N70020

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 30,038 hrs · 14,111 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY LIGHT BATTERY PACK FAIL TEST FWD L (10WL). MAINTENANCE REPLACED EPSU BATTERY, BITE TEST OK.IAW AMM 33-51-38.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 30,038 hrs · 14,111 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY LIGHT BATTERY PACK FAIL TEST EMR R (12WL). MAINTENANCE REPLACED EPSU BATTERY, BITE TEST OK.IAW AMM 33-51-38

Part: ACCUMULATOR — LOW PRESSURE (ZONE 200)

AIRCRAFT WAS NOT GROUNDED: R2 PASSANGER DOOR EMERGENCY CYLINDER ACCUMULATOR READS LOW. MAINTENANCE SERVICED R2 PASSANGER DOOR EMERGENCY CYLINDER ACCUMULATOR IAW AMM 52-10-00.

Part: CONNECTOR — MISINSTALLED (ZONE 200 - FUSE) · airframe 25,093 hrs · 11,517 cycles

AIRCRAFT IN BASE MANITENANCE: CEILING EMERGENCY LIGHT ABOVE 23ABC AND 23 DEF IS INOPERATIVE. MAINTENANCE FOUND THE CONNECTORS FOR THE LIGHT WERE NOT PROPERLY CONNECTED AND PROPERLY CONNECTED THE LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: STRAP — TORN (ZONE 800 - DOORS) · airframe 25,093 hrs · 11,517 cycles

AIRCRAFT IN BASE MAINTENANCE: L1 DOOR SLIDE RAFT HAS TORN PULL STRAPS ATTACHING CORDS. MAINTENANCE REPLACED SLIDE RAFT ASSEMBLY AS REQUIRED.

Part: STRAP — DETACHED (ZONE 800 - DOORS) · airframe 25,093 hrs · 11,517 cycles

AIRCRAFT IN BASE MAINTENANCE: R2 DOOR SLIDE RAFT PULL STRAP DETACHED. MAINTENANCE REPLACED SLIDE RAFT ASSEMBLY AS REQUIRED.

Part: BATTERY — NO TEST (ZONE 200 - FUSE) · airframe 23,619 hrs · 10,753 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 11WL BATTERY INOPERATIVE. MAINTENANCE REPLACED BATTERY FOR EMERGENCY POWER SUPPLY UNIT 11WL PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: POWER SUPPLY — NONE (ZONE 200 - FUSE) · airframe 22,694 hrs · 10,291 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT 10WL FAILED TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 10WL (AALA202210252101) AND BATTERY (AALA202210259052) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BATTERY — NONE (ZONE 200 - FUSE) · airframe 22,694 hrs · 10,291 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT 10WL FAILED TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 10WL (AALA202210252101) AND BATTERY (AALA202210259052) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: LIFE VEST — MISSING (ZONE 200 - FUSE) · airframe 22,553 hrs · 10,218 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANTS REPORT LIFE VEST MISSING FROM SEAT 20C. MAINTENANCE INSTALLED LIFE VEST AT SEAT 20C PER AMM 25-66-52.

Part: WINDOW — DELAMINATED (ZONE 200 - FUSE) · airframe 22,357 hrs · 10,118 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK RIGHT HAND FIXED WINDOW (7DG 2 ) HAS AREAS OF DELAMINATION. , BUBBLES, MULTIPLE SCRATCHES AND VERY DEEP CHIPS THROUGHOUT ENTIRE OUTSIDE WINDOW SURFACE AND THE LOWER BUS BAR HAS DISCOLORATION (BURNT) AND AREAS OS SEPARATION. REPLACED WINDOW PER AMM 56-11-12.

Part: NONE — NONE · airframe 22,357 hrs · 10,118 cycles

AIRCRAFT WAS GROUNDED: DURING TAKE OFF AND INTO CLIMB HAD DIRTY SOCK SMELL. SMELL DISSIPATED AFTER A COUPLE MINUTES. DURING DECENT, SMELL RETURNED WHEN ENGINE POWER INCREASED. ODOR WAS STRONG. STARTED APU AND TRANSFERRED THE BLEEDS TO APU. NOTICEABLE DECREASE IN ODOR ONCE PACKS WERE ON APU BLEED. **SUPPLEMENTAL REPORT WILL NE SUBMITTED** (OPEN)

Part: ENGINE — ODOR (ZONE 400 - NAC/P) · airframe 22,357 hrs · 10,118 cycles

AIRCRAFT WAS GROUNDED: DURING TAKE OFF AND INTO CLIMB HAD DIRTY SOCK SMELL. SMELL DISSIPATED AFTER A COUPLE MINUTES. DURING DECENT, SMELL RETURNED WHEN ENGINE POWER INCREASED. ODOR WAS STRONG. STARTED APU AND TRANSFERRED THE BLEEDS TO APU. NOTICEABLE DECREASE IN ODOR ONCE PACKS WERE ON APU BLEED. **SUPPLEMENTAL REPORT FOR AALA202209061398: MAINTENANCE ACCOMPLISHED SMOKE / ODOR / FUMES INITIAL TROUBLESHOOTING PER TASK CARD 26L00021001 AND MAINTENANCE FOUND EVIDENCE OF OIL AT THE 6:00 POSITION JUST BEHIND FAN AND TOWER SHAFT ON THE #1 ENGINE. ACCOMPLISHED ENGINE SMOKE ODOR FUMES TROUBLESHOOTING PER TASK CARD 26L00021005 WITH NO DEFECTS BEING REPORTED. ACCOMPLISHED DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM PER TASK CARD 26L00021004 WITH NO ODORS BEING NOTED. AIRCRAFT WAS DETERMINED TO BE OK FOR SERVICE. ** (CLOSED)

Part: BATTERY — NONE (ZONE 200 - FUSE) · airframe 22,054 hrs · 9,959 cycles

AIRCRAFT WAS NOT GROUNDED:M EMERGENCY POWER SUPPLY UNIT 10WL BATTERY FAULT MESSAGE NOTED DURING TESTING OF THE EMERGENCY LIGHTING SYSTEM. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.

Part: BATTERY — INOPERATIVE (ZONE 200 - FUSE) · airframe 21,668 hrs · 9,764 cycles

AIRCRAFT WAS NOT GROUNDED: DURING EMERGENCY POWER SUPPLY UNIT TEST PER AMM 33-51-00 FOUND CFDS FAULT, EMERGENCY POWER SUPPLY UNIT 13WL. FOUND EMERGENCY POWER SUPPLY UNIT 13WL BATTERY INOPERATIVE, REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.

Part: PRESSURE SWITCH — WARNING MESSAGE (FUEL SYSTEM) · airframe 17,670 hrs · 8,047 cycles

AIRCRAFT WAS GROUNDED. DURING CLIMB AN ENGINE 1 FUEL FILTER CLOG MESSAGE APPEARED AND AGAIN DURING CRUISE. THE AIRCRAFT DIVERTED TO MIA WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. REMOVED AND REPLACED FUEL DIFFERENTIAL PRESSURE SWITCH, PER AMM 73-34-15.

Part: WINDOW — DELAMINATED (R1) · airframe 17,488 hrs · 7,975 cycles

AIRCRAFT WAS GROUNDED. FLIGHT CREW REPORTS R1 WINDOW DELAMINATED ACROSS THE BOTTOM. REPLACED R1 WINDOW, AS REQURED.

Part: SWITCH — OUT OF POSITION (OUTFLOW VALVE) · airframe 17,461 hrs · 7,964 cycles

AIRCRAFT WAS NOT GROUNDED. THE VENT SKIN AIR OUTLET VALVE WAS PLACED ON MEL, DUE TO A FAULT MESSAGE AFTER TAKE OFF ON THE PREVIOUS FLIGHT. MAINTENANCE ACCOMPLISHED MEL PROCEDURES, AS REQUIRED FOR THE DEFFERAL. THE FOLLOWING FLIGHT THE AIRCRAFT WAS UNABLE TO BE PRESSURIZED AND MAINTENANCE FOUND THE SKIN AIR OUTLET VALVE DEACTIVIATION SWITCH IN THE ON POSITION AND RECONFIGURED THE SWITCH, PER THE PROCEDURES OUTLINED IN MEL 21-07 AND AMM 21-26-00. A SATISFACTORY GROUND PRESSURIZATION TEST WAS ACCOMPLISHED, PER AMM 05-53-00.

Part: SLIDE RAFT — DEFORMED (L1 DOOR) · airframe 16,606 hrs · 7,507 cycles

AIRCRAFT IN BASE MAINTENANCE: DEFORMATION ON DOOR SLIDE RAFT AT PASSENGER/CREW L1 DOOR BETWEEN FR 16 TO FR 20. REPLACED DOOR SLIDE RAFT AT PASSENGER/CREW L1 DOOR PER JOB CARD 26C83152008.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,606 hrs · 7,507 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND AFT DOOR CUT OUT LOWER SILL CENTER FITTING BETWEEN FR 66 AND FR 68 AT S23L. REPLACED CENTER FITTING PER SRM 51-42-11-801 AND DRAWING # D53480505.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,606 hrs · 7,507 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT DOOR CUT OUT LOWER SILL AT FR 68 AND S23R. REPAIRED SILL PER SRM 53-41-14-300-001 PRINCIPLE 7.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,606 hrs · 7,507 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT DOOR CUT OUT LOWER SILL CENTER FITTING BETWEEN FR 66 AND FR 68 AT S23R. REPLACED CENTER FITTING PER SRM 51-42-11 AND DRAWING # D53480505.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,606 hrs · 7,507 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT FR 54 AND +Y1292. REPAIRED SEAT TRACK IAW EA 306057.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 16,606 hrs · 7,507 cycles

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

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,606 hrs · 7,507 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK BETWEEN FR 12 TO FR 24 AT +Y254. REPLACED SEAT TRACK PER SRM 51-72-11 DRAWING # D53112816 AND D53110920.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · corrosion level 2 · airframe 16,606 hrs · 7,507 cycles

AIRCRAFT IN BASE MAINTENANCE: SHEAR PLATE CRACKED AND CORRODED BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-72-11. SUPPLEMENTAL REPORT, DEFECTIVE PART WAS FOUND TO BE CORRODED ALSO AND WAS CLASSIFIED AS A LEVEL 2. UPPDATED REPORT TO REFLECT THIS.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 16,606 hrs · 7,507 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON CABIN FLOOR PANEL 261DF. REPLACED FLOOR PANEL 261DF PER EA 306077.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 16,606 hrs · 7,507 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED AREA ON FLOOR PANEL 221EF AT FORWARD GALLEY AREA BETWEEN FR 16 TO FR 20 AND BETWEEN Y1292 TO Y254. INSTALLED MODIFIED FLOOR PANEL PER SRM 53-12-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 16,606 hrs · 7,507 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED AREA ON FLOOR PANEL 221DF AT FORWARD GALLEY AREA BETWEEN FR 16 TO FR 24 AND BETWEEN Y254 TO -Y254. INSTALLED MODIFIED FLOOR PANEL PER SRM 53-12-00.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 15,984 hrs · 7,225 cycles

AIRCRAFT NOT GROUNDED: REJECTED TAKEOFF 50-60 KNOTS - BRAKE TEMP HIGHEST 275C - LGA RUNAWAY 13 DUE TO "THRUST LEVERS NOT SET" ANNUNICATION. VISUALLY INSPECTED ALL TIRES AND BRAKES, FOUND NO DAMAGE AS IAW MCM-05-96-10 BRAKE TEMPS NOT MEET EXCEEDANCE OPS CKS NORMAL AS IAW AMM 32-42-00.

Part: UNKNOWN — NOISE (NLG) · airframe 15,412 hrs · 6,975 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS ON GEAR RETRACTION 3 SEPARATE TIMES BANGING NOISE FROM NOSE GEAR AREA THEN LG LGCIU FAULT ECAM MESSAGE. MAINTENANCE CHECKED TORQUE LINK GAPS, CHECKED FOR ANY LOOSE COMPONETS, LUBED ALL NLG FITTINGS AND CHECKED NLG SHOCK ABSORBER FLUID LEVEL AND CHARGE PRESSURE. ACCOMPLISHED NLG EXTENSION AND RETRACTION FUNCTIONAL TEST IAW AMM 32-31-00, 32-00-00. AND 07-11-00. NO DEFECTS NOTED AT TIME OF OPS CHECK.

Part: SLIDE — FAULTY (DOOR) · airframe 13,578 hrs · 6,069 cycles

DURING AN EMERGENCY LIGHT SYSTEM BITE TEST, RECEIVED CIDS 1 DEU-B FAULT 300RH1. REMOVED AND REPLACED THE NR 1 DOOR SLIDE IAW MCM 25-94-03. OPS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,578 hrs · 6,069 cycles

MAITENANCE FOUND THE FWD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED THE EMERGENCY LIGHT POWER SUPPLY 10WL IAW AMM 33-51-38.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,578 hrs · 6,069 cycles

MAINTENANCE FOUND THE EMERGENCY CEILING LIGHT ABOVE SEAT 1C-2C INOPERATIVE. REMOVED AND REPLACED THE EPSU IAW AMM 33-51-38. OPS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,578 hrs · 6,069 cycles

MAINTENANCE FOUND THE EMERGENCY LIGHT ON THE CEILING ISLE ABOVE SEAT 9C-10C INOPERATIVE. THE AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED THE EPSU IAW AMM 33-51-38. OPS CHECKED NORMAL.

Part: FEEDER CABLE — NO TEST (EMERGENCY LIGHTS) · airframe 13,474 hrs · 6,028 cycles

MAINTENANCE REPORTED THAT THE CABIN IN SEAT EMERGENCY LIGHTS AT 24C AND 25C WERE INOPERATIVE. THE AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED THE SEAT TO SEAT CABLE IAW AMM 25-21-61.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 13,474 hrs · 6,028 cycles

MAINTENANCE REPORTED THAT THE EPSU SYSTEM TEST RESULTED IN A FAILED POWER SUPPLY 10WL. REMOVED AND REPLACED THE EPSU IAW AMM 33-51-38-040. OPS TESTED GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 12,469 hrs · 5,557 cycles

SEAT EMERGENCY LIGHTS INOPERATIVE AT ROWS 14 AND 15. REPOSITIONED AND SECURED THE CONNECTOR FOR SEAT 15 EMERGENCY LIGHT ASSEMBLY. OPS CHECKED NORMAL IAW MM 33-51-07.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,469 hrs · 5,557 cycles

SEAT EMERGENCY LIGHTS INOPERATIVE, ROWS 14 AND 15. REPOSITIONED AND SECURED CONNECTOR FOR SEAT 14 EMERGENCY LIGHT ASSEMBLY. OPS CHECKED NORMAL IAW MM 33-51-07.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 10,543 hrs · 4,707 cycles

PERFORMED EMERGENCY POWER SUPPLY SYSTEM TEST, TEST FAILED. REPLACED EMERGENCY POWER SUPPLY IAW MM 33-51-38.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 8,801 hrs · 3,941 cycles

SEAT 2C WHITE EMERGENCY EXIT LIGHT INOPERATIVE. FOUND A BROKEN WIRE UNDER SEAT, REPAIRED THE WIRE IAW ESPM 20-43-11. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: SLIDE — OUT OF POSITION (R4 DOOR) · airframe 8,369 hrs · 3,761 cycles

FOUND THE R4 DOOR SLIDE BUSTLE OUT OF POSITION. REPLACED R4 DOOR SLIDE IAW AMM 25-62-44.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 7,570 hrs · 3,427 cycles

DELAMINATION ON AFT CARGO LOWER SLANT PANEL 151AE. REPLACED FLOOR PANEL 151AE IAW AMM 25-55-11. AIRCRAFT WAS GROUNDED.

Part: FLOOR PANEL — DELAMINATED (CARGO) · airframe 7,570 hrs · 3,427 cycles

DELAMINATION ON AFT CARGO LOWER SLANT PANEL 151EF. REPLACED FLOOR PANEL 151EF PER AMM 25-55-11. AIRCRAFT WAS GROUNDED.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 7,408 hrs · 3,355 cycles

DELAMINATION ON AFT CARGO ENTRY FLOOR PANEL, JUST FORWARD OF CARGO OPENING. APPROXIMATELY 24 INCHES BY 50 INCHES. MAINTENANCE REPLACED FLOOR PANEL 151VG PER AMM 53-42-14. AIRCRAFT WAS GROUNDED.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 7,408 hrs · 3,355 cycles

DELAMINATION ON AFT CARGO FLOOR BOARD AT CARGO DOOR ENTRY WAY. ENTRY WAY IS DELAMINATED APPROXIMATELY 24 INCHES BY 48 INCHES. MAINTENANCE REPLACED FLOOR PANEL 151ZG PER AMM 53-42-14. AIRCRAFT WAS GROUNDED.