N925UY

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 33,638 hrs · 13,792 cycles

AIRCRAFT WAS NOT GROUNDED: R4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 33,522 hrs · 13,739 cycles

AIRCRAFT WAS NOT GROUNDED: CIDS PANEL CAUTION: 3L CHECK DOOR PRESSURE. MAINTENANCE SERVICED 3L DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-20-00.

Part: DOOR LATCH — STICKING (ZONE 800) · airframe 33,534 hrs · 13,743 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR LOCKING MECHANISM HARD TO OPEN AND CLOSE. MAINTENANCE LUBED LATCHES ON FLIGHT DECK DOOR AND ACCOMPLISHED A SATISFACTROY OPERATIONAL CHECK PER AMM 52-51-00.

Part: FITTING — FOD (GIRT BAR) · airframe 33,512 hrs · 13,735 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS 4R DOOR DIFFICULT TO ARM. MAINTENANCE REMOVED DEBRIS, LUBRICATED GIRT BAR LATCHES AND ATTACHMENT FITTINGS.

Part: BATTERY — NO TEST (ZONE 200) · airframe 32,012 hrs · 13,128 cycles

AIRCRAFT WAS NOT GROUNDED: DURING SYSTEM TEST OF THE EMERGENCY POWER SUPPLY UNITS A BATTERY FAULT DISPLAYED FOR EMERGENCY POWER SUPPLY UNIT 12WL. MAINTENANCE REPLACED THE BATTERY FOR EMERGENCY POWER SUPPLY UNIT 12WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.

Part: BATTERY — NO TEST (ZONE 200) · airframe 32,012 hrs · 13,128 cycles

AIRCRAFT WAS NOT GROUNDED: DURING SYSTEM TEST OF THE EMERGENCY POWER SUPPLY UNITS A BATTERY FAULT DISPLAYED FOR EMERGENCY POWER SUPPLY UNIT 10WL. MAINTENANCE REPLACED THE BATTERY FOR EMERGENCY POWER SUPPLY UNIT 10WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.

Part: BATTERY — NO TEST (ZONE 200) · airframe 31,770 hrs · 13,028 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND SEAT ROWS 28,29,32,33 AND 34 EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED THE BATTERY FOR EMERGENCY POWER SUPPLY UNIT 14WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM PER AMM 33-51-38.

Part: BATTERY — NO TEST (ZONE 200) · airframe 31,770 hrs · 13,028 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND SEAT ROWS 14,15,17,18,21 AND 22 EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED THE BATTERY FOR EMERGENCY POWER SUPPLY UNIT 11WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM PER AMM 33-51-38.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 31,252 hrs · 12,815 cycles

AIRCRAFT WAS NOT GROUNDED: R4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 31,252 hrs · 12,815 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 29,594 hrs · 12,045 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS 2R EMERGENCY FLASHLIGHT INOPERATIVE. INSTALLED NEW LIGHT AT 2R.

Part: SMOKE DETECTOR — FALSE ACTIVATION (ZONE 900 - LAV/G) · airframe 28,871 hrs · 11,756 cycles

AIRCRAFT WAS NOT GROUNDED: ON DESCENT INTO CLT ECAM ALERT "SMOKE, LAVITORY SMOKE" CAME ON FOR LESS THAN ONE MINUTE THEN CLEARED. FLIGHT ATTENDANTS CHECKED THE LAVITORIES AND DID NOT FIND ANYTHING. MAINTENANCE PERFORMED OPERATIONAL TEST PER TSM 26-17-00. INTERROGATED MCDU, RAN SELF-TEST AND NO FAULTS APPEARED.

Part: GIRT BAR — LACK OF LUBE (R4 DOOR) · airframe 28,592 hrs · 11,641 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 4R ARMING / DISARMING LEVER EXTREMELY DIFFICULT TO ARM. CLEANED AND LUBED GIRT BAR LANDING AREA AND GIRT ATTACHMENT FITTINGS, DOOR ARMING CHECKS NORMAL PER AMM 52-13-00.

Part: ENGINE — STALLED (NR 2) · airframe 28,551 hrs · 11,623 cycles

AIRCRAFT WAS GROUNDED: THE AIRCRAFT DIVERTED TO PHX, AT FL 320 THE #2 ENGINE BEGAN STALLING, FLIGHT CREW REDUCED POWER PER QRH PROCEDURES AND ENGINE WAS ABLE TO ACCEPT SOME POWER AT REDUCED SETTING. THE AIRCRAFT LANDED AT PHX WITHOUT INCIDENT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: ENGINE — STALLED (ZONE 400 - NAC/P) · airframe 28,551 hrs · 11,623 cycles

AIRCRAFT WAS GROUNDED: THE AIRCRAFT DIVERTED TO PHX, AT FL 320 THE #2 ENGINE BEGAN STALLING, FLIGHT CREW REDUCED POWER PER QRH PROCEDURES AND ENGINE WAS ABLE TO ACCEPT SOME POWER AT REDUCED SETTING. THE AIRCRAFT LANDED AT PHX WITHOUT INCIDENT. MAINTENANCE FOUND METAL IN THE BLEED VALVES AND DAMAGE STARTING AT THE 7TH STAGE COMPRESSOR BLADES DURING THE BORESCOPE INPECTION. THE ENGINE WAS REPLACED PER TASK CARD 26L40071004.

Part: DAMPER — LOW PRESSURE (ZONE 800 - DOORS) · airframe 26,278 hrs · 10,541 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT PANEL CHECK DOOR PRESSURE R3 DOOR. SERVICED R3 DOOR DAMPER PER AMM 52-22-00.

Part: RESERVOIR — FAULT MESSAGE (ZONE 800 - DOORS) · airframe 25,361 hrs · 10,071 cycles

AIRCRAFT WAS NOT GROUNDED: FOWARD FLIGHT ATTENDANT CIDS PANEL SHOWS 2L CHECK SLIDE PRESSURE. MAINTENANCE REPLACED 2L DOOR ESCAPE SLIDE RESERVOIR PER AMM 25-62-49 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO MESSAGES NOTED.

Part: O-RING — LEAKING (ZONE 100 - FUSE) · airframe 25,240 hrs · 10,009 cycles

AIRCRAFT WAS GROUNDED: FUMES REPORTED DURING CLIMB AND DURING DESCENT. MAINTENANCE FOUND THE APU STARTER MOTOR O-RING LEAKING OIL AND REPLACED IT PER AMM 49-42-51. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: ENGINE — STALLED (ZONE 400 - NAC/P) · airframe 23,708 hrs · 9,306 cycles

AIRCRAFT WAS GROUNDED: ECAM ENGINE COMPRESSOR 2 STALL ON CLIMB OUT AFTER TAKEOFF. 7000' MSL,250KIAS,CLIMB POWER. LOUD BANG, YAW TO RIGHT, DEGRADED EPR- ENGINE RECOVERED IMMEDIATELY WITH OUT PILOT INTERVENTION. **SUPPLEMENTAL REPORT FOR AALA202209191152: MAINTENANCE ACCOMPLISHED BORESCOPE INSPECTION AND FOUND DAMAGE TO THE 6TH STAGE HIGH STAGE COMPRESSOR AND REPLACED #2 ENGINE PER TASK CARD 26L40071004 ** (CLOSED)

Part: ENGINE — STALLED (ZONE 400 - NAC/P) · airframe 23,708 hrs · 9,306 cycles

AIRCRAFT WAS GROUNDED: ECAM ENGINE COMPRESSOR 2 STALL ON CLIMB OUT AFTER TAKEOFF. 7000' MSL,250KIAS,CLIMB POWER. LOUD BANG, YAW TO RIGHT, DEGRADED EPR- ENGINE RECOVERED IMMEDIATELY WITH OUT PILOT INTERVENTION. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: DECODER — FAULTY (ZONE 800 - DOORS) · airframe 23,326 hrs · 9,145 cycles

AIRCRAFT WAS NOT GROUNDED: 1L EMERGENCY EXIT SLIDE SHOWS LOW PRESSURE. REMOVED AND REPLACED DECODER ENCODER UNIT-B 1L DOOR (300RH1) PER AMM 23-73-47.

Part: NONE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 23,304 hrs · 9,133 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT STATES L1 DOOR SLIDE PRESSURE NEEDS TO BE CHECKED. SERVICED L1 DOOR ASSIST BOTTLE IAW AMM 52-10-00.

Part: PRESSURE SWITCH — NONE (ZONE 400 - NAC/P) · airframe 23,140 hrs · 9,052 cycles

AIRCRAFT WAS GROUNDED: ECAM HYDRAULIC YELLOW ENGINE 2 PUMP LOW PRESSURE ON CLIMB OUT. CREW TURNED ENGINE 2 PUMP OFF PER ECAM ACTION. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ORD WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED ENGINE PUMP PRESSURE SWITCH PER AMM 29-13-17 AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK.

Part: DOOR — LACK OF LUBE (ZONE 800 - DOORS) · airframe 22,958 hrs · 8,977 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR HARD TO OPEN AND CLOSE. LUBED FLIGHT DECK DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: GROUND WIRE — UNSECURE (ZONE 200 - FUSE) · airframe 21,707 hrs · 8,428 cycles

AIRCRAFT WAS NOT GROUNDED: ROW 36 CEILING PANEL OVERHEAD EXIT LIGHT INOPERATIVE. **SUPPLEMENTAL REPORT FOR AALA202201255364: FOUND OVERHEAD EMERGENCY LIGHT GROUND WIRE NOT SECURES AND SECURED IT PER TSM 33-51-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED. **(CLOSED)

Part: NONE — NONE · airframe 21,707 hrs · 8,428 cycles

AIRCRAFT WAS NOT GROUNDED: ROW 36 CEILING PANEL OVERHEAD EXIT LIGHT INOPERATIVE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN)

Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT LAVATORY) · airframe 19,935 hrs · 7,694 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY SMOKE LEFT REAR LAVATORY (LAV D) NO EVIDENCE OF SMOKE/FIRE. WARNING WAS INTERMITTENT ONLY LASTED FIVE SECONDS. NO CURRENT OR PREVIOUS FAULTS. PER AMM 26-17-00. SUSPECTING CUSTOMER WAS VAPING.

Part: TIRE — BLOWN (LT MLG) · airframe 19,726 hrs · 7,609 cycles

AIRCRAFT WAS GROUNDED: AFTER LANDING LEFT MAIN BRAKE TEMP INCREASED RAPIDLY UPON GATE ARRIVAL BOTH LEFT MAIN TIRES BLEW. PREFORMED INSPECTION OF LEFT MAIN LANDING GEAR AXLE PER AMM 32-11-00-200-007 AND FOUND TO BE WITHIN LIMITS FOR HARDNESS CHECK. REPLACED MAIN LANDING GEAR #1 (AALA202106149012) AND #2 (AALA202106229009) BRAKE ASSEMBLIES PER AMM 32-42-27. REPLACED MAIN LANDING GEAR #1 (AALA202106229010) AND #2 (AALA202106229011) WHEEL ASSEMBLIES PER AMM 32-41-11. REPLACED #1 (AALA202106229012) AND #2 (AALA202106229013) TACHOMETERS PER AMM 32-42-57. REPLACED BRAKE TEMPERATURE MONITOR UNIT (AALA202106229014) PER AMM 32-47-18. A SATISFACTORY OPERATIONAL CHECK OF ALL REPLACED ITEMS AND THE BRAKING SYSTEM WAS ACCOMPLISHED.

Part: TIRE — BLOWN (LT MLG) · airframe 19,726 hrs · 7,609 cycles

AIRCRAFT WAS GROUNDED: AFTER LANDING LEFT MAIN BRAKE TEMP INCREASED RAPIDLY UPON GATE ARRIVAL BOTH LEFT MAIN TIRES BLEW. PREFORMED INSPECTION OF LEFT MAIN LANDING GEAR AXLE PER AMM 32-11-00-200-007 AND FOUND TO BE WITHIN LIMITS FOR HARDNESS CHECK. REPLACED MAIN LANDING GEAR #1 (AALA202106149012) AND #2 (AALA202106229009) BRAKE ASSEMBLIES PER AMM 32-42-27. REPLACED MAIN LANDING GEAR #1 (AALA202106229010) AND #2 (AALA202106229011) WHEEL ASSEMBLIES PER AMM 32-41-11. REPLACED #1 (AALA202106229012) AND #2 (AALA202106229013) TACHOMETERS PER AMM 32-42-57. REPLACED BRAKE TEMPERATURE MONITOR UNIT (AALA202106229014) PER AMM 32-47-18. A SATISFACTORY OPERATIONAL CHECK OF ALL REPLACED ITEMS AND THE BRAKING SYSTEM WAS ACCOMPLISHED.

Part: TACHOMETER — DEFECTIVE (LT MLG) · airframe 19,726 hrs · 7,609 cycles

AIRCRAFT WAS GROUNDED: AFTER LANDING LEFT MAIN BRAKE TEMP INCREASED RAPIDLY UPON GATE ARRIVAL BOTH LEFT MAIN TIRES BLEW. PREFORMED INSPECTION OF LEFT MAIN LANDING GEAR AXLE PER AMM 32-11-00-200-007 AND FOUND TO BE WITHIN LIMITS FOR HARDNESS CHECK. REPLACED MAIN LANDING GEAR #1 (AALA202106149012) AND #2 (AALA202106229009) BRAKE ASSEMBLIES PER AMM 32-42-27. REPLACED MAIN LANDING GEAR #1 (AALA202106229010) AND #2 (AALA202106229011) WHEEL ASSEMBLIES PER AMM 32-41-11. REPLACED #1 (AALA202106229012) AND #2 (AALA202106229013) TACHOMETERS PER AMM 32-42-57. REPLACED BRAKE TEMPERATURE MONITOR UNIT (AALA202106229014) PER AMM 32-47-18. A SATISFACTORY OPERATIONAL CHECK OF ALL REPLACED ITEMS AND THE BRAKING SYSTEM WAS ACCOMPLISHED.

Part: BRAKE — OVERTEMP (LT MLG) · airframe 19,726 hrs · 7,609 cycles

AIRCRAFT WAS GROUNDED: AFTER LANDING LEFT MAIN BRAKE TEMP INCREASED RAPIDLY UPON GATE ARRIVAL BOTH LEFT MAIN TIRES BLEW. PREFORMED INSPECTION OF LEFT MAIN LANDING GEAR AXLE PER AMM 32-11-00-200-007 AND FOUND TO BE WITHIN LIMITS FOR HARDNESS CHECK. REPLACED MAIN LANDING GEAR #1 (AALA202106149012) AND #2 (AALA202106229009) BRAKE ASSEMBLIES PER AMM 32-42-27. REPLACED MAIN LANDING GEAR #1 (AALA202106229010) AND #2 (AALA202106229011) WHEEL ASSEMBLIES PER AMM 32-41-11. REPLACED #1 (AALA202106229012) AND #2 (AALA202106229013) TACHOMETERS PER AMM 32-42-57. REPLACED BRAKE TEMPERATURE MONITOR UNIT (AALA202106229014) PER AMM 32-47-18. A SATISFACTORY OPERATIONAL CHECK OF ALL REPLACED ITEMS AND THE BRAKING SYSTEM WAS ACCOMPLISHED.

Part: TACHOMETER — DEFECTIVE (LT MLG) · airframe 19,726 hrs · 7,609 cycles

AIRCRAFT WAS GROUNDED: AFTER LANDING LEFT MAIN BRAKE TEMP INCREASED RAPIDLY UPON GATE ARRIVAL BOTH LEFT MAIN TIRES BLEW. PREFORMED INSPECTION OF LEFT MAIN LANDING GEAR AXLE PER AMM 32-11-00-200-007 AND FOUND TO BE WITHIN LIMITS FOR HARDNESS CHECK. REPLACED MAIN LANDING GEAR #1 (AALA202106149012) AND #2 (AALA202106229009) BRAKE ASSEMBLIES PER AMM 32-42-27. REPLACED MAIN LANDING GEAR #1 (AALA202106229010) AND #2 (AALA202106229011) WHEEL ASSEMBLIES PER AMM 32-41-11. REPLACED #1 (AALA202106229012) AND #2 (AALA202106229013) TACHOMETERS PER AMM 32-42-57. REPLACED BRAKE TEMPERATURE MONITOR UNIT (AALA202106229014) PER AMM 32-47-18. A SATISFACTORY OPERATIONAL CHECK OF ALL REPLACED ITEMS AND THE BRAKING SYSTEM WAS ACCOMPLISHED.

Part: MONITOR — DEFECTIVE (MLG BRAKE) · airframe 19,726 hrs · 7,609 cycles

AIRCRAFT WAS GROUNDED: AFTER LANDING LEFT MAIN BRAKE TEMP INCREASED RAPIDLY UPON GATE ARRIVAL BOTH LEFT MAIN TIRES BLEW. PREFORMED INSPECTION OF LEFT MAIN LANDING GEAR AXLE PER AMM 32-11-00-200-007 AND FOUND TO BE WITHIN LIMITS FOR HARDNESS CHECK. REPLACED MAIN LANDING GEAR #1 (AALA202106149012) AND #2 (AALA202106229009) BRAKE ASSEMBLIES PER AMM 32-42-27. REPLACED MAIN LANDING GEAR #1 (AALA202106229010) AND #2 (AALA202106229011) WHEEL ASSEMBLIES PER AMM 32-41-11. REPLACED #1 (AALA202106229012) AND #2 (AALA202106229013) TACHOMETERS PER AMM 32-42-57. REPLACED BRAKE TEMPERATURE MONITOR UNIT (AALA202106229014) PER AMM 32-47-18. A SATISFACTORY OPERATIONAL CHECK OF ALL REPLACED ITEMS AND THE BRAKING SYSTEM WAS ACCOMPLISHED.

Part: BRAKE ASSY — OVERTEMP (MLG) · airframe 19,725 hrs · 7,608 cycles

AIRCRAFT WAS GROUNDED: AFTER LANDING LEFT MAIN BRAKE TEMP INCREASED RAPIDLY UPON GATE ARRIVAL BOTH LEFT MAIN TIRES BLEW. PREFORMED INSPECTION OF LEFT MAIN LANDING GEAR AXLE PER AMM 32-11-00-200-007 AND FOUND TO BE WITHIN LIMITS FOR HARDNESS CHECK. REPLACED MAIN LANDING GEAR #1 (AALA202106149012) AND #2 (AALA202106229009) BRAKE ASSEMBLIES PER AMM 32-42-27. REPLACED MAIN LANDING GEAR #1 (AALA202106229010) AND #2 (AALA202106229011) WHEEL ASSEMBLIES PER AMM 32-41-11. REPLACED #1 (AALA202106229012) AND #2 (AALA202106229013) TACHOMETERS PER AMM 32-42-57. REPLACED BRAKE TEMPERATURE MONITOR UNIT (AALA202106229014) PER AMM 32-47-18. A SATISFACTORY OPERATIONAL CHECK OF ALL REPLACED ITEMS AND THE BRAKING SYSTEM WAS ACCOMPLISHED.

Part: HINGE ARM — EXCESS PLAY (RT ELEVATOR) · airframe 19,562 hrs · 7,542 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM NUMBER 3 ELEVATOR ON RIGHT HORIZONTAL STABILIZER. REMOVED AND REPLACED HINGE ARM NUMBER 3 ON RIGHT ELEVATOR PER AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (RT ELEVATOR) · airframe 19,562 hrs · 7,542 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 4 ELEVATOR ON RIGHT HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING NUMBER 4 ON RIGHT HORIZONTAL STABILIZER PER AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (RT ELEVATOR) · airframe 19,562 hrs · 7,542 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 6 ELEVATOR ON RIGHT HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING #6 ON RIGHT HORIZONTAL STABILIZER IAW AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 19,562 hrs · 7,542 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 1 ON RIGHT HAND HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM END FITTING 1 PER AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 19,562 hrs · 7,542 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 2 ON RIGHT HAND HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM END FITTING 2 PER AMM 55-16-42-000-001-A. AND 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 19,562 hrs · 7,542 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 5 ON RIGHT HAND HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM END FITTING 5 PER AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (LT ELEVATOR) · airframe 19,562 hrs · 7,542 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 6 ON LEFT HAND HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM END FITTING 6 PER AMM 55-16-42-000-001-A AND 55-16-42-400-001-A.

Part: FLOOR PANEL — DELAMINATED (FWD CARGO) · airframe 19,562 hrs · 7,542 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 131GF IN FORWARD CARGO COMPARTMENT. REPLACED FLOOR PANEL 131GF IN FWD CARGO COMPARTMENT WITH NEW REPLACEMENT MATERIAL IAW A321 SRM 53-02-00-300-011, PARA 2.A FIG 1 AND IRM 9 701, REV K.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 19,562 hrs · 7,542 cycles

AIRCRAFT IN BASE MAINTENANCE: L=1.14 INCH X W=1.03 INCH DELAMINATED AREA ON ELEVATOR AT RIB 1 + 6.46 INCH AND 16.86 INCH FROM TRAILING EDGE. REPAIRED UPPER SKIN ELEVATOR ON LEFT HORIZONTAL STABILIZER IAW SRM 55-21-11-300-032.

Part: HINGE ARM — EXCESS PLAY (LT ELEVATOR) · airframe 19,562 hrs · 7,542 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 3 ELEVATOR ON LEFT HORIZONTAL STABILIZER. REMOVED AND REPLACED HINGE ARM END FITTING # 3 ON LEFT ELEVATOR IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: SKIN — WORN (ZONE 100) · airframe 19,562 hrs · 7,542 cycles

AIRCRAFT IN BASE MAINTENANCE: WEAR FOUND ON SKIN PANEL LOCATED AT STA FR26 + 18 INCHES, BETWEEN STR 41L TO STR 42L. L= 0.125 INCHES, W= 0.120 INCHES, D= 0.006 INCHES. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN AT FR 26 + 18 BETWEEN STR 41L TO 42L ON LOWER FUSELAGE PER SRM 53-00-110-300-029.

Part: HINGE FITTING — EXCESS PLAY (LT ELEVATOR) · airframe 19,562 hrs · 7,542 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 1 ON LEFT HAND HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM END FITTING 1 PER AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (LT ELEVATOR) · airframe 19,562 hrs · 7,542 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 2 ON LEFT HAND HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM END FITTING 2 PER AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (LT ELEVATOR) · airframe 19,562 hrs · 7,542 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 4 ELEVATOR ON LEFT HORIZONTAL STABILIZER. REMOVED AND REPLACED HINGE ARM END FITTING #4 ON LEFT ELEVATOR IAW AMM 55-16-42-000-001-A. AND AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (LT ELEVATOR) · airframe 19,562 hrs · 7,542 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 5 ELEVATOR ON LEFT HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING #5 ON LEFT HORIZONTAL STABILIZER AMM 55-16-42-400-001-A.

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,562 hrs · 7,542 cycles

AIRCRAFT IN BASE MAINTENANCE: CORRODED AREA FOUND AT LOWER SILL IN AFT CARGO COMPARTMENT (BULK CARGO DOOR). L=0.383 INCH, W=0.173 INCH, D=0.079 INCH. PERFORMED PERMANENT DOUBLER REPAIR LOCATED ON LOWER SILL AT FR 60 STR 38R IN AFT CARGO COMPARTMENT.

Part: SHEAR PLATE — CRACKED (ZONE 200 -) · airframe 19,562 hrs · 7,542 cycles

AIRCRAFT IN BASE MAINTENANCE: FOUND 0.095 INCH CRACK BETWEEN FR69 TO FR70 AND STR 23L ON SHEAR PLATE. REPLACED SHEAR PLATE AT AFT GALLEY AREA IAW A321 SRM 51-72-11-911-001 AND DWG 53470100.

Part: FITTING — CORRODED (FRM 66-68 S23L) · corrosion level 2 · airframe 19,562 hrs · 7,542 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SILL CENTER FITTING LOCATED FROM FR66 TO FR68 AT S23L. REPLACED CENTER FITTING PER SRM 51-42-11-801 AND DWG D53480009.

Part: SUPPORT — CORRODED (FRM 68 S23L) · corrosion level 2 · airframe 19,562 hrs · 7,542 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SILL LOCATED AT FR 68 STR 23L. REPAIRED PER SRM 53-41-14-300-001.

Part: SHEAR PLATE — CRACKED (ZONE 200) · airframe 19,562 hrs · 7,542 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK FOUND ON SHEAR PLATE LOCATED BETWEEN FR69 TO FR 70, STR 23R. L= 0.811 INCHES. REPLACED SHEAR PLATE STR 23R BETWEEN FR69 TO FR 70 AT AFT GALLEY AREA PER SRM 51-72-11-911-001.

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 19,562 hrs · 7,542 cycles

AIRCRAFT IN BASE MAINTENANCE: FOUND CORROSION, MEASURING L=1 INCH, W=0.09 INCH, D=0.002 INCH, ON LOWER SILL AT FR68 AND STR 23R. REPLACED LOWER SILL REF A321 SRM 51-72-11-911-001 AND DWG D53480505.

Part: ACTUATOR — DEFECTIVE (RUDDER) · airframe 19,301 hrs · 7,438 cycles

AIRCRAFT WAS GROUNDED: DURING CRUISE, RUDDER HAD 2 SMALL UNCOMMANDED INPUTS THAT NOTICEABLY MOVED NOSE APPROXIMATELY 2-3 DEGREES WITHIN 1 SECOND. AUTO PILOT ON. REPLACED RUDDER TRIM ACTUATOR (10CC)AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 27-22-51.

Part: CONTROL PANEL — DEFECTIVE (ZONE 800) · airframe 17,713 hrs · 6,793 cycles

AIRCRAFT NOT GROUNDED - RIGHT FORWARD PASSENGER/CREW DOOR, SLIDE WARNING LIGHT SHOWS ARMED WHILE HANDLE IS IN DISARM POSITION. ACCOMPLISHED AMM TASK 52-11-00-810-807-A, REMOVED AND REPLACED WARNING LIGHT PANEL PER AMM 52-73-21 (B0401), OKAY FOR SERVICE.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 17,286 hrs · 6,614 cycles

AIRCRAFT IN BASE MAINTENANCE: R4 DOOR DAMPER (CYLINDER) PRESSURE LOW. SERVICED DOOR DAMPER (CYLINDER) TO PROPER PRESSURE PER AMM 52-10-00.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 17,286 hrs · 6,614 cycles

AIRCRAFT IN BASE MAINTENANCE: R1 DOOR DAMPER (CYLINDER) PRESSURE LOW. SERVICED DOOR DAMPER (CYLINDER) TO PROPER PRESSURE PER AMM 52-10-00.

Part: OVEN — ODOR (FWD GALLEY) · airframe 17,093 hrs · 6,536 cycles

AIRCRAFT WAS GROUNDED: DURING TAKEOFF AND CLIMBOUT F/A REPORTED STRONG ODOR THAT WAS LIKE BURNING PLASTIC. ODOR DISSAPETED AWAY IN ABOUT 10 MINUTES. COMPLIED WITH A320F SMOKE ODOR FUMES INITIAL T.S. JOBCARD 26L00021001. REPLACED FWD GALLEY OVEN DUE TO SMELL. OPS CHECK GOOD IAW AMM 25-35-19.

Part: BOTTLE — LOW PRESSURE (R1 DOOR ASSIST) · airframe 16,740 hrs · 6,408 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR ASSIST BOTTLE WAS LOW. MAINTENANCE SERVICED DOOR ASSIST BOTTLE TO PROPER PRESSURE PER AMM 52-10-00.

Part: ACCUMULATOR — LOW PRESSURE (R4 DOOR) · airframe 16,437 hrs · 6,284 cycles

AIRCRAFT WAS NOT GROUNDED: R4 DOOR ACCUMULATOR REQUIRED SERVICING. MAINTENANCE SERVICED DOOR ACCUMULATOR TO PROPER PRESSURE PER AMM 52-10-00.

Part: LIGHT — INOPERATIVE (SEATS 1AB) · airframe 16,437 hrs · 6,284 cycles

AIRCRAFT WAS NOT GROUNDED: AISLE EMERGENCY LIGHT SEAT 1A AND 1B INOPERABLE. MAINTENANCE REPLACED EMERGENCY LIGHT PER AMM 33-50-00.

Part: ACCUMULATOR — LOW PRESSURE (R1 DOOR) · airframe 16,437 hrs · 6,284 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR ACCUMULATOR REQUIRED SERVICING. MAINTENANCE SERVICED DOOR ACCUMULATOR TO PROPER PRESSURE PER AMM 52-10-00.

Part: PUMP — MALFUNCTIONED (NR 1 ENGINE) · airframe 15,444 hrs · 2,891 cycles

AIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY INBOUND TO CLT ON ACCOUNT OF LOST GREEN HYDRAULIC SYSTEM. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED & REPLACED #1 ENG HYD PUMP IAW AMM 29-11-51. NOTE: MAINTENANCE ALSO FOUND HYDRAULIC LINE LEAKING IN THE #1 PYLON. OPS CHECK GOOD. NO LEAKS NOTED.

Part: BOTTLE — LOW PRESSURE (R1 DOOR ASSIST) · airframe 15,360 hrs · 5,864 cycles

AIRCRAFT NOT GROUNDED: 1R EMERGENCY CYLINDER/ACCUMULATOR HAS LOW PRESSURE. SERVICED EMERGENCY CYLINDER/ACCUMULATOR ON DOOR 1R IAW AMM 52-10-00.

Part: WARNING LIGHT — FALSE ACTIVATION (APU FIRE BOTTLE) · airframe 14,646 hrs · 5,602 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS APU DISCHARGE LIGHT CAME ON IN FLIGHT FOR A FEW MINUTES THEN WENT OUT WITHOUT ANY ACTIONS. MAINTENANCE ACCOMPLISHED SATISFACTORY OPERATIONAL TEST OF APU FIRE EXTINGUISHING SYSTEM IAW AMM 26-22-00.

Part: ACM — FAILED (NR 1) · airframe 14,624 hrs · 5,592 cycles

AIRCRAFT WAS GROUNDED: PILOT RETURNED TO PHX ON ACCOUNT OF PRESSURIZATION ISSUES. ACFT WOULD NOT PRESSURIZE, AFTER TO, RECYCLED #1 PACK #1 BLEED, NO HELP. MAINTENANCE FOUND #1 PACK AIR CYCLE MACHINE NOT WORKING PROPERLY. REMOVED AND REPLACED #1 PACK ACM IAW AMM 21-52-21 PB 401. OPS CHECK GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (FIRE BOTTLE) · airframe 14,550 hrs · 5,562 cycles

AIRCRAFT NOT GROUNDED: AT CRUISE FLIGHT APU AGENT DISCHARGED LIGHT ON AFTER LANDING LIGHT WENT OUT. OPS CHK APU FIRE EXTINGUISHING SYS REF AMM 26-22-00 ALL OPS NORMAL ACCOMP VISUAL INSPECTION OF APU COMP AND APU FIRE EXT BOTTLE NO DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU AGENT) · airframe 14,503 hrs · 5,548 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS DURING CRUISE APU AGENT DISCH P.B. ILLUMINATED. MAINTENANCE PERFORMED OPERATIONAL TEST OF APU FIRE EXTINGUISHER LOOP/ SQUIB IAW AMM 26-22-00. OPS CHECK GOOD. NO FAULTS NOTED AT THIS TIME.

Part: FLOOR PANEL — DELAMINATED (FWD CARGO) · airframe 13,886 hrs · 5,319 cycles

AIRCRAFT WAS GROUNDED: FORWARD CARGO FLOOR PANEL 131EF DELAMINATED. REPLACED FLOOR PANEL PER AMM 53-22-14.

Part: BOTTLE — LOW PRESSURE (R4 DOOR ASSIST) · airframe 12,502 hrs · 4,766 cycles

R4 DOOR ASSIST ACTUATOR BOTTLE HAD LOW PRESSURE. MAINTENANCE SERVICED THE R4 DOOR ASSIST BOTTLE IAW AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (R1 DOOR ASSIST) · airframe 12,502 hrs · 4,766 cycles

R1 DOOR ASSIST ACTUATOR BOTTLE HAD LOW PRESSURE. MAINTENANCE SERVICED THE BOTTLE IAW AMM 52-10-00.

Part: BOTTLE — INOPERATIVE (L3 DOOR SLIDE) · airframe 11,838 hrs · 4,502 cycles

F/A PANEL, L3 DOOR SLIDE PRESSURE INDICATION INOPERATIVE. REPLACED THE L3 DOOR ESCAPE SLIDE INFLATION BOTTLE IAW AMM 25-62-49.

Part: SLEEVE — DETACHED (R4 DOOR HANDLE) · airframe 10,612 hrs · 4,057 cycles

EMERGENCY R4 DOOR HANDLE SLEEVE DETACHED. SECURED THE R4 DOOR CONTROL HANDLE SLEEVE IAW EA 280084.

Part: LENS — MISSING (CABIN) · airframe 9,613 hrs · 3,666 cycles

THE AIRCRAFT WAS NOT GROUNDED. ROW 22R EMERGENCY LIGHT LENS COVER MISSING. REMOVED AND REPLACED EMERGENCY LIGHT ROW 22R PER MM 33-51-00. OPERATIONS CHECK NORMAL.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 8,632 hrs · 3,302 cycles

R1 DOOR ASSIST BOTTLE IS LOW. SERVICED R1 DOOR ASSIST BOTTLE IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 7,709 hrs · 2,962 cycles

R4 DOOR WALL MOUNTED EXIT SIGN LENS MISSING. REPLACED LENS PER AMM

Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 7,669 hrs · 2,948 cycles

DELAMINATION ON AFT CARGO FLOOR PANEL 151LF. REPLACED THE FLOOR PANEL IAW AMM 53-42-04.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 5,754 hrs · 2,223 cycles

INOPERATIVE SEAT MOUNTED EMERGENCY EXIT LIGHT AT ROW 30 LEFT. REPLACED SIDEWALL TO LIGHT HARNESS IAW AMM 33-51-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 5,754 hrs · 2,223 cycles

EMERGENCY EXIT LIGHT LENS MISSING AT DOOR 4 LEFT. REPLACED MISSING LIGHT LENS AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 5,610 hrs · 2,171 cycles

MISSING EMERGENCY EXIT LIGHT COVER OVER R4 DOOR. REPLACED THE LIGHT COVER AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: MECHANISM — OBSTRUCTED (L4 DOOR) · airframe 4,669 hrs · 1,826 cycles

AIRCRAFT WAS NOT GROUNDED: 4L DOOR SLIDE WILL NOT ARM. REMOVE DEBRIS FROM 4L DOOR MECHANISM IAW AMM 52-10-00 AND ACCOMPLISHED A SATISFACTORY OPS CHECK.

Part: DIAPHRAGM — LEAKING (R1 DOOR) · airframe 972 hrs · 372 cycles

CIDS PANEL SHOWS DOOR 1R, CHECK LOW PRESS. REPLACED PERCUSSION MECHANISM DIAPHRAGM INCLUDING THE O RINGS. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 52-10-00-610-A.

Part: CYLINDER — LOW PRESSURE (R1 DOOR)

CHECK DOOR PRESS AMBER LIGHT ON FWD CIDS PANEL FOR DOOR 1R. SERVICED R1 DOOR DAMPER CYLINDER IAW MM 52-10-00-614-001A.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 897 hrs · 345 cycles

FLIGHT ATTENDANT REPORTS 1R DOOR CAUTION ON CIDS PANEL WITH CHECK DOOR PRESS. SERVICED 1R DOOR ASSIST BOTTLE IAW AMM 52-10-00.

Part: UNKNOWN — ODOR (CABIN) · airframe 883 hrs · 345 cycles

DURING FLIGHT, THE FLIGHT ATTENDANT REPORTS A CONSTANT OILY ODOR IN THE PAX CABIN & ALSO REPORTS THAT ONE OF THE FLIGHT ATTENDANTS BECAME ILL AS A RESULT. FLIGHT LANDED WITHOUT INCIDENT. NO KNOWN PAX ILLNESSES OCCURRED AS A RESULT. ACCOMPLISHED CABIN AIR QUALITY TROUBLESHOOTING JC 26L0021001 WITH NO SMELL NOTED. ACFT RETURNED TO SERVICE.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 738 hrs · 292 cycles

DOOR 1R HAS LOW PRESS. FWD FLIGHT ATTENDANT PANEL SAYS CHECK DOOR PRESS. SERVICED 1R ASSIST BOTTLE IAW AMM 52-10-00-614-001-A. OPERATIONS CHECKED GOOD.

Part: BOTTLE — LOW (R1 DOOR) · airframe 652 hrs · 252 cycles

FLIGHT ATTENDANT REPORTS ON CIDS PANEL, INDICATES CHECK 1R DOOR PRESS. SERVICED 1R DOOR ASSIST BOTTLE TO GREEN BAND, NORMAL PRESS, LEAK CHECKED GOOD IAW AMM.52-10-00-614-0010-A.

Part: BOTTLE — LOW PRESSURE (R1 DOOR ASSIST) · airframe 545 hrs · 205 cycles

R1 DOOR SLIDE ASSIST BOTTLE PRESS BELOW YELLOW BAND. SERVICED R1 DOOR SLIDE ASSIST BOTTLE TO GREEN BAND IAW AMM 52-10-00-614-0010-A.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 486 hrs · 181 cycles

R1 DOOR BOTTLE PRESS LOW, NEEDS SERVICE, CIDS PANEL INDICATED. SERVICED R1 DOOR ASSIST BOTTLE TO PROPER LEVEL IAW AMM 52-10-00-614-001A.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 444 hrs · 164 cycles

DOOR BOTTLED R1 MSG CIDS 1 SHOWS BOTTLE LOW PRESS. IAW AMM 52-10-00-614-001-A, SERVICED R1 DOOR ASSIST CYLINDER AS REQUIRED. OK FOR SERVICE.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 362 hrs · 132 cycles

1R DOOR ON CID PANEL SAYS CAB STILL PRESSURIZED. SERVICED 1R DOOR ASSIST BOTTLE IAW AMM 52-22-00-614-002A.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHT INOPERATIVE AT ROW 30 LT. R & R EMER POWER SUPPLY UNIT.