N625AW

Part: CONTROL UNIT — INOPERATIVE (THRUST REVERSER) · airframe 76,166 hrs · 34,308 cycles

RETURN TO FIELD DUE TO ENG NR 2 THRUST REVERSER PRESSURIZED ECAM MESSAGE ON CLIMB OUT THROUGH FLIGHT LEVEL 320. REPLACED THE NR 2 ENGINE HYDRAULIC CONTROL UNIT.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,192 hrs · 33,867 cycles

EMERGENCY LIGHT ESPU TEST FAILED. REPLACED ESPU WITH SERVICEABLE UNIT AND OPS CHECKED OK IAW AMM 33-51-38-0401--A.

Part: LENS — MISSING (CABIN) · airframe 74,584 hrs · 33,569 cycles

ROW 22 ACFT LT CLEAR EMERGENCY PATH LIGHT LENS MISSING. REPLACED ROW 22L EMERGENCY PATH LIGHT LENS.

Part: LENS — MISSING (CABIN) · airframe 74,584 hrs · 33,569 cycles

ROW 9 AC LEFT RED EMERGENCY PATH LIGHT MISSING RED LENS. REPLACED ROW 9L EMERGENCY PATH LIGHT LENS.

Part: SPRING — WEAK (LAVATORY) · airframe 74,569 hrs · 33,560 cycles

AFT LAVATORY A/C RT TRASH FLAP INOPERATIVE. REPLACED SPRING ON TRASH RECEPTACLE FLAP.

Part: UNKNOWN — ODOR (CABIN) · airframe 74,524 hrs · 33,543 cycles

F/A REPORTED A CIGARETTE LIKE ODOR IN BACK OF ACFT ALONG WITH AN ACRID ODOR. 1 OF THE F/A REPORTED FEELING NAUSEA AND EYE IRRITATION. ANOTHER F/A FELT DIZZY AND ILL WITH HIVE LIKE SYMPTOMS. THE PILOTS REPORTED NAUSEA ALONG WITH EYE AND THROAT IRRITATION. THE CAPTAIN ADVISED THAT THERE WAS NO SMOKE VISABLE. MX COMPLIED WITH "TROUBLESHOOT AIR QUALITY" JOB CARD. UNABLE TO DUPLICATE CABIN ODOR.

Part: UNKNOWN — ODOR (CABIN) · airframe 74,516 hrs · 33,538 cycles

CABIN ODOR DURING FLIGHT. MX INSPECTED CABIN FOR AIR QUALITY, NO DISCREPANCIES FOUND.

Part: COVER — MISSING (OVERWING EXIT) · airframe 74,471 hrs · 33,515 cycles

EMERGENCY LIGHT COVER MISSING OVER ACFT LT OVERWING. REPLACED MISSING LENS COVER ON THE LT OVERWING.

Part: LENS — MISSING (EXIT SIGN) · airframe 74,106 hrs · 33,346 cycles

EMERGENCY EXIT LIGHT RED LENS 11D MISSING. REPLACED EXIT SIGN ON SEAT 11D.

Part: LENS — MISSING (CABIN) · airframe 74,106 hrs · 33,346 cycles

ROW 11 FLOOR EMERGENCY EXIT LIGHTS WILL NOT ILLUMINATE. EXIT LIGHT ILLUMINATES, NO DEFECT. REPLACED MISSING LENS.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 74,033 hrs · 33,312 cycles

GO GO MOD - DELAMINATION ON FLOOR PANEL 131HF BETWEEN STA 1323 TO STA 1483 & BETWEEN S40L TO S40R. REPLACED FLOOR PANEL 131HF IAW A320 AMM 53-22-12/14 & EA 204786.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 74,033 hrs · 33,312 cycles

GO GO MOD - METAL SURFACE DAMAGE ON FLOOR PANEL 132FF BETWEEN STA 1163 TO STA 1323 & BETWEEN S35R TO S40R. REPLACED FLOOR PANEL 132FF IAW A320 AMM 25-54-11 & EA 204786.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 74,033 hrs · 33,312 cycles

GO GO MOD - DELAMINATION ON FLOOR PANEL 131EF BETWEEN STA 1163 TO STA 1323 & BETWEEN S40L TO S40R. REPLACED FLOOR PANEL 131EF IAW A320 AMM 53-22-12/14 & EA 204786.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 74,033 hrs · 33,312 cycles

GO GO MOD - DELAMINATION ON FLOOR PANEL 132JF BETWEEN STA 1323 TO STA 1483 & BETWEEN S35R TO S40R. REPLACED FLOOR PANEL 132JF IAW A320 AMM 25-54-11 & EA 204786.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 74,033 hrs · 33,312 cycles

GO GO MOD - DELAMINATION ON FLOOR PANEL 151LF BETWEEN STA 2616 TO STA 2723 & BETWEEN S40L TO S40R. REPLACED FLOOR PANEL 151LF IAW A320 AMM 53-22-12/14 & EA 204786.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,029 hrs · 33,311 cycles

GOGO MOD - CORROSION ON STRINGER 43L AT FR56. REPAIRED STRINGER 43L AT FR56 IAW A320 SRM 53-00-13, FIG 202.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 73,991 hrs · 33,288 cycles

FLASHLIGHT AT FORWARD FLIGHT ATTENDANT STATION NEEDS REPLACEMENT. REMOVED AND REPLACED FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT.

Part: LENS — MISSING (CABIN) · airframe 73,876 hrs · 33,229 cycles

ROW 11 EXIT LIGHTING ON BOTTOM OF SEAT IN AISLE IS BROKEN OFF. REPLACED MISSING EXIT LIGHT LENS AT SEAT ROW 11 LEFT.

Part: BOLT — SHEARED (FUSELAGE) · airframe 73,550 hrs · 33,073 cycles

MECHANICS REPORT - FOUND SHEARED BOLT ON SEAT TRACK STRINGER ATTACH POINT AT FORWARD WALL AFT CARGO LEFT SIDE IN CEILING. REPLACED SHEARED BOLT AT SEAT TRACK ATTACH POINT JUST AFT OF FR46 IAW A320 SRM 51-42-11.

Part: DIAPHRAGM — LEAKING (R2 DOOR) · airframe 73,294 hrs · 32,956 cycles

R2 DOOR ASSIST BOTTLE LOW. REPLACED R2 DOOR ASSIST BOTTLE DIAPHRAGM AND SERVICED IAW AIRBUS MAINTENANCE MANUAL 52-10-00.

Part: STRAP — MISROUTED (R1 DOOR) · airframe 73,166 hrs · 32,889 cycles

DOOR 1R WILL NOT ARM. REROUTED GIRT STRAPS ON R1 DOOR SLIDE IAW AIRBUS MAINTENANCE MANUAL 25-62-44-04.

Part: DOOR — OUT OF ADJUST (L2) · airframe 72,584 hrs · 32,611 cycles

BC2 CHECK - OUT ADJUSTMENT DIMENSION "B" BETWEEN STRIKER LEVER AND FINGER AT DOOR 832 (L2). ADJUSTED DIMENSION "B" BETWEEN STRIKER LEVER AND FINGER AT DOOR 832 (L2) IAW AMM 52-13-14-820-002-A ITEM 4A, STEP 1.

Part: DOOR — OUT OF ADJUST (L1) · airframe 72,584 hrs · 32,611 cycles

BC2 CHECK - OUT ADJUSTMENT DIMENSION "A" BETWEEN STRIKER LEVER AND FINGER AT DOOR 831 (L1). ADJUSTED DIMENSION "A" BETWEEN STRIKER LEVER AND FINGER AT DOOR 831 (L1) IAW A320 AMM 52-11-14-820-002-A ITEM 4A, STEP 2.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 72,584 hrs · 32,611 cycles

C2 CHECK - CORROSION ON EXISTING REPAIR DOUBLER ON FUSELAGE SKIN BETWEEN FR69+5 INCHES TO FR69+17 INCHES & BETWEEN S31R TO S33R. REPLACED EXISTING REPAIR DOUBLER IAW A320 SRM 51-72-11, 53-41-11, PAR 5.D, FIG 205.

Part: EXTINGUISHER — UNSERVICEABLE (GALLEY) · airframe 72,364 hrs · 32,501 cycles

H2O FIRE EXTINGUISHER SEAL MISSING. REMOVED AND REPLACED H2O FIRE EXTINGUISHER IN THE AFT GALLEY AS REQUIRED.

Part: AUTOTHRUST SYS — MALFUNCTIONED (COCKPIT) · airframe 71,443 hrs · 32,054 cycles

ON FINAL APPROACH WITH APPROACH ACTUATED, AUTOTHRUST APPARENTLY DISCONNECTED AND WENT TO CLIMB POWER. CONFIGURATION WAS FLAP 2, GEAR DOWN. AIRCRAFT QUICKLY ACCELERATED AND OVERSPEED INDICATED FOR FLAPS 2 (ESTIMATED AT ABOUT 10 KNOTS). PERFORMED INSPECTION OF FLAP/SLAT EXTENSION IAW AIRBUS MAINTENANCE MANUAL 05-51-13-200-001-A. AIRCRAFT OK FOR SERVICE.

Part: EXTINGUISHER — UNSERVICEABLE (CABIN) · airframe 71,283 hrs · 31,975 cycles

AFT PORTABLE FIRE EXTINGUISHER NOT SERVICEABLE. REMOVED AND REPLACED AFT PORTABLE FIRE EXTINGUISHER.

Part: LENS — BROKEN (CABIN) · airframe 71,222 hrs · 31,946 cycles

SEAT 26 EXIT LIGHT BROKEN. REPLACED LENS COVER.

Part: LENS — MISSING (CABIN) · airframe 71,078 hrs · 31,874 cycles

EMERGENCY LIGHT RED LENS MISSING AT ROW 11 RIGHT. REPLACED LENS.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 71,001 hrs · 31,841 cycles

FLT 57 - CREW DISCREPANCY FOUND FLOORBOARD HAS WEAK SOFT SPOT AT CENTER AISLE NEAR ROWS 17 AND 18. REPLACED FLOOR PANEL AT CENTER AISLE NEAR ROWS 17 AND 18 IAW A320 AMM 53-22-12.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 70,926 hrs · 31,807 cycles

EMERGENCY EXIT LIGHT AT SEAT 11A FLICKERS ON AND OFF. MAINTENANCE PERFORMED SEVERAL OPERATIONAL CHECKS WITH NO FAULTS NOTED.

Part: LENS — MISSING (CABIN) · airframe 70,483 hrs · 31,604 cycles

EMERGENCY LIGHT LENS MISSING 9-R. INSTALLED EMERGENCY LIGHT LENS 9-R.

Part: UNKNOWN — FIRE (APU) · airframe 70,397 hrs · 31,568 cycles

AS THE AIRCRAFT WAS IN LINE FOR TAKEOFF, THERE WAS REPORT OF AN APU FIRE FROM THE AIRCRAFT BEHIND US. THE APU HAD BEEN SHUT OFF FOR ABOUT 3 MINUTES. THE APU FIRE BOTTLE WAS DISCHARGED ALTHOUGH THERE WAS NEVER ANY FIRE INDICATION IN FLIGHT DECK. FIRE DEPARTMENT RESPONDED AND CONFIRMED NO FLAMES - FOLLOWED AIRCRAFT BACK TO GATE. VENDOR TEARDOWN REPORTS FOR APU FUEL CONTROL UNIT AND FUEL FLOW DIVIDER BOTH INDICATED 'NO FAULT FOUND'. NO SUBSEQUENT EVENTS REPORTED ON THIS AIRCRAFT.

Part: CHECK VALVE — LEAKING (HYDRAULIC SYS) · airframe 70,318 hrs · 31,531 cycles

DIRTY SOCK SMELL NOTED DURING TAKEOFF, CLIMB, CRUISE AND DESCENT. SMELL DISSIPATED APPROXIMATELY 2 HOURS INTO CRUISE AND RETURNED SHORTLY AFTER TOP OF DESCENT WITH THROTTLES AT FLIGHT IDLE. MAINTENANCE FOUND HYDRAULIC LEAK THAT WAS STREAMING INTO APU INLET. REMOVED AND REPLACED YELLOW SYSTEM HP MANIFOLD CHECK VALVE 3059GM; PERFORMED APU COMPRESSOR WASH AND ECS DECONTAMINATION.

Part: LENS — BROKEN (CABIN) · airframe 69,979 hrs · 31,379 cycles

FORWARD ENTRY BULKHEAD LOWER CORNER EMERGENCY LIGHT LENS BROKEN. INSTALLED NEW LENS COVER ON FORWARD ENTRY BULKHEAD LOWER CORNER EMERGENCY LIGHT IAW AIRBUS MAINTENANCE MANUAL 33-51-13.

Part: APU — LEAKING (APU BAY) · airframe 69,245 hrs · 31,051 cycles

CREW REPORTED A DIRTY SOCK SMELL THROUGHOUT AIRCRAFT IN ALL FLIGHT PHASES. MAINTENANCE TROUBLESHOT TO INTERNAL APU LEAK. REMOVED AND REPLACED APU.

Part: LIGHT — LOOSE (CABIN) · airframe 69,224 hrs · 31,040 cycles

EMERGENCY ESCAPE LIGHTING ROW 9 A/C RIGHT UNSECURED/LOOSE. MAINTENANCE RE-SECURED EMERGENCY LIGHT AT ROW 9 RIGHT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 68,268 hrs · 30,613 cycles

FLT 439 - LAS - EEL - FLIGHT ATTENDANT PANEL EMERGENCY TEST FAILED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY, FORWARD POSITION, IAW AIRBUS MAINTENANCE MANUAL 33-51-38.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 67,656 hrs · 30,331 cycles

PIT - C1 - EEL - WHEN PERFORMING TEST: SLIDE ARMED LIGHT DID NOT COME ON WHEN DOOR WAS ARMED & OPEN HANDLE WAS MOVED OUT OF THE CLOSED & LOCKED POSITION. HOWEVER COCKPIT INDICATORS WERE NORMAL. REPLACED LIGHT ASSEMBLY IN L-2 DOOR. OPS TEST NORMAL.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 67,482 hrs · 30,248 cycles

PIT - C1 - MAJOR REPAIR - NUMEROUS CRACKS IN RIGHT FORWARD OVERWING EMERGENCY EXIT DOOR SEGMENT FRAME FORWARD OF WINDOW. REPLACED RIGHT FORWARD OVERWING EMERGENCY EXIT DOOR SEGMENT FRAME FORWARD OF WINDOW IAW EO 5210Y228.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 67,482 hrs · 30,248 cycles

PIT - C1 - MAJOR REPAIR - NUMEROUS CRACKS IN LEFT AFT OVERWING EMERGENCY EXIT DOOR SEGMENT FRAME AFT OF WINDOW. REPLACED LEFT AFT OVERWING EMERGENCY EXIT DOOR SEGMENT FRAME AFT OF WINDOW IAW EO 5210Y228.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 67,482 hrs · 30,248 cycles

PIT - C1 - MAJOR REPAIR - NUMEROUS CRACKS IN LEFT FORWARD OVERWING EMERGENCY EXIT DOOR SEGMENT FRAME AFT OF WINDOW. REPLACED LEFT FORWARD OVERWING EMERGENCY EXIT DOOR SEGMENT FRAME AFT OF WINDOW IAW EO 5210Y228.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 67,482 hrs · 30,248 cycles

PIT - C1 - MAJOR REPAIR - NUMEROUS CRACKS IN LEFT AFT OVERWING EMERGENCY EXIT DOOR SEGMENT FRAME FORWARD OF WINDOW. REPLACED LEFT AFT OVERWING EMERGENCY EXIT DOOR SEGMENT FRAME FORWARD OF WINDOW IAW AIRWAYS EO 5210Y228.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 67,482 hrs · 30,248 cycles

PIT - C1 - MAJOR REPAIR - NUMEROUS CRACKS IN RIGHT AFT OVERWING EMERGENCY EXIT DOOR SEGMENT FRAME FORWARD OF WINDOW. REPLACED RIGHT AFT OVERWING EMERGENCY EXIT DOOR SEGMENT FRAME FORWARD OF WINDOW IAW EO 5210Y228.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 67,482 hrs · 30,248 cycles

PIT - C1 - MAJOR REPAIR - NUMEROUS CRACKS IN RIGHT FORWARD OVERWING EMERGENCY EXIT DOOR SEGMENT FRAME AFT OF WINDOW. REPLACED RIGHT FORWARD OVERWING EMERGENCY EXIT DOOR SEGMENT FRAME AFT OF WINDOW IAW EO 5210Y228.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 67,482 hrs · 30,248 cycles

PIT - C1 - MAJOR REPAIR - NUMEROUS CRACKS IN LEFT FORWARD OVERWING EMERGENCY EXIT DOOR SEGMENT FRAME FORWARD OF WINDOW. REPLACED LEFT FORWARD OVERWING EMERGENCY EXIT DOOR SEGMENT FRAME FORWARD OF WINDOW IAW EO 5210Y228.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 67,482 hrs · 30,248 cycles

PIT - C1 - MAJOR REPAIR - NUMEROUS CRACKS IN RIGHT AFT OVERWING EMERGENCY EXIT DOOR SEGMENT FRAME AFT OF WINDOW. REPLACED RIGHT AFT OVERWING EMERGENCY EXIT DOOR SEGMENT FRAME AFT OF WINDOW IAW EO 5210Y228.

Part: DIAPHRAGM — DAMAGED (DAMPER) · airframe 67,656 hrs · 30,331 cycles

PIT - EES - C1 CHECK - R1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. REPLACED DIAPHRAGM AND SERVICED IAW A320 AMM 52-22-00-860-002.

Part: EEC — FAULTY (NR 2 ENGINE) · airframe 67,040 hrs · 30,043 cycles

FLT 4 ORD-PHX - RTO - DURING TOGA POWER T/O, NR 2 ENGINE EPR SURGED TWICE - DECREASED TO 1.25 FROM 1.4. REJECTED TAKEOFF AT APPROXIMATELY 100 KTS. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE FUEL METERING UNIT (FMU) AND ELECTRONIC ENGINE CONTROL (EEC).

Part: FMU — FAULTY (NR 2 ENGINE) · airframe 67,040 hrs · 30,043 cycles

FLT 4 ORD-PHX - RTO - DURING TOGA POWER T/O, NR 2 ENGINE EPR SURGED TWICE - DECREASED TO 1.25 FROM 1.4. REJECTED TAKEOFF AT APPROXIMATELY 100 KTS. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE FUEL METERING UNIT (FMU) AND ELECTRONIC ENGINE CONTROL (EEC).

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 66,533 hrs · 29,815 cycles

FLT 271 - LAS - EEL - EMERGENCY EXIT LIGHT TEST FAULTS EXT AND INT AFT LEFT LOADS. MAINTENANCE REMOVED AND REPLACED AFT LEFT EMERGENCY EXIT LIGHT POWER SUPPLY UNIT IAW AIRBUS MAINTENANCE MANUAL 33-51-38-401.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 65,954 hrs · 29,560 cycles

FLT 356 - LAS - EMERGENCY EQUIPMENT - FORWARD L-1 DOOR FLIGHT ATTENDANT MEGAPHONE IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD L-1 DOOR MEGAPHONE.

Part: LENS — LOOSE (CABIN) · airframe 65,880 hrs · 29,525 cycles

FLT 5 - PHL - EEL - FORWARD GALLEY EMERGENCY EXIT LIGHT LENS COVER KEEPS FALLING OFF. MAINTENANCE SECURED FORWARD GALLEY EMERGENCY EXIT LIGHT.

Part: SWITCH — DEFECTIVE (BLEED AIR SYS) · airframe 64,829 hrs · 29,046 cycles

FLT 371 - PHX - RETURN TO FIELD - APU BLEED FAULT ON CLIMB. CREW WAS UNABLE TO CLEAR THE FAULT AND RETURNED TO PHX. MAINTENANCE REMOVED AND REPLACED THE APU BLEED SWITCH IAW TROUBLESHOOTING MANUAL 30-12-00-810-801.

Part: WINDOW — CRACKED (COCKPIT) · airframe 63,868 hrs · 28,628 cycles

FLT 5 - ORD - EMERGENCY LANDING - LEFT AFT COCKPIT WINDOW SHATTERED ON CLIMBOUT AT 13,500 FT. NO LOSS OF PRESSURIZATION. ALSO ANTI-ICE LEFT WINDOW FAULT. CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO ORD. MAINTENANCE REMOVED AND REPLACED THE LEFT AFT FIXED WINDOW IAW AIRBUS MAINTENANCE MANUAL 56-11-12-400-002 AND WINDOW HEAT CONTROLLER IAW AIRBUS MAINTENANCE MANUAL 30-42-34-400-001.

Part: CONTROLLER — FAULTY (COCKPIT) · airframe 63,868 hrs · 28,628 cycles

FLT 5 - ORD - EMERGENCY LANDING - LEFT AFT COCKPIT WINDOW SHATTERED ON CLIMBOUT AT 13,500 FT. NO LOSS OF PRESSURIZATION. ALSO ANTI-ICE LEFT WINDOW FAULT. CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO ORD. MAINTENANCE REMOVED AND REPLACED THE LEFT AFT FIXED WINDOW IAW AIRBUS MAINTENANCE MANUAL 56-11-12-400-002 AND WINDOW HEAT CONTROLLER IAW AIRBUS MAINTENANCE MANUAL 30-42-34-400-001.

Part: LENS — MISSING (CABIN) · airframe 63,767 hrs · 28,584 cycles

FLT 612 - PHX-ATL - EMERGENCY LIGHTS - ROW 9L AISLE EMERGENCY LIGHT LENS MISSING. REPLACED EMERGENCY LIGHTS LENS ROW 9L.

Part: LENS — MISSING (CABIN) · airframe 63,767 hrs · 28,584 cycles

FLT 612 - PHX-ATL - EMERGENCY LIGHTS - ROW 24L AISLE EMERGENCY LIGHT MISSING LENS. REPLACED EMERGENCY LIGHT LENS ROW 24L.

Part: LENS — BROKEN (CABIN) · airframe 63,514 hrs · 28,471 cycles

FLT 1779 - LAS - EEL - PASSENGER BROKE EMERGENCY EXIT FLOOR LIGHT COVER 9D. MAINTENANCE INSTALLED NEW LENS COVER AT 9D EMERGENCY EXIT LIGHT.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 63,398 hrs · 28,418 cycles

FLT 612 - ATL - EMERGENCY EGRESS SYSTEM - L1 ENTRY DOOR DAMPER & EMERGENCY OPERATION CYLINDER PRECHARGE IS LOW. MAINTENANCE SERVICED L1 DOOR DAMPER & EMERGENCY OPERATION CYLINDER AS PER AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 63,338 hrs · 28,391 cycles

FLT 614 - ATL - EMERGENCY EGRESS SYSTEM - L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. MAINTENANCE SERVICED L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER IAW AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.

Part: BATTERY — FAULTED (CABIN) · airframe 63,267 hrs · 28,363 cycles

FLT 128 - PHX - EEL - "L FWD EMER BATTERY" FAULT DURING EMERGENCY LIGHT CHECK. MAINTENANCE REMOVED AND REPLACED LEFT FORWARD EMERGENCY POWER SUPPLY UNIT BATTERY.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 63,059 hrs · 28,274 cycles

FLT 5 - PHX - EEL - FORWARD FLIGHT ATTENDANT'S FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD.

Part: CABLE — BROKEN (SLIDE RESERVOIR) · airframe 62,948 hrs · 28,226 cycles

PIT - C8 - EES - NR 5001032 - RIGHT OVERWING SLIDE RESERVOIR HAS A BROKEN END CABLE. REPLACED RESERVOIR IAW US AIRWAYS TASK CARD F1C52301.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 63,047 hrs · 28,154 cycles

PIT - C8 - MAJOR REPAIR - CRACK IN FORWARD PRESSURE PANEL AT FR36 IN RIGHT AIR CONDITIONING BAY. REPAIRED FORWARD PRESSURE PANEL AT FR36 IN RIGHT AIR CONDITIONING BAY IAW US AIRWAYS ENGINEERING CARD M2C53307.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 63,047 hrs · 2,815 cycles

PIT - C8 - MAJOR REPAIR - CRACKS IN FORWARD PRESSURE PANEL AT FR36 IN LEFT AIR CONDITIONING BAY. REPAIRED FORWARD PRESSURE PANEL AT FR36 IN LEFT AIR CONDITIONING BAY IAW US AIRWAYS ENGINEERING CARD M2C53306.

Part: SKIN — SATURATED (ELEVATOR) · airframe 62,948 hrs · 28,226 cycles

PIT - C8 - MAJOR REPAIR - NR 26-0555-8-0030/001 - RIGHT HAND ELEVATOR HAS TRAPPED WATER IN UPPER SKIN. REPAIRED RIGHT HAND ELEVATOR UPPER SKIN IAW A320 SRM 57-21-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,793 hrs · 28,226 cycles

PIT - C8 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR68, -Y1221. REPLACED FLOORBEAM AT FR68, -Y1221 IAW SRM 51-72-11.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,948 hrs · 28,226 cycles

PIT - C8 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON BEAM AT FR66, BETWEEN Y254 TO Y465. REPLACED BEAM AT FR66, BETWEEN Y254 TO Y465 IAW SRM 51-42-12.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,948 hrs · 28,226 cycles

PIT - C8 - MAJOR REPAIR - LEVEL 2 INTERGRANULAR CORROSION ON LEFT BEAM AT FR66, Y515. REPLACED LEFT BEAM AT FR66, Y515 IAW SRM 51-72-11.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 62,782 hrs · 28,149 cycles

LOG PAGE 4408073 - FLT 350-LAS - EMERGENCY EQUIPMENT - L1 DOOR ASSIST BOTTLE LOW PRESSURE. MAINTENANCE SERVICED DOOR ASSIST BOTTLE PER AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.

Part: LENS — MISSING (CABIN) · airframe 28,233 hrs · 10,982 cycles

FLT 351 - SAN-PHX - EMERGENCY LIGHTS - 24C EMERGENCY EXIT LIGHT COVER BROKEN/MISSING. REPLACED EMERGENCY LIGHT LENS AT SEAT 24C.

Part: LINE — UNSECURE (EVAC SLIDE) · airframe 62,299 hrs · 27,938 cycles

CAMPAIGN EO - PHX - EMERGENCY EGRESS SYSTEM - PRECAUTIONARY INSPECTION OF SLIDE RAFTS FOR PROPER HARNESS/CABLE/LANYARD ROUTING AND CONNECTION FOUND FORWARD RT SLIDE RAFT MOORING LINE NOT SECURED BY VELCRO. MAINTENANCE RETURNED TO SERVICEABLE CONDITION PER EO INSTRUCTIONS.

Part: CYLINDER — LOW (L1 DOOR) · airframe 62,078 hrs · 27,841 cycles

FLT 350 - PHX-LAS - EE - L1 DOOR ASSIST LOW PRESSURE. SERVICED L1 DOOR ASSIST TO PROPER PRESSURE.

Part: POWER SUPPLY — SEPARATED (CABIN) · airframe 61,947 hrs · 27,777 cycles

FLT 202 PHX-ABQ - EMERGENCY LIGHT - PANEL AT FLOOR LEVEL ON SIDEWALL BELOW OVERWING EMERGENCY EXIT, A/C RIGHT CAME OFF. 2 FUSES CAME OUT OF ELECTRICAL UNIT INSIDE. THERE ARE 3 EMPTY SPACES FOR FUSES ON UNIT. CONTRACT MX R&R THE RT OVERWING EMERGENCY EXIT POWER SUPPLY PER MM 33-51-15. OPS TEST GOOD.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 61,785 hrs · 27,708 cycles

FLT 296 LAS-SEA - EMERGENCY EQUIPMENT - L1 DOOR ASSIST BOTTLE REQUIRES SERVICE. MAINTENANCE SERVICED L1 DOOR ASSIST BOTTLE AS REQUIRED.

Part: SPLICE — BROKEN (CABIN) · airframe 60,231 hrs · 26,979 cycles

FLT 401 ORD-PHX - EEL EMERGENCY PATH LIGHT INOP ROW 17 LT. MAINTENANCE REPLACED BROKEN SPLICES UNDER SEAT. OPERATIONAL CHECK WAS GOOD. (A)

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 59,368 hrs · 26,584 cycles

NR 329 - PHX - EEL - EMERGENCY LIGHT AT SEAT 13 INOP. MAINTENANCE RECONNECTED LOOSE WIRES AND ASSEMBLY. OPERATIONAL CHECK WAS GOOD.

Part: PANEL — DEFECTIVE (COCKPIT) · airframe 59,049 hrs · 26,436 cycles

FLT NR 540 - PHX-DFW - AIR TURNBACK - RETURNED TO GATE FOR START FAULT IGNITION B NR 2 ENGINE WITH IGNITION B NR 1 ENGINE ALREADY ON MEL. ACCOMPLISHED MANUAL START PER MX CONTROL AND AIRCRAFT DEPARTED. IGNITION CIRCUIT BREAKERS P-39 THROUGH P-42 POPPED AFTER TAKEOFF. AIRCRAFT RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED THE ENGINE START PANEL.

Part: CONTROL UNIT — DEFECTIVE (TE FLAPS) · airframe 58,904 hrs · 26,367 cycles

FLT NR 441 - YVR-LAS - EMERGENCY LANDING, F/CTL FLAPS LOCKED ALIGNMENT FAULT ON LANDING. FLAPS LOCKED AT ZERO. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR CONTROL INTERFACE UNIT. OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,077 hrs · 26,025 cycles

FLT 350 - MSP-PHX - EEL - ROW 9 & 11 ABC & DEF EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY RIGHT MID IAW A320 AMM 33-51-38.

Part: PSU — NO TEST (ZONE 200) · airframe 58,010 hrs · 25,997 cycles

SAL - EEL - C7 CHECK - L FWD DOOR EMERGENCY LIGHT EPSU FAILED DURING OPERATIONAL TEST. REMOVED AND REPLACED L FWD DOOR EMERGENCY LIGHT EPSU AND PERFORMED OPERATIONAL TEST GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 58,010 hrs · 25,997 cycles

SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON SEAT TRACK, BS 808/FR 20, -Y765. REPLACED SEAT TRACK, BS 808/FR 20, -Y765 IAW A320 SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 58,010 hrs · 25,997 cycles

SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 605 / FR 12 - BS 950 / FR 24, +Y254. REPLACED CABIN FLOORBEAM, BS 605 / FR 12 - BS 950 / FR 24, +Y254 IAW A320 SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 58,010 hrs · 25,997 cycles

SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOOR SUPPORT, BS 3158 / FR 66 - BS 32157 / FR 68, +Y1292. REPLACED CABIN FLOOR SUPPORT, BS 3158 / FR 66 - BS 32157 / FR 68, +Y1292 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 58,010 hrs · 25,997 cycles

SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON SEAT TRACK, BS 808 / FR 20 - BS 843 / FR 21, +Y1292. REPLACED SEAT TRACK, BS 808 / FR 20 - BS 843 / FR 21, +Y1292 IAW A320 SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 58,010 hrs · 25,997 cycles

SAL - MAJOR REPAIR - CRACKED SHEAR PLATE, BS 3257/FR 68 - BS 3310/FR 69, S23L. REPLACED SHEAR PLATE, BS 3257/FR 68 - BS 3310/FR 69, S23L IAW A320 SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 58,010 hrs · 25,997 cycles

SAL - MAJOR REPAIR - C7 CHECK - CRACKED SHEAR PLATE, BS 3257/FR 68 - BS 3310/FR 69, S23R. REPLACED SHEAR PLATE, BS 3257/FR 68 - BS 3310/FR 69, S23R IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 58,010 hrs · 25,997 cycles

SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON FLOORBEAM, BS 657/FR 14, -Y25 TO -Y81. REPLACED FLOORBEAM, BS 657/FR 14, -Y25 TO -Y81 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 58,010 hrs · 25,997 cycles

SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON SEAT TRACK, BS 1810/FR 41 - BS 2136/FR 47, -Y765. REPLACED SEAT TRACK, BS 1810/FR 41 - BS 2136/FR 47, -Y765 IAW A320 SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 58,010 hrs · 25,997 cycles

SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON FLOORBEAM, BS 3257 / FR 68, -Y1165. REPLACED FLOORBEAM, BS 3257 / FR 68 - BS 3310 / FR 69, -Y1165 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 58,010 hrs · 25,997 cycles

SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON FLOORBEAM, BS 605/FR 12 - BS 709/FR 16, -Y81. REPLACED FLOORBEAM, BS 605 FR 12 - BS 709 FR 16, -Y81 IAW A320 SRM 51-72-11.

Part: PLATE — CORRODED (FUSELAGE) · airframe 58,010 hrs · 25,997 cycles

SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON SUPPORT PLATE, BS 3310/FR 69 - BS 3366/FR 70, S23R. REPLACED SUPPORT PLATE, BS 3310/FR 69 - BS 3366/FR 70, S23R IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 58,010 hrs · 25,997 cycles

SAL - MAJOR REPAIR - C7 CHECK - 6016788, CORROSION ON FLOORBEAM, BS 3101/FR 65 - BS 3207/FR 67, -Y464. REPLACED FLOORBEAM, BS 3101/FR 65 - BS 3207/FR 67, -Y464 IAW A320 SRM 51-72-11.

Part: O-RING — LEAKING (NR 1 ENGINE HCU) · airframe 57,681 hrs · 25,861 cycles

PHX - IAH - FLT 274 - THE CREW REPORTED THE A/C LOST GREEN HYDRAULIC SYSTEM WHICH RENDERS NOSE WHEEL STEERING INOP. THE CREW DECLARED AN EMERGENCY. THE LANDING WAS UNEVENTFUL AND THE A/C WAS TOWED TO THE GATE. MX REPLACED THE NR 1 ENGINE HCU DIFFERENTIAL PRESSURE HOUSING O-RING. OPERATIONAL / LEAK CHECK WAS GOOD. THE A/C WAS RETURNED TO SERVICE.

Part: CONTROL BOX — FAILED (E/E BAY) · airframe 56,779 hrs · 25,439 cycles

CREW REPORTED SMOKE LAV & CARGO DET FAULT. MX REPLACED SDCU PER MM26-17-34. OPS CHECK WAS GOOD.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 56,310 hrs · 2,518 cycles

PHX - MAJOR REPAIR - CABIN FLOORBOARD 241EF IN CENTER AISLE IS DELAMINATED AT SEAT ROW 12. REPLACED CABIN FLOORBOARD 241EF IN CENTER AISLE AT SEAT ROW 12 IAW AWA TASK CARD R1C25306.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 56,310 hrs · 25,218 cycles

PHX - MAJOR REPAIR - R2 DOOR ENTRYWAY FLOORBOARD 262 FF DELAMINATED, FR 66 - FR 68, -Y1292 TO -Y1732. REPLACED R2 DOOR ENTRYWAY FLOORBOARD 262 FF DELAMINATED, FR 66 - FR 68, -Y1292 TO -Y1732 IAW AWA TASK CARD R1C25306.

Part: PLATE — CORRODED (L2 DOOR) · airframe 52,979 hrs · 23,723 cycles

SAL - EES - DURING C6 CHECK DISCOVERED HONEYCOMB BROKEN ON PLATE OF GIRT BAR FITTING IN THE L2 DOOR FORWARD POSITION. MAINTENANCE REMOVED AND REPLACED PLATE OF GIRT BAR FITTING IN THE L2 DOOR FORWARD POSITION IAW AIRBUS 320 AMM 52-13-31.

Part: FLOOR PANEL — CRACKED (FWD CARGO BAY) · airframe 52,979 hrs · 23,723 cycles

SAL - MAJOR REPAIR - DURING C6 CHECK DISCOVERED FLOOR PANEL 131CF DELAMINATED OUT OF LIMITS IN THE FWD CARGO COMPARTMENT. MAINTENANCE REMOVED AND INSTALLED FABRICATED FLOORBOARD 131CF IAW IRM 9701F.

Part: FLOOR PANEL — DELAMINATED (FWD CARGO BAY) · airframe 52,979 hrs · 23,723 cycles

SAL - MAJOR REPAIR - DURING C6 CHECK DISCOVERED FLOOR PANEL 131AF IN THE FWD CARGO COMPARTMENT, DOUBLER DISBONDED AND FLOOR PANEL DELAMINATED. MAINTENANCE REMOVED AND INSTALLED FABRICATED FLOOR PANEL 131AF IAW IRM 9701 REV F AND AWA ER 26-5326-05209-RC1C.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 52,979 hrs · 23,723 cycles

SAL - MAJOR REPAIR - DURING BC4 CHECK DISCOVERED FLOOR PANEL 152CF DELAMINATED IN THE AFT CARGO COMPARTMENT. MAINTENANCE REMOVED AND INSTALLED FABRICATED FLOOR PANEL, 152CF IAW IRM 9701 F.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 52,979 hrs · 23,723 cycles

SAL - MAJOR REPAIR - DURING C6 CHECK DISCOVERED FLOOR PANEL 151MF DELAMINATED OUT OF LIMITS IN THE AFT CARGO COMPARTMENT. MAINTENANCE REMOVED AND INSTALLED FABRICATED FLOORBOARD 151MF IAW IRM 9701F.

Part: STRUCTURE — CORRODED (LT MLG) · airframe 52,979 hrs · 23,723 cycles

SAL - MAJOR REPAIR - NR 5912605 - DURING C06 CHECK DISCOVERED CORROSION ON LOWER CARDAN THREAD AREA ON THE LT MLG. MAINTENANCE REMOVED AND REPLACED THE LOWER CARDAN ON THE LT MAIN LANDING GEAR IAW AIRBUS 320 AMM 32-11-16. FREE FALL TEST WAS PERFORMED IAW AIRBUS 320 AMM 32-33-80.

Part: STRUCTURE — CORRODED (LT MLG) · airframe 45,516 hrs · 18,559 cycles

SAL - MAJOR REPAIR - NR 5912601 - DURING C06 CHECK DISCOVERED CORROSION ON UPPER CARDAN THREAD AREA ON THE LT MLG. MAINTENANCE REMOVED AND REPLACED THE UPPER CARDAN ON THE LT MAIN LANDING GEAR IAW AIRBUS 320 AMM 32-11-16. FREE FALL TEST WAS PERFORMED IAW AIRBUS 320 AMM 32-33-80. OPS CHECK GOOD.

Part: SILL — CORRODED (FUSELAGE) · airframe 52,979 hrs · 23,723 cycles

SAL - MAJOR REPAIR - DURING C6 CHECK DISCOVERED CORROSION ON THE L2 DOOR SILL AT FR 66+4 INCHES. MAINTENANCE REMOVED AND REPLACED THE SILL BEAM ON THE L2 DOOR FROM FR 66 TO FR 68 AT Y1340 TO Y1600 IAW AIRBUS 320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,979 hrs · 23,723 cycles

SAL - DURING C6 CHECK DISCOVERED CORROSION ON PASSENGER SEAT TRACK AT Y-765 AND FS 46+18". CORROSION WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK SECTION FROM FS 41 TO FS 47 AT Y-765 IAW AIRBUS 320 SRM 53-31-15 FIG 101.

Part: FITTING — CORRODED (R1 DOOR) · airframe 52,979 hrs · 23,723 cycles

SAL - DURING C6 CHECK DISCOVERED CORROSION ON THE R1 SLIDE SUPPORT STRUCTURE FITTING BETWEEN BEAM 2 AND 3 AT FS 16 AND Y-1292. MAINTENANCE REMOVED AND REPLACED THE R1 SLIDE SUPPORT STRUCTURE FITTING BETWEEN BEAM 2 AND BEAM 3 AT FS 16 AND Y-1292 IAW AIRBUS 320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,979 hrs · 23,723 cycles

SAL - DURING C6 CHECK DISCOVERED CORROSION ON PASSENGER SEAT TRACK AT Y-765 AND FR 39+1". CORROSION WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK SECTION FROM FS 36 TO FS 41 AT Y-765 IAW AIRBUS 320 SRM 53-31-15 FIG 101.

Part: FITTING — CORRODED (R1 DOOR) · airframe 52,979 hrs · 23,723 cycles

SAL - DURING C6 CHECK DISCOVERED CORROSION ON THE L2 SLIDE SUPPORT STRUCTURE FITTING BETWEEN BEAM 2 AND 3 AT FS 68 AND Y1292. MAINTENANCE REMOVED AND REPLACED THE L2 SLIDE SUPPORT STRUCTURE FITTING BETWEEN BEAM 2 AND BEAM 3 AT FS 68 AND Y1292 IAW AIRBUS 320 SRM 51-72-11.

Part: FITTING — CORRODED (L1 DOOR) · airframe 52,979 hrs · 23,723 cycles

SAL - DURING C6 CHECK DISCOVERED CORROSION ON STRUCTURE FITTING OF L1 SLIDE SUPPORT. MAINTENANCE REMOVED AND REPLACED THE L1 SLIDE SUPPORT FITTING IAW AIRBUS 320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,979 hrs · 23,723 cycles

SAL - DURING C6 CHECK DISCOVERED CORROSION ON SEAT TRACK AT Y765 AND FS 39+1" IN THE PASSENGER CABIN. CORROSION WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK FROM FS 36 TO FS 41 IN THE PAX CABIN AT Y765 IAW AIRBUS 320 SRM 51-72-11 PAGE 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,979 hrs · 23,723 cycles

MCN - DURING C6 CHECK DISCOVERED CORROSION ON SEAT TRACK AT Y765 AND FS 41+10" IN THE PASSENGER CABIN. CORROSION WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK SECTION FROM FS 41 TO FS 47 AT Y765 IAW AIRBUS 320 SRM 51-72-11..

Part: PLATE — CORRODED (FUSELAGE) · airframe 52,979 hrs · 23,723 cycles

SAL - MAJOR REPAIR - DURING C6 CHECK DISCOVERED CORROSION ON AFT CARGO COMPARTMENT FLOOR STRUCTURE IN PLATE AT FR52A AND Y-600. NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE SRM. MAINTENANCE REMOVED AND FABRICATED PLATE WAS INSTALLED IAW DRAWING D53974806 AND AIRBUS 320 SRM 51-72-11 AND SRM 51-42-11.

Part: SILL — CORRODED (FUSELAGE) · airframe 52,979 hrs · 23,723 cycles

SAL - MAJOR REPAIR - DURING C6 CHECK DISCOVERED CORROSION ON CENTER FITTING OF THE R2 LOWER SILL. MAINTENANCE REMOVED AND REPLACED SHAPE SILL IAW AIRBUS 320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,979 hrs · 23,723 cycles

MCN - DURING C6 CHECK DISCOVERED CORROSION ON SEAT TRACK AT Y-1292 AND FS 39+2" IN THE PASSENGER CABIN. CORROSION WAS REMOVED AND REWORK WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK SECTION AT Y-1292 AND FROM FS 36 TO FS 41 IAW AIRBUS 320 SRM 51-72-11.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,979 hrs · 23,723 cycles

SAL - MAJOR REPAIR - DURING C6 CHECK DISCOVERED CORROSION LOCATED ON FUSELAGE SKIN UNDER SCUFF PLATE AREA AT THE L2 DOOR, STR 23L, Y1340 AND FR 65+5 INCHES TO FR 65+5.5 INCHES. NO ALLOWABLE LIMITS IN THE SRM. MAINTENANCE REWORKED AREA ON FUSELAGE SKIN UNDER THE SCUFF PLATE AT THE L2 DOOR FROM FR 65+5 INCHES TO FR 65+5.5 INCHES AT STR 23L AND Y1340 IAW AMERICA WEST AIRLINES ENGINEERING REPAIR 26-5341-06151-SS1.

Part: FITTING — CORRODED (FUSELAGE) · airframe 52,979 hrs · 23,723 cycles

SAL - MAJOR REPAIR - DURING C6 CHECK DISCOVERED CORROSION ON CENTER FITTING OF THE L2 LOWER SILL FROM FR66 TO FR 68 AT Y1390. MAINTENANCE REMOVED AND REPLACED THE CENTER FITTING OF THE L2 DOOR LOWER SILL FROM FR66 TO FR68 AT Y1390 IAW AIRBUS 320 SRM 51-42-11 AND SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,979 hrs · 23,723 cycles

SAL - DURING C6 CHECK DISCOVERED CORROSION ON SEAT TRACK AT Y1292 AND FS 45 + 16" IN THE PASSENGER CABIN. CORROSION WAS REMOVED AND REWORK WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK SECTION AT Y1292 AND FROM FS 41 TO FS 47 IAW AIRBUS 320 SRM 51-72-11.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,979 hrs · 23,723 cycles

SAL - MAJOR REPAIR - DURING C6 CHECK DISCOVERED CORROSION LOCATED ON FUSELAGE SKIN UNDER SCUFF PLATE AREA AT THE L2 DOOR, STR 23L, Y1340 FR 67+17 TO FR 68. NO ALLOWABLE LIMITS IN THE SRM. MAINTENANCE REWORKED AREA ON FUSELAGE SKIN UNDER THE SCUFF PLATE AT THE L2 DOOR FROM FR 67+17 INCHES TO FR 68 AT STR 23L AND Y1340 IAW AMERICA WEST AIRLINES ENGINEERING REPAIR 26-5341-06151-SS1.

Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 52,979 hrs · 23,723 cycles

SAL - MAJOR REPAIR - DURING C6 CHECK DISCOVERED CORROSION ON EXISTING REWORKED AREA AT FR 25 TO FR 26 AND STR 41R TO STR 42R. CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS. MAINTENANCE CUT OUT DAMAGED AREA IAW AIRBUS 320 SRM 53-00-11. INSTALLED FABRICATED DOUBLER AND FILLER AT FR 25 TO FR 26 AND STR 41R TO STR 42R IAW AIRBUS 320 SRM 53-00-11 FIG 212.

Part: SUPPORT FITTING — CORRODED (R2 DOOR) · airframe 52,979 hrs · 23,723 cycles

SAL - MAJOR REPAIR - DURING C6 CHECK DISCOVERED CORROSION ON THE R2 SLIDE SUPPORT STRUCTURE FITTING BETWEEN BEAM 2 AND 3 AT FR 68 AND Y-1292. MAINTENANCE REMOVED AND REPLACED THE R2 SLIDE SUPPORT STRUCTURE FITTING BETWEEN BEAM 2 AND BEAM 3 AT FR 68 AND Y-1292 IAW AIRBUS 320 SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FWD CARGO BAY) · airframe 52,979 hrs · 23,723 cycles

SAL - MAJOR REPAIR - DURING C6 CHECK DISCOVERED FLOOR PANEL 131FF IN THE FWD CARGO COMPARTMENT, DOUBLER DISBONDED AND FLOOR PANEL DELAMINATED. MAINTENANCE REMOVED AND INSTALLED FABRICATED FLOOR PANEL 131 FF IAW IRM 9701 REV F AND AWA ER 26-5326-05209-RC1C.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,979 hrs · 23,723 cycles

SAL - MAJOR REPAIR - DURING C6 CHECK DISCOVERED CORROSION ON SEAT TRACK AT Y-1292 AND FR 45+18 INCHES. CORROSION WAS REMOVED AND REWORK AREA WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 103 SECTION 3. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK SECTION FROM FR 41 TO FR 47 AT Y-1292 IAW AIRBUS 320 SRM 51-42-11 AND 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 52,979 hrs · 23,723 cycles

SAL - MAJOR REPAIR - DURING C6 CHECK DISCOVERED FLOOR PANEL 261EF WAS DELAMINATED OUT OF LIMITS. MAINTENANCE REMOVED AND INSTALLED REPLACEMENT 261EF FLOORBOARD.

Part: FLOOR PANEL — CRACKED (FWD CARGO BAY) · airframe 52,979 hrs · 23,723 cycles

SAL - MAJOR REPAIR - DURING C6 CHECK DISCOVERED FLOOR PANEL 132GF IN THE FORWARD CARGO COMPARTMENT WAS CRACKED AND DELAMINATED OUT OF LIMITS. MAINTENANCE REMOVED AND INSTALLED FABRICATED 131GF FLOORBOARD IAW IRM 9701 F.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 52,979 hrs · 23,723 cycles

SAL - MAJOR REPAIR - DURING C6 CHECK DISCOVERED FLOOR PANEL 151BF IN THE AFT CARGO COMPARTMENT, DOUBLER DISBONDED AND FLOOR PANEL DELAMINATED. MAINTENANCE REMOVED AND INSTALLED FABRICATED FLOOR PANEL 151BF IAW IRM 9701 REV F AND AWA ER 26-5326-05209-RC1C.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,900 hrs · 23,689 cycles

CMH - EEL - LOG 7314800 - MAINTENANCE REPORTED THAT THE "A/C LEFT RED OVER WING EPL AND SIDEWALL EMERG EXIT LTS INOP". MAINTENANCE REMOVED AND REPLACED THE RT OVERWING EMERGENCY POWER SUPPLY UNIT IAW AIRBUS 320 AMM 33-51-38. OPERATIONAL CHECKS WERE GOOD.

Part: POWER SUPPLY — MALFUNCTIONED (NLG) · airframe 52,207 hrs · 23,398 cycles

DURING DESCENT RECEIVED BRAKE ANTI-SKID NWS FAULT. TRIED TO CYCLE ANTI-SKID & NW STEERING SWITCH WITH NO HELP. DECLARED EMERGENCY LANDING. ON GROUND, CYCLED CIRCUIT BREAKERS. RECEIVED STEERING BACK. MX REPLACED BSCU, NO HELP. BSCU CHANNEL 1 DEFERRED. ORIGINAL BSCU REINSTALLED. BSCU REPLACED & DEFERRAL CLEARED. MX REPLACED NLG ELECTRICAL BOX IAW MM 32-51-12-401. OPS CHKS GOOD. CONFIRMED FAULT OF BSCU WITH A HARD FAILURE OF THE SYSTEM 2 POWER SUPPLY. CONFIRMED FAULT ON NLG BOX.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 51,411 hrs · 23,070 cycles

EEL - CREW REPORTED THAT THE FORWARD FLIGHT ATTENDANT FLASHLIGHT BATTERY IS DEAD. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT BATTERY. OPERATIONAL CHECKS WERE GOOD.

Part: ACCESS DOOR — CORRODED (RT WING)

RT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT PANEL 650 GB WING STA 274.319 HAS MINOR CORROSION .006 INCH DEEP AND 2 INCH LONG. MAINTENANCE REMOVED MINOR CORROSION IAW REO. MATERIAL REMOVED WAS LESS THAN .010 INCH IAW REINSPECT IS DUE OF HOLE NR 14 AT 38602 FLIGHT CYCLES.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 50,141 hrs · 22,556 cycles

LAS - EEL - DURING 8 DAY CHECK DISCOVERED ROW 17 SEAT MOUNTED EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT ROW 17. OPERATIONAL CHECKS WERE GOOD IAW TASK CARD F1C33301.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 50,141 hrs · 22,556 cycles

LAS - EEL - DURING 8 DAY CHECK, DISCOVERED ROW 12 SEAT MOUNTED EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT ROW 12. OPERATIONAL CHECKS WERE GOOD IAW TASK CARD F1C33301.

Part: BATTERY — DISCHARGED (CABIN) · airframe 49,613 hrs · 22,312 cycles

DURING 4-DAY CHECK, FOUND RIGHT EMERGENCY SUPPLY POWER UNIT HAD LOW BATTERY. MAINTENANCE REMOVED AND REPLACED RIGHT ESPU BATTERY IAW AIRBUS MM 33-51-38-04 STEP 7. OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 49,422 hrs · 22,229 cycles

PHX - EEL - DURING ROUTINE MX ROW 17 ABC EMERGENCY EXIT ESCAPE PATH LIGHTING WAS INOPERATIVE. TERMINALS CONNECTING WIRES TO SEAT ASSEMBLY INOPERATIVE. MAINTENANCE RETERMINATED TERMINALS AT ROW 17 A,B,C IAW AMM 20-48-14. OPERATIONAL CHECK WAS GOOD.

Part: LANDING GEAR — INOPERATIVE (NOSE) · airframe 48,558 hrs · 21,891 cycles

AIR TURNBACK, ON CLIMBOUT OF ORD EN ROUTE TO PHX AFTER SELECTING LANDING GEAR TO THE UP POSITION THE NOSE GEAR WOULD NOT RETRACT, TURNED BACK TO ORD FOR REPAIR. AIRCRAFT CURRENTLY OUT OF SERVICE. MAINTENANCE REPACKED NLG SHOCK STRUT IAW T/C R4N32305, ALSO REPLACED NLG DOWNLOCK SPRING AND LOWER LOCK SPRING ATTACH PIN PER AMM 32-21-18, LEAK AND OPERATIONAL CHECKS WERE GOOD.

Part: PROXIMITY SENSOR — INTERMITTENT (NLG) · airframe 47,852 hrs · 21,591 cycles

DTW - EMERGENCY LANDING - FLT 0096 - WHILE PREPARING FOR LANDING AT DTW EN ROUTE FROM LAS AFTER LANDING GEAR WAS LOWERED RECEIVED A LANDING GEAR SYSTEM DISAGREE MESSAGE WITH LANDING GEAR CONTROL INTERFACE UNIT NR 2 INDICATING THE NOSE GEAR WAS UNSAFE. ABORTED APPROACH AND FLEW BY TOWER TO VERIFY GEAR WAS DOWN. DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER DIFFICULTY. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR DOWNLOCK PROXIMITY SENSOR 19GA IAW AMM 32-31-73-04, OPERATIONAL TEST WAS GOOD.

Part: FILTER — CLOGGED (NR 2 ENGINE) · airframe 47,449 hrs · 21,424 cycles

ON TAKEOFF AT LAS EN ROUTE TO PHX, WHEN TAKEOFF POWER WAS APPLIED RECEIVED NR 2 ENGINE OIL FILTER CLOG MESSAGE ON ECAM, OIL PRESSURE WAS VERY HIGH, REJECTED TAKEOFF LESS THAN 40 KTS. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE OIL SCAVENGE FILTER IAW AMM 79-22-44-000-010, ENGINE RUN OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (ZONE 221) · airframe 46,885 hrs · 21,187 cycles

CMH - EEL - DURING 8-DAY CHECK THE LEFT FORWARD EMERGENCY LIGHT BATTERY PACK FAULTED. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE LEFT FORWARD EMERGENCY POWER SUPPLY UNIT 10WL, OPERATIONAL CHECK WAS GOOD.

Part: BEARING — FAILED (ZONE 128) · airframe 46,871 hrs · 21,181 cycles

EN ROUTE FROM PHX TO MCO, SMELLED A BURNING ELECTRICAL ODOR WITH VISIBLE SMOKE IN COCKPIT, WHILE DIVERTING TO DFW APPROXIMATELY 2 MILES LATER VENT EXTRACT FAULT LIGHT ILLUMINATED. MAINTENANCE PLACED SYSTEM ON MEL AND DEACTIVATED EXTRACT FAN. UPON ARRIVAL AT FIRST MAINTENANCE STATION, REPLACED AVIONICS COOLING (EXTRACT) FAN IAW AMM 21-26-51-04, OPERATIONAL CHECK WAS GOOD. SUPP - VENDOR CONFIRMED FAILURE OF AVIONICS COOLING FAN S/N 675, UNIT SEIZED, COULD NOT PERFORM INCOMING FUNCTIONAL CHECK. FOUND THE FRONT BEARING BROKEN, REAR BEARING LOOSE AND WORN, AND FRONT FLANGE CENTER HOLE WORN. REPLACED DEFECTIVE PARTS AND PERFORMED FUNCTIONAL TEST IAW CMM 21-26-42, REV 6.

Part: ACM — MALFUNCTIONED (ZONE 190) · airframe 45,928 hrs · 20,804 cycles

AIR TURN BACK ON CLIMB OUT, RECEIVED ECAM MESSAGE FOR PACK 1, NR 2 FAULT WITH ASSOC PACK 2 OVERHEAT. PASSING THROUGH FL 250 ECAM DIRECTED NR 2 PACK BE TURNED OFF, NR 1 PACK ALREADY ON MEL, AS A/C DESCENDED BELOW 10000 FT, NR 2 PACK TURNED OFF & OVERHEAT CONDITION CLEARED, TURNED NR 2 PACK BACK ON & SYS WORKED OK FOR REMAINDER OF FLT, BUT NR 2 PACK TEMP REMAINED HOT. MAINT TROUBLESHOT AC PACKS 1, 2, PREFLT REPORT INDICATED PACK 2 BYPASS VALVE & OUTLET TEMP SENSOR (35HH). R & R PACK 2 OUTLET TEMP SENSOR (35HH) IAW AMM, & BYPASS VALVE, LEAK & OPS CHECK GOOD. REPLACED FLOW CNTRL VALVE FOR PACK NR 1, PROBLEM STILL EXISTS, SYS REMAINS ON MEL. TEARDOWN ANALYSIS OF AIR CYCLE MACHINE S/N 01404 CONFIRMED FAILURE OF UNIT.

Part: ODOR — DETECTED (GALLEY) · airframe 45,058 hrs · 20,437 cycles

MSP - DIVERSION - FLT 0232 - APPROXIMATELY 45 MINUTES AFTER TAKEOFF FROM DTW, EN ROUTE FOR LAS, THE FLIGHT ATTENDANTS REPORTED A STRONG ODOR OF GAS OR SULFUR IN THE AFT GALLEY, DIVERTED TO MSP. WHEN MAINTENANCE ARRIVED, FOUND NO ODOR IN AFT GALLEY. THE MSP FIRE DEPARTMENT GAS ANALYZER WAS USED TO DETECT ANY EVIDENCE OF GAS, ANALYZER READ -0-. AFT GALLEY OVENS AND COFFEEMAKERS WERE OPERATED, NO SULFUR ODOR WAS NOTED, RAN BOTH ENGINES AND OPERATED AIR CONDITIONING PACKS, NO ODOR WAS NOTED.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 44,617 hrs · 20,255 cycles

LAS - EEL - DURING 8-DAY CHECK LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL) CAUSES CIDS FAULT. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD.

Part: WIRE — BROKEN (SEAT ROW 11 LT) · airframe 44,341 hrs · 20,141 cycles

DURING 4-DAY CHECK FOUND EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 11 LT, OPERATIONAL CHECK WAS GOOD.

Part: COMPUTER — INTERMITTENT (ZONE 120)

ON TAKEOFF OUT OF SJC EN ROUTE FOR PHX AT 75 FT WITH GEAR RAISED, RECEIVED GEAR NOT DOWN WARNING & BELL & AIRCRAFT WAS NOT PRESSURIZING, ALSO HAD NO FLIGHT DIRECTOR, AUTOPILOT OR AUTOTHRUST. AT 400 FT RECYCLED LANDING GEAR & ALL SYSTEMS RETURNED TO NORMAL, ACARS NEVER LOGGED OFF TIME. MAINTENANCE REMOVED AND REPLACED NR 1 & 2 FLIGHT WARNING COMPUTERS IAW T/C R2A31303, OPERATIONAL CHECK WAS GOOD. VENDOR FUNCTIONAL TEST OF FLIGHT WARNING COMPUTERS S/N'S 317 & 1262 WERE BOTH NO FAULT FOUND. BOTH UNITS WERE TEST AND RETURNED TO SERVICE IAW CMM 31-53-34, REV 14.

Part: LINE — CHAFED (AFT SPAR) · airframe 42,893 hrs · 19,569 cycles

ON DECENT, EN ROUTE RECEIVED ECAM MESSAGE GREEN HYDRAULIC SYSTEM LOW QUANTITY; DECLARED EMERGENCY, NO NOSE WHEEL STEERING, AIRCRAFT TOWED OFF RUNWAY. MAINTENANCE FOUND GREEN SYSTEM HYDRAULIC PRESSURE LINE CHAFED AND LEAKING IN LT WHEEL WELL ON AFT SPAR BETWEEN RIBS 2 AND 5. PERFORMED REPAIR IAW AMM 20-23-11, PG. 201, LEAK CHECK WAS GOOD.

Part: SLIDE — TORN (R-2 DOOR) · airframe 42,485 hrs · 19,403 cycles

DURING C-04 CHECK FOUND THE R-2 DOOR SLIDE LACING TORN. MAINTENANCE REMOVED AND REPLACED THE R-2 DOOR SLIDE IAW T/C R1C25304MT-82.

Part: SPLICE — BROKEN (SEAT ROW 9) · airframe 42,485 hrs · 19,403 cycles

MCN - EEL - DURING C-04 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 RT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED SPLICES ON WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 9 RT, OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — FAULTY (ZONE 241) · airframe 42,485 hrs · 19,403 cycles

DURING C-04 CHECK THE LT OVERWING EMERGENCY POWER SUPPLY UNIT INDICATED A FAULT. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL) AND BATTERY PACK IAW AMM TASKS 33-51-38-000-001 AND 33-51-38-400-001, OPERATIONAL CHECK WAS GOOD.

Part: DAMPER — SHEARED (PAX DOOR) · airframe 42,485 hrs · 19,403 cycles

MCN - EES - DURING C-04 CHECK THE R-1 DOOR DAMPER CYLINDER KNURLED KNOB WAS FOUND SHEARED. MAINTENANCE REMOVED AND REPLACED THE R-1 DOOR DAMPER CYLINDER IAW AMM TASK 52-11-14-000-001, 52-11-14-400-001, AND 52-11-14-04 FIG 401 & 402, SHT 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,485 hrs · 19,403 cycles

DURING C-04 EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y1292 RT, FORWARD FO FR 67. MAINTENANCE REMOVED FLOORBEAM BETWEEN FR 66 AND FR 68, FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 6 AND 7.

Part: PROFILE — CRACKED (FUSELAGE) · airframe 42,485 hrs · 19,403 cycles

DURING C-04 CHECK A .25 INCH CRACK WAS FOUND ON FORWARD CARGO COMPARTMENT FLOOR SUPPORT SPLICE AT FR 31, RBL 28. MAINTENANCE REMOVED DAMAGED SECTION OF PROFILE AT FR 31, RBL 28; FABRICATED A NEW REPLACEMENT SECTION OF PROFILE, AND SPLICE REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW AWA ER 26-5320-03154-SS1.

Part: PROFILE — CORRODED (CARGO BAY) · airframe 42,485 hrs · 19,403 cycles

DURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT CORNER PROFILE FR 59-60, RBL 686 MM. MAINTENANCE REMOVED DAMAGED AFT CARGO COMPARTMENT CORNER PROFILE FR 59-60, RBL 686MM, FABRICATED A NEW REPLACEMENT PROFILE; INSTALLED REPAIR PART IAW AWA E.R. 26-5341-03142-TB5.

Part: PROFILE — CORRODED (FUSELAGE) · airframe 42,485 hrs · 19,403 cycles

DURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT CORNER PROFILE FR 56-58, LBL 686MM. MAINTENANCE CUT OUT DAMAGED AREA OF AFT CARGO COMPARTMENT CORNER PROFILE FR 56-58, LBL 686MM; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW AWA ER 26-5341-03142-TB5.

Part: PROFILE — CORRODED (CARGO BAY) · airframe 42,485 hrs · 19,403 cycles

DURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT CORNER PROFILE FR 56-58, RBL 686 MM. MAINTENANCE CUTOUT DAMAGED SECTION OF AFT CARGO COMPARTMENT CORNER PROFILE FR 56-58, RBL 686 MM; FABRICATED 2 EACH FILLERS AND DOUBLERS; INSTALLED REPAIR PARTS IAW AWA E.R. 26-05341-03142-TB5.

Part: PROFILE — CORRODED (CARGO BAY) · airframe 42,485 hrs · 19,403 cycles

DURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT FLOOR PROFILE FR 59, LBL 660 MM TO RBL 660 MM. MAINTENANCE REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR PROFILE FR 59, LBL 660MM TO RBL 660MM IAW AWA E.R. 26-5341-03142-TB5.

Part: PROFILE — CORRODED (CARGO BAY) · airframe 42,485 hrs · 19,403 cycles

DURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT CENTER FLOOR PROFILE FR 50, STR 38 LT. MAINTENANCE CUTOUT DAMAGED SECTION OF AFT CARGO COMPARTMENT CENTER PROFILE FR 50, STR 38 LT; FABRICATED A NEW REPLACEMENT SECTION OF PROFILE AND 2 EACH SPLICE DOUBLERS; INSTALLED REPAIR PARTS IAW AWA E.R. 26-05341-03142-TB5.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,485 hrs · 19,403 cycles

DURING C-04 CHECK AFTER FIRST OVERSIZE OF FASTENER HOLE COMMON TO SKIN A 1/8 INCH CRACK WAS FOUND ON FRAME 41, THIRD FASTENER HOLE BELOW STR 14 LT. MAINTENANCE REAMED OUT HOLE TO SECOND OVERSIZE AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; CUTOUT DAMAGED SECTION OF FRAME 41 AT THIRD FASTENER HOLE BELOW STR 14 LT; FABRICATED A REPAIR ANGLE AND FRAME FILLER; INSTALLED REPAIR PARTS IAW E.O. 53-14-20.

Part: PROFILE — CORRODED (CARGO BAY) · airframe 42,485 hrs · 19,403 cycles

DURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT FLOOR PROFILE FR 58, LBL 660MM TO RBL 660MM. MAINTENANCE REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR PROFILE FR 58, LBL 660MM TO RBL 660MM IAW AWA E.R. 26-5341-03142-TB5.

Part: PROFILE — CORRODED · airframe 42,485 hrs · 19,403 cycles

MCN - MINOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT CENTER FLOOR PROFILE STR 38 LT TO STR 38 RT, FR-50. MAINTENANCE REMOVED CENTER FLOOR PROFILE FROM STR 38 LT TO STR 38 RT, FR-50; FABRICATED A NEW REPLACEMENT CENTER FLOOR PROFILE; INSTALLED REPAIR PART IAW AWA ER 26-5341-03142-TB5.

Part: STRUCTURE — CORRODED (CARGO BAY) · airframe 42,485 hrs · 19,403 cycles

DURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT CORNER PROFILE FR 58 - 59, LBL 686 MM. MAINTENANCE REMOVED AND REPLACED AFT CARGO COMPARTMENT CORNER PROFILE FR 58-59, LBL 686 MM IAW A320 SRM 53-41-14, FIG. 24, PG. B31-B32.

Part: PROFILE — CORRODED (CARGO BAY) · airframe 42,485 hrs · 19,403 cycles

DURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT CENTER FLOOR PROFILE FR 53, STR 38 L/H TO STR 38 R/H. MAINTENANCE REMOVED AND REPLACED AFT CARGO COMPARTMENT CENTER FLOOR PROFILE FR 53, STR 38 L/H TO STR 38 R/H IAW A320 SRM 53-41-14, PG. B22.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 42,485 hrs · 19,403 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK A .5 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT FLOOR PANEL SUPPORT AT FR 63, LBL 406MM. MAINTENANCE REMOVED DAMAGED FLOOR PANEL SUPPORT AT FR 63, LBL 406MM; FABRICATED A NEW REPLACEMENT FLOOR PANEL SUPPORT; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 8-12 & 22 FIG 2, 3 & 8.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,485 hrs · 19,403 cycles

DURING C-04 CHECK AFTER FIRST OVERSIZE OF FASTENER HOLE COMMON TO SKIN 2 EACH 1/8 INCH CRACKS WERE FOUND ON FRAME 39, THIRD FASTENER HOLE BELOW STR 14 L/H. MAINTENANCE REAMED OUT HOLE TO SECOND OVERSIZE AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; CUTOUT DAMAGED SECTION OF FRAME 39 AT THIRD FASTENER HOLE BELOW STR 14 L/H; FABRICATED A REPAIR ANGLE AND FRAME FILLER; INSTALLED REPAIR PARTS IAW E.O. 53-14-20.

Part: PROFILE — CORRODED (CARGO BAY) · airframe 42,485 hrs · 19,403 cycles

MCN - MINOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CARGO COMPARTMENT CORNER PROFILE FR 59-61, LBL 686MM. MAINTENANCE CUTOUT DAMAGED SECTION OF AFT CARGO COMPARTMENT CORNER PROFILE FR 59-61, LBL 686MM; FABRICATED A NEW REPLACEMENT SECTION OF PROFILE AND A SPLICE DOUBLER; INSTALLED REPAIR PARTS IAW AWA E.R. 26-05341-03142-TB5.

Part: FITTING — ARCED (WING) · airframe 42,485 hrs · 19,403 cycles

DURING C-04 CHECK A HOLE WAS FOUND BURNT INTO THE INBOARD EDGE OF NR 2 PYLON TO WING ATTACH FITTING, ARCING CAUSED FROM NR 2 IDG FEEDER CABLE. MAINTENANCE REMOVED SPIGOT FITTING AND FORWARD INBOARD PYLON ATTACH FITTING; FABRICATED A NEW REPLACEMENT INBOARD PYLON ATTACH FITTING; INSTALLED SPIGOT FITTING AND FORWARD INBOARD PYLON ATTACH FITTING IAW AWA ER 26-5716-03163-ES1.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,485 hrs · 19,403 cycles

DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON CORNER FITTING AT AFT LOWER CORNER OF FORWARD CARGO DOOR CUTOUT. MAINTENANCE REMOVED DAMAGED CORNER FITTING AT AFT LOWER CORNER OF FORWARD CARGO DOOR CUTOUT; FABRICATED A NEW REPLACEMENT FITTING; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 2-7 PG 7-22 & FIG 9-18 PG 23-36.

Part: ANGLE — CORRODED (DOOR CUTOUT) · corrosion level 2 · airframe 42,485 hrs · 19,403 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SPLICE ANGLE AT AFT LOWER CORNER OF THE FORWARD CARGO DOOR CUTOUT, FR-28. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SPLICE ANGLE AT AFT LOWER CORNER OF THE FORWARD CARGO DOOR CUTOUT, FR-28; FABRICATED A NEW REPLACEMENT SPLICE ANGLE PER DWG C2D53231388; INSTALLED REPAIR PART IAW AWA ER 26-5323-03141-SS2.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 42,485 hrs · 19,403 cycles

MCN - MINOR REPAIR - DURING C-04 CHECK A .4375 INCH CRACK WAS FOUND ON FORWARD CARGO COMPARTMENT FLOOR SUPPORT AT FR 28, LBL 28. MAINTENANCE CUT OUT DAMAGED SECTION OF FLOOR SUPPORT AT FR 28, LBL 28; FABRICATED A NEW REPLACEMENT SECTION OF FLOOR SUPPORT AND SPLICE REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW AWA ER 26-5320-03154-SS1.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 42,485 hrs · 19,403 cycles

DURING C-04 CHECK 4 EACH CRACKS WERE FOUND AT RIVET HOLES ON FORWARD CARGO COMPARTMENT CEILING PANEL SUPPORT, AFT BULKHEAD FR 34, RBL 10 & 28, LBL 10 & 28. MAINTENANCE ROUTED OUT HOLES; FABRICATED ANGLE DOUBLERS AND FILLERS; INSTALLED REPAIR PARTS IAW AWA E.R. 26-5327-02143-JS1.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 42,485 hrs · 19,403 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK A 1.5 INCH CRACK WAS FOUND ON FORWARD CARGO COMPARTMENT FLOOR SUPPORT AT FR 28, RBL 11. MAINTENANCE REMOVED DAMAGED FLOOR SUPPORT AT FR 28, RBL 11; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PART IAW A320 SRM 51-44-21, TABLE 3, PG 5.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 42,485 hrs · 19,403 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK A 1.5 INCH CRACK WAS FOUND IN CENTER OF FLOOR PANEL 261NF. MAINTENANCE PERFORMED COMPOSITE REPAIR OF CRACK IN CENTER OF FLOOR PANEL 261NF IAW A320 SRM 53-02-00 PG 203-207 FIG 202.

Part: ANGLE — CRACKED (FAIRING SUPPORT) · airframe 42,285 hrs · 19,403 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK A .5 INCH CRACK WAS FOUND ON ATTACH ANGLE AT FR 34 ON FAIRING SUPPORT STRUCTURE AT AFT UPPER EDGE OF PANEL 192AB. MAINTENANCE REMOVED DAMAGED ATTACH ANGLE AT FR-34; FABRICATED A NEW REPLACEMENT ATTACH ANGLE; INSTALLED REPAIR PART IAW AWA ER 26-5323-03129-TB1.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,485 hrs · 19,403 cycles

DURING C-04 CHECK A 3 INCH CRACK WAS FOUND ON ATTACH ANGLE AT FR 34 ON SUPPORT STRUCTURE AT AFT UPPER EDGE OF PANEL 191AB. MAINTENANCE REMOVED CRACKED ATTACH ANGLE AT FR 34; FABRICATED A NEW REPLACEMENT ATTACH ANGLE; INSTALLED REPAIR PART IAW AWA E.R. 26-5323-03128-TB1.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 42,485 hrs · 19,403 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK A 1 INCH CRACK WAS FOUND AT FASTENER HOLE ON FLOOR SUPPORT Y1292, FR 18. MAINTENANCE CUTOUT DAMAGED AREA ON FLOOR SUPPORT Y1292, AT FR 18; FABRICATED 2 EACH REPAIR ANGLES AND A FILLER; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14 PG 201-210 FIG 201, SRM 51-21-11 PG 5-7, SRM 51-23-11 PG 20 AND SRM 51-42-11 PG 8-12 FIG 2-3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,485 hrs · 19,403 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON THE UPPER SURFACE OF FLOORBEAM Y179 AT FR 20. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED FLOORBEAM; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 53-11-14 FIG 202, PG 211-212.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,485 hrs · 19,403 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y1292, AT AFT SIDE OF FR 66 TO FORWARD SIDE OF FR 68. MAINTENANCE REMOVED DAMAGED FLOORBEAM Y1292, FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 6-7, SRM 51-76-11 PG 9-10 FIG 4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,485 hrs · 19,403 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y1292, FORWARD OF FR 66. MAINTENANCE REMOVED DAMAGED FLOORBEAM Y1292, FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 6-7, SRM 51-76-11 PG 9-10 FIG 4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,485 hrs · 19,403 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y1292, AT FR 68. MAINTENANCE REMOVED DAMAGED FLOORBEAM Y1292, FROM FR 68 TO FR 70; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 6-7, SRM 51-76-11 PG 9-10, FIG 4.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,485 hrs · 19,403 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM Y254, FR-16 -17, RBL 254MM. UPON FURTHER INSPECTION A .625 INCH CRACK WAS FOUND IN SAME LOCATION; MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM Y254, FR-16 -17, RBL 254MM; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM AND 4 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14 PG 211-212 FIG 202.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,485 hrs · 19,403 cycles

DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT Y254, FR 16 TO FR 20. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED FLOOR SUPPORT Y254, FR 16 TO FR 20; FABRICATED 4 EACH REPAIR ANGLES, AND A NEW REPLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14 PG 211-212, FIG 202.

Part: SKIN — CORRODED (FUSELAGE) · airframe 43,090 hrs · 19,603 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON EXTERNAL SKIN BETWEEN FRAMES 60 AND 61, AT BL 0, UNDER ANTENNA CUTOUT. MAINTENANCE CUT OUT CORROSION ON EXTERNAL SKIN BETWEEN FRAMES 60 AND 61, AT BL 0; FABRICATED A DOUBLER; INSTALLED REPAIR PART IAW A320 SRM 53-00-11 PG 203, 208, 210-212 FIG 203.

Part: SKIN — CORRODED (FUSELAGE) · airframe 43,090 hrs · 19,403 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON EXTERNAL SKIN BETWEEN FRAMES 62 AND 63, STR 42-43 LT, UNDER IFPC ANTENNA. MAINTENANCE CUT OUT CORROSION ON EXTERNAL SKIN BETWEEN FRAMES 62 AND 63, STR 42-43 LT, UNDER IFPC ANTENNA; FABRICATED A DOUBLER; INSTALLED REPAIR PART IAW A320 SRM 53-00-11 PG 203, 209-214 FIG 203.

Part: ROD — OUT OF ADJUST (R-1 DOOR) · airframe 42,793 hrs · 19,531 cycles

MCN - EES - DURING C-04 CHECK THE R-1 DOOR PLUNGER TO STRIKE LEVER CLEARANCE WAS FOUND OUT OF LIMITS BETWEEN DIMENSIONS A (J) AND B (J2). MAINTENANCE ADJUSTED THE R-1 DOOR PLUNGER TO STRIKE LEVER CLEARANCE IAW AMM TASK 52-11-14-820-002, SUB TASK 52-11-14-820-052, AND FIG 501, SHT 1.

Part: PLATE — CRACKED (FRAME) · airframe 42,485 hrs · 19,403 cycles

DURING C-04 CHECK 2 EACH .5000 INCH CRACKS WERE FOUND ON AFT CARGO COMPARTMENT FORWARD BULKHEAD, LT UPPER CORNER FRAME PLATE. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED, FABRICATED A REPAIR DOUBLER AND SHIMS; INSTALLED REPAIR PARTS IAW AWA E.R. 26-5314-00011-JS4.

Part: OUTFLOW VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 39,405 hrs · 18,205 cycles

PHX - AIR TURNBACK - FLT 0239 - AFTER TAKEOFF FROM PHX EN ROUTE TO DTW SKIN AIR VALVE FAULTED WITH AVIONICS VENT ALREADY ON MEL 21-26-02 AND EXTRACT FAN OVERRIDE. ECAM INDICATED MAXIMUM ALTITUDE 10,000 MEA, TURNED BACK TO PHX. MAINTENANCE REMOVED AND REPLACED SKIN AIR VALVE IAW AMM 21-26-53-401; SKIN AIR VALVE WAS INSTALLED ONLY ONE FLIGHT EARLIER. MAINTENANCE ALSO REPLACED THE AVIONICS COOLING FAN IAW AMM 21-26-51-401, BITE CHECK ON BOTH COMPONENTS WAS GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 5,144 hrs · 1,897 cycles

NON ROUTINE LINE, EMER LIGHTS. AFT LT EMERGENCY LIGHT POWER SUPPLY UNIT BITE CHECKED BAD. REPLACED POWER SUPPLY UNIT M+E = 26-3350-9-0001. RECOMMENDATION: REMAIN OPEN PENDING REVIEW OF TEARDOWN REPORT, NO RELATED HISTORY.

Part: POWER SUPPLY — INTERMITTENT (CABIN) · airframe 32,576 hrs · 15,535 cycles

EXIT LIGHTS AT DOOR L-2 AND R-2 INTERMITTENT. REPLACED POWER SUPPLY, OPS CHECK GOOD.

Part: WIRE — BROKEN (CABIN)

AISLE EMERGENCY LIGHT INOP AT SEAT ROW 1 LT. REPAIRED BROKEN WIRE.

Part: ADC — MALFUNCTIONED (E/E BAY)

ON TAKEOFF ROLL AT APPROX 80 KNOTS, RECEIVED SPD LIM WARNING ON ECAM. TAKEOFF REJECTED. REPLACED NR 2 AIR DATA (IRU) TT 0096655. CURRENT HISTORY: NR 2 IRU WAS REPLACED 10/11/99 FOR SIMILAR PROBLEM BOTH TIMES IT WAS ASSOCIATED WITH TAT PROBE HEAT ON.

Part: LGCIU — FAULTED (NR 1 / 2)

WHEN LANDING GEAR WAS LOWERED, LGCIU 1 AND 2 BOTH FAULTED. EXECUTED MISSED APPROACH AND RESET LGCIU 1 CB AT C9 AND LGCIU 2 CB AT Q35. BOTH SYSTEMS RESET AND OPERATED NORMALLY. PERFORMED CFDS SYSTEM TEST ON LGCIU 1 AND 2, TEST OK.

Part: CONTROL CABLE — WORN (LT AILERON)

LEFT AILERON INTERCONNECT OB CABLE IS WORN THROUGH ALUMINUM CLAD. REMOVED AND REPLACED LEFT OUTBOARD INTERCONNECT CABLE, TENSIONED AND SAFETIED. GEN W/C FOR FUNCTIONAL TEST 5067.

Part: WIRE — DISCONNECTED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT AT ROW 22 INOP. REPAIRED DAMAGED WIRE UNDER ROW 22 EMERGENCY LIGHT. OPS CHECK GOOD.

Part: WIRE — DISCONNECTED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT AT ROW 22 L INOP. RECONNECTED WIRE AT LIGHT, OPS CHECK GOOD.

Part: CONNECTOR — DISCONNECTED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INOP AT RT WINDOW EXITS. FOUND CANNON PLUG DISCONNECTED FROM BATTERY POWER SUPPLY UNIT. CONNECTED CANNON PLUG, OPS CHECK GOOD.

Part: LIGHT — BROKEN (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT AIRCRAFT RIGHT INOP ABOVE OVERWING EXITS. REMOVED AND REPLACED RIGHT CENTER EMERGENCY EXIT LIGHT POWER SUPPLY AND BATTERY. BATTERY 321430 DISCHARGED RIGHT, CENTER CABIN.

Part: FIRE CONTL PNL — FAILED (COCKPIT)

INFLIGHT SHUTDOWN, DIVERSION TO ABQ. IN CRUISE AT FL370, OBSERVED 'FIRE' INDICATION ON ENGINE CONTROL PANEL AND ON OVERHEAD FIRE PUSH BUTTON BUT NO ECAM INDICATIONS. COMPLETED NR 2 ENGINE SHUTDOWN PROCEDURE. REPLACED FIRE CONTROL PANEL ON OVERHEAD 49VU. PERFORMED OPS CHECK OF ENGINE / APU FIRE PROTECTION SYSTEM, OPS NORMAL AT THIS TIME.

Part: WIRE — BROKEN (CABIN)

PHX - FLT 2541 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT AT SEAT 22L INOP. REPAIRED WIRING AS REQUIRED. OPERATIONS CHECK GOOD. (M)

Part: OIL SCAV PUMP — FAILED (NR 2 ENGINE)

RNO - FLT 2012 - ON ARRIVAL IN RNO AND SHUTDOWN, GROUND CREW REPORTED A TAIL PIPE FIRE IN THE NR 2 ENGINE. AFTER SUBSEQUENT DRY MOTORINGS, GROUND FIRE EXTINGU ISHER WAS USED, THE FIRE WAS PUT OUT. FOUND OIL PUDDLED IN ENGINE CORE TAIL PI PE. REMOVED AND REPLACED NR 2 ENGINE OIL SCAVENGER PUMP PER AWA TASK CARD R5M79301. PERFORMED ENGINE RUN LEAK/CHECK, OPS CHECK NORMAL AT THIS TIME. (M)

Part: BUS BAR — DAMAGED (E/E COMPT)

CMH - FLT 2258 - AIRCRAFT ARRIVED IN CMH WITH NUMEROUS ECAM MESSAGES AND INOP SYSTEMS. AVIONICS COOLING FAN POPPING C/B. DURING TROUBLESHOOTING, FOUND WIRES BURNED AT BUS BAR 2XP-AC BUS 2 (1000XN2). REF WDM 24-51-10. REPAIRED WIRES AND INSTALLED NEW BUS TIE. SYSTEM OPS CHECK NORMAL. (M)

Part: LATCH MECH — OUT OF ADJUST (CARGO DOOR)

CMH - FLT 990 - CMH-LAS - ON CLIMB-OUT, THE DOOR ANNUNCIATOR ECAM MESSAGE APPEARED AT 6000 FEET. AIRCRAFT RETURNED TO CMH LANDING OVERWEIGHT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND AFT CARGO DOOR HANDLE UNLATCHED. MAINTENANCE ADJUSTED HANDLE LINKAGE PER AMM 52-31-11. OPS CHECK GOOD. VERTICAL SPEED WITHIN LIMITS PER AMM 05-51-11. OVERWEIGHT INSPECTION NOT REQUIRED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: EEL BATT PACK — DISCHARGED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, RT CABIN EEL BATTERY FAULTED. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M)

Part: CLAMP — BROKEN (PTU MANIFOLD)

PHX-MSP - DURING CRUISE AT FL 39,000 FEET, CREW SHUT DOWN GREEN SYSTEM HYDRAULIC PUMP DUE TO GREEN HYDRAULIC RESERVOIR LOW QUANTITY MESSAGE. CREW DECLARED AN EMERGENCY LANDING AND MANUALLY EXTENDED GEAR. LANDING WAS UNEVENTFUL. AIRCRAFT WAS TOWED TO GATE WHERE CONTRACT MAINTENANCE ALSO FOUND TWO CLAMPS BROKEN ON THE SAME LINE. MAINTENANCE TIGHTENED FITTING, REPLACED TWO CLAMPS, AND SERVICED GREEN HYDRAULIC SYSTEM. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: EEL WIRING — BROKEN (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 13 INOPERATIVE. REPAIRED SECTION OF BROKEN WIRING BY SEAT FLOOR TRACK, OPS CHECK GOOD. (M)

Part: SUPPORT — CORRODED (CABIN)

PHX - DURING SCHEDULED C4 INSPECTION, FOUND CABIN FLOOR STRUCTURE CORRODED IN SEVERAL AREAS ON TOP SURFACE OF 'I' BEAM UPPER CHORD, FRAME 17 TO FRAME 19 Y 254. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER PER SRM 53-11-14. (M)

Part: CASTING — CRACKED (CARGO DOOR)

PHX - DURING SCHEDULED C4 INSPECTION, FOUND FORWARD CARGO COMPARTMENT DOOR HANDLE CASTING CRACKED AT FORWARD UPPER MOUNT BOLT LUG. REPAIRED PER ER 32-52-30-05. (M)

Part: SUPPORT — CRACKED (CARGO COMPT)

PHX - DURING SCHEDULED C4 INSPECTION, FOUND FORWARD CARGO COMPARTMENT LEFT FLOOR SUPPORT AT FRAME 29 CRACKED AT RIVET. REPAIRED IAW ER 32-53-26-28. (M)

Part: SUPPORT — CORRODED (CABIN)

PHX - DURING SCHEDULED C4 INSPECTION, FOUND CORROSION ON FLOOR BEAM SUPPORT FROM FRAME 16 TO FRAME 20 AT Y 254. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER PER SRM 53-11-14. (M)

Part: SUPPORT — CRACKED (CABIN)

PHX - DURING SCHEDULED C4 INSPECTION, FOUND FLOOR BOARD AFT SUPPORT STRUCTURE AT FR 65 CRACKED AND DEFORMED AT FASTENER HOLE. REPAIRED IAW ER 32-53-26-29. (M)

Part: SUPPORT — CRACKED (CABIN)

PHX - DURING SCHEDULED C4 INSPECTION, FOUND FORWARD CARGO COMPARTMENT FLOOR SUPPORT AT FR 31 CRACKED AND BENT, CENTER OF AIRCRAFT. REPAIRED IAW ER 32-53-26-27. (M)

Part: CASTING — CRACKED (CARGO DOOR)

PHX - DURING SCHEDULED C4 INSPECTION, FOUND AFT CARGO COMPARTMENT DOOR FRAME CRACKED, AFT LOWER CORNER AT HANDLE. REPAIRED PER ER 32-52-30-05. (M)

Part: FLOOR BEAM — CORRODED (CABIN)

PHX - DURING SCHEDULED C4 INSPECTION, FOUND SEVERAL AREAS OF CORROSION ON TOP SURFACE OF CABIN FLOOR 'I' BEAM UPPER CHORD FROM FRAME 17 TO FRAME 19 AT Y 1292. INSTALLED NEW FLOOR BEAM SECTION PER SRM 51-72-11 AND SRM 51-42-21. (M)

Part: O-RING — FAILED (GREEN BRAKE MOD)

PHL-CMH - FLT 265 - EMERGENCY LANDING DECLARED DUE TO LOSS OF GREEN HYDRAULIC SYSTEM AFTER THIRTY MINUTES INTO FLIGHT. AFTER GEAR EXTENSION BY MANUAL SYSTEM, PRESSURE CAME BACK TO 3100 PSI, BUT QUANTITY JUST ABOVE AMBER. CREW HAD NO NOSE GEAR STEERING AFTER LANDING. NO OTHER PROBLEMS WERE NOTED. ACFT TOWED TO GATE. MX REPLACED O RING ON GREEN BRAKE MODULE IN CENTER WHEEL WELL. OPS NORMAL, NO LEAKS NOTED. PERFORMED AMM 32-00-00 TO RETURN LANDING GEAR SYSTEM BACK TO NORMAL AFTER FREE FALL. ACFT RETURNED TO SERVICE. (W)