N582UW

Part: BATTERY — NO TEST (ZONE 200) · airframe 37,167 hrs · 15,285 cycles

AIRCRAFT WAS NOT GROUNDED: BATTERY FAULT FOR EMERGENCY POWER SUPPLY UNIT 11WL DISPLAYED DURING SYSTEM TEST. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38 WITH NO FAULTS NOTED.

Part: BATTERY — NO TEST (ZONE 200) · airframe 37,167 hrs · 15,285 cycles

AIRCRAFT WAS NOT GROUNDED: BATTERY FAULT FOR EMERGENCY POWER SUPPLY UNIT 12WL DISPLAYED DURING SYSTEM TEST. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38 WITH NO FAULTS NOTED.

Part: BATTERY — NO TEST (ZONE 200) · airframe 37,167 hrs · 15,285 cycles

AIRCRAFT WAS NOT GROUNDED: BATTERY FAULT FOR EMERGENCY POWER SUPPLY UNIT 14WL DISPLAYED DURING SYSTEM TEST. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38 WITH NO FAULTS NOTED.

Part: DAMPER PLATE — LOW PRESSURE (ZONE 800) · airframe 36,423 hrs · 14,956 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT PANEL INDICATES 2R DOOR PRESSURE LOW. MAINTENANCE SERVICED 2R DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-22-00.

Part: PIN — DAMAGED (ZONE 200) · airframe 36,026 hrs · 14,804 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 11, 12 AND 13 INOPERATIVE. MAINTENANCE REPINED PLUG 7261VC3A PER ESPM 20-44-11 AND WDM 33-51-06. A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WAS ACCOMPLISHED PER AMM 33-51-00 WITH NO ISSUES NOTED.

Part: THERMOCOUPLE — FAULTED (ZONE 400) · airframe 35,611 hrs · 14,636 cycles

AIRCRAFT WAS GROUNDED: AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO DFW DUE TO THE FLIGHT CREW REPORTING THAT WHILE CLIMBING THROUGH 10000FT, THEY NOTICED THAT THE LEFT ENGINE OIL QUANTITY INDICATION WAS SHOWING XX ALONG WITH AN ECAM ADVISORY FOR ENGINE OIL TEMPERATURE 155C AND THE TEMERATURE REACHED 165C AND THEN CAME DOWN TO 145C ONCE THE AIRCRAFT WAS LEVELED OFF AT FL 290. THE AIRCRAFT LANDED SAFEKLY AT DFW AND TAXIED TO THE GATE UNDER ITS OWN POWER. THE FLIGHT CREW REPORTED THAT AFTER LANDING, QUANTITY WAS SHOWING 25.5. MAINTENANCE REPLACED THE #1 ENGINE ACOC OIL TEMPERATURE THERMOCOUPLE PER AMM 79-32-15 AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 35,225 hrs · 14,467 cycles

AIRCRAFT WAS NOT GROUNDED: CHECK DOOR PRESSURE WARNING MESSAGE DISPLAYED ON FLIGHT ATTENDANT DISPLAY AFTER ARMING DOORS. MAINTNANCE FOUND 2R DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW AND SERVICED IT PER AMM 52-10-00. LOW PRESSURE WARNING MESSAGE ON FLIGHT FLIGHT ATTENDANTS PANEL EXTINGUISHED.

Part: PROXIMITY SENSOR — DEFECTIVE (ZONE 800) · airframe 34,860 hrs · 14,305 cycles

AIRCRAFT WAS NOT GROUNDED: R2 DOOR WOULD NOT DISARM AFTER ARRIVING AT THE GATE. AFTER APPROXIMATLEY 5 MINUTES, AND WITHOUT ANY FURTHER CREW MANIPULATION, DOOR DISARMED ON ITS OWN. MAINTENANCE REPLACED R2 DOOR DETECTOR PROXIMITY SWITCH 5WN2 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-73-11.

Part: PROXIMITY SENSOR — FAULTED (ZONE 800) · airframe 34,848 hrs · 14,300 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 2R SIDE WILL NOT DISARM. MAINTENANCE REPLACED R2 DOOR DETECTOR PROXIMITY SWITCH 5WN2 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-73-11.

Part: LIFE VEST — OPEN (ZONE 200) · airframe 34,812 hrs · 14,286 cycles

AIRCRAFT WAS NOT GROUNDED: OPENED CREW LIFE VEST FOUND UNDER LEFT HAND FLIGHT DECK OBSERVER SEAT. REPLACED LIFE VEST PER AMM 25-66-52.

Part: DOOR — OUT OF ADJUST (ZONE 800) · airframe 34,312 hrs · 14,079 cycles

AIRCRAFT WAS NOT GROUNDED: MID LAVATORY DOOR STUCK, DOOR WON'T OPEN. MAINTENANCE ADJUSTED MID LAVATORY BI FOLD DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-40-00.

Part: VENT LINE — LEAKING (APU) · airframe 33,578 hrs · 13,760 cycles

FLIGHT ATTENDANTS IN REAR OF AIRCRAFT REPORTED AN ODOR DURING DESCENT AND DURING DEPLANING. ODOR HAD A PUNGENT CHARACTERISTIC WITH MILD IRRITATION. MAINTENANCE REPLACED THE GEARBOX VENT LINE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: WARNING MESSAGE — ILLUMINATED (ZONE 800) · airframe 33,250 hrs · 13,620 cycles

AIRCRAFT WAS NOT GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO THE FLIGHT CREW REPORTING AFT CARGO DOOR SHOWED OPEN AT 2000 FEET ON DEPARTURE. ECAM CLEARED ON LANDING. THE AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED ** (OPEN)

Part: PROXIMITY SENSOR — MALFUNCTIONED (ZONE 800) · airframe 33,250 hrs · 13,620 cycles

AIRCRAFT WAS NOT GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO THE FLIGHT CREW REPORTING AFT CARGO DOOR SHOWED OPEN AT 2000 FEET ON DEPARTURE. ECAM CLEARED ON LANDING. THE AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED PROXIMITY SENSOR 32WV AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — INOPERATIVE (FWD FLASHLIGHT) · airframe 32,413 hrs · 13,247 cycles

AIRCRAFT WAS NOT GROUDNED: FLIGHT ATTENDANT ADVISES THAT THE FORWARD FLIGHT ATTENDANT JUMPSEAT EMERGENCY FLASHLIGHT NEEDS TO BE REPLACED. REPLACED EMERGENCY FLASHLIGHT BATTERY

Part: SENSE LINE — LOOSE (NR 2 ENGINE) · airframe 31,998 hrs · 13,049 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT DUE TO #2 ENGINE EPR FAULT, FLIGHT CREW REPORTED LOSS OF ALL ENGINE INDICATIONS. THE AIRCRAFT LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE P2/T2 SENSE LINE LOOSE AT THE #2 ENGINE NOSE COWL AND TIGHTENED THE LINE. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.

Part: SLIDE — NONE (ZONE 800 - DOORS) · airframe 27,513 hrs · 10,970 cycles

AIRCRAFT WAS GROUNDED: DURING CIDS BITE TEST: ESCAPE SLIDE LIGHT/EMERGENCY POWER SUPPLY UNIT (15WL) MID LEFT MESSAGE DISPLAYED. MAINTENANCE ACCOMPLISHED TSM 25-62-00-810-815A AND REPLACED THE 2L DOOR SLIDE PER TASK CARD 26L00025012. A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WAS ACCOMPLISHED.

Part: ENGINE — STALLED (ZONE 400 - NAC/P) · airframe 26,027 hrs · 10,297 cycles

AIRCRAFT WAS GROUNDED: LEFT ENGINE STALL ECAM MESSAGE DURING TAKE OFF ROLL AT APPROXIMATELY 40 KNOTS RESULTING IN AN ABORTED TAKE OFF BEING PERFORMED. MAINTENANCE REPLACED THE LEFT ENGINE PER TASK CARD 26L40071004.

Part: LIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 25,119 hrs · 9,895 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 9C EMERGENCY LIGHT INOPERATIVE. REMOVED/REPLACED LIGHT ASSEMBLY EMERGENCY ROW LIGHT 9C OPERATIONS CHECK GOOD.

Part: LIGHT — BROKEN (ZONE 200 - FUSE) · airframe 24,724 hrs · 9,729 cycles

AIRCRAFT WAS NOT GROUNDED: AT SEAT 19C EMERGENCY LIGHT BROKEN. **SUPPLEMENTAL REPORT FOR AALA202111100508: REPLACED EMERGENCY LIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-50-00 ** (CLOSED)

Part: NONE — NONE · airframe 24,724 hrs · 9,729 cycles

AIRCRAFT WAS NOT GROUNDED: AT SEAT 19C EMERGENCY LIGHT BROKEN. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: SWITCH — OUT OF POSITION (EMERGENCY LIGHTS) · airframe 23,239 hrs · 9,102 cycles

AIRCRAFT WAS NOT GROUNDED: CABIN EMERGENCY LIGHTS WILL NOT TURN OFF. FOUND EMERGENCY SWITCH DEPRESSED ON FORWARD FLIGHT ATTENDANTS PANEL. RELEASED SWITCH EMERGENCY LIGHTS EXTINGUISHED. OK FOR SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 22,263 hrs · 8,642 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT BATTERY 12WL FAILURE FAULT MESSAGE ON CIDS. REPLACED BATTERY PACK AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38-000-002-A

Part: BATTERY — INOPERATIVE (AFT FLASHLIGHT) · airframe 22,193 hrs · 8,599 cycles

AIRCRAFT WAS NOT GROUNDED. AFT LEFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED AFT LEFT FLIGHT ATTENDANT FLASHLIGHT BATTERY, PER AMM 25-65-53.

Part: FLASHLIGHT — INOPERATIVE (RT AFT CABIN) · airframe 21,957 hrs · 8,482 cycles

AIRCRAFT WAS NOT GROUNDED. RT AFT EMERGENCY FLASHLIGHT NEAR RAFT INOPERATIVE . REPLACED RT AFT FLASHLIGHT WITH NEW, IAW AMM 25-60-00. OPERATIONS CHECK GOOD.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 21,394 hrs · 8,262 cycles

AIRCRAFT WAS NOT GROUNDED: CABIN CREW FOUND EXIT SIGN COVER MISSING WITH EXPOSED WIRES, COVER FOUND ON A/C. REPLACED SIGN COVER.

Part: EPSU — INOPERATIVE (CABIN) · airframe 21,101 hrs · 8,152 cycles

AIRCRAFT IN BASE MAINTENANCE - EMERGENCY POWER SUPPLY UNIT 12WL INOP. REMOVED AND REPLACED EPSU (EMERGENCY POWER SUPPLY UNIT) 12WL PER AMM TASK 33-51-38-400. PERFORMED OPERATIONAL AND BITE CHECK PER AMM TASK 33-51-00-710-001-A, TEST OKAY.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 21,101 hrs · 8,152 cycles

AIRCRAFT IN BASE MAINTENANCE - FORWARD CARGO FLOOR PANEL 131FF DELAMINATED. REPLACED FLOOR PANEL 131FF PER A320 SRM 53-02-00-300-011 AND IRM 9701, REV I.

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 21,101 hrs · 8,152 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR LEFT HAND AFT DOOR HAS EXCESSIVE PLAY. REPLACED HINGE FITTINGS OF AFT DOOR LT ON NOSE LANDING GEAR PERCMM 52-82-32400-802-C01 AND AMM 32-22-13-410-001-A.

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 21,101 hrs · 8,152 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR RIGHT HAND AFT DOOR HINGE FITTING HAS EXCESSIVE PLAY/WEAR. REPLACED HINGE FITTING PER CMM 52-82-32-400-802-C01 AND AMM 32-22-13-410-001-A.

Part: MOUNT BOLT — LOOSE (NR 2 ENGINE) · airframe 21,101 hrs · 8,152 cycles

AIRCRAFT IN BASE MAINTENANCE: #2 ENGINE FORWARD MOUNT HAD 1 BOLT TURN DURING TORQUE CHECK. REPLACED ALL MOUNT BOLTS PER AMM 71-21-12.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,101 hrs · 8,152 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT DOOR CUT OUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23R. REPLACED LOWER SILL PER SRM 51-72-11.

Part: HINGE ARM — EXCESS PLAY (LT ELEVATOR) · airframe 21,100 hrs · 8,152 cycles

AIRCRAFT IN BASE VISIT: EXCESSIVE PLAY ELEVATOR HINGE ARM NO.5 BEARING ON LH HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING NO.5 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (LT ELEVATOR) · airframe 21,100 hrs · 8,152 cycles

AIRCRAFT IN BASE VISIT: EXCESSIVE PLAY ELEVATOR HINGE ARM 2 BEARING ON LH HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING NO.2 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (LT ELEVATOR) · airframe 21,100 hrs · 8,152 cycles

AIRCRAFT IN BASE VISIT: EXCESSIVE PLAY ELEVATOR HINGE ARM NO.3 BEARING ON LH HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING # 3 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (LT ELEVATOR) · airframe 21,100 hrs · 8,152 cycles

AIRCRAFT IN BASE VISIT: EXCESSIVE PLAY ELEVATOR HINGE ARM 1 BEARING ON LT HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING NO.1 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-400-001-A.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,101 hrs · 8,152 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR DUMMY RAIL BETWEEN FR 13 AND FR 16 AT +Y503.2. REPLACED DUMMY RAIL PER SRM 51-72-11.

Part: HINGE ARM — EXCESS PLAY (LT ELEVATOR) · airframe 21,100 hrs · 8,152 cycles

AIRCRAFT IN BASE VISIT: EXCESSIVE PLAY ELEVATOR HINGE ARM NO.4 BEARING ON LH HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING NO.4 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (RT ELEVATOR) · airframe 21,100 hrs · 8,152 cycles

AIRCRAFT IN BASE VISIT: EXCESSIVE PLAY ELEVATOR HINGE ARM NO.3 BEARING ON RH HORIZONTALSTABILIZER. REPLACED HINGE ARM END FITTING NO.3 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (RT ELEVATOR) · airframe 21,100 hrs · 8,152 cycles

AIRCRAFT IN BASE VISIT: EXCESSIVE PLAY ELEVATOR HINGE ARM NO.5 BEARING ON RH HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING NO.5 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (RT ELEVATOR) · airframe 21,100 hrs · 8,152 cycles

AIRCRAFT IN BASE VISIT: EXCESSIVE PLAY ELEVATOR HINGE ARM 2 BEARING ON RH HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING NO.2 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (RT ELEVATOR) · airframe 21,100 hrs · 8,152 cycles

AIRCRAFT IN BASE VISIT: EXCESSIVE PLAY ELEVATOR HINGE ARM 1 BEARING ON RH HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING NO.1 ON RH ELEVATOR AS PER AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (LT ELEVATOR) · airframe 21,100 hrs · 8,152 cycles

AIRCRAFT IN BASE VISIT: EXCESSIVE PLAY ELEVATOR HINGE ARM NO.6 BEARING ON LH HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING NO.6 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (RT ELEVATOR) · airframe 21,100 hrs · 8,152 cycles

AIRCRAFT IN BASE VISIT: EXCESSIVE PLAY ELEVATOR HINGE ARM NO.4 BEARING ON RH HORIZONTAL STABILIZER. REPLACED HINGE ARM LEND FITTING NO.4 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (RT ELEVATOR) · airframe 21,100 hrs · 8,152 cycles

AIRCRAFT IN BASE VISIT: EXCESSIVE PLAY ELEVATOR HINGE ARM NO.6 BEARING ON RH HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING NO.6 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-400-001-A.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,101 hrs · 8,152 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT DOOR CUT OUT LOWER SILL AFT CORNER FITTING AT FR 68 AND S23R. REPLACED CORNER FITTING PER SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 21,101 hrs · 8,152 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,101 hrs · 8,152 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL CENTER FITTING BETWEEN FR 66 AND FR 68 AT SS23L. REPLACED CENTER FITTING PER SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 21,101 hrs · 8,152 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: SUPPORT — CORRODED (FRAME 68) · corrosion level 2 · airframe 21,101 hrs · 8,152 cycles

AIRCRAFT IN BASE VISIT: CORROSION ON SILL AT FR68, STR23L (L= 3.041 W=0.065 D= 0.031 IN). PERFORMED PERMANENT REPAIR ON LOWER SILL LOC. FR 68 AT LEVEL STR 23L AFT GALLEY AREA IAW A321 SRM 53-41-14-300-001 FIGURE 001 (SHEET 04) REPAIR PRINCIPLE 7.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 20,699 hrs · 7,984 cycles

AIRCRAFT WAS GROUNDED: FORWARD CARGO COMPARTMENT FLOOR PANEL 131AF DELAMINATED. REPLACED FLOOR PANEL PER AMM 53-22-14.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 20,699 hrs · 7,984 cycles

AIRCRAFT WAS GROUNDED: FORWARD CARGO COMPARTMENT FLOOR PANEL 131EF DELAMINATED. REPLACED FLOOR PANEL PER AMM 53-22-14.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 14,972 hrs · 5,712 cycles

AIRCRAFT WAS NOT GROUNDED. EXIT LENS FOR LIGHT NEAR L1 FELL OFF. REATTACHED L1 EXIT LIGHT LENS.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 14,814 hrs · 5,655 cycles

L3 DOOR FLASHLIGHT WAS INOPERATIVE. REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-65-00, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 14,512 hrs · 5,557 cycles

EMERGENCY LIGHT LENS WAS MISSING AT SEAT 3AC. REPLACED THE LIGHT ASSY.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 14,503 hrs · 5,553 cycles

SEAT 8C AISLE EMERGENCY LIGHT COVER MISSING. INSTALLED A NEW EMERGEMCY LIOGHT. OPS CHECKED GOOD.

Part: COVER — DAMAGED (L4 DOOR HANDLE) · airframe 14,415 hrs · 5,521 cycles

L4 DOOR ASSIST HANDLE DAMAGED. INSTALLED THE DOOR HANDLE GRIP COVER IAW AMM 25-23-45.

Part: LENS — MISSING (CABIN) · airframe 14,014 hrs · 5,380 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 3R LIGHT COVER, FOR EXIT MISSING. MAINTENANCE REPLACED 3R EMERGENCY EXIT LIGHT LENS AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — MISSING (CABIN) · airframe 13,919 hrs · 5,346 cycles

THE AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT AT AISLE 14C LENS MISSING. REPLACED EMERGENCY LIGHT 14C. OPERATIONS CHECK GOOD PER AMM 33-51-19.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 13,258 hrs · 5,111 cycles

DELAMINATION BEYOND LIMITS ON THE AFT CARGO FLOOR PANEL 151PF, FRAMES 41 TO 42. REPLACED THE FLOOR PANEL IAW AMM 53-42-14. AIRCRAFT WAS GROUNDED

Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 13,258 hrs · 5,111 cycles

AFT CARGO FLOOR PANEL 151LF DELAMINATED BEYOND LIMITS. REPLACED THE FLOOR PANEL IAW AMM 53-42-14. THE AIRCRAFT WAS GROUNDED.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 13,258 hrs · 5,111 cycles

DELAMINATED FLOOR PANEL 151GF IN THE AFT CARGO AREA BETWEEN FRAME 41 & 42. REPLACED THE FLOOR PANEL IAW AMM 53-42-14.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 13,059 hrs · 5,032 cycles

THE AIRCRAFT WAS NOT GROUNDED. FORWARD FLIGHT ATTENDANT FLASHLIGHT HOLDER BROKEN. REPLACED FLASHLIGHT HOLDER PER AMM 25-60-10-401. OK FOR SERVICE.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 12,260 hrs · 4,721 cycles

PLASTIC COVER FOR EXIT LIGHT AT 4L DOOR DAMAGED. REPLACED BROKEN EXIT LIGHT AT 4L DOOR IAW AMM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 11,965 hrs · 4,599 cycles

L4 DOOR EXIT SIGN LENS MISSING.

Part: LIGHT — BROKEN (CABIN) · airframe 8,501 hrs · 3,266 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT AT SEAT 1C IS BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY PER AMM 33-51-18.

Part: LIGHT — BROKEN (CABIN) · airframe 8,501 hrs · 3,266 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT AT SEAT 6C IS BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY PER AMM 33-51-18.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 7,739 hrs · 2,970 cycles

DURING DOOR ARMING, THE FLIGHT ATTENDANT REPORTED THAT THE CIDS PANEL MESSAGE INDICATED CHECK R2 DOOR PRESSURE, AMBER PRESSURE. REPLACED R2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER IAW AMM 52-22-14-0401.

Part: DOOR — MISSING (FAN COWL) · airframe 7,658 hrs · 2,945 cycles

ON ARRIVAL, THE NR 1 ENGINE LT FAN COWL OIL SERVICE DOOR WAS FOUND MISSING DURING A WALK AROUND INSPECTION. AIRCRAFT GROUNDED: MAINTENANCE REPLACED THE NR 1 ENGINE OUTBOARD FAN COWL IAW AMM 71-13-11-0401.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 7,649 hrs · 2,943 cycles

AIRCRAFT WAS GROUNDED, CHECK 2R DOOR PRESSURE MESSAGE ON F/A CIDS PANEL. SERVICED 2R DOOR ASSIST BOTTLE IAW AMM 52-22-00-614-002A.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 7,431 hrs · 2,874 cycles

AFTER DEPARTING THE GATE, FLIGHT ATTENDANT REPORTED THE R2 DOOR SLIDE PRESSURE LOW FAULT MESSAGE. AIRCRAFT GROUNDED. MAINTENANCE SERVICED R2 DOOR DAMPER IAW AMM 52-22-00-614-002-A AND ACCOMPLISHED A SATSIFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 7,092 hrs · 2,756 cycles

AIRCRAFT WAS NOT GROUNDED, DOOR 2R BOTTLE PRESSURE LOW. SERVICED R2 DOOR BOTTLE PRESSURE IAW AMM 52-22-00.

Part: SCHRADER VALVE — LEAKING (R2 DOOR) · airframe 6,183 hrs · 2,438 cycles

AIRCRAFT WAS NOT GNDED. 2R DOOR ASSIST BOTTLE PRESS LOW ON PUSHBACK. FOUND SCHRADER VLV ON DOOR ASSIST BOTTLE LEAKING. REPLACED SCHRADER VLV & SERVICED ASSIST BOTTLE IAW GPM 12-02-6.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 6,160 hrs · 2,427 cycles

AIRCRAFT WAS NOT GNDED. 2R SLIDE PRESS LOW. SERVICED 2R DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 6,093 hrs · 2,404 cycles

AIRCRAFT WAS NOT GNDED. R2 DOOR ASSIST BOTTLE BELOW MINIMUM. SERVICED R2 DOOR ASSIST BOTTLE IAW AMM 32-40-00.

Part: DIAPHRAGM — LEAKING (R2 DOOR) · airframe 6,060 hrs · 2,390 cycles

AIRCRAFT WAS NOT GNDED. 2R DOOR LOW PRESS ON CIDS. REPLACED R2 DOOR DAMPER DIAPHRAGM & O RING SEAL FOR FILLING VLV IAW AMM 52-10-00.

Part: SCHRADER VALVE — LOOSE (R2 DOOR) · airframe 6,060 hrs · 2,390 cycles

AIRCRAFT WAS NOT GNDED. FLIGHT ATTENDANT CIDS PANEL HAS AN AMBER CHECK DOOR PRESS MSG, ADJACENT TO DOOR 2R. FOUND SCHRADER VLV LOOSE, TIGHTENED VLV & SERVICED DAMPER IAW AMM 52-10-00-614-001A. CIDS MSG CLEARED.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 6,011 hrs · 2,371 cycles

AIRCRAFT WAS NOT GNDED. CIDS PANEL INDICATED 2R DOOR LOW PRESS. SERVICED 2R DOOR ASSIST BOTTLE IAW AMM 52-10-00 & CIDS MSG CLEARED.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 5,947 hrs · 2,345 cycles

AIRCRAFT WAS NOT GNDED. CIDS CAUTION DOOR 2R PRESS. SERVICED R2 DOOR ASSIST BOTTLE TO PROPER LEVEL IAW AMM IAW 52-22-00-614-002-A.

Part: ACCUMULATOR — LOW PRESSURE (R2 DOOR) · airframe 5,884 hrs · 2,322 cycles

AIRCRAFT WAS NOT GNDED. 2R DOOR PRESS. SERVICED DOOR 2R PRESS ACCUMULATOR IAW AMM 52-22-00. CIDS INDICATION CHECKS OK.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 5,315 hrs · 2,097 cycles

AIRCRAFT WAS NOT GNDED. R2 DOOR ASSIST BOTTLE PRESS LOW ON FAP. SERVICED DOOR ASSIST BOTTLE IAW TASK 52-22-00. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 5,130 hrs · 2,025 cycles

AIRCRAFT WAS NOT GNDED. 2R DOOR PRESS IN AMBER. SERVICED 2R DOOR ASSIST BOTTLE IAW AMM 52-22-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,059 hrs · 1,994 cycles

AIRCRAFT WAS NOT GNDED. EMER PATH LIGHTING INOPERATIVE AT 6C. REPLACED EMER LIGHT AT 6C. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-19.

Part: DAMPER — LOW PRESSURE (R2 DOOR) · airframe 4,717 hrs · 1,861 cycles

R2 DOOR BOTTLE PRESS INDICATION ON FAP. SERVICED R2 DOOR DAMPER IAW AMM 52-10-00-614-001.

Part: DAMPER — LOW PRESSURE (R2 DOOR) · airframe 4,568 hrs · 1,790 cycles

2R DOOR INDICATING DOOR PRESS LOW ON CIDS PANEL. ACCOMPLISHED CHECK IAW AMM 52-22-00-614-002A & SERVICED IAW AMM 52-22-00-614-002A. NO FAULTS FOUND MSGS.

Part: ACTUATOR — LOW PRESSURE (R2 DOOR) · airframe 4,317 hrs · 1,692 cycles

FLIGHT 509, 2R DOOR CHECK DOOR PRESS INDICATION ON FLIGHT ATTENDANT PANEL. ACCOMPLISHED PRESS CHECK IAW AMM 52-22-200-001-A. SERVICED EMER DOOR 2R IAW AMM 52-22-00-614-002-A. NO FAULTS NOTED.

Part: LENS — BROKEN (CABIN) · airframe 4,259 hrs · 1,670 cycles

RED EMER LIGHT LENS BROKEN OFF AT 22C. REPLACED EMER LIGHT.

Part: SCHRADER VALVE — LEAKING (R2 DOOR) · airframe 4,202 hrs · 1,650 cycles

FLIGHT ATTENDANT CIDS PANEL MSG, CHECK PRESS R2 DOOR. R & R THE R2 DOOR ASSIST SHRADER VLV ASSEMBLY. SERVICED DOOR ASSIST BOTTLE & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 52-10-00-614-01-A.

Part: CYLINDER — LOW PRESSURE (EMERGENCY EXIT)

R2 EMER EXIT DOOR DAMPER & CYLINDER INDICATES PRESS IN THE YELLOW BAND RANGE AT 71 DEGREES F. SERVICED DAMPER & CYLINDER TO GREEN BAND IAW AMM TASK 52-22-00-614-002. BAND WITH AN OUTSIDE TEMPERATURE OF 71 DEGREES.

Part: BOTTLE — LOW PRESSURE (R2 DOOR)

R2 DOOR ASSIST BOTTLE LOW. SERVICED BOTTLE IAW AMM 52-10-00.

Part: ACTUATOR — LOW PRESSURE (R2 DOOR) · airframe 4,035 hrs · 1,588 cycles

2R DOOR PRESS OC CIDS PANEL. PERFORMED AMM TASK 52-22-00-614-002-A NOW OK.

Part: ACTUATOR — LOW PRESSURE (R2 DOOR) · airframe 3,956 hrs · 1,564 cycles

FLIGHT 481 EN-ROUTE, DURING DESCENT, DOOR 2R HISSING LOUD. CHECK DOOR PRESS & CHECK DOOR LIGHT IS FLASHING. SERVICED 2R DOOR IAW AMM 52-22-00-614-002A. CLEANED DOOR SEAL. NO DEFECTS NOTED. OK FOR SERVICE.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 3,879 hrs · 1,538 cycles

CIDS PANEL DISPLAYS CHECK 2R DOOR PSI. SERVICED DOOR 2R ASSIST BOTTLE IAW AMM 52-22-00.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 3,796 hrs · 1,499 cycles

FLIGHT ATTENDANT CIDS PANEL DOOR & SLIDE DOOR 2R SHOWS CHECK DOOR PRESSURE. SERVICED 2R DOOR POWER ASSIST BOTTLE PRESSURE TO CORRECT PRESSURE IAW AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (R2 DOOR ASSIST) · airframe 3,736 hrs · 1,477 cycles

CIDS PANEL SHOWS R2 DOOR PRESSURE BUT NOT AT R2. SERVICED R2 DOOR SLIDE EMERGENCY ACCUMULATOR AS REQUIRED IAW AMM 52-22-00-614-002-A.

Part: BOTTLE — LOW PRESSURE (R2 DOOR)

2R DOOR SLIDE PRESSURE SHOWS LOW. SERVICED 2R DOOR BOTTLE IAW AMM 52-22-00. OK FOR SERVICE. CIDS CHECKED OK.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 3,594 hrs · 1,419 cycles

R2 DOOR ASSIST BOTTLE LOW PRESS. SERVICED R2 DOOR ASSIST BOTTLE IAW AMM 52-22-00-0301. LEAK CHECK OK.

Part: ACTUATOR — LOW PRESSURE (R2 DOOR) · airframe 3,513 hrs · 1,388 cycles

FLIGHT 1865 EN-ROUTE, DURING PUSHBACK FLIGHT ATTENDANT PANEL HAD DOOR 2R LOW PRESS INDICATOR ILLUMINATE. ALL INDICATION ON ECAM WERE NORMAL. SERVICED 2R DOOR PRESS IAW AMM 52-22-00-614-002A. CIDS INDICATION CHECKED OK.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 3,421 hrs · 1,352 cycles

CIDS 2R DOOR CHECK PRESS. SERVICED R2 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001A.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 2,377 hrs · 922 cycles

CABIN FLASHLIGHT LOCATED UNDER FWD FLIGHT ATTENDANT JUMP SEAT INOPERATIVE. REPLACED CABIN FLASHLIGHT.

Part: UNKNOWN — ODOR (CABIN) · airframe 520 hrs · 197 cycles

FLIGHT ATTENDANT B NOTIFIED COCKPIT OF DIRTY SOCK SMELL IN CABIN WHEN ACFT DOOR CLOSED & READY FOR PUSHBACK. FLIGHT ATTENDANT B ALSO FELT LIGHT HEADED. MX ACCOMPLISHED JOB CARD 26L00021001, COULD NOT DUPLICATE ANY ODOR.