N125UW

Part: BOTTLE — LEAKING (ZONE 800) · airframe 42,140 hrs · 23,511 cycles

AIRCRAFT WAS GROUNDED: L1 DOOR PRESSURE CAUTION ON FA PANEL. MAINTENANCE REPLACED L1 DOOR DAMPER ASSY IAW AMM 52-11-14.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 42,132 hrs · 23,505 cycles

AIRCRAFT WAS GROUNDED: L1 DOOR ACCUMULATOR REQUIRES SERVICING. MAINTENANCE SERVICED L1 DOOR IAW AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 42,095 hrs · 23,486 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 1L SHOWING AMBER ON FA CIDS PANEL INDICATING CHECK DOOR PRESSURE. MAINTENANCE SERVICED L1 DOOR DAMPER IAW AMM 52-10-00-614-001-A.

Part: POWER SUPPLY — FAULTED (ZONE 200) · airframe 41,734 hrs · 23,285 cycles

AIRCRAFT WAS NOT GROUNDED: DURING L1 SLIDE CHANGE FWD L EPSU FAULT. MAINTENANCE REPLACED FWD L EPSU IAW AMM 33-51-38.

Part: DOOR FRAME — LOOSE (ZONE 200) · airframe 41,447 hrs · 23,114 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR EXTREMELY DIFFICULT TO OPEN IN FLIGHT. DOOR FEELS LIKE IT IS BINDING ON THE BOTTOM. FLIGHT CREW FOUND LOOSE SCREW AT COCKPIT DOOR. MAINTENANCE TIGHTENED COCKPIT DOOR JAM SCREWS AMM 52-10-00.

Part: SLIDE — DAMAGED (ZONE 200) · airframe 39,422 hrs · 21,904 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND PASSENGER / CREW (L1) DOOR ESCAPE SLIDE COVER BUCKLE BROKEN. REPLACED L1 DOOR ESCAPE SLIDE ASSEMBLY PER JOB CARD 26L00025011.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 39,170 hrs · 21,740 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LH PASSENGER/CREW DOOR EMERGENCY CYLINDER/ACCUMULATOR PRESSURE IS BELOW LIMITS. CYLINDER/ACCUMULATOR PRESSURE FOUND BELOW 1700 PSI AT 25 DEGREESCELSIUS. RECHARGED AFT LH CYLINDER BOTTLE TO 1810 PSI IAW AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 39,170 hrs · 21,740 cycles

AIRCRAFT WAS NOT GROUNDED: AFT RH PASSENGER/CREW DOOR EMERGENCY CYLINDER/ACCUMULATOR PRESSURE IS BELOW LIMITS. CYLINDER/ACCUMULATOR PRESSURE FOUND BELOW 1700 PSI AT 25 DEGREESCELSIUS. RECHARGED AFT RH CYLINDER BOTTLE TO 1810 PSI IAW AMM 52-10-00.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 388,094 hrs · 21,055 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: CIDS1 FAULT FPEEPMS CROSS AISLE LT/ EPSU (13WL) AFT L. REINSTALLED LOOSE CONNECTORS AS REQUIRED AND ACCOMPLISHED SUCCESSFUL CHECK.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,094 hrs · 21,055 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: CIDS 1 FAULT EXIT SIGNS/ESPU (13WL) AFT L. REPLACED EPSU BATTERY.

Part: CHECK VALVE — DAMAGED (ZONE 400 - NAC/P) · airframe 33,613 hrs · 18,222 cycles

AIRCRAFT WAS GROUNDED: AT FL 360 IN CLEAR AIR HAD ENGINE 1 STALL. PERFORMED ECAM & QRH PROCEDURES. ENGINE 1 PERFORMANCE RETURNED TO NORMAL. MAINTENANCE FOUND THE SEALING SURFACE ON THE #1 ENGINE INLET PRESSURE CHECK VALVE DAMAGED AND REPLACED IT PER AMM 36-11-41. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO STALL INDICATION PRESENT DURING HIGH POWER RUN.

Part: APU — ODOR (ZONE 100 - FUSE) · airframe 33,563 hrs · 18,185 cycles

AIRCRAFT WAS GROUNDED: MUSTY SMELL NOTICED WHEN WE ARRIVED AT AIRCRAFT IN TPA. DISSIPATED WHILE ENROUTE AND CAME BACK STRONGER WHEN WE STARTED DESCENT. SMELL BECAME NOTICEABLY STRONGER DESCENDING THRU FL 250. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE APU. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: APU — ODOR (ZONE 100 - FUSE) · airframe 33,563 hrs · 18,185 cycles

AIRCRAFT WAS GROUNDED: MUSTY SMELL NOTICED WHEN WE ARRIVED AT AIRCRAFT IN TPA. DISSIPATED WHILE ENROUTE AND CAME BACK STRONGER WHEN WE STARTED DESCENT. SMELL BECAME NOTICEABLY STRONGER DESCENDING THRU FL 250. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE APU. **SUPPLEMENTAL REPORT FOR AALA202205315505: REPLACED APU PER TASK CARD 26L31049003** (CLOSED)

Part: SLIDE RAFT — SWOLLEN (ZONE 800 - DOORS) · airframe 33,452 hrs · 18,111 cycles

AIRCRAFT WAS GROUNDED: DOOR 1L GUST LOCK DIFFICULT TO ENGAGE AND DISENGAGE. MAINTENANCE FOUND THE L1 DOOR SLIDE SWOLLEN AND REPLACED IT PER TASK CARD 25-94-03. A SATISFACTORY OPERATIONAL CHECK OF THE GUST LOCK SYSTEM WAS ACCOMPLISHED.

Part: NONE — NONE · airframe 33,080 hrs · 17,866 cycles

AIRCRAFT WAS GROUNDED: BURNING AND DIRTY SOCK ODOR IN CABIN AND COCKPIT ON CLIMB OUT. FLIGHT DECLARED AN EMERGENCY AND DIVERTED TO BWI, LANDING SAFELY. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: O-RING — LEAKING (ZONE 300 - STABS) · airframe 33,080 hrs · 17,866 cycles

AIRCRAFT WAS GROUNDED: BURNING AND DIRTY SOCK ODOR IN CABIN AND COCKPIT ON CLIMB OUT. FLIGHT DECLARED AN EMERGENCY AND DIVERTED TO BWI, LANDING SAFELY. **SUPPLEMENTAL REPORT FOR AALA202203147690: ACCOMPLISHED SMOKE ODOR FUME JOB CARD 26L00021001, APU SMOKE ODOR FUME JOB CARD 26L00021002, DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM JOB CARD 26L00021004, AND APU LOAD COMPRESSOR CLEAN JOB CARD 26L31049009. FOUND OIL LEAKING FROM APU GEAR BOX TO BE SOURCE OF ODOR. REPLACED O-RING PER IPC 49-21-09-03.** (CLOSED)

Part: REGULATOR VALVE — FAULTY (ZONE 400 - NAC/P) · airframe 31,356 hrs · 16,846 cycles

AIRCRAFT WAS GROUNDED: AFTER TAKEOFF ENGINE 1 & 2 BLEEDS FAULTED AND WOULD NOT RESET. REMOVED AND REPLACED #1 AND #2 BLEED PRESSURE REGULATOR VALVES PER AMM 36-11-52-401 .

Part: POWER SUPPLY — INOPERATIVE (ZONE 200 - FUSE) · airframe 31,355 hrs · 16,845 cycles

AIRCRAFT WAS NOT GROUNDED: FAILED TEST OF EMERGENCY POWER SUPPLY UNIT. REMVOED AND REPLACED EMERGENCY POWER SUPPLY UNIT 10WL IAW AMM 33-51-00.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 31,355 hrs · 16,845 cycles

AIRCRAFT IN BASE MAINTENANCE: R1 DOOR SLIDE HITS AIRCRAFT AFTER INSTALLED. REPLACED SLIDE PER TASK CARD 26C84152006.

Part: STRINGER — CORRODED (ZONE 200 - FUSE) · corrosion level 2 · airframe 31,355 hrs · 16,845 cycles

AIRCRAFT IN BASE MAINTENANCE: STRINGER SURFACE CORROSION AT FR56 TO FR57 AND STR 43L. REMOVED CORRODED AREA AND INSTALLED SPLICE REPAIR ON STRINGER 43L REF EA 328889 AND REPAIR DRAWING R53470620 ISSUE F.

Part: PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 31,355 hrs · 16,845 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND IN COUNTER SINK HOLES ON FUEL PANEL 640HB LOCATED AT STA 13-14, STR 8-11. REPLACED FUEL PANEL 640HB PER SRM 57-27-11-283-002.

Part: PANEL — OUT OF TOLERANCE (RT WING FUEL) · airframe 31,355 hrs · 16,845 cycles

AIRCRAFT IN BASE MAINTENANCE: FASTENER HOLES ARE OBLONG ON FUEL PANEL 640KB AT RIB 15-16. REPLACED FUEL PANEL REF AMM 57-27-11.

Part: FLANGE — CRACKED (ZONE 200 - FUSE) · airframe 31,355 hrs · 16,845 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT FASTENER HOLE HAS A CRACK IN UPPER FLANGE OF RIGHT SIDE BOX BEAM AT FR43. CUT OUT DAMAGED AREA, INSTALLED FILLER AND NEW REINFORCING BRACKET FITTING REF EO 5315Y066.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 31,355 hrs · 16,845 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON FUEL PLATE LOCATED ON RIGHT WING RIBS 21-22, AND STR 8-12. 0.014 INCHES DEEP. REPLACED FUEL PLATE PER SRM 57-27-11.

Part: PANEL — CORRODED (RT WING) · airframe 31,355 hrs · 16,845 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION DAMAGE IN COUNTERSINK HOLES FOUND NEAR FUEL PANEL 640LB. REPLACED FUEL PANEL 640LB REF SRM 57-57-77-283-002.

Part: PANEL — CORRODED (ZONE 200) · airframe 31,355 hrs · 16,845 cycles

AIRCRAFT IN BASE MAINTENANCE: FOUND CORROSION ON FUEL 540NB PANEL AT RIBS 18-19 AND STR 8-11. REPLACED FUEL PANEL REF SRM 57-27-11.

Part: DOOR SILL — CORRODED (FRM 66) · corrosion level 2 · airframe 31,355 hrs · 16,845 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON L2 DOOR SILL AT FR66, Y1467 AND Z-500. CUT OUT DAMAGED AREA AND FABRICATED FILLER AND REPAIR ANGLE. INSTALLED REPAIR REF SRM 53-41-14-300-001 REPAIR PRINCIPLE 6.

Part: DOOR SILL — CORRODED (R2 DOOR) · corrosion level 2 · airframe 31,355 hrs · 16,845 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON R2 DOOR SILL CENTER SHAPE AT FR66, Z-500, AND Y-1292. REMOVED AND REPLACED R2 DOOR SILL CENTER SHAPE REF SRM 51-72-11.

Part: DOOR SILL — CORRODED (FRM 68) · airframe 31,355 hrs · 16,845 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON R2 DOOR SILL PLATE AT FR 68 AND -Y1292. REPAIRED DOOR SILL PLATE PER SRM 53-41-14 REPAIR PRINCIPLE 5.

Part: DOOR SILL — CORRODED (FRM 68 S23L) · airframe 31,355 hrs · 16,845 cycles

AIRCRAFT IN BASE MAINTENANCE: CORRODED AREA FOUND ON L2 DOOR SILL PLATE LOCATED AT STA FR68, STR 23L, AND WATERLINE Z-500. LENGTH = 1.25 INCHES, WIDTH = 0.75 INCHES, DEPTH = 0.030 INCHES. CUT OUT CORRODED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND REPAIR ANGLE PER SRM 53-41-14-300-001.

Part: COVER — DAMAGED (ESCAPE REEL) · airframe 31,271 hrs · 16,791 cycles

AIRCRAFT WAS NOT GROUNDED: OVERWING EXIT ESCAPE ROPE COVER DAMAGED AIRCRAFT RIGHT. REPLACED ESCAPE ROPE AIRCRAFT RIGHT SIDE.

Part: WIRE HARNESS — BROKEN (EMERGENCY LIGHTS) · airframe 29,845 hrs · 15,975 cycles

AIRCRAFT WAS GROUNDED. FOUND ROW 11 ABC HARNESS FOR EMERGENCY EXIT LIGHT IN AISLE BROKEN. REMOVED AND REPLACED SET HARNESS, PER ESPM 20-33-50.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 29,282 hrs · 15,606 cycles

AIRCRAFT NOT GROUNDED. AFT JUMP SEAT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT BATTERY PER AMM 25-65-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,277 hrs · 15,603 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN SEAT TRACK UPPER SURFACE CROWN BETWEEN FR 20 AND FR 24 AT RBL 30. REPAIRED SEAT TRACK PER EA 305776 AND SRM 53-11-15-300-003.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 29,277 hrs · 15,603 cycles

AIRCRAFT IN BASE MAINTENANCE: MAIN CABIN FLOOR PANEL #251LF DELAMINATED BETWEEN FR 51 TO FR 54. REPLACED CABIN FLOOR PANEL PER AMM 53-00-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,277 hrs · 15,603 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN OUTBOARD SEAT TRACK UPPER SURFACE CROWN BETWEEN FR 20 AND FR 24 AT RBL 51 REPAIRED SEAT TRACK PER SRM 53-11-15 AND EA # 305780.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 29,277 hrs · 15,603 cycles

AIRCRAFT IN BASE MAINTENANCE: MAIN CABIN AFT FLOOR PANEL #251FF DELAMINATED BETWEEN FR 51 TO FR 54. REPLACED FLOOR PANEL PER AMM 53-00-00.

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 28,681 hrs · 15,234 cycles

AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT, FLIGHT ATTENDANT SEAT, AT DOOR 1L DOES NOT TURN OFF. MAINTENANCE REPLACED FLASHLIGHT BATTERY PER STANDARD PRACTICES.

Part: APU — LEAKING (APU BAY) · airframe 28,320 hrs · 15,028 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS DIRTY SOCKS FUMES AFTER TAKEOFF FOR 20 MINUTES SUBSIDED AT CRUISE FL360 ODOR RETURNED ON DECENT. MAINTENANCE ACCOMPLISHED JOB CARD 26L00021001, FOUND APU LEAK CAUSING SOURCE OF SMELL. SUPPLEMENTAL INFORMATION: MAINTENANCE REMOVED AND REPLACED APU IAW JOB CARD 26L31049003. OPS CHECK LEAK CHECK GOOD. (CLOSED)

Part: APU — LEAKING (APU BAY) · airframe 27,284 hrs · 14,368 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS DIRTY SOCK SMELL THRU-OUT THE AIRCRAFT. MAINTENANCE FOUND OIL WETTING AT THE APU LOAD COMPRESSOR INLET, OIL IN THE AIR INTAKE AND OIL COMING FROM THE GEARBOX DRAIN.***SUPPLEMENTAL INFORMATION: MAINTENANCE REMOVED AND REPLACED APU IAW CARD 26L31049003. OPS AND LEAK CHECK GOOD.*** (CLOSED)

Part: GIRT BAR — DAMAGED (L1 DOOR SLIDE) · airframe 26,443 hrs · 13,857 cycles

R1 DOOR SLIDE, GIRT BAR DAMAGED. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE R1 DOOR GIRT BAR IAW JOB CARD 26L00025011.

Part: LENS — DAMAGED (CABIN) · airframe 25,334 hrs · 13,234 cycles

AIRCRAFT WAS NOT GROUNDED: ROW 13 AND 19 LEFTHAND EMERGENCY LIGHT LENS COVERS DAMAGED. MAINTENANCE REPLACED LIGHT LENS AND LED ASSEMBLY (SEE AALA201810179021) PER AMM 33-51-19-420-052-C.

Part: LENS — DAMAGED (CABIN) · airframe 25,334 hrs · 13,234 cycles

AIRCRAFT WAS NOT GROUNDED, ROW 13 AND 19 LEFTHAND EMERGENCY LIGHT LENS COVERS DAMAGED. MAINTENANCE REPLACED LIGHT LENS (SEE AALA201810179015) AND LED ASSEMBLY PER AMM 33-51-19-420-052-C.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 24,813 hrs · 12,920 cycles

DELAMINATED FLOOR PANEL 151AF IN THE AFT CARGO BAY. THE AIRCRAFT WAS GROUNDED. REPLACED THE FLOOR PANEL AMM 53-42-14-400-802A. OKAY FOR SERVICE.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 24,813 hrs · 12,920 cycles

DELAMINATED FLOOR PANEL 151GF IN THE AFT CARGO AREA. THE AIRCRAFT WAS GROUNDED. REPLACED THE FLOOR PANEL IAW AMM 53-42-14-400-802A. OKAY FOR SERVICE.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 23,731 hrs · 12,314 cycles

EMERGENCY LIGHT LENS AT THE R2 DOOR WAS FOUND LOOSE. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-13, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: SLIDE — DEFECTIVE (L1 DOOR) · airframe 23,074 hrs · 11,965 cycles

AIRCRAFT WAS NOT GROUNDED. L1 SLIDE/RAFT TOUCHING FUSELAGE. REMOVED & REPLACED L1 SLIDE/RAFT PER J/C 26L00025011.

Part: CIDS — FALSE INDICATION (FA) · airframe 22,678 hrs · 11,739 cycles

F/A CIDS PANEL SHOWS, CHECK L1 DOOR PRESSURE. RESET CIDS IAW AMM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 22,443 hrs · 11,596 cycles

SMALL EXIT LIGHT LENS FOR THE L1 DOOR FOUND BROKEN. REPLACED THE LENS IAW AMM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 22,232 hrs · 11,470 cycles

FWD F/A FLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT BATTERY, CHECKED OK.

Part: LENS — BROKEN (CABIN) · airframe 22,215 hrs · 11,458 cycles

AIRCRAFT WAS NOT GROUNDED. BROKEN EMERGENCY PATH LIGHT LENS AT SEATS 11C. REPLACED EMERGENCY PATH LIGHT ASSEMBLY PER AMM 33-50-00.

Part: LIGHT — BROKEN (CABIN) · airframe 22,215 hrs · 11,458 cycles

AIRCRAFT WAS NOT GROUNDED. BROKEN EMERGENCY PATH LIGHT LENS AT SEATS 17C. REPLACED EMERGENCY PATH LIGHT ASSEMBLY PER AMM 33-50-00.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 22,148 hrs · 11,418 cycles

LEFT AFT GALLEY FLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT BATTERY.

Part: SPAR — CRACKED (RT PYLON) · airframe 22,111 hrs · 11,396 cycles

CRACK ON RIGHT PYLON, AFT FIXED FAIRING UPPER SPAR BETWEEN RIBS 14 AND 15. REPAIRED THE SPAR IAW EA 272485A AND SRM 54-54-12. ACCOMPLISHED DVI PER NDT 51-90-00.

Part: SEAL — FAULTY (DOOR) · airframe 22,081 hrs · 11,383 cycles

DOOR PRESSURE MESSAGE INDICATED ON THE CIDS PANEL. REMOVED & REPLACED DOOR OPENING ASSIST MECHANISM SEALS IAW 52-10-00-610-001, LEAK CHECKED GOOD.

Part: APU — SMOKE · airframe 21,197 hrs · 10,914 cycles

INBOUND CREW REPORTED AFT CABIN SMOKE AND FUMES PASSING THROUGH 6,000 FT. PERFORMED TROUBLESHOOTING AND FOUND APU AS SOURCE OF ODOR. REMOVED AND REPLACED APU. AIRCRAFT WAS GROUNDED.

Part: STRUCTURE — CONTAMINATED (APU BAY) · airframe 21,126 hrs · 10,870 cycles

AIRCRAFT WAS GROUNDED. ACRID ODOR FROM TOP FL 180 TO LANDING AND GATE ARRIVAL. REPORTED BY FWD CABIN AND FWD GALLEY AREA. OBSERVED IN FLT DECK SUSPECT AIR COND/APU BLEED AIR. INSPECTED APU INTAKE PLENUM. FOUND SIGNIFICANT EVIDENCE OF OIL COLLECTION AT PLENUM FRAME CHANNEL, SHAFT AND SCREEN AREA. ACCOMPLISHED VISUAL INSPECTION OF APU FOR EXTERNAL OIL LEAKS, REF J/C 26L00021001. NO OIL LEAKS FOUND AT THIS TIME. MOC NOTIFIED REMOVED MEL 49-1B, C/N 1542C25.

Part: FILTER — ODOR · airframe 20,883 hrs · 10,739 cycles

DURING DESCENT, NOTICED FUMES IN COCKPIT THAT IRRITATED EYES, NOSE AND THROAT. FUMES WERE NOT AS STRONG IN THE CABIN BUT WERE MORE NOTICEABLE AFT OF OVER WING EXITS. NO EVIDENCE OF OIL LEAKING. REMOVED AND REINSTALLED THE AIR FILTERS IAW TASK 21-21-41. NO DEFECTS NOTED. AIRCRAFT WAS GROUNDED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 20,816 hrs · 10,706 cycles

AIRCRAFT GROUNDED. L2 LOWER EMERGENCY LIGHT LENS COVER MISSING. INSTALLED NEW LENS.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 20,816 hrs · 10,706 cycles

AIRCRAFT GROUNDED. R2 DOOR EMERGENCY LIGHT LENS BROKEN. REMOVED AND REPLACED THE LENS.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 20,642 hrs · 10,604 cycles

LENS MISSING FROM EMERGENCY EXIT MARKER LIGHTS AT L1 DOOR.INSTALLED LENS AT L1 DOOR EMERGENCY. MARKER LIGHTS PER AMM 33-51-13

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 20,642 hrs · 10,604 cycles

LENS MISSING FROM EMERGENCY EXIT SIGN LIGHT R4 DOORS. INSTALLED THE LENS IAW AMM 33-51-13, .

Part: SKIN — CORRODED (FRAME 69) · airframe 20,468 hrs · 10,517 cycles

CORROSION ON AFT LAVATORY OUTLET VENT SKIN , LOWER AFT VENT DUCT ATTACHMENT SCREW AT FRAME 69 PLUS 11 INCHES, BETWEEN STRINGER 31R AND 32R.. REPAIRED THE SKIN IAW SRM 53-41-11. AIRCRAFT WAS GROUNDED.

Part: COVER — MISSING (R2 DOOR) · airframe 19,598 hrs · 10,039 cycles

AIRCRAFT WAS NOT GROUNDED: 2-R DOOR MISSING EXIT LIGHT COVER. INSTALLED 2-R DOOR EXIT LIGHT COVER.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 18,901 hrs · 9,654 cycles

AIRCRAFT WAS NOT GROUNDED. FORWARD F/A FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT BATTERY AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 25-65-00.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 18,626 hrs · 9,519 cycles

AIRCRAFT WAS NOT GNDED. EMER POWER SUPPLY UNIT 10WL FAIL LIGHT ILLUMINATED. REPLACED EMER POWER SUPPLY UNIT 10WL & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38-00-001-1.

Part: ENGINE — LEAKING (NR 1) · airframe 18,197 hrs · 9,295 cycles

AIRCRAFT WAS GNDED. DURING DESCENT THE FLIGHT CREW REPORTED A DIRTY SOCK SMELL IN THE CABIN, RESULTING IN THE CREW RECEIVING MEDICAL EVALUATION. FOUND EVIDENCE OF OIL WETTING IN THE HPC SECTION OF THE NR 1 ENG. REPLACED IT IAW TASK CARD 26L40071001. A SATISFACTORY LEAK & OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ODORS BEING NOTED.

Part: REHEATER — ODOR (AC BAY) · airframe 18,191 hrs · 9,291 cycles

AIRCRAFT WAS GNDED. ON TAKEOFF OIL BURNING SMELL TURNED OFF NR 1 PACK SMELL WENT AWAY. FOUND LT PACK REHEATER HAD MOLD & DIRTY MUSTY SMELL. REPLACED IT IAW AMM 21-52-31-400-001-A. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECKS WITH NO ODORS BEING NOTED.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 17,614 hrs · 8,988 cycles

AIRCRAFT WAS GNDED. ELEC & BURNING PLASTIC ODORS DURING DESCENT THRU 10,000, LIGHT ODOR IN THE COCKPIT & FWD GALLEY, STRONGER ODOR IN AFT GALLEY. FLIGHT ATTENDANTS REPORTED IRRITATION TO EYES & THROAT. MX OPERATED ALL LIGHTS, GALLEY EQUIPMENT & CABIN COMPONENTS, COULD NOT DUPLICATE. ENG RUNS & PACKS PRODUCED NO ODORS.

Part: UNKNOWN — ODOR (CABIN) · airframe 17,608 hrs · 8,986 cycles

AIRCRAFT WAS GNDED. ELEC SMELL WITH LIGHT HAZE & WATER LEAKING FROM OVERHEAD COMPARTMENT WAS NOTED. ACFT RETURNED TO THE GATE. ACCOMPLISHED JC 26L00021001 & COULD NOT DUPLICATE ISSUE, NO DEFECTS NOTED AT THIS TIME. THE ACFT WAS RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,692 hrs · 8,481 cycles

1S CHECK, CORROSION ON FLOORBEAM AT FRAME 68 & Y1732. REPAIRED FLOORBEAM IAW SRM 53-41-14-201 REPAIR PRINCIPAL 5.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 13,649 hrs · 6,904 cycles

RON VISIT DELAMINATION ON FLOOR PANEL 222EF BETWEEN FRAME 16 TO 20, BETWEEN STRINGER 23R TO 23L & BETWEEN -Y765 TO -Y1292. REPLACED FLOOR PANEL 222EF IAW AMM 53-12-12.

Part: OIL SYSTEM — OVERSERVICED (NR 2 ENGINE) · airframe 13,645 hrs · 6,902 cycles

CREW RETURN TO GATE WITH OXYGEN MASK DONNED DUE TO A DIRTY SOCK SMELL AFTER ENG START, STRONG IN CABIN. ISOLATED SOURCE TO NR 2 ENG IAW JOB CARD 26L00021001. FINDINGS LIMITED TO OVER SERVICE OF NR 2 ENG OIL TANK. CORRECTED SAME & ACCOMPLISHED ECS DECONTAMINATION IAW JOB CARD 26L00021004.

Part: SLIDE RAFT — DEFECTIVE (L2 DOOR) · airframe 13,395 hrs · 6,782 cycles

PERFORMING EO 2514Y110 FOUND CONTACT BETWEEN THE SLIDE RAFT COVER AT DOOR L2 & THE FUSELAGE, NO DAMAGE FOUND. PLACED ON MONITOR, INSPECT EVERY 100 HRS, REPLACED SLIDE AT NEXT HEAVY CHECK. SUPPLEMENT, REPLACED L2 DOOR SLIDE IAW 26L00025011.

Part: SLIDE RAFT — DEFECTIVE (R2 DOOR) · airframe 13,395 hrs · 6,782 cycles

PERFORMING EO 2514Y110 FOUND CONTACT BETWEEN THE SLIDE RAFT COVER AT DOOR R2 & THE FUSELAGE, NO DAMAGE FOUND. PLACED ON MONITOR, INSPECT EVERY 100 HRS, REPLACED SLIDE AT NEXT HEAVY CHECK. SUPPLEMENT, REPLACED R2 DOOR SLIDE IAW 26C84252006.

Part: PLATE — OUT OF POSITION (EVAC SLIDE) · airframe 12,747 hrs · 6,459 cycles

LEFT OVERWING SLIDE STAINLESS PLATE OUT OF POSITION. REPOSITION LT OVERWING SLIDE STAINLESS PLATE IAW AMM 25-62-42.

Part: BLADE — DAMAGED (NR 1 ENGINE) · airframe 12,394 hrs · 6,280 cycles

HIGH VIBRATION ENG NR 1 DURING DESCENT N1 9.9 N2 NORMAL. ACCOMPLISHED BIRD STRIKE INSPECTION IAW JC 26L00005007. ACCOMPLISHED BORESCOPE INSPECTION IAW JC 26L40072006. FOUND BLADES 27, 28, 29 & 30 DAMAGED. R & R DAMAGED BLADES IAW TASK AMM 72-21-00-300-029A. PERFORMED OPERATIONAL VIBRATION CHECK IAW AMM 71-00-00-710-009B.

Part: LIGHT — MISSING (CABIN) · airframe 11,227 hrs · 5,644 cycles

EMERGENCY EXIT LIGHT COVER BY 3C MISSING. REPLACED EMERGENCY LIGHT ASSY SEAT 3C.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 10,906 hrs · 5,457 cycles

PORTABLE FLASHLIGHT UNDER "B" F/A JUMP SEAT IS NOT FLASHING. REPLACED BATTERY IN FLASHLIGHT.

Part: SLIDE RAFT — LOW PRESSURE (L2 DOOR) · airframe 10,252 hrs · 5,115 cycles

DURING ACCOMPLISHMENT OF WEEKLY CHECK, FOUND L2 DOOR SLIDE BOTTLE PSI LOW IN RED BAND. SLIDE IS REMOVED. REPLACED L2 DOOR SLIDE/RAFT.

Part: CONNECTOR — LOOSE (CABIN) · airframe 8,729 hrs · 4,328 cycles

EMERGENCY LIGHT TEST FAILED ON SLIDE CHANGE. FOUND LOOSE CONNECTOR ON L2 SLIDE. RECONNECTED CONNECTOR. OPERATIONAL CHECK GOOD.

Part: LENS — MISSING (CABIN) · airframe 7,410 hrs · 3,606 cycles

EMERGENCY EXIT LIGHT AT DOOR 2R MISSING LENS. REPLACED MISSING LENS AT 2R DOOR.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 1,992 hrs · 1,008 cycles

PHL - EES - FLIGHT ATTENDANT PANEL CIDS CAUTION, R1 SLIDE BOTTLE PRESSURE BETWEEN GREEN AND RED BAND. MAINTENANCE REMOVED AND REPLACED THE R1 SLIDE ASSEMBLY. SUPP WILL BE ISSUED UPON DETERMINATION OF MFG P/N & S/N.

Part: CYLINDER — LEAKING (R1 DOOR) · airframe 290 hrs · 132 cycles

FLT 803 - PHL-CUN - EMERGENCY EGRESS SYSTEM - CIDS R1 DOOR AMBER CHECK PRESSURE. REMOVED & REPLACED R-1 DOOR DAMPER ASSY PER AMM 52-11-14. OPERATIONAL CHECK WAS GOOD.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 266 hrs · 123 cycles

FLT 1788 - CLT - CHECK DOOR PRESSURE, DOOR R1 ON CIDS PANEL. MAINTENANCE SERVICED DOOR ASSIST BOTTLE AT R1 DOOR PER AIRBUS MAINTENANCE MANUAL 52-10-03-614-001.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 255 hrs · 115 cycles

FLT 816-CLT - EES - FLIGHT ATTENDANT CABIN SCREEN SHOWS MESSAGE CHECK SLIDE PRESSURE DOOR 1R (SLIDE PRESSURE SHOWS NORMAL AT THE DOOR SLIDE). MAINTENANCE SERVICED EMERGENCY OPERATING CYLINDER PER AIRBUS MAINTENANCE MANUAL 52-10-00-03-614.

Part: BOTTLE — LOW PRESSURE (L4 DOOOR) · airframe 247 hrs · 111 cycles

FLT 727 - DEN - EES - FLIGHT ATTENDANT PANEL - CHECK DOOR PRESSURE 4L. MAINTENANCE SERVICED 4L DOOR PER AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 201 hrs · 91 cycles

FLT 1800 - CLT - EES - DOOR BOTTLE 4R LOW. MAINTENANCE SERVICED DOOR ASSIST BOTTLE.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 195 hrs · 87 cycles

FLT 1551 - PIT - PHX - EMERGENCY EGRESS SYSTEM - 1R DOOR ASSIST BOTTLE LOW PRESSURE. SERVICED 1R DOOR ASSIST BOTTLE PER AMM 52-10-00-614-001.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 170 hrs · 73 cycles

FLT 1684 - CLT - EES - DOOR 4L CHECK PRESSURE MESSAGE ON FLIGHT ATTENDANT PANEL. MAINTENANCE SERVICED 4L DOOR ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 93 hrs · 39 cycles

FLT 1525 - BOS - CLT - EMERGENCY EQUIPMENT - R4 DOOR ASSIST BOTTLE LOW. SERVICED ASSIST BOTTLE PER AMM 52-10-00-03-614-001. OPERATIONAL CHECK WAS GOOD.