N125AA

Part: HINGE PIN — DEFECTIVE (RT NR 2 SPOILER) · airframe 35,462 hrs · 11,945 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING #2 SPOILER ATTACH FITTING CENTER HINGE PIN FOUND TO BE DEFECTIVE AND REPLACED IT PER AMM 27-64-42.

Part: HINGE PIN — DEFECTIVE (LT NR 4 SPOILER) · airframe 35,462 hrs · 11,945 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING #4 SPOILER ATTACH FITTING CENTER HINGE PINS FOUND TO BE DEFECTIVE. REPLACED HINGE PINS PER AMM 27-64-44.

Part: SKIN — DELAMINATED (ZONE 600 FLAP) · airframe 35,462 hrs · 11,945 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING OTBD T/E AFT FLAP LOWER SURFACE HAS A PREVIOUS REPAIR LOCATED AT THE CENTER OF THE FLAP THAT IS DELAMINATED. REPAIRED FLAP IAW SRM 57-53-00-300-093.

Part: HINGE PIN — DEFECTIVE (LT NR 2 SPOILER) · airframe 35,462 hrs · 11,945 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING #2 SPOILER ATTACH FITTING CENTER HINGE PINS FOUND TO BE DEFECTIVE. REPLACED HINGE PINS PER AMM 27-64-44.

Part: HINGE PIN — DEFECTIVE (ZONE 500 SPOILER) · airframe 35,462 hrs · 11,945 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING NR 3 SPOILER CENTER HINGE PINS FOUND TO BE DEFECTIVE AND WERE REPLACED IAW AMM 27-64-43.

Part: HINGE PIN — DEFECTIVE (RT NR 3 SPOILER) · airframe 35,462 hrs · 11,945 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING #3 SPOILER ATTACH FITTING CENTER HINGE PIN FOUND TO BE DEFECTIVE AND REPLACED IT PER AMM 27-64-42.

Part: HINGE PIN — DEFECTIVE (RT NR 4 SPOILER) · airframe 35,462 hrs · 11,945 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING #4 SPOILER ATTACH FITTING CENTER HINGE PIN FOUND TO BE DEFECTIVE AND REPLACED IT PER AMM 27-64-42.

Part: HOSE — WORN (ZONE 800) · airframe 35,462 hrs · 11,945 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT-HAND FORWARD ESCAPE SLIDE ENCLOSURE INNER STRUCTURE HAS WORN AND DAMAGED INFLATION HOSE ASSEMBLY. REPLACED INFLATION HOSE PER AMM 25-62-47.

Part: HOSE — MISINSTALLED (SLIDE) · airframe 333,493 hrs · 11,148 cycles

AIRCRAFT WAS NOT GROUNDED: DURING A SCHEDULED TIME CHANGE OF THE R1 DOOR SLIDE MAINTENANCE FOUND THE INFLATION HOSE ON THE REPLACEMENT SLIDE WAS BEYOND THE EDGE OF THE ASPIRATOR WHICH IS NOT ALLOWED PER TCN25-1169 GUIDANCE. THE REPLACEMENT SLIDE WAS INDENTIFIED AS BAD FROM STOCK AND ROUTED TO BE SENT OUT FOR REPAIR. A SERVICEABLE SLIDE WAS INSTALLED ON THE AIRCRAFT.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 33,199 hrs · 11,027 cycles

AIRCRAFT WAS NOT GROUNDED: L2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-22-00.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 33,199 hrs · 11,027 cycles

AIRCRAFT WAS NOT GROUNDED: L3 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-22-00.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 33,199 hrs · 11,027 cycles

AIRCRAFT WAS NOT GROUNDED: R2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-22-00.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 33,199 hrs · 11,027 cycles

AIRCRAFT WAS NOT GROUNDED: R3 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-22-00.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 32,144 hrs · 10,599 cycles

AIRCRAFT WAS NOT GROUNDED: L4 DOOR ASSIST BOTTLE REQUIRES SERVICING. SERVICED THE L4 DOOR ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 32,144 hrs · 10,599 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR ASSIST BOTTLE REQUIRES SERVICING. SERVICED THE L1 DOOR ASSIST BOTTLE.

Part: RIB — CORRODED (ZONE 600) · airframe 31,611 hrs · 10,370 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING MAIN LANDING GEAR RIB 5 AFT LUG AT WS 2580. REPAIRED RIGHT WING MAIN LANDING GEAR RIB 5 AFT LUG PER EA 358198.

Part: WIRE — BROKEN (ZONE 200) · airframe 31,245 hrs · 10,200 cycles

AIRCRAFT WAS NOT GROUNDED: FOUND SEAT 8C EMERGENCY LIGHT INOPERATIVE. FOUND WIRES BROKEN FROM CONNECTER PLUG FOR SEAT 8C, INSTALLED NEW PINS FOR 8C SEAT CONNECTOR.

Part: CABLE — MISSING (R1 DOOR SLIDE) · airframe 31,060 hrs · 10,117 cycles

AIRCRAFT WAS NOT GROUNDED: MAINTENANCE FOUND REPLACEMENT SLIDE RAFT ASSEMBLY FOR THE R1 DOOR WAS BAD FROM STOCK DUE TO THE MANUAL CABLE PULL CONNECTION WAS MISSING. MAINTENANCE RETURNED THE SLIDE RAFT ASSEMBLY BACK TO STORES TO BE SENT BACK TOP THE VENDOR FOR REPAIR.

Part: POWER SUPPLY — FAULTY (R1 DOOR SLIDE) · airframe 31,026 hrs · 10,103 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT FAULT AT 10WL FORWARD EMERGENCY EXIT. FOUND R1 SLIDE FAULTY, REPLACED R1 SLIDE.

Part: FLASHLIGHT — INOPERATIVE (MID CABIN) · airframe 31,022 hrs · 10,102 cycles

AIRCRAFT WAS NOT GROUNDED: MID CABIN FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED EMERGENCY FLASHLIGHT AT FA MID CABIN-SEAT PER AMM 25-20-00.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 30,900 hrs · 10,051 cycles

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

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 30,900 hrs · 10,051 cycles

AIRCRAFT WAS NOT GROUNDED: L4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE BELOW LIMITS. MAINTENANCE SERVICED THE L4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 30,063 hrs · 9,690 cycles

AIRCRAFT WAS NOT GROUNDED: L1 PASSENGER/CREW DOOR DAMPER AND CYLINDER NEED SERVICING. SERVICED L1 PASSENGER/CREW DOOR DAMPER AND CYLINDER AS REQUIRED.

Part: ACTUATOR — TRIPPED (ZONE 600 - RH WI) · airframe 29,993 hrs · 9,665 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED COMMING INTO SEA DUE TO THE SLATS NOT DEPLOYING FOR LANDING DUE TO A FLIGHT CONTROL SLAT FAULT. THE FLIGHT CREW ACCOMPLISHED ECAM PROCEDURES AND LANDED SAFELY AT SEA WITH FLAPS 25. MAINTENANCE FOUND THE RIGHT WING SLAT TRACK #11 ACTUATOR 6091CM TORQUE LIMITER TRIPPED AND REPLACED IT PER AMM 27-84-49. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: LIMITER — ACTIVATED (RT WING SLAT) · airframe 29,644 hrs · 9,518 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO AMBER SLATS FAULT ON APPROACH. THE AIRCRAFT LANDED SAFELY AT ONT. MAINTENANCE ACCOMPLISHED TSM 27-81-00-810-810 AND FOUND THE RIGHT WING #5 INBOARD GEAR BOX TORQUE LIMITER ACTIVED AND RESET THE LIMITER PER AMM 27-80-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED AND THE FAULT CLEARED.

Part: CONNECTOR — DISCONNECTED (ZONE 200 - FUSE) · airframe 29,429 hrs · 9,441 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: CIDS 1 FAULT EPSU 10WL. MAINTENANCE RE-SEATED CONNECTOR 10WL IAW AA A321 AMM 33-51-38.

Part: HANDLE — BROKEN (ZONE 800 - DOORS) · airframe 29,395 hrs · 9,423 cycles

AIRCRAFT IN BASE MAINTENANCE: R1 DOOR SLIDE RED PULL HANDLE BROKEN, **SUPPLEMENTAL REPORT FOR AALA202312197756: MAINTENANCE REPLACED THE SLIDE RAFT ASSEMBLY PER TASK CARD 26C84152002** (CLOSED)

Part: HANDLE — BROKEN (ZONE 800 - DOORS) · airframe 29,395 hrs · 9,423 cycles

AIRCRAFT IN BASE MAINTENANCE: R4 DOOR SLIDE HAS RED PULL HANDLE BROKEN, **SUPPLEMENTAL REPORT FOR AALA202312198108: MAINTENANCE REPLACED THE SLIDE RAFT ASSEMBLY PER TASK CARD 26C84252002. ** (CLOSED)

Part: HANDLE — BROKEN (ZONE 800 - DOORS) · airframe 29,395 hrs · 9,423 cycles

AIRCRAFT IN BASE MAINTENANCE: L1 DOOR SLIDE RED PULL HANDLE BROKEN. **SUPPLEMENTAL REPORT FOR AALA202312195882: MAINTENANCE REPLACED SLIDE RAFT ASSEMBLY PER TASK CARD 26C83152002 ** (CLOSED)

Part: FLOOR PANEL — CRACKED (ZONE 100 - FUSE) · airframe 29,395 hrs · 9,423 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CARGO FLOOR PANEL 151LF CRACKED AT RIGHT HAND OUTBOARD CORNER. SUPPLEMENTAL REPORT FOR AALA202312191620: MAINTENANCE REPLACED FLOOR PANEL.** (CLOSED)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 29,395 hrs · 9,423 cycles

AIRCRAFT IN BASE MAINTENANCE: R1 DOOR SLIDE RED PULL HANDLE BROKEN, **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: FLOOR PANEL — CRACKED (ZONE 100 - FUSE) · airframe 29,395 hrs · 9,423 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CARGO FLOOR PANEL 151LF CRACKED AT RIGHT HAND OUTBOARD CORNER. SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 29,395 hrs · 9,423 cycles

AIRCRAFT IN BASE MAINTENANCE: R4 DOOR SLIDE HAS RED PULL HANDLE BROKEN, **SUPPLEMENTAL REPORT WIL BE SUBMITTED** (OPEN)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 29,395 hrs · 9,423 cycles

AIRCRAFT IN BASE MAINTENANCE: L1 DOOR SLIDE RED PULL HANDLE BROKEN. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: STRUT — CORRODED (LT WING FLAP) · airframe 29,224 hrs · 9,358 cycles

AIRCRAFT WAS GROUNDED: LEFT HAND FLAP INTERCONNECT STRUT ROD ENDS FOUND WORN/CORRODED. REPLACED INTERCONNECT STRUT PER AMM 27-51-44.

Part: STRUT — CORRODED (RT WING FLAP) · airframe 29,224 hrs · 9,358 cycles

AIRCRAFT WAS GROUNDED: RIGHT HAND FLAP INTERCONNECT STRUT ROD ENDS FOUND WORN/CORRODED. REPLACED INTERCONNECT STRUT PER AMM 27-51-44.

Part: WIRE — BROKEN (ZONE 200 - FUSE) · airframe 29,152 hrs · 9,335 cycles

AIRCRAFT WAS NOT GROUNDED: FOUND SEAT MOUNTED EMERGENCY AISLE LIGHTS INOP AT ROW 14 AND 15. FOUND BROKEN WIRE, REPAIRED WIRE.

Part: LIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 28,236 hrs · 8,958 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT MOUNT 11CBA EMERGENCY EXIT LOCATION LIGHT INOPERATIVE. REMOVED AND REPLACED SEAT MOUNT 11 CBA EMERGENCY EXIT LOCATION LIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: OVEN — DEFECTIVE (ZONE 900 - LAV/G) · airframe 27,759 hrs · 8,756 cycles

AIRCRAFT WAS NOT GROUNDED: DURING FLIGHT THE FLIGHT ATTENDANT WAS USING THE FORWARD GALLEY #2 OVEN AND WHEN THE OVEN DOOR WAS OPENED SMOKE WAS VISIBLE BUT NO FIRE WAS NOTED. THE FLIGHT ATTENDANT TURNED OFF THE OVEN AND LOCKED IT TO PREVENT FURTHER USE. MAINTENANCE REPLACED THE OVEN PER AMM 25-35-19 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK/

Part: SELECTOR VALVE — DEFECTIVE (MLG) · airframe 25,890 hrs · 7,954 cycles

AIRCRAFT WAS GROUNDED: ON APROACH AT 2500" CREW PUT GEAR HANDLE DOWN AND GOT LANDING GEAR NOT DOWN / LOCKED ECAM MESSAGE. CREW FOLLOWED ECAM PROCEDURE AND ACCOMPLISHED A MANUAL GEAR EXTENSION. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE GEAR SELECTOR VALVE ASSEMBLY AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER AMM 32-31-31.

Part: LATCH — INOPERATIVE (ZONE 800 - DOORS) · airframe 25,417 hrs · 7,752 cycles

AIRCRAFT WAS GROUNDED: FLIGHT DECK DOOR VERY DIFFICULT TO OPEN. LOWER BOLT DOES NOT OPERATE. WILL NOT RETRACT. MAINTENANCE REPLACED FLIGHT DECK DOOR LOWER LATCH AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-51-21.

Part: BATTERY — DEFECTIVE (ZONE 200 - FUSE) · airframe 24,724 hrs · 7,467 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 13WL BATTERY FAILED BITE TEST PER TASK CARD 26L00005005. REPLACED 13WL EMERGENCY POWER SUPPLY UNIT BATTERY PER AMM 33-51-38, BITE TEST OK.

Part: BATTERY PACK — DISCHARGED (ZONE 200 - FUSE) · airframe 23,604 hrs · 7,001 cycles

AIRCRAFT WAS GROUNDED: 2ND AND 3RD CEILING EMERGENCY LIGHTS INOPERATIVE. RECHARGED BATTERY PACK AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.

Part: BATTERY — FAILED (ZONE 200 - FUSE) · airframe 23,604 hrs · 7,001 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT 14WL BATTERY FAILED CIDS SYSTEM 1 TEST. REPLACED BATTERY PER AMM 33-51-38. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: UNKNOWN — ODOR (COCKPIT-CABIN) · airframe 23,148 hrs · 6,789 cycles

AIRCRAFT WAS GROUNDED: FAINT DIRTY SOCK ODOR IN COCKPIT AND CABIN DURING CRUISE AND DESCENT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: APU — ODOR (AFT) · airframe 23,148 hrs · 6,789 cycles

AIRCRAFT WAS GROUNDED: FAINT DIRTY SOCK ODOR IN COCKPIT AND CABIN DURING CRUISE AND DESCENT. REPLACED APU WITH SERVICEABLE UNIT IAW WORKCARD 26L31049003, OPS CHECK GOOD.

Part: OIL SYSTEM — LEAKING (APU) · airframe 22,978 hrs · 6,716 cycles

AIRCRAFT WAS GROUNDED: DIRTY SOCK SMELL IN FLIGHT DECK, FIRST CLASS AND FRONT OF COACH ON DESCENT, APPROXIMATELY AT 6000' AFTER FIRST FLAPS WENT OUT AT 200 KNOTS. NO SMELL IN AFT OF AIRCRAFT. MAINTENANCE ISOLATED SOURCE OF ODOR TO THE APU. (OPEN)

Part: COOLING FAN — LEAKING (APU) · airframe 22,978 hrs · 6,716 cycles

AIRCRAFT WAS GROUNDED: DIRTY SOCK SMELL IN FLIGHT DECK, FIRST CLASS AND FRONT OF COACH ON DESCENT, APPROXIMATELY AT 6000' AFTER FIRST FLAPS WENT OUT AT 200 KNOTS. NO SMELL IN AFT OF AIRCRAFT. MAINTENANCE ISOLATED SOURCE OF ODOR TO THE APU. MAINTENANCE FOUND THE APU OIL COOLING FAN LEAKING INTERNALLY AND REPLACED IT PER AMM 49-52-51. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: FILTER — DIRTY (CABIN AIR) · airframe 22,948 hrs · 6,704 cycles

AIRCRAFT WAS GROUNDED: ODOR SIMILAR TO DIRTY SOCKS NOTED IN AFT CABIN AFTER TAKE OFF. DISSIPATED AFTER FOLLOW QRH PROCEDURE TURNING PACK #2 OFF. FUMES RETURNED DESCENDING THROUGH 6000. SELECTING FLAPS 1, ODOR RETURNED AND COULD BE SMELLED IN CABIN AND COCKPIT. MAINTENANCE FOUND BOTH RECIRCULATION FILTERS DIRTY AND REPLACED THEM PER AMM 21-51-41.

Part: LIGHT — OUT OF POSITION (ZONE 200 - FUSE) · airframe 22,827 hrs · 6,647 cycles

AIRCRAFT IN BASE MAINTENANCE: L3 EMERGENCY EXT LIGHT ON SEAT ROW 24 SHOULD BE RED WHICH IS INSTALLED ON SEAT 28. FOUND RED AND WHITE EMERGENCY SEAT LIGHTS SWAPPED AT SEAT ROWS 24 AND 28 ABC. REMOVED RED LIGHT FROM SEAT ROW 28 AND WHITE LIGHT FROM SEAT ROW 24 PER A321 AMM 33-51-18-400-001-A. INSTALLED RED LIGHT ON SEAT ROW 24 AND WHITE LIGHT ON SEAT ROW 28 PER A321 AMM 31-51-18-000-001-A. PERFORMED OPERATIONAL CHECK PER A321 AMM 33-51--00-710.

Part: WIRE — DISCONNECTED (ZONE 200 - FUSE) · airframe 22,827 hrs · 6,647 cycles

AIRCRAFT IN BASE MAINTENANCE: L2 DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED EMERGENCY LIGHT ASSEMBLY L2 DOOR PER A321 AMM 33-51-11-00. FOUND WIRE NOT CONNECTED, CONNECT THE WIRE. NEED OK TO INSTALL. INSTALLED EMERGENCY LIGHT ASSEMBLY L2 DOOR PER A321 AMM 33-51-00. OPERATION CHECKED CARRIED OUT FOUND GOOD PER A321 AMM 33-51-00-710.

Part: FLOOR PANEL — DELAMINATED (ZONE 100 - FUSE) · airframe 22,827 hrs · 6,647 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 222EF IS DELAMINATED. **SUPPLEMENTAL REPORT FOR AALA202110159833: REPLACED FLOOR PANEL AS REQUIRED** (CLOSED)

Part: FLOOR PANEL — DELAMINATED (ZONE 100 - FUSE) · airframe 22,827 hrs · 6,647 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 22DEF IS DELAMINATED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: FLASHLIGHT — BROKEN (ZONE 200 - FUSE) · airframe 22,827 hrs · 6,647 cycles

AIRCRAFT IN BASE MAINTENANCE: R4 FLASHLIGHT ASSEMBLY BROKEN. REPLACED R4 FLASHLIGHT ASSEMBLY PER A321 AMM 25-65-00.

Part: FAN — INOPERATIVE (ZONE 100) · airframe 22,130 hrs · 6,404 cycles

AIRCRAFT WAS GROUNDED: SMOKE AND ELECTRICAL ODOR IN FLIGHT DECK AND FORWARD GALLEY. DISSIPATES WITHOUT CREW ACTION. OCCURRED 2 TIMES, ONCE IN CRUISE AND ONCE ON APPROACH. ACCOMPLISHED JOB CARD 26L00021001. FOUND MELTED AND BURNED PINS ON EXTRACT FAN AND CONNECTOR. REMOVED AND REPLACED EXTRACT FAN (AALA202107267539) PER AMM 21-26-51. REPLACED CONNECTOR (AALA202107262364) PER ESPM 20-48-21 AND WM 21-26-09.

Part: CONNECTOR — BURNED (EXTRACT FAN) · airframe 22,130 hrs · 6,404 cycles

AIRCRAFT WAS GROUNDED: SMOKE AND ELECTRICAL ODOR IN FLIGHT DECK AND FORWARD GALLEY. DISSIPATES WITHOUT CREW ACTION. OCCURRED 2 TIMES, ONCE IN CRUISE AND ONCE ON APPROACH. ACCOMPLISHED JOB CARD 26L00021001. FOUND MELTED AND BURNED PINS ON EXTRACT FAN AND CONNECTOR. REMOVED AND REPLACED EXTRACT FAN (AALA202107267539) PER AMM 21-26-51. REPLACED CONNECTOR (AALA202107262364) PER ESPM 20-48-21 AND WM 21-26-09.

Part: BATTERY — FAULTED (EMERGENCY LIGHTS) · airframe 21,829 hrs · 6,298 cycles

AIRCRAFT WAS NOT GROUNDED. FOUND L4 EPSU BATTERY IN FAULT. REPLACED BATTERY PER AMM 33-51-38.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 21,300 hrs · 6,105 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 10WL FAILED EMERGENCY POWER SUPPLY UNIT SYSTEM TEST. REMOVED AND REPLACED 10WL EMERGENCY POWER SUPPLY UNIT BATTERY PER AMM 33-51-38.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 21,300 hrs · 6,105 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 14WL FAILED EMERGENCY POWER SUPPLY UNIT SYSTEM TEST. REMOVED AND REPLACED 14WL EMERGENCY POWER SUPPLY UNIT BATTERY PER AMM 33-51-38.

Part: DAMPENER — LOW PRESSURE (L4 DOOR) · airframe 19,990 hrs · 5,667 cycles

AIRCRAFT WAS NOT GROUNDED. L4 DOOR DAMPER PRESSURE LOW 1450 REQUIRES SERVICE. SERVICED L4 DOOR ASSIST DAMPER TO CORRECT PSI 1750, PER AMM 52-10-00.

Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT LAVATORY) · airframe 19,884 hrs · 5,634 cycles

AIRCRAFT WAS NOT GROUNDED. SMOKE LAVATORY ELECTRONIC CENTRALIZED AIRCRAFT MONITOR MESSAGE ILLUMINATED IN CRUISE. FLIGHT ATTENDANT NOTED RIGHT AFT LAVATORY SMOKE LIGHT IN CABIN. UPON INVESTIGATION NO SMOKE IN RIGHT AFT LAVATORY. ELECTRONIC CENTRALIZED AIRCRAFT MONITOR MESSAGE EXTINGUISHED. NO FAULTS LOGGED AND LAVATORY SMOKE BUILT IN TEST EQUIPMENT TEST PASSED.

Part: WINDSHIELD — DAMAGED (CAPTAIN'S) · airframe 19,699 hrs · 5,563 cycles

AIRCRAFT IN BASE MAINTENANCE: BLURRED FIXED WINDOW CAPTAIN SIDE COCKPIT. REMOVED AND INSTALLED NEW FIXED WINDOW CAPTAIN SIDE IN COCKPIT PER AMM 56-11-12-000-001-A, AMM 56-11-12-400-002-A, AND AMM 30-42-00-710-001-A.

Part: DAMPER — INOPERATIVE (PAX DOOR) · airframe 19,699 hrs · 5,563 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER CREW DOOR 831 DAMPING FUNCTION FAILED OPERATIONAL TEST. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER IAW AMM 52-11-14-400-001-B, OPS CHECK GOOD.

Part: CYLINDER — NO TEST (PAX DOOR DAMPER) · airframe 19,699 hrs · 5,563 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER CREW DOOR 841 DAMPING FUNCTION AT FWD GALLEY AREA DID NOT PASS OPERATIONAL TEST. REPLACED DOOR DAMPER (AALA202008239013) AND EMERGENCY OPERATION CYLINDER (AALA202008249015) IAW 52-11-14-400-001-B.

Part: DAMPER — NO TEST (PAX DOOR) · airframe 19,699 hrs · 5,563 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER CREW DOOR 841 DAMPING FUNCTION AT FWD GALLEY AREA DID NOT PASS OPERATIONAL TEST. REPLACED DOOR DAMPER (AALA202008239013) AND EMERGENCY OPERATION CYLINDER (AALA202008249015) IAW 52-11-14-400-001-B.

Part: SLIDE — OUT OF TOLERANCE (PAX DOOR) · airframe 19,699 hrs · 5,563 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING OPERATIONAL TEST OF SLIDE COVER PASSENGER/CREW DOOR 831, FOUND THAT THERE IS NOT ENOUGH CLEARANCE BETWEEN DECORATIVE COVER AND FUSELAGE AT FWD GALLEY AREA. REPLACED SLIDE RAFT AT PASSENGER/CREW DOOR.

Part: SHEAR PLATE — CRACKED (FRAMES 69-70) · airframe 19,699 hrs · 5,563 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED SHEAR PLATE BETWEEN FRAMES 69 AND 70, STRINGER 23L, MEASURING L=0.786 IN. REPLACED THE SHEAR PLATE WITH NEW IAW SRM 51-42-11-801, AND DRAWING D53474180.

Part: SUPPORT — CORRODED (FRAME 68) · corrosion level 2 · airframe 19,699 hrs · 5,563 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION OF SILL AT FR68 AND STR 23L, MEASURING L=0.856 IN, W=0.678 IN, D=0.063 IN. ACCOMPLISHED PERMANENT REINFORCING REPAIR WITH NESTED ANGLES IAW SRM 53-41-14-300-001.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 19,699 hrs · 5,563 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: CABIN FLOOR PANEL 222EF WAS FOUND TO HAVE DELAMINATED AREA WITH DIMENSIONS L= 1.03 IN W=0.89 IN. REMOVED AND REPLACED PANEL.

Part: FITTING — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 19,699 hrs · 5,563 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION OF CENTER FITTING BETWEEN FR66 AND FR68 AT STR 23L, MEASURING L=1.145 IN, W=0.348 IN, D=0.042 IN. REPLACED CENTER FITTING WITH NEW IAW A321 SRM 51-72-11-911-001 AND DRAWING D53480505.

Part: DOOR SILL — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 19,699 hrs · 5,563 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT AFT PASSENGER CREW DOOR CUT OUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23R. REPLACED LOWER SILL IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FRAME 20) · airframe 19,699 hrs · 5,563 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION OF FLOOR BEAM AT FR20 AND BL -Y254, MEASURING L=2.690 IN, W=1.348 IN, D=0.023 IN. REMOVED CORROSION, FLOOR BEAM WITHIN LIMITS IAW A321 SRM 51-74-11-801 AND 53-11-14-283-007.

Part: SHEAR PLATE — CRACKED (FRAMES 69-70) · airframe 19,699 hrs · 5,563 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN SHEAR PLATE ON STR 23R BETWEEN FR69 AND FR70, MEASURING L=1.42 IN. REPLACED SHEAR PLATE WITH NEW IAW A321 SRM 51-72-11-911-001 AND DRAWING D53474180.

Part: SEAT TRACK — CORRODED (FRAME 20) · corrosion level 2 · airframe 19,657 hrs · 5,549 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION OF SEAT TRACK AT FR20 AND BL -Y1292, MEASURING L=1.48 IN, W=0.63 IN, D=0.049 IN. REPLACED SEAT TRACK WITH MODIFIED PART IAW A321 SRM 51-42-11-801 AND DRAWINGS D53110920 AND D53110984.

Part: BOTTLE — UNSERVICEABLE (L1 DOOR ASSIST) · airframe 19,653 hrs · 5,548 cycles

AIRCRAFT GROUNDED - ELONGATED SHEAR PIN HOLE, L1 DOOR ASSIST CYLINDER. REMOVED AND REPLACED L1 DOOR ASSIST BOTTLE PER AMM 52-11-14.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 19,524 hrs · 5,509 cycles

AIRCRAFT NOT GROUNDED - RIGHT AFT PAX/CREW DOOR, ASSIST BOTTLE PRESSURE LOW AT 100PSI. SERVICED DOOR ASSIST BOTTLE PER AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 19,352 hrs · 5,454 cycles

AIRCRAFT WAS NOT GROUNDED: DURING INSPECTION FOUND L4, R4, AND R1 DOOR ASSIST BOTTLES UNDER LIMITS. MAINTENANCE SERVICED L4 (SEE AALA202003079004), R4, AND R1 (SEE AALA202003079005) DOOR ASSIST BOTTLES TO PROPER PRESSURE PER AMM 52-11-00-610-001-A.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 19,352 hrs · 5,454 cycles

AIRCRAFT WAS NOT GROUNDED: DURING INSPECTION FOUND L4, R4, AND R1 DOOR ASSIST BOTTLES UNDER LIMITS. MAINTENANCE SERVICED L4, R4 (SEE AALA202003079003), AND R1 (SEE AALA202003079005) DOOR ASSIST BOTTLES TO PROPER PRESSURE PER AMM 52-11-00-610-001-A.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 19,352 hrs · 5,454 cycles

AIRCRAFT WAS NOT GROUNDED: DURING INSPECTION FOUND L4, R4, AND R1 DOOR ASSIST BOTTLES UNDER LIMITS. MAINTENANCE SERVICED L4 (SEE AALA202003079004), R4 (SEE AALA202003079003), AND R1 DOOR ASSIST BOTTLES TO PROPER PRESSURE PER AMM 52-11-00-610-001-A.

Part: ACCUMULATOR — LOW PRESSURE (L4 DOOR) · airframe 18,415 hrs · 5,206 cycles

AIRCRAFT WAS NOT GROUNDED: L4 DOOR EMERGENCY OPERATING CYLINDER CHARGE PRESSURE LOW. MAINTENANCE SERVICED DOOR ACCUMULATOR TO PROPER PRESSURE PER AMM 52-10-00.

Part: ACCUMULATOR — LOW PRESSURE (R4 DOOR) · airframe 18,415 hrs · 5,206 cycles

AIRCRAFT WAS NOT GROUNDED: R4 DOOR EMERGENCY OPERATING CYLINDER CHARGE PRESSURE LOW. MAINTENANCE SERVICED DOOR ACCUMULATOR TO PROPER PRESSURE PER AMM 52-10-00.

Part: SLIDING WINDOW — OVERHEATED (COCKPIT) · airframe 18,282 hrs · 5,172 cycles

AIRCRAFT WAS GROUNDED: CAPT SLIDING WINDOW EXTREMELY HOT IN FLIGHT UNABLE TO TOUCH CRACKING AND PINGING NOISES HEARD. SIGNS OF DELAMINATION AND BUBBLING. MAINTENANCE REMOVED AND REPLACED CAPTAINS SLIDING WINDOW IAW AMM 56-12-11. OPS AND LEAK CHECK GOOD.

Part: ACCUMULATOR — LOW PRESSURE (R1 DOOR) · airframe 18,196 hrs · 5,140 cycles

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

Part: ACCUMULATOR — LOW PRESSURE (R4 DOOR) · airframe 18,196 hrs · 5,140 cycles

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

Part: ACCUMULATOR — LOW PRESSURE (L4 DOOR) · airframe 18,196 hrs · 5,140 cycles

AIRCRAFT WAS NOT GROUNDED: L4 EMERGENCY DOOR ACCUMULATOR PRESSURE LOW. MAINTENANCE SERVICED DOOR ACCUMULATOR TO PROPER PRESSURE PER AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 17,739 hrs · 5,013 cycles

AIRCRAFT NOT GROUNDED: R4 DOOR ACCUMULATOR PRESSURE LOW. SERVICED R4 DOOR IAW AMM 52-10-00.

Part: ACCUMULATOR — LOW PRESSURE (L4 DOOR) · airframe 17,735 hrs · 5,012 cycles

AIRCRAFT IN BASE VISIT: L4 DOOR ACCUMULATOR PRESSURE LOW. SERVICED L4 DOOR ACCUMULATOR IAW AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 17,739 hrs · 5,013 cycles

AIRCRAFT NOT GROUNDED: L4 DOOR ACCUMULATOR PRESSURE LOW. SERVICED L4 DOOR ACCUM IAW AMM 52-10-00.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 17,455 hrs · 4,935 cycles

AIRCRAFT WAS NOT GROUNDED: 4R DOOR EMERGENCY CYLINDER PRESSURE LOW. MAINTENANCE SERVICED CYLINDER TO PROPER PRESSURE PER AMM 52-10-00.

Part: CYLINDER — LOW PRESSURE (L4 DOOR) · airframe 17,455 hrs · 4,935 cycles

AIRCRAFT WAS NOT GROUNDED: 4L DOOR EMERGENCY CYLINDER PRESSURE LOW. MAINTENANCE SERVICED CYLINDER TO PROPER PRESSURE PER AMM 52-10-00.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 17,455 hrs · 4,935 cycles

AIRCRAFT WAS NOT GROUNDED: 1R DOOR EMERGENCY CYLINDER PRESSURE LOW. MAINTENANCE SERVICED CYLINDER TO PROPER PRESSURE PER AMM 52-10-00.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 17,236 hrs · 4,882 cycles

AIRCRAFT WAS NOT GROUNDED: R4 CABIN DOOR EMERGENCY OPERATING CYLINDER CHARGE PRESSURE LOW. MAINTENANCE SERVICED CYLINDER TO PROPER PRESSURE PER AMM 52-10-00.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 17,118 hrs · 4,852 cycles

AIRCRAFT WAS NOT GROUNDED: 4R DOOR EMERGENCY OPERATIONAL CYLINDER PRESSURE LOW. MAINTENANCE SERVICED CYLINDER TO PROPER PRESSURE PER AMM 52-10-00.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 17,118 hrs · 4,852 cycles

AIRCRAFT WAS NOT GROUNDED: 1R DOOR EMERGENCY OPERATIONAL CYLINDER PRESSURE LOW. MAINTENANCE SERVICED CYLINDER TO PROPER PRESSURE PER AMM 52-10-00.

Part: CYLINDER — LOW PRESSURE (L4 DOOR) · airframe 17,118 hrs · 4,852 cycles

AIRCRAFT WAS NOT GROUNDED: 4L DOOR EMERGENCY OPERATIONAL CYLINDER PRESSURE LOW. MAINTENANCE SERVICED CYLINDER TO PROPER PRESSURE PER AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (R4 DOOR ASSIST) · airframe 16,785 hrs · 4,781 cycles

AIRCRAFT WAS NOT GROUNDED: R4 DOOR CYLINDER NEEDED TO BE SERVICED. MAINTENANCE SERVICED R4 DOOR CYLINDER TO PROPER PRESSURE PER AMM 52-22-00-614-002.

Part: DAMPER — LOW PRESSURE (R4 DOOR) · airframe 16,227 hrs · 4,624 cycles

AIRCRAFT WAS NOT GROUNDED: R4 DOOR EMERGENCY DAMPER HAD LOW PRESSURE. MAINTENANCE SERVICED R4 DOOR EMERGENCY DAMPER TO PROPER PRESSURE PER AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 16,020 hrs · 4,577 cycles

AIRCRAFT WAS NOT GROUNDED: 1R, 4R, AND 4L PASSENGER DOOR ASSIST PRESSURE LOW. MAINTENANCE SERVICED 1R (SEE AALA20190403001), 4R, AND 4L (SEE AALA201904039016) DOOR ASSIST BOTTLE TO PROPER PRESSURE PER MM 52-10-00.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 16,020 hrs · 4,577 cycles

AIRCRAFT WAS NOT GROUNDED: 1R, 4R, AND 4L PASSENGER DOOR ASSIST PRESSURE LOW. MAINTENANCE SERVICED 1R (SEE AALA20190403001), 4R (SEE AALA201904039015), AND 4L DOOR ASSIST BOTTLE TO PROPER PRESSURE PER MM 52-10-00.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 16,020 hrs · 4,577 cycles

AIRCRAFT WAS NOT GROUNDED: 1R, 4R, AND 4L PASSENGER DOOR ASSIST PRESSURE LOW. MAINTENANCE SERVICED 1R, 4R, AND 4L DOOR ASSIST BOTTLE TO PROPER PRESSURE PER MM 52-10-00.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 15,372 hrs · 4,394 cycles

AIRCRAFT WAS NOT GROUNDED: AFT EMERGENCY EXIT LIGHTING FAILED OPERATIONAL CHECK, DID NOT ILLUMINATE. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 14,882 hrs · 4,272 cycles

AFT CARGO BAY FLOOR PANEL 151NF WAS DELAMINATED. THE AIRCRAFT WAS GROUNDED. REPLACED THE FLOOR PANEL IAW AMM 53-42-14.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 14,774 hrs · 4,247 cycles

R4 DOOR EMERGENCY OPERATING CYLINDER PRESSURE WAS LOW. 400 PSI AT 72 DEGREES F. SERVICED THE CYLINDER IAW AMM 52-10-00.

Part: CYLINDER — LOW PRESSURE (L4 DOOR) · airframe 14,774 hrs · 4,247 cycles

L4 DOOR EMERGENCY OPERATING CYLINDER PRESSURE WAS LOW. 1500 PSI AT 72 DEGREES F. SERVICED THE CYLINDER IAW AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 14,548 hrs · 4,185 cycles

R1 DOOR DAMPER BOTTLE PRESSURE WAS BEYOND LIMITS, 1500PSI. THE AIRCRAFT WAS GROUNDED. SERVICED R1 DOOR DAMPER BOTTLE IAW AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 14,548 hrs · 4,185 cycles

L4 DOOR DAMPER BOTTLE PRESSURE BEYOND LIMITS, 1425 PSI. SERVICED THE BOTTLE IAW AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 14,548 hrs · 4,185 cycles

R4 DOOR DAMPER PRESSURE BEYOND LIMITS, 450 PSI. SERVICED THE R4 DOOR DAMPER BOTTLE IAW AMM 52-10-00.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 14,141 hrs · 4,073 cycles

EMERGENCY LIGHTS EPSU SYSTEM TEST FAILED 14WL. REPLACED THE BATTERY PACK IAW AMM 33-51-38. CHECKED GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 14,141 hrs · 4,073 cycles

EMERGENCY LIGHTS EPSU SYSTEM TEST FAILED 12WL, REPLACED THE BATTERY PACK IAW AMM 33-51-38 . EPSU SYSTEM TEST CHECKED GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 14,141 hrs · 4,073 cycles

EMERGENCY LIGHTS EPSU SYSTEM TEST FAILED, 15WL. REPLACED THE BATTERY PACK IAW AMM 33-51-38 . CHECKED GOOD.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 14,147 hrs · 4,074 cycles

R4 DOOR DAMPER BOTTLE PRESSURE WAS BELOW LIMITS. SERVICED THE BOTTLE IAW AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 14,147 hrs · 4,074 cycles

R1 DOOR DAMPER BOTTLE PRESSURE BELOW LIMITS. MAINTENANCE SERVICED THE BOTTLE IAW AMM 52-10-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 14,147 hrs · 4,074 cycles

R1 DOOR DAMPER BOTTLE PRESSURE WAS BELOW LIMITS. SERVICED THE R1 BOTTLE IAW AMM 52-10-00. OK FOR SERVICE.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 12,951 hrs · 3,789 cycles

R4 DOOR CYLINDER DAMPER PRESSURE BELOW LIMITS. SERVICED THE R4 DOOR CYLINDER IAW AMM 52-10-00.

Part: CYLINDER — LOW PRESSURE (L4 DOOR) · airframe 12,951 hrs · 3,789 cycles

L4 DOOR CYLINDER DAMPER PRESSURE BELOW LIMIT. SERVICED THE CYLINDER IAW AMM 52-10-00.

Part: DAMPER — LOW PRESSURE (L4 DOOR) · airframe 12,957 hrs · 3,790 cycles

AIRCRAFT WAS NOT GROUNDED: L4 DOOR CYLINDER (DAMPER) PRESSURE BELOW LIMIT (1400PSI). MAINTENANCE SERVICED L4 DOOR CYLINDER (DAMPER) TO PROPER PRESSURE PER AMM 52-10-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 12,066 hrs · 3,583 cycles

R4 DOOR EMERGENCY CYLINDER PRESSURE IS AT 400PSI. SERVICED THE CYLINDER IAW AMM 52-10-00-614-001A. OK FOR SERVICE.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 11,887 hrs · 3,542 cycles

R4 DOOR EMERGENCY OPERATIONS CYLINDER PRESSURE LOW, 500 PSI AT 75 DEGREES FARENHEIT. SERVICED THE CYLINDER IAW AMM 52-10-00.

Part: CYLINDER — LOW PRESSURE (L4 DOOR) · airframe 11,887 hrs · 3,542 cycles

L4 DOOR EMERGENCY OPERATING CYLINDER PRESSURE LOW AT 1500 PSI AT 75 DEGREES F. SERVICED THE CYLINDER IAW AMM 52-10-00.

Part: DAMPER — LOW PRESSURE (L4 DOOR) · airframe 11,779 hrs · 3,518 cycles

L4 DOOR DAMPER HAD LOW PRESSURE. SERVICED DAMPER IAW AMM 52-22-00.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 11,193 hrs · 3,389 cycles

AIRCRAFT NOT GROUNDED. FOUND R4 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED R4 DOOR ASSIST BOTTLE PER AMM 52-10-00.

Part: DAMPENER — LOW PRESSURE (L4 DOOR) · airframe 10,529 hrs · 3,243 cycles

AIRCRAFT WAS NOT GROUNDED. L4 DOOR DAMPENER LOW PRESSURE. SERVICED L4 DOOR DAMPENER AS REQUIRED PER AMM 52-10-00.

Part: DAMPENER — LOW PRESSURE (R4 DOOR) · airframe 10,529 hrs · 3,243 cycles

AIRCRAFT WAS NOT GROUNDED. R4 DOOR DAMPENER LOW PRESSURE. SERVICED R4 DOOR DAMPENER AS REQUIRED PER AMM 52-10-00.

Part: THERMOCOUPLE — FAULTY (LT ENGINE) · airframe 10,112 hrs · 3,132 cycles

AIRCRAFT WAS NOT GROUNDED. AT FLIGHT IDLE, N1 AND N2 SPLIT BETWEEN LEFT AND RIGHT ENGINE. MAINTENANCE REPLACED LEFT ENGINE FUEL TEMPERATURE THERMOCOUPLE PER AMM 73-35-15. FADEC OPERATIONS TEST AND IDLE LEAK CHECKS ACCOMPLISHED SATISFACTORY.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 10,038 hrs · 3,112 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR 4R EMERGENCY CYLINDER / ACCUMULATOR PRESSURE IS LOW. SERVICED DOOR 4R EMERGENCY CYLINDER/ ACCUMULATOR TO PROPER PRESSURE PER AMM 52-10-00-860-001-A.

Part: CYLINDER — LOW PRESSURE (L4 DOOR) · airframe 10,038 hrs · 3,112 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR 4L EMERGENCY CYLINDER / ACCUMULATOR PRESSURE IS LOW. SERVICED DOOR 4L EMERGENCY CYLINDER / ACCUMULATOR TO PROPER PRESSURE PER AMM 52-10-00-860-001-A.

Part: WIRE HARNESS — LOOSE (EMERGENCY LIGHTS) · airframe 9,683 hrs · 3,029 cycles

EMERGENCY LIGHTS MOUNTED ON THE SIDES OF SEATS 35C AND 36C ARE INOPERATIVE. FOUND LOOSE BROKEN WIRE 7260VC14-A IN LOWER SIDE WALL ROW 36L APPEARS TO BELONG TO EFFECTED EMERGENCY LIGHTS. REPLACED WIRE HARNESS 350WL14 IAW SWP 20-33-11. AIRCRAFT WAS GROUNDED.

Part: LIGHT — DAMAGED (CABIN) · airframe 9,683 hrs · 3,029 cycles

EMERGENCY LIGHTS MOUNTED ON THE SIDES OF SEATS 35C AND 36C ARE INOPERATIVE. FOUND LOOSE BROKEN WIRE 7260VC14-A AT LOWER SIDE WALL IN ROW 36L APPEARS TO BELONG TO EFFECTED EMERGENCY LIGHTS. REPLACED SEAT MOUNTED LIGHT AT ROW 35C AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS GROUNDED.

Part: LIGHT — DAMAGED (CABIN) · airframe 9,683 hrs · 3,029 cycles

EMERGENCY LIGHTS MOUNTED ON THE SIDES OF SEATS 35C AND 36C ARE INOPERATIVE. FOUND LOOSE BROKEN WIRE 7260VC14-A AT LOWER SIDE WALL IN ROW 36L APPEARS TO BELONG TO EFFECTED EMERGENCY LIGHTS. REPLACED SEAT MOUNTED LIGHT AT ROW 36C AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS GROUNDED.

Part: LIGHT — BROKEN (CABIN) · airframe 9,558 hrs · 2,999 cycles

BROKEN R1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY PER MM 33-51-13. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — BROKEN (CABIN) · airframe 9,558 hrs · 2,999 cycles

BROKEN L4 DOOR EMERGENCY EXIT LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY IAW MM 33-51-13. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — BROKEN (CABIN) · airframe 9,558 hrs · 2,999 cycles

BROKEN R4 DOOR EMERGENCY EXIT LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY PER MM 33-51-13. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 9,537 hrs · 2,994 cycles

R1 DOOR EMERGENCY EXIT SIGN LOWER FASTENER LIBERATED FROM SIGN. REPLACED EXIT SIGN IAW AMM 33-51-13.

Part: SIGN — BROKEN (CABIN) · airframe 9,512 hrs · 2,989 cycles

EMERGENCY EXIT SIGN AT R4 DOOR IS BROKEN OFF LOWER FASTNERS. MAINTENANCE REPLACED THE EXIT SIGN IAW AMM 33-51-13.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 9,512 hrs · 2,989 cycles

R1 DOOR EMERGENCY CYLINDER PRESSURE LOW. SERVICED THE R1 DOOR EMERGENCY CYLINDER IAW AMM 52-10-00.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 9,512 hrs · 2,989 cycles

R4 DOOR EMERGENCY CYLINDER PRESSURE LOW. SERVICED THE R4 DOOR CYLINDER IAW AMM 52-10-00.

Part: SIGN — BROKEN (CABIN) · airframe 9,512 hrs · 2,989 cycles

EMERGENCY EXIT SIGN AT THE L4 DOOR IS BROKEN OFF LOWER FASTNERS. MAINTENANCE TO REPLACE EXIT SIGN IAW AMM 33-51-13. REPLACED EXIT SIGN PER MM 33-51-13.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 9,471 hrs · 2,979 cycles

THE R4 DOOR CYLINDER HAD LOW PRESSURE. SERVICED THE CYLINDER IAW AMM 52-13-14.

Part: DAMPER — LOW PRESSURE (L4 DOOR) · airframe 8,809 hrs · 2,820 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR L4 EMERGENCY CYLINDER LOW PRESSURE. SERVICED DOOR DAMPER / CYLINDER AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: DAMPER — LOW PRESSURE (R4 DOOR) · airframe 8,809 hrs · 2,820 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR R4 EMERGENCY CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER / CYLINDER AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: DAMPER — LOW PRESSURE (L1 DOOR) · airframe 8,809 hrs · 2,820 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR L1 EMERGENCY CYLINDER / DAMPER PRESSURE LOW. SERVICED L1 DOOR AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: DAMPER — LOW PRESSURE (R1 DOOR) · airframe 8,809 hrs · 2,820 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR R1 EMERGENCY CYLINDER LOW PRESSURE. SERVICED DOOR DAMPER / CYLINDER AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 8,748 hrs · 2,801 cycles

R4 DOOR EMERGENCY CYLINDER PRESSURE LOW. SERVICED R4 DOOR CYLINDER IAW AMM 52-10-00. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 8,680 hrs · 2,776 cycles

R4 DOOR EMERGENCY CYLINDER PRESSURE IS LOW. SERVICED THE DOOR DAMPER IAW AMM 52-10-00.

Part: LIGHT — BROKEN (CABIN) · airframe 8,667 hrs · 2,772 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT PATH LIGHTING LENS IS BROKEN AT LAVATORY L. REPLACED EMERGENCY PROXIMITY LIGHT PER AMM 33-51-18.

Part: LIGHT — BROKEN (CABIN) · airframe 8,667 hrs · 2,772 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR R1 EMERGENCY EXIT SIGN IS BROKEN OFF LOWER FASTENER. REPLACED R1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY PER AMM 33-51-13.

Part: DAMPER — LOW PRESSURE (R4 DOOR) · airframe 8,539 hrs · 2,741 cycles

R4 DOOR DAMPER IS BELOW LIMITS, LOW PRESSURE. SERVICED THE DAMPER IAW AMM 52-10-00. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: DAMPER — LOW PRESSURE (R4 DOOR) · airframe 8,396 hrs · 2,704 cycles

R4 DOOR DAMPER HAD LOW PRESSURE. SERVICED THE R4 DOOR DAMPER IAW 52-10-00.

Part: DAMPER — LOW PRESSURE (L4 DOOR) · airframe 8,396 hrs · 2,704 cycles

L4 DOOR DAMPER HAD LOW PRESSURE. SERVICED THE L4 DOOR DAMPER IAW 52-10-00.

Part: CYLINDER — LOW (R4 DOOR) · airframe 7,672 hrs · 2,502 cycles

AIRCRAFT WAS NOT GROUNDED. R4 EMERGENCY DOOR DAMPER CYLINDER PRESSURE IS LOW. SERVICED CYLINDER IAW AMM 52-10-00. OPERATIONAL CHECK GOOD.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 7,612 hrs · 2,487 cycles

R4 EMERGENCY DOOR DAMPER CYLINDER PRESSURE IS LOW. SERVICED CYLINDER IAW AMM 52-10-00. LEAK AND OPERATIONAL CHECKED GOOD.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 7,612 hrs · 2,487 cycles

AIRCRAFT NOT GROUNDED. R4 DOOR DAMPER CYLINDER PRESSURE IS LOW. SERVICED CYLINDER IAW AMM 52-22-00. OPERATIONAL CHECK GOOD.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 7,430 hrs · 2,438 cycles

AIRCRAFT NOT GROUNDED. R4 EMERGENCY DOOR DAMPER CYLINDER PRESSURE IS LOW. SERVICED CYLINDER IAW AMM 52-10-00. OPERATIONAL CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 6,961 hrs · 2,304 cycles

R1 EMERGENCY DOOR DAMPER CYLINDER PRESSURE LOW. SERVICED CYLINDER IAW AMM 52-10-00. OPERATIONAL CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 6,961 hrs · 2,304 cycles

R4 EMERGENCY DOOR DAMPER CYLINDER PRESSURE LOW. SERVICED CYLINDER IAW AMM 52-10-00. OPERATIONAL CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 6,961 hrs · 2,304 cycles

L4 EMERGENCY DOOR DAMPER CYLINDER PRESSURE LOW. SERVICED CYLINDER IAW AMM 52-10-00. OPERATIONAL CHECKED GOOD.

Part: DAMPER — READS LOW (R4 DOOR) · airframe 6,326 hrs · 2,126 cycles

R4 DOOR EMERGENCY CYLINDER ACCUMULATOR PRESSURE IS BELOW ALLOWABLE LIMITS. SERVICED R4 DOOR EMERGENCY CYLINDER ACCUMULATOR IAW AMM 52-10-00.

Part: CYLINDER — LOW PRESSURE (R4 DOOR ASSIST) · airframe 6,239 hrs · 2,095 cycles

R4 DOOR CYLINDER ACCUMULATOR PRESSURE BELOW ALLOWABLE LIMITS. SERVICED THE CYLINDER IAW AMM 52-10-00.

Part: CYLINDER — LOW PRESSURE (R1 DOOR ASSIST) · airframe 6,239 hrs · 2,095 cycles

R1 DOOR EMERGENCY CYLINDER ACCUMULATOR PRESSURE LOW. SERVICED THE CYLINDER IAW AMM 52-10-00.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 5,321 hrs · 1,863 cycles

AIRCRAFT WAS NOT GROUNDED. R4 DOOR EMERGENCY CYLINDER ACCUMULATOR BOTTLE PRESSURE READS LOW. SERVICED R4 DOOR EMERGENCY/CYLINDER ACCUMULATOR BOTTLE TO PROPER LEVEL IAW AMM 52-10-00.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 4,697 hrs · 1,716 cycles

AIRCRAFT WAS NOT GNDED. EMER POWER SUPPLY UNIT 11WL FAILED OPERATIONAL TEST. R & R EMER POWER SUPPLY UNIT 11WL. ACCOMPLISHED OPERATIONAL TEST IAW AMM 33-51-38-400-001-A. SYS CHECKED NORMAL.

Part: LIFE RAFT — DEFECTIVE (CABIN) · airframe 4,288 hrs · 1,600 cycles

WHILE PERFORMING CABIN INSPECTION FOR DAMAGE OR IRREGULARITIES, FOUND THE LIFT RAFT IN MID CABIN COMING APART. R & R CABIN OVERHEAD BIN LIFE RAFT IAW AMM 25-66-41. OK FOR SERVICE. THE ACFT WAS NOT GNDED.

Part: SENSOR — FAULTY (BRAKE SYSTEM) · airframe 2,970 hrs · 1,237 cycles

RECEIVED HOT BRAKES MSG DURING TAKEOFF ROLL. TAKEOFF ABORTED AT APPROX 80 - 90 KNOTS. FOUND NR 4 BRAKE TEMPERATURE SENSOR FAULTY. R & R NR 4 BRAKE TEMPERATURE SENSOR IAW AMM 32-47-15. ACCOMPLISHED ACFT TAXI. BRAKE TEMPERATURE INDICATION CHECKED NORMAL IAW AMM 71-00-00.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 1,405 hrs · 614 cycles

R1 DOOR DAMPER & EMER OPERATION CYLINDER PRESS LOW. CHARGED CYLINDER TO WITHIN LIMITS IAW AMM 52-10-00.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 1,405 hrs · 614 cycles

R4 DOOR DAMPER & EMER OPERATION CYLINDER PRESS LOW. CHARGED CYLINDER TO WITHIN LIMITS IAW AMM 52-10-00.

Part: CONTROLLER — FAILED (PNUMATIC SYS)

PDX - FLT 25 - NR 3 MANIFOLD FAIL LIGHT CAME ON DURING FLIGHT. FOLLOWED CHECKLIST AND TURNED OFF NR 3 PNEU AND NR 3 PACK. PRESSURIZED PNEU SYSTEM 3. INSPECTED ALL DUCTING FOR LEAKS. NONE FOUND. INSPECTED WIRING TO DETECTORS IN WING, RES SWITCH AND LOOPS. NO DEFECTS FOUND. REMOVED AND REPLACED MANIFOLD FAIL CONTROLLER PER MM 36-23-00. NR 3 MANIFOLD FAIL TESTS NORMAL. (M)

Part: FIRE LOOP — FAILED (NR 1 ENGINE)

HNL - FLT 931 - NR 1 ENGINE B LOOP WILL NOT TEST. CHECKED SERIES RESISTANCE B LOOP AT 7 OHMS. REPLACED TEST RELAY K2-154 PRECAUTIONARY CHANGE, OPS AND FIRE TEST OK. (M)

Part: ENGINE — FAILED (NR 1)

FLT 3 - LAX - SLIGHT SMELL STARTED, 1 MINUTE LATER AIRCRAFT SHUDDERED. NR 1 EGT WENT OVER 900 DEG N2 DECAYED SHUT NR 1 ENGINE DOWN. ALTITUDE 12,000 FEET. REMOVED AND REPLACED NR 1 ENGINE. (M)

Part: HOUSING — CRACKED (HYD SYSTEM)

HNL - FLT 939 - HYDRAULIC SYSTEM 3 LEVEL OFF LIGHT ON. SYSTEM 3 HYDRAULIC QUANTITY ZERO, IT HAPPENED ON FINAL APPROACH AFTER ALL FLAPS OUT. PUMPS WERE TURNED OFF BEFORE 0. FOUND TRIM CYL INTERLOCK FUSE HOUSING CRACKED. REMOVED AND REPLACED FUSE PER MM 32-31-06.. OPS LEAK CHECK OK. RESERVICED QUANTITIES. (M)

Part: BUS CONTROL — FAILED (NR 2 GENERATOR)

SEA - FLT 21 - NR 2 GEN OFF LIGHT ON. ISSUED MEL 24-01 AUTH NR 9-194C-B. DURING OVERNIGHT MAINTENANCE RREMOVED AND REPLACED BUS CONTROL UNIT CHECKS OK. REMOVED PLACARD CLEARED MIC SHEET. (M)

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS)

HNL - FLT 466 - AFTER LANDING SLAT YELLOW DISAGREE LIGHT REMAINED ON AFTER RETRACTING FLAPS. RECYCLED FLAPS TO 50 DEGREES AND BACK AND LIGHT REMAINED ON. SECURITY AND CONDITION OF SLAT CHECKED OK. CHECKED SLAT SENSORS CHECKED OK. CHECKED SLAT HANDLE SWITCH CHECKED OK. BITE CHECK PROX BOX, CHECKED OK. OPERATED SLAT AND FLAP NUMEROUS TIMES, COULD NOT DUPLICATE AT THIS TIME. OK FOR SERVICE. (M)

Part: SENSOR — FAILED (NR 4 LE SLAT)

FLT 939 - LAX - SLAT DISAGREE LIGHT ILLUMINATED WHEN FLAPS ARE SET FOR 2 DEGREE, TAKEOFF DISAGREE LIGHT DOES NOT GO OUT UNTIL FLAP SLAT RETRACTED. REPLACED RIGHT NR 4 SLAT 'A' AND 'B' SENSOR, OPS CHECK OK. (M)

Part: SENSOR — MALFUNCTIONED (NR 3 ENGINE)

HNL - FLT 482 - NR 3 ENGINE 'A' LOOP WILL NOT TEST, 'B' TEST OK. REMOVED AND REPLACED CONNECTOR PYLON LOOP 'A' NR 3 ENGINE. 'A' LOOP TEST OP CHECKED GOOD. (M)

Part: RELAY — MALFUNCTIONED (NR 3 ENGINE)

HNL - FLT 25 - NR 3 ENGINE 'A' LOOP WILL NOT TEST. LOOP 'B' TEST OK. REMOVED AND REPLACED R2-153 RELAY GRN TEST GOOD. (M)

Part: OVEN — FAILED (GALLEY)

FLT 21 - HNL - OVEN NR 3 STARTED TO SMOKE IN FLIGHT. INSPECTION SHOWED THIS WAS NOT DUE TO MEAL BURNING. SMOKE CAME OUT THROUGH BOTTOM OF OVEN ONLY. OPS CHECK, OF NR 3 OVEN FOUND NO SMOKE COMING FROM OVEN. AFTER 45 MINUTES OF OP AT 375 DEGREES, OK THIS STATION LAX. (M)

Part: VALVE — FAILED (RT FUEL DUMP)

FLT NR 1 - LAX - RIGHT DUMP VALVE DID NOT OPEN DURING DUMP OPERATION. COMPLIED WITH AFM AND VALVE DID NOT OPEN. AIRCRAFT HAD ABORTED FLIGHT WITH STRONG ODOR IN CABIN AND COCKPIT. CHECKED AND REPLACED RIGHT FUEL DUMP VALVE ACT. ACCOMPLISHED REQUIRED GROUND OPS CHECK, AS PER MM. RIGHT F/DUMP VALVE GROUND OPS CHECK NORMAL. (M)

Part: AIR DIST — ODOR (CABIN)

LAX - FLT 1 - STRONG ODOR IN CABIN AND COCKPIT, ABORTED FLIGHT. AIRCRAFT RETURNING TO LAX. ACCOMP CLEANING OF HEAT EXCHANGERS PER MM 21-53-01. CLEANED APU INLET, RAN ENGINES 1 AT A TIME WITHOUT APU RUNNING TRYING TO ISOLATE THE SMELL OF OIL OR THE SOURCE. NO HELP. FOUND RESIDUAL, OIL IN APU COMPARTMENT AND INLET AREA. CLEANED UP OIL. ACCOMPLISHED HEAT EXCHANGER CLEAN OUT PROCEDURES PER MM 21-53-01 PAGES 209-210. REPLACED COALESCAR BAGS AND CABIN RECIRCULATION FILTERS. ACCOMPLISHED TAKEOFF POWER RUN WITH ALL PNEUMATIC SYSTEMS ON AIRCRAFT PACKS ON, NO STRONG ODOR DETECTED THROUGHOUT CABIN OR COCKPIT, OK FOR SERVICE. (M)

Part: WIRE — BROKEN (NR 1 ENGINE)

HNL - FLT 482 - ENGINE NR 1 ANTI-ICE DISAGREE LIGHT ILLUMINATED WITH NR 1 ENGINE ANTI-ICE SWITCH OFF. ACCOMPLISHED ABNORMAL PROCEDURES SECTION 6-6. REPAIRED BROKEN WIRE ON PIN E OF PLUG. OPS CHECK ON E58 AND OPS CHECK NORMAL ON ENGINE RUN. (M)

Part: PROX BOX — FAILED (E/E COMPT)

HNL - FLT 10 - SLAT DISAGREE LIGHT CAME ON WITH SLAT IN TAKEOFF POSITION ON APPROACH, THEN WENT BACK TO TAKEOFF. REMOVED AND REPLACED PROX BOX. (M)

Part: BATTERY — DISCHARGED (CABIN)

HNL - FLT 3 - FLASHLIGHT BATTERY WEAK. REMOVED AND REPLACED FLASHLIGHT BATTERY. OPS CHECK GOOD. (M)

Part: PUMP — FAILED (NR 3 SYSTEM)

HNL - FLT 1215 - LOST HYDRAULIC QTY ON NR 3 SYSTEM, DURING FLIGHT. ALTERNATE GEAR EXTENTION PERFORMED. FOUND 2/3 REVERSIBLE PUMP BYPASSING TO OVERFLOW. REPLACED 2/3 REVERSIBLE PUMP. INSPECTED NR 3 ENGINE FILTERS, OPS CHECK, LEAK CHECK OK. (M)

Part: LONGERON — CORRODED (BS 1154-1144)

TUL - LONGERON NR 48R OUTBOARD ATTACHMENT FLANGE CORRODED IN SEVERAL LOCATIONS. REPAIRED LONGERON BY INSTALLING 7075-T6 .063 INCH DOUBLER REF DC-10 SRM 53-00-01 VOL 1, DC-10 SRM 53-10-00 VOL 1 AND DC-10 ESO 7349 DATED 6-12-97. (M)

Part: SUPPORT — CRACKED (BS 755)

TUL - FLOOR SUPPORT CRACKED AT STATION 755 UPPER ATTACH FLANGE. REMOVED DAMAGED SECTION OF FLOOR SUPPORT. INSTALLED NEW SUPPORT SECTION AND DOUBLER PER SRM VOL 1 53-60-01. (M)

Part: SHEAR TIE — CORRODED (BS 1139)

TUL - SHEAR TIES CORRODED BETWEEN LONGERON 51 RT AND 51 LT STATION 1139. REMOVED AND REPLACED SHEAR TIES PER AARD 51-21-00. (M)

Part: FITTING — CORRODED (BS 1156)

TUL - AFT END OF LONGERON 52 CORRODED AT 'T' FITTING FOR PRESS DOM. REMOVED LONGERON 52 DUE TO EXCESS CORROSION REF DC10 AARD 51-01-00-03. INSTALLED NEW FABRICATED AFT END OF LONGERON 52 AT 'T' FITTING FOR PRESS DOME SRM 51-01-00-05 TREATED PRIMED AND PAINTED AREA PER SRM 51-21-01. (M)

Part: SKIN — CORRODED (BS 1156)

TUL - BULGE IN BEAUTY STRIP SKIN AT STATION 1156 LONGERON 48 RIGHT. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM VOL 1 53-20-00. (M)

Part: ROLLER TRAY — CORRODED (BS 999)

TUL - CENTER ROLLER TRAY AT STATION 999 HAS SURFACE CORROSION ON RIGHT FLANGE DOUBLER. INSTALLED NEW ANGLES PER AARD 51-01-00-05 ITEMS 5, AARD 51-10-00-21 REPAIR 1. (M)

Part: SUPPORT — CORRODED (BS 1099)

TUL - FOUND CORROSION ON SUPPORT STRUCTURE FOR ROLLER TRAY 2ND FROM RT OUTBOARD. INSTALLED NEW ROLLER SUPPORT PER AARMD 51-10-00-21 REPAIR 1. (M)

Part: SILL — CORRODED (BS 1099)

TUL - STATION 1099 AFT SILL BELOW AND AFT OF RT UNLOAD BAR PULLEY CONFIG, SILL HAS HEAVY CORROSION AROUND NUTPLATE. INSTALL NEW SILL PER AARD 51-01-00-05 ITEM 5, AARD 51-10-00-21 REPAIR 1. (M)

Part: ANGLE — CORRODED (BS 1099)

TUL - FLOORBOARD NUT PLATE ANGLE HAS CORROSION INBOARD OF Z-ANGLE. INSTALLED NEW ANGLE PER AARD 51-01-00-05 ITEM 5, AARD 51-10-00-21 REPAIR 1. (M)

Part: FLOORBOARD — CORRODED (BS 1099)

TUL - FOUND FLOORBOARD LANDING CORRODED LOCATED BETWEEN LEFT Z-ANGLE AND 2ND TRACK INBOARD FROM Z-ANGLE. INSTALLED NEW LANDING PER AARD 51-01-00-5 ITEMS AARD 51-10-00-21 REPAIR 1. (M)

Part: SEAT TRACK — CORRODED (BS 1902)

TUL - NR 1 SEAT TRACK CORRODED FROM RIGHT SIDE JUST AFT OF RIGHT DOOR IN SEVERAL PLACES. INSTALL REPAIR PER SRM 53-70-00 P 66 AND ALODINE, PRIME. (M)

Part: SPLICE — CORRODED (BS 979-999)

TUL - FOUD STRINGER SPLICE FROM STATION 979 TO 999 HAS SURFACE CORROSION AT STRINGER 52. INSTALLED NEW STRINGER SPLICE AS PER SRM 53-10-00. (M)

Part: SUPPORT — CORRODED (BS 839)

TUL - FOUND CORROSION ON THE RIGHT SIDE OF G1A GALLEY (FWD EDGE). ACCOMPLISHED REPAIR OF FORWARD BEAM RIGHT SIDE OF P-LIFT IAW ESO DATED 5-29-97 ADN 7349. (M)

Part: SUPPORT — CORRODED (BS 775-795)

TUL - FIRST SUPPORT RIGHT OF CENTER SEAT TRACK UNDER GALLEY 1, HAS CORROSION AROUND MOUNT HOLES. INSTALLED F/B SUPPORT RT OF CENTER SEAT TRACK UNDER GALLER 1 PER SRM 51-72-10-0. ALODINED, PRIMED AND PAINTED. (M)

Part: SUPPORT — CORRODED (BS 775-795)

TUL - FOUND CORROSION ON FLOOR SUPPORT, FIRST SUPPORT LEFT OF CENTER SEAT TRACK UNDER GALLEY 1. INSTALLED FLOORBOARD SUPPORT LEFT OF CENTE RSEAT TRACK UNDER GALLEY 1 PER SRM 51-72-10-0, ALODINED, PRIMED AND PAINTED. (M)

Part: DOOR TRACK — CORRODED (BS 879)

TUL - LEFT FIRE BLOCK DOOR TRACK STA 879 INBOARD OF LOWER LOBE GALLEY. TRACK NR 2 HEAVY CORROSION. REPLACED CORRODED PORTION OF FIRE BLOCK DOOR TRACK PER DC 10-10 AARD 51-01-00-05 AND 51-10-00-21 REPAIR 1. TST: 65,993 HRS. CYCLES, 22,816. (X)