N162UW

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 77,551 hrs · 29,975 cycles

AIRCRAFT WAS NOT GROUNDED: R4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.

Part: ENGINE — OVERTEMP (NR 2) · airframe 77,056 hrs · 2,970 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ABQ DUE TO THE FLIGHT CREW REPORTING THAT ON TAKEOFF #2 ENGINE OVERTEMP OCCURRED, FLIGHT CREW ACCOMPLISHED ECAM PROCEDURES AND SHUT DOWN THE ENGINE. THE AIRCRAFT LANDED SAFELY AT ABQ AND TAXIED TO THE GATE UNDER ITS OWN POWER. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: ENGINE — OVERTEMP (NR 2) · airframe 77,056 hrs · 2,970 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ABQ DUE TO THE FLIGHT CREW REPORTING THAT ON TAKEOFF #2 ENGINE OVERTEMP OCCURRED, FLIGHT CREW ACCOMPLISHED ECAM PROCEDURES AND SHUT DOWN THE ENGINE. THE AIRCRAFT LANDED SAFELY AT ABQ AND TAXIED TO THE GATE UNDER ITS OWN POWER. **SUPPLEMENTAL REPORT FOR AALA202507152094: MAINTENANCE DETERMINED THAT THE EGT EXCEEDANCE WAS WITHIN AREA "A" LIMITS, AND ACCOMPLISHED A BORESCOPE INSPECTION OF THE #2 ENGINE HPT / LPT STAGE 1 PER AMM 72-00-00-200-008-A WITH NO FINDING REPORTED. MAINTENANCE ACCOMPLISHED A WATER WASH ON THE #2 ENGINE PER TASK CARD 26L40072018. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ISSUES NOTED. ** (CLOSED)

Part: BATTERY — NO TEST (ZONE 200) · airframe 76,028 hrs · 29,366 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED THAT THE FLASHLIGHT AT THE 4R FLIGHT ATTENDANT LOCATION IS NOT CHARGING. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY PER AMM 25-60-00.

Part: ARMING LEVER — STICKING (ZONE 800) · airframe 75,911 hrs · 29,315 cycles

AIRCRAFT WAS GROUNDED: UPON BEING NOTIFIED THE 4R DOOR ARMING LEVER WAS STIFF IN ITS MOVEMENT, THE FLIGHT ATTENDANTS ATTEMPTED TO CHECK THE FUNCTION OFTHE LEVER AND FOUND THAT NOT ONLY WAS IT VERY STIFF BUT WAS ALSO MAKING GRINDING NOISES FROM THE INSIDE OF THE DOOR. THEY MENTIONED IT WAS DIFFERENT THAN ANYTHING THEY'VE EXPERIENCED IN TRAINING OR PAST OPERATIONS. MAINTENANCE CHECKED THE LEVER AND FOUND THAT WAS HARD TO MOVE WITH LOUD GRINDING SOUNDS AS REPORTED BY THE FLIGHT ATTENDANTS. MAINTENANCE ACCOMPLISHED AN INSPECTION OF THE AFT RIGHT PASSENGER / CREW DOOR INTERNAL STRUCTURE WITH NO ISSUES REPORTED. MAINTENANCE LUBRICATED THE ARM / DISARM MECHANISM PER AMM 12-22-52.

Part: HINGE — OUT OF POSITION (ZONE 800) · airframe 75,852 hrs · 29,284 cycles

AIRCRAFT WAS NOT GROUNDED: MID LAVATORY DOOR WILL NOT OPEN. MAINTENANCE ATTACHED BACK MID LAVATORY DOOR HINGES BACK TO GROOVE PER AMM 25-40-00.

Part: GIRT BAR — FAULTED (ZONE 800) · airframe 75,198 hrs · 29,007 cycles

AIRCRAFT WAS GROUNDED: DOOR 1R WILL NOT REMAIN ARMED WHEN SELECTED TO ARM. MAINTENANCE REPLACED GIRT BAR ASSY ON DOOR 1R SLIDE IAW AMM 25-62-44.

Part: SLAT SYSTEM — MALFUNCTIONED · airframe 75,198 hrs · 29,007 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INBOUND INTO CLT DUE TO THE FLIGHT CREW REPORTING THAT A FLIGHT CONTROL SLAT SYSTEM 1 FAULT DISPLAYED IN FLIGHT AND THE SLATS WERE FROZEN IN LESS THAN 1 POSITION. THE AIRCRAFT LANDED SAFELY AT CLT AND TAXIED TO THE GATE UNDER ITS OWN POWER. (OPEN)

Part: ACTUATOR — FAULTED (ZONE 600 SLAT) · airframe 75,198 hrs · 29,007 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INBOUND INTO CLT DUE TO THE FLIGHT CREW REPORTING THAT A FLIGHT CONTROL SLAT SYSTEM 1 FAULT DISPLAYED IN FLIGHT AND THE SLATS WERE FROZEN IN LESS THAN 1 POSITION. THE AIRCRAFT LANDED SAFELY AT CLT AND TAXIED TO THE GATE UNDER ITS OWN POWER. **SUPPLEMENTAL REPORT FOR AALA202412125064: MAINTENANCE FOUND RIGHT WING SLAT ACTUATOR 6087CM TRIPPED AND REPLACED IT PER AMM 27-84-49. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED. ** (CLOSED)

Part: SWITCH — MISINSTALLED (ZONE 800) · airframe 75,040 hrs · 28,930 cycles

AIRCRAFT IN BASE MAINTENANCE: EVACUATION SIGNAL DOES NOT SOUND AT DOOR 3 HOWEVER DOOR 3 RESET DOES SILENCE DOOR 4 SIREN. MAINTENANCE CORRECTLY INSTALLED EVACUATION PUSH BUTTON SWITCH AT DOOR 3 AND ACCOMPISHED A SATISFACTORY OPERATIONAL TEST PER AMM 23-73-00.

Part: SLIDE — DEFORMED (ZONE 800) · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 831 SLIDE IS DEFORMED. REPLACED SLIDE PER TASK CARD 26C83152008.

Part: FRAME SPLICE — WORN (ZONE) · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLES ON SPLICE FRAME 66 OF FLOOR BEAM -Y765. REPLACED SPLICE OF FLOOR BEAM PER NCN 6798546.

Part: WINDOW — SCRATCHED (ZONE 800) · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER CREW DOOR 834 WINDOW SCRATCHED. REPLACED WINDOW PER AMM 56-31-15.

Part: WINDOW — SCRATCHED (ZONE 800) · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER CREW DOOR 833 WINDOW SCRATCHED. REPLACED WINDOW PER AMM 56-31-15.

Part: BOTTLE — LOW PRESSURE (ZONE 800 SLDE) · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT DOOR DOOR 843 SLIDE INFLATION RESERVOIR PRESSURE LOW. **SUPPLEMENTAL REPORT FOR AALA202410296161: MAINTENANCE REPLACED SLIDE INFLATION RESERVOIR PER AMM 25-62-49.** (CLOSED)

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENNACE: EMERGENCY EXIT DOOR DOOR 843 SLIDE INFLATION RESERVOIR PRESSURE LOW. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: FITTING — WORN (ZONE 200) · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL AFT CORNER SHAPE FITTING HAS ELONGATE FASTENER HOLE AT FR 68 AND S23R. REPLACED AFT CORNER SHAPE FITTING PER SRM 51-72-11.

Part: CLEAT — CORRODED (ZONE 100) · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT CLEAT AT FR 35.1 BETWEEN S39R AND S40R. REPLACED CLEAT PER SRM 51-72-11.

Part: BOLT — CORRODED (ZONE 600) · corrosion level 2 · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON BOLT ATTACHMENT LOCATED AT SLAT TRACK 10 IN THE LOWER AFT POSITION ON RIGHT-HAND WING. REPLACED BOLT PER AMM 27-84-66-400-002-A.

Part: BOLT — CORRODED (SLAT TRACK) · corrosion level 2 · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON BOLT ATTACHMENT LOCATED AT SLAT TRACK 5 LOWER POSITION RIGHT-HAND WING. REPLACED BOLT PER AMM 27-84-64-400-002-A.

Part: FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SPIGOT FITTING RECEPTACLE ON LEFT HAND PYLON. REPLACED SPIGOT FITTING PER A319 SRM 54-51-12-300-001.

Part: RECEPTACLE — CORRODED (ZONE 400) · corrosion level 2 · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SPIGOT FITTING RECEPTACLE ON RIGHT HAND PYLON. REPLACED SPIGOT FITTING RECEPTACLE PER A321 SRM 54-51-12.

Part: PRESSURE DECK — CRACKED (ZONE 200) · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK MEMEBRANE OPEN HOLE AT FR 36 AND -Y1516. REPAIRED PRESSURE DECK MEMBRANE PER EA 357693.

Part: PRESSURE DECK — CRACKED (ZONE 200) · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK MEMEBRANE OPEN HOLE AT FR 36 AND +Y1516. REPAIRED PRESSURE DECK MEMBRANE PER EA 357693.

Part: FRAME — CRACKED (ZONE 200) · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT RIGHT PASSENGER / CREW DOOR CUT OUT FRAME AFT FACE AT FR 68 AND S8R. REPLACED FRAME PER SRM 53-41-12.,

Part: SKIN PANEL — CORRODED (ZONE 500) · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE UPPER SKIN PANEL LOWER SURFACE AT RIB 14. REPAIRED SKIN PANEL PER EA 357758.

Part: SKIN PANEL — CORRODED (ZONE 600) · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING REAR SPAR TRAILING EDGE TOP SKIN PANEL #2 LOWER SURFACE AT RIB 14. REPAIRED SKIN PANEL PER EA 357759.

Part: SKIN PANEL — CORRODED (ZONE 600) · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING REAR SPAR TRAILING EDGE TOP SKIN PANEL #2 LOWER SURFACE AT RIB 10. REPAIRED SKIN PANEL PER EA 357759.

Part: DOUBLER — NONE (ZONE 200 - FUSE) · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR AND FRAME REPLACEMENT AT FR 16 RIGHT AND THE #7 DOOR STOP FITTING THE UPPER CORNER DOUBLER NEEDS TO BE REPLACED PER THE INSTRUCTIONS ON EA 357331. REPLACED THE UPPER CORNER DOUBLER PER EA 357331.

Part: FRAME — CRACKED (ZONE 200) · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME DOUBLE JOGGLE AREA AT FR 16 RIGHT AND #7 DOOR STOP FITTING. REPLACED FRAME PER EA 357331.

Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT AFT PASSENGER / CREW DOOR CUTOUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23R. REPLACED SILL PER SRM 51-42-11.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SILL LOCATED AT LEVEL STR 23L, BETWEEN FR 66 AND FR 68 IN AFT GALLEY AREA. ACCOMPLISHED PERMANENT REPAIR ON LOWER SILL PER SRM 53-41-14-300-001.

Part: FITTING — CRACKED (ZONE 200) · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT DOOR STOP #7 BETWEEN FR 20 AND FR 21 AT S10L. REPLACED INTERCOSTAL FITTING PER SRM 51-42-11.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK ON FORWARD GALLEY FLOOR BEAM LOCATED BETWEEN AT FR 24 ON -Y160. REPLACED FLOOR BEAM PER SRM 51-42-11-801.

Part: FLOORBEAM — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT GALLEY FLOOR BEAM LOCATED BETWEEN ON FR 70 AT -Y765 REPLACED FLOOR BEAM PER SRM 51-42-11-801.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK -Y765 LOCATED BETWEEN FR 21 AND FR 23 IN FORWARD GALLEY AREA. REPLACED SEAT TRACK PER SRM 51-42-11-801.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD GALLEY AREA FLOOR BEAM AT FR 16 AT +Y1292. REPLACED FLOOR BEAM PER SRM 51-42-11.

Part: SHEAR PLATE — CRACKED (ZONE 100) · airframe 75,039 hrs · 28,929 cycles

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

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT GALLEY FLOOR BEAM LOCATED BETWEEN FR 68 AND FR 70 AT -Y160. REPLACED FLOOR BEAM PER SRM 51-42-11-801.

Part: SHEAR PLATE — CRACKED (ZONE 200) · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK ON AFT GALLEY SHEAR PLATE LOCATED BETWEEN FR 59 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-72-11.

Part: TAB — DEBONDED (ZONE 500 FLAP) · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: DEBONDED OUTBOARD FLAP TAB ON LEFT-HAND WING. PERFORMED PERMANENT REPAIR ON UPPER SKIN OUTBOARD FLAP TAB LEFT-HAND WING PER EA #326690A.

Part: SKIN PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING REAR SPAR TRAILING EDGE TOP SKIN PANEL #2 LOWER SURFACE AT RIB 7. REPAIRED SKIN PANEL PER EA 357759.

Part: SKIN PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 75,039 hrs · 28,929 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION LEFT WING TRAILING EDGE TOP SKIN PANEL #2 UPPER SURFACE BETWEEN RIBS 24 AND 25. REPAIRED SKIN PANEL PER EA 357758.

Part: CHILLER — ODOR (CABIN) · airframe 74,788 hrs · 28,796 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTS LIGHT BURNING SMELL COMING FROM THE FWD CHILLER/1R DOOR AREA. OPEN

Part: CHILLER — DEFECTIVE (FWD GALLEY) · airframe 74,788 hrs · 28,796 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTS LIGHT BURNING SMELL COMING FROM THE FORWARD CHILLER AT THE 1R DOOR AREA. MAINTENANCE REPLACED THE CHILLER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-34-51.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 74,569 hrs · 28,689 cycles

AIRCRAFT WAS NOT GROPUNDED: DURING A BITE TEST OF THE PROGRAMMING TEST PANEL, MAINTENANCE FOUND MESSAGE SLIDE BOTTLE MID RIGHT. MAINTENANCE SERVICED THE R3 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-22-00.

Part: ENGINE — POWER LOSS (ZONE 400 - NAC/P) · airframe 74,327 hrs · 28,596 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO MCO: FLIGHT CREW REPORTED A SUDDEN LOSS OF POWER EXPERIENCED ON NUMBER 2 ENGINE DURING ROTATION. THE AIRCRAFT EXPERIENCED A VIOLENT YAW MOTION TO THE RIGHT. THE FLIGHT CREW REPORTED THAT THERE WERE BIRDS WERE OBSERVED DURING ROTATION AND SUSPECTED IT WAS A BIRD STRIKE. THE AIRCRAFT LANDED SAFELY AT MCO AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE REVIEWED THE FDR DATA FOR THIS EVENT AND COULD NOT FIND ANY ANOMALIES WITH EITHER ENGINE. THEY DID NOTE THERE WAS A SPOT OF APPROXIMATLEY 3 SECONDS WHEN MOVING THE THROTTLES TO TAKE-OFF WHERE THE THROTTLE LEVER ANGLES WERE SLIGHTLY DIFFERENT BUT BOTH ENGINES PARAMETERS WERE MATCHED (N1 AND N2) AND FF WAS SLIGHTLY LAGGING ON THE RIGHT ENGINE BUT ONLY FOR THESE 3 SECONDS. ALL ENGINE PARAMETERS WERE MATCHED THROUGH TAKEOFF AFTER THAT. MAINTENANCE ACCOMPLISHED A BIRD STRIKE INSPECTION AND FOUND NO EVIDENCE OF A BIRD STRIKE. MAINTENANCE ACCOMPLISHED AN ENGINE POWER ASSURANCE CHECK WITH NO SURGES OR POWER LOSS NOTED.

Part: OIL SYSTEM — LEAKING (ENGINE) · airframe 73,480 hrs · 28,211 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT, FLIGHT CREW SHUT DOWN ENGINE #2 DUE TO LOSS OF ENGINE OIL AND PRESSURE.. THE AIRCRAFT LANDED SAFELY AT CLT AND TAXIED TO THE GATE UNDER ITS OWN POWER. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: OIL SYSTEM — LEAKING (NR 2 ENGINE) · airframe 73,480 hrs · 28,211 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT, FLIGHT CREW SHUT DOWN ENGINE #2 DUE TO LOSS OF ENGINE OIL AND PRESSURE.. THE AIRCRAFT LANDED SAFELY AT CLT AND TAXIED TO THE GATE UNDER ITS OWN POWER. **SUPPLEMENTAL REPORT FOR AALA202402145589: MAINTENANCE NOTED THAT THE OIL SCAVENGE FILTER HOUSING INSERTS ARE PULLING OUT AND THE SEAL WAS SHOWING . A REVIEW OF THE DFDR DATA REVEALED THAT THE ENGINE OPERATED BELOW 13 PSI FOR MORE THAN 2 MINUTES REQUIERING THE ENGINE TO BE CHANGED. MAINTENANCE REPLACED ENGINE PER TASK CARD 26L40071001. ** (CLOSED)

Part: BATTERY — FAULTY (EMERGENCY LIGHTS) · airframe 73,372 hrs · 28,162 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT MID RIGHT FAULTED DURING EMERGENCY LIGHTS BUILT IN TEST EQUIPMENT CHECK. REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY (14WL) PER AMM 33-51-38.

Part: BATTERY — FAULTY (EMERGENCY LIGHTS) · airframe 73,372 hrs · 28,162 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT BATTERY MID LEFT FAULTED DURING EMERGENCY LIGHTS BUILT IN TEST EQUIPMENT CHECK. REMOVED AND REPLACED (15WL) EMERGENCY POWER SUPPLY UNIT BATTERY PER AMM 33-51-38.

Part: DAMPER — LOW PRESSURE (DOOR) · airframe 73,297 hrs · 28,126 cycles

AIRCRAFT WAS NOT GROUNDED: CIDS PANEL CAUTION LIGHT ILLUMINATED. RESET DID NOT HELP. ACCOMPLISHED R3 DOOR CHARGING OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER.

Part: WIRE — PINCHED (ZONE 200 - FUSE) · airframe 72,666 hrs · 27,803 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY AISLE LIGHTS AT SEAR ROWS 21 ABC AND 22 ABC ARE INOPERATIVE. MAINTENANCE FOUND WIRE PINCHED UNDER SEAT 21ABC AND REPAIRED IT PER ESPM 20-43-11. A SATISFACTORY OPERATIONAL CHECK OF TEH EMERGENCY LIGHTS AT SEAT ROWS 21 ABC AND 22 ABC AS ACCOMPLISHED.

Part: BOTTLE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 72,393 hrs · 27,659 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR ASSIST BOTTLE LOW. SERVICED DOOR ASSIST BOTTLE PER AMM 52-10-00.

Part: HINGE FITTING — WORN (MLG DOOR) · airframe 72,209 hrs · 27,567 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND MAIN LANDING GEAR DOOR FORWARD HINGE FITTING WORN. REPLACED LANDING GEAR DOOR ASSEMBLY PER AMM 32-12-11.

Part: HINGE FITTING — CRACKED (ZONE 700 - GEARS) · airframe 72,209 hrs · 27,567 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND MAIN LANDING GEAR DOOR FORWARD HINGE FITTING ON THE KEEL BEAM SIDE IS CRACKED. REPLACED HINGE FITTING PER EA 347361.

Part: BATTERY — DISCHARGED (ZONE 200 - FUSE) · airframe 72,073 hrs · 27,495 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHTS FLASHING AT DOORS 4 AND 2. MAINTENANCE REPLACED THE BATTERY FOR EMERGENCY POWER SUPPLY UNIT 13WL (AALA202308033907) AND THE BATTERY FOR EMERGENCY POWER SUPPLY UNIT 15WL (AALA202308036553) PER AMM 33-51-38.

Part: BATTERY — DISCHARGED (ZONE 200 - FUSE) · airframe 72,073 hrs · 27,495 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHTS FLASHING AT DOORS 4 AND 2. MAINTENANCE REPLACED THE BATTERY FOR EMERGENCY POWER SUPPLY UNIT 13WL (AALA202308033907) AND THE BATTERY FOR EMERGENCY POWER SUPPLY UNIT 15WL (AALA202308036553) PER AMM 33-51-38.

Part: BOTTLE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 72,064 hrs · 27,486 cycles

AIRCRAFT WAS NOT GROUNDED: R2 DOOR ASSIST BOTTLE REQUIRES SERVICING. SERVICED DOOR ASSIST BOTTLE PER AMM 52-13-00.

Part: SCREW — MISSING (DOOR SLIDE) · airframe 71,494 hrs · 27,212 cycles

AIRCRAFT WAS GROUNDED: L3 EMERGENCY DOOR SLIDE PACK MISSING SCREW. MAINTENANCE INSTALLED SCREW.

Part: ENGINE — OVERTEMP (ZONE 400 - NAC/P) · airframe 71,495 hrs · 27,214 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO LAS. ON TAKEOFF #1 ENGINE HAD OVER TEMPERATURE INDICATION. THE AIRCRAFT LANDED SAFELY AT LAS WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED TSM 77-00-00-810-849-A EGT 971 21 SECONDS AREA "B". ACCOMPIHSED ENGINE BORESCOPE OF THE HPT BLADES AND STAGE 1 LPT BLADES WITH NO FINDINGS. ENGINE #1 PLACED ON PERFORMANCE WATCH FOR EGT AND DETERIORATION PER ENGIINE MOC.

Part: ENGINE — OVERTEMP (ZONE 400 - NAC/P) · airframe 71,495 hrs · 27,214 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO LAS. ON TAKEOFF #2 ENGINE HAD OVER TEMPERATURE INDICATION. THE AIRCRAFT LANDED SAFELY AT LAS WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED TSM 77-00-00-810-849-A EGT 962 24 SECONDS AREA "A". ENGINE #2 PLACED ON PERFORMANCE WATCH FOR EGT AND DETERIORATION PER ENGIINE MOC.

Part: BATTERY — NO TEST (ZONE 200 - FUSE) · airframe 70,903 hrs · 26,949 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR EMERGENCY POWER SUPPLY UNIT 10WL BATTERY FAULT DURING SYSTEM TEST. REPLACED BATTERY PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: DAMPER — LOW PRESSURE (ZONE 800 - DOORS) · airframe 69,709 hrs · 26,403 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 3R DOOR DAMPER REQUIRES SERVICE. MAINTENANCE SERVICED DOOR 3R DAMPER PER TASK CARD 26L00005005.

Part: PRESSURE SWITCH — NONE (ZONE 100 - FUSE) · airframe 69,489 hrs · 26,313 cycles

AIRCRAFT WAS GROUNDED: AIRCRAFT RETURNED TO CLT AND DECLARED AN EMERGENCY DUE TO A BLUE HYDRAULIC SYSTEM ELECTRIC PUMP LOW PRESSURE ECAM. PUMP INDICATED INOPERATIVE ON THE HYDRAULIC PAGE. THE AIRCRAFT LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE BLUE HYDRAULIC PUMP PRESSURE SWITCH 2074GJ PER AMM 29-12-17.

Part: DOOR — STICKING (ZONE 800 - DOORS) · airframe 68,801 hrs · 26,013 cycles

AIRCRAFT WAS NOT GROUNDED: MID-CABIN LAVATORY DOOR STUCK CLOSED. UNJAMMED MID CABIN LAVATORY DOOR AS REQUIRED.,

Part: COMPUTER — FALSE INDICATION (ZONE 500 - LH WI) · airframe 68,616 hrs · 25,937 cycles

AIRCRAFT WAS GROUNDED: FUEL LEFT WING TANK OVERFLOW ECAM CONTINUOUSLY AFTER TAKEOFF UNTIL CENTER TANK EMPTY. 1 HR 45 MIN INTO FLIGHT CAME ON AGAIN. LEFT WING TANK 8460 RIGHT 8240. REPLACED FUEL QUANTITY INDICATION COMPUTER AND ACCOMPLISHED A SATISFACTORY OPERATION CHECK PER AMM 28-42-34.

Part: HANDLE — BROKEN (ZONE 800 - DOORS) · airframe 68,194 hrs · 25,730 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR ARMING LEVER AT 3R DOOR IS BROKEN. REPLACED HANDLE AS REQUIRED.

Part: FRAME — CRACKED (ZONE 200 - FUSE) · airframe 67,424 hrs · 25,387 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FR 43 BETWEEN S18R AND S24R. REPLACED FRAME PER EA 333011.

Part: CYLINDER — FAULT MESSAGE (ZONE 800 - DOORS) · airframe 67,040 hrs · 25,234 cycles

AIRCRAFT WAS NOT GROUNDED: CABIN INTERCOMMUNICATION DATA SYSTEM CAUTION LIGHT ON, RESET ON GROUND BEFORE LEAVING WITH MAINTENANCE HELP-CAME ON AGAIN SHORTLY AFTER TAKE OFF. SERVICED RIGHT DOOR NUMBER 3 EMERGENCY OPERATION CYLINDER PER AMM 52-10-00, CABIN INTERCOMMUNICATION DATA SYSTEM CAUTION LIGHT CLEARS.

Part: DOOR — STICKING (ZONE 800 - DOORS) · airframe 66,798 hrs · 25,135 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR DIFFICULT TO OPEN. ADJUSTED FLIGHT DECK DOOR PER 52-51-00 OPERATIONS CHECK NORMAL.

Part: HANDLE — INOPERATIVE (ZONE 800 - DOORS) · airframe 66,782 hrs · 25,130 cycles

AIRCRAFT WAS NOT GROUNDED: COCKPIT DOOR HANDLE JAMMED. ADJUSTED AND APPLY LUBRICANT COCKPIT DOOR HANDLE. OPERATIONS CHECK GOOD PER AMM 25-10-00.

Part: SEAL — BLOWN (ZONE 700 - GEARS) · airframe 66,629 hrs · 25,063 cycles

AIRCRAFT WAS GROUNDED: VERY ROUGH TAKE OFF ROLL AFTER TAKE OFF LANDING GEAR SHOCK ABSORBER FAULT ON ECAM. RECYCLED LANDING GEAR WITH SAME SAME RESULT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHL WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NOSE LANDING GEAR STRUT FLAT DUE TO BLOWN SEALS. REPLACED SEALS AND ACCOMPLISHED NOSE LANDING GEAR STRUT REPACK PER TASK CARD 26L71032001.

Part: BRAKE — ABNORMAL (LT MLG) · airframe 66,229 hrs · 24,901 cycles

AIRCRAFT WAS NOT GROUNDED: UPON LANDING, BRAKES ON LEFT SIDE GRABBED AND PULLED AIRCRAFT LEFT. TEMPERATURES ON 1&2 GOT TO 610/585 AND 3&4 STAYED AT 125/120. PULLING INTO GATE MADE A ROUGH STOP AND NOISE FROM LEFT SIDE. JACKED L/H GEAR & SPUN WHEELS, BOTH SPIN FREELY, NO SIGN OF DAMAGE. #2 BRAKE CHANGED YESTERDAY, BLED EXCESSIVE AIR FROM #2 BRAKE LINE PER AMM 32-42-00.

Part: LIGHT — INOPERATIVE (ROW 19C) · airframe 65,556 hrs · 24,612 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT ROW 19C ESCAPE PATH LIGHTING LOOSE / INOPERATIVE. **SUPPLEMENTAL REPORT FOR AALA202105260929: REPLACED LIGHT ASSEMBLY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-19** (CLOSED)

Part: LIGHT — INOPERATIVE (ROW 19C) · airframe 65,556 hrs · 24,612 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT ROW 19C ESCAPE PATH LIGHTING LOOSE / INOPERATIVE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: LIGHT — BROKEN (SEAT 21C) · airframe 65,503 hrs · 24,590 cycles

AIRCRAFT WAS NOT GROUNDED: 21C EMERGENCY EXIT LIGHT BROKE OFF SEAT. REMOVED AND REPLACED ESCAPE PATH LIGHT AT 21C. CHECKS GOOD, OK FOR SERVICE PER AMM 33-51-19.

Part: HINGE FITTING — WORN (LT WING SPOILER) · airframe 65,183 hrs · 24,469 cycles

AIRCRAFT WAS GROUNDED: LEFT WING #4 SPOILER CENTER HINGE FITTING ANTI ROTATIONAL STRUCTURE WORN BEYOND LIMITS AT THE SPOILER SERVO ATTACHMENT POINT. REPAIRED SPOILER CENTER HINGE FITTING PER SRM 57-70-00-300-004.

Part: TAB — DEBONDED (LT WING TE FLAP) · airframe 65,161 hrs · 24,457 cycles

AIRCRAFT WAS GROUNDED: LEFT WING OUT BOARD FLAP TAB IS DEBONDED ON BOTH UPPER AND LOWER SURFACES.. REPAIRED FLAP TAB PER EA 326690.

Part: PUMP — LEAKING (GREEN HYD SYS) · airframe 64,837 hrs · 24,313 cycles

AIRCRAFT WASD GROUNDED: IN CRUISE, LOSS OF GREEN HYDRAULIC QUANTITY. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. REPLACED # 1 ENGINE GREEN HYDRAULIC SYSTEM PUMP AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL PER AMM 29-11-51.

Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 64,645 hrs · 24,233 cycles

AIRCRAFT WAS NOT GROUNDED. CLASS 1 WARNING LAVATORY SMOKE, WENT AWAY AFTER 30 SECONDS. FLIGHT ATTENDANT REPORT RIGHT AFT LAVATORY WARNING CAME ON. NO EVIDENCE OF SMOKE. PERFORMED OPERATIONAL TEST OF LAVATORY SMOKE DETECTION, IAW AMM 26-17-00. OKAY FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 64,562 hrs · 24,193 cycles

AIRCRAFT WAS NOT GROUNDED. AFT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT AS NEEDED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,932 hrs · 23,929 cycles

AIRCRAFT WAS GROUNDED (SHORT TERM STORAGE):: EMERGENCY POWER SUPPLY UNIT 15WL PRESS TO TEST BITE INOPERATIVE. BITE TEST SATISFACTORY FROM PTP PANEL. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT15WL PER AMM 33-51-38. BITE TEST SATISFACTORY IAW AMM 33-51-00.

Part: PIN — OUT OF POSITION (CABIN) · airframe 62,346 hrs · 23,335 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS EMERGENCY LIGHTS ON LOWER PORTION OF BINS AT L2 AND L3 DOOR INOP. ACCOMPLISHED EA 298670. L2 AND L3 EMERGENCY LIGHTS PINNING CORRECTED AND OPS CHECKED GOOD.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 62,346 hrs · 23,334 cycles

AIRCRAFT IN BASE MAINTENANCE: SEAT TRACK WORN AT FR 35 AND +Y1292. REPLACED SEAT TRACK PER SRM 53-21-15-04, 51-72-11 AND EA 298371.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 62,346 hrs · 23,334 cycles

AIRCRAFT IN BASE MAINTENANCE: SEAT TRACK WORN AT FR 59 AND +Y1292. REPAIRED SEAT TRACK PER SRM 53-41-15-300-002.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 62,346 hrs · 23,334 cycles

AIRCRAFT IN BASE MAINTENANCE: SEAT TRACK WORN AT FR 46 AND +Y765. REPLACED SEAT TRACK PER SRM 53-31-15-04A AND 51-72-11.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 62,346 hrs · 23,334 cycles

AIRCRAFT IN BASE MAINTENANCE: SEAT TRACK WORN AT FR 58 AND +Y765. REPLACED SEAT TRACK PER SRM 53-41-15-42A AND 51-72-11.

Part: FLOOR SUPPORT — BROKEN (FUSELAGE) · airframe 62,346 hrs · 23,334 cycles

AIRCRAFT IN BASE MAINTENANCE: BROKEN FLOOR SUPPORT AT FR 34. REPLACED FLOOR SUPPORT PER DRAWING D53112760 003 ISSUE K.

Part: FLOOR SUPPORT — BROKEN (FUSELAGE) · airframe 62,346 hrs · 23,334 cycles

AIRCRAFT IN BASE MAINTENANCE: BROKEN FLOOR SUPPORT AT FR 33. REPLACED FLOOR SUPPORT PER DRAWING D53112760 003 ISSUE K.

Part: TEE FITTING — DAMAGED (HYDRAULIC SYS) · airframe 62,111 hrs · 23,244 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS HYD B SYS LO LEVEL AND HYD B SYS LOW PRESS AT CRUISE ALTITUDE. HYDRAULIC SYSTEM PAGE CONFIRMS LOW QUANITY. TURNED OFF BLUE PUMP AND FOLLOWED ECAM LANDING INSTRUCTIONS FOR APPROACH. MAINTENANCE FOUND DAMAGED TEE FITTING AND FLEX HOSE AT THE RAT ACTUATOR. REMOVED AND REPLACED HIGH PRESSURE HOSE AND TEE FITTING ON TOP OF RAT ACTUATOR IAW AMM 29-22-53. OPS CHECK OK IAW AMM 29-22 00. SERVICED BLUE SYSTEM TO FULL.

Part: FIRE DETECTOR — UNRELIABLE (NR 2 NACELLE) · airframe 61,095 hrs · 22,871 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS RETURNED TO MIA ON ACCOUNT OF RIGHT HAND ENGINE BLEED AIR LEAK. EMERGENCY DECLARED. LANDED OVERWEIGHT WITHOUT INCIDENT. MAINTENANCE REMOVED & REPLACED #2 ENG DETECTOR 1HF2 IAW AMM 36-22-15. OPS TEST GOOD.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 60,964 hrs · 22,821 cycles

AIRCRAFT WAS GROUNDED: AFT CARGO COMPARTMENT FLOOR PANEL 161AF SPONGY. REPLACED FLOOR PANEL PER AMM 53-42-14.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 60,964 hrs · 22,821 cycles

AIRCRAFT WAS GROUNDED: AFT CARGO COMPARTMENT FLOOR PANEL 151LF SPONGY. REPLACED FLOOR PANEL PER AMM 53-42-14.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 60,964 hrs · 22,821 cycles

AIRCRAFT WAS GROUNDED: AFT CARGO COMPARTMENT FLOOR PANEL 151PF SPONGY. REPLACED FLOOR PANEL PER AMM 53-42-14.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 60,960 hrs · 22,819 cycles

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

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 59,815 hrs · 22,351 cycles

R1 DOOR ASSIST BOTTLE HAD LOW PRESSURE. SERVICED THE DOOR ASSIST BOTTLE IAW AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (R3 DOOR ASSIST) · airframe 59,362 hrs · 22,181 cycles

R3 DOOR ASSIST BOTTLE HAD LOW PRESSURE. CHARGED THE BOTTLE IAW AMM 52-22-00 AND PERFORMED LEAK CHECK. CHECK IS OK, NO LEAK FOUND.

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 59,353 hrs · 22,178 cycles

NOSE LANDING GEAR RIGHT AFT DOOR FORWARD HINGE HAS EXCESSIVE PLAY. REPLACED THE DOOR HINGE IAW CMM 52-82-32-400-802, AND 52-82-32-400-805-A001.

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 59,353 hrs · 22,178 cycles

NOSE LANDING GEAR RIGHT AFT DOOR AFT HINGE HAS EXCESSIVE PLAY. REPLACED THE DOOR HINGE IAW CMM 52-82-32-400-802, AND 52-82-32-400-805-A001.

Part: BEARING — MIGRATED (THRUST REVERSER) · airframe 59,353 hrs · 22,178 cycles

RIGHT PYLON, INBOARD THRUST REVERSER MIDDLE ATTACHMENT POINT HINGE FITTING BEARING HAS MIGRATED. REPLACED HINGE FITTING IAW AMM 54-57-17-400-003-A.

Part: BEARING — MIGRATED (THRUST REVERSER) · airframe 59,353 hrs · 22,178 cycles

RIGHT PYLON OUTBOARD THRUST REVERSER AFT ATTACHMENT POINT HINGE FITTING BEARING HAD MIGRATED. REPLACED HINGE FITTING IAW AMM 54-57-17-400-003-A.

Part: HINGE FITTING — EXCESS PLAY (LT MLG DOOR) · airframe 59,353 hrs · 22,178 cycles

LEFT MAIN LANDING GEAR DOOR FORWARD HINGE FITTING BEARING HAD EXCESSIVE PLAY. REPLACED THE HINGE FITTING IAW CMM 52-81-18.

Part: RUB STRIP — DETERIORATED (PAX DOOR) · airframe 59,353 hrs · 22,178 cycles

AIRCRAFT IN BASE MAINTENANCE. DETERIORATED RUBBER STRIP PASSENGER CREW DOOR 831 AND 841 IN PASSENGER CABIN. REPLACED RUBBER STRIP PER AMM 52-11-18-300-002-A.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-67) · corrosion level 2 · airframe 59,353 hrs · 22,178 cycles

CORROSION FOUND ON THE FLOOR SUPPORT BETWEEN FRAMES 66 TO 67 + 15 INCHES, -Y1162.5. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53472780.

Part: FLOOR PANEL — PERFORATED (FWD CARGO BAY) · airframe 59,353 hrs · 22,178 cycles

PERFORATION ON FLOOR PANEL 131XF IN FWD CARGO BAY. REPAIRED FLOOR PANEL IAW SRM 53-02-00-300-004, PARA2A (1) (2) (7) TO (9).

Part: HINGE ARM — EXCESS PLAY (RT ELEVATOR) · airframe 59,353 hrs · 22,178 cycles

RIGHT ELEVATOR NR 6 HINGE ARM HAD EXCESSIVE PLAY. REPLACED THE HINGE ARM IAW AMM 55-11-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (RT ELEVATOR) · airframe 59,353 hrs · 22,178 cycles

RIGHT ELEVATOR NR 4 HINGE ARM HAD EXCESSIVE PLAY. REPLACED THE HINGE ARM IAW AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (RT ELEVATOR) · airframe 59,353 hrs · 22,178 cycles

RIGHT ELEVATOR NR 5 HINGE ARM HAD EXCESSIVE PLAY. REPLACED HINGE ARM IAW AMM 55-16-42-400-001-A.

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 59,353 hrs · 22,178 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR, LEFT HAND AFT DOOR AFT HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER AMM 32-22-13-410-001-A

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 59,353 hrs · 22,178 cycles

NOSE LANDING GEAR, LEFT HAND AFT DOOR FORWARD HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER AMM 32-22-13-410-001-A

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 59,353 hrs · 22,178 cycles

DELAMINATION FOUND ON FLOOR PANEL 221EF, IN THE FORWARD GALLEY. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006.

Part: COVER — CORRODED (FRAMES 12-16) · corrosion level 2 · airframe 59,353 hrs · 22,178 cycles

CORROSION ON JOINT COVER IN THE FORWARD GALLEY AREA LOCATED BETWEEN FRAMES 12 TO 16, -Y81. REPLACED THE JOINT COVER IAW SRM 51-72-11, DWG D53112829, AND D53110984.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 59,353 hrs · 22,178 cycles

CORROSION FOUND ON THE FLOOR SUPPORT BETWEEN FRAMES 12 - 24 IN THE FORWARD GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DRAWINGS D53112812, AND D53110984.

Part: FLOOR PANEL — DELAMINATED (COCKPIT) · airframe 59,353 hrs · 22,178 cycles

DELAMINATION FOUND ON FLOOR PANEL 211EF IN THE COCKPIT. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006.

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 59,353 hrs · 22,178 cycles

DELAMINATION FOUND ON FLOOR PANEL 261AG IN THE AFT GALLEY. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 59,353 hrs · 22,178 cycles

DELAMINATED FLOOR PANEL 221DF, IN THE FORWARD GALLEY. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006.

Part: COUPLING — DAMAGED (FUSELAGE) · airframe 59,353 hrs · 22,178 cycles

AIRCRAFT IN BASE MAINTENANCE. L2 DOOR CUTOUT LOWER SILL OUTBOARD COUPLING AT FR 66 AND S23L HAS ELONGATED HOLE. REPLACED COUPLING PER SRM 51-72-11.

Part: FITTING — CORRODED (FRAMES 16-20) · corrosion level 2 · airframe 59,353 hrs · 22,178 cycles

CORROSION ON THE L1 DOOR SILL CENTER FITTING BETWEEN FRAMES 16 AND 20, STRINGER 23L. REPLACED CENTER FITTING IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 59,353 hrs · 22,178 cycles

CORROSION FOUND ON THE FORWARD GALLEY FLOOR SUPPORT BETWEEN FRAMES 12 AND 24, -Y1292. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, AND 51-72-11.

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 59,353 hrs · 22,178 cycles

DELAMINATION FOUND ON FLOOR PANEL 261BG IN THE AFT GALLEY. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011.

Part: FITTING — CORRODED (FRAMES 16-20) · corrosion level 2 · airframe 59,353 hrs · 22,178 cycles

CORROSION ON FOUND ON THE R1 DOOR LOWER SILL CENTER FITTING BETWEEN FRAMES 16 AND 20, STRINGER 23R. REPLACED CENTER FITTING IAW SWRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 59,353 hrs · 22,178 cycles

DELAMINATION FOUND ON FLOOR PANEL 261PF IN THE AFT GALLEY. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011.

Part: SEAT TRACK — CORRODED (FRAMES 12-16) · corrosion level 2 · airframe 59,353 hrs · 22,178 cycles

CORROSION ON THE SEAT TRACK BETWEEN FRAMES 12 TO 16, IN THE FORWARD GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM A321 51-72-11, AND DRAWING D53112825.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,353 hrs · 22,178 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON L2 DOOR CUTOUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23L. REPLACED SILL PER SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,353 hrs · 22,178 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON L2 DOOR CUT OUT LOWER SILL CENTER SILL SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23L. REPLACED SILL CENTER SILL SHAPE FITTING PER SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (COCKPIT) · airframe 59,353 hrs · 22,178 cycles

DELAMINATION FOUND ON FLOOR PANEL 212EF IN THE COCKPIT. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 59,353 hrs · 22,178 cycles

DELAMINATED FLOOR PANEL 231CF IN THE FORWARD GALLEY. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006.

Part: COUPLING — DAMAGED (FUSELAGE) · airframe 59,353 hrs · 22,178 cycles

AIRCRAFT IN BASE MAINTENANCE. L2 DOOR CUTOUT LOWER SILL INBOARD COUPLING AT FR 66 AND S23L HAS ELONGATED HOLE. REPLACED COUPLING PER SRM 51-72-11.

Part: ANGLE — CRACKED (FRAME 42) · airframe 59,353 hrs · 22,178 cycles

CRACKED VERTICAL ANGLE AT FRAME 42 IN THE RIGHT HYDRAULIC COMPARTMENT. REPLACED THE ANGLE IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (COCKPIT) · airframe 59,353 hrs · 22,178 cycles

DELAMINATED FLOOR PANEL 211FF, IN THE COCKPIT. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 59,353 hrs · 22,178 cycles

DELAMINATED FLOOR PANEL 222EF, IN THE FORWARD GALLEY. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006.

Part: FLOOR SUPPORT — CORRODED (FRAME 67) · corrosion level 2 · airframe 59,353 hrs · 22,178 cycles

CORROSION FOUND ON THE FLOOR SUPPORT, FRAME 67, +Y1162.5. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 59,353 hrs · 22,178 cycles

CORROSION ON THE SEAT TRACK BETWEEN FRAMES 64 TO 66, -Y1292. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING D53472816.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-69) · corrosion level 2 · airframe 59,353 hrs · 22,178 cycles

CORROSION FOUND ON THE FLOOR SUPPORT BETWEEN FRAMES 67 + 15 INCHES TO FRAME 69, +Y1162.5. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53472780.

Part: BUTTSTRAP — CORRODED (FRAMES 26-28) · airframe 59,353 hrs · 22,178 cycles

CORROSION ON FORWARD CARGO DOOR CUTOUT LOWER BUTT STRAP BETWEEN FRAMES 26 AND 28, STRINGER 38R. REPLACED THE BUTT STRAP IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 59,353 hrs · 22,178 cycles

CORRRODED FOUND ON THE FLOOR SUPPORT BETWEEN FRAMES 64 TO 66, -Y765. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53472816.

Part: TRAY — CRACKED (FRAMES 68-69) · airframe 59,353 hrs · 22,178 cycles

CRACKED TRAY BETWEEN FRAMES 68 AND 69, STRINGER 23L. REPLACED THE TRAY IAW SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 59,353 hrs · 22,178 cycles

CORRODED SEAT TRACK, BETWEEN FRAMES 64 TO 66 + 5 INCHES, LBL Y765. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING D53472780.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 59,353 hrs · 22,178 cycles

CORRODED FLOOR SUPPORT BETWEEN FRAMES 64 TO 66 + 5, +Y1292. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53472815.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-69) · corrosion level 2 · airframe 59,353 hrs · 22,178 cycles

CORROSION FOUND ON THE FLOOR SUPPORT BETWEEN FRAMES 67 TO 69, -Y1162.5. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53472780.

Part: FITTING — CRACKED (FRAME 16) · airframe 59,353 hrs · 22,178 cycles

CRACKED INTERCOSTAL FITTING AT THE R1 DOOR CUTOUT, AT FRAME 16, STRINGER 10R. REPLACED THE INTERCOSTAL FITTING IAW SRM 51-72-11.

Part: INTERCOSTAL — CRACKED (FRAME 20) · airframe 59,353 hrs · 22,178 cycles

CRACK INDICATION FOUND ON THE INTERCOSTAL, FRAME 20, STRINGERS 10 - 11. REPLACED THE INTERCOSTAL IAW SRM A321 51-72-11, AND DRAWING D53112331.

Part: FITTING — CRACKED (FUSELAGE) · airframe 59,353 hrs · 22,178 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED INTERCOSTAL FITTING AT FR 16 AND S10L. REPLACED INTERCOSTAL FITTING PER SRM 51-72-11.

Part: FITTING — CRACKED (ZONE 200 - FUSE) · airframe 59,353 hrs · 22,178 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRONT WINDSHIELD FRAME CONTINUITY FITTING AT FR 4 AND S20L. REPLACED FRONT WINDSHIELD FRAME CONTINUITY FITTING PER EA 284805.

Part: FITTING — CRACKED (WINDSHIELD) · airframe 59,353 hrs · 22,178 cycles

CRACKED FRONT WINDSHIELD FRAME FITTING AT FRAME 4, STRINGER 20R. REPLACED THE FITTING IAW EA 284805.

Part: COVER — LOOSE (R4 DOOR SLIDE) · airframe 59,353 hrs · 22,178 cycles

R4 DOOR SLIDE COVER LOOSE. MAINTENANCE INSTALLED THE SLIDE COVER IAW AMM 25-62-50, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 58,465 hrs · 21,861 cycles

AIRCRAFT WAS GROUNDED. LEFT MID EMERGENCY POWER SUPPLY UNIT INOPERABLE, DURING CIDS OPERATIONAL CHECK, TASK 33-51-00-710-001. MAINTENANCE REPLACED LEFT MID EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 58,465 hrs · 21,861 cycles

AIRCRAFT WAS GROUNDED: LEFT 2 MID EMERGENCY POWER SUPPLY UNIT INOPERABLE, DURING CIDS OPERATIONAL CHECK, TASK 33-51-00-710-001. MAINTENANCE REPLACED LEFT 2 MID EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 58,368 hrs · 21,821 cycles

R3 FLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT IAW AMM 25-65-00.

Part: FAN — INOPERATIVE (ZONE 200) · airframe 57,601 hrs · 21,533 cycles

AIRCRAFT WAS NOT GROUNDED. DUE TO CABIN ELECTRICAL ODOR. CABIN ODOR TROUBLESHOOTING CARD 26L0021001 WAS OPENED. ACCOMPLISHED CABIN ODOR TROUBLESHOOTING CARD 26L0021001. ODOR AND NOISE ISOLATED TO AVEC EXTRACT FAN. REPLACED AVIONICS FAN PER AMM 21-26-51.

Part: WARNING MESSAGE — FALSE ACTIVATION (BRAKES) · airframe 57,314 hrs · 21,424 cycles

AUTO BRAKE FAULT, BRAKE RELEASED ECAM MASSAGE ANNUNCIATED DURING CLIMB AFTER 1500FT. FOLLOWED ECAM PROCEDURE, NO CHANGE. ACCOMPLISHED A BITE CHECK OF BOTH BRAKING AND STEERING CONTROLS NR 1 & 2 IAW AMM 32-46-00. NO FAULTS NOTED. OPS CHECKED NORMAL IAW AMM 32-42-00. UNABLE TO DUPLICATE FAULT. NO HISTORY 30 DAYS. ACFT OK FOR SERVICE.

Part: DOOR — OBSTRUCTED (R1) · airframe 57,085 hrs · 21,336 cycles

R1 DOOR SLIDE DOES NOT ARM. REMOVED DEBRIS FROM R1 DOOR SILL. DOOR ARMS NORMAL.

Part: BUSTLE — LOOSE (R4 DOOR SLIDE) · airframe 56,810 hrs · 21,231 cycles

AIRCRAFT WAS NOT GROUNDED: LOOSE SLIDE BUSTLE AT DOOR 4R. MAINTENANCE SECURED 4R SLIDE COVER AND PERFORMED SATISFACTORY CHECK.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 56,745 hrs · 21,203 cycles

AIRCRAFT WAS NOT GROUNDED. BOTH FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHTS ARE DEAD. REMOVED AND REPLACED LEFT FORWARD FLASHLIGHT (AALA201711279032) AND RIGHT FORWARD FLASHLIGHT. OPERATIONAL CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 56,745 hrs · 21,203 cycles

AIRCRAFT WAS NOT GROUNDED. BOTH FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHTS ARE DEAD. REMOVED AND REPLACED LEFT FORWARD FLASHLIGHT AND RIGHT FORWARD FLASHLIGHT (AALA201711289036). OPERATIONAL CHECK GOOD.

Part: LENS — MISSING (CABIN) · airframe 56,462 hrs · 21,103 cycles

EMERGENCY EXIT LIGHT AT 2L IS BROKEN AND MISSING BULB. EMERGENCY EXIT LIGHT AT 2L REPLACED IAW AMM.

Part: PROXIMITY SENSOR — FAULTY (MLG)

JUST AFTER TAKEOFF, UNABLE TO MOVE LANDING GEAR HANDLE TO UP POSITION. A FEW MINUTES LATER, ECAM CLASS 1 FAULT L/G SHOCK ABSORBER FAULT, 2 MINUTE LATER FAULT CLEARED AND WERE ABLE TO RETRACT GEAR. FOUND FAULTY PROXMITY SENSOR, REPLACED THE PROXIMITY SENSOR IAW AMM.

Part: PROXIMITY SENSOR — FAULTY (MLG) · airframe 56,013 hrs · 20,915 cycles

UNABLE TO RETRACT GEAR ON INITIAL GEAR UP SELECTION. FEW MINUTES LATER, ECAM CLASS 1 FAULT MLG SHOCK ABSORBER FAULT, TWO MINUTES LATER, FAULT CLEARED AND WERE ABLE TO RETRACT GEAR. REPLACED PROXIMITY SENSOR IAW AMM. OPS CHECKED GOOD.

Part: SHOCK ABSORBER — LOW PRESSURE (MLG) · airframe 56,010 hrs · 20,913 cycles

AFTER LIFT OFF, UNABLE TO RETRACT LANDING GEAR. ECAM L/G SHOCK ABSORBER FAULT. AFTER ABOUT 30 SEC, HEARD A LOUD BANG. ECAM CLEARED AND WAS ABLE TO RETRACT GEAR. ACCOMPLISHED TSM 32-31-00-810-876 AND TSM 32-31-00-810-868 AND SERVICED NLG . ACCOMPLISHED FUNCTIONAL TEST OF NLG IAW 32-31-00, OPS CHECKED GOOD.

Part: STRUT — INCORRECT (NLG) · airframe 56,009 hrs · 20,912 cycles

LANDING GEAR SHOCK ABSORBER FAULT MESSAGE AFTER TAKEOFF. COULDN'T RAISE GEAR LEVER. AFTER 30 SECONDS GEAR CAME UP NORMALLY. FOUND NLG INCORRECT SERVICE. SERVICE TO CORRECT HEIGHT IAW AMM.

Part: TACHOMETER — FAULTY (AUTOBRAKE) · airframe 55,750 hrs · 20,817 cycles

ECAM RIGHT AFTER TAKEOFF "BRAKES AUTO BRK FAULT BRAKE RELEASED (AFTER TAXI IN TO GATE-BRAKE TEMP 1: 580 2:50. TROUBLESHOT AUTO BRAKE SYS AND FOUND THE NR 2 TACH, AUTOBRAKE FAULTY. REPLACED NR 2 WHEEL AUTOBRAKE TACH IAW AMM 32-42-57-400-001-A.

Part: SLIDE — DEFORMED (R1 DOOR) · airframe 55,706 hrs · 20,803 cycles

R1 DOOR HANDLE CREEPS OUT OF ARMED POSITION. ECAM PAGE SHOWS SLIDE DISARMED. MAINTENANCE FOUND SPRING BACK OF ARMING HANDLE CAUSED BY DEFORMED FABRIC AT GIRT BAR ATTACH POINTS. REPLACED ESCAPE SLIDE IAW JOB CARD 26L00025010. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS GROUNDED.

Part: PIN — CORRODED (RT MLG) · airframe 55,704 hrs · 20,802 cycles

CORROSION ON RIGHT MAIN LANDING GEAR REAR PINTLE PIN. REPLACED THE PINTLE PIN IAW TASK CARD 26T00032001.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 55,278 hrs · 20,653 cycles

EMERGENCY LIGHT LENS MISSING 1C. INSTALLED A NEW LENS.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 54,769 hrs · 20,457 cycles

AIRCRAFT NOT GROUNDED. EMERGENCY BATTERY POWER SUPPLY UNIT NR 2L INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY NR 2.

Part: LENS — DETACHED (EMERGENCY LIGHTS) · airframe 54,567 hrs · 20,376 cycles

EMERGENCY EXIT LIGHT COVER AT THE L4 DOOR FELL OFF. REPLACED EMERGENCY EXIT LIGHT LENS.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 54,555 hrs · 20,372 cycles

AIRCRAFT NOT GROUNDED. LENS COVER FOR EMERGENCY EXIT LIGHT FELL OFF LENS ON CENTER PEDESTAL IN COCKPIT. INSTALLED LENS COVER FOR EMERGENCY EXIT SIGN AT AFT RIGHT EXIT DOOR.

Part: MECHANISM — LACK OF LUBE (L4 DOOR ARMING) · airframe 54,364 hrs · 20,301 cycles

FLIGHT ATTENDANT REPORTED THE L4 DOOR IS HARD TO DISARM, AND HARD TO MOVE LEVER. LUBRICATED THE L4 DOOR DISARM MECHANISM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 54,114 hrs · 20,212 cycles

MISSING EMERGENCY LIGHT LENS COVER AT ROW 22R. REPLACED THE LENS IAW AMM 33-51-18.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 53,956 hrs · 20,143 cycles

FLIGHT CREW REPORTED THAT WHILE ENROUTE THE CIRCUIT BREAKER FOR THE HYDRAULIC B ELECTRIC PUMP TRIPPED AND ECAM MESSAGES FOR HYD B ELECTRIC PUMP PRESSURE LOW AND HYD B SYSTEM LOW PRESSURE. DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE BLUE SYSTEM HYDRAULIC ELECTRIC PUMP ASSEMBLY AND ACCOMPLISHED A SATISFACTORY LEAK AND OPERATIONAL CHECK PER AMM 29-12-51.

Part: SWITCH — NO TEST (EMERGENCY LIGHTS) · airframe 53,911 hrs · 20,125 cycles

EMERGENCY EXIT LIGHTS STAY ILLUMINATED WITH OVERHEAD SWITCH SELECTED OFF. REPLACED EMERGENCY EXIT LIGHT ARMING SWITCH IAW ESPM 20-45-21.

Part: STRAP — OUT OF POSITION (L1 DOOR SLIDE) · airframe 53,812 hrs · 20,087 cycles

L1 DOOR DIFFICULT TO ARM, STRAP HANGING IN FRONT OF GIRT BAR. REPOSITIONED STRAP IAW AMM 52-70-00.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 53,651 hrs · 20,029 cycles

SEAT EMERGENCY LIGHT AT 22R INOPERATIVE DUE TO BROKEN WIRES AT SIDEWALL CONNECTOR ON EMERGENCY LIGHT AT SEAT 22R. REPAIRED WIRES PER ESPM 20-44-19 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (CABIN) · airframe 52,820 hrs · 19,694 cycles

AIRCRAFT WAS NOT GROUNDED. R1 DOOR EMERGENCY ESCAPE PATH COVER LENS MISSING. INSTALLED LENS IAW AMM 33-51-13.

Part: UNKNOWN — ODOR (CABIN) · airframe 52,412 hrs · 19,541 cycles

AT THE GATE, THE FLGHT CREW REPORTED A VERY STRONG OIL ODOR THROUGHOUT THE ACFT WITH THE APU BLEED ON, ACFT WAS ON THE GROUND WITH NO EXTERNAL AIR, AND ENGINES SHUTDOWN. THE ODOR DISSIPATED SOME WHEN THEY TURNED THE APU BLEED OFF. MAINTENANCE SUSPECTS THE APU TO BE THE SOURCE OF THE ODOR. AIRCRAFT WAS GROUNDED. MAINTENANCE INSPECTED APU COMPARTMENT FOR CONTAMINATION & LEAKS, NONE FOUND, OIL LEVEL GOOD. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 52,351 hrs · 19,518 cycles

AFT CARGO ENTRY FLOOR PANEL 151GF SUSPECT DELAMINATION. AIRCRAFT WAS GROUNDED. REPLACED FLOOR PANEL IAW AMM 53-42-17.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 52,351 hrs · 19,518 cycles

AFT CARGO FLOOR PANEL 151MK SUSPECT DELAMINATION. AIRCRAFT WAS GROUNDED. REPLACED AFT CARGO FLOOR PANEL IAW AMM 53-42-17.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 52,347 hrs · 19,516 cycles

AFT CARGO FLOOR PANEL 151PF DELAMINATED. AIRCRAFT WAS GROUNDED. REPLACED FLOOR PANEL IAW AMM 53-42-14.

Part: FLOOR PANEL — DELAMINATED (FORWARD CARGO) · airframe 52,347 hrs · 19,516 cycles

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

Part: LENS — MISSING (CABIN) · airframe 52,139 hrs · 19,440 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY AISLE LIGHT LENS IS MISSING AT SEAT ROW 23L. INSTALLED MISSING EMERGENCY LIGHT LENS AT SEAT ROW 23L.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 51,700 hrs · 19,270 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHTS AT LR3 DOOR WILL NOT TEST. REPLACED EMER POWER SUPPLY & BATTERY IAW AMM 33-51-38. SEE AALA 201605099005 FOR ADDITIONAL PART INFORMATION.

Part: SLIDE — DEFECTIVE (L1 DOOR) · airframe 51,700 hrs · 19,270 cycles

AIRCRAFT WAS NOT GNDED. EXTERNAL LOAD FWD EXTERNAL LOAD, FWD LT FAULT DURING EMER LIGHT TEST. REPLACED L1 DOOR SLIDE IAW TASK CARD 26L00025010.

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,700 hrs · 19,270 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHTS AT LR3 DOOR WILL NOT TEST. REPLACED EMER POWER SUPPLY & BATTERY IAW AMM 33-51-38. SEE AALA 201605089004 FOR ADDITIONAL PART INFORMATION.

Part: O-RING — LEAKING (APU) · airframe 51,657 hrs · 19,250 cycles

AIRCRAFT WAS GNDED. CABIN ODOR COMING FROM PACK SYS. ODOR WAS SEVERE & TOXIC NATURE. FOUND AN OIL LEAK AT THE APU STARTER & REPLACED THE O RINGS ON THE STARTER & STARTER ADAPTER IAW AMM 49-42-51. A SATISFACTORY LEAK & OPERATIONAL CHECK WAS ACCOMPLISHED. NO ADDITIONAL ODORS WERE NOTED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 51,338 hrs · 19,115 cycles

AIRCRAFT WAS NOT GNDED. AFT LT EMER FLASHLIGHT NO FLASHING INDICATION. REPLACED FLASHLIGHT BATTERY.

Part: POWER SUPPLY — FAULTED (CABIN) · airframe 51,094 hrs · 19,017 cycles

AIRCRAFT WAS IN BASE MX. RT CTR EMER POWER SUPPLY UNIT 12WL FAULTED. R & R EMER POWER SUPPLY UNIT, 12WL, IAW AMM 33-51-38-401. PERFORMED OPERATIONAL TEST IAW AMM 33-51-00-710-001A, TEST IS GOOD.

Part: LENS — MISSING (CABIN) · airframe 51,090 hrs · 19,016 cycles

AIRCRAFT IN BASE MX. EMER EXIT LIGHT ABOVE DOOR 3R INSTALLED BACKWARD & LENS MISSING. INSTALLED NEW LENS & CORRECTLY POSITIONED LIGHT AT 3R DOOR IAW AMM 33-51-16-400-001-A.

Part: LENS — MISSING (CABIN) · airframe 51,090 hrs · 19,016 cycles

AIRCRAFT IN BASE MX. EMER EXIT LIGHT ABOVE DOOR 2R INSTALLED BACKWARD & LENS MISSING. INSTALLED NEW LENS & CORRECTLY POSITIONED LIGHT AT 2R DOOR IAW AMM 33-51-16-400-001-A.

Part: LIGHT — MISINSTALLED (CABIN) · airframe 51,090 hrs · 19,016 cycles

AIRCRAFT IN BASE MX. EMER EXIT LIGHT SEAT 3C UPSIDE DOWN. INSTALLED CORRECTLY EMER LIGHT SEAT 3C IN PAX CABIN IAW AMM 33-51-19-400-001-A.

Part: POWER SUPPLY — DEFECTIVE (EMERGENCY LIGHTS) · airframe 51,090 hrs · 19,016 cycles

EMERGENCY EXIT LIGHT ABOVE L3 DOOR INOPERATIVE. DETERMINED POWER SUPPLY UNIT 11WL TO BE DEFECTIVE. REPLACED POWER SUPPLY UNIT 11WL & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW 33-51-00-710-001A.

Part: LIGHT — MISINSTALLED (SEAT 3C)

EMERGENCY LIGHT AT SEAT 3C UPSIDE DOWN IN PAX CABIN. INSTALLED CORRECTLY IAW AMM 33-51-19-400-001-A.

Part: SKIN — SATURATED (RUDDER) · airframe 51,089 hrs · 19,015 cycles

AIRCRAFT IN BASE MX. RUDDER HAS EVIDENCE OF TRAPPED WATER ON THE RT SIDE AT THE TE NEAR THE FASTENERS IN TWO LOCATIONS, BETWEEN RUDDER STATIONS 120 & 163 & BETWEEN 249 & 389. RUDDER WAS REPAIRED IAW EA 258302.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 51,089 hrs · 19,015 cycles

AIRCRAFT IN BASE MX. RT SIDE BOX BEAM FLANGE, HAS CRACK INDICATIONS, AT FRAME 43 & -Y1650. REPAIRED IAW EO 5315Y066.

Part: PLATE — CRACKED (FUSELAGE) · airframe 51,089 hrs · 19,015 cycles

AIRCRAFT IN BASE MX. RT PRESS PLATE CRACKED AT FRAME 43 & -Y1650. REPLACED PRESS PLATE IAW SRM 51-72-11 & EO 5315Y066.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 51,089 hrs · 19,015 cycles

AIRCRAFT IN BASE MX. LT SIDE BOX BEAM FLANGE, HAS CRACK INDICATION AT FRAME 43 & Y1650. REPAIRED BOX BEAM IAW EO 5315Y066.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 51,089 hrs · 19,015 cycles

AIRCRAFT IN BASE MX. CRACK INDICATIONS ON DOOR STOP FITTING, SECTION FRAME, HOLES AT FRAME 68 & STRINGER 10L. REPAIRED IAW SRM A321 53-41-12 PB 201 PARAGRAPH 5 E FIGURE 2.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 51,089 hrs · 19,015 cycles

AIRCRAFT IN BASE MX. RT SIDE BOX BEAM FLANGE, HAS CRACK INDICATION IN 2 HOLES AT FRAME 43 & -Y1650. REPAIRED BOX BEAM IAW EO 5315Y066.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 51,089 hrs · 19,015 cycles

AIRCRAFT IN BASE MX. LT SIDE BOX BEAM FLANGE, HAS 2 HOLES WITH CRACK INDICATION AT FRAME 43 & Y1650. REPAIRED BOX BEAM IAW EO 5315Y066.

Part: CASE — CRACKED (CABIN) · airframe 50,450 hrs · 18,762 cycles

SEAT 9D EMER PATH LIGHTING CASE CRACKED. REPLACED CASING & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW CMM 25-28-72.

Part: DOOR — OBSTRUCTED (CABIN) · airframe 49,827 hrs · 18,520 cycles

DOOR 4L ARMING LEVER VERY DIFFICULT TO ARM & DISARM. REMOVED DEBRIS FROM 4L DOOR THRESHOLD AREA.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 49,390 hrs · 18,334 cycles

AFT FLIGHT ATTENDANT FLASHLIGHT NOT FLASHING. REPLACED BATTERY IN THE FLASHLIGHT.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 48,386 hrs · 17,930 cycles

EMERGENCY EXIT LIGHT COVER AT SEAT 9D MISSING. INSTALLED EMERGENCY EXIT LIGHT COVER AT SEAT 9D.

Part: BATTERY — DISCHARGED (CABIN) · airframe 48,123 hrs · 17,824 cycles

EMERGENCY LIGHT TEST FAILED WITH EPSU INTERNAL & EXTERNAL LOAD FAULTS. INSTALLED NEW BATTERY & UPDATED LOAD PROGRAMMING IAW AMM 33-51-38-400-002A. GOOD OPERATIONAL CHECK.

Part: EPSU — FAULTY (CABIN) · airframe 48,123 hrs · 17,824 cycles

EMERGENCY LIGHT TEST FAILED WITH EPSU INTERNAL & EXTERNAL LOAD FAULTS. REPLACED EPSU IAW AMM 33-51-38-400-001-A.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 48,123 hrs · 17,824 cycles

EMERGENCY POWER SUPPLY UNIT 13WL HAS FAULT. REPLACED EPSU IAW AMM 33-51-38-400-001A. GOOD OPERATIONAL TEST.

Part: WIRE — CHAFED (CABIN) · airframe 48,123 hrs · 17,824 cycles

EMERGENCY LIGHT TEST FAILED WITH EPSU INTERNAL & EXTERNAL LOAD FAULTS. FOUND EMER IDENTIFIER AT ROW 8L WITH A LOOSE CONNECTION & CHAFED WIRE. REPAIRED WIRE IAW AMM CHAPTER 20. GOOD OPERATIONAL CHECK.

Part: LENS — MISSING (CABIN) · airframe 48,002 hrs · 17,771 cycles

SEAT MOUNTED EMER LIGHT LENS MISSING AT ROW 8L. INSTALLED SEAT MOUNTED EMER LIGHT LENS AT ROW 8L IAW AMM 33-51-13-0401.

Part: LENS — MISSING (CABIN) · airframe 47,500 hrs · 17,572 cycles

EMERGENCY LIGHT LENS MISSING. REPLACED EMER LIGHT LENS.

Part: LENS — MISSING (CABIN) · airframe 47,269 hrs · 17,480 cycles

EMERGENCY EXIT AISLE LIGHTING LENS MISSING AT SEAT ROW 3AB. REPLACED SEAT 3AB EMER LIGHTING LENS.

Part: BATTERY — DISCHARGED (CABIN) · airframe 46,963 hrs · 17,345 cycles

EMER LIGHT FAULT. FOUND EPSU INT LOAD EXIT LT & EPSU INT LOAD FWD LT FAULT ON EMER LIGHT TEST. REPLACED BATTERIES FOR BOTH EPSU IAW AMM 33-51-38-000-001-A. EMER LIGHT TESTED OK.

Part: LENS — MISSING (CABIN) · airframe 46,950 hrs · 17,339 cycles

ROW 22D EXIT LIGHT LENS MISSING & BROKEN. REPLACED ROW 22D EXIT LIGHT LENS AS REQUIRED.

Part: COVER — BROKEN (CABIN) · airframe 46,326 hrs · 17,113 cycles

SEAT 3C EMER EXIT LIGHT COVER 3C IS BROKEN. REPLACED SEAT 3C EMER EXIT LIGHT COVER.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 45,807 hrs · 16,925 cycles

AN EPSU MID RT FAULT FIN 14WL. R & R EPSU 14WL IAW AMM 33-51-38-0401.

Part: LENS — MISSING (CABIN) · airframe 45,752 hrs · 16,905 cycles

THE EMER AISLE LIGHT LENS IS MISSING AT ROW 3L. INSTALLED NEW EMER AISLE LIGHT LENS AT ROW 3L.

Part: TERMINAL — MISSING (CABIN) · airframe 44,949 hrs · 16,566 cycles

MAINTENANCE FOUND EMERGENCY LIGHT AT 37WL 3L DOOR INOPERATIVE. FOUND WIRE MISSING TERMINAL TO LIGHT HOUSING. REPLACED EMERGENCY LIGHT AT 37WL 3L DOOR TERMINAL END & HOUSING IAW ESPM 20-48-14 & WDM 33-51-02-W-030019-AB. OPERATIONS CHECKED GOOD, ACFT OK FOR SERVICE.

Part: COVER — UNSECURE (CABIN) · airframe 44,839 hrs · 16,520 cycles

CREW REPORTED THE PLASTIC COVER CAME OFF OF EMERGENCY EXIT LIGHT, ROW 3. REPLACED COVER, OPERATIONS OK IAW MPPM 54-01-10.

Part: BATTERY — INOPERATIVE (MEGAPHONE) · airframe 43,365 hrs · 15,848 cycles

FORWARD MEGAPHONE INOPERATIVE. REPLACED BATTERIES IN FWD MEGAPHONE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,250 hrs · 15,794 cycles

EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY IAW AMM 33-51-38-400-001A.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 43,101 hrs · 15,723 cycles

EMERGENCY EXIT LIGHT COVER AT SEAT 8C DETACHED. RESECURED EMERGENCY EXIT LIGHT COVER.

Part: LENS — MISSING (CABIN) · airframe 42,631 hrs · 15,502 cycles

EMERGENCY LIGHT LENS COVER AT FLOOR LIGHT SEAT 3C MISSING. REPLACED LENS COVER AT SEAT 3C.

Part: SLIDE — LOW PRESSURE (L4 DOOR) · airframe 40,854 hrs · 14,761 cycles

L4 DOOR SLIDE PRESSURE LOW. MAINTENANCE REMOVED AND REPLACED L4 DOOR SLIDE.

Part: CYLINDER — LOW PRESSURE (DOOR) · airframe 40,697 hrs · 14,698 cycles

CIDS CAUTION LIGHT ON FLIGHT ATTENDANT PANEL DOOR PRESSURE LOW MID RIGHT. SERVICED MID RIGHT DOOR DAMPER EMERGENCY OPERATION CYLINDER IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614-002A.

Part: RESERVOIR — LOW PRESSURE (EVAC SLIDE) · airframe 40,697 hrs · 14,698 cycles

CIDS CAUTION 'SLIDE PRESS LOW MID LEFT'. REMOVED AND REPLACED L2 SLIDE BOTTLE IAW AIRBUS MAINTENANCE MANUAL 25-62-49.

Part: LENS — CRACKED (CABIN) · airframe 40,546 hrs · 14,624 cycles

EMERGENCY LIGHT LENS COVER CRACKED ROW 9D. REMOVED AND REPLACED EMERGENCY LIGHT LENS COVER ROW 9D.

Part: PROXIMITY SWITCH — FAULTY (R4 DOOR) · airframe 40,521 hrs · 14,611 cycles

ON GROUND DOOR 4R SLIDE ARMED. IN-FLIGHT AT ALTITUDE 4R DOOR SLIDE NOT ARMED. REPLACED DOOR 4R PROXIMITY SWITCH IAW AIRBUS MAINTENANCE MANUAL 52-71-11-000-001A.

Part: CONNECTOR — UNSECURE (NLG) · airframe 40,505 hrs · 14,605 cycles

ECAM MESSAGE "WHEEL, N/W STEER FAULT" ON APPROACH AFTER GEAR WAS SELECTED DOWN. CREW FOLLOWED ECAM PROCEDURES, CONTACTED MOC AND CYCLED NOSE WHEEL STEERING SWITCH AS INSTRUCTED WITH NO SUCCESS. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS TOWED TO HANGAR. UPON VISUAL INSPECTION OF NOSE WHEEL STEERING 4GC, FOUND ELECTRICAL CONNECTOR 4GCA OFF OF RVDT (ROTARY VARIABLE DIFFERENTIAL TRANSDUCER). RE-INSTALLED CONNECTOR - LOCKING FUNCTIONS CHECKED OK, BUT REMOVED AND REPLACED 4GCA CONNECTOR FOR PRECAUTIONARY PURPOSES. ACCOMPLISHED OPERATIONAL TEST OF NOSE WHEEL STEERING SYSTEM IAW AIRBUS MAINTENANCE MANUAL 32-51-00-710-001-A.

Part: LENS — BROKEN (CABIN) · airframe 40,502 hrs · 14,603 cycles

S2 CHECK - L3 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. INSTALLED NEW L3 DOOR EMERGENCY LIGHT LENS IAW A321 AMM 33-51-11.

Part: SIGN — INOPERATIVE (CABIN) · airframe 40,502 hrs · 14,603 cycles

S2 CHECK - AFT CABIN R4 DOOR WALL MOUNTED LOWER EXIT MARKER INOP. REMOVED RIGHT AFT DOOR SURROUND PANEL TO ACCESS WIRES FOR EMERGENCY LIGHT EXIT MARKER. INSTALLED & OPERATIONAL CHECKED EMERGENCY LIGHT EXIT MARKER IAW A321 AMM 33-51-1-400-001A. CHECKS GOOD INSTALLED RIGHT AFT DOOR SURROUND PANEL IAW A321AMM 25-23-45-400-005A.

Part: LENS — BROKEN (CABIN) · airframe 40,502 hrs · 14,603 cycles

S2 CHECK - IN SEAT EMERGENCY EXIT LIGHT LENS ON SEAT 14ABC & 16 ABC BROKEN. REPLACED BROKEN IN SEAT EMERGENCY LIGHT LENS ON SEAT 14ABC & 16ABC IAW A321 AMM 33-51-19.

Part: LENS — BROKEN (CABIN) · airframe 40,502 hrs · 14,603 cycles

S2 CHECK - L4 DOOR LWR EMERGENCY EXIT MARKER LENS BROKEN. REPLACED L4 DOOR LWR EMERGENCY EXIT MARKER LENS IAW A321 AMM 33-51-13 -400-001-A.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 40,502 hrs · 14,603 cycles

S2 CHECK - EMERGENCY LIGHTS ON RIGHT SEATS 8 & 9 INOP. REPLACED EMERGENCY POWER SUPPLY UNIT (ESPU)14WL IAW A321 AMM 33-51-00, OPS CHECK GOOD.

Part: MECHANISM — DIRTY (EMERGENCY EXIT) · airframe 40,502 hrs · 14,603 cycles

2S CHECK - LEFT AFT EMERGENCY EXIT FAILED OPS TEST OF DOOR UNLOCKING IN ARMIED POSITION (BELLCRANK LEVER DID NOT MOVE REARWARD). CLEANED AND LUBRICATED DOOR SLIDE RELEASE MECHANISM. PERFORMED FUNCTIONAL CHECK IAW AMM 52-22-00-720-001-A. CHECKED SATISFACTORY.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 40,502 hrs · 14,603 cycles

C11 CHECK - CRACK ON FLOOR PANEL 251TF BETWEEN FR57 TO FR62, -Y254. REPAIRED FLOOR PANEL 251TF IAW A321 SRM 53-02-00.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,502 hrs · 14,603 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT AFT DOOR SILL UPPER SURFACE AT FR66, Y1427. REPAIRED LEFT AFT DOOR SILL AT FR66, Y1427 IAW A321 SRM 53-41-14 FIG 101 & FIG 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,502 hrs · 14,603 cycles

2S CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT RAIL ASSEMBLY AT FR66, Y1292. REPLACED SEAT RAIL ASSEMBLY AT FR66, Y1292 IAW A321 53-00-14 FIG 102 & 51-42-11.

Part: PANEL — CORRODED (LT WING) · airframe 40,502 hrs · 14,603 cycles

2S CHECK - CORROSION ON WING PANEL 413CL BETWEEN WS 5369 TO WS 6077 & BETWEEN WING RIB 7 TO RIB 8. REPAIRED WING PANEL 413CL IAW A312 SRM 54-52-11 FIG 203.

Part: UNKNOWN — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 40,399 hrs · 14,564 cycles

EMERGENCY LIGHTS ALONG SEAT BOTTOM WILL NOT EXTINGUISH. POWERED DOWN AIRCRAFT AND POWERED BACK UP, EMERGENCY LIGHTS FUNCTION NORMALLY.

Part: SWITCH — MALFUNCTIONED (CABIN) · airframe 40,310 hrs · 14,530 cycles

EMERGENCY LIGHTS ON WITH COCKPIT SWITCH IN ARM POSITION. CYCLED EMERGENCY LIGHT SWITCH ON FLIGHT ATTENDANT PANEL - OPERATIONAL CHECK WAS GOOD.

Part: EPSU — FAULTY (CABIN) · airframe 39,935 hrs · 14,388 cycles

RIGHT FORWARD EMERGENCY POWER SUPPLY UNIT IS FAULTING. REPLACED EPSU - OPERATIONAL CHECK GOOD IAW AIRBUS MAINTENANCE MANUAL 33-51-39.

Part: UNKNOWN — ODOR (ZONE 100) · airframe 39,846 hrs · 14,347 cycles

STRONG DIRTY SOCK ODOR ON TAKEOFF FROM ORD WHICH DISSIPATED SHORTLY AFTER TAKEOFF BUT RETURNED AGAIN ON DESCENT. MAINTENANCE REMOVED AND REPLACED THE APU AND PERFORMED ECS DECONTAMINATION. VENDOR REPORT FROM HONEYWELL INDICATED NO EVIDENCE OF OIL LEAK. DRAIN MAST AND LOAD COMPRESSOR SEAL HAD NO SIGNS OF LEAKAGE. CONFIRMED BY US AIRWAYS ENGINEER. APU WAS RETURNED TO SERVICE AND INSTALLED ON ANOTHER AIRCRAFT. NO SUBSEQUENT CABIN ODOR REPORTS ON EITHER AIRCRAFT.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 39,797 hrs · 14,329 cycles

AFT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT BATTERY.

Part: SLIDE — LOW PRESSURE (SERVICE DOOR) · airframe 39,308 hrs · 14,140 cycles

AFT RIGHT SERVICE DOOR ESCAPE SLIDE PRESSURE LOW. REMOVED AND REPLACED AFT RIGHT SERVICE DOOR ESCAPE SLIDE PER J/C 26L00025010. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 39,230 hrs · 14,112 cycles

EMERGENCY LIGHTS NEAR L2/R2 DOORS WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 14WL AND INSTALLED NEW BATTERY PACK IAW AIRBUS MAINTENANCE MANUAL 33-51-38-000-002-A.

Part: COOLING FAN — LEAKING (APU) · airframe 39,178 hrs · 14,090 cycles

CREW REPORTED AN OILY SMELL IN CABIN AT GATE WITH APU BLEED ON. FOUND OIL LEAK ON APU COOLING FAN. REPLACED COOLING FAN. ALSO REPLACED ALL PACK COMPONENTS DUE TO CONTAMINATION, PERFORMED APU WASH AND DECONTAMINATION.

Part: UNKNOWN — ODOR (CABIN) · airframe 38,997 hrs · 14,028 cycles

OILY, MUSTY ODOR NOTED WITH APU BLEED TURNED ON. ODOR DISSIPATED WHEN APU BLEED WAS TURNED OFF. MAINTENANCE REMOVED AND REPLACED THE APU AND PERFORMED ECS DECONTAMINATION. APU SHOWED SIGNS OF INGESTION BUT REMOVAL REASON WAS NOT CONFIRMED AND AIRCRAFT CONTINUED TO HAVE REPORTS OF DIRTY, MUSTY ODORS. HEPA FILTERS AND OZONE FILTERS WERE SUBSUEQUENTLY REPLACED AS WELL AS ALL PACK COMPONENTS AND APU COOLING FAN.

Part: SELECTOR VALVE — LEAKING (CARGO DOOR) · airframe 38,850 hrs · 13,978 cycles

DIRTY SOCK ODOR WAS REPORTED ON DESCENT AROUND 10,000 FEET. MAINTENANCE CORRECTED OIL LEAK AT APU FUEL CONTROL AND LUBE MODULE. SUBSEQUENT EVENT THE FOLLOWING DAY FOUND A LEAKING CARGO DOOR SELECTOR VALVE THAT WAS STREAMING INTO THE APU INLET. REMOVED AND REPLACED THE AFT CARGO DOOR SELECTOR VALVE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 38,183 hrs · 13,715 cycles

EMERGENCY FLASHLIGHT INOP AT LEFT AFT DOOR. REPLACED BATTERY IN FLASHLIGHT AT LEFT AFT DOOR AND INSTALLED WITH SERVICEABLE RETAINER STRAP.

Part: EXTINGUISHER — DEFECTIVE (CABIN) · airframe 37,956 hrs · 13,639 cycles

MID CABIN FIRE EXTINGUISHER SAFETY BROKE. INSTALLED NEW FIRE EXTINGUISHER IN MID CABIN PER AIRBUS MAINTENANCE MANUAL 26-24.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 37,718 hrs · 13,533 cycles

C11/SY6 CHECK, FLOOR PANEL 262HG BETWEEN FR 64 AND FR 66, BETWEEN Y464.8 AND Y-1589 AT Z-500 HAS DELAMINATED CORNER. REPLACED FLOOR PANEL 262HG BETWEEN FR 64 AND FR 66, BETWEEN Y464.8 AND Y-1589 AT Z-500 IAW MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 37,718 hrs · 13,533 cycles

C11/SY6 CHECK, FLOOR PANEL 232DF BETWEEN FR 20 AND FR 24 AT Z-500 IIS DELAMINATED AT THE AFT OUTBOARD CORNER. REPLACED FLOOR PANEL 232DF BETWEEN FR 20 AND FR 24 AT Z-500 IAW MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 37,718 hrs · 13,533 cycles

C11/SY6 CHECK, FLOOR PANEL 222EF BETWEEN FR 16 AND FR 20 AT -Y765 AND Z-500 HAS SEVERAL CORRODED INSERTS. REPLACED FLOOR PANEL 222EF BETWEEN FR 16 AND FR 20 AT -Y765 AND Z-500 IAW MCGILL IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 37,718 hrs · 13,533 cycles

C11/SY6 CHECK, FLOOR PANEL 222CF BETWEEN FR 12 AND FR 16 AT Z-500 HAS DELAMINATION. REPLACED FLOOR PANEL 222CF BETWEEN FR 12 AND FR 16 AT Z-500 HAS DELAMINATION IAW MCGILL IRM 9701 REV G.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,718 hrs · 13,533 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR64 TO FR66, Y765. REPLACED SEAT TRACK BETWEEN FR64 TO FR66, Y765. IAW A321 SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 37,718 hrs · 13,533 cycles

C11 CHECK - CRACK ON LATERAL SHEAR PLATE BETWEEN FR68 TO FR69, -Y1292. REPLACED LATERAL SHEAR PLATE BETWEEN FR68 TO FR69, -Y1292 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,718 hrs · 13,533 cycles

C11/SY6 CHECK, CORROSION ON SEAT TRACK BEAM BETWEEN FR 64 AND FR 66 AT Y765 AND Z-500. REPLACED SEAT TRACK BEAM BETWEEN FR 64 AND FR 66 AT Y765 AND Z-500 IAW A321 SRM 51-72-11AND 53-41-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,718 hrs · 13,533 cycles

C11/SY6 CHECK, CORROSION ON FLOOR BEAM BETWEEN FR 18 AND FR 20 AT Y-765 AND Z-500. REPLACED FLOORBEAM BETWEEN FR 18 AND FR 20 AT Y-765 AND Z-500 IAW A321 SRM 51-72-11 AND 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,718 hrs · 13,533 cycles

C11/SY6 CHECK, CORROSION ON FLOOR BEAM AT FR 66 - 3" AT -Y1292 AND Z-500. REPLACED FLOOR BEAM AT FR 66 - 3" AT -Y1292 AND Z-500 IAW A321 SRM 51-42-11 AND 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,718 hrs · 13,533 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SILL PLATE AT FR66, Y1732. REPAIRED SILL PLATE AT FR66, Y1732 IAW A321 SRM 53-41-14, FIGURE 201 REPAIR PRINCIPLE 6.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,718 hrs · 13,533 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR66 TO FR70, -Y765. REPLACED SEAT TRACK BETWEEN FR66 TO FR70, -Y765 IAW A321 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,718 hrs · 13,533 cycles

C11/SY6 CHECK, CORROSION ON SEAT TRACK BETWEEN FR 64 AND FR 66, AT Y-1292 AND Z-500. REPLACED SEAT TRACK BETWEEN FR 64 AND FR 66 AT Y-1292 AND Z-500 IAW A321 SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,718 hrs · 13,533 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BETWEEN FR64 TO FR66, -Z500, -Y464.8. REPLACED FLOOR SUPPORT BETWEEN FR64 TO FR66, -Z500, -Y464.8 IAW A321 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,718 hrs · 13,533 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, -Z500, -Y254. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, -Z500, -Y254 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53112816.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,718 hrs · 13,533 cycles

C11 CHECK - LEVEL 2 CORROSION ON SEAT TRACK AT FR64, -Z500, Y1292. REPLACED SEAT TRACK AT FR64, -Z500, Y1292 IAW A321 SRM 51-72-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,718 hrs · 13,533 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON LEFT SHEAR TIE BETWEEN FR69 TO FR70, Y1160, -Z500. REPLACED LEFT SHEAR TIE BETWEEN FR69 TO FR70, Y1160, -Z500 IAW A320 SRM 51-72-11 & TYPICAL REPAIR 320-2528-10-0011.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,718 hrs · 13,533 cycles

C11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR16, Z500, Y502.3. REPLACED FLOORBEAM AT FR16, Z500, Y502.3 IAW A321 SRM 51-72-11 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,718 hrs · 13,533 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR20 TO FR23, -Z500, Y254. REPLACED FLOORBEAM BETWEEN FR20 TO FR23, -Z500, Y254 IAW A321 SRM 51-72-11, 51-42-11 & 51-21-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,718 hrs · 13,533 cycles

C11/SY6 CHECK, CORROSION ON FLOORBEAM BETWEEN FR 16 AND FR 24 AT Y-1292 AND Z-500. REPLACED FLOORBEAM BETWEEN FR 16 AND FR 24 AT Y-1292 AND Z-500 IAW A321 SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,718 hrs · 13,533 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BETWEEN FR68-8 INCHES TO FR70, -Z500, -Y464.8. REPLACED FLOOR SUPPORT BETWEEN FR68-8 INCHES TO FR70, -Z500, -Y464.8 IAW A321 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,718 hrs · 13,533 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR12 TO FR16, -Z500, -Y81. REPLACED FLOORBEAM BETWEEN FR12 TO FR16, -Z500, -Y81 IAW A321 SRM 53-11-14, 51-43-00 & 51-42-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,718 hrs · 13,533 cycles

C11 CHECK - LEVEL 2 CORROSION ON FLOORBEAM BETWEEN FR66 TO FR69, -Z500, Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR69, -Z500, Y1292 IAW A321 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,718 hrs · 13,533 cycles

C11/SY6 CHECK, CORROSION ON FLOORBEAM AT FR 68 - 2.5" AT -Y1292 AND Z-500. REPLACED FLOORBEAM AT FR 68 - 2.5" AT -Y1292 AND Z-500 IAW A321 SRM 51-42-11 AND 53-00-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,718 hrs · 13,533 cycles

C11 CHECK - LEVEL 2 CORROSION ON FLOORBEAM AT FR66, -Z500, Y1292. REPLACED FLOORBEAM AT FR66, -Z500, Y1292 IAW A321 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,718 hrs · 13,533 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON RIGHT SHEAR PLATE BETWEEN FR69 TO FR70, S23R, Z500, -Y1160. REPLACED RIGHT SHEAR PLATE BETWEEN FR69 TO FR70, S23R, Z500, -Y1160 IAW A321 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,718 hrs · 13,533 cycles

C11/SY6 CHECK, CORROSION ON FLOORBEAM BETWEEN FR 16 AND FR 20 AT Y1292 AND Z-500. REPLACED FLOORBEAM BETWEEN FR 16 AND FR 20 AT Y1292 AND Z-500 IAW A321 SRM 52-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,718 hrs · 13,533 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR20 TO FR23, -Z500, -Y180. REPLACED FLOORBEAM BETWEEN FR20 TO FR23, -Z500, -Y180 IAW A321 SRM 51-42-11, 51-72-11 & AIRBUS DRAWING D53111406.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,718 hrs · 13,533 cycles

C11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR70, -Z500, Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR70, -Z500, Y765 IAW A321 SRM 51-42-11.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 35,459 hrs · 12,781 cycles

FLT 1546 - PHX - EES - CIDS CAUTION LIGHT MESSAGE FOR MID LEFT DOOR PRESSURE. MAINTENANCE SERVICED 2L DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-20-00-614-002.

Part: ACTUATOR — LOW PRESSURE (L2 DOOR) · airframe 34,769 hrs · 12,534 cycles

FLT 1797 PHL - EES - CIDS CAUTION FOR L-2 DOOR. MAINTENANCE SERVICED L-2 DOOR ASSIST IAW AIRBUS MAINTENANCE MANUAL 52-22-00.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 34,629 hrs · 12,490 cycles

FLT 1538 - CLT-BOS - EMERGENCY EGRESS SYSTEM - CIDS CAUTION LIGHT ON. SERVICED L2 DOOR ASSIST BOTTLE PER TSM 52-22-000-02-810-808. CIDS LIGHT OUT. OPERATIONAL CHECK WAS GOOD.

Part: BOTTLE — LOW PRESSURE (EMERGENCY EXIT) · airframe 34,407 hrs · 12,402 cycles

FLT 1790 - CLT - EES - FLIGHT ATTENDANT REPORTED CIDS CAUTION LIGHT FLASHING - WIIL NOT RESET. AIRCRAFT RETURNED TO GATE. MAINTENANCE SERVICED THE 2-L EMERGENCY EXIT DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614-002.

Part: ACTUATOR — LOW PRESSURE (DOOR) · airframe 34,227 hrs · 12,333 cycles

FLT 907 CLT - EES - CIDS PANEL CAUTION LIGHT ILLUMINATED. MAINTENANCE SERVICED MID LEFT DOOR ASSIST IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614-002.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 33,861 hrs · 12,214 cycles

FLT 1719 - MCO - EES - POWER ASSIST BOTTLE PRESSURE LOW L-2 DOOR. MAINTENANCE SERVICED L-2 DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-22-00.

Part: BOTTLE — LOW PRESSURE (EMERGENCY EXIT) · airframe 33,861 hrs · 12,214 cycles

FLT 1719 - SFO - EES - POWER ASSIST BOTTLE PRESSURE LOW L-2 DOOR. MAINTENANCE ACCOMPLISHED SERVICING OF L-2 EMERGENCY EXIT DOOR POWER ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614-002.

Part: LENS — MISSING (CABIN) · airframe 33,692 hrs · 12,141 cycles

MX CK-LAS - EEL - EMERGENCY LIGHT LENS COVER MISSING ON 3L. MAINTENANCE INSTALLED EMERGENCY LIGHT LENS COVER.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 33,414 hrs · 12,031 cycles

FLT 863 - PHL-MCO - EMERGENCY EGRESS SYSTEM - CIDS TEST INDICATE LOW BOTTLE PRESSURE LEFT SIDE FORWARD MID CABIN (DOOR L2). ADDED PRESSURE TO 1783 PSI PER AMM 52-22-00-03.

Part: BOTTLE — LOW PRESSURE (EMERGENCY EXIT) · airframe 32,756 hrs · 11,758 cycles

FLT 801 - PHL - FORWARD FLIGHT ATTENDANT'S CIDS PANEL HAS CAUTION LIGHT. MAINTENANCE SERVICED MID LEFT EMERGENCY DOOR BOTTLE.

Part: CYLINDER — BLOWN (R1 DOOR) · airframe 32,312 hrs · 11,589 cycles

FLT 1490 - LGA - EES - R1 DOOR ASSIST BOTTLE DISC BLOWN. MAINTENANCE SERVICED R1 DOOR ASSIST BOTTLE AND REPLACED DISC IAW AIRBUS MAINTENANCE MANUAL 52-10-00 AND 52-10-00-610.

Part: BOTTLE — LOW PRESSURE (EMERGENCY EXIT) · airframe 32,165 hrs · 11,527 cycles

PIT - EES - CIDS CAUTION ON FORWARD FLIGHT ATTENDANT PANEL. MAINTENANCE SERVICED DOOR ASSIST BOTTLE PER AIRBUS MAINTENANCE MANUAL 52-22-00.

Part: LENS — MISSING (CABIN) · airframe 31,488 hrs · 11,260 cycles

FLT 1544 - PHL - EEL - SEAT 9D MISSING EMERGENCY EXIT LIGHT COVER. MAINTENANCE REPLACED LENS.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 30,543 hrs · 10,941 cycles

FLT 1561 - CLT - EMERGENCY EGRESS SYSTEM - CIDS PANEL RED LIGHTS ON FOR L3 DOOR ASSIST BOTTLE PRESSURE. MAINTENANCE SERVICED L3 DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-22-14.

Part: FIRE DETECTOR — DEFECTIVE (NR 1 ENGINE) · airframe 30,482 hrs · 10,924 cycles

FLT 9225 - CLT - FALSE FIRE WARNING - DURING CRUISE AT FL390 DURING LIGHT TURBULENCE, MASTER CAUTION AND FIRE BELL RANG FOR 3 RINGS AND WENT SILENT. FULL SYSTEMS CHECK AND FIRE/SMOKE CHECK ACCOMPLISHED. NO FAULTS OR ECAMS INDICATED AND NO REOCCURRENCE OF EVENT DURING FLIGHT. MAINTENANCE FOUND LAST LEG FAULT "CK FDU ENG 1 SUPPLY". REPLACED NR 1 ENGINE FIRE DETECTION UNIT 2WD1 IAW AIRBUS MAINTENANCE MANUAL 26-12-34.

Part: LENS — MISSING (CABIN) · airframe 30,467 hrs · 10,921 cycles

FLT 1529 - DEN - EEL - SEAT 26C EMERGENCY LIGHT LENS MISSING. MAINTENANCE INSTALLED LENS AS REQUIRED.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 30,360 hrs · 10,882 cycles

FLT 162 - PHL - EMERGENCY EGRESS SYSTEM - CIDS RED LIGHT ON. MAINTENANCE SERVICED L3 DOOR ASSIST BOTTLE LIGHT CLEARED.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 30,205 hrs · 10,825 cycles

FLT 1498 - LAX - EMERGENCY EGRESS SYSTEM - CAUTION LIGHT ON CIDS PANEL ILLUMINATED. MAINTENANCE SERVICED L-3 DOOR ASSIST BOTTLE.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 30,138 hrs · 10,808 cycles

LOG PAGE 8615044 - FLT 701-PHL - EMERGENCY EGRESS SYSTEM - CIDS CAUTION LIGHT ILLUMINATED. MAINTENANCE SERVICED L1 & L2 EXIT DOOR ASSIST BOTTLES PER AIRBUS MAINTENANCE MANUAL 52-22-00-614.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 30,138 hrs · 10,808 cycles

LOG PAGE 8615044 - FLT 701-PHL - EMERGENCY EGRESS SYSTEM - CIDS CAUTION LIGHT ILLUMINATED. MAINTENANCE SERVICED L1 & `L2 EXIT DOOR ASSIST BOTTLES PER AIRBUS MAINTENANCE MANUAL 52-22-00-614.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 29,735 hrs · 10,666 cycles

FLT 1406 - LAX - EMERGENCY EGRESS SYSTEM - CIDS CAUTION LIGHT FOR L2 DOOR. MAINTENANCE SERVICED L2 DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614-002.

Part: BOTTLE — LOW PRESSURE (EXIT DOOR) · airframe 29,625 hrs · 10,635 cycles

FLT 1418 - PHL - EMERGENCY EGRESS SYSTEM - CIDS CAUTION LIGHT ON FLIGHT ATTENDANT PANEL. MAINTENANCE SERVICED LT EMERGENCY EXIT DOOR ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 29,539 hrs · 10,614 cycles

FLT 1510 - PHL - EMERGENCY EGRESS SYSTEM - L2 & L3 DOOR ASSIST BOTTLES LOW. MAINTENANCE SERVICED IAW AIRBUS MAINTENANCE MANUAL 52-22-00-03.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 29,539 hrs · 10,614 cycles

FLT 1510 - PHL - EMERGENCY EGRESS SYSTEM - L2 & L3 DOOR ASSIST BOTTLES LOW. MAINTENANCE SERVICED IAW AIRBUS MAINTENANCE MANUAL 52-22-00-03.

Part: BOTTLE — LOW PRESSURE (MID DOOR) · airframe 29,497 hrs · 10,597 cycles

LOG PAGE 8413950 - FLT 941-PHX - EMERGENCY EGRESS SYSTEM - DOOR BOTTLE MID L CIDS CAUTION RED LIGHT ON INTERMITTENTLY. MAINTENANCE SERVICED DOOR ASSIST BOTTLE PER AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.

Part: BOTTLE — LOW PRESSURE (EMERGENCY EXIT) · airframe 29,472 hrs · 10,585 cycles

LOG PAGE 8287794-1 - FLT 987-MSP - EMERGENCY EGRESS SYSTEM - PILOT REPORTED CIDS CAUTION LIGHT ON. MAINTENANCE SERVICED BOTH LEFT MID EMERGENCY EXIT DOOR ASSIST BOTTLES (LEFT FORWARD & LEFT AFT) IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614-002.

Part: BOTTLE — LOW PRESSURE (EXIT DOOR) · airframe 29,472 hrs · 10,585 cycles

LOG PAGE 8287794 - FLT 987-MSP - EMERGENCY EGRESS SYSTEM - PILOT REPORTED CIDS CAUTION LIGHT ON. MAINTENANCE SERVICED BOTH LEFT MID EMERGENCY EXIT DOOR ASSIST BOTTLES (LEFT FORWARD & LEFT AFT) IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614-002.

Part: ACTUATOR — LOW PRESSURE (DOOR) · airframe 29,412 hrs · 10,560 cycles

LOG PAGE 8287781 - FLT 1573-CLT - EMERGENCY EQUIPMENT - CABIN CIDS CAUTION / EXIT DOOR MID LEFT. MAINTENANCE SERVICED MID L DOOR BOTTLE PER AIRBUS MAINTENANCE MANUAL 52-22-00-614-002.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 29,366 hrs · 10,540 cycles

LOG PAGE 8287771 - FLT 1492-LAX - EMERGENCY EQUIPMENT - CIDS CAUTION LIGHT ON. MAINTENANCE SERVICED DOOR ASSIST BOTTLE AT L3 CABIN DOOR.

Part: BOTTLE — LOW PRESSURE (EMERGENCY EXIT) · airframe 29,317 hrs · 10,528 cycles

FLT 707 - PHL - EMERGENCY EQUIPMENT - DURING PREFLIGHT CHECK FLIGHT ATTENDANT NOTICED RED LIGHT ON CIDS PANEL. MAINTENANCE SERVICED LEFT MID EXIT DOOR ASSIST BOTTLE PER AIRBUS MAINTENANCE MANUAL 52-22-00-03.

Part: CYLINDER — LOW PRESSURE (L3 DOOR) · airframe 29,220 hrs · 10,497 cycles

FLT 1500-PHL - EMERGENCY EQUIPMENT - CIDS CAUTION LIGHT ILLUMINATED AT FORWARD FLIGHT ATTENDANT'S PANEL. SERVICED L3 DOOR PRESSURE TO NORMAL RANGE.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 29,152 hrs · 10,471 cycles

FLT 937 - PHX - EMERGENCY EQUIPMENT - CIDS CAUTION ILLUMINATED FOR L-3 DOOR BOTTLE PRESSURE. SERVICED L-3 DOOR ASSIST BOTTLE PER AIRBUS MAINTENANCE MANUAL 52-22-00.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 29,088 hrs · 10,450 cycles

FLT 1507 - RSW-CLT - EMERGENCY EQUIPMENT - CIDS-RED LIGHT ON PANEL. SERVICED L-2 DOOR ASSIST BOTTLE TO FULL. CIDS LIGHT OUT.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 29,063 hrs · 10,443 cycles

FLT 1431 - CLT-LAX - EMERGENCY EQUIPMENT - CIDS FAULT ON FLIGHT ATTENDANT PANEL ILLUMINATED. DOOR L-2 ASSIST BOTTLE LOW PRESSURE. SERVICED TO REQUIRED PRESSURE PER MAINTENANCE MANUAL 52-20-00.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 28,952 hrs · 10,404 cycles

FLT 1416 - LAX - EMERGENCY EQUIPMENT - L3 EMERGENCY EXIT DOOR ASSIST BOTTLE PRESSURE LOW TURNING ON CIDS CAUTION. SERVICED L3 DOOR ASSIST BOTTLE PER AIRBUS MAINTENANCE MANUAL 52-22-00-614-002-0.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 28,739 hrs · 10,324 cycles

FLT 1514 - LAX-PHX - EMERGENCY EQUIPMENT - CIDS FAULT LIGHT ON. SERVICED DOOR ASSIST BOTTLES AT L2 & L3 PASSENGER DOORS. CIDS TEST NORMAL.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 28,739 hrs · 10,324 cycles

FLT 1514 - LAX-PHX - EMERGENCY EQUIPMENT - CIDS FAULT LIGHT ON. SERVICED DOOR ASSIST BOTTLES AT L2 & L3 PASSENGER DOORS. CIDS TEST NORMAL.

Part: CYLINDER — LOW PRESSURE (L3 DOOR) · airframe 28,531 hrs · 10,243 cycles

FLT 1426 LAX - PHL - EMERGENCY EQUIPMENT - PILOT REPORT INDICATES CIDS CAUTION. MAINTENANCE SERVICED THE L-3 DOOR ASSIST BOTTLE PER 52-22-00.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 28,458 hrs · 10,217 cycles

FLT 1551 FLL-PHX - EMERGENCY EQUIPMENT - CIDS CAUTION LIGHT ILLUMINATED. MX SERVICED THE L-2 RESERVOIR PER AIRBUS MM 52-10-00-614-001.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 28,458 hrs · 10,217 cycles

FLT 1551 FLL-PHX - EMERGENCY EQUIPMENT - CIDS CAUTION LIGHT ILLUMINATED. MX SERVICED THE L-3 RESERVOIR PER AIRBUS MM 52-10-00-614-001.

Part: BOTTLE — LOW PRESSURE (EMERGENCY EXIT) · airframe 28,272 hrs · 10,145 cycles

FLT 1426 PHX-PHL - EMERGENCY EQUIPMENT - MID LEFT LAV EMERGENCY EXIT DOOR LOW ASSIST PRESSURE. MAINTENANCE SERVICED DOOR ASSIST ACCUMULATOR TO PROPER LEVEL. OPERATIONAL CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 28,192 hrs · 10,119 cycles

LOG PAGE 8288247 - FLT NR 1498 LAX-CLT - EMERGENCY EQUIPMENT - CIDS CAUTION LIGHT LOW DOOR ASSIST PRESSURE. MX SERVICED L3 DOOR ASSIST BOTTLE PRESSURE TO PROPER LEVEL PER AIRBUS MM 52-22-00-03-814-002.

Part: EPSU — FAULTY (EMERGENCY LIGHTS)

TPA - SEVERAL EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE RIGHT HAND, CENTER EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.

Part: SLIDE — LOW PRESSURE (PAX DOOR)

CLT - THE FORWARD ENTRY DOOR EMERGENCY ESCAPE SLIDE HAS LOW PRESSURE. MAINTENANCE REPLACED THE FORWARD ENTRY DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · airframe 17,281 hrs · 17,281 cycles

FOUND FWD WET AREA FS 20 - Y200. REMOVED AND REPLACED BEAM PER SRM 51-72-11; CORROSION LEVEL 1; TASK JA-220-53500, DEFECT SIZE: 3' BY 4".

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 17,281 hrs · 17,281 cycles

FOUND FLOOR SUPPORT CORRODED, Y-503 AT FS 16. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-11-14; 51-42-11; CORROSION LEVEL 1; TASK JA-220-53500 DEFECT SIZE: 1" DIA.

Part: BUSHING — LOOSE (ZONE 200) · airframe 17,281 hrs · 17,281 cycles

FOUND BUSHING LOOSE, ZONE 200 PANEL 262 EF. MANUFACTURED PER AIRBUS SRM 53-02-00, MCGILL IRM 9701, DEFECT SIZE: BUSHING INSERT LOOSE LOWER SURFACE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,281 hrs · 17,281 cycles

FOUND CORROSION LT INBD SEAT TRACK BETWEEN FRAMES 47 AND 47.2. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-00-15, DEFECT SIZE: 1" BY 30".

Part: SILL — CORRODED (FUSELAGE) · airframe 17,281 hrs · 17,281 cycles

FOUND CORROSION -Y1732 FS C66. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-42-11; CORROSION LEVEL 1; TASK JA-26053500, DEFECT SIZE: .125 BY .125.

Part: FLOORBEAM — CORRODED (BS 1732) · airframe 17,281 hrs · 17,281 cycles

AT 1732L AND FR 66 CORROSION. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-41-14; CORROSION LEVEL 1; TASK JA216053500, DEFECT SIZE: .25 X .25 INCH.

Part: BEAM — CORRODED (FR 16 & Y-81) · airframe 17,281 hrs · 17,281 cycles

FOUND CORROSION FS 16 AND Y-81. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11; CORROSION LEVEL 1; TASK JA-220-53500, DEFECT SIZE: 1" BY 1".

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 17,281 hrs · 17,281 cycles

FOUND FLOOR SUPPORT CORRODED, Y1292, FRAME 64 - 70. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-00-14, 51-72-11; CORROSION LEVEL 1; TASK JA26053500, DEFECT SIZE: 1" DIA 4 EA.

Part: BEAM — CORRODED (-Y1292 FR 65 - 6) · airframe 17,281 hrs · 17,281 cycles

FOUND BEAM CORRODED -Y1292 FR 65 - 69. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-10-15; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 1" BY 52".

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 17,281 hrs · 17,281 cycles

FOUND FLOOR SUPPORT CORRODED, Y254 AT FR 21. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-11-14, 51-42-11; CORROSION LEVEL 1; TASK JA-220-53500 DEFECT SIZE: 3/4" DIA.

Part: EPSU — DISCHARGED (EMERGENCY LIGHT)

DCA - THE EMERGENCY LIGHT SYSTEM FAILED THE SYSTEM TEST. MAINTENANCE REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT BATTERY. OPERATIONALLY CHECKS OK.

Part: COMPUTER — MALFUNCTIONED (WINDSHIELD HEAT)

PHL - FLT 167 - EN ROUTE PHL-PHX - AFTER TAKEOFF, RECEIVED 'R WSHLD HEAT, R WNDW HEAT' ECAM WARNINGS. CREW ALSO NOTICED AN ELECTRICAL ODOR THROUGHOUT THE AIRCRAFT. FLT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 WINDSHIELD HEAT COMPUTER. OPERATIONALLY CHECKED OK. (M)