N3014R

Part: SLIDING WINDOW — SCRATCHED (ZONE 200) · airframe 32,667 hrs · 16,029 cycles

AIRCRAFT WAS GROUNDED: FLIGHT DECK LEFT HAND SLIDING WINDOW HAS EXTENSIVE EXTERNAL SCRATCHES THAT CREATE A DAZZLING EFFECT IN SUNLIGHT FROM ANY ANGLE NOT ALIGNED WITH THAT WINDOW. MAINTENANCE REPLACED THE SLIDING WINDOW AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 56-12-11.

Part: LIGHT — MISWIRED (ZONE 200) · airframe 32,207 hrs · 15,702 cycles

AIRCRAFT IN BASE MAINTENANCE: LAST AISLE CEILING EMERGENCY LIGHT DOES NOT ILLUMINATE. MAINTENANCE FOUND LIGHT ASSEMBLY ELECTRICAL HOOKUPS INSTALLED INCORRECTLY, SWAPPED CONNECTIONS AND REINSTALLED LIGHT ASSEMBLY, OPS CHECK GOOD IAW AMM 33-51-11-400-001-A.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 31,624 hrs · 15,353 cycles

AIRCRAFT WAS NOT GROUNDED: DURING CIDS 1 EPSU SYS TEST PER P/S CHECK, FAULT 335100 BAT/EPSU(10WL) FWD L FAULT. REMOVED AND REPLACED EMERGEMCY LIGHTS BATTERY AND OPS TEST GOODIAW AMM 33-51-38.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 31,624 hrs · 15,353 cycles

AIRCRAFT WAS NOT GROUNDED: DURING CIDS 1 EPSU SYS TEST PER P/S CHECK, FAULT 335100 BAT/EPSU(11WL) EMER L FAULT. MAINTENANCE REPLACED EMERGEMCY LIGHTS BATTERY AND OPS TEST GOODIAW AMM 33-51-38.

Part: PILOT VALVE — DEFECTIVE (ZONE 700) · airframe 30,087 hrs · 14,501 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO THE FLIGHT CREW REPORTING THAT AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT ALONG WITH A LANDING GEAR CONTROL ECAM MESSAGE ON GEAR PAGE IN AMBER. THE AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT FOR AALA202411147216: MAINTENANCE REPLACED THE PILOT VALVE ON THE LANDING GEAR SAFETY VALVE PER AMM 32-31-17 A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED. ** (CLOSED)

Part: PILOT VALVE — FAULTY (ZONE 700) · airframe 30,088 hrs · 14,501 cycles

AIRCRAFT WAS GROUNDED: AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. L/G CTL MESSAGE ON GEAR PAGE IN AMBER. PRIOR TO PUSHBACK, LGCIU 1 FAULT BUT WA SCLEARED WITH MAINTENANCE AND BYTE TESTED OK. RETUIRNED TO FIELD EMEREGNCY DECLARE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED PILOT VALVE ON LANDING GEAR SAFET VALVE IAW AMM 32-31-17.

Part: LANDING GEAR — FAILED (ZONE 700) · airframe 30,087 hrs · 14,501 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO THE FLIGHT CREW REPORTING THAT AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT ALONG WITH A LANDING GEAR CONTROL ECAM MESSAGE ON GEAR PAGE IN AMBER. THE AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,989 hrs · 13,824 cycles

AIRCRAFT WAS NOT GROUNDED: AFT CEILING EMERGENCY LAMP 206WL INOPERATIVE. REPLACED AFT CEILING EMERGENCY LAMP 206WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-11.

Part: BATTERY — NO TEST (ZONE 200 - FUSE) · airframe 27,007 hrs · 12,788 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 13WL BATTERY FAULT MESSAGE DISPLAYED DURING SYSTEM TEST. REPLACED BATTERY PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: WIRE — DISCONNECTED (ZONE 200 - FUSE) · airframe 26,961 hrs · 12,760 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. MAINTENANCE FOUND THE POWER WIRE TO BE DISCONNECTED UNDER THE SEAT AND RE-CONNECTED IT. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: ENGINE — FOD (ZONE 400 - NAC/P) · airframe 26,033 hrs · 12,289 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PEI. FLIGHT REPORTED A BIRDSTRIKE TO THE #1 ENGINE THAT RESULTED IN AN INFLIGHT SHUTDOWN AND INDICATION OF AN ENGINE FIRE. THE FLIGHT CREW DISCHARGED ONE FIRE BOTTLE AND THE ENGINE FIRE WAS EXTINGUISHED. THE AIRCRAFT LANDED A PEI SAFELY WITHOUT FURTHER INCIDENT AND THE AIRCRAFT TAXIED TO THE GATE UNDER ITS OWN POWER. DUE TO THE EXTENT OF THE DAMAGE THE ENGINE WILL BE REPLACED. **SUPPLEMENTAL REPORT FOR AALA202305168654: MAINTENANCE REPLACED #1 ENGINE PER TASK CARD 26L4007100** (CLOSED)

Part: ENGINE — FOD (ZONE 400 - NAC/P) · airframe 26,033 hrs · 12,289 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PEI. FLIGHT REPORTED A BIRDSTRIKE TO THE #1 ENGINE THAT RESULTED IN AN INFLIGHT SHUTDOWN AND INDICATION OF AN ENGINE FIRE. THE FLIGHT CREW DISCHARGED ONE FIRE BOTTLE AND THE ENGINE FIRE WAS EXTINGUISHED. THE AIRCRAFT LANDED A PEI SAFELY WITHOUT FURTHER INCIDENT AND THE AIRCRAFT TAXIED TO THE GATE UNDER ITS OWN POWER. DUE TO THE EXTENT OF THE DAMAGE THE ENGINE WILL BE REPLACED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: BALL — DETACHED (ZONE 800 - DOORS) · airframe 25,864 hrs · 12,192 cycles

AIRCRAFT IN BASE MAINTENANCE: R1 DOOR SLIDE, COVER RELEASE RETAINING BALL DETACHED FROM MOUNT,SLIDE. REPLACED R1 DOOR SLIDE ASSEMBLY.

Part: GIRT BAR — STICKING (ZONE 800 - DOORS) · airframe 25,864 hrs · 12,192 cycles

AIRCRAFT IN BASE MAINTENANCE: L1 DOOR SLIDE GIRT-BAR DOES NOT MOVE FREELY. REPLACED GIRT BAR PER AMM 25-62-44 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: HINGE ARM — CRACKED (ZONE 300 - STABS) · airframe 25,864 hrs · 12,192 cycles

AIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER RUDDER #1 HINGE ARM AT FORK END HAS 3 EACH FASTENER HOLES CRACKED AT RIB 2. REPLACED HINGE ARM FITTING PER SRM 51-42-11 AND EA 343845.

Part: LIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 25,864 hrs · 12,192 cycles

AIRCRAFT IN BASE MAINTENANCE: SEAT ROW 10 ABC EMERGENCY AISLE LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY PER AMM 33-51-18 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: HANDLE — BROKEN (ZONE 800 - DOORS) · airframe 25,864 hrs · 12,192 cycles

AIRCRAFT IN BASE MAINTENANCE: R-2 DOOR SLIDE RAFT PULL HANDLE HAS BROKEN THREADS. REPLACED SLIDE RAFT ASSEMBLY.

Part: DOOR LATCH — BROKEN (ZONE 800 - DOORS) · airframe 25,801 hrs · 12,158 cycles

AIRCRAFT WAS GROUNDED: FLIGHT DECK DOOR WILL NOT OPEN USING HANDLE. MUST USE FLIGHT DECK DOOR SWITCH TO OPEN. MAINTENANCE FOUND THE FLIGHT DECK DOOR LATCH MECHAISM BROKEN AT THE CENTER LATCH ASSEMBLY AND REPLACED THE DOOR LATCH MECHANISM PER AMM 52-51-21. A SATISFACTORY OPERATIONAL CHECK.

Part: SLIDING WINDOW — OUT OF ADJUST (CAPTAIN'S) · airframe 25,319 hrs · 11,935 cycles

AIRCRAFT WAS GROUNDED: CAPTAINS SLIDING WINDOW VERY DIFFICULT TO OPEN. MAINTENANCE ADJUSTED CAPTAINS SLIDING WINDOW PER AMM 56-12-11.

Part: CONTROL UNIT — FAULTED (FUEL SYSTEM) · airframe 25,026 hrs · 11,811 cycles

AIRCRAFT WAS GROUNDED, FUEL USED, FUEL ON BOARD DISAGREE MESSAGE ON ECAM. FUEL PROGRAM ON FUEL PLAN SHOWED INITIAL FUEL ON BOARD TO BE 1000 LBS BELOW FLLIGHT PLAN BURN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO MIA WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 FUEL LEVEL SENSING CONTROL UNIT IAW AMM 28-46-00 (AALA202212202244) AND THE FUEL QUANITY INDICATION COMPUTER IAW AMM 28-42-34. (AAALA202212203286) A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: COMPUTER — FAULTED (FUEL SYSTEM) · airframe 25,026 hrs · 11,811 cycles

AIRCRAFT WAS GROUNDED: FUEL USED/ FUEL ON BOARD DISAGREE MESSAGE ON ECAM. FUEL PROGRAM ON FUEL PLAN SHOWED INITIAL FUEL ON BOARD TO BE 1000 LBS BELOW FLLIGHT PLAN BURN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO MIA WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE #2 FUEL LEVEL SENSING CONTROL UNIT PER AMM 28-46-00 (AALA202212202244) AND THE FUEL QUANITY INDICATION COMPUTER PER AMM 28-42-34. (AAALA202212203286) A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: UNKNOWN — ODOR (CABIN) · airframe 24,894 hrs · 11,756 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO BAQ DUE TO A STRONG SMOKEY OIL FUME COMING FROM THE RIGHT HAND SIDE OF THE AIRCRAFT NEAR SEATS 15 DEF. AIRCRAFT LANDED SAFELY AT BAQ WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED SMOKE /ODOR / FUME TROUBLE SHOOTING TASK CARD 26L00021001 INCLUDING ENGINE / APU OPERATIONAL CHECKS WITH NO ODORS BEING NOTED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — NONE (ZONE 200 - FUSE) · airframe 24,533 hrs · 11,567 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT 12WL BATTERY FAILED FUNCTIONAL TEST. MAINTENANCE REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.

Part: POWER SUPPLY — NONE (ZONE 200 - FUSE) · airframe 24,533 hrs · 11,567 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT 13WL FAILED CIDS OPERATIONAL TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 13WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL TEST PER AMM 33-51-38.

Part: BATTERY — NONE (ZONE 200 - FUSE) · airframe 24,533 hrs · 11,567 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT 11WL BATTERY FAILED FUNCTIONAL TEST. MAINTENANCE REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.

Part: FUSE — BLOWN (ZONE 200 - FUSE) · airframe 24,527 hrs · 11,564 cycles

AIRCRAFT WAS GROUNDED: STRONG HOT ELECTRICAL SMELL ON DESCENT THROUGH 13,000 ONLY NOTICEABLE IN THE FLIGHT DECK. MAINTENANCE FOUND THE APU START FUSE (6KA) BURNT / BLOWN IN THE FLIGHT DECK AND REPLACED IT PER AMM 49-42-00-960-003-A. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ODORS BEING NOTED.

Part: POWER SUPPLY — NONE (ZONE 200 - FUSE) · airframe 24,439 hrs · 11,524 cycles

AIRCRAFT WAS GROUNDED: ESCAPE SLIDE LIGHT / EMERGENCY POWER SUPPLY UNIT 10WL FORWARD LEFT FAULT MESSAGE DISPALYED DURING FUNCTIONAL TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 10WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL / BITE CHECK PER AMM 33-51-38 AND AMM 33-51-00.

Part: NONE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 24,439 hrs · 11,524 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT HAND AFT DOOR ASSIST BOTTLE PRESSURE LOW. MAINTENANCE SERVICED DOOR ASSIST BOTTLE PER AMM 52-10-00.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200 - FUSE) · airframe 24,010 hrs · 11,334 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY EXIT LIGHTS INOPERATIVE AT OVER WING EXIT CEILING AND SIDEWALL.. REPLACED EMERGENCY POWER SUPPLY UNIT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.

Part: HINGE — BINDS (ZONE 900 - LAV/G) · airframe 22,344 hrs · 10,569 cycles

AIRCRAFT WAS NOT GROUNDED: FIRST CLASS LAVATORY DOOR BINDS AT BOTTOM. LUBED DOOR HINGE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: NONE — NONE (ZONE 100 - FUSE) · airframe 21,366 hrs · 10,117 cycles

AIRCRAFT WAS NOT GROUNDED: FUEL AUTO FEED FAULT ON DESCENT. **SUPPLEMENTAL REPORT FOR AALA202109290510: REPLACED CENTER TANK #1 FUEL PUMP 37QA AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 28-21-25** (CLOSED)

Part: NONE — NONE · airframe 21,366 hrs · 10,117 cycles

AIRCRAFT WAS NOT GROUNDED: FUEL AUTO FEED FAULT ON DESCENT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: RESERVOIR — LOW PRESSURE (RT OVRWG SLIDE) · airframe 21,262 hrs · 10,067 cycles

AIRCRAFT WAS GROUNDED: RIGHT OVER WING EXIT SLIDE PRESSURE LOW ON RIGHT FLIGHT ATTENDANTS PANEL. REPLACED SLIDE RESERVOIR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-62-46.

Part: SMOKE DETECTOR — FALSE ACTIVATION (MONITOR PANEL) · airframe 21,041 hrs · 9,960 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANTS REPORT SMOKE ALARMS ON FLIGHT ATTENDANT PANEL. NO SMOKE FOUND. NO ELECTRONIC CENTRALIZED AIRCRAFT MONITOR SHOWN ON FLIGHT DECK. AT SOME POINT ENROUTE ALARMS SHUT OFF. ACCOMPLISHED RESET OF CABIN INTERCOMMUNICATION DATA SYSTEM 1 AND 2 PER TSM 24-00-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (SLIDE BOTTLE) · airframe 20,942 hrs · 9,919 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT PANEL SHOWS "CHECK SLIDE PRESSURE" RIGHT OVER WING EXIT. SUPPLEMENTAL REPORT FOR AALA202108028912: ACCOMPLISHED TSM 25-62-00-810-806-A AND AMM TEST 23-73-00 WITH NO FAULTS NOTED, VERIFIED THAT RESERVOIR BOTTLE PRESSURE / LEVEL WERE CORRECT. ** (CLOSED)

Part: WARNING MESSAGE — ILLUMINATED (DOOR SLIDE) · airframe 20,942 hrs · 9,919 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT PANEL SHOWS "CHECK SLIDE PRESSURE" RIGHT OVER WING EXIT. SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: DECODER — FAULTED (SLIDE PRESSURE) · airframe 20,359 hrs · 9,660 cycles

AIRCRAFT WAS GROUNDED: RIGHT EMERERGENCY EXIT OVER WING AMBER CHECK SLIDE PRESSURE INDICATION ON FLIGHT ATTENDANT PANEL. ** SUPPLEMENTAL REPORT: REPLACED DECODER / ENCODER UNIT B AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 23-73-47.

Part: SLIDE — LOW PRESSURE (R4 DOOR) · airframe 19,776 hrs · 9,403 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR R4 SLIDE PRESSURE LOW AT 1520 AT 70 DEG. DOOR R4 SLIDE PRESSURE SERVICED PER AMM 52-10-00.

Part: RECEPTACLE — MALFUNCTIONED (EXTERNAL POWER) · airframe 18,146 hrs · 8,652 cycles

AIRCRAFT WAS GROUNDED. RAMP EMPLOYEE NOTIFIED PILOTS THAT EXTERNAL POWER CORD WAS HOT TO THE TOUCH AND SMOKING. BURN INDICATIONS ON CORD AND AIRCRAFT. REMOVED AND REPLACED EXTERNAL POWER RECEPTACLE PER AMM 24-41-51.**SUPPLEMENTAL CLOSED**.

Part: HINGE — WORN (RUDDER) · airframe 17,046 hrs · 8,170 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #7 HAS EXCESSIVE PLAY / WEAR AT RIB 11 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: HINGE — WORN (RUDDER) · airframe 17,046 hrs · 8,170 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #2 HAS EXCESSIVE PLAY / WEAR AT RIB 4 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: HINGE — WORN (RUDDER) · airframe 17,046 hrs · 8,170 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #6 HAS EXCESSIVE PLAY / WEAR AT RIB 9 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: HINGE — WORN (RUDDER) · airframe 17,046 hrs · 8,170 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #4 HAS EXCESSIVE PLAY / WEAR AT RIB 6 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: HINGE — WORN (RUDDER) · airframe 17,046 hrs · 8,170 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #5 HAS EXCESSIVE PLAY / WEAR AT RIB 7 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: HINGE — WORN (RUDDER) · airframe 17,046 hrs · 8,170 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #1 HAS EXCESSIVE PLAY / WEAR AT RIB 2 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: FRAME — CRACKED (FRAME 82) · airframe 17,046 hrs · 8,170 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AUXILARY FRAME IN APU COMPARTMENT AT FR 82A BETWEEN S17R AND S18R. REPLACED AUXILARY FRAME PER SRM 51-42-11.

Part: FITTING — CORRODED (FRAME 68) · corrosion level 2 · airframe 17,046 hrs · 8,170 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND AFT PASSENGER / CREW DOOR CUT OUT LOWER AFT CORNER FITTING AT FR 68 AND S23L. REPLACED CORNER FITTING PER SRM 51-72-11.

Part: COUPLING — CORRODED (FRAME 66) · airframe 17,046 hrs · 8,170 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SPLICE COUPLING AT FR 66 AND S23R. REPLACED SPLICE COUPLING PER SRM 51-72-11.

Part: FITTING — CORRODED (FRAME 68) · corrosion level 2 · airframe 17,046 hrs · 8,170 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT DOOR CUT OUT LOWER CORNER FITTING AT FR 68 AND S23R. REPLACED CORNER FITTING PER SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (FRAME 69) · airframe 17,046 hrs · 8,170 cycles

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

Part: SHEAR PLATE — CRACKED (FRAME 69) · airframe 17,046 hrs · 8,170 cycles

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

Part: DOOR SILL — CORRODED (FRAME 68) · corrosion level 2 · airframe 17,046 hrs · 8,170 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT DOOR CUT OUT LOWER SILL AT FR 68 AND S23R. REPLACED LOWER SILL PER SRM 51-71-11.

Part: FITTING — CORRODED (FRAME 67) · corrosion level 2 · airframe 17,046 hrs · 8,170 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND AFT DOOR CUT OUT LOWER CENTER SILL SHAPE FITTING AT FR 67 AND S23L. REPLACED SILL SHAPE FITTING PER SRM 51-72-11.

Part: OUTLET — ODOR (JUMPSEAT) · airframe 16,935 hrs · 8,103 cycles

AIRCRAFT WAS GROUNDED: DURING DECENT FLIGHT ATTENDANTS REPORTED BURNING SMELL WHICH SEEMED TO ORIGINATE IN AREA AROUND 2L JUMPSEAT POWER OUTLET. ODOR WENT AWAY AT LANDING. MAINTENANCE REPLACED OUTLET AT 2L JUMPSEAT PER MM 25-29-00.

Part: PUMP — OVERHEATED (HYD SYSTEM) · airframe 15,938 hrs · 7,620 cycles

AIRCRAFT WAS GROUNDED: PILOT RETURNED TO MIA ON ACCOUNT OF YELLOW HYDRAULIC SYSTEM ENGINE PUMP OVERHEAT. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED #2 EDP CASE DRAIN FILTER AND FOUND CONTAMINATION IN THE DRAIN FILTER. MAINTENANCE REMOVED AND REPLACED THE #2 EDP IAW AMM 29-13-51. OPS CHECK GOOD. UPON REMOVAL, FOUND THE DRIVE SHAFT SHEARED AT THE ACCESSORY GEAR BOX.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 15,559 hrs · 7,443 cycles

AIRCRAFT WAS GROUNDED: FIRST OFFICERS FORWARD WINDSHIELD DELAMINATING AT BOTTOM EDGE. REPLACED WINDSHIELD PER TASK CARD 56-94-01.

Part: ACCUMULATOR — LOW PRESSURE (PAX DOOR) · airframe 14,894 hrs · 7,103 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT HAND AFT PASSENGER/CREW DOOR CYLINDER ACCUMULATOR PRESSURE LOW. MAINTENANCE SERVICED ACCUMULATOR TO PROPER PRESSURE PER AMM 52-10-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: SMOKE DETECTOR — FAULTED (LAVATORY) · airframe 12,922 hrs · 6,227 cycles

LAVATORY SMOKE DETECTION FAULT ILLUMINATED ON ECAM. DID RESET, DISPLAY CLEARED THEN RETURNED. REPLACED FORWARD LAVATORY SMOKE DETECTOR IAW AMM 26-17-15.

Part: PANEL — DETACHED (EMERGENCY LIGHTS) · airframe 12,384 hrs · 5,995 cycles

CLEANERS REPORTED A PANEL LAYING ON THE FLOOR ROW 14DEF. SECURED THE EMERGENCY LIGHT P/S PANEL DOOR IAW AMM 33-51-38. OK FOR SERVICE.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 12,120 hrs · 5,885 cycles

AFT CABIN EMERGENCY POWER SUPPLY FAULTED DURING CIDS TEST. REPLACED AFT CABIN EMERGENCY POWER SUPPLY IAW AMM 33-51-38.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 12,115 hrs · 5,882 cycles

DURING CIDS FUNCTIONAL CHECK, THE AFT CABIN EMERGENCY LIGHT BATTERY PACK FAULTED. REPLACED THE BATTERY PACK IAW AMM 33-51-38.

Part: GIRT BAR — OBSTRUCTED (R3 DOOR SLIDE) · airframe 11,012 hrs · 5,393 cycles

R3 DOOR SLIDE WILL NOT REMAIN ARMED. REMOVED DEBRIS FROM THE GIRT BAR AND ACCOMPLISHED SATISFACTORY TEST IAW AMM 25-62-44.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 10,107 hrs · 4,979 cycles

EMERGENCY LIGHT BY THE R2 DOOR IS MISSING A LENS. REPLACED THE LENS IAW MM 33-51-13. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 9,313 hrs · 4,633 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT 25C EMERGENCY EXIT LIGHT TO ISLE INOPERATIVE. RECONNECTED EMERGENCY LIGHT CONNECTOR PER 33-50-00.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 8,278 hrs · 4,178 cycles

EMERGENCY LIGHTS AT SEATS 24ABC AND 25 ABC ARE INOPERATIVE. REPAIRED BROKEN WIRE AT CONNECTOR 7260VC9 IAW ESPM 20-48-29. OPERATIONAL CHECK NORMAL.

Part: SLIDE — FAILED (L1 DOOR) · airframe 7,896 hrs · 4,009 cycles

DURING CLOSURE OF L1 DOOR FOR DEPARTURE THE ESCAPE SLIDE DISLODGED FROM THE PACK BUT DID NOT DEPLOY. REMOVED AND REPLACED L1 DOOR SLIDE IAW AMM 25-62-44. AIRCRAFT WAS GROUNDED.

Part: TRIM SYSTEM — FAULTY (AUTOFLIGHT SYS) · airframe 7,712 hrs · 3,924 cycles

USING AUTOPILOT NR 2 ACCELERATING OUT OF 10K, AIRCRAFT FLEW IN A RIGHT BANK WITH NO RUDDER TRIM. TURNED OFF AUTOPILOT, COULD NOT TRIM THE AIRCRAFT INTO COORDINATED FLIGHT. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. REPLACED THE NR 1 FAC IAW MM 22-66-34. ACCOMPLISHED OPS TEST OF RUDDER TRIM IAW MM 22-62-00-710-001-A, AFS IAW MM 22-96-00-710-001-A, AND LAND 3 CAPABILITY IAW MM 22-97-00-710-001-A. ALL TESTED GOOD. THE AIRCRAFT WAS GROUNDED.

Part: GROMMET — WORN (SLIDE) · airframe 7,326 hrs · 3,752 cycles

SLIDE LACING GROMMETS HAVE CORROSION AND LACING CORD SHOWS WEAR.

Part: GROMMET — CORRODED (SLIDE) · airframe 7,326 hrs · 3,752 cycles

SLIDE LACING GROMMETS HAVE CORROSION AND LACING CORD SHOWS WEAR.

Part: BRAKE — DRAGGING (MLG) · airframe 5,445 hrs · 2,917 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL. DURING CLIMB RECEIVED NR 1 BRAKE OVERHEAT INDICATION. FOUND BRAKE LOCKED & DRAGGING. R & R NR 1 BRAKE ASSEMBLY IAW AMM 32-42-27-400-001. OPERATIONAL CHECKED GOOD.

Part: SENSOR — NOT SEATED (MLG BRAKE) · airframe 2,045 hrs · 1,248 cycles

HOT BRAKES INDICATION. GEAR LT IN DOWN POSITION IAW QRH FOR COOLING EFFECT. FLIGHT RETURNED & LANDED WITHOUT INCIDENT. RESEATED NUMBER 3 BRAKE TEMP SENSOR & FLIGHT RE DEPARTED. SYS GND CHECKED NORMAL OPERATION CLOSED.