N103US

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST SYS) · airframe 66,156 hrs · 38,377 cycles

AIRCRAFT WAS NOT GROUNDED: R3 DOOR PRESSURE ASSIST LOW. SERVICED R3 DOOR PRESSURE.

Part: BOTTLE — LOW PRESSURE (L3 DOOR ASSIST) · airframe 66,156 hrs · 38,377 cycles

AIRCRAFT WAS NOT GROUNDED: L3 DOOR PRESSURE ASSIST LOW. SERVICED L3 DOOR PRESSURE ASSIST PER AMM 52-10-00.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 64,490 hrs · 37,276 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT DUE TO A LOUD ELECTRICAL ARCHING SOUND IN FLIGHT. RESET GALLEY AND CABIN SWITCH WITH MOC. SOUND WENT AWAY AFTER RESET AT ABOUT 26,000 FT. NO SMOKE NO FLICKERING NO ECAM MESSAGES NO CIRCUIT BREAKERS POPPED. NOISE CAME BACK LOUDER AT AROUND 4,000FT ON APPROACH THEN WENT AWAY AND EVERYTHING WAS NORMAL. THE AIRCRAFT LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: CONTACTOR — DEFECTIVE (ZONE 200 - FUSE) · airframe 64,490 hrs · 37,276 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT DUE TO A LOUD ELECTRICAL ARCHING SOUND IN FLIGHT. RESET GALLEY AND CABIN SWITCH WITH MOC. SOUND WENT AWAY AFTER RESET AT ABOUT 26,000 FT. NO SMOKE NO FLICKERING NO ECAM MESSAGES NO CIRCUIT BREAKERS POPPED. NOISE CAME BACK LOUDER AT AROUND 4,000FT ON APPROACH THEN WENT AWAY AND EVERYTHING WAS NORMAL. THE AIRCRAFT LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT FOR AALA202312195778: MAINTENANCE FOUND CONTACTOR 27XN WOULD RELAX INTERMITTENTLY WITHOUT COMMAND AND REPLACED IT PER AMM 24-51-55. A SATISFACTORY OPERATIONAL CHECK.** (CLOSED)

Part: FITTING — CRACKED (ZONE 100 - FUSE) · airframe 64,453 hrs · 37,249 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND MAIN LANDING GEAR DOOR ACTUATOR FORWARD FITING CRACKED AT KEEL BEAM RIB W10 AND FR 42. MAINTENANCE REPLACED FITTING PER EA 350064.

Part: PIN — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 63,965 hrs · 36,954 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY D DOOR HARD TO OPEN/CLOSE. MAINTENANCE ADJUSTED AFT LAVATORY D DOOR LOWER PIN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: GIRT BAR — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 63,645 hrs · 36,750 cycles

AIRCRAFT WAS NOT GROUNDED: 2L DOOR MADE METALLIC SOUND WHEN CLOSING / ARMING AND WAS DIFFICULT TO ARM. MAINTENANCE ADJUSTED THE GIRT BAR PER AMM 52-11-00 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: FAN — ODOR (ZONE 100 - FUSE) · airframe 62,830 hrs · 36,206 cycles

AIRCRAFT WAS GROUNDED: SMOKE AND ODOR REPORTED BY INFLIGHT CREW AT SEAT ROW 26 AFT INTO THE GALLEY. A BURNING RUBBER ODOR MOST NOTICABLE NEAR SIDEWALLS, STARTING SHORTLY AFTER TAKEOFF. MAINTENANCE ACCOMPLISHED TASK CARD 26L00021001 SMOKE/ ODOR FUMES TROUBLE SHOOTING AND FOUND AFT CARGO COMPARTMENT VENTILATION EXTRACTION FAN AT FAULT. REPLACED AFT CARGO COMPARTMENT VENTILATION EXTRACTION FAN PER AMM 21-28-54. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ODOR NOTED IN AIRCRAFT.

Part: BATTERY — NO TEST (ZONE 200 - FUSE) · airframe 62,535 hrs · 35,986 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING TEST OF PTP PANEL 110RH (NEXT TO FAP PANEL) RECEIVED "EPSU INT LOAD EMER R" MESSAGE. ON EPSU RH (12WL) SIDE "INTERIOR LIGHTS FAULT" IS ILLUMUNATED. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 12WL (AALA202303209220) AND BATTERY (AALA202303204015) PER AMM33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: POWER SUPPLY — NO TEST (ZONE 200 - FUSE) · airframe 62,535 hrs · 35,986 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING TEST OF PTP PANEL 110RH (NEXT TO FAP PANEL) RECEIVED "EPSU INT LOAD EMER R" MESSAGE. ON EPSU RH (12WL) SIDE "INTERIOR LIGHTS FAULT" IS ILLUMUNATED. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 12WL (AALA202303209220) AND BATTERY (AALA202303204015) PER AMM33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: AXLE — CORRODED (ZONE 700 - GEARS) · airframe 62,141 hrs · 35,732 cycles

AIRCRAFT WAS GROUNDED: DURING INSPECTION OF #3 MAIN AXLE PER EA 338915, FOUND STREAK AND SPOTS OF EXPOSED METAL BETWEEN THE THREE AND 8 O'CLOCK POSITION IN THE CHROME PLATING AND ADDITIONAL PITTING ON CHROME. IT WAS DETERMINED THAT THE DAMAGE WAS OUTSIDE THE ON WING REPAIRABLE LIMITS AND THE RIGHT HAND MAIN LANDING GEAR LOWER LEG / SHOCK ABSORBER ASSEMBLY WAS REPLACED PER TASK CARD 26L70032006.

Part: AXLE — CORRODED (ZONE 700 - GEARS) · airframe 62,141 hrs · 35,732 cycles

AIRCRAFT WAS GROUNDED: DURING INSPECTION OF # 4 MAIN AXLE PER EA 338915, FOUND SPOTS OF EXPOSED METAL BETWEEN FIVE AND 10 O'CLOCK POSITIONS IN THE CHROME PLATING AND ADDITIONAL PITTING ON CHROME. IT WAS DETERMINED THAT THE DAMAGE WAS OUTSIDE THE ON WING REPAIRABLE LIMITS AND THE RIGHT HAND MAIN LANDING GEAR LOWER LEG / SHOCK ABSORBER ASSEMBLY WAS REPLACED PER TASK CARD 26L70032006.

Part: CONTROL SERVO — NONE (ZONE 600 - RH WI) · airframe 61,444 hrs · 35,333 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING POST HEAVY MAINTENANCE TEST FLIGHT THE AIRCRAFT ROLLS RIGHT WHEN AUTOPILOT DISENGAGED. APROXIMATELY 1-2 DEGREES. MAINTENANCE ACCOMPLISHED TSM 27-10-00-810-842-A AND REPLACED #1 ELEVATOR AILERON COMPUTER (ELAC) PER AMM 27-93-34-400-001-A. (AALA202210178865). REPLACED RIGHT WING AILERON INBOARD SERVO CONTROL ACTUATOR 33CE2 (AALA202210171606) AND LEFT WING AILERON OUTBOARD SERVO CONTROL ACTUATOR 33CE3 (AALA202210175454) PER AMM 27-14-51-400-001-A.

Part: CONTROL SERVO — NONE (ZONE 500 - LH WI) · airframe 61,444 hrs · 35,333 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING POST HEAVY MAINTENANCE TEST FLIGHT THE AIRCRAFT ROLLS RIGHT WHEN AUTOPILOT DISENGAGED. APROXIMATELY 1-2 DEGREES. MAINTENANCE ACCOMPLISHED TSM 27-10-00-810-842-A AND REPLACED #1 ELEVATOR AILERON COMPUTER (ELAC) PER AMM 27-93-34-400-001-A. (AALA202210178865). REPLACED RIGHT WING AILERON INBOARD SERVO CONTROL ACTUATOR 33CE2 (AALA202210171606) AND LEFT WING AILERON OUTBOARD SERVO CONTROL ACTUATOR 33CE3 (AALA202210175454) PER AMM 27-14-51-400-001-A.

Part: NONE — NONE (ZONE 100 - FUSE) · airframe 61,444 hrs · 35,333 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING POST HEAVY MAINTENANCE TEST FLIGHT THE AIRCRAFT ROLLS RIGHT WHEN AUTOPILOT DISENGAGED. APROXIMATELY 1-2 DEGREES. MAINTENANCE ACCOMPLISHED TSM 27-10-00-810-842-A AND REPLACED #1 ELEVATOR AILERON COMPUTER (ELAC) PER AMM 27-93-34-400-001-A. (AALA202210178865). REPLACED RIGHT WING AILERON INBOARD SERVO CONTROL ACTUATOR 33CE2 (AALA202210171606) AND LEFT WING AILERON OUTBOARD SERVO CONTROL ACTUATOR 33CE3 (AALA202210175454) PER AMM 27-14-51-400-001-A.

Part: SWITCH — INTERMITTENT (ZONE 200 - FUSE) · airframe 61,443 hrs · 35,332 cycles

AIRCRAFT IN BASE MAINTENANCE: EVACUATION COMMAND SWITCH INTERMITTENT. REPLACED EVACUATION PUSH BUTTON SWITCH (3WP) AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER ESPM 20-45-11 AND AMM 23-73-00.

Part: FITTING — CRACKED (ZONE 700 - GEARS) · airframe 61,443 hrs · 35,332 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND AFT MAIN LANDING GEAR DOOR ACTUATOR FORWARD FITTING BETWEEN FR 42 AND FR 43 AT S42R. REPLACED FITTING PER EA 338751.

Part: WINDOW — DELAMINATED (ZONE 200 - FUSE) · airframe 61,443 hrs · 35,332 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK LEFT HAND FIXED WINDOW DELAMINATED. REPLACED WINDOW PER AMM 56-11-12.

Part: BOLT — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 61,443 hrs · 35,332 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION RIGHT WING SLAT TRACK #6 LOWER AFT BOLT AT WS 6132 AND RIB 11. REPLACED BOLT PER AMM 27-84-64-400-002.

Part: BOLT — WORN (ZONE 500 - LH WI) · airframe 61,443 hrs · 35,332 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING #4 SPOILER HINGE BOLT HAS WORN THREADS. REPLACED HINGE BOLT PER AMM 27-64-44.

Part: BEARING — CORRODED (ZONE 400 - NAC/P) · corrosion level 2 · airframe 61,443 hrs · 35,332 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING PYLON AFT SHACKLES UPPER SLEEVE WAS HARD TO REMOVE FOR INSPECTION. MAINTENANCE FOUND THE PYLON REAR ATTACHMENT BEARING CORRODED AT PYLON STATION 8293 AND RIB 10. REPLACED BEARING PER AMM 57-26-12.

Part: SEAL — MISSING (ZONE 800 - DOORS) · airframe 61,443 hrs · 35,332 cycles

AIRCRAFT IN BASE MAIN_MISSING DOOR DAMPER CYLINDER ACCUMULATOR GAGE SEAL DOOR 842 AT AFT GALLEY AREA (1 EACH). REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PASSENGER CREW DOOR 842 AT AFT GALLEY AREA (1 EACH) IN ACCORDANCE WITH AMM 52-13-14-400-001-B. **SUPPLEMENTAL REPORT FOR AALA202209075968: CHANGES MADE TO SECTION 5 AND 5 ADDING SPECIFIC PART INFORMATION AND COMPONENT INFORMATION**

Part: CYLINDER — INADEQUATE (ZONE 800 - DOORS) · airframe 61,443 hrs · 35,332 cycles

AIRCRAFT IN BASE MAINTENANCE: MISSING DOOR DAMPER CYLINDER ACCUMULATOR GAGE SEAL DOOR 842 AT AFT GALLEY AREA (1 EACH). REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PASSENGER CREW DOOR 842 AT AFT GALLEY AREA (1 EACH) IN ACCORDANCE WITH AMM 52-13-14-400-001-B.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 61,443 hrs · 35,332 cycles

AIRCRAFT IN BASE MAINTENACE: CORROSION LEFT WING SLAT TRACK 3 LOWER BOLT (ECCENTRINC). REPLACED BOLT PER AMM 27-84-63-400-002.

Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 61,443 hrs · 35,332 cycles

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

Part: NONE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 61,443 hrs · 35,332 cycles

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

Part: FITTING — CRACKED (ZONE 100 - FUSE) · airframe 61,443 hrs · 35,332 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND MAIN LANDING GEAR DOOR ACTUATOR FITTING AT FR 43 BETWEEN S41R AND S42R. REPLACED ACTUATOR FITTING PER EA 338751.

Part: FRAME — CRACKED (ZONE 200 - FUSE) · airframe 61,443 hrs · 35,332 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FR 68 AND S22R AT THE RIGHT HAND DOOR STOP FITTING #1. REPAIRED FRAME PER SRM 53-41-12-300-011

Part: NONE — CRACKED (ZONE 200 - FUSE) · airframe 61,443 hrs · 35,332 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING CRACKED BETWEEN FR 1 AND FR 2 AT Y0. REPLACED CONTINUITY FITTING PER EO 5319Y017-002.

Part: FRAME — CRACKED (ZONE 100 - FUSE) · airframe 61,443 hrs · 35,332 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FR 43 BETWEEN S21L AND S22L REPLACED FRAME PER EA 338568

Part: NONE — CRACKED (ZONE 200 - FUSE) · airframe 61,443 hrs · 35,332 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING CRACKED BETWEEN FR 1 AND FR 2 AT Y0. REPLACED CONTINUITY FITTING PER EO 5319Y017-002.

Part: LENS — MISSING (ZONE 200 - FUSE) · airframe 60,580 hrs · 34,834 cycles

AIRCRAFT WAS NOT GROUNDED: LENS COVER MISSING OFF OF EMERGENCY EXIT LIGHT SEAT 1C. INSTALLED MISSING LENS COVER PER AMM 33-51-19. OPERATIONAL CHECK NORMAL.

Part: APU — LEAKING (ZONE 100) · airframe 59,522 hrs · 34,211 cycles

AIRCRAFT WAS GROUNDED: ON APPROACH SMELLED OIL/FUMES IN FLIGHT DECK. MAINTENANCE FOUND OIL COMING FROM THE APU LOAD COMPRESSOR DRAIN CAVITY DURING THE INITIAL TROUBLESHOOTING . **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: OIL SYSTEM — LEAKING (APU) · airframe 59,522 hrs · 34,211 cycles

AIRCRAFT WAS GROUNDED: ON APPROACH SMELLED OIL/FUMES IN FLIGHT DECK. MAINTENANCE FOUND OIL COMING FROM THE APU LOAD COMPRESSOR DRAIN CAVITY DURING THE INITIAL TROUBLESHOOTING . REPLACED APU AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER TASK CARD 26L31049003.

Part: LOCK — FAULTY (ZONE 900 - LAV/G) · airframe 59,182 hrs · 34,011 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY DOOR AFT RIGHT SIDE, HAS COM OFF ITS HINGE. REPLACED DOOR LOCK ASSEMBLY PER AMM 25-45-21.

Part: HINGE FITTING — EXCESS PLAY (LT ELEVATOR) · airframe 58,541 hrs · 33,613 cycles

AIRCRAFT WAS GROUNDED: LEFT HAND ELEVATOR #1 HINGE FITTING FAILS FREE PLAY CHECK DUE TO EXCESSIVE PLAY. REPLACED HINGE FITTING PER EO 5518Y004.

Part: FITTING — CRACKED (DOOR ACTUATOR) · airframe 1 hrs · 1 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND MAIN LANDING GEAR DOOR AFT ACTUATOR FITTING CRACKED AT 2ND FROM TOP FASTENER HOLE. REPLACED FITTING PER EA 328335.

Part: FITTING — CRACKED (MLG ACTUATOR) · airframe 58,513 hrs · 33,596 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND MAIN LANDING GEAR DOOR AFT ACTUATOR FITTING CRACKED AT 2ND FROM TOP FASTENER HOLE. REPLACED FITTING PER EA 328335.**SUPPLEMENTAL REPORT TO ADD CORRECT AIRCRAFT TIMES AND CYCLES TO SECTION 3**

Part: BATTERY — INOPERATIVE (AFT FLASHLIGHT) · airframe 58,156 hrs · 33,377 cycles

AIRCRAFT WAS NOT GROUNDED: AFT RIGHT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED BATTERY IN FLASHLIGHT ON AFT RIGHT FLIGHT ATTENDANT JUMPSEAT PER AMM 25-56-00.

Part: UNKNOWN — UNKNOWN (FLIGHT CONTROLS) · airframe 57,344 hrs · 32,929 cycles

AIRCRAFT WAS GROUNDED. WHEN SPEED BRAKE WAS USED & FLAPS 2, 180 KNOTS AIRCRAFT WENT INTO A 5-10 DEGREE BANK. HAPPENED AT 9000 FEET AND AGAIN AT 4000 FEET. NO ECAM MESSAGES DISPLAYED DUE TO A UNCOMMANDED ROLL INCIDENT. TROUBLESHOT, REF TSM 27-10-00-810-842-A, NO FAULTS.

Part: AUTOTHRUST SYS — DISCONNECTED · airframe 55,542 hrs · 31,756 cycles

AIRCRAFT NOT GROUNDED: 2 TIMES ALL AUTOMATION DISCONNECTS + GOES INTO THRUST LOCK. PERFORMED TSM TASK 22-31-00-810-816-A.

Part: COOLING FAN — LEAKING (APU) · airframe 54,918 hrs · 31,351 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS DIRTY SOCK FUME SMELL IN AIRCRAFT. MAINTENANCE ACCOMPLISHED JOB CARD 26L00021001. FOUND APU OIL COOLER LEAKING. ***SUPPLEMENTAL INFORMATION: MAINTENANCE REMOVED AND REPLACED APU OIL COOLING FAN IAW AMM 49-57-51. OPS AND LEAK CHECKS GOOD.*** (CLOSED)

Part: LENS — MISSING (CABIN) · airframe 54,600 hrs · 31,149 cycles

AIRCRAFT WAS NOT GROUNDED: FLOOR PATH LIGHTING LENS MISSING AT ROW 13C. MAINTENANCE REPLACED LENS PER MM 33-50-00.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 54,036 hrs · 30,832 cycles

AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT AT 2L FLIGHT ATTENDANT JUMP SEAT INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT PER ATA 25-23-00.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 53,366 hrs · 30,443 cycles

AIRCRAFT NOT GROUNDED: MULTIPLE INFORMATION RELATED TO FMGC MISSING ON CA'S SIDE. RESET CIRCUIT BREAKERS FOR BOTH FMGC. PERFORMED OPERATIONAL TEST IAW AMM 22-83-34. OPS CHECK GOOD.

Part: WINDOW — MISSING (ASSIST BOTTLE) · airframe 51,950 hrs · 29,594 cycles

R1 DOOR ASSIST GAUGE VIEWING WINDOW MISSING. AIRCRAFT WAS GROUNDED. REPLACED THE DOOR ASSIST GAUGE VIEWING WINDOW IAW AMM 52-11-00.

Part: COVER — MISSING (ASSIST HANDLE) · airframe 51,761 hrs · 29,500 cycles

L1 DOOR ASSIST HANDLE COVER MISSING. REPLACED THE HANDLE COVER IAW AMM 52-10-00. OK FOR SERVICE.

Part: FLASHLIGHT — FAULTY (CABIN) · airframe 50,793 hrs · 28,972 cycles

AIRCRAFT WAS NOT GROUNDED. AFT FLIGHT ATTENDANT DIRECT VIEW FLASHLIGHT OPERATIVE BUT LED DOES NOT FLASH. REPLACED AFT FLIGHT ATTENDANT DIRECT VIEW FLASHLIGHT.

Part: BATTERY — FAULTY (MASTER) · airframe 50,264 hrs · 28,661 cycles

AIRCRAFT WAS GROUNDED. FLIGHT DIVERTED DUE TO A BATTERY ISSUE. EMERGENCY DECLARED. FLIGHT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 50,257 hrs · 28,657 cycles

MISSING EMERGENCY LIGHT LENS AT SEAT 4C. INSTALLED NEW THE LENS AT SEAT 4C IAW AMM 33-51-18 AND PERFORMED SUCCESSFUL OPS CHECKS.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 50,074 hrs · 28,563 cycles

F/A REPORTED THAT THE AISLE EMERGENCY LIGHT LENS WAS DAMAGED ON SEAT 4C. REMOVED AND REPLACED EMERGENCY LIGHT LENS. OPS CHECKED GOOD IAW AMM 35-51-18.

Part: SLIDE — NO TEST (L2 DOOR) · airframe 49,961 hrs · 28,505 cycles

L2 DOOR, EMERGENCY BATTERY FAILED TO TEST DURING SLIDE CHANGE, SHOWED FAULT EPSU EXT LOAD AFT LT. REMOVED AND REPLACED LEFT AFT SLIDE. OPS CHECKED GOOD.

Part: FLOORBOARD — DELAMINATED (AFT CARGO BAY) · airframe 49,861 hrs · 28,453 cycles

DELAMINATION ON THE AFT CARGO BAY FLOORBOARD 151DF. REPLACED FLOORBOARD IAW AMM 53-42-14.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 49,861 hrs · 28,453 cycles

DELAMINATION ON AFT CARGO FLOOR PANEL 151GF. REPLACED THE FLOOR PANEL IAW AMM 53-42-14.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 49,804 hrs · 28,421 cycles

LIGHT LENS DETACHED. INSTALLED THE EMERGENCY LIGHT LENS.

Part: CONNECTOR — DIRTY (LANDING LIGHT)

LANDING LIGHT MESSAGE DISAGREES WITH AIRCRAFT CONFIGURATION RIGHT SIDE ONLY, STAYS EXTENDED UNTIL RECYCLED. CLEANED THE CONNECTOR ON RIGHT LANDING LIGHT. OPERATIONAL CHECKED GOOD IAW AMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 49,030 hrs · 27,973 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR 2R EMERGENCY EXIT SIGN COVER MISSING. REPLACED EMERGENCY EXIT LIGHT LENS AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 48,869 hrs · 27,898 cycles

L1 DOOR EMERGENCY EXIT LIGHT MISSING THE LENS. INSTALLED THE LENS IAW AMM 33-51-13-400-001-A, LIGHT OPS CHECKED OK.

Part: PIN — CORRODED (RT MLG) · airframe 48,815 hrs · 27,872 cycles

CORROSION ON RIGHT MAIN GEAR REAR PINTLE PIN. REPLACED PINTLE PIN PER CARD 26T00032001.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 1 FUEL PUMP) · airframe 48,749 hrs · 27,834 cycles

CENTER NR 1 PUMP FAULT. OPS CHECK OF THE CENTER FUEL PUMP, CHECKED GOOD IAW AMM 28-21-51.

Part: ENGINE — FAULTED (NR 2) · airframe 48,192 hrs · 27,526 cycles

NR 2 ENGINE STALL ECAM MESSAGE AT INITIAL CLIMB LEVEL OFF AT 32,000 FT. MESSAGE APPEARED THREE TIMES WITH ENGINE BANGS. PAX REPORTED SEEING FLASH. RECOVERED BACK TO NORMAL OPS. REMOVED AND REPLACED THE ENGINE. AIRCRAFT GROUNDED.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 48,033 hrs · 27,463 cycles

EXIT LENS OVER THE RT AFT SERVICE DOOR FOUND BROKEN. INSTALLED A NEW LENS.

Part: GIRT BAR — OBSTRUCTED (R2 DOOR SLIDE) · airframe 48,020 hrs · 27,454 cycles

R2 DOOR VERY HARD TO ARM AND DISARM. REMOVED OBSTRUCTION FROM GIRT BAR.

Part: SLIDE RAFT — BULGED (L2 DOOR) · airframe 47,450 hrs · 27,139 cycles

AIRCRAFT WAS NOT GROUNDED: L2 DOOR SLIDE BULGING WHICH IS PREVENTING THE SLIDE BUSTLE FROM FITTING PROPERLY OVER THE SLIDE. MAINTENANCE REPLACED THE SLIDE ASSEMBLY PER TASK CARD 26L00025011.

Part: STRUCTURE — CRACKED (EMERGENCY EXIT) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON LOAD TRANSMITTING PROFILE SEGMENT AT EMERGENCY EXIT DOOR 834, AFT POSITION IN PASSENGER CABIN. REPLACED LOAD TRANSMITTING PROFILE SEGMENT PER EA 264342 AND EO 5210Y228.

Part: PIN — WORN (RT MLG) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. WEAR ON RIGHT HAND MAIN LANDING GEAR, OUTBOARD ACTUATOR RETRACTION PIN. REPLACED PIN PER AMM 32-31-46.

Part: SLIDE RAFT — DEFORMED (ZONE 800) · airframe 47,235 hrs · 27,048 cycles

AIRCRAFT IN BASE MAINTENANCE. DEFORMATION ON FORWARD GALLEY SLIDE RAFT PASSENGER CREW DOOR 831, WHEN DOOR IS FULL OPEN SLIDE RAFT TOUCH THE FUSELAGE. REPLACED SLIDE RAFT PER AMM 25-62-44-400-007-A.

Part: SLIDE RAFT — DEFORMED (ZONE 800) · airframe 47,235 hrs · 27,048 cycles

AIRCRAFT IN BASE MAINTENANCE. DEFORMATION ON AFT GALLEY SLIDE RAFT PASSENGER CREW DOOR 842, WHEN DOOR IS FULL OPEN SLIDE RAFT TOUCH THE FUSELAGE. REPLACED SLIDE RAFT PER AMM 25-62-44-400-803-A.

Part: SLIDE RAFT — DEFORMED (ZONE 800) · airframe 47,235 hrs · 27,048 cycles

AIRCRAFT IN BASE MAINTENANCE. DEFORMATION ON FORWARD GALLEY SLIDE RAFT PASSENGER CREW DOOR 841, WHEN DOOR IS FULL OPEN SLIDE RAFT TOUCH THE FUSELAGE. REPLACED SLIDE RAFT PER AMM 25-62-44-400-803-A.

Part: BOLT — CORRODED (LE SLAT) · corrosion level 2 · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND WING SLAT TRACK NR 5 LOWER BOLT BETWEEN RIB 9-10. REPLACED LOWER BOLT PER AMM 27-84-64-400-002-A.

Part: BOLT — CORRODED (TE FLAP) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT WING TRACK NR 4 OUTBOARD FLAP PIVOT BOLT. REPLACED PIVOT BOLT PER AMM 27-54-62.

Part: BOLT — CORRODED (TE FLAP) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT WING TRACK NR 3 OUTBOARD FLAP PIVOT BOLT. REPLACED PIVOT BOLT PER AMM 27-54-62.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY COVER FITTING AT FR 68 AND STRINGER 23L. REPLACED COVER FITTING PER SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY CORNER FITTING AT STRINGER 23R AND FR 68. REPLACED CORNER FITTING PER SRM A320 51-72-11 AND DWG D53480019.

Part: FLAP — EXCESS PLAY (RT WING) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON RIGHT HAND WING OUTBOARD FLAP. REPLACED OUTBOARD FLAP PER AMM 27-54-62.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BAE MAINTENANCE. CRACK INDICATIONS ON LEFT HAND SIDE BOX BEAM FLANGE 2 HOLE FITTINGS. REPAIRED SIDE BOX BEAM PER EO 5315Y066.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. TRAPPED WATER INDICATION ON RIGHT HAND ELEVATOR UPPER SKIN PANEL AT TWO LOCATIONS 6" FROM FASTENER LEADING EDGE BETWEEN RIB 7-9. REPAIRED UPPER SKIN PANEL PER SRM 55-21-11-300-005.

Part: STRIKER — OUT OF ADJUST (PAX DOOR) · airframe 47,234 hrs · 27,047 cycles

PASSENGER CREW DOOR FINGER AND STRIKER LEVER DAMPER MECHANISM IS OUT OF ADJUSTMENT. MAINTENANCE PROPERLY ADJUSTED IAW AMM 52-13-14-820-002-A.

Part: PLATE — CRACKED (FUSELAGE) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK INDICATION ON LEFT HAND SIDE CENTER WING BOX (2) HOLES 1'' AND 2'' FORWARD OF FRAME 43. REPLACED PRESSURE PLATE PER SRM 51-72-11.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK INDICATIONS ON LEFT HAND SIDE BOX BEAM FLANGE HOLE FITTINGS AT STRINGER 24R AND FR 43. REPAIRED SIDE BOX BEAM PER EO 5315Y066.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 47,234 hrs · 27,047 cycles

LEFT ELEVATOR NR 6 HINGE ARM FITTING AT RIB 13 HAS EXCESSIVE PLAY. REPLACED HINGE ARM FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 47,234 hrs · 27,047 cycles

LT ELEVATOR NR 3 HINGE ARM FITTING BETWEEN RIB 7-8 HAS EXCESSIVE PLAY. REPLACED THE HINGE ARM FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 47,234 hrs · 27,047 cycles

LEFT ELEVATOR NR 2 HINGE ARM FITTING BETWEEN RIB 6-7 HAS EXCESSIVE PLAY. REPLACED HINGE ARM FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 47,234 hrs · 27,047 cycles

RIGHT ELEVATOR NR 6 HINGE ARM FITTING AT RIB 13 HAS EXCESSIVE PLAY. REPLACED HINGE ARM FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 47,234 hrs · 27,047 cycles

LEFT ELEVATOR NR 1 HINGE ARM FITTING AT RIB 5 HAS EXCESSIVE PLAY. REPLACED THE HINGE ARM FITTING IAW AMM 55-16-42.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD CARGO COMPARTMENT SHEAR TIE AT FR 34 BETWEEN STRINGERS 41L AND 42L. REPLACED SHEAR TIE PER SRM 51-72-11 AND DRAWING D532 31712.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD CARGO COMPARTMENT CLEAT AT FR 33 BETWEEN STRINGER 42L AND STRINGER 43L. REPLACED CLEAT PER SRM 51-72-11.

Part: STRUCTURE — CRACKED (EMERGENCY EXIT) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON LOAD TRANSMITTING PROFILE SEGMENT AT EMERGENCY EXIT DOOR 833 FORWARD POSITION IN PASSENGER CABIN. REPLACED LOAD TRANSMITTING PROFILE SEGMENT PER EA 264342 AND EO 5210Y228.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SILL BEAM, INTERNAL STRUCTURE AT STRINGER 38R BETWEEN FR 60 AND FR62. REPLACED SILL BEAM PER SRM 51-72-11 AND 53-41-49-300-02.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 47,234 hrs · 27,047 cycles

LEFT ELEVATOR NR 5 HINGE ARM FITTING AT RIB 10 HAS EXCESSIVE PLAY. REPLACED HINGE ARM FITTING IAW AMM 55-16-42.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD GALLEY LOWER SILL FITTING AT STRINGER 23R BETWEEN FR 16 AND FR 20. REPLACED FITTING PER SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATION ON FORWARD GALLEY FLOOR PANEL 222EF. REPLACED FLOOR PANEL PER SRM 53-02-00 AND IRM 9701 REV G.

Part: COUPLING — DAMAGED (FUSELAGE) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLE ON AFT GALLEY COUPLING AT STRINGER 23R AND FR 66. REPLACED COUPLING PER SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON FORWARD GALLEY FLOOR PANEL 221EF. REPLACED FLOOR PANEL PER SRM 53-12-00-300-006 FIGURE 20106 AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON FORWARD GALLEY FLOOR PANEL 221PF. REPLACED FLOOR PANEL PER SRM 53-12-00 AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT GALLEY FLOOR PANEL 261PF. REPLACED FLOOR PANEL PER SRM 53-02-00 AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON FORWARD GALLEY FLOOR PANEL 221DF. REPLACED FLOOR PANEL PER SRM 53-12-00 AND IRM 9701 REV G.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD GALLEY LOWER SILL BETWEEN FR 16 AND FR 20 AT STRINGER 23L. REPLACED LOWER SILL PER SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT GALLEY FLOOR PANEL 261DF. REPLACED FLOOR PANEL PER SRM 53-02-00, IRM 9701 REV G AND EA 264132.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT GALLEY FLOOR PANEL 261BG. REPLACED FLOOR PANEL PER SRM 53-02-00 AND IRM 9701 REV G.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. TRAPPED WATER INDICATION ON LEFT HAND ELEVATOR UPPER SKIN PANEL AT 3 PLACES LOCATED 6" TO 13" FROM LEADING EDGE BETWEEN RIB 1-7; AND 2 PLACES LOCATED 6.5' TO 12' FROM TRAILING EDGE BETWEEN RIB 2-7. REPAIRED UPPER SKIN PANEL PER SRM 55-21-11-300-005.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY LOWER SILL AT STRINGER 23R BETWEEN FR 66 AND FR 68. REPLACED LOWER SILL PER SRM 51-72-11 AND EA 264153.

Part: DOOR SILL — DAMAGED (FUSELAGE) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLES ON AFT GALLEY LOWER SILL AT STRINGER 23R BETWEEN FR 66 AND FR 68. REPLACED LOWER SILL PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT -Y765 BETWEEN FR 21 AND FR24. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING D53110900.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT GALLEY FLOOR PANEL 261AG. REPLACED FLOOR PANEL PER SRM 53-02-00 AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED FORWARD GALLEY FLOOR PANEL 222CF. REPLACED FLOOR PANEL PER SRM 53-12-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT GALLEY FLOOR PANEL 262BG. REPLACED FLOOR PANEL PER EA 264130 AND SRM 53-02-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOOR BEAM AT -Y464.8 AND STRINGER 23L, BETWEEN FR 66 AND FR 70. REPLACED FLOOR BEAM PER SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-70) · corrosion level 2 · airframe 47,234 hrs · 27,047 cycles

CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 68 AND 70, +Y160.5. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53472800.

Part: COUPLING — DAMAGED (FUSELAGE) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLE ON AFT GALLEY UPPER INBOARD SPLICE COUPLING AT STRINGER 23L AND FR 66. REPLACED COUPLING PER SRM 51-72-11 AND DWG D53474250.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY FLOORBEAM AT FR 66 AND -Y318. REPLACED FLOORBEAM PER SRM A320 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD GALLEY SEAT TRACK AT -Y1292 BETWEEN FR 12 AND FR 24. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING D53112812.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON PASSENGER CABIN FLOOR PANEL 251DF. REPLACED FLOOR PANEL PER SRM 53-02-00 AND IRM 9701 REV G.

Part: COUPLING — DAMAGED (FUSELAGE) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLE AT AFT GALLEY UPPER OUTBOARD SPLICE COUPLING AT STRINGER 23L AND FR 66. REPLACED COUPLING PER SRM 51-72-11 AND DWG D53474250.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD GALLEY WEB AT FR 20 AND STRINGER 23R. REPLACED WEB PER SRM 51-72-11 AND DRAWING NR D53114392.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY LOWER SILL AT STRINGER 23L BETWEEN FR 66 AND FR 68. REPLACED LOWER SILL PER SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT Y765 BETWEEN FR 12 AND FR24. REPLACED SEAT TRACK PER SRM 51-72-11.

Part: HINGE FITTING — DAMAGED (NLG DOOR) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLES ON RIGHT HAND NOSE LANDING GEAR DOOR AFT HINGE FITTINGS. REPLACED HINGE FITTINGS PER CMM 52-82-32 AND AMM 32-22-13.

Part: HINGE FITTING — DAMAGED (NLG DOOR) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLES ON RIGHT HAND NOSE LANDING GEAR DOOR FORWARD HINGE FITTINGS. REPLACED HINGE FITTINGS PER CMM 52-82-32 AND 32-22-13.

Part: HINGE FITTING — DAMAGED (NLG DOOR) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLES ON LEFT HAND NOSE LANDING GEAR DOOR FORWARD HINGE FITTINGS. REPLACED HINGE FITTINGS PER CMM 52-82-32 AND 32-22-13.

Part: HINGE FITTING — DAMAGED (NLG DOOR) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLES ON LEFT HAND NOSE LANDING GEAR DOOR AFT HINGE FITTINGS. REPLACED HINGE FITTINGS PER CMM 52-82-32 AND AMM 32-22-13.

Part: HINGE FITTING — DAMAGED (NLG DOOR) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLES ON RIGHT HAND NOSE LANDING GEAR DOOR AFT HINGE FITTINGS. REPLACED HINGE FITTINGS PER CMM 52-82-32 AND AMM 32-22-13.

Part: HINGE FITTING — DAMAGED (NLG DOOR) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLES ON LEFT HAND NOSE LANDING GEAR DOOR AFT HINGE FITTINGS. REPLACED HINGE FITTINGS PER CMM 52-82-32 AND AMM 32-22-13.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 151CF. REPLACED FLOOR PANEL PER SRM 53-02-00 AND IRM 9701 REV G.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON VERTICAL STABILIZER RUDDER HINGE ARM NR 5 BEARING. REPLACED HINGE FITTING PER AMM 55-36-41 AND SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED AFT CARGO COMPARTMENT FLOOR PANEL 151EF. REPLACED FLOOR PANEL PER SRM 53-02-00 AND IRM 9701 REV G.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON VERTICAL STABILIZER RUDDER HINGE ARM NR 7 BEARING. REPLACED HINGE FITTING PER SRM 51-42-11.

Part: HINGE FITTING — EXCESS PLAY (VERTICAL STAB) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON VERTICAL STABILIZER HINGE ARM FITTING NR 3 BEARING. REPLACED HINGE ARM FITTING NR 3 PER AMM 55-36-41-0401 AND SRM 51-72-11-401.

Part: HINGE FITTING — EXCESS PLAY (VERTICAL STAB) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON VERTICAL STABILIZER HINGE ARM FITTING NR 1 BEARING. REPLACED HINGE ARM FITTING NR 1 PER SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 151RF. REPLACED FLOOR PANEL PER SRM 53-02-00 / IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 151LF. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REV G.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK INDICATION ON FORWARD CARGO COMPARTMENT PRESSURE DECK AT FR 36 BETWEEN Y1292 AND Y1523. REPAIRED PRESSURE DECK PER EA 263899.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON NR 4 RUDDER HINGE ARM FITTING. REPLACED HINGE ARM FITTING PER SRM 51-72-11 AND AMM 55-36-41-400-001-A.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 152CF. REPLACED FLOOR PANEL PER SRM 53-02-00 AND IRM 9701 REV G.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON RIGHT HAND FORWARD CARGO COMPARTMENT PRESSURE DECK AT FR 36 BETWEEN -Y1292 AND -Y1523. REPAIRED PRESSURE DECK PER EA 263900.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON FORWARD CARGO COMPARTMENT FLOOR PANEL 131FF BETWEEN FR 28 AND FR 31, AND BETWEEN -Y765 AND -Y1353. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 152FF. REPLACED FLOOR PANEL PER SRM 53-02-00 AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 47,234 hrs · 27,047 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 151QF. REPLACED FLOOR PANEL PER SRM 53-02-00 AND IRM 9701 REV G.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 46,334 hrs · 26,570 cycles

AIRCRAFT WAS NOT GNDED. FLASHLIGHT AT FWD ENTRANCE NEEDS TO BE REPLACED. R & R FLASHLIGHT BATTERY IAW AMM 25-60-10.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 46,215 hrs · 26,511 cycles

AIRCRAFT WAS NOT GNDED. LT CTR EMER POWER SUPPLY IS INOPERATIVE. R & R EMER POWER SUPPLY IAW AMM 33-51-38 PB 0401. OPERATIONAL CHECKED NORMAL.

Part: CHANNEL — CRACKED (NR 1 PYLON) · airframe 45,543 hrs · 26,173 cycles

AIRCRAFT WAS GNDED. NR 1 ENG PYLON HAT CHANNEL CRACKED ON INBD SIDE, UNDER PANEL 413CL, FWD UPPER CORNER OF PANEL. NR 1 ENG PYLON WEB, CHANNEL, R & R IAW SRM 51-42-11 & DWG 52, D54630485.

Part: BATTERY — DISCHARGED (CABIN) · airframe 44,795 hrs · 25,719 cycles

EMERGENCY LIGHTING OPERATIONAL TEST IAW AMM 33-51-00-710-001-A, PRODUCES EPSU BATTERY FWD LT FAILURE MSG. REPLACED POWER SUPPLY UNIT 10WL BATTERY. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-00-810-802-A & 53-51-38.

Part: BUSHING — LOOSE (LT MLG DOOR)

BUSHING IN FWD LUG OF ACTUATOR ATTACH FITTING ON DOOR IS LOOSE IN FITTING. REPLACED LT MLG DOOR IAW AMM 52-81-00. REFER TO MX NON-ROUTINE 26-0553-8-0722 005, SN 18 FOR INFORMATION OF WORK ACCOMPLISHED.

Part: PROXIMITY SENSOR — DEFECTIVE (NLG) · airframe 43,557 hrs · 25,011 cycles

FLIGHT 1870 EN-ROUTE, AFTER ROTATION, THE FLIGHT CREW HEARD A UN-NORMAL CLUNK. THE GEAR HANDLE WAS PLACED UP. THE GEAR INDICATORS SHOWED GREEN SOLID ALL 3 & FLASHING RED ON NOSE & RT MAIN GEAR. ALSO, A GEAR UNSAFE ECAM MSG CAME ON. THE CREW TRIED CYCLING THE GEAR, BUT WAS UNSUCCESSFUL. THE FLIGHT DECLARED AN EMER, RETURNED & DID A FLYBY OF THE TOWER TO CONFIRM THAT THE GEAR WAS DOWN. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. REPLACED NLG EXTENSION PROXIMITY SENSOR 25GA. PERFORMED A GEAR SWING & FUNCTIONAL CHECKS WITH NO ABNORMAL INDICATIONS OR NOISE NOTED.

Part: SLIDE — UNSECURE (L2 DOOR) · airframe 42,283 hrs · 24,320 cycles

2L DOOR SLIDE PACK FELL OFF DOOR EN ROUTE. REINSTALLED ASSEMBLY AS REQUIRED.

Part: O-RING — WORN (RT ENGINE) · airframe 41,944 hrs · 24,155 cycles

FLIGHT ATTENDANT & TWO PAXS NOTICED AN ODOR, BOTH GOT LIGHT HEADED AS WELL. ACCOMPLISHED JOB CARD 26L00021005 CABIN ODOR TROUBLESHOOT. REPLACED RT ENG LPT SHAFT PLUG O RINGS IAW AMM TASK 72-55-00-960-002A. ACCOMPLISHED JOB CARD 26L00021004 DECONTAMINATION OF THE ECS ENGS & APU.

Part: COVER — BROKEN (RUDDER PEDAL) · airframe 41,125 hrs · 23,789 cycles

AT TOUCHDOWN RUDDER PEDALS JAMMED. TRAVELLING APPROX 1/2 MILE, FORCIBLY PUSHING ON PEDALS PRODUCED A MECHANICAL CRUNCH SOUND FOLLOWED BY NORMAL PEDAL OPERATION. FOUND PLASTIC COVER FOR FIRST OFFICERS PEDAL POSITION ADJUSTER BROKEN & INTERFERING WITH PEDAL TRAVEL. REPLACED SAME IAW AMM 27-21-43-400-002-A.

Part: OXYGEN BOTTLE — LEAKING (CREW O2) · airframe 40,847 hrs · 23,655 cycles

FLIGHT DIVERTED TO MIA DUE TO CREW O2 LEAKING DOWN TO 640 PSI INFLIGHT. REPLACED O2 BOTTLE IAW AMM 35-11-41 PB 0401. NO LEAKS NOTED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 40,110 hrs · 23,279 cycles

C11 CHECK, LT SIDE CABIN EMERGENCY LIGHTS WILL NOT TEST IAW WEEKLY CHECK. REPLACED LT SIDE CABIN EMERGENCY POWER SUPPLY UNIT.

Part: SCREW — LOOSE (EVAC SLIDE) · airframe 40,032 hrs · 23,237 cycles

RIGHT OVERWING SLIDE HAS LOOSE SCREW. RE-TORQUED RT OVERWING SLIDE SCREW IAW A320 SRM 5149-00.

Part: ATTACH FITTING — LACK OF LUBE (GIRT BAR) · airframe 39,727 hrs · 23,067 cycles

DOOR 2L HARD TO ARM & DISARM. LUBED LOWER GIRT BAR ATTACHMENT.

Part: BRAKE — MALFUNCTIONED (LE SLAT) · airframe 39,493 hrs · 22,946 cycles

FLIGHT CONTROL SLAT LOCKED WING TIP BRAKE ON. REPLACED LT SLAT WING TIP BRAKE, 35CV, IAW A320 AMM 27-81-51. OPERATIONS CHECKED GOOD, NO LEAKS NOTED.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 39,300 hrs · 22,834 cycles

CARGO FLOOR PANEL 151MF CRACKED. R & R FLOOR PANEL IAW AMM 53-42-14-400-001A.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 39,300 hrs · 22,834 cycles

CARGO FLOOR PANEL 151GF DELAMINATED. R & R FLOOR PANEL IAW AMM 53-42-14-400-001A.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 39,300 hrs · 22,834 cycles

CARGO FLOOR PANEL 131FF HAS ONE CRACK. REPAIRED FLOOR PANEL IAW SRM 53-02-00, P/B 101.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 39,300 hrs · 22,834 cycles

CARGO FLOOR PANEL 151QF CRACKED. REPAIRED FLOOR PANEL IAW SRM 53-02-00, P/B 101.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 39,300 hrs · 22,834 cycles

CARGO FLOOR PANEL 152RF CRACKED. REPAIRED FLOOR PANEL IAW SRM 53-02-00, P/B 101.

Part: LENS — MISSING (CABIN) · airframe 37,515 hrs · 21,845 cycles

ROW 3 EMERGENCY FLOOR PATH LIGHTING LENS MISSING. REPLACED ROW 3 EMERGENCY FLOOR PATH LIGHTING LENS AS REQUIRED.

Part: LENS — MISSING (CABIN) · airframe 37,515 hrs · 21,845 cycles

ROW 13 EMERGENCY FLOOR PATH LIGHTING LENS MISSING. REPLACED ROW 13 EMERGENCY FLOOR PATH LIGHTING LENS AS REQUIRED.

Part: LENS — MISSING (CABIN) · airframe 37,515 hrs · 21,845 cycles

AFT RIGHT DOOR EXIT LIGHT LENS MISSING. REPLACED LENS AS REQUIRED AT AFT RIGHT DOOR.

Part: SLAT — STUCK (WING) · airframe 37,417 hrs · 21,797 cycles

CREW REPORTED THE SLATS BECAME STUCK IN THE FIRST POSITION AFTER REQUESTING FLAPS 1. FLAPS RESPONDED AND WORKED NORMALLY WITH THE SLATS STUCK. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. SUP WILL BE PROVIDED AFTER COMPLETION OF CORRECTIVE ACTION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,273 hrs · 21,730 cycles

EMERGENCY LIGHT SYSTEM TEST FAILED DUE TO EXTERNAL POWER SUPPLY UNIT (EPSU) INTERNAL LOAD FAULT TASK 33-51-00-710-001A. RELAMPED CABIN EXIT MARKING AND LOCATION SIGNS AS REQUIRED RESTORING EPSU MEMORIZED INTERNAL LOADS. CABIN EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECKS SATISFACTORY REFERENCE AIRBUS A/M/M 33-51-00-710-009-A AND 33-51-00-710-001-A.

Part: SEAL — LEAKING (APU) · airframe 37,182 hrs · 21,684 cycles

THERE IS AN ODOR ON THE AIRCRAFT WITH APU ON OR OFF AND BOTH ENGINES ON. ODOR REMAINED WITH BLEEDS OFF DURING DE-ICE. ALSO HAD STATUS MESSAGE ON ECAM "ONE PACK ONLY IF WAI ON". BLEED PAGE NORMAL. MAINTENANCE REMOVED AND REPLACED THE APU. LOAD COMPRESSOR SEAL DETERMINED TO BE ROOT CAUSE OF FAILURE.

Part: OVEN — ODOR (GALLEY)

FORWARD FLIGHT ATTENDANTS REPORTED MODERATE ELECTRICAL SMELL IN FORWARD GALLEY. DIVERTED BACK TO CLT AFTER REPORTS OF BREATHING ISSUES. FOUND OVEN IN FORWARD GALLEY CAUSING ODOR. REMOVED AND REPLACED THE OVEN.

Part: OVEN — DEFECTIVE (GALLEY) · airframe 36,168 hrs · 21,106 cycles

FORWARD FLIGHT ATTENDANT REPORTED A MODERATE ELECTRICAL SMELL IN THE FORWARD GALLEY SHORTLY AFTER TAKEOFF. FLIGHT DECK CREW NOTICED A SLIGHT SMELL AFTER TAKEOFF THAT QUICKLY DISSIPATED. ALL THREE F/A'S REPORTED BREATHING DIFFICULTIES SO THE FLIGHT RETURNED TO CLT. THERE WERE NO PASSENGER COMPLAINTS. MAINTENANCE FOUND THE OVEN IN THE FORWARD GALLEY TO BE THE CAUSE OF THE SMELL. OVEN WAS REMOVED AND REPLACED IAW AIRBUS MAINTENANCE MANUAL 25-35-19-400-003-A.

Part: RESERVOIR — LOW PRESSURE (EVAC SLIDE) · airframe 36,080 hrs · 21,052 cycles

CIDS CAUTION LIGHT FOR LEFT WING SLIDE RESERVOIR PRESSURE LOW. MAINTENANCE REMOVED AND REPLACED LEFT WING SLIDE RESERVOIR BOTTLE IAW AIRBUS MAINTENANCE MANUAL 25-62-46-400-001-A.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 35,696 hrs · 20,842 cycles

MULTIPLE SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED MID-CABIN POWER SUPPLY UNIT IAW AIRBUS MAINTENANCE MANUAL 33-51-38.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 35,516 hrs · 20,748 cycles

SEAT MOUNTED EMERGENCY EXIT LIGHTS ROWS 3, 7, 15, 20-24 AND 26 INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY UNIT IAW AIRBUS MAINTENANCE MANUAL 33-51-38.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 34,268 hrs · 20,112 cycles

AFT JUMPSEAT EMERGENCY FLASHLIGHT INOPERATIVE. INSTALLED NEW BATTERY IN AFT JUMPSEAT EMERGENCY FLASHLIGHT.

Part: GIRT BAR — DIRTY (L2 DOOR) · airframe 33,908 hrs · 19,909 cycles

THE 2L EMERGENCY EXIT DOOR DIFFICULT TO ARM. CLEANED AND LUBED 2L DOOR GIRT BAR.

Part: LENS — MISSING (CABIN) · airframe 33,518 hrs · 19,714 cycles

TWO FLOOR LEVEL EMERGENCY LIGHT COVERS IN FIRST CLASS MISSING. REPLACED LIGHT COVERS.

Part: BALL LOCK — OBSTRUCTED (EVAC SLIDE) · airframe 33,096 hrs · 19,508 cycles

FAA SAFETY INSPECTOR FOUND THE FOLLOWING UPON PREFLIGHT, 'ESCAPE SLIDE BALL LOCKS PAINTED OVER'. MAINTENANCE REMOVED PAINT AS REQUIRED PER ENGINERING ORDER EO2508Y025, REV 'A'.

Part: SLIDE — FAILED (SERVICE DOOR) · airframe 33,073 hrs · 19,494 cycles

AFT RIGHT SERVICE DOOR SLIDE FAILED EMERGENCY LIGHT TEST. MAINTENANCE REPLACED AFT RIGHT DOOR SLIDE (R2).

Part: WIRE HARNESS — MISROUTED (R1 DOOR) · airframe 32,725 hrs · 19,343 cycles

LAX - EES - ELECTRICAL HARNESS MISROUTED ON R-1 DOOR ESCAPE SLIDE RAFT PACK. REROUTED ELECTRICAL HARNESS ON R-1 DOOR ESCAPE SLIDE RAFT PACK IAW AMM 25-62-44-400-007-0.

Part: WIRE HARNESS — MISROUTED (R2 DOOR) · airframe 32,725 hrs · 19,343 cycles

LAX - EES - ELECTRICAL HARNESS MISROUTED ON R-2 DOOR ESCAPE SLIDE RAFT PACK. REROUTED ELECTRICAL HARNESS ON R-2 DOOR ESCAPE SLIDE RAFT PACK.IAW AMM 25-62-44-400-007-0.

Part: WIRE HARNESS — DISCONNECTED (L2 DOOR) · airframe 32,725 hrs · 19,343 cycles

LAX - EES - ELECTRICAL HARNESS NOT CONNECTED ON L-2 DOOR ESCAPE SLIDE RAFT. RECONNECTED ELECTRICAL HARNESS ON L-2 DOOR ESCAPE SLIDE RAFT PACK IAW AMM 25-62-44-400-007-0.

Part: WIRE HARNESS — MISROUTED (L1 DOOR) · airframe 32,725 hrs · 19,343 cycles

LAX - EES - ELECTRICAL HARNESS MISROUTED ON L-1 DOOR ESCAPE SLIDE RAFT PACK. REROUTED ELECTRICAL HARNESS ON L-1 DOOR ESCAPE SLIDE RAFT PACK IAW AMM 25-62-44-400-007-0.

Part: PTU — DEFECTIVE (HYDRAULIC SYS)

PHL-DEN - EMERGENCY LANDING - WHILE EN ROUTE PHL-DEN, CREW RECEIVED YELLOW HYDRAULIC SYSTEM LOW PRESSURE AND LOW QUANTITY CAUSED BY PTU RUNNING CONTINUOUSLY. YELLOW QUANTITY DROPPED TO ZERO, CREW DECLARED AN EMERGENCY AND DIVERTED TO PIT. MAINTENANCE REMOVED AND REPLACED THE HYDRAULIC POWER TRANSFER UNIT IAW AIRBUS MAINTENANCE MANUAL 29-23-41.

Part: RELAY — FAILED (L2 DOOR) · airframe 30,942 hrs · 18,452 cycles

FLT 1809 - CLT - EES - IN FLIGHT, THE 2-L DOOR SLIDE RED CABIN PRESSURE LIGHT AND THE SLIDE ARMED LIGHT ON THE FORWARD F/A PANEL WERE FLASHNG. THE FLIGHT ATTENDANT NUDGED THE 2-L DOOR ARMING HANDLE SEVERAL TIMES AND BOTH LIGHTS EXTINGUISHED. MAINTENANCE REMOVED AND REPLACED RELAY 3EN1 IAW AIRBUS MAINTENANCE MANUAL 52-71-00-820-002.

Part: SLIDE — DEFECTIVE (L1 DOOR) · airframe 30,941 hrs · 18,451 cycles

FLT 1840 CLT-PIT - EES - DOORS 1-L, 1-R, 2-L & 2-R SLIDES ARE VERY DIFFICULT TO ARM AND CIDS PANEL INDICATES SLIDES KEEP DISARMING DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED 1-L SLIDE AND LUBED DOOR SLIDE DISARM MECHANISM.

Part: SLIDE — DEFECTIVE (R2 DOOR) · airframe 30,941 hrs · 18,451 cycles

LOG PAGE 7184362 - FLT 1840 CLT-PIT - EES - DOORS 1-L, 1-R, 2-L & 2-R SLIDES ARE VERY DIFFICULT TO ARM AND CIDS PANEL INDICATES SLIDES KEEP DISARMING DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED 2-R SLIDE AND LUBED DOOR SLIDE DISARM MECHANISM.

Part: SLIDE — DEFECTIVE (R1 DOOR) · airframe 30,941 hrs · 18,451 cycles

FLT 1840 CLT-PIT - EES - DOORS 1-L, 1-R, 2-L & 2-R SLIDES ARE VERY DIFFICULT TO ARM AND CIDS PANEL INDICATES SLIDES KEEP DISARMING DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED 1-R SLIDE AND LUBED DOOR SLIDE DISARM MECHANISM.

Part: SLIDE — DEFECTIVE (L2 DOOR) · airframe 30,941 hrs · 18,451 cycles

FLT 1840 CLT-PIT - EES - DOORS 1-L, 1-R, 2-L & 2-R SLIDES ARE VERY DIFFICULT TO ARM AND CIDS PANEL INDICATES SLIDES KEEP DISARMING DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED 2-L SLIDE AND LUBED DOOR SLIDE DISARM MECHANISM.

Part: SLIDE RAFT — FAULTY (L2 DOOR) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - EEL - L-2 DOOR SLIDE RAFT DIRECTIONAL GUIDANCE LIGHTS FAILED TO ILLUMINATE DURING SLIDE RAFT DEPLOYMENT. REPLACED SLIDE RAFT ASSEMBLY IAW JOB CARD 26L00025007.

Part: SILL — CORRODED (FUSELAGE) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON UPPER SURFACE OF LOWER SILL AT FR19 + 6 INCHES, S23R AT R-1 DOOR. REPLACED LOWER SILL BETWEEN FR16 TO FR20, S23R AT R-1 DOOR IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53110339.

Part: BOLT — CORRODED (NR 4 SLAT TRACK) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON 2 EACH NR 4 SLAT ATTACHMENT BOLTS ON SLAT TRACK NR 10 RIGHT WING. REPLACED 2 EACH NR 4 SLAT ATTACHMENT BOLTS ON SLAT TRACK NR 10 RIGHT WING IAW A320 AMM 27-84-66.

Part: BOLT — CORRODED (LE SLAT) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON NR 5 SLAT ATTACHMENT BOLT ON SLAT TRACK NR 12 RIGHT WING. REPLACED NR 5 SLAT ATTACHMENT BOLT ON SLAT TRACK NR 12 RIGHT WING IAW A320 AMM 27-84-67.

Part: BOLT — CORRODED (LE SLAT) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON NR 2 SLAT ATTACHMENT BOLT ON SLAT TRACK NR 5 RIGHT WING. REPLACED NR 2 SLAT ATTACHMENT BOLT ON SLAT TRACK NR 5 RIGHT WING IAW A320 AMM 27-84-64.

Part: RING — CORRODED (LT WING) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540AB BETWEEN WS 700 TO WS 1406 & BETWEEN RIBS 2 TO RIB 3. REPLACED LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540AB BETWEEN WS 4862 TO WS 5512 & BETWEEN WS 700 TO WS 1406 & BETWEEN RIBS 2 TO RIB 3 IAW A320 SRM 51-72-11.

Part: RING — CORRODED (LT WING) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540BB BETWEEN WS 3758 TO WS 2508 & BETWEEN RIBS 6 TO RIB 7. REPLACED LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540BB BETWEEN WS 3758 TO WS 2508 & BETWEEN RIBS 6 TO RIB 7 IAW A320 SRM 51-72-11.

Part: RING — CORRODED (RT WING) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640EB BETWEEN WS 5512 TO WS 6132 & BETWEEN RIBS 10 TO RIB 11. REPLACED RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640EB BETWEEN WS 5512 TO WS 6132 & BETWEEN RIBS 10 TO RIB 11 IAW A320 SRM 51-72-11.

Part: ACCESS DOOR — CORRODED (RT WING) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - GALVANIC CORROSION ON COUNTER SINK HOLES OF RIGHT WING LOWER FUEL ACCESS DOOR 640JB BETWEEN WS 7792 TO WS 8268 & BETWEEN RIBS 14 TO RIB 15. REPLACED RIGHT WING LOWER FUEL ACCESS DOOR 640JB BETWEEN WS 7792 TO WS 8268 & BETWEEN RIBS 14 TO RIB 15 IAW A320 SRM 51-72-11.

Part: RING — CORRODED (RT WING) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640CB BETWEEN WS 4067 TO WS 4862 & BETWEEN RIBS 8 TO RIB 9. REPLACED RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640CB BETWEEN WS 4067 TO WS 4862 & BETWEEN RIBS 8 TO RIB 9 IAW A320 SRM 51-72-11.

Part: RING — CORRODED (RT WING) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640FB BETWEEN WS 6132 TO WS 6699 & BETWEEN RIBS 11 TO RIB 12. REPLACED RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640FB BETWEEN WS 6132 TO WS 6699 & BETWEEN RIBS 11 TO RIB 12 IAW A320 SRM 51-72-11.

Part: RING — CORRODED (RT WING) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640FB BETWEEN WS 4862 TO WS 5512 & BETWEEN RIBS 9 TO RIB 10. REPLACED RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640FB BETWEEN WS 4862 TO WS 5512 & BETWEEN RIBS 9 TO RIB 10 IAW A320 SRM 51-72-11.

Part: RING — CORRODED (LT WING) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540EB BETWEEN WS 5512 TO WS 6132 & BETWEEN RIBS 10 TO RIB 11. REPLACED LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540EB BETWEEN WS 5512 TO WS 6132 & BETWEEN RIBS 10 TO RIB 11 IAW A320 SRM 51-72-11.

Part: RING — CORRODED (LT WING) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540FB BETWEEN WS 6132 TO WS 6699 & BETWEEN RIBS 11 TO RIB 12. REPLACED LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540FB BETWEEN WS 6132 TO WS 6699 & BETWEEN RIBS 11 TO RIB 12 IAW A320 SRM 51-72-11.

Part: RING — CORRODED (RT WING) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640GB BETWEEN WS 6699 TO WS 7316 & BETWEEN RIBS 12 TO RIB 13. REPLACED RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640GB BETWEEN WS 6699 TO WS 7316 & BETWEEN RIBS 12 TO RIB 13 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON SEAT TRACK RAIL BETWEEN FR56 TO FR64, -Y1292. REPAIRED SEAT TRACK RAIL BETWEEN FR56 TO FR64, -Y1292 IAW A320 SRM 53-41-15.

Part: BOLT — CORRODED (NR 4 SLAT TRACK) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON NR 4 SLAT ECCENTRIC ATTACHMENT BOLT ON SLAT TRACK NR 9 RIGHT WING. REPLACED NR 4 SLAT ECCENTRIC ATTACHMENT BOLT ON SLAT TRACK NR 9 RIGHT WING IAW A320 AMM 27-84-66.

Part: BOLT — CORRODED (NR 3 SLAT TRACK) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON NR 3 SLAT ECCENTRIC ATTACHMENT BOLT ON SLAT TRACK NR 7 RIGHT WING. REPLACED NR 3 SLAT ECCENTRIC ATTACHMENT BOLT ON SLAT TRACK NR 7 RIGHT WING IAW A320 AMM 27-84-65.

Part: SILL — CORRODED (ZONE 100) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON LOWER SILL AT FR62, S38R. REPAIRED LOWER SILL AT FR62, S38R IAW A320 SRM 51-41-49.

Part: BOLT — CORRODED (LE SLAT) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON SLAT ATTACHMENT BOLT ON TRACK NR 1 ON RIGHT WING. REPLACED SLAT ATTACHMENT BOLT ON TRACK NR 1 ON RIGHT WING IAW A320 AMM 27-84-63.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LOWER FORWARD CORNER FITTING AT FR66, S23L AT L-2 DOOR CUTOUT AREA. REPLACED LOWER FORWARD CORNER FITTING AT FR66, S23L AT L-2 DOOR CUTOUT AREA IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53480009.

Part: BOLT — CORRODED (LE SLAT) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON ATTACHMENT BOLTS 2 EACH ON SLAT TRACK NR 4 RIGHT WING. REPLACED ATTACHMENT BOLTS 2 EACH ON SLAT TRACK NR 4 RIGHT WING IAW A320 AMM 27-84-63.

Part: BOLT — CORRODED (LE SLAT) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON ATTACHMENT BOLT ON SLAT TRACK NR 3 RIGHT WING. REPLACED ATTACHMENT BOLT ON SLAT TRACK NR 3 RIGHT WING IAW A320 AMM 27-84-63.

Part: BOLT — CORRODED (LE SLAT) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON ATTACHMENT BOLTS 3 EACH ON SLAT TRACK NR 2 RIGHT WING. REPLACED ATTACHMENT BOLTS 3 EACH ON SLAT TRACK NR 2 RIGHT WING IAW A320 AMM 27-84-63.

Part: BOLT — CORRODED (LE SLAT) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON NR 1 SLAT TRACK ATTACHMENT BOLTS 3 EACH AT AFT UPPER, FORWARD UPPER, & FORWARD LOWER POSITIONS OF NR 1 SLAT LEFT WING. REPLACED NR 1 SLAT TRACK ATTACHMENT BOLTS 3 EACH AT AFT UPPER, FORWARD UPPER, & FORWARD LOWER POSITIONS OF NR 1 SLAT LEFT WING IAW A320 AMM 27-84-63.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR49 TO FR50, -Y1292. REPAIRED SEAT TRACK BETWEEN FR49 TO FR50, -Y1292 IAW A320 SRM 53-00-15.

Part: FITTING — CORRODED (FUSELAGE) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON CORNER FITTING AT FR68, S23R AT R-2 DOOR AREA. REPLACED CORNER FITTING AT FR68, S23R AT R-2 DOOR AREA IAW A320 SRM 51-72-11 & AIRBUS DRAWING 6279150.

Part: BOLT — CORRODED (LE SLAT) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON NR 1 SLAT TRACK TO SLAT ECCENTRIC ATTACHMENT BOLT ON RIGHT WING. REPLACED NR 1 SLAT TRACK TO SLAT ECCENTRIC ATTACHMENT BOLT IAW A320 AMM 27-84-63.

Part: DUMMY RAIL — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON DUMMY RAIL BETWEEN FR12 TO FR18, Y503.2. REPLACED DUMMY RAIL BETWEEN FR12 TO FR18, Y503.2 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK FLANGE BETWEEN FR24 TO FR25 + 8 INCHES, -Y765. REPAIRED SEAT TRACK FLANGE BETWEEN FR24 TO FR25 + 8 INCHES, -Y765 IAW A320 SRM 53-21-15.

Part: FASTENER — CORRODED (SPOILER) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON HARDWARE OF CENTER HINGE FITTING ATTACHMENT ON LEFT WING NR 2 SPOILER. REPLACED HARDWARE OF CENTER HINGE FITTING ATTACHMENT ON LEFT WING NR 2 SPOILER IAW A320 CMM 57-72-21.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR12 TO FR24, Y254. REPLACED FLOOR SUPPORT BETWEEN FR12 TO FR24, Y254 IAW A320 SRM 51-72-11.

Part: COUPLING — CORRODED (FUSELAGE) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - NR 6282214 - CORROSION ON INBOARD COUPLING OF FLOORBEAM AT FR67 + 16 INCHES, -Y1162. REPLACED INBOARD COUPLING OF FLOORBEAM AT FR67 + 16 INCHES, -Y1162 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67, -Y465. REPLACED FLOORBEAM BETWEEN FR64 TO FR67, -Y465 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66 + 5 INCHES, -Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66 + 5 INCHES, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D5347219020300.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR70, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67 + 16 INCHES TO FR69, -Y1162. REPLACED FLOORBEAM BETWEEN FR67 + 16 INCHES TO FR69, -Y1162 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67 + 15 INCHES TO FR69, Y1162.5. REPLACED FLOORBEAM BETWEEN FR67 + 15 INCHES TO FR69, Y1162.5 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 19,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RAIL SEAL BEAM BETWEEN FR64 TO FR66 + 5 INCHES, Y765. REPLACED RAIL SEAL BEAM BETWEEN FR64 TO FR66 + 5 INCHES, Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR70, Y765. REPLACED FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR70, Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23L. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23L IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR65 TO FR66, -Y1732. REPLACED FLOORBEAM BETWEEN FR65 TO FR66, -Y1732 IAW A320 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23R. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23R IAW A320 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - NR 6282202 - CORROSION ON CENTER SHAPE SILL AT L-2 DOOR BETWEEN FR66 TO FR68, S23L. REPLACED CENTER SHAPE SILL AT L-2 DOOR BETWEEN FR66 TO FR68, S23L IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR65 TO FR66, Y512.5. REPLACED FLOORBEAM BETWEEN FR65 TO FR66, Y512.5 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR70, -Y254. REPLACED FLOORBEAM BETWEEN FR68 TO FR70, -Y254 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM Z-PROFILE ASSEMBLY BETWEEN FR64 TO FR65, -Y1732. REPLACED FLOORBEAM Z-PROFILE ASSEMBLY BETWEEN FR64 TO FR65, -Y1732 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SEAT FLOORBEAM BETWEEN FR64 TO FR66 + 4 INCHES, -Y1292. REPLACED SEAT FLOORBEAM BETWEEN FR64 TO FR66 + 4 INCHES, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR41 TO FR47, Y1292. REPLACED SEAT TRACK BETWEEN FR41 TO FR47, Y1292 IAW A320 SRM 51-72-11.

Part: COUPLING — CORRODED (FUSELAGE) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON INBOARD COUPLING OF FLOORBEAM AT FR67 + 5 INCHES, Y1162. REPLACED INBOARD COUPLING OF FLOORBEAM AT FR67 + 5 INCHES, Y1162 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 + 11 INCHES TO FR67 + 15 INCHES, Y1292. REPLACED FLOORBEAM BETWEEN FR66 + 11 INCHES TO FR67 + 15 INCHES, Y1292 IAW A320 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · airframe 309,361 hrs · 8,449 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON LOWER SHAPE SILL OF R-2 DOOR WAY BETWEEN FR66 TO FR68, S23R. REPLACED LOWER SHAPE SILL OF R-2 DOOR WAY BETWEEN FR66 TO FR68, S23R.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 + 4 INCHES TO FR67 + 17 INCHES, -Y1292. REPLACED FLOORBEAM BETWEEN FR66 + 4 INCHES TO FR67 + 17 INCHES, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR65 + 10.5 INCHES TO FR66 + 4 INCHES, Y1292. REPLACED FLOORBEAM BETWEEN FR65 + 10.5 INCHES TO FR66 + 4 INCHES, Y1292 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR65 + 10 INCHES TO FR65 + 20 INCHES, -Y1732. REPLACED FLOORBEAM BETWEEN FR65 + 10 INCHES TO FR65 + 20 INCHES, -Y1732 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (ZONE 100 - FUSEL) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112812.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S-5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SUPPORT STRUCTURE BETWEEN FR28 TO FR29 & BETWEEN S43L TO S43R. REPLACED STAMPING SUPPORT BETWEEN FR28 TO FR29 & BETWEEN S43L TO S43R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53230861.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - NR 6284552 - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, -Y1292. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53370500.

Part: SEAT TRACK — CORRODED (ZONE 100 - FUSEL) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y765. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112812.

Part: SUPPORT FITTING — WORN (R2 DOOR) · airframe 30,936 hrs · 78,449 cycles

SAL - S5 - MAJOR REPAIR - WEAR ON SUPPORT FITTING ASSEMBLY AT R-2 DOOR. REPLACED SUPPORT FITTING ASSEMBLY AT R-2 DOOR IAW A320 CMM 52-13-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, -Y1292. REPLACED SEAT TRACK BETWEEN FR24 TO FR35, -Y1292 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR37 TO FR39, -Y765. REPLACED SEAT TRACK BETWEEN FR37 TO FR39, -Y765 IAW A320 SRM 51-72-11.

Part: SKIN — SATURATED (ELEVATOR) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - TRAPPED WATER FOUND IN LEFT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA131 TO STAB STA 227, 23 INCHES OUTBOARD FROM HORIZ STAB RIB 1 TO RIB 3 & 6 INCHES FROM LEADING EDGE. REPAIRED LEFT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 131 TO STAB STA 227, 23 INCHES OUTBOARD FROM HORIZ STAB RIB 1 TO RIB 3 & 6 INCHES FROM LEADING EDGE IAW A320 SRM 55-77-13.

Part: SKIN — SATURATED (ELEVATOR) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - TRAPPED WATER FOUND IN LEFT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 527 TO STAB STA 601, 37 INCHES INBOARD FROM HORIZ STAB RIB 8 TO RIB 10 & 7 INCHES FROM LEADING EDGE. REPAIRED LEFT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 527 TO STAB STA 601, 37 INCHES INBOARD FROM HORIZ STAB RIB 8 TO RIB 10 & 7 INCHES FROM LEADING EDGE IAW A320 SRM 55-77-13.

Part: SKIN — SATURATED (ELEVATOR) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - TRAPPED WATER FOUND IN RIGHT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 271 TO STAB STA 404, 56 INCHES OUTBOARD FROM HORIZ STAB RIB 5 TO RIB 8 & 10 INCHES FROM LEADING EDGE. REPAIRED RIGHT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 271 TO STAB STA 404, 56 INCHES OUTBOARD FROM HORIZ STAB RIB 5 TO RIB 8 & 10 INCHES FROM LEADING EDGE IAW A320 SRM 55-21-00.

Part: SKIN — SATURATED (ELEVATOR) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - NR 6284654 - TRAPPED WATER FOUND IN RIGHT HAND ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA181 TO STAB STA271, 32 INCHES OUTBOARD FROM HORIZ STAB RIB 1 TO RIB 3 & 5 INCHES FROM TRAILING EDGE. REPAIRED RIGHT HAND ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA181 TO STAB STA271, 32 INCHES OUTBOARD FROM HORIZ STAB RIB 1 TO RIB 3 & 5 INCHES FROM TRAILING EDGE IAW A320 SRM 55-77-13.

Part: SKIN — SATURATED (ELEVATOR) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - TRAPPED WATER FOUND IN RIGHT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 271 TO STAB STA 404, 42 INCHES OUTBOARD FROM HORIZ STAB RIB 5 TO RIB 8 & 5 INCHES FROM LEADING EDGE. REPAIRED RIGHT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 271 TO STAB STA 404, 42 INCHES OUTBOARD FROM HORIZ STAB RIB 5 TO RIB 8 & 5 INCHES FROM LEADING EDGE IAW A320 SRM 55-77-13.

Part: SKIN — SATURATED (ELEVATOR) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - TRAPPED WATER FOUND IN RIGHT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 446 TO STAB STA 601, 32 INCHES INBOARD FROM HORIZ STAB RIB 9 TO RIB 10 & 5 INCHES FROM LEADING EDGE. REPAIRED RIGHT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 446 TO STAB STA 601, 32 INCHES INBOARD FROM HORIZ STAB RIB 9 TO RIB 10 & 5 INCHES FROM LEADING EDGE IAW A320 SRM 55-77-13.

Part: SKIN — SATURATED (ELEVATOR) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - TRAPPED WATER FOUND IN LEFT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 466 TO STAB STA 589, 69 INCHES INBOARD FROM HORIZ STAB RIB 8 TO RIB 10 & 6 INCHES FROM LEADING EDGE. REPAIRED LEFT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 466 TO STAB STA 589, 69 INCHES INBOARD FROM HORIZ STAB RIB 8 TO RIB 10 & 6 INCHES FROM LEADING EDGE IAW A320 SRM 55-77-13.

Part: SKIN — SATURATED (ELEVATOR) · airframe 30,936 hrs · 18,449 cycles

SAL - S5 - MAJOR REPAIR - TRAPPED WATER FOUND IN LEFT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 131 TO STAB STA 227, 13 INCHES OUTBOARD FROM HORIZ STAB RIB 1 TO RIB 3 & 9 INCHES FROM LEADING EDGE. REPAIRED LEFT ELEVATOR UPPER SKIN HONEYCOMB STRUCTURE BETWEEN STAB STA 131 TO STAB STA 227, 13 INCHES OUTBOARD FROM HORIZ STAB RIB 1 TO RIB 3 & 9 INCHES FROM LEADING EDGE IAW A320 SRM 55-77-13.

Part: LENS — MISSING (CABIN) · airframe 28,538 hrs · 17,249 cycles

FLT 727 - DEN - EEL - R2 DOOR EMERGENCY LIGHT LENS MISSING. MAINTENANCE INSTALLED LENS AS REQUIRED.

Part: LIGHT — ODOR (CABIN) · airframe 27,022 hrs · 16,585 cycles

LOG PAGE 8599434 - FLT 1781-OKC - BURNING ODOR AROUND ROW 20 RT - NO VISIBLE SMOKE. MAINTENANCE FOUND NO OBVIOUS DEFECTS TO CAUSE BURNING ODOR. MAINTENANCE RELAMPED THE READING LIGHT AT 20D. NO SUBSEQUENT EVENTS.

Part: POWER SUPPLY — MALFUNCTIONED (CABIN) · airframe 26,226 hrs · 16,258 cycles

FLT 1195 - PHL - EEL - FORWARD CEILING EMERGENCY LIGHT WILL NOT ILLUMINATE. MAINTENANCE RESET THE POWER SUPPLY UNIT - OPERATIONAL CHECK GOOD.

Part: UNKNOWN — FUMES (CABIN) · airframe 25,597 hrs · 15,995 cycles

FLT 873 LAS-SAN - FUMES - PASSENGERS SEATED AFT OF THE WING COMPLAINED OF FUMES IN THE CABIN, EYE IRRITATION AND SNEEZING. MAINTENANCE INSPECTED THE APU FOR LEAKS - NONE NOTED. RAN THE APU AND BOTH ENGINES INDEPENDENTLY WITH NO ODORS NOTED. AIRCRAFT IS OK FOR SERVICE.

Part: HOSE — RUPTURED (ZONE 400) · airframe 23,650 hrs · 15,238 cycles

FLT NR 1910 CLT-LGA - DIV - CREW REPORTED GREEN HYDRAULIC LOW LEVEL LIGHT DURING CRUISE. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO PHL. AIRCRAFT WAS TOWED TO GATE DUE TO LOSS OF NOSE WHEEL STEERING. MAINTENANCE REPLACED RUPTURED HYDRAULIC SENSE LINE, AND DUE TO FILTER DEBRIS, REPLACED HYDRAULIC PUMP AND ASSOCIATED FILTERS.

Part: EPSU — FAULTED (EMERGENCY LIGHT)

CLT - RECEIVED -EMER L- MESSAGE DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE MID-CABIN, LEFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.

Part: CONTROL UNIT — FAULTY (MLG)

RDU - FLT 873 ON TAKEOFF, RDU TO PHL, DURING TAKEOFF ROLL, THE AIRCRAFT RIGHT BRAKE LOCKED UP. THE FLIGHT REJECTED TAKEOFF AT ABOUT 50-60 KNOTS. AFTERWARDS, THE TOWER REPORTED TO THE CREW THAT THE NR 3 MAIN GEAR WHEEL ASSEMBLY APPEARED TO HAVE SMOKE COMING FROM IT. THE CREW REQUESTED EMERGENCY EQUIPMENT FOLLOW THE FLIGHT BACK TO THE GATE. THE FLIGHT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 3 BRAKE ASSEMBLY FOR WEAR, ALL FOUR MAIN GEAR WHEEL ASSEMBLIES FOR FLAT SPOTTING, AND THE BRAKE STEERING CONTROL UNIT. OK FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2

BFM - S1 - FLOOR SUPPORT, 2 INCH X 3 INCH X 0.075 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500; MAIN CABIN FLOOR - Y254 BET FR 16 AND 20. FABRICATED PARTS IAW SRM 53-00-14 FIG 206 PR SRM 53-11-14, 51-74-00, 53-14-00, 51-42-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

PIT - S1 - SILL, 1 INCH X 1 INCH X .07 INCH DEEP; CORROSION; LEVEL 2; TASK NR JA-260-53500-006; CABIN FLOOR, R-2 DOOR SEAL ASSY ON CROSSBEAM C66 AND AFT ENDI OF FRAME - Y1732. REPLACED DOOR SEAL IAW SRM 51-74-00, 53-41-14, 51-42-11.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2

BFM - S1 - FLOOR WEB, 1.5 INCH X 2 INCHES X 0.50 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500, MAIN CABIN FLOOR; Y1584, BET FR14 AND 16. REMOVED AND REPLACED IAW SRM.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2

BFM - S1 - TRACK ASSEMBLY, 2 INCH X 2 INCH X 0.50 INCH AREA, CORROSION LEVEL 2; TASK NR JA-220-53500, MAIN CABIN FLOOR- Y254 BET FR16 AND 23. REMOVED AND REPLACED IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2

BFM - S1 - SUPPORT, 2 INCH X 5 INCHES X .025 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500, MAIN CABIN FL -Y189, FR 20. REMOVED AND REPLACED IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2

BFM - S1- SEAL SUPPORT, .5 INCH X .5 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500-015, MAIN CABIN FLOORBOARD SEAL SUPPORT AT Y1584 BETWEEN 14 AND 16. REMOVED AND REPLACED FLOORBOARD SEAL SUPPORT IAW SRM 51-74-00, SRM 53-11-14, SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2

BFM - S1 - FLOOR SUPPORT, 1.5 INCH X 2 INCHES X .040 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-200-53500, BTW FR 16 AND 20, Y1292, FLOOR SUPPORT. REPLACED FLOOR SUPPORT IAW SRM 51-74-00, 53-11-14, 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2

BFM - S1 - FLOOR SUPPORT, 2 INCHES X 12 INCHES X 0.020 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500, MAIN CABIN FLOOR BET FR 16, 20, BL-Y1292. REPLACED FLOOR SUPPORT IAW SRM 51-74-00, 53-11-14, 51-42-11.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2

BFM - S1 - DUMMY RAIL, 2 INCHES X 1 INCH X .050 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500. MAIN CABIN FLOOR @ FR 16, LB -Y81. REPLACED DUMMY RAIL IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

BFM - S1 - BEAM, 18 INCHES X 2 INCHES X .03 INCH AREA, CORROSION; LEVEL 2; TSK NR JA 260-53500-004, MAINT CABIN FLOOR Y1292 BET C66 AND C68. REMOVED AND REPLACED FLOORBEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

BFM - S1 - FLOORBEAM- 2 INCHES X 1.5 INCHES X .04 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-260-53500-012, Y1292, BTW C68 AND C69 MAIN CABIN FLOOR. REMOVED AND REPLACED FLOOR BEAM IAW SRM 53-00-14, SRM 51-42-11.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2

PIT - S1 - DUMMY RAIL, 2.5 INCHES X 2 INCHES X .075 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500; MAIN CABIN FLOOR FR 16, Y503.2. REPLACED DUMMY RAIL (BEAM) ALT PN INSTALLED IAW SRM 51-74-00, 53-11-14, 51-42-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2

BFM - S2 - SHEAR PLATE, 1 INCH X 1 INCH X .030 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, MAIN CABIN FLOOR BTW 69 AND 70, BL - Y1292. REMOVED AND REPLACED SHEAR PLATE (WEB) IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

BFM - S1 - BEAM, 3 INCHES X 2 INCHES X .030 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500; MAIN DECK FLOOR RAIL, FRAME 68, -Y765. REMOVED AND REPLACED FLOORBEAM IAW SRM 53-00-14, 51-42-11.

Part: SLIDE — SEPARATED (CABIN)

THE SLIDE SHOP FOUND THAT THE BRIDGING ON UPPER TUBE AT RUNWAY END HAD A SEAM SEPARATION. THE REPAIR SHOP SENT THE SLIDE BACK TO THE VENDOR FOR REPAIR.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DURING EMERGENCY LIGHTS TEST, RECEIVED 'EPSU INT LOAD EMER R' FAULT. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY PACK AT THE RIGHT EMERGENCY EXIT. OPERATIONALLY CHECKS OK. (M)

Part: RELAY — FAILED (CABIN)

LGA - THE EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE WHEN PED SWITCH IS TURNED ON. MAINTENANCE REPLACED RELAY. OPERATIONALLY CHECKS OK. (M)

Part: CAM — BROKEN (L1 DOOR)

BOS - L1 DOOR ARMING CAM BROKE. MAINTENANCE REPLACED THE CAM. SMELL PIECE FELL FROM MAIN ENTRY DOOR. REPLACED DOOR HOOK. OPS OK. (M)

Part: ELECTRONIC UNIT — ODOR (CABIN)

DCA-LGA - FLT 6360 - PASSENGER REPORTED ELECTRICAL FUMES AT ROW 20. MAINTENANCE REPLACED SEB AT ROW 20. SYSTEM TEST OK. (M)

Part: SLIDE — MALFUNCTIONED (CABIN)

BOS - FOUND FORWARD LEFT ESCAPE SLIDE FAILED EMERGENCY LIGHT CHECK. CIDS DISPLAYED EPSU EXT LOAD FWD LT. MAINTENANCE REPLACED THE FORWARD LEFT ESCAPE SLIDE. OPERATIONAL CHECK OK. (M)

Part: SKIN — DISBONDED (SLIDE DOOR)

DURING A-2 CHECK VISUAL INSPECTION, FOUND A 12 INCH BY 36 INCH DISBONDED AREA AT SLIDE DOOR COVERING OUTER SKIN AND LEFT A/C RT OFF WING SLIDE DOOR. REMOVED AND REPLACED SLIDE. (X)