N542UW

Part: LEVER — LOOSE (ZONE 800) · airframe 52,897 hrs · 20,445 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 3R ARMING LEVER LOOSE. MAINTENANCE SECURED ARMING LEVER PER AMM 52-22-22.

Part: BRACKET — CRACKED (ZONE 800) · airframe 52,275 hrs · 20,181 cycles

AIRCRAFT WAS GROUNDED: REF MIC 1561675 R-2 DOOR INFLATION RESERVOIR BRACKET WAS CRACKED. MAINTEANCE REPLACED R-2 INFLATION RESERVOIR BRACKET PER THE AMM 25-62-00 REF E.A 368558.

Part: BATTERY — NO TEST (ZONE 200) · airframe 52,074 hrs · 20,098 cycles

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

Part: HANDLE — LOOSE (ZONE 800) · airframe 50,503 hrs · 19,447 cycles

AIRCRAFT WAS NOT GROUNDED: R2 EMERGENCY EXIT DOOR ARMED HANDLE REQUIRES TIGHTENING. RESECURED R2 EMERGENCY EXIT DOOR ARMED HANDLE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-20-00.

Part: SPAR — WORN (ZONE 400 - NAC/P) · airframe 49,603 hrs · 19,002 cycles

AIRCRAFT IN BASE MAINENANCE: #2 ENGINE PYLON SPAR WORN AT CNA SPRING SEAL CONTACT POINT AND PYLON RIB 5. REPAIRED SPAR PER SRM 54-51-12-283-003 AND EA 358940.

Part: BATTERY — FAULTY (ZONE 200) · airframe 49,347 hrs · 18,879 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT OPERATIONAL TEST FAILED DURING REPLACEMENT OF L4 DOOR SLIDE. FAULT CALL OUT 15WL EMERGENCY POWER SUPPLY UNIT. REMOVED AND REPLACED 15WL EMERGENCY POWER SUPPLY UNIT BATTERY PER AMM 33-51-38.

Part: POWER SUPPLY — FAULTY (ZONE 200) · airframe 49,022 hrs · 18,753 cycles

AIRCRAFT WAS NOT GROUNDED: DURING PS CHECK EPSU SYSTEM TEST BATTERY/EPSU (15WL) MIDDLE LEFT FAULT. REPLACED EPSU 15WL.

Part: BATTERY — NO TEST (ZONE 200) · airframe 49,022 hrs · 18,753 cycles

AIRCRAFT WAS NOT GROUNDED: DURING PS CHECK EPSU SYSTEM TEST BATTERY/EPSU (12WL) EXTERNAL RIGHT FAULT. REPLACED BATTERY

Part: DIAPHRAGM — FAILED (ASSIST BOTTLE) · airframe 49,054 hrs · 18,765 cycles

AIRCRAFT WAS NOT GROUNDED: R2 EMERGENCY DOOR ASSIST BOTTLE AT ZERO. REPLACED R2 EMERGENCY EXIT DOOR ASSIST BOTTLE DIAPHRAGM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 48,535 hrs · 18,545 cycles

AIRCRAFT WAS GROUNDED: DURING EMERGENCY POWER SUPPLY UNIT SYSTEM TEST, FAULT MESSAGE EMERGENCY POWER SUPPLY UNIT (14WL) MID RIGHT. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY AT 14WL PER AMM 33-51-38.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,535 hrs · 18,545 cycles

AIRCRAFT WAS GROUNDED: DURING EMERGENCY POWER SUPPLY UNIT SYSTEM TEST FAULT MESSAGE EMERGENCY POWER SUPPLY UNIT (10WL) FORWARD LEFT. REPLACED 10WL EMERGENCY POWER SUPPLY UNIT BATTERY.

Part: SELECTOR VALVE — DEFECTIVE (NLG) · airframe 48,530 hrs · 18,543 cycles

AIRCRAFT WAS GROUNDED: THE FLIGHT CREW REPORTED THAT AFTER GEAR RETRACTION A RED NOSE WHEEL UNLOCK WARNING LIGHT REMAINED ILLUMINATED. AIR NOISE AND VIBRATION CONFIRMED NOSE GEAR DOORS STILL OPEN. AS PER ECAM GEAR WAS RECYCLED AND RETRACTED NORMALLY. MAINTENANCE REPLACED THE LANDING GEAR SELECTOR VALVE MANIFOLD ASSEMBLY AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK.

Part: BYPASS VALVE — FAULTED (MLG) · airframe 48,508 hrs · 18,535 cycles

AIRCRAFT WAS GROUNDED: AFTER TAKEOFF AND LANDING GEAR RETRACTION, NOSE GEAR RED UNLOCK LIGHT REMAINED ILLUMINATED. WE OBSERVE A LANDING GEAR DOORS NOT CLOSED ECAM SHORTLY AFTER. HAVING SEEN THE HISTORY ON THIS ISSUE, WE PAUSED BEFORE STARTING ECAM ACTIONS AND THE PROBLEM SELF-CORRECTED AFTER 10 TO 15 SECONDS. CFDS SHOWS THAT THE LANDING GEAR NOT UPLOCKED ECAM WAS ALSO TRIGGERED AND WAITING FOR US IF WE HAD CLEARED THE FIRST ECAM MESSAGE. MAINTENANCE REPLACED THE NOSE LANDING GEAR DOOR GROUND OPENING BYPASS VALVE 2533GM AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER AMM 32-22-17.

Part: SELECTOR VALVE — DEFECTIVE (MLG) · airframe 48,490 hrs · 18,527 cycles

AIRCRAFT WAS GROUNDED: LANDING GEAR NOT UPLOCKED ECAM CAUTION AFTER GEAR RETRACTION. CONDITION SELF-CORRECTED AFTER 1 SECOND. MAINTENANCE REPLACED THE FORWARD LANDING GEAR DOOR SELECTOR VALVE PER AMM 32-31-12. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: UPLOCK — DEFECTIVE (MLG) · airframe 48,483 hrs · 18,523 cycles

AIRCRAFT WAS GROUNDED: AFTER GEAR RETRACTION, RED NOSE WHEEL UNLOCK WARNING LIGHT REMAINED. AS PER ECAM GEAR WAS RECYCLED AND AFTER ABOUT A 30 SECOND DELAY THE WARNING LIGHT EXTINGUISHED. MAINTENANCE REPLACED THE NOSE LANDING GEAR UPLOCK ASSEMBLY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER TASK CARD 26L70032005.

Part: PROXIMITY SENSOR — CONTAMINATED (NLG) · airframe 48,287 hrs · 18,435 cycles

AIRCRAFT WAS GROUNDED: AFTER TAKEOFF LANDING GEAR NOT UPLOCKED ECAM. NOSE GEAR LIGHT WAS RED. FLIGHT CREW COMPLETED ECAM ACTIONS. RED LIGHT EXTINGUISHED. MAINTENANCE ACCOMPLISHED TSM 32-31-00-810-865-A, 32-31-00-810-846-A AND FOUND PROXIMITY SENSORS 12GA (AALA202405158670) AND 13GA (AALA202405151305) HAVE GREASE CONTAMINATION. MAINTENANCE CLEANED THE SENSORS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: PROXIMITY SENSOR — CONTAMINATED (NLG) · airframe 48,287 hrs · 18,435 cycles

AIRCRAFT WAS GROUNDED: AFTER TAKEOFF LANDING GEAR NOT UPLOCKED ECAM. NOSE GEAR LIGHT WAS RED. FLIGHT CREW COMPLETED ECAM ACTIONS. RED LIGHT EXTINGUISHED. MAINTENANCE ACCOMPLISHED TSM 32-31-00-810-865-A, 32-31-00-810-846-A AND FOUND PROXIMITY SENSORS 12GA (AALA202405158670) AND 13GA (AALA202405151305) HAVE GREASE CONTAMINATION. MAINTENANCE CLEANED THE SENSORS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: DOOR LATCH — INOPERATIVE (COCKPIT) · airframe 47,836 hrs · 18,207 cycles

AIRCRAFT WAS NOT GROUNDED: COCKPIT DOOR LOCKING MECHANISM NOT OPERATING ALL PLUNGERS TO OPEN THE DOOR. REMOVED AND REPLACED COCKPIT DOOR LATCH MECHANISM.

Part: RELAY — DEFECTIVE (ZONE 100 - FUSE) · airframe 47,265 hrs · 17,952 cycles

AIRCRAFT WAS GROUNDED: INBOUND CREW REPORTED NOSE LANDING GEAR AND LEFT MAIN LANDING GEAR GREEN SAFE INDICATION WAS FLASHING ON APPROACH. MAINTENANCE REPLACED THE #1 LAND GEAR CONTROL INTERFACE UNIT (LGCIU) PER AMM 32-31-71. (AALA202401233242) AND REPLACED RELAY 53GA (AALA202401236512). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: LGCIU — WARNING MESSAGE (ZONE 100 - FUSE) · airframe 47,265 hrs · 17,952 cycles

AIRCRAFT WAS GROUNDED: INBOUND CREW REPORTED NOSE LANDING GEAR AND LEFT MAIN LANDING GEAR GREEN SAFE INDICATION WAS FLASHING ON APPROACH. MAINTENANCE REPLACED THE #1 LAND GEAR CONTROL INTERFACE UNIT (LGCIU) PER AMM 32-31-71. (AALA202401233242) AND REPLACED RELAY 53GA (AALA202401236512). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: SCREW — LOOSE (ZONE 200 - FUSE) · airframe 46,125 hrs · 17,384 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR DIFFICULT TO OPEN/CLOSE DURING FLIGHT. TOP DOOR STRIKER STUCK. FOUND LOOSE SCREW IN DOOR FRAME LOOSE. TIGHTENED SCREW.

Part: HINGE — STICKING (ZONE 800 - DOORS) · airframe 45,520 hrs · 17,108 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR IS SQUEAKY AND DIFFICULT TO OPEN/CLOSE. LUBRICATED UPPER HINGE MECHANISM PER AMM 52-51-11.

Part: POWER SUPPLY — NO TEST (ZONE 200 - FUSE) · airframe 45,318 hrs · 17,015 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING THE EMERGENCY LIGHT TEST THE EMERGENCY POWER SUPPLY UNIT (11WL) EXIT LEFT FLAGGED. REPLACED EMERGENCY POWER SUPPLY UNIT 11WL PER AMM 33-51-38-400-001-A.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 43,629 hrs · 16,241 cycles

AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT AT 1L INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-65-00.

Part: STRAP — DETACHED (ZONE 800 - DOORS) · airframe 42,182 hrs · 15,606 cycles

AIRCRAFT WAS NOT GROUNDED: RI DOOR SLIDE STRAP IN FIRST CLASS GALLEY HANGING DOWN PREVENTING DOOR CLOSURE. RE-ATTACHED R1 DOOR SLIDE STRAP AND VERIFIED SLIDE PACK INSTALLATION PER AMM 25-62-44.

Part: COVER — OUT OF POSITION (ZONE 200 - FUSE) · airframe 42,156 hrs · 15,594 cycles

AIRCRAFT WAS NOT GROUNDED: ESCAPE ROPE COVER WONT STAY IN POSITION. RE-SECURED ESCAPE ROPE COVER AS REQUIRED

Part: SMOKE DETECTOR — FALSE INDICATION (ZONE 900 - LAV/G) · airframe 41,965 hrs · 15,504 cycles

AIRCRAFT WAS NOT GROUNDED: IN FLIGHT LAVATORY SMOKE ECAM INDICATION AS WELL AS FLIGHT ATTENDANT PANEL FOR AFT RIGHT LAVATORY. NO INDICATION OF SMOKE, TRASH CANS DOUSED CONTINUED NORMALLY. MAINTENANCE PERFORMED A SATISFACTORY OPERATIONAL CHECK OF THE LAVATORY SMOKE DETECTION SYSTEM PER AMM 26-17-00.

Part: STRIKER — STICKING (ZONE 800 - DOORS) · airframe 41,235 hrs · 15,174 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR TOP STRIKER APPEARS TO NOT LATCH AND DIFFICULT TO OPEN AND CLOSE. LUBRICATED STRIKER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: DIAPHRAGM — LOW PRESSURE (ZONE 800 - DOORS) · airframe 41,132 hrs · 15,126 cycles

AIRCRAFT WAS GROUNDED: R4 DOOR, CHECK DOOR PRESSURE LIGHT ON FLIGHT ATTENDANT PANEL. REPLACED DOOR ASSIST BOTTLE DIAPHRAGM PER AMM 52-10-00.

Part: CYLINDER — LOW PRESSURE (ZONE 800 - DOORS) · airframe 41,132 hrs · 15,125 cycles

AIRCRAFT WAS GROUNDED: ENTRY DOOR "CABIN PRESSURE" LIGHT DISAGREE WITH AIRCRAFT AT DOOR 4R. SERVICED 4R DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.

Part: CYLINDER — LOW PRESSURE (ZONE 800 - DOORS) · airframe 41,082 hrs · 15,102 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 4R PRESSURE LOW ON FLIGHT ATTENDANTS PANEL. SERVICED 4R DOOR DAMPER & EMERGENCY OPERATION CYLINDER PER AMM 52-10-00. FLIGHT ATTENDANTS PANEL LOW PRESSURE WARNING CLEARED.

Part: PROXIMITY SWITCH — FALSE INDICATION (ZONE 800 - DOORS) · airframe 40,561 hrs · 14,876 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 3L SLIDE INDICATION BLINKS ARMED AND DISARMED ON ECAM AND FLIGHT ATTENDANT PANEL. SLIDE VERIFIED DISSARMED. REPLACED 3L DOOR ARM HANDLE PROXIMITY SWITCH PER AMM 52-73-11.

Part: RESERVOIR — LOW PRESSURE (ZONE 200 - FUSE) · airframe 40,312 hrs · 14,766 cycles

AIRCRAFT IN BASE MAINTENANCE: LOW PRESSURE SLIDE INFLATION RESERVOIR ON EMERGENCY EXIT DOOR 843. REPLACED RESERVOIR PER AMM 25-62-49-400-001-A.

Part: POWER CABLE — CHAFED (ZONE 400 - NAC/P) · airframe 40,312 hrs · 14,766 cycles

AIRCRAFT IN BASE MAINTENANCE: #2 ENGINE INTEGRATED DRIVE GENERATOR POWER CABLES CHAFFED. REPLACED POWER CABLES AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 24-21-43.

Part: CONNECTOR — INOPERATIVE (ZONE 200 - FUSE) · airframe 40,312 hrs · 14,766 cycles

AIRCRAFT WAS NOT GROUNDED: INOPERATIVE EMERGENCY EXIT LIGHT IN AFT PASSENGER CABIN ON SEAT (32, 33, 34 LEFT SIDE) IN PASSENGER CABIN (3 EA). PERFORMED CORRECTLY CONNECTION OF CONNECTOR 7260VC 13 PER ESPM 20-44-11

Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 40,313 hrs · 14,766 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT GALLEY AREA CRACKED SHEAR PLATE LOCATED BETWEEN FR 69 TO FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11-801 AND DRAWING D53474180.

Part: FLOOR SUPPORT — CRACKED (ZONE 100 - FUSE) · airframe 40,313 hrs · 14,766 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED COCKPIT FLOOR SUPPORT ANGLE FITTING LOCATED BETWEEN FR 11 AND FR 12 AT LEVEL OF Y1292. REPLACED FITTING PER SRM 51-42-11-801-A AND DWG D53113448.

Part: FLOOR PANEL — DELAMINATED (ZONE 200 - FUSE) · airframe 40,312 hrs · 14,766 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT PASSENGER CABIN FLOOR PANEL 251AF DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 970.

Part: NONE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 40,313 hrs · 14,766 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION MEASURING L=0.828 IN, W=0.612 IN, D=0.006 IN, ON BULK CARGO COMPARTMENT DOOR FRAME LOWER SILL LOCATED AT FR 62 AT LEVEL OF S38R. REPAIRED PER SRM 53-41-49-300-003.

Part: PIN — WORN (ZONE 700 - GEARS) · airframe 40,312 hrs · 14,766 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: WEAR ON TORQUE LINKS CENTER HINGE PIN ON NOSE LANDING GEAR (1EA). REPLACED NEW CENTER PIN NOSE LANDING GEAR PER AMM 32-27-27-400-002-A.

Part: SUPPORT ANGLE — CRACKED (ZONE 100 - FUSE) · airframe 40,313 hrs · 14,766 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN FLOOR SUPPORT ANGLE LOCATED FROM FR 11 TO FR 12 AND -Y765. REPLACED ANGLE PER SRM 51-72-11-911-001, SRM 51-42-11-801 AND DWG D53113448.

Part: SUPPORT ANGLE — CRACKED (ZONE 100 - FUSE) · airframe 40,313 hrs · 14,766 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN FLOOR SUPPORT ANGLE LOCATED FROM FR 11 TO FR 12 AND Y765. REPLACED ANGLE PER SRM 51-72-11-911-001, SRM 51-42-11-801 AND DWG D53113448.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 - STABS) · airframe 40,312 hrs · 14,766 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER # 6 ELEVATOR HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER AMM 55-16-42-400-001-A.

Part: FLOOR PANEL — DELAMINATED (ZONE 200 - FUSE) · airframe 40,312 hrs · 14,766 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD GALLEY AREA FLOOR PANEL 221LF DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701.

Part: HINGE FITTING — EXCESS PLAY (ZONE 200 - FUSE) · airframe 40,312 hrs · 14,766 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER # 5 ELEVATOR HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 - STABS) · airframe 40,312 hrs · 14,766 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER # 1 ELEVATOR HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER AMM 55-16-42-400-001-A.

Part: FITTING — CRACKED (ZONE 100 - FUSE) · airframe 40,313 hrs · 14,766 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK ON AFT GALLEY AREA CORNER FITTING LOCATED AT FR 68 AND S23R. REPLACED FITTING PER SRM 51-42-11-801 AND DRAWING D53480505.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 - STABS) · airframe 40,312 hrs · 14,766 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND STABILIZER # 1 ELEVATOR HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER AMM 55-46-42-400-001-A.

Part: FLOOR PANEL — CRACKED (ZONE 100 - FUSE) · airframe 40,312 hrs · 14,766 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO COMPARTMENT FLOOR PANEL 131EF CRACKED. REPAIRED FLOOR PANEL PER SRM 53-02-00-283-00 AND SRM 53-02-00-300-004.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 - STABS) · airframe 40,312 hrs · 14,766 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER # 3 ELEVATOR HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 - STABS) · airframe 40,312 hrs · 14,766 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER # 5 ELEVATOR HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER AMM 55-16-42-400-001-A.

Part: FLOOR PANEL — CRACKED (ZONE 100 - FUSE) · airframe 40,312 hrs · 14,766 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO COMPARTMENT FLOOR PANEL 131CF CRACKED. REPLACED FLOOR PANEL.

Part: FLOOR PANEL — DEBONDED (ZONE 100 - FUSE) · airframe 40,312 hrs · 14,766 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CARGO COMPARTMENT FLOOR PANEL 151RF DEBONDED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: NONE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 40,313 hrs · 14,766 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION MEASURING L:0.991 IN, W: 0.497 IN, D: 0.123 IN, ON AFT GALLEY AREA LOWER SILL LOCATED BETWEEN FR 66 TO FR 68 AND S23R. REPLACED SILL PER SRM 51-42-11-801, DRAWING D53480505 AND DRAWING D53474250.

Part: NONE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 40,313 hrs · 14,766 cycles

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

Part: FLOORBEAM — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 40,313 hrs · 14,766 cycles

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

Part: SHEAR PLATE — CRACKED (ZONE 200 - FUSE) · airframe 40,313 hrs · 14,766 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN AFT GALLEY AREA SHEAR PLATE LOCATED FROM FR69 TO FR70 AT LEVEL S23L. REPLACED SHEAR PLATE PER SRM 51-42-11-801 AND DWG D53474180.

Part: DUMMY RAIL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 40,313 hrs · 14,766 cycles

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

Part: FLOORBEAM — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 40,313 hrs · 14,766 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR BEAM AT FR 20 AND -Y1292. REPLACED FLOOR BEAM PER SRM 51-42-11.

Part: FITTING — LACK OF LUBE (L4 GIRT BAR) · airframe 40,093 hrs · 14,676 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS DOOR L4 DIFFICULT TO ARM. CLEANED AND LUBRICATED GIRT BAR FITTINGS PER AMM 52-13-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: FITTING — LACK OF LUBE (R4 GIRT BAR) · airframe 40,093 hrs · 14,676 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS DOOR 4R DIFFICULT TO ARM. CLEANED AND LUBRICATED GIRT BAR FITTINGS PER AMM 52-13-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,107 hrs · 14,270 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT AT SEAT ROWS ON 21R, 22L/R AND 23L INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY UNIT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38-000-001A

Part: SWITCH — STICKING (FUEL PUMPS) · airframe 38,730 hrs · 14,121 cycles

AIRCRAFT WAS NOT GROUNDED: AFTER TURNING ON ALL FUEL PUMPS, 200 LBS FUEL TRANSFERRED FROM CENTER TANK TO RIGHT WING. FOUND DEFUEL/TRANSFER SWITCH STICKING. RESET SWITCH.

Part: BOTTLE — LOW PRESSURE (R3 DOOR ASSIST) · airframe 38,668 hrs · 14,095 cycles

AIRCRAFT WAS NOT GROUNDED: R3 DOOR ASSIST BOTTLE/DAMPER IS IN THE YELLOW RANGE. SERVICED R3 DOOR ASSIST BOTTLE/DAMPER PER AMM TASK 52-22-00-614-002.

Part: MEGAPHONE — INOPERATIVE (ZONE 200 FUS) · airframe 38,503 hrs · 14,023 cycles

AIRCRAFT IN BASE MAINTENANCE: MEGAPHONE INOPERATIVE. REPLACED MEGAPHONE AS REQUIRED.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 37,867 hrs · 13,762 cycles

AIRCRAFT WAS GROUNDED. CABIN PRESSURIZATION FLUCTUATING AT 350. THE CABIN CLIMBED TO 8800 FEET THEN DESCENDED NORMALLY. CABIN PRESSURE WAS USING SYSTEM 2. NO ECAM WARNING. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER 2 AND PERFORMED SATISFACTORY OPERATIONAL TEST, IAW AMM 21-31-34.

Part: CONTROLLER — DEFECTIVE (CABIN PRESSURE) · airframe 37,832 hrs · 13,751 cycles

AIRCRAFT WAS GROUNDED. AT CRUISE FL 360 SYSTEM 1 CABIN PRESSURE VS ERRATIC AND CABIN ALT 8850 FT FLASHING GREEN, DESCENDED TO FL 320 CABIN ALT RETURNED TO NORMAL AND 7500 FT STEADY VS AND ALT. REPLACED NR 1 CABIN PRESSURE CONTROLLER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK, PER AMM 21-31-34.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 36,390 hrs · 13,162 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTED FLOOR PANEL HAS SOFT SPOT IN AISLE AT MID CABIN EXIT. REPLACED FLOOR PANEL PER AMM 53-00-00.

Part: PINTLE PIN — CORRODED (RT MLG) · airframe 36,049 hrs · 13,031 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROISON ON RIGHT HAND MAIN LANDING GEAR REAR PINTLE PIN ON RIGHT WING. REPLACED PINTLE PIN PER TASK CARD 26T00032001.

Part: PTU — LEAKING · airframe 34,879 hrs · 12,597 cycles

AIRCRAFT WAS GROUNDED: CREW REPORTS OIL/MUSTY SMELL ON DECENT IN COCKPIT AND AFT CABIN. ALSO PRONOUNCED ON THE GROUND IN THE COCKPIT WHEN ON APU BLEED AIR. MAINTENANCE FOUND THE PTU LEAKING. REMOVED AND REPLACED THE PTU IAW AMM 29-23-41. OPS AND LEAK CHECK GOOD.

Part: LENS — MISSING (CABIN) · airframe 34,176 hrs · 12,348 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY AISLE LIGHT 34C LENS MISSING. MAINTENANCE REPLACED EMERGENCY LIGHT ASSEMBLY PER AMM 33-51-18.

Part: WARNING MESSAGE — FALSE ACTIVATION (LAVATORY SMOKE) · airframe 33,833 hrs · 12,216 cycles

AIRCRAFT WAS NOT GROUNDED: VERY BRIEF "SMOKE LAV SMOKE" MESSAGE DISPLAYED ON ECAM AND CLEARED ITSELF. MAINTENANCE BITE CHECKED SYSTEM, NO UNUSUAL ODORS OR SIGNS DISPLAYED.

Part: STRAP — MISSING (R1 DOOR SLIDE) · airframe 32,508 hrs · 11,658 cycles

R1 DOOR SLIDE HOOK AND LOOP ARM STRAP WAS MISSING. MAINTENANCE REPLACED THE STRAP AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,242 hrs · 11,550 cycles

SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE AT THE R2 DOOR. MAINTENANCE REPLACED THE LAMPS IAW AMM 33-51-18, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: SLIDE — NO TEST · airframe 31,947 hrs · 11,415 cycles

AIRCRAFT WAS NOT GROUNDED. REPLACED R2 DOOR SLIDE FOR TIME CHANGE AND NEW SLIDE FROM STOCK WOULD NOT PASS TEST. REINSTALLED ORIGINAL SLIDE PER JOB CARD, DEFERRED TIME CHANGE. TEST PASSED NO FAULTS.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 31,955 hrs · 11,419 cycles

EMERGENCY LIGHT ROW 22R WAS INOPERATIVE. CONNECTED EMERGENCY LIGHT IAW MM 33-51-00. OPS CHECKED NORMAL.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 31,955 hrs · 11,419 cycles

EMERGENCY LIGHT TEST FAILED . REPLACED THE POWER SUPPLY BATTERY PACK 10WL IAW MM 33-51-00. OPS NORMAL.

Part: APU — LEAKING · airframe 31,884 hrs · 11,393 cycles

DUE TO CABIN ODOR MIC 8858738 MON REQ GENERATION TO ACCOMPLISH J/C 26L00021004. REPLACED THE APU AND ACCOMPLISHED A PACK BURN OUT IAW J/C 26L31049003. LEAK AND OPS CHECKED OK.

Part: FILTER — DEFECTIVE (A/C PACKS) · airframe 31,804 hrs · 11,364 cycles

DIRTY, MUSTY ODOR WITH PACKS ON. AFTER DECONTAMINATION, NO FURTHER CABIN ODOR. TROUBLESHOT THE CABIN ODOR WITH LT AND RT PACKS OZONE FILTERS REPLACED IAW AMM 21-51-41-000 AND 400-001-A. LEAK CHECKED GOOD.

Part: FILTER — ODOR (CABIN) · airframe 31,804 hrs · 11,364 cycles

DIRTY, MUSTY ODOR WITH PACKS ON. AFTER DECONTAMINATION, NO FURTHER CABIN ODOR. TROUBLESHOT CABIN ODOR WITH LT & RT PACKS OZONE FILTERS REPLACED IAW AMM 21-51-41-000 AND 400-001-A. LEAK CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 31,164 hrs · 11,146 cycles

THE AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY LIGHT LENS MISSING. REPLACED LIGHT ASSEMBLY PER AMM 33-51-19. OPERATIONS CHECK NORMAL.

Part: BATTERY — DISCHARGED (FWD FLASHLIGHT) · airframe 30,265 hrs · 10,812 cycles

FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT DOES NOT OPERATE, WILL NOT RECHARGE. REPLACED THE BATTERY.

Part: LIGHT — INOPERATIVE (ROW 18) · airframe 30,167 hrs · 10,771 cycles

EMERGENCY LIGHT AT ROW 18 LEFT IS INOPERATIVE. REPAIRED THE LIGHT. THE AIRCRAFT WAS GROUNDED.

Part: SLIDE — FOD (L4 DOOR) · airframe 30,151 hrs · 10,765 cycles

L4 DOOR SLIDE ARMING MECHANISM IS VERY DIFFICULT TO OPERATE. REMOVED DEBRIS AND LUBRICATED THE DOOR SLIDE ARMING MECHANISM IAW AMM 52-11-21.

Part: PANEL — DETACHED (EMERGENCY LIGHTS) · airframe 30,131 hrs · 10,758 cycles

L1 DOOR, RIGHT SIDE COVER PANEL KEEPS FALLING OFF BRAKET. SECURED, AND CLOSED THE L1 EXIT LIGHT PANEL IAW AMM 25-28-00.

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,006 hrs · 10,710 cycles

AISLE LIGHT AT ROW 33L INOPERATIVE. REMOVED AND REPLACED THE BALLAST. OPS CHECKED GOOD IAW AMM 33-21-11.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 29,933 hrs · 10,685 cycles

FLOOR EMERGENCY LIGHT LENS AT THE R4 DOOR WAS MISSING. MAINTENANCE INSTALLED THE LENS AND PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-18.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 29,849 hrs · 10,652 cycles

AIRCRAFT WAS NOT GROUNDED. CENTER TANK RIGHT TRANSFER FAIL. FOLLOWED ECAM PLUS OPENED CROSS FEED AND TURNED ENG PUMPS 1 + 2 OFF. PERFORMED OPERATIONS CHECK ON RIGHT CENTER TANK TRANSFER VALVE. NO DEFECTS NOTED PER AMM 28-23-00.

Part: CYLINDER — DAMAGED (R2 DOOR) · airframe 29,027 hrs · 10,327 cycles

R2 SLIDE RESERVOIR BOTTLE UNION FITTING IS STRIPPED. REMOVED R2 SLIDE RESERVOIR BOTTLE PER AMM.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 28,899 hrs · 10,276 cycles

L1 DOOR EXIT LIGHT LENS DETACHED. REPLACED THE LENS IAW AMM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 28,643 hrs · 10,185 cycles

EMERGENCY LIGHT, WHITE COVER AT BOTTOM RIGHT NEAREST THE DOOR, IS MISSING. REPLACED THE COVER IAW AMM.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 28,178 hrs · 10,015 cycles

SOFT SPOTS ON CABIN CENTER FLOORBOARD 251AF. REPAIRED THE FLOOR PANEL DWG 53-02-00-2, REPAIR 2, SRM 53-02-00-300-010, AND AMM 53-42-400-001-A.

Part: BATTERY — MALFUNCTIONED (FLASHLIGHT) · airframe 27,732 hrs · 9,837 cycles

AFT F/A JUMP SEAT FLASHLIGHT CAME ON AND WILL NOT TURN OFF. REPLACED FLASHLIGHT BATTERY.

Part: RETAINER — DIRTY (GIRT BAR) · airframe 27,035 hrs · 9,578 cycles

FLIGHT ATTENDANT REPORTED THE L4 DOOR HARD TO ARM AND DISARM. LEVER MAKES GRINDING NOISE WHEN MOVED. CLEANED AND LUBED FLOOR GIRT BAR RETAINERS.

Part: GIRT BAR — OBSTRUCTED (L4 DOOR SLIDE) · airframe 26,892 hrs · 9,534 cycles

L4 DOOR SLIDE WON'T ARM. MAINTENANCE REMOVED DEBRIS FROM FLOOR AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 26,872 hrs · 9,525 cycles

EMERGENCY LIGHT LENS AFT OF THE L2 DOOR IS MISSING. INSTALLED A NEW LENS.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 26,217 hrs · 9,255 cycles

BROKEN EXIT LIGHT LENS. MAINTENANCE REPLACED THE LENS AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (CABIN) · airframe 25,741 hrs · 9,080 cycles

EXIT LITE COVERS DOORS 4L & 4R MISSING. REPLACED EXIT LIGHT COVERS AT DOORS 4L AND 4R. THE AIRCRAFT WAS NOT GROUNDED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 25,207 hrs · 8,875 cycles

EMERGENCY EXIT LIGHT LENS COVER 4L MISSING. INSTALLED LENS COVER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: VALVE — FAULTED (FUEL DIVERTER) · airframe 24,866 hrs · 8,751 cycles

FLIGHT CREW REPORTED AN ENGINE 1 FUEL HEAT SYSTEM FUEL RETURN VALVE OPEN FAULT MESSAGE. THE AIRCRAFT WAS GROUNDED. REPLACED THE 1ENGINE FUEL DIVERTER AND RETURN VALVE IAW AMM 73-13-42-400-010-A AND ACCOMPLISHED A SATISFACTORY LEAK & OPS CHECK.

Part: LENS — MISSING (CABIN) · airframe 22,716 hrs · 7,910 cycles

AIRCRAFT WAS NOT GNDED. ROW 22C EMER LIGHT LENS COVER MISSING. REPLACED EMER LIGHT ASSEMBLY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 21,821 hrs · 7,551 cycles

1S CHECK, FLOOR PANEL 231BF HAS DELAMINATION. REPLACED FLOOR PANEL IAW IRM 9701 REV G.

Part: HANDLE — WORN (R3 DOOR) · airframe 21,821 hrs · 7,551 cycles

1S CHECK, R3 DOOR ARM & DISARM HANDLE ASSEMBLY WORN AT ARMING HANDLE GRIP PLATE ANTI-ROTATION LUG. REPLACED HANDLE ASSEMBLY IAW AMM 52-22-22-408-001-A.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 21,821 hrs · 7,551 cycles

1S CHECK, FLOOR PANEL 222CF HAS DELAMINATION. REPLACED FLOOR PANEL IAW 9701 REV G.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,821 hrs · 7,551 cycles

1S CHECK, CORROSION ON RT SHEAR PLATE, BETWEEN FRAME 69 - 70, -Y1160. REPLACED IAW SRM 51-42-11 & DWG D5347418002.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,821 hrs · 7,551 cycles

1S CHECK, CORROSION ON RT AFT DOOR CUT OUT, LOWER SILL PLATE AT FRAME 68 & -Y1165. REPAIRED IAW SRM 53-41-14-201 REPAIR PRINCIPLE 5.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,821 hrs · 7,551 cycles

1S CHECK, CORROSION ON LT AFT DOOR CUT OUT, LOWER SILL PLATE AT FRAME 68 & Y1165. REPAIRED IAW SRM 53-41-14.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 21,821 hrs · 7,551 cycles

1S CHECK, LT SHEAR PLATE CRACKED, BETWEEN FRAME 69 - 70, +Y1162.5 & +Y1589. REPLACED IAW SRM 51-72-11, DWG 18D53471124.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 21,572 hrs · 7,451 cycles

FLIGHT ATTENDANT REPORTS SOFT SPOT ON FLOOR AT DOOR 4R. R & R AFT GALLEY FLOOR PANEL 261DF IAW AMM 53-42-12-000-002 & 53-42-12-400-002.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 21,037 hrs · 7,252 cycles

AFT CARGO COMPARTMENT FLOOR PANEL AFT OF ACT TANK HAS A DELAMINATION. REPLACED AFT CARGO COMPARTMENT FLOOR PANEL AFT OF ACT TANK IAW AMM 53-42-14.

Part: SENSOR — MALFUNCTIONED (BRAKE TEMP) · airframe 21,025 hrs · 7,246 cycles

FLIGHT 451 EN-ROUTE, AT BRAKE RELEASE THE TEMP AT RT OTBD BRAKE WAS 90 DEG. AFTER GEAR RETRACTION IT JUMPED TO 350 DEG, THEN OSCILLATED BACK & FORTH BETWEEN 350 & 275 & TRIGGERING THE ECAM SEVERAL TIMES. AFTER IT WAS LOWERED IT IMMEDIATELY DROPPED TO 90 DEG. THE GEAR WAS RETRACTED & THE FLIGHT CONTINUED, LANDING WITHOUT FURTHER INCIDENT. R & R NR 4 MLG BRAKE TEMP SENSOR IAW AMM 32-47-15-400-001-A. OPERATIONS CHECKED OK.

Part: LENS — MISSING (CABIN) · airframe 20,817 hrs · 7,167 cycles

EMERGENCY EXIT LIGHT COVERS AT DOORS L4 & R4 ARE MISSING. INSTALLED EMER EXIT LIGHT LENS COVERS AT DOORS L4 & R4.

Part: UNKNOWN — ODOR (CABIN) · airframe 20,128 hrs · 6,881 cycles

FLIGHT ATTENDANTS NOTED FUEL & CHEMICAL SMELL THROUGHOUT CABIN SHORTLY AFTER LANDING. COMPLIED WITH CABIN AIR QUALITY CHECK CARD 26L00021001. NO ODORS NOTED AFTER ENG RUN & ACFT RETURNED TO SERVICE.

Part: FILTER — RESTRICTED (HYDRAULIC SYS) · airframe 17,883 hrs · 5,976 cycles

AIRCRAFT RETURNED TO FIELD & PILOT DECLARED AN EMER DUE TO YELLOW HYD SYS OVERHEAT AFTER DEPARTING. RETURNED FOR PRECAUTIONARY LANDING. SERVICED YELLOW HYD SERVER IAW MM 12-12-29 & REPLACED NR 2 ENG YELLOW HYD SYS PUMP HP FILTER IAW AMM 29-13-45. RAN NR 2 ENG & PERFORMED OPERATIONAL TEST OF YELLOW HYD SYS IAW MM 29-13-00-710-002.

Part: RESERVOIR — UNSERVICEABLE (EVAC SLIDE) · airframe 17,280 hrs · 5,745 cycles

WARNING MAINTENANCE STATUS MESSAGE SLIDE BOTTLE 2L. REPLACED L2 DOOR SLIDE INFLATION RESERVOIR IAW AMM 25-62-49-000-001-A & AMM 25-62-49-400-001-A.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 15,970 hrs · 5,290 cycles

DOOR L2 ASSIST BOTTLE LOW. SERVICED DOOR L2 ASSIST BOTTLE.

Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 15,551 hrs · 5,140 cycles

FLIGHT ATTENDANT REPORTED EXIT SIGN OVER DOOR 2L REMAINS ON DURING FLIGHT. FOUND 2L EMERGENCY EXIT SIGN OUT ON ARRIVAL. ACCOMPLISHED CIDS EMERGENCY POWER SUPPLY SYS TEST. OPERATED EMERGENCY LIGHTS, ALL TESTED OK IAW AMM 33-51-00-710-001A.

Part: HOUSING — UNSECURE (CABIN) · airframe 15,486 hrs · 5,111 cycles

EMERGENCY EXIT LIGHT HOUSING AT FWD PART OF DOOR 1L NEAR FLOOR IS NOT PROPERLY ATTACHED. SECURED LIGHT HOUSING BY 1L DOOR.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 15,086 hrs · 4,960 cycles

LENS COVER FOR EMERGENCY EXIT SIGN MISSING. REPLACED LENS COVER FOR EMERGENCY EXIT SIGN.

Part: RESERVOIR — INOPERATIVE (R2 DOOR SLIDE) · airframe 14,457 hrs · 4,750 cycles

R2 DOOR LOW SLIDE PRESSURE. R & R R2 DOOR SLIDE INFLATION RESERVOIR IAW AMM 25-62-49-400-001-A. TEARDOWN REPORT CONFIRMED FAILURE OF SLIDE INFLATION RESERVOIR.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 14,214 hrs · 4,667 cycles

EMERGENCY LIGHT AT FLOOR LEVEL, L1 DOOR COVER IS BROKEN. REPLACED COVER.

Part: LANYARD — OUT OF POSITION (L4 DOOR SLIDE) · airframe 14,163 hrs · 4,648 cycles

L4 DOOR NOT SHOWING ARMED ON ECAM. REPOSITIONED DOOR SLIDE LANYARD FOR ARMING LEVER.

Part: GUST LOCK — INOPERATIVE (R1 DOOR) · airframe 14,128 hrs · 4,637 cycles

GUST LOCK AT R1 DOOR INOPERATIVE. CLEANED GUST LOCK CONTROL MECHANISM AT DOOR 1R IAW AMM 52-10-00-100-801-A.

Part: GUST LOCK — DIRTY (R1 DOOR) · airframe 13,542 hrs · 4,438 cycles

GUST LOCK ON DOOR R1 INOPERATIVE. CLEANED GUST LOCK RELEASE SWITCH.

Part: DIAPHRAGM — DAMAGED (L4 DOOR) · airframe 13,051 hrs · 4,270 cycles

C11 CHECK - L4 DOOR ASSIST BOTTLE DEPLETED. REMOVED AND REPLACED DIAPHRAGM AND O-RING AT L-4 DOOR PERCUSSION MECHANISM AND SERVICED BOTTLE AND DAMPER REF A321 AMM 52-10-00-610-001.

Part: LENS — MISSING (CABIN) · airframe 13,046 hrs · 4,268 cycles

C11 CHECK - AFT REAR DOOR EMERGENCY EXIT LIGHT (KNEE LEVEL) COVER MISSING. INSTALLED LENS FOR EMERGENCY LIGHT AT AFT RIGHT ENTRY DOOR IAW A321 AMM 33-51-13.

Part: MECHANISM — STICKING (PAX DOOR) · airframe 13,046 hrs · 4,268 cycles

C11 CHECK - RIGHT FORWARD PASSENGER/CREW DOOR STAY MECHANISM WILL NOT LOCK DOOR IN THE FOIL OPEN POSITION. REMOVED CORROSION INHIBITING COMPOUND FROM DOOR MECHANISM AREA TO FREE UP STICKING LOCK MECHANISM IAW A321 AMM 52-10-00-100-801-A.

Part: CONNECTOR — BROKEN (CABIN) · airframe 12,539 hrs · 4,085 cycles

L3 DOOR OVERHEAD EMERGENCY LIGHT HAS A BROKEN CONNECTOR. REMOVED AND REPLACED BROKEN CONNECTOR.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 12,123 hrs · 3,941 cycles

MID SHIP STATION EMERGENCY FLASHLIGHT INOP. DOES NOT FLASH. REPLACED FLASHLIGHT BATTERY.

Part: LIGHT — DETACHED (CABIN) · airframe 11,609 hrs · 3,784 cycles

THE 24C EMERGENCY LIGHT HANGING TO THE GROUND. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AT 24C.

Part: LENS — BROKEN (EXIT SIGN) · airframe 11,353 hrs · 3,693 cycles

R4 EXIT SIGN BROKEN. REMOVED AND REPLACED R4 EMERGENCY EXIT LIGHT LENS COVER. OPS CHECKED GOOD.

Part: LENS — BROKEN (EXIT SIGN) · airframe 11,353 hrs · 3,693 cycles

DOOR L4 SMALL EXIT SIGN BROKEN. REMOVED AND REPLACED L4 EXIT SIGN LENS COVER. OPS CHECKED GOOD.

Part: CIDS — FAULTY (CABIN) · airframe 10,504 hrs · 3,425 cycles

APPROXIMATELY 30 MINUTES AFTER TAKEOFF, CREW RECEIVED INTERMITTENT ECAM WARNINGS FOR CARGO SMOKE, FORWARD AND AFT COMPARTMENTS. NO ASSOCIATED ODORS OR SENSOR WARNINGS. CREW ELECTED TO DO A PRECAUTIONARY LANDING AND DIVERTED TO ABQ BUT DECLARED AN EMERGENCY FOR LANDING. AIRCRAFT ARRIVED WITH MAINTENANCE STATUS MESSAGES FOR CIDS 1 AND SMOKE. UNABLE TO CLEAR CIDS 1 SO UNIT WAS REMOVED AND REPLACED. ALSO REPLACED OBRM AND RANG WIRES FOR CONTINUITY AND GROUND BETWEEN CIDS 1 & 2 WITH NO FAULTS FOUND.

Part: EXTINGUISHER — INOPERATIVE (CABIN) · airframe 10,457 hrs · 3,411 cycles

MID-CABIN HALON FIRE EXTINGUISHER AT L2 DOG HOUSE INOP. REMOVED AND REPLACED PORTABLE HALON FIRE EXTINGUISHER WITH NEW UNIT.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 9,425 hrs · 3,074 cycles

PILOT REPORT - 12 INCH CRACK IN FLOOR PANEL BETWEEN AT FR25, Y=0. REPLACED FLOOR PANEL BETWEEN AT FR25, Y=0 IAW A321 SRM 53-12-12-000-001-A.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 8,963 hrs · 2,910 cycles

RAMP REPORT - AFT BAG PIT FLOORBOARD 151GF DELAMINATED AT ENTRANCE BETWEEN FR52 TO FR56, S32R. REPLACED FLOOR PANEL 151GF IAW A321AMM 53-42-14.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 8,083 hrs · 2,585 cycles

MEGAPHONE REPORTED INOPERATIVE. MAINTENANCE REMOVED AND REPLACED MEGAPHONE AS REQUIRED.

Part: LENS — BROKEN (CABIN) · airframe 7,053 hrs · 2,224 cycles

EMERGENCY LIGHT LENS BROKEN AT L1 DOOR. MAINTENANCE REPLACED L1 DOOR EMERGENCY LIGHT LENS.

Part: FLOOR PANEL — DEFECTIVE (CABIN) · airframe 6,970 hrs · 2,195 cycles

FLT 0383 - FORWARD GALLEY FLOOR HAS TWO SOFT SPOTS IN FLOORING (IN FRONT OF OVENS). APPLIED DOUBLER REPAIR IN R-1 DOORWAY BEHIND (AFT) OF GALLEY IAW SRM 53-12-00 PG 215-217.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 6,330 hrs · 1,976 cycles

EE - MCO-PHX - AFT FLIGHT ATTENDANT EMERGENCY MEGAPHONE INOPERATIVE. REMOVED AND REPLACED MEGAPHONE.

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 4,074 hrs · 1,226 cycles

FLT 434 - LAS - EES - 3-R SLIDE BOTTLE PRESSURE LOW. MAINTENANCE REMOVED AND REPLACED SLIDE BOTTLE AT 3-R DOOR.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 4,074 hrs · 1,226 cycles

FLT 435 - LAS - EEL - EMERGENCY LIGHT SYSTEM TEST FAIL - EMERGENCY POWER SUPPLY UNIT 12WL FAULT. MAINTENANCE REMOVED AND REPLACED 12WL IAW AIRBUS MAINTENANCE MANUAL 33-51-38.

Part: RESERVOIR — LOW PRESSURE (EVAC SLIDE) · airframe 2,518 hrs · 756 cycles

FLT 192 - SAN - EES - 3R SLIDE LOW PRESSURE. MAINTENANCE REMOVED AND REPLACED 3R SLIDE INFLATION RESERVOIR IAW AIRBUS MAINTENANCE MANUAL 25-62-49.

Part: BATTERY — DISCHARGED (CABIN) · airframe 1,987 hrs · 600 cycles

FLT 574 - TPA - EEL - OPERATIONAL TEST OF EMERGENCY LIGHTS FAILED. FOUND EMERGENCY POWER SUPPLY UNIT 12WL FAULT. REPLACED POWER SUPPLY BATTERY IAW AIRBUS MAINTENANCE MANUAL 33-51-38.