N676AW

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 38,580 hrs · 14,079 cycles

AIRCRAFT WAS GNDED. LT SIDE EMER FLOOR LIGHTS AT ROWS 26, 24, 22, 17 & 13 INOPERATIVE. REPLACED EPSU 11WL & 13WL. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38 & 33-51-00-710-001. PLEASE SEE AALA201512159006 FOR ADDITIONAL POWER SUPPLY INFORMATION.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,580 hrs · 14,079 cycles

AIRCRAFT WAS GROUNDED. LT SIDE EMERGENCY LIGHTS AT ROWS 26, 24, 22, 17 & 13 WERE INOPERATIVE. REPLACED EPSU 11WL & 13WL. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38 & 33-51-00-710-001.

Part: LIGHT — DETACHED (CABIN) · airframe 38,580 hrs · 14,079 cycles

AIRCRAFT WAS GNDED. ROW 23 LT EMERGENCY LIGHT WAS DETACHED. ATTACHED THE EMERGENCY LIGHT AT ROW 23L & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-00-710-001.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 38,573 hrs · 14,076 cycles

AIRCRAFT WAS NOT GNDED. SEAT EMER LIGHTS AT 13, 17, 22 & 26 INOPERATIVE. REPLACED EMER POWER SUPPLY UNIT IAW AMM 33-51-38-000-001-A.

Part: ENGINE — BIRD INGESTION (LEFT) · airframe 38,482 hrs · 14,037 cycles

UPON APPROACH, SEVERAL MEDIUM SIZED BIRDS HIT THE LT ENG COWLING. THE FLIGHT CREW DID NOT DECLARE AN EMER, BUT ATC HAD EMER TRUCKS RESPOND. THE FLIGHT LANDED SAFELY WITH NO INCIDENTS. INSPECTED THE ACFT & DISCOVERED THAT THE LT ENG HAD INGESTED BIRDS. MAINTENANCE REPLACED THE LEFT ENGINE PER TASK CARD 26L40071004.

Part: LIGHT — LOOSE (CABIN) · airframe 38,300 hrs · 13,955 cycles

EMERGENCY ESCAPE PATH LIGHT BELOW SEAT 4C IS LOOSE. REPLACED EMER ESCAPE PATH LIGHT & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,079 hrs · 13,852 cycles

EMERGENCY LIGHT AT 4C INOPERATIVE. REPLACED EMER LIGHT.

Part: LENS — MISSING (CABIN) · airframe 36,898 hrs · 13,373 cycles

EMERGENCY EXIT LIGHT LENS AT ROW 10 RT MISSING. INSTALLED ROW 10 RT EMER EXIT LIGHT LENS.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 36,472 hrs · 13,199 cycles

EPSU BATTERY BAD UNDER LT OVERWING DOORS. R & R EPSU BATTERY ON EPSU UNDER LT OVERWING DOORS.

Part: PUMP — FAILED (HYD SYSTEM)

FLT 504 EN-ROUTE, WHILE IN CRUISE FLIGHT, THE ACFT EXPERIENCED A GREEN HYD SYS OVERHEAT WARNING, FOLLOWED BY A GREEN HYD ENG 1 PUMP LOW PRESS FAULT, THEN A PTU FAULT. AS A PRECAUTION, THE FLIGHT DIVERTED. THE FLIGHT CREW DECLARED AN EMER. THE FLIGHT LANDED WITHOUT INCIDENT & THE ACFT WAS TOWED TO THE GATE. REPLACED THE NR 1 ENG HYD PUMP & FILTERS ASSOCIATED WITH THE GREEN HYD SYS.

Part: PIN — INOPERATIVE (EMERGENCY EXIT) · airframe 36,336 hrs · 13,145 cycles

LEFT FWD OVERWING EXIT HATCH DISARM PIN INOPERATIVE. R & R PIN IAW AMM 52-22-22. GOOD OPERATIONAL CHECK.

Part: LIGHT — DISLODGED (CABIN) · airframe 36,219 hrs · 13,094 cycles

EMERGENCY EXIT LIGHT AT SEAT 7C REPORTED BROKEN. REINSERTED EMER LIGHT ASSEMBLY. GOOD OPERATIONAL CHECK.

Part: SLIDER — OBSTRUCTED (R1 DOOR) · airframe 35,933 hrs · 12,986 cycles

FLIGHT ATTENDANT CANNOT DISARM SLIDE AT DOOR R1. REMOVED DEBRIS FROM R1 DOOR ARM SLIDER. OPERATIONS NORMAL.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 35,769 hrs · 12,915 cycles

AFT FLIGHT ATTENDANT JUMP SEAT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT AS REQUIRED.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,740 hrs · 12,906 cycles

EMERGENCY LIGHT INOPERATIVE AT 19L. REPLACED SEAT AND FLOOR WIRE HARNESS AT ROW 19L IAW AMM 33-51-19.

Part: HANDLE — DIRTY (L2 DOOR) · airframe 35,430 hrs · 12,784 cycles

AFT DOOR 2L DIFFICULT TO ARM, GETS STUCK HALFWAY. REMOVED DEBRIS. OPERATIONS CHECKED GOOD.

Part: FASTENER — LOOSE (NLG DOOR) · airframe 34,637 hrs · 12,489 cycles

AIRFRAME VIBRATION, LIGHT TO MODERATE INTENSITY. FOUND LOOSE & WORN HARDWARE ON NLG DOOR ASSEMBLY AFT RT. REPLACED LOWER BOY PIVOT POINT & HARDWARE, DIDN'T DISTURB ADJUSTMENT IAW AMM 32-22-13-410-001A.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 33,374 hrs · 12,021 cycles

RON VISIT DELAMINATION ON FWD CARGO FLOOR PANEL 131AF BETWEEN FRAME 24A TO FRAME 28 & BETWEEN STRINGER 38R TO STRINGER 38L AT BL0. REPLACED FWD CARGO FLOOR PANEL 131AF IAW AMM 53-22-14-401.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 32,955 hrs · 11,886 cycles

EXIT ROW RED INDICATION LIGHT ON SEAT MISSING. INSTALLED MISSING LIGHT COVER AT EXIT ROW RED INDICATION LIGHT.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHT OUT AT ROW 8 DEF. REPLACED EMERGENCY LIGHT ASSEMBLY AT ROW 8 DEF.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 31,931 hrs · 11,510 cycles

CREW REPORTS EMERGENCY EXIT LIGHT 4C STICKING OUT, WIRES EXPOSED. REPOSITIONED EMERGENCY LIGHT ASSEMBLY AT SEAT 4C & OPERATIONS CHECKED GOOD IAW AMM 33-51-00 PB501.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 31,561 hrs · 11,372 cycles

SMOKE LAV DETECTOR FAULT. MAINTENANCE R & R LAV "A" SMOKE DETECTOR.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 31,493 hrs · 11,345 cycles

CREW REPORTED LAVATORY "A" SMOKE DETECTOR FAULT. MX R & R LAVATORY "A" SMOKE DETECTOR IAW AMM 26-17-15. OPS TEST GOOD.

Part: OIL COOLER — LEAKING (APU) · airframe 31,493 hrs · 11,345 cycles

CREW REPORTED A DIRTY MUSTY ODOR IN AFT CABIN. SHORTY AFTER, SMOKE DETECTOR FAULTED, ABOUT 10 MINUTES BEFORE LANDING. MAINTENANCE INSPECTED APU COMPARTMENT AND FOUND APU OIL COOLER LEAKING OIL. R & R APU OIL COOLER FAN ASSY IAW AMM 49-52-51. OPS AND LEAK CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 31,448 hrs · 11,324 cycles

DIRTY SOCK ODOR IN CABIN. ACCOMPLISHED INSPECTION, NO DEFECTS NOTED.

Part: LIGHT — DAMAGED (CABIN) · airframe 30,423 hrs · 10,983 cycles

ROW 3 ACFT LT- EMERGENCY EXIT LIGHT TORE OFF. REINSTALLED EMERGENCY EXIT LIGHT AT ROW 3.

Part: MEGAPHONE — BROKEN (CASBIN) · airframe 30,301 hrs · 10,945 cycles

AFT MEGAPHIONE HANDLE LOOSE AND DETACHING. REPLACED MEGAPHONE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 29,994 hrs · 10,852 cycles

INFO ONLY. MOMENTARY LAV SMOKE WARNING. F/A REPORT NO EVIDENCE OF SMOKE. RESET LAV SMOKE DETECTION SYS IAW MM 26-17-00-710-A. NO FAULTS OR HISTORY NOTED.

Part: LIGHT — BROKEN (CABIN) · airframe 29,933 hrs · 10,836 cycles

EMERGENCY EXIT LIGHT ON SEAT 1C IS BROKEN, CRACKED. REPLACED EMERGENCY LIGHT AT SEAT 1C.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,100 hrs · 10,211 cycles

EMERGENCY LIGHT SEAT ROW 13 INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT AT ROW 13.

Part: LENS — MISSING (CABIN) · airframe 26,839 hrs · 9,772 cycles

LENS COVER OVER DOOR LIGHT LEFT REAR MISSING. REPLACED MISSING EMERGENCY EXIT LIGHT LENS AT LEFT AFT DOOR.

Part: LIGHT — BROKEN (CABIN) · airframe 26,095 hrs · 9,547 cycles

FLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHTING ON SEAT 11C BROKEN. RE-SECURED EMERGENCY LIGHT AT ROW 11C, OPERATIONAL CHECK GOOD.

Part: SHUTOFF VALVE — FAULTY (THRUST REVERSER) · airframe 25,579 hrs · 9,383 cycles

ENGINE 1 REVERSER FAULT AFTER LANDING. REMOVED AND REPLACED NR 1 ENGINE HCU SHUTOFF VALVE IAW AIRBUS MAINTENANCE MANUAL 78-37-51.

Part: RELAY — FAULTY (THRUST REVERSER) · airframe 25,439 hrs · 9,338 cycles

ON LANDING ROLLOUT, 'ENG 1 REVERS UNLOCK' ECAM MESSAGE. MAINTENANCE REMOVED AND REPLACED RELAYS 3EG1 AND 2EG1 IAW TROUBLESHOOTING MANUAL 78-00-810-807 AND ELECTRICAL STANDARD PRACTICES MANUAL 20-46-50. OPERATIONAL CHECK OF NR 1 ENGINE T/R WAS GOOD.

Part: CONTROL UNIT — FAILED (THRUST REVERSER) · airframe 25,418 hrs · 9,331 cycles

NR 1 THRUST REVERSER FAILED ON LANDING ROLLOUT. MAINTENANCE REMOVED AND REPLACED NR 1 HYDRAULIC CONTROL UNIT IAW AIRBUS MAINTENANCE MANUAL 78-31-51.

Part: ATTACH FITTING — WORN (MLG DOOR) · airframe 25,225 hrs · 9,254 cycles

LEFT AFT NOSE LANDING GEAR DOOR HAS BUSHING WORN BEYOND LIMITS AT FORWARD ATTACH FITTING PER MM 32-22-00-220-002. REPLACED LEFT AFT NOSE LANDING GEAR DOOR ASSEMBLY IAW AMM 32-22-00-120-001.

Part: LENS — BROKEN (CABIN) · airframe 24,573 hrs · 9,026 cycles

SMALL EXIT SIGN COVER BROKEN BY L1 DOOR. REPLACED LENS BY L1 DOOR.

Part: LIGHT — LOOSE (CABIN) · airframe 24,464 hrs · 8,983 cycles

EMERGENCY EXIT LIGHT 7A LOOSE. MAINTENANCE SECURED EMERGENCY EXIT LIGHT ON SEAT 7A.

Part: LIGHT — OUT OF ADJUST (CABIN) · airframe 24,445 hrs · 8,973 cycles

1S CHECK, SEATS 9C, 13C, 17C, 22C, AND 26C EMERGENCY EXIT LIGHTS REQUIRE ADJUSTMENT SO THE LIGHT SHINES DOWN ON THE FLOOR. ADJUSTED SEATS 9C, 13C, 17C, 22C, AND 26C EMERGENCY EXIT LIGHTS SO THEY SHINES DOWN ON THE FLOOR IAW A320 AMM 33-51-00-710-001.

Part: CONNECTOR — MISSING (CABIN) · airframe 24,445 hrs · 8,973 cycles

1S CHECK , SEAT 11C EMERGENCY EXIT LIGHT INOPERATIVE. UPON REMOVAL OF THE LIGHT 1 SLIP ON CONNECTOR WAS FOUND TO BE MISSING. INSTALLED CONNECTOR AND LIGHT. PERFORMED OPERATIOAL CHECK OF THE LIGHT WITH NO DEFECTS NOTED.

Part: LIGHT — OUT OF ADJUST (CABIN) · airframe 24,445 hrs · 8,973 cycles

1S CHECK, LEFT FORWARD WINDSCREEN EMERGENCY EXIT LIGHT IS RECESSED AND HARD TO SEE. ADJUSTED LIGHT AS REQUIRED.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 24,445 hrs · 8,973 cycles

1S CHECK - DELAMINATION ON FLOOR PANEL 221PF BETWEEN FR12 TO FR16, BETWEEN Y453 TO Y1732. REPLACED FLOOR PANEL 221PF IAW JOB CARD 26C22053014.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 24,445 hrs · 8,973 cycles

1S CHECK - DELAMINATION ON FLOOR PANEL 221EF BETWEEN FR16 TO FR20 & BETWEEN Y260 TO Y1292. REPLACED FLOOR PANEL 221EF IAW JOB CARD 26C22053014.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 24,445 hrs · 8,973 cycles

1S CHECK - 4 AREAS OF DELAMINATION ON FLOOR PANEL 242KF BETWEEN FR42 TO FR47 & BETWEEN -Y254 TO -Y765. REPLACED FLOOR PANEL 242KF IAW JOB CARD 26C22053014.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 24,445 hrs · 8,973 cycles

1S CHECK - DELAMINATION ON FLOOR PANEL 241GF BETWEEN FR36 TO FR42 & BETWEEN Y765 TO Y1292. REPLACED FLOOR PANEL 241GF IAW JOB CARD 26C24053002.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 24,445 hrs · 8,973 cycles

1S CHECK - AREA OF DELAMINATION ON FLOOR PANEL 151AF AT FR49, Y=0. REPLACED FLOOR PANEL 151AF IAW A320 SRM 53-02-00 PARA G FIG 209.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 24,445 hrs · 8,973 cycles

1S CHECK - AREA OF DELAMINATION ON FLOOR PANEL 151DF AT FR53, -Y12. REPLACED FLOOR PANEL 151DF IAW A320 SRM 53-02-00 PARA G FIG 209.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 24,445 hrs · 8,973 cycles

1S CHECK - DELAMINATION ON CARGO FLOOR PANEL 151LF AT FR57, Y4 TO -Y18. REPAIRED CARGO FLOOR PANEL 151LF IAW A320 SRM 53-02-00 PAR C FIGURE 204.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 24,445 hrs · 8,973 cycles

1S CHECK - CRACK ON FLOOR PANEL 131AF AT FR27, Y16. REPAIRED FLOOR PANEL 131AF IAW A320 SRM 53-02-00 PARA C, FIG 204.

Part: CONNECTOR — LOOSE (CABIN) · airframe 24,303 hrs · 8,915 cycles

EMERGENCY LIGHT ROW 1 INOPERATIVE. FOUND CONNECTOR UNDER ROW 1 SEAT LOOSE. SECURED CONNECTOR. OPS CHECKED GOOD IAW AIRBUS MAINTENANCE MANUAL 33-15-19.

Part: REGULATOR VALVE — FAULTY (AC BAY) · airframe 23,191 hrs · 8,529 cycles

RECEIVED HOT AIR FAULT DURING CLIMB. COULD NOT SHUT OFF HOT AIR VALVE WITH THE SWITCH. RETURNED TO PHX AND DECLARED EMERGENCY. REMOVED AND REPLACED PRESSURE REGULATING VALVE 14KH, ALL SYSTEMS OPS CHECK GOOD.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 22,703 hrs · 8,370 cycles

FLT 84 - SEA - EEL - ROW 3L EMERGENCY AISLE LIGHTING INOPERATIVE. MAINTENANCE RECONNECTED ELECTRICAL CONNECTORS TO LIGHT ASSEMBLY.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 22,181 hrs · 8,187 cycles

PIT - C11/SY6 - SOFT SPOT ON CABIN FLOOR PANEL 251YF BETWEEN FR62 TO FR64 & BETWEEN Y765 TO Y1292. REPLACED FLOOR PANEL 251YF BETWEEN FR62 TO FR64 & BETWEEN Y765 TO Y1292 IAW MCGILL IRM 9701 REV G.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,181 hrs · 8,187 cycles

PIT - C11/SY6 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67, Y1160. REPLACED FLOORBEAM BETWEEN FR64 TO FR67, Y1160 IAW A320 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,181 hrs · 8,187 cycles

PIT - C11/SY6 - LEVEL 2 EXFOLIATION CORROSION ON RIGHT SHEAR PLATE BETWEEN FR68 TO FR70, S23R. REPLACED RIGHT SHEAR PLATE BETWEEN FR68 TO FR70, S23R IAW SRM 51-72-1 & TYPICAL REPAIR 320-2528-10-0011A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,181 hrs · 8,187 cycles

PIT - C11/SY6 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67, Y1160. REPLACED FLOORBEAM BETWEEN FR64 TO FR67, Y1160 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,181 hrs · 8,187 cycles

PIT - C11/SY6 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR66, S23L. REPLACED FLOORBEAM AT FR66, S23L IAW A320 SRM 51-42-11.

Part: LENS — MISSING (CABIN) · airframe 19,408 hrs · 7,146 cycles

FLT 73 - SEA - EEL - L1 EMERGENCY LIGHT LENS MISSING. MAINTENANCE INSTALLED LENS FOR EMERGENCY LIGHT ON FORWARD SIDE OF L1 DOOR.

Part: LIGHT — MISSING (CABIN) · airframe 17,680 hrs · 6,552 cycles

FLT 186 - SAN - EEL - FOUND EMERGENCY EXIT LIGHT MISSING AT ROW 13 AIRCRAFT LEFT. MAINTENANCE REPLACED LIGHT.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 16,949 hrs · 6,304 cycles

FLT 652 - PHX - EMERGENCY EQUIPMENT - FORWARD FLIGHT ATTENDANT STATION FLASHLIGHT BATTERY INOPERATIVE. MAINTENANCE REPLACED BATTERY.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 16,817 hrs · 6,251 cycles

FLT 680 PHX - EEL - EMERGENCY EXIT ROW LIGHT NEEDS TO BE REPLACED AT ROW 7L. MAINTENANCE REPLACED LIGHT ASSEMBLY AT ROW 7L.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 16,363 hrs · 6,102 cycles

FLT 394 - LAS - EEL - AISLE EMERGENCY LIGHT AT ROW 24 INOPERATIVE. MAINTENANCE RECONNECTED CONNECTION FOR AISLE LIGHT AT ROW 24.

Part: LENS — MISSING (EMERGNECY LIGHTS) · airframe 16,131 hrs · 6,026 cycles

FLT 532 - EMERGENCY LIGHT FIXTURE ROW 13 IS MISSING. MAINTENANCE REPLACED MISSING LIGHT FIXTURE ROW 13 PER MM 33-51-19.

Part: SLIDE — FAILED (L1 DOOR) · airframe 14,907 hrs · 5,627 cycles

FLT 71 - MCO-PHX - EMERGENCY EQUIPMENT - FLIGHT ATTENDANT OPENED THE L1 DOOR WHILE ARMED AND THE SLIDE FELL OUT OF THE AIRCRAFT AND UNRAVELED. THE SLIDE DID NOT INFLATE. REMOVED AND REPLACED L1 DOOR SLIDE ASSEMBLY IN ACCORDANCE WITH TASK CARD R1C25305. VENDOR REPORTS A DEEP SCORE ON THE BALL SEAT. REMOVED AND REPLACED BALL SEAT.

Part: RESERVOIR — FAULTY (EVAC SLIDE) · airframe 14,484 hrs · 5,480 cycles

FLT 409 PHX-SFC - EMERGENCY EQUIPMENT - CIDS CAUTION CFDS MESSAGE SLIDE BOTTLE EMERGENCY R. MAINTENANCE REMOVED AND REPLACED THE SLIDE BOTTLE PER AIRBUS MAINTENANCE MANUAL 25-62-46-400-001.

Part: CONNECTOR — BROKEN (CABIN) · airframe 11,503 hrs · 4,448 cycles

P-9 CHECK PHX - EEL - ROW 19 AISLE EMERGENCY EXIT LIGHT INOPERATIVE LED LIGHT. REPLACED BROKEN CONNECTOR AT WALL. OPERATIONAL CHECK GOOD.