N827AW

Part: CONNECTOR — LOOSE (ZONE 200) · airframe 73,064 hrs · 34,937 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT AT ROW 27 ABC INOPERATIVE. MAINTENANCE FOUND EMERGENCY LIGHT CONNECTOR 7260VC LOOSE, AT ROW 27, CONNECTED EMERGENCY LIGHT CONNECTOR IAW WDM 33-51-08. OPS CHECK GOOD IAW AMM 33-51-00.

Part: BATTERY — NO TEST (ZONE 200) · airframe 72,524 hrs · 34,624 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD FA FLASHLIGHT DOES NOT TEST PROPERLY. MAINTENANCE REPLACED BATTERY AND PLASTIC EMERGENCY USE ONLY BAND IAW AMM 25-65-00.

Part: OVEN — CONTAMINATED (ZONE 900) · airframe 71,584 hrs · 33,974 cycles

AIRCRAFT WAS NOT GROUNDED: FA REPORTS BURNING SMELL COMING FROM FWD RIGHT OVEN (98-06-10861). WE COULD SMELL IT IN THE COCKPIT AS WELL. OVEN CONFIRMED AS SOURCE CB COLLARD. **SUPPLEMENTAL REPORT FOR SDR AALA202506162806.** (CLOSED)** MAINTENANCE FOUND BURNED FOOD AT BOTTOM RACK CLEANED AND OPS CK GOOD IAW AMM 25-35-19.

Part: OVEN — ODOR (ZONE 900) · airframe 71,584 hrs · 33,974 cycles

AIRCRAFT WAS NOT GROUNDED: FA REPORTS BURNING SMELL COMING FROM FWD RIGHT OVEN (98-06-10861). WE COULD SMELL IT IN THE COCKPIT AS WELL. OVEN CONFIRMED AS SOURCE CB COLLARD. (OPEN)

Part: ACCUMULATOR — READS LOW (ZONE 800) · airframe 71,429 hrs · 33,863 cycles

AIRCRAFT WAS NOT GROUNDED: AFT R/H PASSENGER/CREW DOOR EMERGENCY CYLINDER/ACCUMULATOR REQUIRES SERVICING (READS 1350PSI AT 50 DEGREES FAHRENHEIT). MAINTENANCE SERVICED AFT R/H PASSENGER/CREW DOOR EMERGENCY CYLINDER/ACCUMULATOR TO 1700PSI AT 50 DEGREES FAHRENHEIT IAW AMM 52-10-00.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 69,128 hrs · 32,406 cycles

AIRCRAFT WAS GROUNDED: DURING PS CHECK FOUND IN SEAT EMERGENCY LIGHTS ON ROWS 22 AND 23ABC INOPERATIVE. ACCOMPLISHED BUILT IN TEST EQUIPMENT CHECK OF EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-00. FOUND INTERNAL LOAD FAULT MESSAGE FOR EMERGENCY POWER SUPPLY UNIT. INSPECTED WIRING AND FOUND BROKEN WIRE AT ROW 23 AT CONNECTOR 72BC8. ACCOMPLISHED SPLICE REPAIR PER ESPM 20-43-11.

Part: SWITCH — DEFECTIVE (EMERGENCY LIGHTS) · airframe 68,838 hrs · 32,204 cycles

AIRCRAFT WAS GROUNDED: CABIN EMERGENCY LIGHTS ALL ILLUMINATED IN THE ARM POSITION. FLIGHT CREW RESET PER MOC UNSUCCESSFUL. MAINTENANCE REPLACED FLIGHT DECK EMERGENCY LIGHT SWITCH 4WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: CIDS — FAULTY (ZONE 100 - FUSE) · airframe 68,026 hrs · 31,680 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT ADVISED THAT THE EMERGENCY LIGHTS GO ON AND OFF PERIODICALLY DURING THE FLIGHT. REPLACED CIDS DIRECTOR PER AMM 31-32-34.

Part: RELAY — FAULTY (EMERGENCY LIGHTS) · airframe 68,229 hrs · 31,805 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT ADVISED EMERGENCY LIGHTS WERE INTERMITTENT THROUGHOUT ENTIRE CABIN. REPLACED RELAY (8WL) ((AALA202401248428)), DIODE (1158VD) ((AALA202401244430)) AND SWITCH (4WL) ((AALA202401245878)). PERFORMED SATISFACTORY OPERATIONAL TEST OF THE EMERGENCY LIGHT SYSTEM PER AMM 33-51-00-710-001.

Part: DIODE — FAULTY (EMERGENCY LIGHTS) · airframe 68,229 hrs · 31,805 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT ADVISED EMERGENCY LIGHTS WERE INTERMITTENT THROUGHOUT ENTIRE CABIN. REPLACED RELAY (8WL) ((AALA202401248428)), DIODE (1158VD) ((AALA202401244430)) AND SWITCH (4WL) ((AALA202401245878)). PERFORMED SATISFACTORY OPERATIONAL TEST OF THE EMERGENCY LIGHT SYSTEM PER AMM 33-51-00-710-001.

Part: SWITCH — FAULTY (EMERGENCY LIGHTS) · airframe 68,229 hrs · 31,805 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT ADVISED EMERGENCY LIGHTS WERE INTERMITTENT THROUGHOUT ENTIRE CABIN. REPLACED RELAY (8WL) ((AALA202401248428)), DIODE (1158VD) ((AALA202401244430)) AND SWITCH (4WL) ((AALA202401245878)). PERFORMED SATISFACTORY OPERATIONAL TEST OF THE EMERGENCY LIGHT SYSTEM PER AMM 33-51-00-710-001.

Part: LEVER — STICKING (ZONE 800 - DOORS) · airframe 67,922 hrs · 31,626 cycles

AIRCRAFT WAS GROUNDED: L2 WILL NOT ARM THE SLIDE. MAINTENANCE LUBRICATED THE L2 DOOR SLIDE ARMING LEVER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: WIRE — BROKEN (ZONE 200 - FUSE) · airframe 67,547 hrs · 31,397 cycles

AIRCRAFT WAS NOT GROUNDED: ROW 22 ABC AND ROW 23 ABC SEAT MOUNTED ESCAPE LIGHTING INOPERATIVE. REPAIRED BROKEN WIRE AT CONNECTORY 7260VC10.

Part: HINGE — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 67,531 hrs · 31,392 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR DIFFICULT TO OPEN/CLOSE IN FLIGHT, RUBBING ON BOTTOM. ADJUSTED FORWARD LAVATORY DOOR HINGE.

Part: DOOR — STUCK (ZONE 900 - LAV/G) · airframe 67,411 hrs · 31,327 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR DIFFICULT TO OPEN/CLOSE. REMOVED AND REINSTALL LAVATORY DOOR.

Part: DOOR — LACK OF LUBE (ZONE 900 - LAV/G) · airframe 67,320 hrs · 31,259 cycles

AIRCRAFT WAS NOT GROUNDED: FRONT LAVATORY DOOR HARD TO OPEN / CLOSE. CLEANED AND LUBED DOOR.

Part: HINGE ARM — WORN (ZONE 300 - STABS) · airframe 66,976 hrs · 31,040 cycles

AIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILZER #4 RUDDER HINGE ARM LOWER MIDDLE FASTENER HOLE IS WORN / OBLONGED AT STATION 263 AND RIB 6. REPLACED HINGE ARM PER SRM 55-36-42.

Part: DOOR FRAME — LOOSE (ZONE 900 - LAV/G) · airframe 66,469 hrs · 30,736 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR STICKS. MAINTENANCE TIGHTENED FORWARD LAVATORY DOOR FRAME AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: POWER SUPPLY — NO TEST (ZONE 200 - FUSE) · airframe 65,992 hrs · 30,417 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT 10WL BATTERY FAILED SYSTEM TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 10WL PER AMM 33-51-38 AND ACCOMPISHED A SATISFACTORY OPERATIONAL CHECK.

Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 65,884 hrs · 30,338 cycles

AIRCRAFT WAS NOT GROUNDED: FIRST CLASS LAVATORY DOOR HARD TO OPEN AND CLOSE. MAINTENANCE LUBRICATED AND ADJUSTED LAVATORY DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: PRESSURE SWITCH — INOPERATIVE (FUEL SYSTEM) · airframe 65,467 hrs · 30,078 cycles

AIRCRAFT WAS NOT GROUNDED: APU FUEL LOW PRESSURE. MAINTENANCE PERFORMED TSM 28-22-00-810-801-A AND FOUND APU FUEL PRESSURE SWITCH INOPERATIVE. REPLACED APU FUEL PRESSURE SWITCH PER AMM 28-22-15 AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK.

Part: DOOR — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 64,989 hrs · 29,770 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR DIFFICULT TO OPEN. MAINTENANCE ADJUSTED FLIGHT DECK DOOR PER AMM 52-50-00.

Part: HINGE — LACK OF LUBE (ZONE 900 - LAV/G) · airframe 64,236 hrs · 29,333 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR DIFFICULT TO OPEN AND CLOSE. LUBRICATED DOOR HINGE (AALA202207138695) AND LATCHES (AALA202207135288) PER AMM 25-40-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: LATCH — LACK OF LUBE (ZONE 900 - LAV/G) · airframe 64,236 hrs · 29,333 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR DIFFICULT TO OPEN AND CLOSE. LUBRICATED DOOR HINGE (AALA202207138695) AND LATCHES (AALA202207135288) PER AMM 25-40-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: HINGE — STICKING (ZONE 800 - DOORS) · airframe 64,137 hrs · 29,269 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR - DIFFICULT TO OPEN AND CLOSE IN FLIGHT. APPEARS TO BE MISALIGNED IN FLIGHT PINS AND PLATES DO NOT LINE UP. LUBED HINGE AND LATCH ASSEMBLY CHECKS GOOD ON GROUND.

Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 64,131 hrs · 29,264 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR STICKS IN FLIGHT (ABOVE 10,0000) DOOR JAMMED. MAINTENANCE ADJUSTED FORWARD LAVATORY DOOR AS REQUIRED.

Part: LAMP — BURNED OUT (ZONE 200 - FUSE) · airframe 63,479 hrs · 28,882 cycles

AIRCRAFT WAS NOT GROUNDED: AISLE EXIT SIGN BETWEEN AFT LAVATORIES HALF OF THE LIGHTS ARE OUT. RELAMPED AISLE EXIT SIGN BETWEEN AFT LAVATORIES AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-17-400-001A.

Part: LAMP — BURNED OUT (ZONE 200 - FUSE) · airframe 63,479 hrs · 28,882 cycles

AIRCRAFT WAS NOT GROUNDED: AISLE EXIT SIGNS AT WINDOW EXIT HALF OF THE LIGHTS ARE OUT. RELAMPED AISLE EXIT SIGN AT WINDOW EXIT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-17-400-001A.

Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 62,623 hrs · 28,384 cycles

AIRCRAFT WAS NOT GROUNDED: 1ST CLASS LAVATORY DOOR STICKS. ADJUSTED LAVATORY DOOR PER AMM 25-40-00.

Part: BRAKE — OVERTEMP (NR 4) · airframe 61,286 hrs · 27,651 cycles

AIRCRAFT WAS GROUNDED: ON TAKE OFF BRAKE NUMBER 4 REACHED 350 DEGREES CELSIUS. LOW SPEED ABORT, LESS THAN 80 KNOTS. ACCOMPLISHED SATISFACTORY OPERATIONS CHECK OF NORMAL BRAKING SYSTEM PER AMM 32-42-00.

Part: LAMP — INOPERATIVE (EMERGENCY SIGN) · airframe 60,888 hrs · 27,454 cycles

AIRCRAFT WAS NOT GROUNDED: R4 EXIT SIGN HAS MULTIPLE LAMPS INOPERATIVE. REMOVED REPLACED AND PERFORMED SATISFACTORY OPERATIONS CHECK OF RIGHT EXIT SIGN PER A320 AMM 33-51-16-000-001.

Part: SIGN — INOPERATIVE (CABIN) · airframe 60,888 hrs · 27,454 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD OVERHEAD EXIT SIGN IS VERY DIM. REMOVED AND REPLACED AND PERFORMED SATISFACTORY OPERATIONS CHECK OF FORWARD OVER WING EXIT SIGNS PER A320 AMM 33-51-16.

Part: LAMP — INOPERATIVE (EMERGENCY SIGN) · airframe 60,888 hrs · 27,454 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT OVER WING EXIT SIGN HAVE MULTIPLE LAMPS INOPERATIVE. REMOVED REPLACED AND PERFORMED SATISFACTORY OPERATIONS CHECK OF RIGHT OVER WING EXIT SIGN PER AMM 33-51-16.

Part: SIGN — INOPERATIVE (LT OVERWING) · airframe 60,888 hrs · 27,454 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT OVER WING EXIT SIGN HAVE MULTIPLE LAMPS INOPERATIVE. REMOVED REPLACED AND PERFORMED SATISFACTORY OPERATIONS CHECK OF LEFT OVER WING EXIT SIGN PER AMM 33-51-16.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 59,974 hrs · 26,966 cycles

AIRCRAFT WAS NOT GROUNDED: FLOOR EXIT SIGN BY FLIGHT ATTENDANT JUMPSEAT MISSING. INSTALLED NEW EMERGENCY LIGHT LENS COVER PER AMM 33-50-00.

Part: SWITCH — BURNED (COCKPIT) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE - COCKPIT OVERHEAD PANEL, 40VU, YELLOW ELECTRIC PUMP (3804GX)PUSHBUTTON SWITCH BURNED. REPLACED PUSHBUTTON SWITCH 3804GX IN OVERHEAD PANEL 40VU PER ESPM 20-45-11, AND PERFORMED OPERATIONAL TEST OF HYDRAULIC YELLOW ELECTRIC PUMP PER AMM 29-24-00-863-001-A, TESTED OK.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CABIN FLOOR PANEL 222CF DELAMINATED. REPLACED FLOOR PANEL PER TASK CARD 26C22053014.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CABIN FLOOR PANEL 232EF DELAMINATED REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CABIN FLOOR PANEL 262BG DELAMINATED REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CABIN FLOOR PANEL 222FF DELAMINATED REPLACED FLOOR PANEL PER TASK CARD 26C2205314.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CABIN FLOOR PANEL 261AG DELAMINATED REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: HINGE — WORN (NLG DOOR) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR RIGHT HAND AFT DOOR FORWARD HINGE HAS EXCESSIVE PLAY / WEAR. REPLACED HINGE PER CMM 52-82-32.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CABIN FLOOR PANEL 221PF DELAMINATED REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CABIN FLOOR PANEL 261PF DELAMINATED REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CABIN FLOOR PANEL 221LF DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011

Part: SWITCH — BURNED (COCKPIT) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE - COCKPIT OVERHEAD PANEL, 30VU, HOT AIR (7HK) PUSHBUTTON SWITCH BURNED. REPLACED PUSHBUTTON SWITCH 7HK IN OVERHEAD PANEL 30VU PER ESPM 20-45-11 AND PERFORMED OPERATIONAL CHECK OF LIGHT TEST SYSTEM PER AMM 33-14-00-710-001-A, TESTED OK.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CABIN WET AREA FLOOR PANEL 231CF DELAMINATED REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: PLATE — BURNED (COCKPIT) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE - COCKPIT INSTRUMENT PANEL, LIGHT PLATE 301VU AND 500VU BURNED. REPLACED INTEGRALLY LIGHTED PLATE 500VU IN COCKPIT AREA PER AMM 33-13-43-400-802-A. PERFORMED OPERATIONAL TEST OF INSTRUMENT AND PANEL INTEGRAL LIGHTING PLATE PER AMM 33-13-00-710-001-A, TESTED OK. [SEE ASSOCIATED REPORT AALA202004029010]

Part: PLATE — BURNED (COCKPIT) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE - COCKPIT INSTRUMENT PANEL, LIGHT PLATE 301VU AND 500VU BURNED. REPLACED INTEGRALLY LIGHTED PLATE 301VU IN COCKPIT AREA PER AMM 33-13-43-400-802-A. PERFORMED OPERATIONAL TEST OF INSTRUMENT AND PANEL INTEGRAL LIGHTING PLATE PER AMM 33-13-00-710-001-A, TESTED OK. [SEE ASSOCIATED REPORT AALA202004029009]

Part: SWITCH — BURNED (COCKPIT) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE - COCKPIT OVERHEAD PANEL, 40VU, R TK PUMP 1 (14QA) PUSHBUTTON SWITCH BURNED. REPLACED PUSHBUTTOM SWITCH IN OVERHEAD PANEL PER ESPM 20-45-11, AND PERFORMED OPERATIONAL CHECK OF LIGHT TEST SYSTEM PER AMM 33-14-00-710-001-A, TESTED OK.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE - AFT CABIN WET AREA, FLOOR PANEL 261BG DELAMINATED. REPLACED FLOOR PANEL 261BG PER SRM 53-02-00-300-011, AND IRM 9701, REV. I.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE - PASSENGER CABIN, FLOOR PANEL 241JF DELAMINATED. REPLACED FLOOR PANEL 241JF PER A319 SRM 53-02-00-300-011, AND IRM 9701, REV. I.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE - PASSENGER CABIN, FLOOR PANEL 241FF DELAMINATED. REPLACED FLOOR PANEL 241FF PER A319 SRM 53-02-00-300-011, AND IRM 9701, REV. I.

Part: HINGE — WORN (RUDDER) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #3 HAS EXCESSIVE PLAY / WEAR AT RIB 5 ON THE VERTICAL STABILIZER. REPLACED HINGE PER TASK CARD 26C32027008.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE - FORWARD CABIN WET AREA, FLOOR PANEL 222EF DELAMINATED. REPLACED FLOOR PANEL 222EF PER A319 SRM 53-12-00-300-006, AND IRM 9701, REV. I.

Part: HINGE — WORN (RUDDER) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #7 HAS EXCESSIVE PLAY / WEAR AT RIB 11 ON THE VERTICAL STABILIZER. REPLACED HINGE PER TASK CARD 26C32027008.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE - FORWARD CABIN WET AREA FLOOR PANEL 231FF DELAMINATED. REPLACED FLOOR PANEL PER A319 SRM 53-12-00-300-006 AND IRM 9701, REV. I.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE - FORWARD CABIN WET AREA, FLOOR PANEL 221EF DELAMINATED. REPLACED FLOOR PANEL 221EF PER A319 SRM 53-12-00-300-006, AND IRM 9701, REV. I.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE - FORWARD CABIN WET AREA FLOOR PANEL 231BF DELAMINATED. REPLACED FLOOR PANEL PER A319 SRM 53-12-00-300-006 AND IRM 9701, REV. I.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE - MAIN CABIN FLOOR PANEL 241HF DELAMINATED . REPLACED FLOOR PANEL PER A319 SRM 53-02-00-300-011 AND IRM 9701, REV. I.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE - FORWARD CABIN WET AREA FLOOR PANEL 232FF DELAMINATED. REPLACED FLOOR PANEL PER A319 SRM 53-12-00-300-006 AND IRM 9701, REV. I.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED PRESSURE PANEL AT FR 36 AND +Y1292. REPAIRED PRESSURE PANEL PER EA 304449 REV A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED LEFT HAND INTERCOSTAL FITTING AT FR 16 AND DOOR STOP 7. REPLACED INTERCOSTAL FITTING PER SRM 51-72-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 RIGHT AT THE #7 DOOR STOP UPPER INBOARD HOLE. REPLACED INTERCOSTAL FITTING PER SRM 51-72-11.

Part: FITTING — CRACKED (COCKPIT) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAME RIGHT HAND CONTINUITY FITTING CRACKED BETWEEN FR 2 AND FR 3 AT Y0. REPLACED CONTINUITY FITTING PER SRM 51-72-11 AND EA 304094.

Part: FITTING — CRACKED (COCKPIT) · airframe 59,545 hrs · 26,746 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAME LEFT HAND CONTINUITY FITTING CRACKED BETWEEN FR 2 AND FR 3 AT Y0. REPLACED CONTINUITY FITTING PER SRM 51-72-11 AND EA 304094.

Part: ACTUATOR — INTERMITTENT (VSV) · airframe 57,902 hrs · 25,897 cycles

AIRCRAFT WAS GROUNDED: PILOT REJECTED TAKEOFF DUE TO ECAM "ENGINE 1 COMPRESSOR VANE". MAINTENANCE TROUBLESHOT IAW TSM 75-30-00-810-852-A. VSV SYSTEM INTERACTION ISSUE ON ENG 1. FOUND THE VSV ACTUATOR INTERMITTENTLY FAULTY. REMOVED AND REPLACED THE VSV ACTUATOR IAW JOB CARD 26T40075005. OPS CHECK GOOD.

Part: SHAFT — BENT (TACHOMETER) · airframe 57,877 hrs · 25,878 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS ON GEAR EXTENSION - BRAKES - AUTO BRAKE FAULT- AUTO BRAKES RELEASED. ON TAXI IN NR 1 BRAKE 580 NR 2 BRAKE 60, NR 3 560, NR 4 390. BRAKES CHATTERING - A/C HARD TO STOP. TOWED IN TO GATE. MAINTENANCE ACCOMPLISHED TSM 32-42-00-810-819-A. FOUND NR 2 TACH SHAFT BENT. REMOVED AND REPLACED NR 2 TACHOMETER AND SHAFT IAW AMM 32-42-57-401. OPS CHECK GOOD. TAXI CHECKED A/C . ALL OPS AND INDICATIONS NORMAL.

Part: CYLINDER — FAULTY (PAX DOOR) · airframe 57,838 hrs · 25,861 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR DAMPER AT PASSENGER CREW DOOR 841 AT FORWARD GALLEY AREA WAS NOT WORKING CORRECTLY. MAINTENANCE REPLACED CYLINDER PER AMM 52-11-14-400-001-B.

Part: COVER — CRACKED (FUSELAGE) · airframe 57,838 hrs · 25,861 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED RAIL DUMMY JOINT COVER BETWEEN FR 12 AND FR 16 AT -Y81. REPLACED JOINT COVER PER SRM 51-42-11.

Part: HINGE FITTING — WORN (HORIZONTAL STAB) · airframe 57,838 hrs · 25,861 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR HINGE #3 HAS EXCESSIVE PLAY / WEAR ON THE RIGHT HAND HORIZONTAL STABILZER. REPLACED HINGE FITTING PER AMM 55-16-42-400-001-A.

Part: HINGE — WORN (RT ELEVATOR) · airframe 57,838 hrs · 25,861 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR HINGE #4 HAS EXCESSIVE PLAY / WEAR ON THE RIGHT HAND HORIZONTAL STABILZER. REPLACED HINGE FITTING PER AMM 55-16-42-400-001-A.

Part: DUMMY RAIL — CORRODED (FRAMES 12-16) · corrosion level 2 · airframe 578,378 hrs · 25,861 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON DUMMY RAIL BETWEEN FR 12 AND FR 16 AT +Y503.2. REPLACED DUMMY RAIL PER SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FRAME 18) · corrosion level 2 · airframe 57,838 hrs · 25,861 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR BEAM AT FR 18 AND +Y254. REPLACED FLOOR BEAM PER SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 57,838 hrs · 25,861 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK BETWEEN FR 12 AND FR 24 AT -Y765. REPLACED SEAT TRACK PER SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 57,838 hrs · 25,861 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR BEAM BETWEEN FR 12 AND FR 24 AT -Y254. REPLACED FLOOR BEAM PER 51-72-11.

Part: DOOR SILL — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 57,838 hrs · 25,861 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT DOOR CUT OUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001 FIG 20101 REPAIR PRINCIPLE 4. CORROSION LEVEL 2 WAS REMOVED BASED UPON ENGINEERING REVIEW OF THIS EVENT WHICH DETERMINED IT WAS NOT A LEVEL 2 FINDING.**

Part: SEAT TRACK — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 57,838 hrs · 25,861 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK BETWEEN FR 12 AND FR 24 AT -Y1292. REPLACED SEAT TRACK PER SRM 51-72-11.

Part: TERMINAL — UNSECURE (EMERGENCY LIGHT) · airframe 56,225 hrs · 24,949 cycles

EMERGENCY LIGHT AT THE L1 DOOR NEXT TO FLIGHT ATTENDANT JUMPSEAT WAS INOPERATIVE. FOUND TERMINALS NOT FULLY ENGAGED TO THE LIGHT ASSEMBLY. SECURED TERMINALS TO THE LIGHT ASSEMBLY IAW AMM 33-51-13. OPS CHECKED SATISFACTORY.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 54,371 hrs · 23,869 cycles

FORWARD FLIGHT ATTENDANT SEAT FLASHLIGHT STRAP BROKEN. REPLACED FORWARD FLIGHT ATTENDANT FLASHLIGHT STRAP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,265 hrs · 23,801 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT SEAT 23C INOPERABLE. MAINTENANCE REPLACED EMERGENCY LIGHT AT SEAT 23C AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: A/C PACK — CONTAMINATED · airframe 54,246 hrs · 23,788 cycles

CREW REPORTS CABIN ODOR ON TAKEOFF AND ON DESCENT. NO 30 DAY HISTORY. LAST WORK UP WAS JAN 27 (2 MONTHS AGO). RIGHT HAND PACK COMPONENTS REQUIRE REPLACEMENT OR CLEANING DUE TO OIL CONTAMINATION, PER J/C 26L000210004. REPLACED RIGHT HAND PACK CONDENSER, RE-HEATER, OZONE FILTER, PACK CONTROL VALVE, WATER EXTRACTOR, AND WATER INJECTOR PER AMM 21-52-32, 21-52-31, 2151-41, 21-51-51, 21-52-16 AND 21-52-42. OPERATIONS CHECKS GOOD. NO CABIN ODOR AFTER ACCOMPLISHMENT OF J/C 26L000210004. THIS SDR IS FOR THE AIR CONDITIONER PACK CONDENSER. AIRCRAFT WAS GROUNDED.

Part: FILTER — CONTAMINATED · airframe 54,246 hrs · 23,788 cycles

CREW REPORTS CABIN ODOR ON TAKEOFF AND ON DESCENT. NO 30 DAY HISTORY. LAST WORK UP WAS JAN 27 (2 MONTHS AGO). RIGHT HAND PACK COMPONENTS REQUIRE REPLACEMENT OR CLEANING DUE TO OIL CONTAMINATION, PER J/C 26L000210004. REPLACED RIGHT HAND PACK CONDENSER, RE-HEATER, OZONE FILTER, PACK CONTROL VALVE, WATER EXTRACTOR, AND WATER INJECTOR PER AMM 21-52-32, 21-52-31, 2151-41, 21-51-51, 21-52-16 AND 21-52-42. OPERATIONS CHECKS GOOD. NO CABIN ODOR AFTER ACCOMPLISHMENT OF J/C 26L000210004. THIS SDR IS FOR THE OZONE FILTER. AIRCRAFT WAS GROUNDED.

Part: REHEATER — CONTAMINATED · airframe 54,246 hrs · 23,788 cycles

CREW REPORTS CABIN ODOR ON TAKEOFF AND ON DESCENT. NO 30 DAY HISTORY. LAST WORK UP WAS JAN 27 (2 MONTHS AGO). RIGHT HAND PACK COMPONENTS REQUIRE REPLACEMENT OR CLEANING DUE TO OIL CONTAMINATION, PER J/C 26L000210004. REPLACED RIGHT HAND PACK CONDENSER, RE-HEATER, OZONE FILTER, PACK CONTROL VALVE, WATER EXTRACTOR, AND WATER INJECTOR PER AMM 21-52-32, 21-52-31, 2151-41, 21-51-51, 21-52-16 AND 21-52-42. OPERATIONS CHECKS GOOD. NO CABIN ODOR AFTER ACCOMPLISHMENT OF J/C 26L000210004. THIS SDR IS FOR THE REHEATER. AIRCRAFT WAS GROUNDED.

Part: FLOW VALVE — CONTAMINATED · airframe 54,246 hrs · 23,788 cycles

CREW REPORTS CABIN ODOR ON TAKEOFF AND ON DESCENT. NO 30 DAY HISTORY. LAST WORK UP WAS JAN 27 (2 MONTHS AGO). RIGHT HAND PACK COMPONENTS REQUIRE REPLACEMENT OR CLEANING DUE TO OIL CONTAMINATION, PER J/C 26L000210004. REPLACED RIGHT HAND PACK CONDENSER, RE-HEATER, OZONE FILTER, PACK CONTROL VALVE, WATER EXTRACTOR, AND WATER INJECTOR PER AMM 21-52-32, 21-52-31, 2151-41, 21-51-51, 21-52-16 AND 21-52-42. OPERATIONS CHECKS GOOD. NO CABIN ODOR AFTER ACCOMPLISHMENT OF J/C 26L000210004. THIS SDR IS FOR THE FLOW CONTROL VALVE. AIRCRAFT WAS GROUNDED.

Part: OIL COOLER — LEAKING (APU) · airframe 53,745 hrs · 23,564 cycles

AIRCRAFT WAS GROUNDED: DIRTY WET SOCKS PREVALENT FROM TAKEOFF THROUGH MID CLIMB, ODOR BECOMES VERY STRONG DURING DESCENT BELOW 5,000. APU FOUND TO BE SOURCE OF CABIN ODOR. MAINTENANCE ACCOMPLISHED JOBCARD 26L00021002 AND FOUND OIL COOLER LEAKING EXTERNALLY. MAINTENANCE ALSO REPLACED APU OIL COOLER AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 49-91-44.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 52,817 hrs · 23,093 cycles

AFT FLASHLIGHT INOPERATIVE. REPLACED THE BATTERY IAW AMM.

Part: RETAINER — INOPERATIVE (GIRT BAR) · airframe 52,672 hrs · 23,013 cycles

GIRT BAR RETAINER INOPERATIVE FWD DOOR. REMOVED AND REPLACED FWD LEFT GIRT BAR RETAINER IAW AMM.

Part: SPRING — FAULTY (GIRT BAR) · airframe 52,672 hrs · 23,013 cycles

L1 DOOR HAS FAULTY GIRT BAR SPRING. REPLACED L1 DOOR AFT GIRT BAR FITTING SPRING PER AMM.

Part: FLOORBOARD — DELAMINATED (AFT GALLEY) · airframe 52,663 hrs · 23,009 cycles

DELAMINATION ON THE AFT GALLEY PASSENGER CABIN FLOOR NEAR ROW 26. REPLACED CABIN FLOORBOARD 251WF IAW AMM 53-42-12.

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 52,663 hrs · 23,009 cycles

DELAMINATION ON THE AFT GALLEY PASSENGER CABIN FLOOR PANEL NEAR ROW 26. REPLACED FLOOR PANEL 251RF IAW AMM 53-42-12. AIRCRAFT WAS GROUNDED.

Part: LIGHT — BROKEN (CABIN) · airframe 52,646 hrs · 23,003 cycles

LOWER EMERGENCY LIGHT PANEL BY L1 DOOR BROKEN. ATTACHED THE PANEL BY L1 DOOR.

Part: HANDLE — MISSING (R1 DOOR) · airframe 52,535 hrs · 22,946 cycles

DOOR 1R ASSIST HANDLE COVER MISSING. INSTALLED R1 DOOR ASSIST HANDLE AS REQUIRED.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 51,979 hrs · 22,648 cycles

EMERGENCY LIGHT OVER RIGHT WING EMERGENCY DOOR INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY UNIT IAW AMM 33-51-38. OPS CHECKED GOOD.

Part: OVEN — SMOKE (GALLEY) · airframe 51,935 hrs · 22,629 cycles

GALLEY OVEN NR 1, SMOKING. UNABLE TO DUPLICATE PROBLEM ON GROUND, OPS OF THE OVEN AT 450 DEGREES FOR 5 MINUTES, NO SMOKE WAS NOTED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 51,818 hrs · 22,555 cycles

OVERWING EXIT LIGHT MID CABIN DOES NOT ILLUMINATE.

Part: FILTER — CLOGGED (VENT) · airframe 49,755 hrs · 21,428 cycles

FLIGHT CREW REPORTED A STRONG ODOR IN THE COCKPIT AND AROUND ROW 9 WHICH LASTED 10-15 MIN THEN DISAPPATED WHILE IN CRUISE. AIRCRAFT GROUNDED. MAINTENANCE FOUND THE AVIONICS VENT FILTER CLOGGED, REPLACED THE FILTER AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 21-26-43-400-003A AND TASK CARD 26L00021001.

Part: SEAL — MISSING (L1 DOOR ASSIST) · airframe 49,683 hrs · 21,381 cycles

L1 DOOR ASSIST CYLINDER DOOR DAMPER, NO FLUID SHOWING IN PRESSURE GAUGE. FOUND CENTER SEAL MISSING. REPLACED ASSIST CYLINDER IAW AMM 52-11-14-400-001-B.

Part: FLOW DIVIDER — LEAKING (APU) · airframe 48,895 hrs · 20,951 cycles

AIRCRAFT WAS GNDED. SIGNIFICANT ODOR IN CABIN & COCKPIT SIMILAR TO DIRTY SOCKS OR OIL SMELL. FOUND SEVERAL FUEL LEAKS ON APU IGV ACTUATOR FUEL LINE & FUEL FLOW DIVIDER LEAKING FUEL AT DRAIN LINE DURING RUN OPERATION. TIGHTENED FUEL LINE & REPLACED FUEL FLOW DIVIDER IAW AMM 49-32-12-400-001-A. OPERATIONS & LEAK CHECK GOOD. ACCOMPLISHED APU JC 26L00021001, 26L00021002, 26L00021004 & 26L31049009. NO ODOR FOUND DURING OPERATIONAL CHECKS. SEE AALA201604209011 FOR ADDITIONAL PART.

Part: FUEL LINE — LEAKING (APU) · airframe 48,895 hrs · 20,951 cycles

AIRCRAFT WAS GNDED. SIGNIFICANT ODOR IN CABIN & COCKPIT SIMILAR TO DIRTY SOCKS OR OIL SMELL. FOUND SEVERAL FUEL LEAKS ON APU IGV ACTUATOR FUEL LINE & FUEL FLOW DIVIDER LEAKING FUEL AT DRAIN LINE DURING RUN OPERATION. TIGHTENED FUEL LINE & REPLACED FUEL FLOW DIVIDER IAW AMM 49-32-12-400-001-A. OPERATIONS & LEAK CHECK GOOD. ACCOMPLISHED APU JC 26L00021001, 26L00021002, 26L00021004 & 26L31049009. NO ODOR FOUND DURING OPERATIONAL CHECKS. SEE AALA201604209010 FOR ADDITIONAL PART.

Part: O-RING — LEAKING (APU) · airframe 48,819 hrs · 20,897 cycles

AIRCRAFT WAS GNDED. FLIGHT ATTENDANTS REPORTED BURNING SOCK ODOR STARTING ON DESCENT. FOUND APU TURBINE BEARING CAVITY LUBRICATION LINE O RINGS LEAKING & REPLACED THEM IAW 49-91-53. A SATISFACTORY LEAK & OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ODOR BEING NOTED.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 48,659 hrs · 20,799 cycles

AIRCRAFT WAS NOT GNDED. EMER SLIDE 1R OFF, THEN ON INFLIGHT. PRESSURIZATION LIGHT ON, THEN OFF, ON DOOR. CLEANED DEBRIS FROM 1R DOOR SLIDE ARMING ATTACH POINTS, GIRT BAR LOCATION. SLIDE ARM INDICATION CHECKED OK AT THIS TIME.

Part: SIGN — DETACHED (CABIN) · airframe 48,438 hrs · 20,693 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHT IN AFT GALLEY CAME OUT. REINSTALLED EMER EXIT SIGN IAW AMM 33-51-16-400-001-A.

Part: APU — ODOR · airframe 48,132 hrs · 20,538 cycles

CABIN ODOR IN ENTIRE CABIN FROM ENG START FOR ENTIRE LEG. VERY STRONG IN FLIGHT & DESCENT, RESULTED IN THE CREW EXPERIENCING HEADACHES & EYE IRRITATION. AIRCRAFT WAS GROUNDED. THE CAUSE WAS THE APU. MAINTENANCE REPLACED APU IAW TC 26L31049005 AND ACCOMPLISHED A SATISFACTORY OPS CHECK.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 47,729 hrs · 20,328 cycles

SEAT 22C AISLE EMER LIGHT HAS A BROKEN WIRE. REPAIRED & SECURED WIRE ON EMER LIGHT IAW AMM 33-51-06. OPERATIONAL CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 47,702 hrs · 20,310 cycles

MASTER WARNING ANNUNCIATED THEN WENT OFF AT ABOUT 100 KNOTS ON TAKEOFF. ABORTED THE TAKEOFF & RETURNED TO THE GATE. THE APU FIRE LOOP FAULT FLASHED AFTER THE TAKEOFF WAS REJECTED. PERFORMED BITE TEST OF THE APU FIRE & OVERHEAT DETECTION SYS IAW AMM 26-13-00-710-002-A, NO FAULTS NOTED. ACCOMPLISHED AFS GND SCAN 22-91-00-710-001-A & OPERATIONS CHECK OF THE FWS 31-50-00-710-002-A, NO FAULTS IN AIRMAN.

Part: HYDRAULIC LINE — CHAFED (ZONE 400) · airframe 47,300 hrs · 20,054 cycles

FLIGHT 565, EXPERIENCED A NR 1 GREEN HYD SYS LOW PRESS ECAM MSG. THE DECISION WAS TO CONTINUE TO ORIGINAL & FINAL DESTINATION. FLIGHT DECLARED AN EMER PRIOR TO LANDING. FLIGHT LANDED WITHOUT INCIDENT & WAS TOWED TO THE GATE. FOUND THE GREEN SYS PRESS LINE CHAFING AGAINST A BRACKET, AFTER HAVING WORN THROUGH THE TEFLON SLEEVE IN THE LT PYLON. THE DAMAGED LINE WAS REPLACED.

Part: LENS — MISSING (CABIN) · airframe 47,006 hrs · 19,909 cycles

RED EMER LIGHT LENS COVER MISSING. INSTALLED LENS.

Part: BEAM — CRACKED (FUSELAGE) · airframe 46,797 hrs · 19,805 cycles

RIGHT SIDE BOX BEAM FLANGE CRACKED AT FRAME 43 & -Y1650. REPAIRED IAW EA 252782 & EO 5313Y026.

Part: BEAM — CRACKED (FUSELAGE) · airframe 46,797 hrs · 19,805 cycles

LEFT SIDE BOX BEAM FLANGE CRACKED AT FRAME 43 & +Y1650. REPAIRED IAW EA 252782 & EO 5313Y026.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 46,045 hrs · 19,392 cycles

FORWARD FLIGHT ATTENDANT STATION FLASHLIGHT NOT CHARGED. REPLACED BATTERY IAW AMM 25-65-00.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 45,987 hrs · 19,361 cycles

LOST PRESSURIZATION OF SYS 1 & 15 SECONDS LATER SYS 2 FAULTED DURING CRUISE AT FL 340. CREW WAS ABLE TO CONTROL PRESS MANUALLY. FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. TROUBLESHOOTING ACCOMPLISHED IAW TSM 21-31-00-810-802-A & AMM 21-31-00-710-002-A WITH NO FINDINGS. GOOD OPERATIONAL CHECKS.

Part: PRESSURE SWITCH — FAULTY (FUEL SYSTEM) · airframe 45,948 hrs · 19,337 cycles

NUMBER 2 ENG FUEL FILTER CLOG INDICATION. TROUBLE SHOT IAW TSM 73-00-00-810-858A & FOUND FUEL DIFFERENTIAL PRESS SWITCH INOPERATIVE. REPLACED PRESS SWITCH IAW AMM 73-34-15-000-010 & 73-34-15-400-010.

Part: COVER — UNSECURE (EMERGENCY EXIT) · airframe 45,926 hrs · 19,325 cycles

EMERGENCY EXIT LIGHT OVERWING ECAM ARMING WARNING CAME ON AT 4000'. EMER EXIT HATCH COVER CAME OFF IN FLIGHT. ADJUSTED & REINSTALLED COVER FLAP IAW TSM TASK 52-21-00-816-806-A. SLIDE ARMED INDICATION ON ECAM NORMAL. ACFT OK FOR SERVICE AT THIS TIME.

Part: SHADE — JAMMED (CABIN) · airframe 45,914 hrs · 19,319 cycles

JAMMED WINDOW SHADE EXIT ROW WINDOW, ACFT LT. REPLACED WINDOW SHADE IAW AMM 52-21-11-401, 25-23-47-401 & 25-23-43-401. OK FOR SERVICE.

Part: LENS — MISSING (CABIN) · airframe 45,828 hrs · 19,266 cycles

L2 DOOR EMER LIGHT LENS MISSING. REPLACED EMER LIGHT LENS.

Part: UNKNOWN — ODOR (CABIN) · airframe 45,772 hrs · 19,226 cycles

DURING PUSHBACK CABIN FILLED WITH BURNING SMELL FOLLOWED BY AN APU SHUTDOWN. CAPTAIN OBSERVED A STRONG ODOR OF ELEC BURNING SMELL. INSPECTION ACCOMPLISHED IAW JC 26L00021001 & 26L00021002. ODOR COULD NOT BE DUPLICATED & THERE WAS NO PREVIOUS 30 DAY HISTORY.

Part: SPOILER — MALFUNCTIONED (WING) · airframe 45,368 hrs · 19,002 cycles

ON LANDING, SPOILERS DID NOT DEPLOY. PERFORMED BITE TEST OF THE SFCS IAW AMM 27-81-00-740-002-A. NO FAULTS FOUND.

Part: REGULATOR VALVE — FAULTY (BLEED AIR SYS) · airframe 45,143 hrs · 18,885 cycles

NUMBER 1 ENG SURGED AFTER TAKEOFF TURNED PACK OFF & SURGE STOPPED. REPLACED NR 1 ENG PRESS REGULATING VLV.

Part: UNKNOWN — ODOR (CABIN) · airframe 44,720 hrs · 18,652 cycles

AFTER ENG SHUT DOWN, APU BLEED ON, CREW REPORTED FUMES IN CABIN FRONT TO AFT. FUMES WERE SO BAD FLIGHT ATTENDANTS OPENED REAR DOORS. SMELLED LIKE PAINT THINNER. ACCOMPLISHED JOB CARD 26L00021001. RAN ENGS & APU WITH DIFFERENT SCENARIOS WITH BLEED ON & OFF, PACKS ON & OFF & APU BLEED. NO OVERBEARING SMELL NOTICED, ONLY NORMAL ACFT SMELL, COULD NOT DUPLICATE PAINT THINNER SMELL. ACFT OK FOR SERVICE IAW JOB CARD 26L00021003 PARA 11 A 2 IAW AMM 73-10-00.

Part: LENS — MISSING (CABIN) · airframe 44,646 hrs · 18,600 cycles

AIRCRAFT LT AT ROW 18 SEAT 18C LENS CAP MISSING ON ESCAPE PATH LIGHT. ATTACHED LENS COVER ON 18C ESCAPE PATH LIGHT. CHECKED OK.

Part: EEC — FAULTY (NR 2 ENGINE) · airframe 44,331 hrs · 18,420 cycles

NUMBER 2 ENG COMPRESSOR VANE FAULT & EGT OVER LIMIT ECAM ON TAKEOFF AS TAKEOFF POWER APPLIED. REPLACED NR 2 ENG EEC IAW JOB CARD 26L40073002.

Part: SHADE — STUCK (EMERGENCY EXIT) · airframe 43,868 hrs · 18,111 cycles

RIGHT EMERGENCY EXIT WINDOW SHADE WILL NOT OPEN FULLY. REPLACED RIGHT OVERWING EMERGENCY EXIT WINDOW SHADE IAW AMM 25-23-43.

Part: THERMOSTAT — FAULTY (BLEED AIR SYS) · airframe 43,691 hrs · 18,030 cycles

AT FL370, CREW RECEIVED AN ENG NR 2 BLEED FAULT. OPENED CROSSFEED IAW ECAM & GOT ENG NR 1 BLEED FAULT. FOLLOW UP SHOWED ECAM PROCEDURE WAS INCORRECT. CREW DECLARED AN EMERGENCY & DESCENDED TO MAINTAIN CABIN PRESS. FLIGHT LANDED WITHOUT INCIDENT. R & R NR 2 ENG FAN AIR VLV THERMOSTAT TEMP CONTROL IAW AMM 36-11-43. R & R NR 1 & NR 2 ENG HP BLEED VLVS IAW AMM 36-11-51. ACCOMPLISHED ENG GND RUN, NO LEAKS & NO FAULTS.

Part: COVER — MISSING (CABIN) · airframe 43,575 hrs · 17,968 cycles

CREW REPORTED EMERGENCY EXIT LIGHT 2R COVER MISSING. REPLACED COVER AT 2R AS REQUIRED.

Part: HOSE — LEAKING (LT MLG DOOR) · airframe 43,057 hrs · 17,760 cycles

A FEW MINUTES AFTER DEPARTING PHX, CREW REPORTED THE GREEN HYD FLUID LEVEL WENT TO ZERO. FLIGHT RETURNED TO FIELD AT PHX & LANDED WITHOUT INCIDENT. FOUND THE LT MLG DOOR ACTUATOR FLEXIBLE HOSE LEAKING. R & R LT MLG DOOR ACTUATOR FLEXIBLE HOSE IAW AMM 32-31-39. SERVICED & BLED GREEN HYD SYS IAW AMM 29-00-00-870-002A & 29-00-00-870-001A, LEAK CHECKED GOOD. OPERATIONS CHECK OF LG DOORS GOOD IAW AMM 32-31-00-710-002-A01, WITHOUT FALSE TARGETS.

Part: GIRT BAR — DIRTY (R2 DOOR) · airframe 42,030 hrs · 17,334 cycles

R2 DOOR WAS REPORTED TO BE DIFFICULT TO ARM & DISARM. LUBED AND CLEANED ALL FITTINGS AND ATTACHMENTS FOR R2 DOOR GIRT BAR. OPS CHECKED NORMAL.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 41,696 hrs · 17,192 cycles

AFT EMERGENCY FLASHLIGHT INOPERATIVE, REPLACED AFT EMERGENCY FLASHLIGHT BATTERY.

Part: PROXIMITY SWITCH — OUT OF ADJUST (R2 DOOR SLIDE) · airframe 41,175 hrs · 16,969 cycles

MX REPORTED DOOR R2 SLIDE INDICATOR ON ECAM WILL NOT STAY ILLUMINATED WITHOUT HANDLE BEING HELD DOWN. SHOWED ARMED ON GROUND PRIOR TO DEPARTURE. MX ADJUSTED ARMED HANDLE PROXIMITY SWITCH ON R2 DOOR IAW MM 52-71-00. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (R2 DOOR SLIDE) · airframe 41,152 hrs · 16,956 cycles

CREW REPORTED THE SLIDE AT R2 DOOR DOES NOT SHOW ARMED ON ECAM AFTER TAKEOFF, BUT DOES SHOW ARMED WHEN ON GROUND. MX R & R AFT RT PASSENGER DOOR SLIDE ARMED LIGHT (3WN2) IAW AMM 52-73-21-401.

Part: PROXIMITY SWITCH — SHORTED (ESCAPE SLIDE) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - DURING OPS TEST OF EMERGENCY EXIT ESCAPE SLIDE LIGHT SWITCHES, FWD RT DOOR SWITCH SHOWED AN OPEN CIRCUIT BETWEEN PIN "M" & "S". REPLACED PROXIMITY SWITCH IAW AMM 52-73-11-000-001-A & AMM 52-73-11-400-001-A. VERIFIED CONTINUITY CHECK BETWEEN CONECTOR PIN "S" & "M" IS OK. OPS TEST SWITCH OF THE EMERGENCY EXIT ESCAPE SLIDE LIGHTING IS OK IAW AMM 33-51-00-720-001-A.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,106 hrs · 16,935 cycles

2S CHECK - CORROSION ON SHAPE SILL (CENTER FITTING) BETWEEN FR66 TO FR68, S23R. REPLACED SHAPE SILL (CENTER FITTING) BETWEEN FR66 TO FR68, S23R IAW SRM 51-72-11, DWG, D53480048 & D53480505.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - CRACK ON EMERGENCY EXIT DOOR HATCH NR 834 SEGMENT FRAME ANGLE AT FR40 BETWEEN BEAM 1 TO BEAM 3. REPLACED FRAME ANGLE IAW EO 210Y228.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - CRACK ON EMERGENCY EXIT DOOR HATCH NR 844 SEGMENT FRAME ANGLE AT FR40 BETWEEN BEAM 1 TO BEAM 3. REPLACED FRAME ANGLE IAW EO 210Y228.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL NR 222CF BETWEEN FR12 TO FR16 & BETWEEN -Y254 & -Y1292. REPLACED FLOOR PANEL IAW SRM 53-12-00, PAR. 4C (1) FIG 101, DIAGRAM 101.

Part: HINGE FITTING — WORN (NR 2 SPOILER) · corrosion level 2 · airframe 41,106 hrs · 16,935 cycles

2S CHECK - WEAR ON RT WING NR 2 SPOILER HINGE FITTING BETWEEN WS 551 TO 732 & BETWEEN RIB 10 TO RIB 13. REPAIRED RT WING NR 2 SPOILER HINGE FITTING IAW SRM 57-70-00, PAR 5D (2), PAGE 210, FIG 201.

Part: HINGE FITTING — WORN (NR 3 SPOILER) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - WEAR ON RT WING NR 3 SPOILER HINGE FITTING BETWEEN WS732 TO WS874 & BETWEEN RIB 13 TO RIB 16. REPAIRED RT WING NR 3 SPOILER HINGE FITTING BETWEEN WS732 TO WS874 & BETWEEN RIB 13 TO RIB 16 IAW SRM 57-70-00, PAR 5D (2), PAGE 210, FIG 201.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,106 hrs · 16,935 cycles

2S CHECK - CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11 & DWG D53370500.

Part: FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,106 hrs · 16,935 cycles

2S CHECK - CORROSION ON CORNER FITTING AT FR68, S23R. REPLACED CORNER FITTING IAW SRM 51-72-11 & DWG D53480505.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,106 hrs · 16,935 cycles

2S CHECK - CORROSION ON SEAT TRACK AT FR41+5", -Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11, DWG D53371112 & EA 514175.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,106 hrs · 16,935 cycles

2S CHECK - CORROSION ON SEAT TRACK AT FR42+18", -Y765. REPLACED SEAT TRACK IAW SRM 51-72-11, DWG D53370500 & D53371110.

Part: SEAT TRACK — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 41,106 hrs · 16,935 cycles

2S CHECK - CORROSION ON SEAT TRACK AT FR36, -Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11 & DWG D57130300.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,106 hrs · 16,935 cycles

2S CHECK - CORROSION ON SHAPE SILL BETWEEN FR66 TO FR68, S23L. REPLACED SHAPE SILL IAW SRM 51-72-11 & EA 504172.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,106 hrs · 16,935 cycles

2S CHECK - CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, Y765. REPLACED SEAT TRACK IAW SRM 51-72-11 & DWG D53370500.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,106 hrs · 16,935 cycles

2S CHECK - CORROSION ON SEAT TRACK AT FR38+4", -Y765. REPLACED SEAT TRACK IAW SRM 51-72-11, DWG D57130300 & D57130147.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,106 hrs · 16,935 cycles

2S CHECK - CORROSION ON SEAT TRACK BETWEEN FR 41 TO FR47/51, Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11 & DRAWING D53371000.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,106 hrs · 16,935 cycles

2S CHECK - CORROSION ON SILL BETWEEN FR66 TO FR68, S23R. REPLACED SILL IAW SRM 51-72-11, DWG D53480505 & EA 504171.

Part: SILL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 41,106 hrs · 16,935 cycles

2S CHECK - CORROSION ON LOWER SILL FITTING BETWEEN FR16 TO FR20, S23R. REPLACED LOWER SILL FITTING IAW SRM 51-72-11, DWG D53112320.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL NR 211HF BETWEEN FR6 TO FR12 & BETWEEN Y765 TO Y1732. REPLACED FLOOR PANEL IAW SRM 53-12-00, FIG 206 & IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,106 hrs · 16,935 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 212GF BETWEEN FR 6--12 & BETWEEN -Y765 TO -Y254. REPLACED FLOOR PANEL IAW SRM 53-12-00, FIG 206 & IRM 9701, REV. G.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,106 hrs · 16,935 cycles

2S CHECK - CORROSION ON SEAT TRACK BETWEEN FR46+16" TO FR64, Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11 & DWG D53476977.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,106 hrs · 16,935 cycles

2S CHECK - CORROSION ON SEAT TRACK BETWEEN FR46 TO FR64, -Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11 & DWG D53476977.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,106 hrs · 16,935 cycles

2S CHECK - CORROSION ON SEAT TRACK BETWEEN FR46+16" TO FR64, -Y765. REPLACED SEAT TRACK IAW SRM 51-72-11 & DWG D53476977.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,106 hrs · 16,935 cycles

2S CHECK - CORROSION ON SEAT TRACK BETWEEN FR46+16" TO FR64, Y765. REPLACED SEAT TRACK IAW SRM 51-72-11 & DWG D53476977.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,106 hrs · 16,935 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK AT FR30+1", Y1292. REPLACED SEAT TRACK AT FR30+1", Y1292 IAW SRM 51-72-11 & DWG D53233450.

Part: FLOOR PANEL — DELAMINATED (ZONE 100 - FUSE) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 211FF BETWEEN FR7 TO FR11 & BETWEEN Y254 TO -Y254. REPLACED FLOOR PANEL IAW SRM 53-12-00, FIG 206 & IRM 9701, REV. G.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,106 hrs · 16,935 cycles

2S CHECK, CORROSION ON SEAT TRACK AT FR 21, Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11 & DWG NR D53112812.

Part: FLOOR PANEL — DELAMINATED (ZONE 100 - FUSE) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 241LF BETWEEN FR42 TO FR47 & BETWEEN Y765 TO Y1292. REPLACED FLOOR PANEL IAW SRM 53-02-00, TABLE 103, FIG. 209 & IRM 9701, REV. G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 261BG BETWEEN FR64 TO FR66 & BETWEEN Y254 TO Y1732. REPLACED FLOOR NR IAW SRM 53-02-00, TABLE 103 & IRM 9701 REV. G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 261PF BETWEEN FR68 TO FR70 & BETWEEN -Y1292 TO Y1292. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & IRM 9701, REV. G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100 - FUSE) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL NR 241EF BETWEEN FR36 TO FR42 & BETWEEN -Y254 TO Y254. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG. 209 & IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL NR 261AG BETWEEN FR64 TO FR66 & BETWEEN -Y765 TO Y254. REPLACED FLOOR PANEL IAW SRM 53-02-00, TABLE 103 & IRM 9701, REV. G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL NR 241MF BETWEEN FR42 TO FR47 & BETWEEN Y1292 TO Y1732. REPLACED FLOOR PANEL IAW SRM 53-02-00, TABLE 103, FIG. 209 & IRM 9701, REV. G.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,106 hrs · 16,935 cycles

2S CHECK - CORROSION ON SEAT TRACK AT FR64+1", -Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11, DWG D53472816.

Part: HINGE FITTING — EXCESS PLAY (ZONE 100) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - EXCESSIVE PLAY ON NR 4 RUDDER HINGE FITTING AT BR 4, RIB 6. REPLACED NR 4 RUDDER HINGE FITTING IAW SRM 51-72-11 & AMM 27-21-00-720-003-A.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 161CF BETWEEN FR59 TO FR63 & BETWEEN Y1328 TO Y1042.1. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG. 209 & IRM 9701, REV. G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 151FE BETWEEN FR55 TO FR59 & BETWEEN Y1328 TO Y1042.1. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & IRM 9701, REV. G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 151DE BETWEEN FR55 TO FR59 & BETWEEN Y1042.1 TO Y765. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & IRM 9701, REV. G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100 - FUSE) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 131DG BETWEEN FR28 TO FR34 & BETWEEN Y1042.1 TO Y765. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG. 209 & IRM 9701 REV. G.

Part: SKIN — CONTAMINATED (LT ELEVATOR) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - TRAPPED WATER INDICATION ON LT ELEVATOR UPPER SKIN AT 1.5 INCHES INBD FROM LIGHTING STRIP 4 BETWEEN ELEVATOR RIB 8 TO RIB 9. REPAIRED LEFT ELEVATOR UPPER SKIN IAW SRM 55-21-11, PAR 5.E.

Part: SKIN — CONTAMINATED (LT ELEVATOR) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - TRAPPED WATER INDICATION ON LT ELEVATOR UPPER SKIN AT 6" OTBD FROM LIGHTNING STRIP NR 1 BETWEEN ELEVATOR RIB 2 TO RIB 3. REPAIRED LT ELEVATOR UPPER SKIN IAW SRM 55-21-11, PAR 5.E.

Part: SKIN — CONTAMINATED (RT ELEVATOR) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - TRAPPED WATER INDICATION ON RT ELEVATOR UPPER SKIN AT 10" FROM INBD LIGHTING STRIP NR 3 BETWEEN ELEVATOR RIB 6 TO RIB 7. REPAIRED RT ELEVATOR UPPER SKIN IAW SRM 55-21-11, PAR 5.E.

Part: SKIN — CONTAMINATED (LT ELEVATOR) · airframe 41,106 hrs · 16,935 cycles

2S CHECK -TRAPPED WATER INDICATION ON LT ELEVATOR UPPER SKIN AT 9.5" OTBD FROM LIGHTNING STRIP NR 1 BETWEEN ELEVATOR RIB 2 TO RIB 3. REPAIRED LT ELEVATOR UPPER SKIN IAW SRM 55-21-11, PAR 5.E.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 161BF BETWEEN FR59 TO FR63 & BETWEEN Y1042.1 TO Y765. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG. 209 & IRM 9701, REV. G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 151AE BETWEEN FR53 TO FR55A & BETWEEN Y1042.1 TO Y765. REPLACED FLOOR PANEL IAW SRM 53-02-00, PAR 8H, FIG 209 & IRM 9701, REV G.

Part: SKIN — CONTAMINATED (RT ELEVATOR) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - TRAPPED WATER INDICATION ON RT ELEVATOR UPPER SKIN AT 3.5" FROM T/E BETWEEN ELEVATOR RIB 9 TO RIB 10. REPAIRED RT ELEVATOR UPPER SKIN IAW SRM 55-21-11, PAR 5.E.

Part: SKIN — CONTAMINATED (RT ELEVATOR) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - TRAPPED WATER INDICATION ON RT ELEVATOR UPPER SKIN AT 8.5" OTBD FROM LIGHTNING STRIP NR 2 BETWEEN ELEVATOR RIB 6 TO RIB 7. REPAIRED RT ELEVATOR UPPER SKIN IAW SRM 55-21-11, PAR 5.E.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL NR 152TG BETWEEN FR51 TO FR53 & BETWEEN -Y1042.1 TO -Y765. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 151BE BETWEEN FR53 TO FR55A & BETWEEN Y1328 TO Y1042.1. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG. 209 & IRM 9701, REV. G.

Part: SKIN — DEBONDED (LT ELEVATOR) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - TRAPPED WATER INDICATION & DEBONDING ON LT ELEVATOR UPPER SKIN AT 3.5" FROM T/E BETWEEN ELEVATOR RIB 3 TO RIB 4. REPAIRED LT ELEVATOR UPPER SKIN IAW SRM 55-21-11, PAR 5.E.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 152XG BETWEEN FR53 TO FR55A & BETWEEN -Y1328 TO -Y1042.1. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & IRM 9701, REV. G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,106 hrs · 16,935 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL NR 251PE BETWEEN FR51 TO FR53 & BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL IAW SRM 53-02-00, PAR 8H, FIG. 209 & IRM 9701, REV. G.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,941 hrs · 16,861 cycles

2S CHECK - CORROSION ON SHAPE SILL BETWEEN FR66 TO FR68, S23L. REPLACED SHAPE SILL IAW SRM 51-72-11, DWG D53480048 & D53480505.

Part: APU — LEAKING (APU BAY) · airframe 40,318 hrs · 16,579 cycles

WITH AIRCRAFT PARKED AT GATE, FLIGHT ATTENDANT HAD NOTICED A "DIRTY SOCK" SMELL AFTER APU BLEED WAS ON FOR ABOUT FIVE MINUTES. MAINTENANCE FOUND INTERNAL OIL LEAKING IN APU. OIL WAS COMING OUT OF PLENUM DRAIN. REMOVED AND REPLACED APU IAW JOB CARD 26L31049005. OPS LEAK AND BITE CHECK GOOD.

Part: COOLING FAN — LEAKING (APU) · airframe 40,275 hrs · 16,561 cycles

DURING CRUISE, EN ROUTE FROM MEX TO PHX, CREW REPORTED A DIRTY SOCK SMELL IN MID CABIN. FLIGHT LANDED UNEVENTFUL IN PHX. MAINTENANCE DETERMINED ENGINES WERE NOT SOURCE OF SMELL. RAN BOTH ENGINES EXTENSIVELY WITH NO ODOR. FOUND APU AIR INLET AND COMPARTMENT OIL SOAKED. FOUND THE APU ACCESSORY COOLING FAN LEAKING. REPLACED COOLING FAN ASSEMBLY PER AMM 49-52-51-400. OPS AND LEAK CHECKS GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 40,190 hrs · 16,524 cycles

FLIGHT ATTENDENTS REPORTED A DIRTY SOCK SMELL ON DESCENT BELOW 10,000 FEET. SMELL NOT NOTICED IN FLIGHT DECK. MAINTENANCE TROUBLESHOT AIRCRAFT AND FOUND A SLIGHT ODOR DURING ENGINE NR 1 START WHICH DISSIPATED QUICKLY. ACCOMPLISHED CHECKS AND DECONTAMINATION OF ENVIRONMENT CONTROL SYSTEM. AIRCRAFT OK FOR SERVICE.

Part: OIL SYSTEM — OVERSERVICED (NR 1 ENGINE) · airframe 39,869 hrs · 16,382 cycles

CREW REPORTED ENGINE 1 OIL QUANTITY INDICATOR SHOWS XX. FLIGHT RETURNED TO FIELD AT PHX AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED CONNECTOR WIRING AND PINS. NO DEFECTS NOTED. FOUND ENGINE 1 OVERSERVICED WITH OIL. REMOVED 2 GALLONS OF OIL. REMOVED AND REPLACED OIL QUANTITY TRANSMITTER AS PRECAUTION REF AMM 79-31-15. INDICATION OPS GOOD. ENGINE 1 HAD NO FUEL SMELL IN OIL.

Part: SEAL — LEAKING (NR 1 ENGINE) · airframe 39,494 hrs · 16,215 cycles

ON APPROACH TO LANDING, CREW REPORTED A DIRTY SOCK SMELL FROM ABOUT 5,000 FEET UNTIL LANDING. APU WAS OFF AT THE TIME. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE DE-OILER SEAL PER AMM 72-60-31-400-010A. COMPLIED WITH TASK CARDS 26L00021001, 26L00021003 AND 26L00021004.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,290 hrs · 16,118 cycles

SY6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON L2 DOORWAY LOWER SILL FITTING AT FR68, Y1732. REPAIRED L2 DOORWAY LOWER SILL FITTING AT FR68, Y1732 IAW A319 SRM 53-41-14 FIG 101 & 201 & SRM 51-74-00.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,290 hrs · 16,118 cycles

SY6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, Y1732. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, Y1732 IAW TYPICAL REPAIR # TR320-2528-10-0011E & A319 SRM 53-41-14.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,290 hrs · 16,118 cycles

SY6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, -Y1732. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, -Y1732 IAW TYPICAL REPAIR # TR320-2528-10-0011E & A319 SRM 53-41-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,290 hrs · 16,118 cycles

SY6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR BEAM AT FR68, -Y1292. REPLACED FLOORBEAM AT FR68, -Y1292 IAW A319 SRM 51-42-11.

Part: DIAPHRAGM — PUNCTURED (L2 DOOR) · airframe 39,290 hrs · 16,119 cycles

SY6 CHECK - L-2 PAX DOOR PERCUSSION DIAPHRAGM IS PUNCTURED. REPLACED L-2 PASSENGER DOOR PERCUSSION DIAPHRAGM & SERVICED DAMPER, LEAK CHECK NORMAL IAW A319 AMM-52-10-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,290 hrs · 16,118 cycles

SY6 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BEAM AT FR68, Y1292. REPLACED FLOOR SUPPORT BEAM AT FR68, Y1292 IAW A319 SRM 51-42-11, 53-00-14 & 51-74-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,290 hrs · 16,118 cycles

SY6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR68, Y765. REPLACED FLOORBEAM AT FR68, Y765 IAW A319 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,290 hrs · 16,118 cycles

SY6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR68, -Y1292. REPLACED FLOORBEAM AT FR68, -Y1292 IAW A319 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,290 hrs · 16,118 cycles

SY6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BEAM AT FR66, Y765. REPLACED SEAT TRACK BEAM AT FR66, Y765 IAW A319 SRM 51-42-11.

Part: LENS — BROKEN (CABIN) · airframe 39,290 hrs · 16,119 cycles

SY6 CHECK - EMERGENCY EXIT LIGHT LENS DOOR L-2 CRACKED (LEFT LOWER). REPLACED EMERGENCY EXIT LIGHT LENS AT L-2 (AFT LOWER) IAW A320 AMM 33-51-13.

Part: SPLICE — BROKEN (CABIN) · airframe 39,920 hrs · 16,118 cycles

SY6 CHECK - EMERGENCY EXIT LIGHT AT SEAT 10C IS INOP. ACCOMPLISHED TROUBLESHOOTING & FOUND TERMINAL SPLICE BROKEN UNDER SEAT 10C. REMOVED & INSTALLED NEW SPLICE IAW A319 SWDM 20-48-13 & 20-48-25. PERFORMED OPS CHECK OF EMERGENCY LIGHT GOOD IAW A319 AMM 33-51-00.

Part: COMPUTER — FAULTY (NR 1) · airframe 38,559 hrs · 15,781 cycles

DURING TAKEOFF ROLL IN PHX THE AIRCRAFT HAD A FAST BUT MOMENTARY UNCOMMANDED RUDDER MOVEMENT AT APPROXIMATELY 115 KTS. THE FIRST OFFICER WAS FLYING AND HE THOUGHT IT WAS A NOSE RIGHT MOVEMENT. REMOVED AND REPLACED FAC 1 (FLIGHT AUGMENTATION COMPUTER) AND TESTED WIRING IAW TSM 27-26-00-810-801 AND PERFORMED YAW DAMPER TEST.

Part: YAW DAMPER — FAULTY (RUDDER)

DURING TAKEOFF ROLL IN PHX THE AIRCRAFT HAD A FAST BUT MOMENTARY UNCOMMANDED RUDDER MOVEMENT AT APPROXIMATELY 115 KTS. THE FIRST OFFICER WAS FLYING AND HE THOUGHT IT WAS A NOSE RIGHT MOVEMENT. PER LOG PAGE 4854424, REMOVED AND REPLACED LEFT YAW DAMPER. OPS CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 38,294 hrs · 15,657 cycles

EMERGENCY LIGHT LENS COVER MISSING FROM AFT SIDE OF AFT RIGHT SERVICE DOOR. REPLACED LENS COVER AS REQUIRED.

Part: LIMITER — FAULTY (RUDDER) · airframe 37,911 hrs · 15,480 cycles

RUDDER TRAVEL LIMITER SYSTEM FAULT 1 AND 2 WHILE EN ROUTE TO STL. DECLARED EMERGENCY LANDING. CREW WAS ABLE TO RESET THE SYSTEM PRIOR TO LANDING. DUE TO HISTORY ON THE RUDDER TRAVEL LIMITER SYSTEM, REMOVED AND REPLACED RUDDER TRAVEL LIMITER UNIT PER AMM 27-23-51-001-001-A. OPS CHECKED GOOD.

Part: SWITCH — FAULTY (CABIN) · airframe 34,161 hrs · 13,796 cycles

EMERGENCY EXIT LIGHTS ON WHILE SWITCH IN THE ARMED POSITION. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 32,932 hrs · 13,255 cycles

FLT 471 - LAS - EEL - FORWARD INBOARD FLIGHT ATTENDANT FLASHLIGHT BATTERY DEAD. REMOVED AND REPLACED FORWARD INBOARD FLIGHT ATTENDANT FLASHLIGHT BATTERY.

Part: ACM — DEFECTIVE (AC BAY) · airframe 32,409 hrs · 13,027 cycles

FLT 622 - LAS - BURNING SMELL - ON TAKEOFF WITH FLEX POWER SET, CREW NOTICED AN ACRID BURNING SMELL WITH LIGHT HAZE OF SMOKE. AFTER LIFT OFF, A LOW GRINDING NOISE WAS ALSO NOTICED UNTIL AFTER FLAP RETRACTION WHICH RETURNED FOR A SHORT TIME ON DESCENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 AIR CYCLE MACHINE IAW AIRBUS MAINTENANCE MANUAL 21-52-21.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 31,640 hrs · 12,665 cycles

FLT 113 - LAX - EEL - FOUND FORWARD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT.

Part: DAMPER — OUT OF ADJUST (R2 DOOR) · airframe 30,809 hrs · 12,314 cycles

SAL - C6 - EES - R-2 DOOR IS OUT OF ADJUSTMENT AT DIMENSION "A" BETWEEN STRIKER & FINGER ON THE DOOR DAMPER MECHANISM & EMERGENCY OPERATION CYLINDER. ACCOMPLISHED ADJUSTMENT AT DIMENSION "A" BETWEEN STRIKER & FINGER ON THE DOOR DAMPER MECHANISM & EMERGENCY OPERATION CYLINDER AT R-2 DOOR IAW A319 AMM 52-13-14-820-052.

Part: DAMPER — OUT OF ADJUST (L2 DOOR) · airframe 30,809 hrs · 12,314 cycles

SAL - C6 - EES - L-2 DOOR IS OUT OF ADJUSTMENT AT DIMENSION "A" BETWEEN STRIKER & FINGER ON THE DOOR DAMPER MECHANISM & EMERGENCY OPERATION CYLINDER. ACCOMPLISHED ADJUSTMENT AT DIMENSION "A" BETWEEN STRIKER & FINGER ON THE DOOR DAMPER MECHANISM & EMERGENCY OPERATION CYLINDER AT L-2 DOOR IAW A319 AMM 52-13-14-820-052.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 30,177 hrs · 12,022 cycles

FLT 393 - LAS-DFW - EMERGENCY EGRESS SYSTEM - R1 DOOR ASSIST BOTTLE NEEDS SERVICING. SERVICED R1 DOOR PER AMM 52-10-00-010-075.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 30,177 hrs · 12,022 cycles

FLT 393 - LAS-DFW - EMERGENCY EGRESS SYSTEM - L2 DOOR ASSIST BOTTLE NEEDS SERVICING. SERVICED L2 DOOR PER AMM 52-10-00-010-075.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 30,177 hrs · 12,022 cycles

FLT 393 - LAS-DFW - EMERGENCY EGRESS SYSTEM - R2 DOOR ASSIST BOTTLE NEEDS SERVICING. SERVICED R2 DOOR PER AMM 52-10-00-010-075.

Part: LENS — MISSING (CABIN) · airframe 29,496 hrs · 11,729 cycles

FLT 504 - IAD-PHX - EMERGENCY LIGHTS - EMERGENCY EXIT LIGHT LENS AT 22C IS MISSING. INSTALLED NEW EMERGENCY LIGHT LENS AT 22C.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 28,191 hrs · 11,078 cycles

FLT 683 - PHX-EWR - EMERGENCY LIGHTS - EMERGENCY EXIT LIGHTS ARE ON WITH THE SWITCH IN THE ARM POSITION. REMOVED AND REPLACED 12WL BATTERY AND EMERGENCY POWER SUPPLY. OPERATIONAL CHECK WAS GOOD.

Part: BALLAST — DEFECTIVE (CABIN)

FLT 632 - PHX-PIT - SMOKE - PRIOR TO LANDING, CABIN LIGHTS FLICKERING. UPON LANDING IN PIT, SMOKE WAS REPORTED IN THE CABIN (POWDERY SMOKE), SOURCE WAS AROUND ROW 4. CREW DECLARED EMERGENCY, FIRE AND RESCUE EQUIPMENT RESPONDED. INSTALLED NEW BALLAST. OPERATIONAL CHECK WAS GOOD.

Part: WIRE HARNESS — FAULTY (EMERGENCY LIGHTS) · airframe 26,049 hrs · 10,153 cycles

FLT 655 - SNA-PHX- EEL - EMERGENCY PATH LIGHT AT SEAT 22C INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT HARNESS ON SEAT 22C. OPERATIONAL CHECK WAS GOOD. (S)

Part: ACTUATOR — FAILED (NR 3 SPOILER) · airframe 25,340 hrs · 9,868 cycles

FLT 687 - PHX - EWR - RETF - DURING CLIMB THE LT SPOILER REMAINED DEPLOYED 2 INCHES CAUSING EXCESSIVE VIBRATION. CABIN VERIFIED CONDITION. CAPTAIN RETURNED TO THE FIELD. MX REPLACED THE NR3 SPOILER ACTUATOR IAW WITH AIRCRAFT MAINTENANCE MANUAL 27-64-51. OPERATIONAL CHECK WAS GOOD. (S)

Part: SMOKE DETECTOR — FAILED (E/E BAY) · airframe 22,095 hrs · 8,511 cycles

PHX - EES - LOG NR 7848154 - CREW REPORTED SMOKE LAV AND CRG DET FAULT. MX REMOVED AND REPLACED SDCU IAW AMM 26-17-34, OPERATIONAL CHECK WAS GOOD.

Part: O-RING — LEAKING (NR 1 ENGINE) · airframe 20,453 hrs · 7,816 cycles

PHX - DURING INITIAL CLIMB, LOST ALL OIL QUANTITY IN NR 1 ENGINE. OIL PRESS AND ALL OTHER PARAMETERS REMAINED IN THE GREEN. RETURNED TO FIELD AT IDLE THRUST. INSTALLED TEMP THERMOCOUPLE IN NR 1 ENG ACOC WITH NEW O-RING IAW MM 79-32-15 PB401. RAN ENG, LEAK CHECK GOOD. INSPECTED MASTER CHIP DETECTOR, NO DISCREPANCIES NOTED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 19,685 hrs · 7,473 cycles

SAL - CORROSION ON MAIN CABIN FLOORBEAM, FS 67 + 11" - FS 70, -Y765. REPLACED MAIN CABIN FLOORBEAM, FS 67 + 11" - FS 70, -Y765 IAW A319 SRM 51-72-11 AND 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 19,685 hrs · 7,473 cycles

SAL - CORROSION ON MAIN CABIN FLOORBEAM, FS 64 - FS 66, + Y1292. REPLACED MAIN CABIN FLOORBEAM, FS 64 - FS 66, + Y1292 IAW A319 SRM 51-72-11 AND 51-42-11.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,685 hrs · 7,473 cycles

SAL - MAJOR REPAIR - BC-4 CHECK, CORROSION ON R2 DOOR CUT OUT LOWER SILL CENTER FITTING, FS 66 TO FS 68, S23R. REPLACED R2 DOOR CUT OUT LOWER SILL CENTER FITTING, FS 66 TO FS 68, S23R IAW A319 SRM 51-72-11.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 19,685 hrs · 7,473 cycles

SAL - MAJOR REPAIR - BC-4 CHECK - CORROSION ON MAIN CABIN SHEAR WEB, FS 69 TO FS 70, -Y1732. REPLACED MAIN CABIN SHEAR WEB, FS 69 TO FS 70, -Y1732 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 19,685 hrs · 7,473 cycles

SAL - MAJOR REPAIR - BC-4 CHECK, CORROSION ON MAIN CABIN FLOORBEAM, FS 66, -Y1292. REPLACED MAIN CABIN FLOORBEAM, FS 66, -Y1292 IAW A319 SRM 51-72-11.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · airframe 19,685 hrs · 7,473 cycles

SAL - MAJOR REPAIR - BC -4 CHECK - CORROSION ON MAIN CABIN DUMMY RAIL, FS 20 AND -Y254. REPAIRED MAIN CABIN DUMMY RAIL, FS 20 AND -Y254 IAW A319 SRM 53-00-14 FIGURE 204.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,685 hrs · 7,473 cycles

SAL - CORROSION ON L2 DOOR CUT OUT LOWER SILL, FS 67+16" - FS 68, -Y1732. REPAIRED L2 DOOR CUT OUT LOWER SILL, FS 67+16" - FS 68, -Y1732 IAW A319 SRM 53-41-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 19,685 hrs · 7,473 cycles

SAL - CORROSION ON MAIN CABIN FLOORBEAM, FS 68 - FS 70, + Y765. REPLACED MAIN CABIN FLOORBEAM, FS 68 - FS 70, + Y765 IAW A319 SRM 51-72-11 AND 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 19,685 hrs · 7,473 cycles

SAL - CORROSION ON MAIN CABIN FLOORBEAM, FS 66 - FS 68, -Y1292. REPLACED MAIN CABIN FLOORBEAM, FS 66 - FS 68, -Y1292 IAW A319 SRM 51-42-11 AND 51-72-11.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · airframe 19,685 hrs · 7,473 cycles

SAL - MAJOR REPAIR - BC-4 CHECK - CORROSION ON MAIN CABIN DUMMY RAIL, FS 16+7", -Y1292. REPAIRED MAIN CABIN DUMMY RAIL, FS 16+7", -Y1292 IAW A319 SRM 53-11-15 FIGURE 203.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 19,685 hrs · 7,473 cycles

SAL - CORROSION ON SHEAR WEB IN AFT PASSENGER CABIN, FROM FS 69 TO FS 70, +Y1732. REPLACED SHEAR WEB IN AFT PASSENGER CABIN, FROM FS 69 TO FS 70, +Y1732, IAW A320 SRM 51-72-11 AND 51-42-11.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · airframe 19,685 hrs · 7,473 cycles

SAL - MAJOR REPAIR - BC-4 CHECK - CORROSION ON MAIN CABIN DUMMY RAIL, FS 20 - FS 24, -Y189. REPLACED MAIN CABIN DUMMY RAIL, FS 20 - FS 24, -Y189 IAW A319 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 19,685 hrs · 7,473 cycles

SAL - MAJOR REPAIR - BC-4 CHECK - CORROSION ON MAIN CABIN FLOORBEAM, FS 67 + 16" TO FS 69 + 4", -Y1162. REPLACED MAIN CABIN FLOORBEAM, FS 67 + 16" TO FS 69 + 4", -Y1162 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 19,685 hrs · 7,473 cycles

SAL - MAJOR REPAIR - BC-4 CHECK - CORROSION ON MAIN CABIN FLOORBEAM, FS 66 + 5", -Y1162. REPLACED MAIN CABIN FLOORBEAM, FS 66 + 5", -Y1162 IAW A319 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,685 hrs · 7,473 cycles

SAL - CORROSION ON MAIN CABIN SEAT TRACK, +Y765, FS 41 + 7", FS 44 + 5" AND FS 45 + 16". REPLACED MAIN CABIN SEAT TRACK, +Y765, FS 41 - FS 47 IAW A319 SRM 51-72-11.

Part: CONDENSER — FAILED (NR 1) · airframe 16,418 hrs · 6,091 cycles

CREW REPORTED THAT THE NR 1 PACK WOULD NOT HOLD CABIN PRESSURE WHILE EN ROUTE TO LAS AT FL 270 CABIN CLIMBED TO 9650 FL. CREW PERFORMED EMERGENCY DESCENT TO 10,000 FLT. AT 10,000 FLT CABIN ALT WAS 5500FT. AIRCRAFT LANDED IN LAS WITHOUT FURTHER INCIDENT. MX R & R NR 1 PACK CONDENSER DUE TO FAILURE IAW AIRBUS MM 21-52-32. OPS CHK OK. VENDOR CONFIRMS FAILURE. FOUND A BLOWN PAN ON UNIT. UNIT WAS CLEANED, RECORED AND PASSED ALL TESTS. REPAIRS WERE ACCOMPLISHED IAW OHM/CMM 21-52-10 REV.6.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 15,703 hrs · 5,812 cycles

PHX - EEL - ON THE GROUND REPORTED THAT THE AFT FLIGHT ATTENDANT RT EMERGENCY FLASHLIGHT DOES NOT BLINK. MAINTENANCE REMOVED AND REPLACED THE RT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECKS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 12,622 hrs · 4,650 cycles

PHX - EMERGENCY EQUIPMENT - DURING THROUGH FLIGHT INSPECTION THE FORWARD INBOARD EMERGENCY FLASHLIGHT WAS NOT FLASHING. MAINTENANCE REMOVED AND REPLACED THE FORWARD INBOARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.

Part: PRESSURE SWITCH — CRACKED (GREEN HYD SYS) · airframe 9,486 hrs · 3,646 cycles

PHX - EMERGENCY LANDING - FLT 0154 - EN ROUTE FROM SFO TO PHX RECEIVED GREEN HYDRAULIC SYSTEM RESERVOIR LOW LEVEL INDICATION. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND NR 1 ENGINE (GREEN SYSTEM) HYDRAULIC PRESSURE SWITCH CRACKED AND LEAKING. REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PRESSURE SWITCH IAW AMM 29-11-17, LEAK AND OPERATIONAL CHECK WAS GOOD.

Part: IRU — FAULTY (E/E BAY) · airframe 8,415 hrs · 3,287 cycles

LAX - ABORTED TAKEOFF - FLT 0408 - ON TAKEOFF ROLL AT LAX EN ROUTE FOR BOS THE CAPTAINS AIRSPEED INDICATOR SHOWED 40 KTS AT THE 80 KTS CROSS CHECK. REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED NR 1 AIR DATA INERTIAL REFERENCE UNIT (ADIRU) IAW T/C R2A34304, OPERATIONAL CHECK WAS GOOD. VENDOR FUNCTIONAL TEST OF ADIRU S/N 3248 CONFIRMED FAILURE OF UNIT. REPLACED 2 EACH VIBRATION ISOLATORS AND ISOLATOR COVER (P/N 465301-01). INCORPORATED SERVICE BULLETIN SB 101-34-57 PER CEO 3412-01020, REPAIR PERFORMED IAW CMM TP1011, REV. 23.

Part: WARNING HORN — FALSE ACTIVATION (COCKPIT) · airframe 4,873 hrs · 1,931 cycles

ON TAKEOFF ROLL ENROUTE FOR SET N1 THRUST AT 80 KTS AND HEARD REPETITIVE "RETARD" OVER THE LOUD SPEAKER; REJECTED TAKEOFF AND RETURNED TO GATE. MAX SPEED INDICATED WAS 87 KTS. MAINTENANCE REVIEWED POST FLIGHT REPORT THAT INDICATED AIRCRAFT WENT FROM PHASE 2 TO PHASE 8 AND NEVER LEFT THE GROUND. RAN GROUND SCAN OF CENTRAL WARNING SYSTEM IAW AMM, AND PERFORMED AN OPERATIONAL TEST OF FLIGHT WARNING COMPUTER IAW AMM. NO FAILURE MESSAGES WERE NOTED.

Part: CIRCUIT BOARD — FAILED (ZONE 100) · airframe 4,836 hrs · 1,918 cycles

ON CLIMB FROM LAX EN ROUTE FOR CMH WITH AIR DATA SWITCH IN FIRST OFFICER 3 POSITION; FIRST OFFICERS AIR SPEED INDICATOR RED LINE DECREASED TO APPROXIMATELY 240 KTS. SWITCHED BACK TO AIR DATA NORMAL POSITION AND INDICATIONS WENT BACK TO NORMAL. DUE TO FIRST OFFICERS STATIC HEATER PORT ON MEL, DIVERTED TO PHX FOR REPAIR. MAINTENANCE REMOVED AND REPLACED THE #3 AIR DATA INERTIAL REFERENCE UNIT IAW AWA T/C R2A34304, ALL INTERFACE TESTS WERE GOOD. MAINTENANCE ALSO CLEARED THE MEL FOR F/O'S STATIC PORT HEATER BY REPLACING THE HEAT PROBE COMPUTER IAW AMM 30-31-34-401. VENDOR TEARDOWN OF HEAT PROBE COMPUTER SN B4988 CONFIRMED FAILURE OF UNIT FINDING DIODE CR09 BURNED OPEN ON THE PRINTED CIRCUIT BOARD. REPLACED PRINTED