N9016

Part: LAMP — NO TEST (ZONE 200) · airframe 31,275 hrs · 15,272 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT AT LEFT SIDE SEAT ROW 19 INOPERATIVE. MAINTENANCE RELAMPED AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-18.

Part: LAMP — NO TEST (ZONE 200) · airframe 31,275 hrs · 15,272 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT AT LEFT SIDE SEAT ROW 14 IS INOPERATIVE. MAINTENANCE RELAMPED AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-18.

Part: LAMP — NO TEST (ZONE 200) · airframe 31,275 hrs · 15,272 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT AT LEFT SIDE SEAT ROW 18 INOPERATIVE. MAINTENANCE RELAMPED AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-18.

Part: LAMP — NO TEST (ZONE 200) · airframe 31,275 hrs · 15,272 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT AT LEFT SIDE SEAT ROW 15 IS INOPERATIVE. MAINTENANCE RELAMPED AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-18.

Part: PACKING — LEAKING (ZONE 100) · airframe 30,971 hrs · 15,077 cycles

AIRCRAFT WAS GROUNDED: PUNGENT ODOR SMELL ON DOWNWIND LANDING IN CLT. MAINTENANCE REPLACED APU OIL DRAIN PLUG PACKAGING.

Part: UNKNOWN — ODOR (CABIN) · airframe 30,967 hrs · 15,073 cycles

AIRCRAFT WAS GROUNDED: POSSIBLE FUME EVENT TOWARDS REAR OF AC ONLY ON INITIAL CLIMB THEN AGAIN ON IDLE DESCENT, NEVER ON GROUND AFT FA DETECTED ACRID EXHAUST TYPE ODOR.DESCRIBED AS SMELLY FEET AND METALLIC. NOT DETECTED WHILE ON GROUND AIR OR APU BLEED. (OPEN)

Part: PLUG — LEAKING (APU OIL DRAIN) · airframe 30,967 hrs · 15,073 cycles

AIRCRAFT WAS GROUNDED: POSSIBLE FUME EVENT TOWARDS REAR OF AC ONLY ON INITIAL CLIMB THEN AGAIN ON IDLE DESCENT, NEVER ON GROUND AFT FA DETECTED ACRID EXHAUST TYPE ODOR.DESCRIBED AS SMELLY FEET AND METALLIC. NOT DETECTED WHILE ONGROUND AIR OR APU BLEED. **SUPPLEMENTAL REPORT FOR SDR AALA202510129316**(CLOSED) MAINTENANCE ACCOMPLISHED W/C 26L00021001, APU WAS THE SOURCE OF ODOR. REPLACED APU OIL DRAIN PLUG IAW AMM 24-23-51.

Part: POWER SUPPLY — FAULTED (ZONE 200) · airframe 28,871 hrs · 13,868 cycles

AIRCRAFT WAS NOT GROUNDED: FWD EMER EPSU FAULT DURING EPSU TEST. MAINTENANCE REPLACED FWD EPSU BATTERY REF AMM 33-51-38,.

Part: POWER SUPPLY — FAULTED (ZONE 200) · airframe 28,871 hrs · 13,868 cycles

AIRCRAFT WAS NOT GROUNDED: AFT EPSU FAULT AND LEFT EMER EPSU FAULT DURING EPSU TEST.MAINTENANCE REPLACED EPSU BATTERIES AT FWD AND LEFT EMER LOCATIONS REF CMM 33-51-1.

Part: OIL SYSTEM — LEAKING (APU) · airframe 28,051 hrs · 13,376 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED WHILE PASSING 12000 IN DESCENT, WITH ENGINES IDLE 300 KNOTS A STRONG OILY/DIRTYSOCK SMELL OCCURED. MAINTENANCE FOUND THE APU LEAKING OIL AT THE V-BAND SEAL AND REPLACED THE APU PER TASK CARD 26L31049003. ** (CLOSED)

Part: UNKNOWN — ODOR (CABIN) · airframe 28,051 hrs · 13,376 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED WHILE PASSING 12000 IN DESCENT, WITH ENGINES IDLE 300 KNOTS A STRONG OILY/DIRTYSOCK SMELL OCCURED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: SEAL — LEAKING (APU V BAND) · airframe 27,995 hrs · 13,345 cycles

AIRCRAFT WAS GROUNDED: ON DECENT PASSING 6,700 FEET, STRONG OIL/DIRTY SOCK ODOR. ENGINES AT IDLE POWER AND 250 KNOTS. FOUND THE APU LEAKING OIL AT THE V-BAND SEAL AND REPLACED THE APU PER TASK CARD 26L31049003.

Part: UNKNOWN — ODOR (CABIN) · airframe 27,995 hrs · 13,345 cycles

AIRCRAFT WAS GROUNDED: ON DECENT PASSING 6,700 FEET, STRONG OIL/DIRTY SOCK ODOR. ENGINES AT IDLE POWER AND 250 KNOTS. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: CONCENTRATOR — WARNING MESSAGE (NR 1) · airframe 27,653 hrs · 13,118 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO A FLIGHT CONTROL DATA CONCENTRATOR #1 FAULT MESSAGE DURING CLIMBOUT, OUT OF 5000 FEET. THE AIRCRAFT LANDED SAFELY AT DFW AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE REPLACED THE #1 FLIGHT CONTROL DATA CONCENTRATOR 3CE1 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 27-95-34.

Part: FEEDER CABLE — CUT (EMERGENCY LIGHTS) · airframe 27,370 hrs · 12,992 cycles

AIRCRAFT WAS NOT GROUNDED: IN SEAT EMERGENCY LIGHT 13C INOP. FOUND CABLES AT LIGHT CONNECTOR CUT. REPLACED MALE CONTACTS IAW ESPM 20-48-31. LIGHT FULLY OPERATIONAL AND OK FOR SERVICE.

Part: LIFE VEST — MISSING (CABIN) · airframe 27,303 hrs · 12,959 cycles

AIRCRAFT WAS NOT GROUNDED: AIRCRAFT MISSING TWO SPARE LIFE VEST. MAINTENANCE INSTALLED MISSING LIFE VESTS AS REQUIRED.

Part: LIFE VEST — OPEN (COCKPIT) · airframe 27,217 hrs · 12,914 cycles

AIRCRAFT WAS NOT GROUNDED: LIFE-VEST AT FLIGHT DECK ADDITIONAL OBSERVER SEAT OPENED. REPLACED LIFE VEST PER AMM 25-66-00.

Part: DOOR LATCH — LACK OF LUBE (AFT LAVATORY) · airframe 26,910 hrs · 12,761 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT AFT LAVATORY LOCK HARD TO UNLOCK WHEN LOCKED FROM THE INSIDE. PASSENGERS NEED HELP TO UNLOCK THE DOOR. LUBED LATCH ON LEFT AFT LAV DOOR LOCK.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 26,462 hrs · 12,540 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTED CABIN ODOR DIRTY SOCK SMELL, AT TOP OF DESCENT FL280 POWER IDLE TO LANDING STRONGER SMELLING IN AFT CABIN. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: ENGINE — LEAKING (ZONE 400 - NAC/P) · airframe 26,462 hrs · 12,540 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTED CABIN ODOR DIRTY SOCK SMELL, AT TOP OF DESCENT FL280 POWER IDLE TO LANDING STRONGER SMELLING IN AFT CABIN. **SUPPLEMENTAL REPORT FOR AALA202401106459: MAINTENANCE FOUND EVIDENCE OF OIL BEHIND THE #2 ENGINE SPINNER CONE AND IN THE BOOSTER SECTION AND HIGH PRESSURE COMPRESSOR. THE #2 ENGINE WAS REPLACED PER TASK CARD 26L40071001. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.** (CLOSED)

Part: DOOR — INOPERATIVE (ZONE 900 - LAV/G) · airframe 26,206 hrs · 12,411 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS AFT LEFT RIGHT HAND SIDE DOOR INOPERATIVE. HARD TO CLOSE AND HAD TO TAKE OFF HINGES TO OPEN. REPLACED LAVATORY DOOR PER AMM 25-45-19.

Part: LIFE VEST — DAMAGED (ZONE 200 - FUSE) · airframe 26,115 hrs · 12,362 cycles

AIRCRAFT WAS NOT GROUNDED: LIFE VEST AT 26B OPENED AND DAMAGED. MAINTENANCE REPLACED LIFE VEST PER AMM 25-66-52.

Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 25,939 hrs · 12,257 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LAV DOOR LOCK DIFFICULT TO OPERATE FROM THE INSIDE. RE-ADJUSTED THE AFT LAV DOOR AS NEEDED.

Part: DOOR LATCH — LACK OF LUBE (ZONE 200 - FUSE) · airframe 24,993 hrs · 11,712 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR IS DIFFICULT TO OPEN AND CLOSE. CLEANED AND LUBED FLIGHT DECK DOOR LATCHES PER AMM 52-10-00.

Part: BATTERY — DISCHARGED (ZONE 200 - FUSE) · airframe 24,463 hrs · 11,426 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD FLIGHT ATTENDANT SEAT FLASHLIGHT BATTERY DEPLETED. REPLACED BATTERY PER TASK CARD 26L00005005 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: SLIDE RAFT — NO TEST (ZONE 800 - DOORS) · airframe 24,463 hrs · 11,426 cycles

AIRCRAFT WAS GROUNDED: AFTER OPERATIONAL TEST OF EMERGENCY LIGHTS ERROR MESSAGE: CLASS 1 ATA 25-62-41, ESCAPE SLIDE LIGHT EMERGENCY POWER SUPPLY UNIT 10WL FORWARD LEFT MESSAGE ON MCDU. REPLACED THE L1 DOOR SLIDE RAFT PER TASK CARD 26L00025011 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO FAULTS NOTED DURING THE EMERGENCY LIGHTING SYSTYEM.

Part: CONNECTOR — NOT SEATED (ZONE 800 - DOORS) · airframe 24,341 hrs · 11,363 cycles

AIRCRAFT IN BASE MAINTENANCE: L4 DOOR SHOWS OPEN ON LOWER ECAM DOOR PAGE AND FLIGHT ATTENDANT PANEL WHEN IN THE CLOSE POSITION. MAINTENANCE RESEATED ELECTRICAL CONNECTOR TO THE SLIDE ARM INDICATOR LIGHT PER AMM 25-23-46 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-73-00.

Part: HINGE ARM — CRACKED (ZONE 300 - STABS) · airframe 24,341 hrs · 11,363 cycles

AIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER RUDDER #4 BEARING HINGE ARM ASSEMBLY FASTENER HOLE CRACKED. REPLACED HINGE ARM ASSEMBLY PER SRM 51-42-11,

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 24,341 hrs · 11,363 cycles

AIRCRAFT IN BASE MAINTENANCE LEFT HAND HORIZONTAL STABILIZER, #6 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 24,341 hrs · 11,363 cycles

AIRCRAFT IN BASE MAINTENANCE RIGHT HAND HORIZONTAL STABILIZER, #5 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 24,341 hrs · 11,363 cycles

AIRCRAFT IN BASE MAINTENANCE RIGHT HAND HORIZONTAL STABILIZER, #4 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 24,341 hrs · 11,363 cycles

AIRCRAFT IN BASE MAINTENANCE LEFT HAND HORIZONTAL STABILIZER, #4 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 24,341 hrs · 11,363 cycles

AIRCRAFT IN BASE MAINTENANCE RIGHT HAND HORIZONTAL STABILIZER, #1 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 24,341 hrs · 11,363 cycles

AIRCRAFT IN BASE MAINTENANCE RIGHT HAND HORIZONTAL STABILIZER, #2 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 24,341 hrs · 11,363 cycles

AIRCRAFT IN BASE MAINTENANCE LEFT HAND HORIZONTAL STABILIZER, #2 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 24,341 hrs · 11,363 cycles

AIRCRAFT IN BASE MAINTENANCE LEFT HAND HORIZONTAL STABILIZER, #1 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 24,341 hrs · 11,363 cycles

AIRCRAFT IN BASE MAINTENANCE LEFT HAND HORIZONTAL STABILIZER, #3 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 24,341 hrs · 11,363 cycles

AIRCRAFT IN BASE MAINTENANCE RIGHT HAND HORIZONTAL STABILIZER, #6 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 24,341 hrs · 11,363 cycles

AIRCRAFT IN BASE MAINTENANCE LEFT HAND HORIZONTAL STABILIZER, #5 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 24,341 hrs · 11,363 cycles

AIRCRAFT IN BASE MAINTENANCE RIGHT HAND HORIZONTAL STABILIZER, #3 ELEVATOR HINGE FITTING WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: LOCK — LACK OF LUBE (ZONE 900 - LAV/G) · airframe 23,940 hrs · 11,190 cycles

AIRCRAFT WAS NOT GROUNDED: AFT RIGHT LAVATORY DOOR DIFFICULT TO OPEN. MAINTENANCE CLEANED AND LUBRICATED AFT RIGHT LAVATORY DOOR LOCK PER AMM 25-45-21 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 23,334 hrs · 10,915 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT 10WL CLASS 1 FAULT MESSAGE. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 10WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38 AND AMM 33-51-00.

Part: APU — LEAKING (ZONE 100 - FUSE) · airframe 22,239 hrs · 10,341 cycles

AIRCRAFT WAS GROUNDED: MILD TRANSIENT ODOR DURING DECENT AT IDLE THRUST CATEGORY I ODOR NO CLEAR SOURCE NO IRRITATION JUST NOTED BY BOTH PILOTS DISSIPATED AFTER FIVE MINUTES. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE APU. FOUND THE APU LUBE MODULE PACKING LEAKING AND REPLACED IT HOWEVER DURING THE LEAK CHECK MAINTENANCE FOUND OIL LEAKING FROM THE APU LOAD COMPRESSOR DRAIN AND THE APU WILL BE PLACED ON MEL **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: APU — LEAKING (ZONE 100 - FUSE) · airframe 22,239 hrs · 10,341 cycles

AIRCRAFT WAS GROUNDED: MILD TRANSIENT ODOR DURING DECENT AT IDLE THRUST CATEGORY I ODOR NO CLEAR SOURCE NO IRRITATION JUST NOTED BY BOTH PILOTS DISSIPATED AFTER FIVE MINUTES. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE APU. FOUND THE APU LUBE MODULE PACKING LEAKING AND REPLACED IT HOWEVER DURING THE LEAK CHECK MAINTENANCE FOUND OIL LEAKING FROM THE APU LOAD COMPRESSOR DRAIN AND THE APU WILL BE PLACED ON MEL **SUPPLEMENTAL REPORT FOR AALA202206284528: REPLACED APU PER TASK CARD 26L3104900. ** (CLOSED)

Part: OIL CAP — LOOSE (ZONE 100 - FUSE) · airframe 22,184 hrs · 10,316 cycles

AIRCRAFT WAS GROUNDED: FUME/ODOR EVENT DURING DESCENT. FOLLOWED QUICK ACTIONS AND THE ODOR WENT AWAY. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE APU. **SUPPLEMENTAL REPORT FOR AALA202206213194: MAINTENANCE FOUND THE APU OIL SERVICING CAP LEVER LOOSE AND LEAKING. RE-INSTALLED APU OIL SERVICING CAP. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED. ** (CLOSED)

Part: APU — ODOR (ZONE 100 - FUSE) · airframe 22,184 hrs · 10,316 cycles

AIRCRAFT WAS GROUNDED: FUME/ODOR EVENT DURING DESCENT. FOLLOWED QUICK ACTIONS AND THE ODOR WENT AWAY. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE APU. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: SLIDING WINDOW — OUT OF ADJUST (ZONE 200 - FUSE) · airframe 21,904 hrs · 10,193 cycles

AIRCRAFT WAS GROUNDED: FIRST OFFICERS SLIDING WINDOW DIFFICULT TO OPEN. ADJUSTED SLIDING WINDOW AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 56-12-11.

Part: SLIDING WINDOW — OUT OF ADJUST (ZONE 200 - FUSE) · airframe 21,904 hrs · 10,193 cycles

AIRCRAFT WAS GROUNDED: CAPTAIN'S SLIDING WINDOW DIFFICULT TO OPEN. ADJUSTED SLIDING WINDOW AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 56-12-11.

Part: OVEN — ODOR (FWD GALLEY) · airframe 20,281 hrs · 9,502 cycles

AIRCRAFT WAS NOT GROUNDED: FIRST CLASS GALLEY OVEN NUMBER 2 HAS A STRONG ELECTRICAL BURNING SMELL WHEN OPERATING. CIRCUIT BREAKER DID NOT POP. REMOVED AND REPLACED FORWARD GALLEY NUMBER 2 OVEN PER AMM 25-35-19-0401.

Part: MOTOR — NONE (ZONE 100 - FUSE) · airframe 20,073 hrs · 9,386 cycles

AIRCRAFT WAS GROUNDED: CABIN PRESSURE SYSTEM 1 AND 2 FAULT UNABLE TO CONTROL PRESSURIZATION WITH MANUAL. REPLACED OUTFLOW VALVE MANUAL MOTOR (10HL-50) AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-31-51.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 19,822 hrs · 9,296 cycles

AIRCRAFT WAS NOT GROUNDED: IN FLIGHT ON CLIMB OUT AT 3000 CABIN PRESSURE SYSTEM INOPERATIVE. REPLACED #2 CABIN PRESSURE CONTROLLER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 21-31-00-710-002A.

Part: SLIDE — DEFECTIVE (R1 DOOR) · airframe 19,744 hrs · 9,260 cycles

AIRCRAFT WAS GROUNDED: WHILE REPLACING R1 DOOR SLIDE WITH A NEW SLIDE THE REPLACEMENT SLIDE UNWRAPPED RESULTING IN THE DEPLOYMENT OF THE DOOR DAMPER CYLINDER. MAINTENANCE REMOVED THE DEFECTIVE SLIDE AND INSTALLED A SERVICEABLE UNIT PER TASK CARD 26L00025011.

Part: COMPUTER — FAULTED (E/E VENTILATION) · airframe 18,561 hrs · 8,739 cycles

AIRCRAFT WAS NOT GROUNDED: TEN MINUTES AFTER TAKEOFF BOTH THE BLOWER AND EXTRACT FANS FAULTS LIGHTS ILLUMINATED AMBER BLOWER VENT EXTRACT ILLUMINATED ON CABIN PRESSURE PAGE AVIONICS SMOKE ON LANDING. REPLACED THE AVIONIC EQUIPMENT VENTILATION COMPUTER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 21-26-34

Part: WARNING MESSAGE — FALSE ACTIVATION (EXHAUST FAN) · airframe 18,561 hrs · 8,739 cycles

AIRCRAFT WAS GROUNDED: EICAS BLOWER EXTRACT FAN FAULT. PERFORMED SYSTEM RESET PER AMM 21-26-00-710-001-A.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 18,173 hrs · 8,586 cycles

AIRCRAFT WAS NOT GROUNDED. AFT LEFT FLIGHT ATTENDANT FLASHLIGHT DOES NOT FLASH GREEN OR RED. REMOVED AND REPLACED FLASHLIGHT, PER AMM 25-65-00.

Part: CONNECTOR — MISROUTED (EMERGENCY LIGHTS) · airframe 17,589 hrs · 8,333 cycles

AIRCRAFT WAS GROUNDED. FOUND NR 1 CABIN CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED THAT LIGHT ASSEMBLY AND FOUND THE TWO PLUGS CRISSCROSSED. RESEATED PLUGS, IAW AMM 33.50.00 THE EMERGENCY LIGHTING SYSTEM TESTED NORMAL.

Part: CONTROL UNIT — LEAKING (APU) · airframe 17,546 hrs · 8,314 cycles

AIRCRAFT WAS GROUNDED. CREW REPORTED ODOR IN THE CABIN. ACCOMPLISHED TASK CARD 26L00021001 AND FOUND OIL IN THE APU PLENUM. SUPPLEMENTAL INFORMATION: REMOVED AND REPLACED FUEL CONTROL UNIT, IAW AMM 49-32-11, LEAK CHECK GOOD. NO OIL LEAK NOTED AT THIS TIME. FUEL CONTROL UNIT OPERATIONAL CHECK GOOD. ACCOMPLISHED J/C 26L00021004.

Part: PIN — CRACKED (MLG) · airframe 17,498 hrs · 8,292 cycles

AIRCRAFT WAS NOT GROUNDED. CRACK IN APEX PIN OF LT MLG TORQUE LINK. REPLACED APEX PIN WITH NEW, IAW AMM 32-11-29.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 17,282 hrs · 8,174 cycles

AIRCRAFT WAS GROUNDED: FIRST OFFICER`S AFT WINDOW EXCESSIVELY HOT TO TOUCH AND DELAMINATING. REMOVED AND REPLACED RIGHT COCKPIT FIXED WINDOW (R3), PER AMM 56-11-12.

Part: BATTERY — DISCHARGED (CABIN) · airframe 16,663 hrs · 7,862 cycles

AIRCRAFT NOT GROUNDED: FWD L EPSU (10WL) FAILED ON EPSU SYS TEST. REPLACED EPSU BATTERY AT FWD L EPSU (10WL) IAW AMM 33-51-38.

Part: BATTERY — DISCHARGED (CABIN) · airframe 16,663 hrs · 7,862 cycles

AIRCRAFT NOT GROUNDED: EMER L EPSU (11WL) FAILED ON EPSU SYS TEST. REPLACED EPSU BATTERY AT EMER L EPSU (11WL) IAW AMM 33-51-38.

Part: SEAT — OUT OF ADJUST (CABIN) · airframe 16,251 hrs · 7,670 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 13F EXTENDS INTO THE EMERGENCY EXIT ROW. ADJUSTED SEAT 13F PER AMM 25-21-00.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 16,236 hrs · 7,661 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN WET AREA SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.

Part: HINGE — WORN (RUDDER) · airframe 16,236 hrs · 7,661 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 16,236 hrs · 7,661 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 16,236 hrs · 7,661 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: HINGE — WORN (RUDDER) · airframe 16,236 hrs · 7,661 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 16,236 hrs · 7,661 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: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 16,236 hrs · 7,661 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN WET AREA SHEAR PLATE AT FR 69 AND S23R. REPLACED SHEAR PLATE PER SRM 51-42-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,236 hrs · 7,661 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CENTER FITTING BETWEEN FR 66 AND FR 68 AT S23L. REPLACED CENTER FITTING PER SRM 51-72-11. SUPPLEMENT TO DEFINE STRINGER DIMENSION SIDE (S23L) IN SECTION 4 & 7.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 14,015 hrs · 6,601 cycles

CIDS DISPLAYED AN EPSU FAILED 13WL, AFT LEFT. DURING A SYSTEM FUNCTIONAL CHECK. REMOVED AND REPLACED THE ESPU IAW AMM 33-51-38. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 13,882 hrs · 6,545 cycles

EMERGENCY FLASHLIGHT AT THE FLIGHT ATTENDANT L1 STATION WAS INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: UNKNOWN — VIBRATION (AIRFRAME) · airframe 13,412 hrs · 6,340 cycles

DURING DECENT FROM 14000 FT TO 10000 FT, WITH SPEED BRAKE DEPLOYED AT 1/4 TO 1/2 WAY, THE AIRCRAFT VIBRATED MODRATLY AND MORE THAN NORMAL, 260 KNOTS AND DECENDING. THE AIRCRAFT WAS GROUNDED. MAINTENANCE ACCOMPLISHED TSM 27-30-00-810 AND GVI OF ALL SPOILERS FOR CONDITION AND SECURITY. ALL SPOILERS WERE SECURE IAW AMM 27-64-00. MAINTENANCE ALSO PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 12,657 hrs · 5,989 cycles

WHILE PERFORMING AN OPERATIONAL TEST OF THE EMERGENCY POWER SUPPLY UNIT SYSTEMS, RECEIVED CODE 335100 BATTERY/EPSU 12, EMER R. REPLACED THE POWER SUPPLY BATTERY PACK 12WL IAW AMM 33-51-38. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 11,259 hrs · 5,373 cycles

THE AIRCRAFT WAS GROUNDED. REF 3390977 REPORTED CABIN ODOR. SUSPECT LEFT HAND ENGINE AS ODOR SOURCE. AIRCRAFT REQUIRE MAINTENANCE FERRY FLIGHT. INSPECTED AIRCRAFT FOUND IN SAFE CONDITION FOR MAINTENANCE FERRY FLIGHT CTG-MIA.

Part: A/C PACK — ODOR (LEFT) · airframe 11,259 hrs · 5,373 cycles

AIRCRAFT HAS OILY ODOR, VERY STRONG, LIKE DIRTY SOCKS OR VAPORZED OIL. PACKS WITH GROUND AIR CART, LEFT PACK HAD OILY ODOR FOR 5 MINUTES OF OPERATION. RIGHT PACK DID NOT HAVE ANY ODOR. RAN PACKS WITH GROUND AIR CART AND ENGINES IAW 5A1/213, NO FURTHER ODOR FOUND. ALSO RAN ENGINES FOR 30 MINUTES AT POWER SETTINGS WITH NO ODOR FOUND. BLEED LEFT AIR SUPPLY SYSTEM FOUND TO BE INOPERABLE. AIRCRAFT WAS GROUNDED. REACTIVATED THE LEFT AIR CONDITIONING PACK, ACCOMPLISHED A PACK OPS CHECK IAW MM 21-35-00. COMPLETED CARD 05-96-72 AND CARD 05-96-86, FOR DECONTAMINATION CONTROL SYSTEMS.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PUMP) · airframe 10,986 hrs · 5,251 cycles

AFTER TAKE OFF, THE CENTER TANK PUMP 2 LOW PRESSURE ECAM ILLUMINATED. ACCOMPLISHED ECAM PROCEDURE AND TURNED OFF THE PUMP. PERFORMED AN OPERATIONAL TEST OF THE CENTER TANK PUMP 2, FOUND SATISFACTORY IAW AMM 28-21-51-710-052-A.

Part: WARNING LIGHT — FALSE ACTIVATION (NR 2 FUEL PUMP) · airframe 9,072 hrs · 4,426 cycles

CENTER TANK NR 2 FUEL PUMP ECAM FAULT, WHEN PUMP TURNED ON. MAINTENANCE ACCOMPLISHED OPERATIONAL TEST OF THE NR 2 CENTER FUEL PUMP IAW AMM 28-21-00-710-007A. NO FAULTS FOUND.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 8,562 hrs · 4,197 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY EXIT LIGHTS ILLUMINATED OVER ALL DOORS EXITS AND OVER WINGS UPON POWER TRANSFER (STAY ON WHEN TURNED OFF). MAINTENANCE FOUND EMERGENCY POWER SUPPLY UNIT FORWARD L (10WL) AT FAULT. REPLACED 10WL POWER SUPPLY PER AMM 33-51-38.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 8,301 hrs · 4,070 cycles

DURING CHECK OF EMERGENCY CYLINDER PRESSURE, FOUND IT TO BE LOW AT THE R2 DOOR. SERVICED CYLINDER IAW AMM 52-10-00. AIRCRAFT WAS GROUNDED.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 8,240 hrs · 4,042 cycles

R2 DOOR EMERGENCY CYLINDER HAD LOW PRESSURE. SERVICED THE CYLINDER IAW AMM 52-10-00.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 7,958 hrs · 3,915 cycles

AIRCRAFT WAS NOT GROUNDED. R2 EMERGENCY DOOR DAMPER CYLINDER PRESSURE IS LOW. SERVICED CYLINDER IAW AMM 52-10-00. OPERATIONAL CHECK GOOD.

Part: CYLINDER — LOW PRESSURE (ENTRY DOOR) · airframe 7,919 hrs · 3,899 cycles

AIRCRAFT WAS NOT GROUNDED. AFT ENTRY DOOR DAMPER CYLINDER PRESSURE IS LOW. SERVICED CYLINDER IAW AMM 52-10-00. OPERATIONAL CHECK GOOD.

Part: EXTRACTOR — CLOGGED (AC BAY) · airframe 5,859 hrs · 2,965 cycles

AIRCRAFT WAS GNDED. LT AIR CONDITIONING PACK PUTS OUT VISIBLE MOISTURE & EXCESSIVE ODOR THROUGHOUT CABIN WHILE ON APU AS SOURCE. R & R WATER EXTRACTOR IAW AMM 21-52-16.

Part: SELECTOR VALVE — INOPERATIVE (ZONE 700) · airframe 1,461 hrs · 918 cycles

DURING GEAR RETRACTION MAIN & NOSE GEAR DOORS DID NOT RETRACT. FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LG DOOR SELECTOR VLV. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: SAFETY VALVE — INOPERATIVE (LANDING GEAR) · airframe 1,431 hrs · 899 cycles

WHEN SELECTING GEAR UP, LG DOORS DID NOT CLOSE. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LG SAFETY VLV 49GA & RELAY 53GA. SYS GND CHECKED NORMAL, OPERATIONS CLOSED.