT RECEIVED ECAM MSG LAVATORY SMOKE. NO INDICATION OF SMOKE OR SMELL OF SMOKE IN ANY OF THE LAVATORIES. PERFORMED LAVATORY SMOKE DETECTOR TEST IAW A321 AMM 26-17-00 ALL TESTS PASSED.

Part: COMPUTER — FAULTY (FUEL SYSTEM) · airframe 7,998 hrs · 2,677 cycles

FLIGHT DIVERTED TO MEM FOR FUEL, RT CTR TANK TRANSFER VLV FAULT. REPLACED FQIS COMPUTER IAW A321 AMM 28-42-34. PERFORMED OPERATIONAL TEST OF MAIN TRANSFER SYS IAW A321 AMM 28-26-00-710-001, OPERATIONS CHECKED GOOD.

Part: DAMPER — OUT OF TOLERANCE (L4 DOOR) · airframe 7,735 hrs · 2,597 cycles

L4 DOOR DAMPER PRESS GAUGE POINTER IS IN THE YELLOW ZONE, OUT OF TOLERANCE AT 50F. SERVICED L4 DOOR DAMPER IAW A321 AMM 52-10-00-614-001A.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 7,286 hrs · 2,459 cycles

CREW REPORTED THE EXIT LIGHT COVER AT R4 DOOR MISSING. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT LENS. OPS CHECKED GOOD IAW AMM 33-51-13.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 5,613 hrs · 1,887 cycles

PILOT REPORT - FLOOR MAKING CRACKING NOISE AT ROW 18 AISLE AT BS22962 BETWEEN Y10 TO -Y10. REPLACED DAMAGED CABIN FLOORBOARD WITH NEW FLOORBOARD AT BS22962 BETWEEN Y10 TO -Y10 IAW AMM 53-22-12, PB 401.

Part: MEGAPHONE — DEFECTIVE (CABIN) · airframe 4,974 hrs · 1,668 cycles

FORWARD MEGA PHONE VOLUME KNOB MISSING. REMOVED AND REPLACED FORWARD MEGAPHONE.

Part: BUSHING — NOT SEATED (L4 DOOR) · airframe 4,808 hrs · 1,613 cycles

GUST LOCK ON DOOR L4 WILL NOT ENGAGE. RESEATED BUSHING FOR L4 DOOR STAY MECHANISM.

Part: LIGHT — BROKEN (CABIN) · airframe 4,770 hrs · 1,601 cycles

ROW 4 LEFT SEAT MOUNTED EMERGENCY EXIT LIGHT BROKEN. REPLACED ROW 4 SEAT MOUNTED EMERGENCY EXIT LIGHT IAW AIRBUS MAINTENANCE MANUAL 33-51-19.

Part: LINKAGE — STUCK (L4 DOOR) · airframe 4,665 hrs · 1,567 cycles

DOOR STAY MECHANISM AT DOOR 4L WILL NOT STAY LOCKED. REMOVED STUCK LINKAGE AT 4L DOOR STAY MECHANISM.

Part: LENS — MISSING (EXIT SIGN) · airframe 3,693 hrs · 1,239 cycles

EXIT SIGN DOOR 4R IS MISSING. REPLACED LENS AT 4R EMERGENCY EXIT LIGHT.

Part: SLIDE — LOW PRESSURE (R4 DOOR) · airframe 3,083 hrs · 1,028 cycles

DOOR 4R BOTTLE PRESSURE IS AT THE BOTTOM OF THE GREEN RANGE AND FLIGHT ATTENDANT REPORTED INTERMITTENT WARNING MESSAGE FOR LOW SLIDE PRESSURE DOOR 4R. REMOVED AND REPLACED DOOR 4R ESCAPE SLIDE.

Part: LENS — MISSING (CABIN) · airframe 2,742 hrs · 911 cycles

DOOR 4L EMERGENCY LIGHT COVER MISSING. REPLACED DOOR 4L EMERGENCY LIGHT LENS.

Part: OXYGEN MASK — OUT OF ADJUST (COCKPIT) · airframe 2,597 hrs · 865 cycles

FIRST OFFICER'S OXYGEN MASK EMERGENCY PRESSURE SELECTOR WILL NOT TEST - NO AIR FLOW. MAINTENANCE ADJUSTED MASK IN BOX. PRESS-TO-TEST WORKS NORMAL WITH AIRFLOW AND TEST INDICATION FUNCTIONS NORMAL.

Part: RESERVOIR — FAULTY (EVAC SLIDE) · airframe 2,181 hrs · 729 cycles

CHECK SLIDE PRESSURE ON L3 CIDS PANEL. REMOVED AND REPLACED SLIDE RESERVOIR ASSEMBLY.

Part: DEU — INOPERATIVE (ZONE 200) · airframe 2,157 hrs · 723 cycles

SHORTLY AFTER TAKEOFF, FIRST FLIGHT ATTENDANT REPORTS CAUTION LIGHT FLASHING CIDS PANEL SLIDE L3 PRESSURE NEEDS TO BE CHECKED. ALL INDICATIONS COCKPIT ECAM NORMAL. L3 SLIDE PRESSURE CHECKED ON GROUND AND IN GREEN, PREVIOUSLY WRITTEN UP. REMOVED AND REPLACED (DECODER/ENCODER UNIT) DEU B (300RH6) IAW AMM 23-73-47. OPS CHECKED GOOD, ALL INDICATIONS AND L3 SLIDE PRESSURE NORMAL.

Part: RESERVOIR — LOW PRESSURE (EVAC SLIDE) · airframe 2,101 hrs · 703 cycles

DOOR 2L LOW BOTTLE PRESSURE NOTED ON CIDS PANEL. FOUND BOTTLE PRESSURE INDICATOR IN GREEN BAND BUT NEAR BOTTOM. REMOVED AND REPLACED 2L SLIDE RESERVOIR IAW AIRBUS MAINTENANCE MANUAL 25-62-49.

Part: LENS — DETACHED (CABIN) · airframe 1,460 hrs · 496 cycles

EXIT COVER 4R ON FLOOR DETACHED. RE-INSTALLED EXIT COVER (LENS) AT 4R AS REQUIRED.