N805AW

Part: BATTERY — DISCHARGED (ZONE 200) · airframe 78,767 hrs · 37,309 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD FA JUMPSEAT FLASHLIGHT NOT FLASHING ON PREFLIGHT CHECK. MAINTENANCE REPLACED BATTERY ON FLASHLIGHT ON FA JUMP SEAT.

Part: FLASHLIGHT — NO TEST (ZONE 200) · airframe 78,670 hrs · 37,251 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT 1 JUMPSEAT EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-65-00.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 78,628 hrs · 37,218 cycles

AIRCRAFT IN BASE MAINTENANCE: SEAT 9 AND14 CELLING EMERGENCY LIGHT IS NOT WORKING. MAINTENANCE REPLACED EMERGENCY LIGHT LOCATED ON CEILING PANEL BETWEEN ROWS 9 AND 14, IAW AMM 33-51-11.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 78,628 hrs · 37,218 cycles

AIRCRAFT IN BASE MAINTENANCE: RT EMERGENCY EXIT DOOR LIGHT IS NOT WORKING. MAINTENANCE REPLACED RT EMERGENCY EXIT DOOR LIGHT, IAW AMM 33-51-16. OPS-CHECK GOOD.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 78,628 hrs · 37,218 cycles

AIRCRAFT IN BASE MAINTENANCE: SEAT 23 CELLING EMERGENCY LIGHT IS NOT WORKING. MAINTENANCE REPLACED EMERGENCY CEILING LIGHT AT SEAT 23, OPS CHK GOOD IAW AMM 33-51-11.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 78,432 hrs · 37,065 cycles

AIRCRAFT WAS NOT GROUNDED: L2 DOOR CYLINDER PRESSURE IS 1640PSI AT 74 DEGREES. NEEDS TO BEAT 1770PSI. MAINTENANCE SERVICED L2 DOOR DAMPER CYLINDER IAW AMM 52-10-00 TO 1770PSI.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 78,432 hrs · 37,065 cycles

AIRCRAFT WAS NOT GROUNDED: R2 DOOR CYLINDER PRESSURE IS 1680PSI AT 74 DEGREES. NEEDS TO BEAT 1770PSI. MAINTENANCE SERVICED R2 DOOR DAMPER CYLINDER IAW AMM 52-10-00. TO 1770PSI.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 78,432 hrs · 37,065 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR CYLINDER PRESSURE IS 1650PSI AT 74 DEGREES. NEEDS TO BEAT 1770PSI. MAINTENANCE SERVICED R1 DOOR DAMPER CYLINDER IAW AMM 52-10-00. TO 1770PSI.

Part: POWER SUPPLY — INOPERATIVE (ZONE 800) · airframe 77,966 hrs · 36,768 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR EPSU FAILED TO TEST OK. MAINETNANCE REPLACED L1 DOOR EMERGENCY POWER SUPPLY UNIT (EPSU) IAWE AMM 33-51-38.

Part: BATTERY — FAULTY (ZONE 200) · airframe 77,290 hrs · 36,331 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY EXIT LIGHTS ARE ON IN THE ARMED POSITION. EPSU'S FAULTING RIGHT AND REAR LEFT BATTERIES. MAINTENANCE REPLACED REAR RIGHT BATTERIES IAW AMM 33-51-38.

Part: BATTERY — FAULTED (ZONE 200) · airframe 77,290 hrs · 36,331 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY EXIT LIGHTS ARE ON IN THE ARMED POSITION. EPSU'S FAULTING RIGHT AND REAR LEFT BATTERIES. MAINTENANCE REPLACED REAR RIGHT BATTERIES IAW AMM 33-51-38.

Part: BULB — BURNED OUT (ZONE 200) · airframe 77,212 hrs · 36,279 cycles

AIRCRAFT WAS NOT GROUNDED: FA REPORTS "EMERGENCY EXIT" SIGNS AT 2L AND OVERWING POSITIONS HAVE BURNED OUT LIGHT BULBS. MAINTENANCE REPLACED EMER EXIT LOCATION LIGHT ASSY AT 2L IAW AMM:31-51-16.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 77,056 hrs · 36,191 cycles

AIRCRAFT WAS NOT GROUNDED: EXIT ROW 14 EXIT SIGN NOT ILLUMINATING. MAINTENANCE REPLACED ROW 14 LIGHT ASSYS IAW AMM 33-51-16.

Part: SENSOR — DEFECTIVE (TE FLAPS) · airframe 75,135 hrs · 34,966 cycles

AIRCRAFT WAS NOT GROUNDED: AN EMERGENCY WAS DECLARED ON APPROACH INTO DFW DUE TO THE FLIGHT CREW REPORTING THAT WHEN FLAPS 2 WERE SELECTED A FLAPS FAULT MESSAGE FOR THE SLAT FLAP CONTROL COMPUTER 2 FLAP CHANNEL. MAINTENANCE REPLACED THE COMMAND SENSOR UNIT PER AMM 27-51-17. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: PROXIMITY SENSOR — LOOSE (MLG DOOR) · airframe 74,290 hrs · 34,422 cycles

AIRCRAFT WAS GROUNDED: LANDING GEAR DOORS NOT CLOSED CAUTION AFTER LANDING GEAR EXTENSION. MAINTENANCE FOUND NOSE LANDING GEAR SENSOR 19GA TARGET LOOSE DUE TO A MISSING FASTENER, INSTALLED FASTENER AND SECURED TARGET PER AMM 32-32-73. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: CONNECTOR — LOOSE (ZONE 200 - FUSE) · airframe 73,152 hrs · 33,762 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT ROWS 22 ABC AND 23ABC EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE TIGHTENED LOOSE CONNECTOR 7260VC8 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: SLIDE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 72,453 hrs · 33,326 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: DOOR R1 SLIDE PRESSURE NOT IN GREEN BAND. REPLACED DOOR R1 SLIDE PER AMM 25-62-44-000-802-A AND AMM 25-62-44-400-802-A.

Part: SHEAR PLATE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11.

Part: DAMPER — NO TEST (ZONE 800 - DOORS) · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 DAMPER FAILED FUNCTIONAL CHECK. REPLACED DAMPER PER AMM 52-11-14.

Part: WEB — CRACKED (ZONE 800 - DOORS) · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CARGO COMPARTMENT DOOR EXTERNAL SKIN LOWER AREA WEB CRACK. REPLACED WEB PER SRM 51-42-11

Part: SPLICE — WORN (ZONE 100 - FUSE) · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE FORWARD CABIN FLOOR BEAM OUTBOARD SPLICE HAS ELONGATED FASTENER HOLES AT FR 24 AND -Y1292. REPLACED SPLICE PER SRM 51-72-11.

Part: SPLICE — WORN (ZONE 100 - FUSE) · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE FORWARD CABIN FLOOR BEAM INBOARD SPLICE HAS ELONGATED FASTENER HOLES AT FR 24 AND -Y1292. REPLACED SPLICE PER SRM 51-72-11.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE CORROSION ON LEFT WING LEADING EDGE #2 SLAT TRACK #5 LOWER BOLT BETWEEN WS 4067 AND WS 4862, BETWEEN RIBS 8 AND 9. REPLACED BOLT PER TASK CARD 26C51057005.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE CORROSION ON LEFT WING LEADING EDGE #2 SLAT TRACK #5 UPPER BOLT BETWEEN WS 4067 AND WS 4862, BETWEEN RIBS 8 AND 9. REPLACED BOLT PER TASK CARD 26C51057005.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE CORROSION ON LEFT WING LEADING EDGE #2 SLAT TRACK #5 FORWARD BOLT BETWEEN WS 4067 AND WS 4862, BETWEEN RIBS 8 AND 9. REPLACED BOLT PER TASK CARD 26C51057005.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE CORROSION ON LEFT WING LEADING EDGE #2 SLAT TRACK #6 LOWER AFT BOLT BETWEEN WS 6132 AND WS 6699, BETWEEN RIBS 11 AND 12. REPLACED BOLT PER TASK CARD 26C51057005.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #1 LOWER BOLT BETWEEN WS 700 AND WS 1406, BETWEEN RIBS 2 AND 3. REPLACED BOLT PER TASK CARD 26C51057005.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #1 UPPER AFT BOLT BETWEEN WS 700 AND WS 1406, BETWEEN RIBS 2 AND 3. REPLACED BOLT PER TASK CARD 26C51057005.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #1 MID FORWARD BOLT BETWEEN WS 700 AND WS 1406, BETWEEN RIBS 2 AND 3. REPLACED BOLT PER TASK CARD 26C51057005.

Part: BOLT — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #1 FORWARD MIDDLE BOLT BETWEEN RIBS 2 AND 3. REPLACED BOLT PER TASK CARD 26C61057005.

Part: BOLT — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #1 AFT MIDDLE BOLT BETWEEN RIBS 2 AND 3. REPLACED BOLT PER TASK CARD 26C61057005.

Part: COUPLING — WORN (ZONE 100 - FUSE) · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE AFT CABIN FLOOR STRUCTRE UPPER OUTBOARD COUPLING HAS ELONGATED FASTENER HOLES AT FR 66 AND S23R. REPLACED COUPLING PER SRM 51-72-11.

Part: COUPLING — WORN (ZONE 100 - FUSE) · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE AFT CABIN FLOOR STRUCTRE UPPER INBOARD COUPLING HAS ELONGATED FASTENER HOLES AT FR 66 AND S23R. REPLACED COUPLING PER SRM 51-72-11.

Part: BOLT — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #3 LOWER AFT BOLT BETWEEN RIBS 5 AND 6. REPLACED BOLT PER TASK CARD 26C61057005.

Part: BOLT — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #10 LOWER MIDDLE BOLT BETWEEN RIBS 21 AND 22. REPLACED BOLT PER TASK CARD 26C61057005.

Part: SLEEVE — CORRODED (ZONE 400 - NAC/P) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT PYLON SHACKLES OUTBOARD SIDE UPPER PIN SLEEVE AT PYLON RIB 4. REPLACED PIN SLEEVE PER TASK CARD 26C41554028

Part: SLEEVE — CORRODED (ZONE 400 - NAC/P) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT PYLON SHACKLES OUTBOARD SIDE LOWER PIN SLEEVE AT PYLON RIB 4. REPLACED PIN SLEEVE PER TASK CARD 26C41554028

Part: COUPLING — CRACKED (ZONE 100 - FUSE) · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE WEB COUPLING AT FR 35 AND S30L REPLACED COUPLING PER EA 343018.

Part: FITTING — CORRODED (ZONE 400 - NAC/P) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5, BETWEEN PYLON STATION 679 AND 829. REPLACED SPIGOT FITTING PER SRM 51-72-11.

Part: ANCHOR FITTING — CORRODED (ZONE 600 - RH WI) · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING MAIN LANDING GEAR RETRACTION ACTUATOR ANCHORAGE FITTING UPPER AND LOWER SURFACE BETWEEN WS 70 AND WS 141, BETWEEN RIB 2-3. REPAIRED ANCHORAGE FITTING PER EA 343864.

Part: FITTING — CORRODED (ZONE 400 - NAC/P) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5, BETWEEN PYLON STATION 679 AND 829. REPLACED SPIGOT FITTING PER SRM 51-72-11.

Part: HINGE PIN — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING AILERON #2 HINGE PIN. REPLACED HINGE PIN PER TASK CARD 26C50027005.

Part: ANCHOR FITTING — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING MAIN LANDING GEAR RETRACTION ACTUATOR ANCHORAGE FITTING LOWER SURFACE BETWEEN WS 70 AND WS 141, BETWEEN RIB 2-3. REPLACED ANCHORAGE FITTING PER EA 343814.

Part: SUPPORT — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR WEB SUPPORT BETWEEN FR 69 AND FR 70 AT S23R. REPLACED FLOOR WEB SUPPORT PER SRM 51-72-11.

Part: FLOORBEAM — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM AT FR 20 AND -Y1292. REPLACED FLOOR BEAM PER SRM 51-72-11.

Part: FLOORBEAM — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM BETWEEN FR 20 AND FR 21 AT -Y765. REPLACED FLOOR BEAM PER SRM 51-72-11.

Part: DOOR SILL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUT OUT LOWER SILL AT FR 68 AND S23L. REPLACED LOWER SILL PER SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11.

Part: SUPPORT — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

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

Part: SEAT TRACK — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM-SEAT TRACK BETWEEN FR 64 AND FR 66 AT -Y1292. REPLACED BEAM -SEAT TRACK PER SRM 51-72-11.

Part: FRAME — CRACKED (ZONE 200 - FUSE) · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENACE: CRACKED FRAME WEB AFT FACE ON THE HORIZONTAL FLANGE UPPER RADIUS AT FR 68 AND S22L. REPAIRED FRAME PER EA 343089.

Part: FITTING — CRACKED (ZONE 200 - FUSE) · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD CENTER POST LEFT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 2 AT Y0. REPLACED CONTINUITY FITTING PER EA 343072

Part: WINDOW FRAME — CRACKED (ZONE 200 - FUSE) · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD CENTER POST LEFT HAND SIDE WINDSHIELD FRAME UPPER RADIUS UPPER FASTENER HOLE AT FR 2 AND Y0. REPAIRED WINDSHIELD FRAME PER EA 343072.

Part: FITTING — CRACKED (ZONE 200 - FUSE) · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD CENTER POST RIGHT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 2 AT Y0. REPLACED CONTINUITY FITTING PER EA 343072.

Part: WINDOW FRAME — CRACKED (ZONE 200 - FUSE) · airframe 72,453 hrs · 33,325 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD CENTER POST RIGHT HAND SIDE WINDSHIELD FRAME UPPER RADIUS UPPER FASTENER HOLE AT FR 2 AND Y0. REPAIRED WINDSHIELD FRAME PER EA 343072.

Part: TARGET — DETACHED (ZONE 800 - DOORS) · airframe 72,325 hrs · 33,228 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR ARM TARGET CAME OFF. MAINTENANCE: SECURED R1 ARM TARGET AND VERIFIED OPERATION OF ARM/DISARM FUNCTION PER AMM 52-11-00.

Part: NONE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 71,629 hrs · 32,820 cycles

AIRCRAFT WAS GROUNDED: CABIN DOOR 1L INTERMITTENTLY INDICATES THAT THE SLIDE IS NOT ARMED WHEN IT IS IN FLIGHT. DOOR PRESSURE SWITCH LIGHTS ILLUMINATES. MAINTENANCE SERVICED 1L CABIN DOOR ASSIST BOTTLE PER AMM 52-10-00., DOOR INDICATING CORRECTLY NOW.

Part: BATTERY — INOPERATIVE (ZONE 200 - FUSE) · airframe 71,599 hrs · 32,800 cycles

AIRCRAFT WAS NOT GROUNDED: INBOARD FORWARD FLIGHT ATTENDANT SEAT FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT BATTERY PER AMM 25-60-00.

Part: TRANSDUCER — DEFECTIVE (ZONE 100 - FUSE) · airframe 70,596 hrs · 32,192 cycles

AIRCRAFT WAS GROUNDED: RIGHT BRAKE DRAGGING, WHEN BRAKES APPLIED THE BRAKE RELEASES AND WHEN THE BRAKES ARE RELEASED THE BRAKE ENGAGES. **ORIGINAL REPORT WAS AALA202205265254** MAINTENANCE REPLACED THE FOLLOWING ITEMS: AUTOMATIC BRAKE SELECTOR VALVE PER AMM 32-42-27, PARKING BRAKE VALVE PER AMM 32-42-16 (AALA202206020979), NORMAL BRAKE SERVO VALVE MANIFOLD (AALA202206026331) AND TRANSDUCER (AALA202206025092) PER AMM 32-42-48. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: VALVE — DEFECTIVE (ZONE 100 - FUSE) · airframe 70,596 hrs · 32,192 cycles

AIRCRAFT WAS GROUNDED: RIGHT BRAKE DRAGGING, WHEN BRAKES APPLIED THE BRAKE RELEASES AND WHEN THE BRAKES ARE RELEASED THE BRAKE ENGAGES. **ORIGINAL REPORT WAS AALA202205265254** MAINTENANCE REPLACED THE FOLLOWING ITEMS: AUTOMATIC BRAKE SELECTOR VALVE PER AMM 32-42-27, PARKING BRAKE VALVE PER AMM 32-42-16 (AALA202206020979), NORMAL BRAKE SERVO VALVE MANIFOLD (AALA202206026331) AND TRANSDUCER (AALA202206025092) PER AMM 32-42-48. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: MANIFOLD — DEFECTIVE (ZONE 100 - FUSE) · airframe 70,596 hrs · 32,192 cycles

AIRCRAFT WAS GROUNDED: RIGHT BRAKE DRAGGING, WHEN BRAKES APPLIED THE BRAKE RELEASES AND WHEN THE BRAKES ARE RELEASED THE BRAKE ENGAGES. **ORIGINAL REPORT WAS AALA202205265254** MAINTENANCE REPLACED THE FOLLOWING ITEMS: AUTOMATIC BRAKE SELECTOR VALVE PER AMM 32-42-27, PARKING BRAKE VALVE PER AMM 32-42-16 (AALA202206020979), NORMAL BRAKE SERVO VALVE MANIFOLD (AALA202206026331) AND TRANSDUCER (AALA202206025092) PER AMM 32-42-48. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: NONE — NONE · airframe 70,596 hrs · 32,192 cycles

AIRCRAFT WAS GROUNDED: RIGHT BRAKE DRAGGING, WHEN BRAKES APPLIED THE BRAKE RELEASES AND WHEN THE BRAKES ARE RELEASED THE BRAKE ENGAGES. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: SELECTOR VALVE — DEFECTIVE (ZONE 100 - FUSE) · airframe 70,596 hrs · 32,192 cycles

AIRCRAFT WAS GROUNDED: RIGHT BRAKE DRAGGING, WHEN BRAKES APPLIED THE BRAKE RELEASES AND WHEN THE BRAKES ARE RELEASED THE BRAKE ENGAGES. **SUPPLEMENTAL REPORT FOR AALA202205265254: MAINTENANCE REPLACED THE FOLLOWING ITEMS: AUTOMATIC BRAKE SELECTOR VALVE PER AMM 32-42-27, PARKING BRAKE VALVE PER AMM 32-42-16 (AALA202206020979), NORMAL BRAKE SERVO VALVE MANIFOLD (AALA202206026331) AND TRANSDUCER (AALA202206025092) PER AMM 32-42-48. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED. ** (CLOSED)

Part: SPRING — BROKEN (ZONE 800 - DOORS) · airframe 70,183 hrs · 31,907 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR GIRT BAR FLOOR FITTING FORWARD LEVER FAILED TO RETURN. FOUND BROKEN SPRING AND REPLACED SPRING PER AMM 52-11-31.

Part: NONE — NONE · airframe 70,026 hrs · 31,808 cycles

AIRCRAFT WAS GROUNDED: AIRCRAFT REPORTED DURING CLIMB WITH NO FAULT MESSAGES. AIRCRAFT SKIPPED FROM TAKE-OFF (CLIMB) MODE TO DESCENT MODE WHILE CLIMBING OUT OF MIA. DFDR DOWNLOAD EVALUATED BY ESC NO ABNORMALITIES OBSERVED PER ESC CHIEF DISPATCH FOUND NO ISSUES WITH FLIGHT PLAN. PER MOC NO HISTORY LIKE EVENTS FOR 30 DAYS PERFORMED OPERATIONAL TEST OF AUTO FLIGHT SYSTEM PER AMM 22-96-00, TEST PASSED. PER POST FLIGHT REPORT #1 DME MESSAGE, PERFORMED BITE OF DME SYSTEM PER AMM 34-57-00, NO FAULTS. PERFORMED BITE OF BOTH LRRA PER AMM 34-42-00, NO FAULTS. NOTED CREW REPORTED VERBALLY NO UN-COMMANDED DECENT, OK FOR SERVICE. ALSO PERFORMED TSM 34-42-00 LRRA POSSIBLE 5G INTERFERENCE, NO ISSUE FOUND.

Part: EEC — NONE (ZONE 400 - NAC/P) · airframe 70,013 hrs · 31,802 cycles

AIRCRAFT WAS GROUNDED: REJECTED TAKEOFF AT APPROXIMATELY 70 KNOTS DUE TO ECAM ENGINE 1 ECU FAULT. SAFELY RETURNED TO GATE. REPLACED ENGINE 1 EEC PER JOB CARD 26L40073002.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 68,099 hrs · 30,755 cycles

AIRCRAFT WAS NOT GROUNDED: RH OVERWING EMERGENCY LIGHT COVER MISSING. INSTALLED LIGHT COVER IAW AMM 25-23-44, OPS CHECK GOOD.

Part: DOOR — LACK OF LUBE (L1) · airframe 67,679 hrs · 30,503 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 1L ID HARD TO ARM. L1 DOOR SLIDE REMOVED DEBRIS FROM GIRT BAR ARMING LATCHES AND LUBED SAME DOOR/ARMING IAW AMM 25-62-00.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 67,450 hrs · 30,385 cycles

AIRCRAFT WAS NOT GROUNDED. R1 DOOR LOWER EMERGENCY LIGHT HAS BROKEN WIRE. CRIMPED WIRE, PER ESPM 20-48-14. OPERATIONS CHECK GOOD.

Part: APU — ODOR (CABIN) · airframe 66,981 hrs · 30,122 cycles

AIRCRAFT WAS GROUNDED: DIRTY SOCK SMELL IN CABIN ON GROUND AND INFLIGHT. REPLACED APU PER TASK CARD 26L31049005.

Part: REGULATOR VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 66,585 hrs · 29,897 cycles

AIRCRAFT NOT GROUNDED. ECAM MESSAGE AIR ENGINE 2 BLEED ABNORMAL PRESSURE CAME & WENT 3 OR MORE TIMES AT FL 330, CABIN WAS FLUCTUATING & CLIMBING 300-400 FEET PER MINUTE STARTED EARLY DECENT. REMOVED AND REPLACED # 2 ENGINE PRESSURE REGULATING VALVE PER AMM 36-11-52.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 66,437 hrs · 29,818 cycles

AIRCRAFT WAS GROUNDED: RIGHT HAND ELEVATOR HINGE FITTING #3 HAS EXCESSIVE PLAY / WEAR. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 66,388 hrs · 29,784 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED PRESSURE PANEL BETWEEN FR 35 AND FR 36 AT +Y1292. REPAIRED PRESSURE PANEL PER EA 303892.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 66,388 hrs · 29,784 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT PROFILE ANGLE AT FR 58 AND S38L. REPLACED PROFILE ANGLE PER SRM 51-42-11.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 66,388 hrs · 29,784 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT PROFILE ANGLE BETWEEN FR 54 AND FR 55 AT S38L. REPLACED PROFILE ANGLE PER SRM 51-42-11.

Part: CIDS — FAULTED (EMERGENCY LIGHTS) · airframe 65,451 hrs · 29,231 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTED EMERGENCY EXIT LIGHTS WERE ILLUMINATED AND WOULD NOT EXTINGUISH. MAINTENANCE RESET CIDS AND EMERGENCY LIGHT CIRCUIT BREAKER AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.

Part: RIB — CRACKED (NR 2 NACELLE) · airframe 64,150 hrs · 28,495 cycles

AIRCRAFT GROUNDED, NR 2 ENGINE PYLON , OUTBOARD UPPER FAIRING PANEL ATTACHMENT RIB NR 8 WAS CRACKED. REPLACED RIB PER SRM 51-42-11.

Part: CONTROL SERVO — DEFECTIVE (RT WING) · airframe 62,690 hrs · 27,613 cycles

AFTER DEPARTURE THRU 10000 NOTED/FELT VIBRATION, CHANGING FROM CONFIGURATION #3 TO FULL, GOT HEAVY SHAKING WITH ADDITIONAL VIBRATION. SELECTED CONFIGURATION #3 VIBRATION LESSENED. LANDING UNEVENTFUL AND FULL. AIRCRAFT IN CONTROL AT ALL TIMES. DECLARED AN EMERGENCY, LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. INSPECTION FOUND #1 SPOILER BOARD FLOATING. REACTIVATED SPOILER SERVO CONTROL AND THEN DEACTIVATED SPOILER SERVO CONTROL PER AMM 27-64-00-440-001-A AND 27-64-00-040-001-A. OPERATIONS CHECK OF #1 SPOILER BOARDS CHECK GOOD. REPLACED RIGHT HAND #1 SPOILER SERVO PER AMM 27-64-41-0401. LEAK AND OPERATIONS CHECK GOOD PER MM 27-64-00-710-001-A.

Part: CONTROL UNIT — FAULTY (BRAKES) · airframe 62,638 hrs · 27,570 cycles

DURING INITIAL TAKEOFF ROLL, AFTER POWER WAS SET TO FLEX, LEFT BRAKES APPEARED TO LOCK UP CAUSING THE ACFT TO LOOSE DIRECTIONAL CONTROL. REJECTED TAKEOFF AND RETURNED TO THE GATE. ACFT PULLED TO LEFT. BRAKES WERE NORMAL ON TAXI BACK TO GATE. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED 32-51-00-810-831-A, AMM 32-46-00-740-001, 32-42-34-400-001-A, AND 32-42-34-000-001-A. REPLACED BRAKING AND STEERING UNIT. CHECKED NORMAL.

Part: FITTING — CRACKED (FRAMES 42-43) · airframe 61,791 hrs · 27,032 cycles

CRACK FOUND ON THE RT MAIN LANDING GEAR DOOR KEEL BEAM, AFT ACTUATOR FITTING, EMINATING FROM LOWER FORWARD EDGE OF FITTING TO APPROXIMATELY 1/4 INCH ABOVE EDGE TO APPROXIMATELY 1/4 INCH AFT OF EDGE. REPAIRED THE ACTUATOR FITTING IAW EA 280709.

Part: PIN — CORRODED (RT MLG) · airframe 61,791 hrs · 27,032 cycles

AIRCRAFT IN BASE MAINTENANCE. RIGHT HAND MAIN LANDING GEAR REAR PINTLE PIN CORRODED. REPLACED RIGHT HAND MAIN LANDING GEAR REAR PINTLE PIN PER 26T00032001.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 61,674 hrs · 26,963 cycles

DURING CRUISE, LOST GREEN HYDRAULIC SYSTEM, LOW LEVEL FOLLOWED BY LOSS OF PRESSURE. EMERGENCY DELCARED AND AIRCRAFT DIVERTED. FLIGHT LANDED WITHOUT INCIDENT. REPLACED A HYDRAULIC LINE IAW AMM 20-23-11. ACCOMPLISHED A FUNCTIONAL CHECK OF THE MLG IAW AMM 32-31-00-720-002-A. NO LEAKS NOTED. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: BYPASS VALVE — INOPERATIVE (OUTLET) · airframe 61,351 hrs · 26,790 cycles

CABIN ODOR. REPLACED THE AVIONICS EXTRACT FAN IAW AMM 21-26-51-400-0 01-A DUE TO SMOKEY ODOR AND REPLACED OUTLET BYPASS VALVE WHICH WAS INOPERATIVE IAW AMM 21-26-55. ACFT GROUNDED.

Part: FAN — SMOKE (EXTRACT) · airframe 61,351 hrs · 26,790 cycles

CABIN ODOR, REPLACED AVIONICS EXTRACT FAN IAW AMM 21-26-51-400-0 01-A, DUE TO SMOKEY ODOR, AND REPLACED OUTLET BYPASS VALVE WHICH WAS INOPERATIVE IAW AMM 21-26-55. AIRCRAFT WAS GROUNDED.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 61,318 hrs · 26,770 cycles

EMERGENCY LIGHTING NOT ALL WORKING. RESET EMEGENCY LIGHT SWITCHES AND ALLOWED AIRCRAFT TO CHARGE OVERNIGHT.

Part: OVEN — DEFECTIVE (GALLEY) · airframe 61,060 hrs · 26,611 cycles

AIRCRAFT WAS GROUNDED. FLIGHT ATTENDANT REPORTED FUMES/SMELL OF BURNING SMELLY SOCKS IN FORWARD AND AFT CABIN AFTER TAKEOFF. CREW OXYGEN WAS USED. AN EMERGENCY WAS DECLARED AND FLIGHT LANDED WITHOUT INCIDENT. ACCOMPLISHED JOB CARD #26L00021001-CABIN AIR QUALITY AND FOUND FORWARD OUTBOARD OVEN TO BE BAD. REPLACED OVEN PER AMM 25-35-19-401.

Part: PANEL — DETACHED (LT OVERWING EXIT) · airframe 59,973 hrs · 25,952 cycles

AFTER LANDING, EMERGENCY LEFT WING EXIT TURNED AMBER. PASSENGER REPORTED PANEL FELL OFF ON LANDING. ADJUSTED EMERGENCY DOOR COVER. NO FAULTS NOTED OK FOR CONT SERVICE.

Part: BUSTLE — LOOSE (L2 DOOR SLIDE) · airframe 59,928 hrs · 25,914 cycles

L2 DOOR SLIDE BUSTLE INDICATES UNLOCKED. SECURED THE L2 DOOR SLIDE BUSTLE IAW AMM.

Part: SLIDING WINDOW — BINDING (COCKPIT) · airframe 59,722 hrs · 25,772 cycles

FIRST OFFICER SLIDING WINDOW IS HARD TO OPEN AND CLOSE. REPLACED SLIDING WINDOW IAW AMM 56-12-11. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS GROUNDED.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 59,627 hrs · 25,704 cycles

EXIT LIGHT LENS, LEFT SIDE CAME OFF. REINSTALLED EMERGENCY LIGHT LENS.

Part: LAMP — BROKEN (EMERGENCY LIGHT) · airframe 59,617 hrs · 25,694 cycles

EMERGENCY EXIT HAS A BROKEN LAMP AT FOWARD LEFT BULKHEAD. REPLACED THE LAMP, OPS CHECKED GOOD.

Part: COVER — OUT OF ADJUST (OVERWING DOOR) · airframe 59,568 hrs · 25,666 cycles

LEFT WING EMERGENCY EXIT ECAM ON LANDING. MAINTENANCE PROPERLY INSTALLED EXIT THE COVER IAW AMM 52-21-11-400-001-A.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR SLIDE) · airframe 59,210 hrs · 25,454 cycles

R1 DOOR SLIDE WILL NOT ARM. REMOVED DEBRIS FROM R1 DOOR GIRT BAR AREA.

Part: HOOK AND LOOP — WORN (L2 DOOR) · airframe 59,114 hrs · 25,398 cycles

THE HOOK AND LOOP ON THE RED WARNING STRAP AT THE 2L DOOR IS WORN OUT. STRAP WILL NOT REMAIN IN POSITION. SECURED THE HOOK AND LOOP ON L2 DOOR.

Part: LOCK WIRE — BROKEN (R1 DOOR SLIDE) · airframe 59,084 hrs · 25,379 cycles

LOCK WIRE BROKEN FOR RELEASE CABLE RETAINER BALLS, & PINS FOR THE R1 ESCAPE SLIDE. REPLACED R1 DOOR ESCAPE SLIDE.

Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 59,084 hrs · 25,379 cycles

INTERGRANULAR CORROSION ON FLOOR SUPPORT AT INTERSECTION OF FR 16 AND BACK EDGE OF FLOOR PANEL 221PF UNDER FORWARD LAVATORY. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FRAME 66) · corrosion level 2 · airframe 59,084 hrs · 25,379 cycles

AIRCRAFT IN BSE MAINTENANCE. CORROSION IN 3 HOLES IN FLOOR BEAM FOR FLIGHT ATTENDANTS SEAT AT RBL 16 AND FROM FR 66 PLUS AND MINUS 6 INCHES. REPLACED FLOOR BEAM PER SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 59,084 hrs · 25,379 cycles

CORROSION ON LEFT AFT FLOOR SUPPORT AROUND LAVATORY MOUNT HOLES AT LBL 20 BETWEEN FRAMES 64 AND 66. REPLACED THE FLOOR SUPPORT IAW SRM-51-42-11, AND DRAWING D53472815.

Part: THRESHOLD — CORRODED (FRAME 68) · airframe 59,084 hrs · 25,379 cycles

CORROSION ON R2 DOOR FTHRESHOLD AT FRAME 68 AND STRINGER 23R. REPAIRED THRESHOLD IAW SRM 53-41-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,084 hrs · 25,379 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT WET AREA FLOORBEAM AROUND HOLE MOUNT AT 2.75 INCHES FORWARD OF FR 66 AND -Y765.

Part: FLOOR SUPPORT — CORRODED (FRAME 66) · corrosion level 2 · airframe 59,084 hrs · 25,379 cycles

NTERGRANULAR CORROSION ON FLOOR SUPPORT 2.75 INCHES FORWARD OF FRAME 66 AT -Y765. R EPLACED FLOOR BEAM PER SRM 51-42-11 AND DRAWING 18D5347219.

Part: FLOOR SUPPORT — CORRODED (FRAME 68) · airframe 59,084 hrs · 25,379 cycles

CORROSION ON FLOOR SUPPORT AFT OF LEFT DOOR SILL INBOARD OF AFT GIRT FITTING AT FRAME 68 AND 50 INCHES LEFT OF CENTER. REPAIRED THE FLOOR SUPPORT SRM 53-41-14.

Part: BOX BEAM — CRACKED (FRAME 43) · airframe 57,544 hrs · 24,524 cycles

RIGHT SIDE BOX BEAM UPPER FLANGE AFT OPEN HOLE IS CRACKED AT FRAME 43. REPAIRED THE BOX BEAM IAW EO 5315Y066 REV B PG IV -32 THRU IV=50 AND PG IV-12.

Part: FITTING — DIRTY (GIRT BAR) · airframe 57,263 hrs · 24,359 cycles

AIRCRAFT WAS NOT GROUNDED. F/A REPORTED THAT THE L2 DOOR ARM LEVER IS STIFF AND GRINDS. CLEANED AND LUBED FLOOR GIRT BAR FITTINGS. OPS CHECK GOOD.

Part: TRACK — DIRTY (COCKPIT WINDOW) · airframe 57,208 hrs · 24,332 cycles

AIRCRAFT WAS NOT GROUNDED. F/O EMERGENCY EXIT WINDOW VERY DIFFICULT TO CLOSE. FOUND DEBRIS IN TRACK, CLEANED TRACK AND ACCOMPLISHED A SATISFACTORY OPS CHECK. WINDOW OPERATES SMOOTHLY.

Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY) · airframe 56,440 hrs · 23,898 cycles

AIRCRAFT WAS NOT GNDED. INFLIGHT LAVATORY E, SMOKE & FIRE ALARM, SYS RESET. NO PAX IN OR NEAR LAVATORY. INSPECTED LAVATORY, NO EVIDENCE OF SMOKE OR FIRE. REPLACED LAVATORY E SMOKE DETECTOR & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 26-17-15.

Part: ACTUATOR — DEFECTIVE (NR 1 ENGINE) · airframe 56,372 hrs · 23,860 cycles

AIRCRAFT WAS GNDED. DURING TAKEOFF THE CREW RECEIVED A COMPRESSOR VANE FAULT ON NR 1 ENG AT 60 KNOTS & THE TAKEOFF WAS ABORTED. REPLACED VSV ACTUATOR ON NR 1 ENG IAW TASK CARD 26T40075005.

Part: LENS — MISSING (EXIT SIGN) · airframe 55,540 hrs · 23,449 cycles

SMALL EMER EXIT SIGN BELOW & AHEAD OF LT OVERWING EXIT MISSING. INSTALLED LENS & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-00.

Part: CONTAINER — MALFUNCTIONED (CABIN)

PASSENGER OXYGEN TEST FAILED TO DROP AT ROWS 2R, 5L & 18L. REPLACED THE PAX EMER OXYGEN CONTAINERS.

Part: SLIDE — DELAMINATED (CABIN)

RIGHT OVERWING SLIDE PANEL LOOKS DELAMINATED. REPLACED THE RT OVERWING SLIDE.

Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 53,919 hrs · 22,567 cycles

EMERGENCY LIGHT AT SEAT ROW 18 LT INOPERATIVE. WIRES PULLED OUT. R & R SEAT HARNESS AT ROW 18 LT.

Part: LENS — LOOSE (CABIN) · airframe 53,861 hrs · 22,533 cycles

EMERGENCY FLOOR LIGHT FROM ROW 3 IS STICKING OUT. REPLACED ROW 3 LENS WITH GOOD OPERATIONAL CHECK IAW CMM 25-40-06.

Part: LENS — MISSING (CABIN) · airframe 52,692 hrs · 21,961 cycles

SEAT MOUNTED EMER EXIT LIGHT LENS MISSING AT SEAT 3C. REPLACED THE LENS IAW AMM 33-51-19 PB401. OPERATIONS CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 52,349 hrs · 21,759 cycles

SEATS 1C & 3C, EXIT MARKER ESCAPE PATH LIGHTING LENS MISSING. INSTALLED LENS ON SEATS 1C & 3C IAW 33-51-19.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,349 hrs · 21,759 cycles

THE L1 DOOR EMER EXIT MARKER PATH LIGHT INOPERATIVE. R & R L1 DOOR EMER EXIT MARKER PATH LIGHT IAW AMM 33-51-13. OPERATIONS CHECKED OK.

Part: SENSOR — FAULTY (ANTI-ICE SYSTEM) · airframe 52,261 hrs · 21,704 cycles

EN ROUTE CREW RECEIVED AN ANTI-ICE L WINDSHIELD ECAM MSG. FLIGHT RETURNED TO FIELD & LANDED WITHOUT INCIDENT. TROUBLE SHOT IAW TSM 30-42-00-810-801A, SENSORS ALL CHECKED NORMAL WITH ACFT PRESSURIZED OR UNPRESSURIZED. WIRES CHECKED NORMAL. SUSPECT NOT ONLY PRESS BUT TEMPERATURE TO CAUSE SENSOR 1 FAULT IN FLIGHT. SWAPPED SENSOR USAGE FROM SENSOR 1 TO SPARE SENSOR 2 IAW ESPM 20-44-11. OPERATIONS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (NLG) · airframe 51,520 hrs · 21,288 cycles

AFTER TO, THE NOSE GEAR DOOR DID NOT CLOSE WITH GEAR UP. RECYCLED GEAR, NOSE GEAR DOOR VERY SLOW TO CLOSE, THEN OPERATIONS WERE NORMAL. UPON LANDING, LGCIU DISAGREE ECAM MOMENTARILY DISPLAYED, THEN BACK TO NORMAL. FOUND NO CURRENT FAULTS DISPLAYED. ACCOMPLISHED BITE CHECK OF LGCIU 1 & 2. NO FAULTS FOUND & NO PRIOR HISTORY.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,749 hrs · 20,959 cycles

C11 SY6 CHECK, CABIN FLOOR BEAM FROM FRAME 65 TO FRAME 67 CORRODED AT Y -304. R & R FLOOR BEAM IAW A320 SRM 53-00-14.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 49,967 hrs · 20,637 cycles

CREW REPORTED THE R1 DOOR LOWER FORWARD EXIT LIGHT LENS FELL OFF. MAINTENANCE REPLACED R1 DOOR EMERGENCY EXIT LIGHT LENS. OPS CHECK GOOD.

Part: UPLOCK SENSOR — INOPERATIVE (MLG) · airframe 49,640 hrs · 20,494 cycles

AFTER TAKEOFF, CREW REPORTED LANDING GEAR DOORS ECAM, PLUS LANDING GEAR, NOSE GEAR NOT UPLOCKED. IAW ECAM, RECYCLED LANDING GEAR. NOSE GEAR WOULD NOT UPLOCK. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. FLIGHT LANDED WITHOUT INCIDENT. MX INSPECTED SYS AND FOUND NLG UPLOCK SENSOR 12GA INOP. REPLACED SENSOR IAW AMM 32-31-73-400-005-A. BITE CHECK GOOD. ACCOMPLISHED NLG EXTENSION/RETRACTION TEST IAW AMM 32-31-00-720-003-A. ALL CHECKS GOOD WITH NO FAULTS NOTED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 49,489 hrs · 20,430 cycles

MX REPORTED THE R2 DOOR FRAME EXIT LIGHT MISSING LENS. MX REPLACED R2 DOOR FRAME EXIT LIGHT LENS AS REQUIRED.

Part: COMPUTER — UNKNOWN (NR 1 & 2 ELAC) · airframe 49,234 hrs · 20,326 cycles

ENROUTE, CREW REPORTED A FLT CTL ELAC 1 & 2 PITCH FAULT. FLIGHT RETURNED TO FIELD LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MX PERFORMED TROUBLESHOOTING IAW REF TSM 27-93-00-810-837-A AND 27-93-00-810-843-A. NO FAULTS. AS PRECAUTION, R & R ELAC NR 1 IAW AMM 27-93-34-000-001-A. OPS CHECKED GOOD. ALSO, R & R RELAY 36CE1. REF WDM 27-93. OPS CHECKED GOOD. PERFORMED CAT 3 DUAL CHECK. REF AMM 22-97.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 47,725 hrs · 19,632 cycles

MAINTENANCE REPORTED THE AFT FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT BATTERY IS ALMOST DEAD. MAINTENANCE REPLACED AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,419 hrs · 19,497 cycles

CREW REPORTED EXIT LIGHT 2L INOP. MAINTENANCE REPLACED EXIT LIGHT LENS COVER AT 2L DOOR.

Part: LENS — MISSING (CABIN) · airframe 47,329 hrs · 19,459 cycles

MAINTENANCE REPORTED PASSENGER SEAT 6C AND 16C EMERGENCY EXIT LIGHT LENS COVERS MISSING. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT LENS COVERS AT PASSENGER SEATS 6C AND 16C.

Part: BOTTLE — LOW PRESSURE (EVAC SLIDE) · airframe 47,078 hrs · 19,354 cycles

MAINTENANCE REPORTED THE SLIDE BOTTLE, EMERGENCY RIGHT, LOW INDICATION. REMOVED AND REPLACED RIGHT HAND EMERGENCY EXIT SLIDE BOTTLE PER AMM 25-6-46-440-001A CIDS STATUS OK.

Part: SEAL — LEAKING (APU) · airframe 46,839 hrs · 19,247 cycles

CREW REPORTED A STINKY SOCK SMELL THAT STARTED AT 12,000 FEET DURING DESCENT. MAINTENANCE FOUND APU OIL LEAK AT TURBINE BEARING LUBE TUBE ASSEMBLY. REPLACED SEALS ON LUBE TUBES AND TUBE ASSEMBLY PER AMM 49-91-53-000-001-A. LEAK CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 43,455 hrs · 17,704 cycles

EMERGENCY LIGHT SYSTEM NOT PASSING SYSTEM TEST. FAULT MESSAGES "ESPU115 VAC EMER L", "ESPU INT LOAD AFT L", & "ESPU UNIT EMERG L" ARE DISPLAYED. REMOVED AND DISPLAYED EMERGENCY POWER SUPPLY UNIT (ESPU) ON AIRCRAFT MID LEFT IAW AMM 33-51-38-400-001. OPS CHECKED GOOD.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 40,714 hrs · 16,434 cycles

SAL - S4 - MAJOR REPAIR - CORROSION ON SUPPORT FITTING AT FR58 BETWEEN S40R TO S43R. REPLACED SUPPORT FITTING AT FR58 BETWEEN S40R TO S43R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53476358.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,714 hrs · 16,434 cycles

SAL - S4 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR42 + 13 INCHES, S23R. REPLACED SEAT TRACK AT FR42 + 13 INCHES, S23R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53370500 & D53371110.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,714 hrs · 16,434 cycles

MAJOR REPAIR - S4 CHECK - CORROSION ON SEAT TRACK LOCATED AT Y765, FR 44+7. REPLACED SEAT TRACK LOCATED AT Y765, FR 44+7 IAW A319 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,714 hrs · 16,434 cycles

SAL - MAJOR REPAIR - S4 CHECK - CORROSION ON SEAT TRACK LOCATED Y765 AT FR 61. REPAIRED SEAT TRACK LOCATED Y765 AT FR 61 IAW A319 SRM 53-00-15.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,714 hrs · 16,434 cycles

SAL - MAJOR REPAIR - S4 CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY BEAM AT -Y503.2, FR 14. REPLACED RAIL DUMMY BEAM AT -Y503.2, FR 14 IAW A319 SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,714 hrs · 16,434 cycles

SAL - MAJOR REPAIR - S4 CHECK - LEVEL 2 GALVANIC CORROSION ON THE L1 DOOR CUTOUT AFT LOWER CORNER FITTING, FR 20, S23L, -Z510. REPLACED THE L1 DOOR CUTOUT AFT LOWER CORNER FITTING, FR 20, S23L, -Z510 IAW A319 SRM 51-72-11.

Part: SLEEVE — CORRODED (RT PYLON) · corrosion level 2 · airframe 40,714 hrs · 16,434 cycles

SAL - MAJOR REPAIR - S4 CHECK - LEVEL 2 PTTING CORROSION ON THE RIGHT PYLON SPIGOT SLEEVE. REPLACED THE RIGHT PYLON SPIGOT SLEEVE IAW TASK CARD 26C40054031 AND 26C40054035.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,714 hrs · 16,434 cycles

MAJOR REPAIR - S4 CHECK - CORROSION ON SEAT TRACK LOCATED AT -Y1292, FR 45+16. REPLACED SEAT TRACK LOCATED AT -Y1292, FR 45+16 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,714 hrs · 16,434 cycles

SAL - MAJOR REPAIR - S4 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM LOCATED FR. 68 AND Y-765. REPLACED FLOORBEAM LOCATED FR 68 AND Y-765 IAW A319 SRM 51-72-11.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,714 hrs · 16,434 cycles

SAL - S4 - MAJOR REPAIR - CRACK ON FUSELAGE SKIN ABOVE EMERGENCY EXIT CUTOUT BETWEEN FR40 TO FR41, S13R. REPAIRED FUSELAGE SKIN ABOVE EMERGENCY EXIT CUTOUT BETWEEN FR40 TO FR41, S13R IAW EA 133252.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 40,719 hrs · 16,434 cycles

MAJOR REPAIR - S4 CHECK - CORROSION ON LEFT WING FUEL ACCESS PANEL 540NB, BETWEEN RIB 18 AND RIB 19. REPLACED LEFT WING FUEL ACCESS PANEL 540NB IAW TASK CARD 26C50057092.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 40,719 hrs · 16,434 cycles

MAJOR REPAIR - S4 CHECK - CORROSION ON LEFT WING FUEL ACCESS PANEL 550DB BETWEEN RIB 25 AND RIB 26. REPLACED LEFT WING FUEL ACCESS PANEL 550DB IAW TASK CARD 26C50057092.

Part: STRUCTURE — CRACKED (EMERGENCY EXIT) · airframe 40,714 hrs · 16,434 cycles

SAL - S4 - MAJOR REPAIR - CRACK ON EMERGENCY EXIT DOOR 834 SEGMENT BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO 3. ACCOMPLISHED MODIFICATION EMERGENCY EXIT DOOR 834 SEGMENT BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO 3 IAW EO 5210Y228.

Part: STRUCTURE — CRACKED (EMERGENCY EXIT) · airframe 40,714 hrs · 16,434 cycles

SAL - S4 - MAJOR REPAIR - CRACK ON EMERGENCY EXIT DOOR NR 844 SEGMENT BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO 3. ACCOMPLISHED MODIFICATION EMERGENCY EXIT DOOR NR 844 SEGMENT BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO 3 IAW EO 5210Y228.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,714 hrs · 16,434 cycles

SAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR67 + 18 INCHES, -Y1162. REPLACED FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR67 + 18 INCHES, -Y1162 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472000.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,714 hrs · 16,434 cycles

SAL - MAJOR REPAIR - S4 CHECK - LEVEL 2 GALVANIC CORROSION ON THE L2 DOOR CUTOUT LOWER SILL AT FR 67 + 18 - FR 68, +Y1732. REPAIRED THE L2 DOOR CUTOUT LOWER SILL AT FR 67 + 18 - FR 68, +Y1732 IAW A319 SRM 53-41-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,714 hrs · 16,434 cycles

SAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67 + 18 INCHES TO FR69 +3 INCHES, -Y1165. REPLACED FLOORBEAM BETWEEN FR67 + 18 INCHES TO FR69 +3 INCHES, -Y1165 IAW A319 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,714 hrs · 16,434 cycles

SAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON R-2 DOOR WAY LOWER SILL AT FR66. REPAIRED R-2 DOOR WAY LOWER SILL AT FR66 IAW A319 SRM 53-41-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,714 hrs · 16,434 cycles

SAL - MAJOR REPAIR - S4 CHECK - CORROSION ON SEAT RAIL BEAM AT FR 55 + 14, S23R, -Y765. REPAIRED SEAT RAIL BEAM AT FR 55 + 14, S23R, -Y765 IAW A319 SRM 53-00-15 FIGURE 201.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 40,714 hrs · 16,434 cycles

SAL - S4 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251RF BETWEEN FR58 TO FR62 & BETWEEN -Y254 TO Y254. REPLACED FLOOR PANEL 251RF BETWEEN FR58 TO FR62 & BETWEEN -Y254 TO Y254 IAW A319 SRM 53-02-00 & IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 40,714 hrs · 16,434 cycles

SAL - S4 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251WF BETWEEN FR62 TO FR64 & BETWEEN -Y765 TO Y765. REPLACED FLOOR PANEL 251WF BETWEEN FR62 TO FR64 & BETWEEN -Y765 TO Y765 IAW A319 SRM 53-02-00 & IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 40,714 hrs · 16,434 cycles

SAL - S4 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251LF BETWEEN FR54 TO FR58 & BETWEEN -Y254 TO Y254. REPLACED FLOOR PANEL 251LF BETWEEN FR54 TO FR58 & BETWEEN -Y254 TO Y254 IAW A319 SRM 53-02-00 & IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 40,714 hrs · 16,434 cycles

SAL - S4 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 241EF BETWEEN FR36 TO FR42 & BETWEEN -Y254 TO Y254. REPLACED FLOOR PANEL 241EF BETWEEN FR36 TO FR42 & BETWEEN -Y254 TO Y254 IAW A319 SRM 53-02-00 & IRM 9701 REV G.

Part: PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 40,714 hrs · 16,434 cycles

S4 CHECK- MAJOR REPAIR - CORROSION ON COUNTERSUNK HOLES OF LEFT LOWER WING FUEL PANEL 550AB BETWEEN RIB 22 TO RIB 23 & BETWEEN S8L TO S11L. REPLACED LEFT LOWER WING FUEL PANEL 550AB BETWEEN RIB 22 TO RIB 23 & BETWEEN S8L TO S11L IAW A319 SRM 51-72-11 & CARD 26C50057092.

Part: OXYGEN MASK — DAMAGED (CABIN) · airframe 40,714 hrs · 16,434 cycles

SAL - S4 - EES - CUT RESERVOIR BAG ON OXYGEN MASK CONTAINER AT POSITION 17 & 15 LEFT. REPLACED OXYGEN MASK CONTAINER AT POSITION 17 & 15 LEFT IAW A319 AMM 35-21-43.

Part: DAMPER — LOW PRESSURE (DOOR) · airframe 40,714 hrs · 16,434 cycles

SAL - S4 - EES - LOW PRESSURE IN DOOR DAMPER AT DOOR 831. CHARGED DAMPER & EMERGENCY OPERATION CYLINDER AT DOOR 831 IAW A319 AMM 52-10-00-614-001. LEAK TEST GOOD.

Part: OXYGEN MASK — DAMAGED (CABIN) · airframe 40,714 hrs · 16,434 cycles

SAL - S4 - EES - CUT HOSE ON OXYGEN MASK IN POSITION 20 LEFT. REPLACED OXYGEN MASK IN POSITION 20 LEFT IAW A319 AMM 35-21-43.

Part: DAMPER — LOW PRESSURE (DOOR) · airframe 40,714 hrs · 16,434 cycles

SAL - S4 - EES - LOW PRESSURE IN DOOR DAMPER AT DOOR 842. CHARGED DAMPER & EMERGENCY OPERATION CYLINDER AT DOOR 842 IAW A319 AMM 52-10-00-614-001. LEAK TEST GOOD.

Part: DAMPER — LOW PRESSURE (DOOR) · airframe 40,714 hrs · 16,434 cycles

SAL - S4 - EES - LOW PRESSURE IN DOOR DAMPER AT DOOR 832. CHARGED DAMPER & EMERGENCY OPERATION CYLINDER AT DOOR 832 IAW A319 AMM 52-10-00-614-001. LEAK TEST GOOD.

Part: DAMPER — LOW PRESSURE (DOOR) · airframe 40,714 hrs · 16,434 cycles

SAL - S4 - EES - LOW PRESSURE IN DOOR DAMPER AT DOOR 841. CHARGED DAMPER & EMERGENCY OPERATION CYLINDER AT DOOR 841 IAW A319 AMM 52-10-00-614-001. LEAK TEST GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,714 hrs · 16,434 cycles

SAL - S4 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR36, S23R, -Y765. REPLACED SEAT TRACK AT FR36, S23R, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING 3D57130146.

Part: DAMPER — OUT OF ADJUST (R2 DOOR) · airframe 40,714 hrs · 16,434 cycles

SAL - EES - S4 CHECK - R2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER FINGER AND STRIKER ADJUSTMENT DIMENSION "A" AND "B" WERE FOUND TO BE OUT OF TOLERANCE. ADJUSTED THE R2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER FINGER AND STRIKER ADJUSTMENT DIMENSION "A" AND "B" DIMENSIONS IAW A319 AMM 52-13-14-820-002.

Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 40,714 hrs · 16,434 cycles

SAL - S4 - MAJOR REPAIR - EXCESS PLAY ON NR 3 RUDDER HINGE FITTING AT STA 2289 RIB 5. REPLACED NR 3 RUDDER HINGE ARM FITTING AT STA 2289 RIB 5 IAW A319 55-36-41.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 39,966 hrs · 16,111 cycles

FLT 46 - BUR-PHX - EMERGENCY LIGHTS - L1 OUTBOARD AND L2 INBOARD FLASHLIGHTS HAS NO FLASHING RED LIGHT. REMOVED AND REPLACED FLASHLIGHT BATTERIES AND SEALS AT L1 OUTBOARD & L2 INBOARD. OPERATIONAL CHECK WAS GOOD.

Part: SOLENOID — DEFECTIVE (BLEED AIR SYS) · airframe 39,193 hrs · 15,756 cycles

FLT 9207 PIT-PHX - CABIN ODOR - ECAM MESSAGE 'AIR ENG 1 HP VLV FAULT' ON DESCENT SHORTLY AFTER GOT A STRONG DIRTY SOCK SMELL THROUGHOUT THE AIRCRAFT. MAINTENANCE REMOVED AND REPLACED BLEED PRESSURE REGULATOR VALVE CONTROL SOLENOID (10HA1) IAW AIRBUS MAINTENANCE MANUAL 36-11-55.

Part: CABLE — BROKEN (EVAC SLIDE) · airframe 37,339 hrs · 14,960 cycles

PIT - C11 - EES - LEFT SIDE OVERWING EMERGENCY EXIT WHILE ACCOMPLISHING MONITOR ITEM 25-9752-8-0118, FOUND INNER TELEFLEX CABLE ASSEMBLY BROKEN AT QUICK DISCONNECT ON INFLATION BOTTLE. REPLACED CABLE CONTROL ASSEMBLY.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 37,904 hrs · 15,202 cycles

FLT 468 - DCA - LAS - EMERGENCY LIGHTS - EMERGENCY EXIT LIGHTS FAILED TEST. REMOVED AND REPLACED FAULTY EMERGENCY POWER SUPPLY UNIT (EPSU) OVERWING EXIT RT PER AMM 33-51-38-400. OPERATIONAL CHECK WAS GOOD.

Part: WATER HEATER — FAULTY (CABIN) · airframe 37,499 hrs · 15,034 cycles

FLT 337 - PHX - SJD - BURNING SMELL - FLIGHT ATTENDANT REPORTS BURNING SMELL ON DESCENT. SMELL COMING FROM FORWARD LAV / GALLEY AREA SMELLING LIKE BURNING RUBBER. REMOVED AND REPLACED WATER HEATER AT FORWARD LAV PER AMM 38-10-01A.

Part: COMPUTER — DEFECTIVE (COCKPIT) · airframe 37,418 hrs · 14,990 cycles

FLT 64 LAS-BOS - EMERGENCY LANDING - WHILE EN ROUTE AT FL370, RIGHT WINDOW HAD ARCING AND SPARKS. COMPLIED WITH QRH PROCEDURES. FIVE MINUTES LATER, RIGHT WINDOW SHATTERED. CREW DECLARED AN EMERGENCY AND MADE AN EMERGENCY DESCENT (DIVERSION) INTO ORD. MAINTENANCE REMOVED AND REPLACED THE RIGHT WINDSHIELD AND RT WINDOW HEAT COMPUTER PER AIRBUS MAINTENANCE MANUAL 56-11-11-400-001-01 AND 30-42-34.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 37,418 hrs · 14,990 cycles

FLT 64 LAS-BOS - EMERGENCY LANDING - WHILE EN ROUTE AT FL370, RIGHT WINDOW HAD ARCING AND SPARKS. COMPLIED WITH QRH PROCEDURES. FIVE MINUTES LATER, RIGHT WINDOW SHATTERED. CREW DECLARED AN EMERGENCY AND MADE AN EMERGENCY DESCENT (DIVERSION) INTO ORD. MAINTENANCE REMOVED AND REPLACED THE RIGHT WINDSHIELD AND RT WINDOW HEAT COMPUTER PER AIRBUS MAINTENANCE MANUAL 56-11-11-400-001-01 AND 30-42-34.

Part: EPSU — DISCHARGED (CABIN) · airframe 37,299 hrs · 14,941 cycles

FLT 596 - PHX - EEL - EMERGENCY LIGHT SYSTEM TEST FAILED EMERGENCY POWER SUPPLY UNIT FORWARD LEFT. MAINTENANCE REMOVED AND REPLACED THE EPSU IAW AIRBUS MAINTENANCE MANUAL 33-51-38.

Part: WIRE — SHORTED (CABIN) · airframe 37,288 hrs · 14,938 cycles

FLT 596 - PHX - EEL - EMERGENCY LIGHT AT ROW 1 CEILING LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB, NO HELP. FOUND SHORTED WIRE AT SEAT 1L. REPLACED WIRE. OPERATIONAL CHECK GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 36,299 hrs · 14,449 cycles

FLT 9245 - EMERGENCY FLOOR LIGHT COVER MISSING ABEAM SEAT 3C. MAINTENANCE INSTALLED LENS AT 3C EMERGENCY LIGHT.

Part: LENS — MISSING (CABIN) · airframe 36,119 hrs · 14,361 cycles

FLT 48 - EMERGENCY LIGHTS - EMERGENCY LIGHT LENS MISSING ON SEAT 3 AIRCRAFT LEFT. REPLACED EMERGENCY LIGHT LENS. OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 62,753 hrs · 42,991 cycles

FLT 504 - DFW-PHX - EMERGENCY LIGHTS - LEFT EMERGENCY BATTERY FAULT DURING TEST (MID CABIN). REMOVED AND REPLACED LEFT EMERGENCY BATTERY (MID CABIN).

Part: DAMPER — LEAKING (PAX DOOR) · airframe 34,589 hrs · 13,692 cycles

SAL - C7 - EES - NR 6143454 - LEAK IN DAMPER EMERGENCY OPERATION CYLINDER OF THE PASSENGER/CREW AT R2 DOOR . REPLACED DAMPER EMERGENCY OPERATION CYLINDER OF THE PASSENGER/CREW AT R2 DOOR IAW A319 AMM 52-13-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,589 hrs · 13,692 cycles

SAL MAJOR REPAIR C7 CHECK NR 6141076, CORROSION ON CABIN SEAT TRACK AT FR 36 - FR 41, +Y1292. REPAIRED CABIN SEAT TRACK AT FR 36 - FR 41, +Y1292 IAW A319 SRM 51-72-11.

Part: PIN — CORRODED (RT MLG) · airframe 34,589 hrs · 13,692 cycles

SAL - C7 - MAJOR REPAIR - NR 6143508 - CORROSION ON REAR PINTLE PIN OF RIGHT MAIN LANDING GEAR. REPLACED REAR PINTLE PIN OF RIGHT MAIN LANDING GEAR IAW US AIRWAYS TASK CARD R4M3211.

Part: REPAIR — CORRODED (R2 SILL) · airframe 34,589 hrs · 13,692 cycles

SAL - C7 - MAJOR REPAIR - NR 6142505 - GALVANIC CORROSION ON EXISTING REPAIR AT SILL OF R2 DOOR, FR66, -Y1732. REPAIRED SILL IAW A319 SRM 53-41-14.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 34,589 hrs · 13,692 cycles

SAL - MAJOR REPAIR - C7 CHECK - NR 6142693, CORROSION ON SHEAR PLATE AT FR 54 - FR 55, S38L. REPLACED SHEAR PLATE AT FR 54 - FR 55, S38L IAW A319 SRM 51-72-11.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · airframe 34,589 hrs · 13,692 cycles

SAL MAJOR REPAIR C7 CHECK NR 6142503, CORROSION ON CABIN DUMMY RAIL AT FR 16, -Y1379. REPLACED CABIN DUMMY RAIL AT FR 16, -Y1379 IAW A319 SRM 51-72-11.

Part: ANCHOR FITTING — CORRODED (RT MLG) · airframe 34,589 hrs · 13,692 cycles

SAL C7 MAJOR REPAIR NR 6142519 CORROSION ON LOWER SURFACE OF RT MLG ANCHORAGE FITTING. REPAIRED RT MLG ANCHORAGE FITTING IAW US AIRWAYS EA NR 132186.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,589 hrs · 13,692 cycles

SAL - C7 - MAJOR REPAIR - NR 6142629 - GALVANIC CORROSION ON CABIN FLOORBEAM BETWEEN FR68 TO FR70, Y165. REPLACED CABIN FLOORBEAM BETWEEN FR68 TO FR70, Y165 IAW A319 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,589 hrs · 13,692 cycles

SAL - C7 - MAJOR REPAIR - NR 6142502 - GALVANIC CORROSION ON CABIN FLOORBEAM SEAT TRACK AT FR20, -Y1292. REPLACED CABIN FLOORBEAM SEAT TRACK AT FR20, -Y1292 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,589 hrs · 13,692 cycles

SAL C7 MAJOR REPAIR NR 6142389 GALVANIC CORROSION ON FLOOR BEAM BETWEEN FR64 TO FR66, Y1292. REPLACED FLOOR BEAM BETWEEN FR64 TO FR66, Y1292 IAW A319 SRM 51-72-11.

Part: BEAM — CORRODED (FUSELAGE) · airframe 34,589 hrs · 13,692 cycles

SAL MAJOR REPAIR C7 CHECK NR 6142380, CORROSION ON CABIN BEAM AT FR 66 - FR 68, -Y1167. REPLACED CABIN BEAM AT FR 66 - FR 68, -Y1167 IAW A319 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · airframe 34,589 hrs · 13,692 cycles

SAL - MAJOR REPAIR - C7 CHECK - NR 6142382, CORROSION ON R2 DOOR CUT OUT LOWER SILL AT FR 66 - FR 68, -Y1732. REPAIRED R2 DOOR CUT OUT LOWER SILL AT FR 66 - FR 68, -Y1732 IAW US AIRWAYS EA 132178.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 34,589 hrs · 13,692 cycles

SAL - C7 - MAJOR REPAIR - NR 6142383 - CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, -Y1732. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, -Y1732 IAW A319 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,589 hrs · 13,692 cycles

SAL - C7 - MAJOR REPAIR - NR 6142378 - GALVANIC CORROSION ON BEAM SEAT RAIL BETWEEN FR64 TO FR66, -Y1292. REPLACED BEAM SEAT RAIL BETWEEN FR64 TO FR66, -Y1292 IAW A319 SRM 51-72-11.

Part: BEAM — CORRODED (FUSELAGE) · airframe 34,589 hrs · 13,692 cycles

SAL MAJOR REPAIR C7 CHECK NR 6142387, CORROSION ON CABIN BEAM AT FR 68 - FR 69, +Y1292. REPLACED CABIN BEAM AT FR 68 - FR 69, +Y1292 IAW A319 SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 34,589 hrs · 13,692 cycles

SAL - MAJOR REPAIR - C7 CHECK - NR 6142386, CRACKED SHEAR PLATE AT FR 68 - FR 69, +Y1732. REPLACED SHEAR PLATE AT FR 68 - FR 69, +Y1732 IAW A319 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,589 hrs · 13,692 cycles

SAL - C7 - MAJOR REPAIR - NR 6142384 - GALVANIC CORROSION ON BEAM SEAT RAIL BETWEEN FR64 TO FR66, Y765. REPLACED BEAM SEAT RAIL BETWEEN FR64 TO FR66, Y765 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,589 hrs · 13,692 cycles

SAL - MAJOR REPAIR - C7 CHECK - NR 6142381, CORROSION ON CABIN BEAM AT FR 67 - FR 69, -Y1165. REPLACED BEAM AT FR 67 FR 69, -Y1165 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,589 hrs · 13,692 cycles

SAL MAJOR REPAIR C7 CHECK NR 6142388, CORROSION ON CABIN BEAM AT FR 66 - FR 68, +Y1292. REPLACED CABIN BEAM AT FR 66 - FR 68, +Y1292 IAW A319 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 34,589 hrs · 13,692 cycles

SAL - C7 - MAJOR REPAIR - NR 6142385 - GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, Y1732. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, Y1732 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,589 hrs · 13,692 cycles

SAL - C7 - MAJOR REPAIR - NR 6142390 - GALVANIC CORROSION ON CABIN FLOORBEAM BETWEEN FR66 TO FR70, Y765. REPLACED CABIN FLOORBEAM BETWEEN FR66 TO FR70, Y765 IAW A319 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,589 hrs · 13,692 cycles

SAL MAJOR REPAIR C7 CHECK NR 6141071, CORROSION ON CABIN SEAT TRACK AT FR 32 - FR 35, +Y765. REPAIRED CABIN SEAT TRACK AT FR 32 - FR 35, +Y765 IAW A319 SRM 53-21-15.

Part: HINGE FITTING — WORN (VERTICAL STAB) · airframe 34,589 hrs · 13,692 cycles

SAL - MAJOR REPAIR - C7 CHECK - NR 6141112, NR 5 RUDDER HINGE FITTING AT VERTICAL STABILIZER STATION 2985 / RIB7 HAS EXCESSIVE PLAY. REPLACED NR 5 RUDDER HINGE FITTING AT VERTICAL STABILIZER STATION 2985 / RIB7 IAW A319 AMM 55-36-41.

Part: HINGE FITTING — WORN (VERTICAL STAB) · airframe 34,589 hrs · 13,692 cycles

SAL - MAJOR REPAIR - C7 CHECK - NR 6141111, NR 4 RUDDER HINGE FITTING AT VERTICAL STABILIZER STATION 2632 / RIB6 HAS EXCESSIVE PLAY. REPLACED NR 4 RUDDER HINGE FITTING AT VERTICAL STABILIZER STATION 2632 / RIB6 I/A/W A319 AMM 55-36-41.

Part: FITTING — WORN (RUDDER) · airframe 34,589 hrs · 13,692 cycles

SAL C7 MAJOR REPAIR NR 6141110 EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 3 AT HORIZONTAL STABILIZER STATION 2279. REPLACED RUDDER HINGE FITTING NR 3 AT HORIZONTAL STABILIZER STATION 2279 IAW A319 AMM 55-36-41.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 34,490 hrs · 13,650 cycles

FLT 160 - PHX-LAS - EEL - AFT RECHARGEABLE EMERGENCY FLASHLIGHT HAS DEAD BATTERY. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 34,384 hrs · 13,599 cycles

LOGPAGE:4327505 - FLT#700 - PHX-SEA - EEL - AISLE EMERGENCY LIGHT AT ROW 10R IS INOPERATIVE. FOUND EMERGENCY LIGHT AT ROW 10R TO BE UNPLUGGED. RECONNECTED PLUG. OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,517 hrs · 13,226 cycles

FLT 0573-SFO-LAS-EEL - EMERGENCY EXIT LIGHT OVERWING CEILING (AFT FACING) AND ACFT LT SIDEWALL INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY UNIT. OPERATIONAL CHECK WAS GOOD. (S)

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 29,329 hrs · 11,499 cycles

SAL - CORROSION ON CABIN FLOORBEAM, FR 67 + 13", -Y1192. REPLACED CABIN FLOOR BEAM, FR 66 - FR 68, -Y1192 IAW A319 SRM 51-72-11.

Part: DAMPER — BROKEN (ZONE 200) · airframe 29,329 hrs · 11,499 cycles

SAL - EES - BROKEN ASSIST DAMPER ASSEMBLY ON R1 DOOR, FR 16 - FR 20. REPLACED ASSIST DAMPER ASSEMBLY ON R1 DOOR, FR 16 - FR 20 IAW A319 AMM 52-11-14. [06-19-07] REMOVED INFORMATION FROM STRUCTURE CAUSING DIFFICULTY SECTION SINCE DEFECTIVE ITEM IS NOT A STRUCTURAL ITEM AND MADE CORRECTIONS TO THE PROBLEM DESCRIPTION SECTION.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 29,329 hrs · 11,499 cycles

SAL - CORROSION ON CABIN FLOORBEAM, FR 67 + 18", -Y1162. REPLACED CABIN FLOOR BEAM, FR 68 - FR 69, -Y1162 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 29,329 hrs · 11,499 cycles

SAL - CORROSION ON CABIN FLOORBEAM, FR 69 + 19", -Y254. REPLACED CABIN FLOOR BEAM, FR 68 - FR 70, -Y254 IAW A319 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (ZONE 200) · airframe 29,329 hrs · 11,499 cycles

SAL - FOUND CORROSION ON CABIN SHEAR PLATE, FR 69 - FR 70, -Y1162. REPLACED CABIN SHEAR PLATE, FR 69 - FR 70, -Y1162 IAW A319 SRM 51-72-11.

Part: SILL — CORRODED (ZONE 200) · airframe 29,329 hrs · 11,499 cycles

SAL - CORROSION ON R2 DOOR LOWER SILL, FR 67 + 19", -Y1230. REPAIRED R2 DOOR LOWER SILL, FR 67 + 19", -Y1230 IAW A319 SRM 53-41-14.

Part: FITTING — CORRODED (ZONE 200) · airframe 29,329 hrs · 11,499 cycles

SAL - CORROSION ON L1 DOOR LOWER SILL CENTER FITTING, FR 16 - FR 20, -Y1732. REPLACED L1 DOOR LOWER SILL CENTER FITTING, FR 16 - FR 20, -Y1732 IAW A319 SRM 51-72-11.

Part: SLEEVE — CRACKED (ESCAPE SLIDE) · airframe 29,329 hrs · 11,499 cycles

SAL - EES - RIGHT OVERWING EMERGENCY EXIT SLIDE RESERVOIR CONNECTION SLEEVE CRACKED. REPLACED AND OPERATIONAL CHECKED RIGHT OVERWING EMERGENCY EXIT SLIDE RESERVOIR IAW A319 AMM 25-62-46.

Part: BLEED VALVE — FAILED (ENGINE) · airframe 27,548 hrs · 10,730 cycles

LAS - IN CRUISE, AT FLT LEVEL 390 IN LIGHT OCCASIONAL MODERATE TURBULENCE. THE CREW HEARD A LOUD COMPRESSOR STALL, ACCOMPANIED BY ECAM ENG 2 STALL MSG. NO ABNORMAL ENGINE PARAMETERS. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO SEA. THE LANDING WAS UNEVENTFUL. MAINTENANCE PERFORMED TROUBLESHOOTING PER TSM 71-00-00-810-809, FOUND 7TH(B) STAGE BLEED VALVE FAILING FUNCTIONAL TEST PER AMM 75-32-52-700-011. MAINTENANCE REPLACED THE 7TH (B) STAGE VALVE PER AMM 75-32-52 (TQ0058,TQ0212). PERFORMED POWER ASSURANCE RUN PER TC F5M71312. OPS CHECK WAS GOOD.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 22,689 hrs · 8,689 cycles

LAS - EEL - DURING GROUND HANDLING IN LAS, TECH DISCOVERED THE FORWARD FLIGHT ATTENDANT'S JUMPSEAT FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLASHLIGHT BATTERY AS REQUIRED.

Part: ADIRU — FAILED (NR 2) · airframe 22,210 hrs · 8,529 cycles

DURING TAKEOFF RECEIVED MULTIPLE FAULTS BEGINNING TAKE OFF ROLL. ACFT ABORTED T/O & RETURNED TO GATE WITHOUT INCIDENT. MX R & R FAC 1 IAW AMWEST TASK CARD R2A22301. OPS TESTS GOOD. ATTEMPTED ANOTHER TAKEOFF & RECEIVED AUTO FLT RUD TRV LIM SYS ECAM MSG DURING TAKEOFF ROLL. AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MX R & R NR 2 ADIRU IAW AMERICA WEST AIRLINES TASK CARD R2A34304. OPS TESTS GOOD. VENDOR TEAR DOWN REPORT CONFIRMS FAILURE. VENDOR INCOMING TESTS SHOWS PRIMARY FAULT OF GYRO. GYRO WAS REPLACED WITH ALL WORK AND OPERATIONAL TESTS BEING DONE IAW AT261847-01, CMM TP1011 REV 24.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 19,986 hrs · 7,726 cycles

PHX - EEL - DURING E-04 CHECK THE LT OVERWING EMERGENCY POWER SUPPLY UNIT WAS FOUND TO HAVE AN INTERNAL FAILURE. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 19,877 hrs · 7,685 cycles

LAX - EEL - DURING 8-DAY CHECK FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM, FOUND THE LT OVERWING EMERGENCY POWER SUPPLY UNIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 19,553 hrs · 7,565 cycles

DURING 4-DAY CHECK, OPERATIONAL TEST OF THE EMERGENCY LIGHT SYSTEM FOUND THE LT OVERWING EMERGENCY POWER SUPPLY UNIT FAULTED. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD.

Part: COMPUTER — MALFUNCTIONED (ZONE 120) · airframe 18,683 hrs · 7,280 cycles

EN ROUTE, FLT MANAGEMENT GUIDANCE COMPUTER NR 1 FAILED AND FMGC NR 2 FAULTED, FIRST OFFICER LOST MAP DISPLAY 3 TIMES, DIVERTED TO CMH & LANDED WITHOUT FURTHER DIFFICULTY. MX R & R FMGC NR 1 IAW T/C R2A22302, PERFORMED OPS TEST OF FMGC NR 1 & 2, BOTH CHECK GOOD. FUNCTIONAL TEST OF FMGC CONFIRMED REASON FOR REMOVAL, UNIT FAILED FREQUENCY MODULATION (FM) TESTS ON AUTOMATIC TEST EQUIPMENT. R & R A51 PROCESSOR CIRCUIT BOARD (PCB) (P/N E12843AC02) FOR (FM) TEST FAILURE, A52 PCB & A53 PCB FOR FM DBP & FM MP BITE DATA FAILURES, & FG EEPROMS FOR ARINC FAILURE. UNIT REPAIRED AND TESTED IAW CMM.

Part: EPSU — FAILED (ZONE 221) · airframe 20,745 hrs · 8,543 cycles

PHX - EEL - DURING E-01 CHECK THE FORWARD LT EMERGENCY POWER SUPPLY UNIT FAULTED. MAINTENANCE REMOVED AND REPLACED FORWARD LT EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 18,133 hrs · 7,084 cycles

DURING B-04 CHECK FOUND FLOOR PANEL 262BG MISSING AN INSERT WITH DELAMINATION TO BOTTOM OF LAMINATE. MAINTENANCE REPLACED INSERT AND PERFORMED BOND REPAIR TO BOTTOM LAMINATE OF FLOOR PANEL 262BG IAW SRM 53-02-00, FIG. 201.

Part: FLOORBEAM — CORRODED (CORRODED) · airframe 18,133 hrs · 7,084 cycles

DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 FROM FR 67 TO FR 68. MAINTENANCE REMOVED AND REPLACED BEAM Y765 FROM FR 67 TO FR 68 IAW SRM 51-42-11 FIG. 9-12, AND 18.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 18,133 hrs · 7,084 cycles

DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 AT FR 66. MAINTENANCE REMOVED AND REPLACED BEAM Y765 AT FR 66 IAW A319 SRM 51-72-11 PG. 1 AND 2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,133 hrs · 7,084 cycles

DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT AFT OF FR 66. MAINTENANCE REMOVED BEAM Y1292 RT FROM FR 64 TO FR 66+5 INCH; FABRICATED A NEW REPLACEMENT BEAM; DRILLED SPLICE COUPLING TO FORWARD END OF NEW BEAM; INSTALLED NEW BEAM NR COUPLING IAW A319 SRM 51-42-11, FIG. 9-17.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 18,133 hrs · 7,084 cycles

DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 AT FR 68. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 AT FR 68 IAW SRM 51-42-11 FIG. 2, 3, AND 18.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,133 hrs · 7,084 cycles

DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT AFT OF FR 66 TO FORWARD SIDE OF FR 68. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 LT FROM FR 66 TO FR 68 IAW A319 SRM 51-42-11, FIG. 2, 3, & 18.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 18,133 hrs · 7,084 cycles

DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 (2 PLACES) AT FR 64 AND FR 65. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 FROM FR 64 TO FR 65 IAW A319 SRM 51-42-11 FIG. 2, 3, 8, 18.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 18,133 hrs · 7,084 cycles

MAJOR REPAIR, DURING B-04 CHECK FOUND 2 EACH 1INCH CRACKS IN FLOOR PANEL 221EF. MAINTENANCE CUTOUT DAMAGE IN FLOOR PANEL 221EF, AND PERFORMED BOND REPAIR IAW A319 SRM 53-02-00, FIG. 202.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,133 hrs · 7,084 cycles

DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 AT FR 66. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 AT FR 66 IAW A319 SRM 51-42-11 PG. 6, 7, & 41, FIG. 18. REGISTRATION NR WAS CHANGED TO REFLECT THE CORRECT AIRCRAFT, THIS EVENT DID NOT OCCUR ON A/C 160.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 18,133 hrs · 7,084 cycles

DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1732 AT FR 66. MAINTENANCE REPAIRED BEAM Y1732 DOOR SILL AT FR 66 IAW A319 SRM 53-41-14 FIG. 201.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,133 hrs · 7,084 cycles

DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 BETWEEN FR 64 AND FR 66. MAINTENANCE REMOVED AND REPLACED BEAM Y765 FROM FR 64 TO FR 66 IAW A319 SRM 51-42-11 PG. 39 AND 41 FIG. 18.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,133 hrs · 7,084 cycles

DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 AT FR 68. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 AT FR 68 IAW A319 SRM 51-42-11 FIGURES 2-18.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 18,133 hrs · 7,084 cycles

DURING B-04 CHECK FOUND CORROSION ON AFT SIDE CORNER OF FLOOR PANEL 261FF FROM FR 66 TO FR 68, AND Y1292 LT TO 1732 LT. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 261FF IAW AWA T/C C1D25310.

Part: PLATE — CORRODED (DOOR SILL) · corrosion level 2 · airframe 18,133 hrs · 7,084 cycles

DURING B-04 CHECK CORROSION (4 SPOTS) WAS FOUND ON AFT CARGO DOOR SILL PLATE. MAINTENANCE REMOVED AND FABRICATED A NEW AFT CARGO DOOR SILL PLATE IAW A319 SRM 51-42-11 FIGURES 3,4,5,9 AND MFG DRAWING 17D53477153.

Part: BATTERY PACK — DISCHARGED (ZONE 241) · airframe 18,248 hrs · 7,117 cycles

PHX - EEL - DURING 4-DAY CHECK THE LT OVERWING EMERGENCY BATTERY PACK AT EMERGENCY POWER SUPPLY UNIT (11WL) FAILS PUSH BUTTON TEST. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD.

Part: COMPUTER — FAULTY (ZONE 121) · airframe 17,777 hrs · 6,982 cycles

EN ROUTE, RECEIVED ECAM MESSAGE FOR ANTI-ICE LT WINDOW THEN HEARD A LOAD NOISE AS LT AFT SIDE WINDOW SHATTERED, PRESSURE WAS NOT LOST, DIVERTED TO GJT. MAINT R & R LT AFT SIDE WINDOW IAW AMM 56-11-12, & REPLACED LT WINDOW HEAT COMPUTER IAW AMM 30-42-34. OPS CHK OF WINDOW HEAT CONTROL UNIT GOOD. FUNCTIONAL CHECK OF WINDOW HEAT COMPUTER S/N 4160031800258 WAS NO FAULT FOUND. UNIT TESTED IAW CMM 30-42-36.

Part: SOLENOID VALVE — LOOSE (NR 1 ENGINE) · airframe 15,637 hrs · 6,237 cycles

DURING CLIMB OUT OF CMH EN ROUTE FOR LAS RECEIVED NR 1 ENGINE SYSTEM FAULT AT 6000 FT, EGT AT 617 DEGREES, PLACED NR 1 ENGINE THRUST LEVER TO IDLE AND MAINTAINED 567 DEG EGT UNTIL LANDING AND SHUTDOWN. MAINTENANCE FOUND THE 10TH STAGE BLEED SOLENOID VALVE BOTTOM PLATE LOOSE AT CONNECTOR, REMOVED AND REPLACED 10TH STAGE BLEED SOLENOID VALVE IAW AMM 75-23-52, ALSO REPLACED IGNITION RELAY BOX. OPS CK NR 1 ENG GOOD, NO DEFECTS NOTED. FUNCTIONAL CHECK OF IGNITION BOX S/N 2151 WAS NO FAULT FOUND, UNIT TESTED GOOD UNDER ALL TEMPERATURES. VENDORS FUNCTIONAL TEST OF 10TH STAGE BLEED SOLENOID VALVE CONFIRMED FAILURE OF UNIT. PISTON SEALS FOUND WORN & PISTON SEALING SURFACE WAS DAMAGED BEYOND REPAIR.

Part: BATTERY — DISCHARGED (ZONE 900 - LAVAT) · airframe 15,583 hrs · 6,215 cycles

EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT LT EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LT EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 14,305 hrs · 5,708 cycles

FLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT IN THE AFT CABIN WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (ZONE 242) · airframe 13,905 hrs · 5,546 cycles

PHX - EEL - FLIGHT CREW REPORTED THE RT OVERWING EMERGENCY EXIT LIGHT WAS FLASHING ON AND OFF. MAINTENANCE REMOVED AND REPLACED THE RT OVERWING EMERGENCY POWER SUPPLY UNIT BATTERY PACK, OPERATIONAL CHECK WAS GOOD.

Part: BOTTLE — DISCHARGED (ZONE 125) · airframe 13,880 hrs · 5,539 cycles

OMA - DIVERSION - FLT 0012 - APPROXIMATELY 1 HOUR AND 30 MINUTES INTO FLIGHT EN ROUTE FROM PHX TO JFK CREW OXYGEN WENT DOWN TO 20 PSI AND REGULATOR PRESSURE WAS LOW, FLIGHT DIVERTED TO OMA. EMERGENCY OXYGEN SWITCH WAS STUCK IN 100 PERCENT POSITION AFTER GROUND TEST, MASK WAS NOT STOWED PROPERLY CAUSING OXYGEN TO DEPLETE. CONTRACT MAINTENANCE REMOVED AND REPLACED CREW OXYGEN BOTTLE IAW T/C S2A35301, PERFORMED LEAK CHECK, NO LEAKS NOTED.

Part: BATTERY — DISCHARGED (ZONE 221) · airframe 13,598 hrs · 5,432 cycles

DURING INSPECTION THE FORWARD LT EMERGENCY POWER SUPPLY LOAD WAS FOUND INOPERATIVE ON FLIGHT ATTENDANT PANEL. MAINTENANCE REMOVED AND REPLACED THE BATTERY AT FORWARD LT EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD.

Part: FILTER — CONTAMINATED (ZONE 130) · corrosion level 0 · airframe 13,095 hrs · 5,249 cycles

PHX - AIR TURN BACK - FLT 0001 - ON TAKEOFF FROM PHX EN ROUTE FOR ORD FUMES WERE NOTICED IN MID-CABIN, TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE PERFORMED POWER RUN AT ALL SETTINGS ISOLATING THE NO.1 AND NO. 2 ENGINES BLEEDS AND APU BLEED, UPON INSPECTION FOUND RE-CIRCULATION FAN FILTERS DIRTY. REMOVED AND REPLACED BOTH FILTERS.

Part: BOTTLE — DISCHARGED (OXYGEN SYS) · airframe 13,080 hrs · 5,245 cycles

FLT 0820 - WHILE EN ROUTE FROM BOS TO PHX CREW OXYGEN WENT TO ZERO, DIVERTED TO ROC. MAINTENANCE REMOVED AND REPLACED THE CREW OXYGEN BOTTLE IAW AWA T/C R2A35301. PERFORMED LEAK CHECK OF ALL CONNECTIONS AT BOTTLE, ALSO CHECK ALL MASKS FOR CORRECT STOWAGE AND LEAKS, NO LEAKS NOTED DURING 2 HOUR PERIOD.

Part: APU — MALFUNCTIONED (APU BAY)

TAILPIPE FIRE, AFTER (APU) SHUT DOWN, A TAILPIPE FIRE WAS NOTICED BY GROUND CREW. MAINTENANCE INSPECTED THE APU AND FOUND NO DAMAGE TO TAILPIPE OR SURROUNDING AREA. PLACED SYSTEM ON MEL, COND. 1.

Part: FMC — MALFUNCTIONED (COCKPIT) · airframe 12,326 hrs · 4,984 cycles

FLT 0822 - EN ROUTE FROM PHX TO BOS FT MANAGEMENT GUIDANCE COMPUTER (FMGC) NR 2 FAILED, DIVERTED TO CMH AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE FMGC NR 2 IAW AWA; NAV DATA UPLOADED IAW T/C A1B34321. FUNCTIONAL TEST GOOD. UNIT CHECKED AND NO PROBLEMS FOUND. RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 11,379 hrs · 4,615 cycles

LAS - EMERGENCY LIGHT HARNESS SEAT ROW 9 RT HAS A BROKEN WIRE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT HARNESS AT SEAT ROW 9 RT, OPERATIONAL CHECK OF LIGHTING SYSTEM CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 10,567 hrs · 4,312 cycles

PHX - EMERGENCY EQUIPMENT - F/A REPORTED THAT THE AFT EMERGENCY FLASHLIGHT NEAR THE RIGHT AFT F/A JUMPSEAT IS INOPERATIVE. MAINTENANCE REPLACED BATTERIES IN THE EMERGENCY FLASHLIGHT AT THE AFT F/A JUMPSEAT.

Part: CABLE — BROKEN (SEAT ROW 12 L/H) · corrosion level 0 · airframe 10,296 hrs · 4,212 cycles

PHX - EEL - DURING INSPECTION EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 12 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE FOR EMERGENCY ESCAPE PATH SEAT LIGHT AT SEAT ROW 12 L/H, OPERATIONAL CHECK GOOD.

Part: PRESSURE SWITCH — CRACKED (NR 1 ENGINE) · airframe 10,227 hrs · 4,181 cycles

LAX - ABORTED TAKEOFF - FLT 0694 - AT APPROXIMATELY 60 KTS ON TAKEOFF ROLL OUT OF LAX BOUND FOR CMH RECEIVED GREEN HYDRAULIC SYSTEM NR 1 ENGINE PUMP LOW PRESSURE INDICATION, T/O WAS REJECTED AND AIRCRAFT RETURNED TO GATE. AT GATE MAINTENANCE FOUND THE NR 1 ENGINE HYDRAULIC PRESSURE SWITCH CRACKED, THE SWITCH WAS REMOVED AND REPLACED IAW AMM 29-11-17-000-010, OPERATIONAL CHECK WAS GOOD.

Part: CABLE — BROKEN (SEAT ROW 10 R/H) · airframe 9,731 hrs · 3,972 cycles

PHX - EEL - EMERGENCY ESCAPE PATH EXIT LIGHT WILL NOT ILLUMINATE AT SEAT ROW 10 R/H. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH EXIT LIGHT HARNESS AT SEAT ROW 10 R/H IAW ESPM 20-53-20.

Part: CONTROL CABLE — STUCK (LT MLG DOOR)

LEFT GEAR DOOR LIGHT REMAINS ILLUMINATED AFTER GEAR RETRACTION. FOUND ALT RELEASE CABLE FOR AFT DOORS HUNG UP ON FWD DOOR ACTUATOR. ROUTED CABLE CORRECTLY AND ADJUSTED FWD DOOR. PROX SWITCH RETRACTION CHECK GOOD. ACFT RETURNED TO SERVICE. ACTC: 12971. (X)