N812AW

Part: VENT LINE — LEAKING (ZONE 100) · airframe 77,760 hrs · 36,554 cycles

AIRCRAFT WAS GROUNDED: REPLACED APU GEARBOX VENT TUBE IAW AMM 49-26-55. R & R APU AIR-OIL SEPARATOR ASSY. IAW AMM 49-26-54.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 77,119 hrs · 36,121 cycles

AIRCRAFT WAS NOT GROUNDED: EPSU BATTERY EMERGENCY R MESSAGE AFTER OPERATIONAL TEST OF THE EMERGENCY LIGHTS. MAINTENANCE REPLACED THE EPSU BATTERY EMERGENCY R IAW AMM 33-51-38.

Part: UNKNOWN — ODOR (CABIN) · airframe 75,821 hrs · 35,240 cycles

AIRCRAFT WAS GROUNDED: SMELLED SMOKE ON TAKEOFF FLIGHTS ATTENDANTS AND PAX SMELT SMOKE IN THE CABIN DECLARED EMERGENCY AND RETURNED TO KBFL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED J/C 26L00021001 SMOKE/ODOR/FUMES INITIAL TROUBLESHOOTING FOUND NO FINDINGS. NO PREVIOUS HISTORY. NO FAULTS NOTED. COULDN'T DUPLICATE SMELL.

Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 75,314 hrs · 34,896 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD MEGAPHONE INOPERATIVE BUTTON CLICKS NO VOICE AMPLIFICATION. REMOVED AND REPLACED FORWARD MEGAPHONE PER AMM 25-65-51.

Part: GIRT BAR — LACK OF LUBE (L2 DOOR) · airframe 74,042 hrs · 34,125 cycles

AIRCRAFT WAS NOT GROUNDED: 2L DOOR ARMING DEVICE, DIFFICULT TO OPERATE. CLEANED AND LUBRICATED GIRT BAR PAWS ON L2 DOOR.

Part: LEVER — LOOSE (L1 DOOR) · airframe 73,862 hrs · 34,006 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 1L ARMING LEVER IS LOOSE. TIGHTENED LOOSE HARDWARE.

Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 73,782 hrs · 33,951 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR DIFFICULT TO OPEN DURING FLIGHT. FLIGHT ATTENDANT REPORTS THAT THE DOOR "CATCHES" AT THE BOTTOM OF THE DOOR. MAINTENANCE ADJUSTED THE LAVATORY DOOR.

Part: FIRE BOTTLE — WARNING MESSAGE (ZONE 400 - NAC/P) · airframe 73,475 hrs · 33,756 cycles

AIRCRAFT WAS GROUNDED: ON INITIAL CLIMB OUT ENGINE 1 AGENT 1 "DISCH" LIGHT ILLUMINATED. REPLACED ENGINE 1 FIRE EXTINGUISHER BOTTLE PER AMM 26-21-41.

Part: FITTING — NONE (ZONE 200 - FUSE) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING NEEDS TO BE REPLACED AS PART OF THE MAJOR REPAIR BEING ACCOMPLISHED ON THE WINDSHIELD FRAMING AS OUTLINED IN EA 348298. REPLACED CONTINUITY FITTING PER EA 348298.

Part: STRINGER SPLICE — CRACKED (ZONE 200 - FUSE) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED UPPER SPLICE COUPLING FASTENER HOLE AT FR 16 AND S5R. REPLACED SPLICE COUPLING PER SRM 51-42-11.

Part: FITTING — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23R. REPLACED CENTER SHAPE FITTING PER SRM 51-42-11.

Part: SUPPORT — WORN (ZONE 100 - FUSE) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CABIN FLOOR SUPPORT WEB HAS ELONGATED / WORN FASTENER HOLE BETWEEN FR 69 AND FR 70 AT S23L REPLACED SUPPORT WEB PER SRM 51-42-11.

Part: BOLT — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #6 LOWER MID BOLT BETWEEN WS 6132 AND 6699, BETWEEN RIBS 11 AND 12. REPLACED BOLT PER AMM 27-84-64.

Part: BOLT — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #5 LOWER BOLT BETWEEN WS 4067 AND WS 4862, BETWEEN RIBS 8 AND 9. REPLACED BOLT PER AMM 27-84-64.

Part: DOOR SILL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUTOUT LOWER SILL AT FR 68 AND S23L. REPAIRED LOWER SILL PER SRM 53-41-14.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 - STABS) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR HINGE ARM #5 BEARING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 - STABS) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR HINGE ARM #4 BEARING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 - STABS) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR HINGE ARM #2 BEARING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 - STABS) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR HINGE ARM #6 BEARING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 - STABS) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR HINGE ARM #3 BEARING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.

Part: SKIN PANEL — SCRATCHED (ZONE 200 - FUSE) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: SCRATCH ON EXTERNAL SKIN PANEL BETWEEN FR 52 AND FR 53, BETWEEN S3L AND S4L. REPAIRED SKIN PER EA EA348949.

Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-72-11.

Part: PLATE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PLATE LOCATED AT FR 12 AND STR 23 BETWEEN -Y503.2 AND -Y1292. REPLACED PLATE PER SRM 51-72-11-911-001.

Part: SEAT TRACK — CORRODED (ZONE 200 - FUSE) · corrosion level 2 · airframe 73,381 hrs · 33,706 cycles

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

Part: DOOR SILL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23R. REPLACED LOWER SILL PER SRM 51-42-11.

Part: FITTING — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUT OUT LOWER CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23L. REPLACED CENTER SHAPE FITTING PER SRM 51-72-11.

Part: DOOR SILL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUTOUT LOWER SILL AT FR 66 AND S23L. REPAIRED LOWER SILL PER SRM 53-41-14-300-001.

Part: FITTING — CRACKED (ZONE 200 - FUSE) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING FASTENER HOLE H3 OF DOOR STOP #7 AND FR 16 RIGHT. REPLACED INTERCOSTAL FITTING PER SRM 51-42-11.

Part: FRAME — CRACKED (ZONE 200 - FUSE) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FASTENER HOLE #8 IN THE DOUBLE JOGGLE AREA AT FR 16 BETWEEN S10R AND S11R. REPAIRED FRAME PER EA 348278A

Part: FITTING — CRACKED (ZONE 200 - FUSE) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING FASTENER HOLE H3 FOR DOOR STOP #7 AT FR 16 BETWEEN S10L AND S11L. REPLACED INTERCOSTAL FITTING PER SRM 51-42-11.

Part: FITTING — CRACKED (ZONE 200 - FUSE) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 BETWEEN S21L AND S22L AT DOOR STOP #1 FASTENER HOLE #3. REPLACED INTERCOSTAL FITTING PER SRM 51-42-11.

Part: FITTING — WORN (ZONE 100 - FUSE) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: AVIONICS COMPARTMENT RACK 80VU LEFT HAND LOWER LATERAL FITTING WORN BETWEEN FR 23 AND FR 24 AT S32L. REPLACED FITTING PER EA 348350.

Part: FRAME — CRACKED (ZONE 200 - FUSE) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AFT FACE FRAME WEB HORIZONTAL FLANGE LOWER RADIUS AT FR 68 AND S22R AT THE #1 DOOR STOP FITTING. REPAIRED FRAME PER EA 348419.

Part: FITTING — WORN (ZONE 100 - FUSE) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: AVIONICS COMPARTMENT RACK 80VU RIGHT HAND LOWER LATERAL FORKEND FITTING WORN BETWEEN FR 23 AND FR 24 AT S32R. REPLACED FORKEND FITTING PER EA 348350.

Part: WINDOW FRAME — CRACKED (ZONE 200 - FUSE) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD RIGHT HAND CENTER POST FRAMING LOWER RADII CRACKED AT FR 2 AND Y0. REPAIRED FRAME PER EA 348298.

Part: WINDOW FRAME — CRACKED (ZONE 200 - FUSE) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD LEFT HAND CENTER POST FRAMING UPPER RADII CRACKED AT FR 2 AND Y0. REPAIRED FRAME PER EA 348298.

Part: FRAME — CRACKED (ZONE 200 - FUSE) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AFT FACE FRAME WEB HORIZONTAL FLANGE LOWER RADIUS AT FR 68 AND S22L AT THE #1 DOOR STOP FITTING. REPAIRED FRAME PER EA 348423.

Part: WINDOW FRAME — CRACKED (ZONE 200 - FUSE) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD LEFT HAND CENTER POST FRAMING LOWER RADII CRACKED AT FR 2 AND Y0. REPAIRED FRAME PER EA 348298.

Part: FITTING — CRACKED (ZONE 200 - FUSE) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING CRACKED BETWEEN FR 1 AND FR 2 AT Y0. REPLACED CONTINUITY FITTING PER EA 348298.

Part: WINDOW FRAME — CRACKED (ZONE 200 - FUSE) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD RIGHT HAND CENTER POST FRAMING UPPER RADII CRACKED AT FR 2 AND Y0. REPAIRED FRAME PER EA 348298.

Part: SKIN PANEL — DENTED (ZONE 100 - FUSE) · airframe 73,381 hrs · 33,706 cycles

AIRCRAFT IN BASE MAINTENANCE: DENT LOWER SKIN LOCATED BETWEEN FR 68 AND FR 69, BETWEEN S42L AND S43L. REPAIRED SKIN PER SRM 53-41-11-300-016.

Part: LEVER — STICKING (ZONE 800 - DOORS) · airframe 71,434 hrs · 32,553 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT REAR DOOR ARMING LEVER HARD TO MOVE. MAINTENANCE CLEANED AND LUBED RIGHT REAR DOOR ARMING LEVER PER AMM 12-22-52. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: FLASHLIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 70,849 hrs · 32,164 cycles

AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT LED NOT FLASHING BY DOOR 1L LEFT SIDE. REPLACED FLASHLIGHT.

Part: LIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 70,501 hrs · 31,950 cycles

AIRCRAFT WAS GROUNDED: AFT CABIN EMERGENCY LIGHTS MISSING MULTIPLE BULBS. REMOVED AND REPLACED RIGHT AND LEFT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY (AALA202208032725) AND UPPER AFT MID CABIN OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY (AALA202208030977).

Part: LIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 70,501 hrs · 31,950 cycles

AIRCRAFT WAS GROUNDED: AFT CABIN EMERGENCY LIGHTS MISSING MULTIPLE BULBS. REMOVED AND REPLACED RIGHT AND LEFT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY (AALA202208032725) AND UPPER AFT MID CABIN OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY (AALA202208030977).

Part: LIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 70,501 hrs · 31,950 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD OVERHEAD MID CABIN EMERGENCY LIGHT ASSEMBLY HAS SEVERAL LIGHTS NOT LED LIGHT OUT. REMOVED AND REPLACED FORWARD OVERHEAD MID CABIN EMERGENCY LIGHT ASSEMBLY PER AMM 33-51-17.

Part: BULB — OUT OF ADJUST (ZONE 200 - FUSE) · airframe 69,368 hrs · 31,290 cycles

AIRCRAFT WAS GROUNDED: AFT MAIN AISLE OVERHEAD EXIT SIGN INOPERATIVE. ADJUSTED BULBS PER A319/1320 AMM 33-51-16.

Part: COMPUTER — NONE (ZONE 100 - FUSE) · airframe 69,273 hrs · 31,230 cycles

AIRCRAFT WAS GROUNDED: AIRCRAFT RETURNED TO DFW AND DECLARED AN EMERGENCY DUE TO A CAPTAINS AOA PROBE INOPERATIVE MESSAGE AND A CAPTAINS PITOT PROBE INOPERATIVE MESSAGE. MAINTENANCE REPLACED #1 PROBE HEAT CONTROL COMPUTER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 30-31-34.

Part: NONE — NONE · airframe 68,613 hrs · 30,827 cycles

AIRCRAFT WAS GROUNDED: LOW SPEED REJECTED TAKEOFF DUE TO INABILITY TO STEER TO CENTERLINE. AIRCRAFT WAS VEERING TO RIGHT. MAINTENANCE TROUBLESHOT PER TSM 32-51-00-810-823-A. PREFORMED FUNCTION TEST OF NOSE WHEEL STEERING PER AMM 32-51-00. TAXI CHECK GOOD. NO DEFECTS NOTED TO NOSE LANDING GEAR OR TIRES. NO HISTORY NOTED. AIRCRAFT OK FOR RETURN TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,168 hrs · 30,583 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT BATTERY AT 13WL REQUIRED REPLACEMENT, PER JOB CARD 26L00005005. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY AT 13WL PER AMM 33-51-38.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 68,130 hrs · 30,556 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTED ALL EMERGENCY "EXIT" LIGHTS ON CABIN DOORS ILLUMINATED. NO OTHER EMERGENCY LIGHTS IN CABIN ILLUMINATED. PURSER PANEL EMERGENCY BUTTON VERIFIED OFF. ACCOMPLISHED TSM 33-51-00 AND FOUND BATTERY PACK AT 10WL FAULTED. REPLACED BATTERY PACK AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.

Part: BATTERY — INOPERATIVE (FWD FLASHLIGHT) · airframe 67,559 hrs · 30,251 cycles

AIRCRAFT WAS NOT GROUNDED: NUMBER 1 FLIGHT ATTENDANT FLASHLIGHT DOES NOT FLASH. REPLACED BATTERY PER AMM 25-65-00.

Part: FLASHLIGHT — INOPERATIVE (MID CABIN) · airframe 67,120 hrs · 30,011 cycles

AIRCRAFT WAS NOT GROUNDED: 2R FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT PER AMM 25-60-00.

Part: SIGN — INOPERATIVE (CABIN) · airframe 67,102 hrs · 30,003 cycles

AIRCRAFT WAS NOT GROUNDED: LIGHT BULB OUT EMERGENCY EXIT SIGN OVERHEAD BETWEEN DOORS 1L AND 1R. REPLACED EMERGENCY EXIT LIGHT FIXTURE PER AMM 33-51-16.

Part: VALVE — DEFECTIVE (OIL SYSTEM) · airframe 66,341 hrs · 29,570 cycles

AIRCRAFT WAS GROUNDED: ON TAKEOFF AT 1500 THE ECAM ENG2 BEARING 4 OIL SYS (PRESS HI) CAME ON FOR ABOUT TWO MINUTES, THEN WENT OUT. THE AIRCRAFT RETURNED TO DFW, WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. REPLACED NR 2 ENGINE, NR 4 BEARING COMPARTMENT SCAVENGE VALVE, AND ACCOMPLISHED A SATISFACTORY LEAK/OPERATIONAL CHECK PER AMM 79-23-51.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 66,003 hrs · 29,385 cycles

AIRCRAFT NOT GROUNDED - FORWARD FLIGHT ATTENDANT FLASHLIGHT INOP. FWD F/A FLASHLIGHT AUTHORIZED 14JUL2020T1335Z. REMOVED AND REPLACED FLASHLIGHT BATTERY, OPERATIONAL CHECK GOOD. CLEARED MEL.

Part: UNKNOWN — MALFUNCTIONED (AUTOPILOT SYS) · airframe 65,661 hrs · 29,217 cycles

AIRCRAFT NOT GROUNDED: DURING APPROACH UPON GLIDE SCOPE INTERCEPT, A/C FAILED TO CAPTURE WITH AUTOPILOT AND AUTO THRUST DID NOT HOLD AIR SPEED. LANDEDWITH MANUAL CONTROL OF THRUST UNEVENTFULLY NOTED ELAC 2 MSG AT BLOCK IN. T/S FOUND ELAC 2 REPORTING RT OK. C/W AFS TEST 22-96-00-0501 AND LAND CAT III CAPABILITY TEST F/C GOOD PASSED TESTS OK FOR SERVICE AT THIS TIME IAW AMM 22-97-00-0501.

Part: BUSHING — WORN (MLG) · airframe 64,390 hrs · 28,503 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS AFTER T/O FROM KPIT, THE LANDING GEAR LVR INITIALLY WOULDN'T RAISE. 2ND ATTEMPT HANDLE RAISED & ALL GEAR DOORS WOULDN'T CLOSE. THE GEAR SHOWED RETRACTED, BUT THERE WAS A VIBRATION & MOMENTS LATER ECAM STATED "DOORS NOT CLOSE" WHICH HAD CREW RECYCLE GEAR HANDLE. AFTER GEAR WAS RECYCLED THE FOLLOWING ECAM " L/G GEAR NOT UPLOCKED" SHOWED & ALL GEAR INDICATIONS WERE NORMAL. CREW PETURNED TO KPIT. MAINTENANCE FOUND BUSHED LEVER & BOLT WORN ON FLIGHT / GROUND SENSING MECHANISM. REMOVED & REPLACED BUSHED LEVER & BOLT ON FLIGHT / GROUND SENSING MECHANISM IAW AMM 32-21-45. ADJ NLG PROX SENSORS 24GA & 25GA IAW AMM 32-31-73. ACCOMPLISHED SATISFACTORY FUNCTIONAL TEST OF THE EXTENSION & RETRACTION OF THE LANDING GEAR IAW AMM 32-30-00-867-001-A.

Part: LIGHT — BROKEN (SEAT 24C) · airframe 62,379 hrs · 27,359 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 24C EMERGENCY PATH LIGHT BROKEN. MAINTENANCE REPLACED LIGHT PER AMM 33-51-18.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 64,345 hrs · 28,477 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS CABIN DOOR (1L) ARM HANDLE MAY NEED ADJUSTMENT. DOOR ARMS W/ HANDLE ARMED BUT UNSEATS SLIGHTLY ONCE PUSHED DOWN. MAINTENACNE INSTALLED NEW ESCAPE SLIDE AT L1 DOOR IAW JOB CARD 26L00025010.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 62,379 hrs · 27,359 cycles

FA FLASHLIGHT 1L DOOR INOPERATIVE. REPLACED THE BATTERY IAW AMM 25-60-00.

Part: RELAY — FAULTED (MLG) · airframe 61,809 hrs · 27,019 cycles

LANDING GEAR DID NOT EXTENDED, CYCLED THE GEAR AND POSITIVE GEAR EXTENSION. REPLACED THE LANDING GEAR RELAY IAW AMM, SWUNG THE LANDING GEAR, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK IAW AMM 32-32-00-810-A.

Part: UNKNOWN — ODOR (CABIN) · airframe 61,809 hrs · 27,019 cycles

ABOVE 10000 FT, FLIGHT ATTENDANT REPORTED A BURNING FROM FORWARD GALLEY OVEN 1 ODOR LIKE HAIR OR PLASTIC. A PILOT IN BUISNESS CLASS CAME FORWARD AND SMELLED NOTHING. COCKPIT SMELLED NOTHING. SHE SMELLED IT FROM TAKE OFF THROUGH 10,000FT. FORWARD GALLEY OVEN C/B COLLARD. PERFORMED OPERATIONS CHECK ON FORWARD GALLEY OVEN 1. NO BURNING SMELL. OPERATIONS CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (BRAKE SYS) · airframe 61,250 hrs · 26,661 cycles

AFTER TAKEOFF, IMMEDIATELY AFTER GEAR RETRACTION, AN ECAM MESSAGE APPEARED FOR BRAKES AUTOBRAKE FAULT BRAKES RELEASED. MAINTENANCE ACCOMPLISHED A SATISFACTORY RESET OF BRAKE SYSTEM CONTROL UNIT IAW TSM 24-00-00, NO FAULTS DISPLAYED.

Part: LENS — MISSING (CABIN) · airframe 60,805 hrs · 26,467 cycles

AIRCRAFT WAS NOT GROUNDED: R1 EMERGENCY EXIT LIGHT LENS MISSING. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT LENS PER AMM 33-51-13 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: WIRE — BROKEN (BOOST PUMP) · airframe 60,421 hrs · 26,269 cycles

CENTER FUEL TANK PUMP 1 WAS INOPERATIVE. THE PUMP DOES NOT AUTO SHUT OFF, ALWAYS STAYS CROSSED AND AMBER IN AUTO MODE, MANUAL WORKED GOOD. FOUND WIRE 3154-1358 BROKEN IN 2M BUNDLE. REPAIRED THE WIRE IAW ESPM 20-53-21. OPS CHECKED GOOD IAW AMM 28-21-00-710-005A.

Part: GIRT BAR — BINDING (GALLEY DOOR) · airframe 60,319 hrs · 26,226 cycles

FORWARD GALLEY DOOR GIRT BAR IS HARD TO STOW AND UNSTOW. INSTALLED THE FORWARD GALLEY DOOR GIRT BAR IAW AMM 25-66-01-000-804.

Part: PUMP — LOW PRESSURE (FUEL BOOST) · airframe 60,319 hrs · 26,226 cycles

LOW PRESSURE INDICATION FOR THE NR 1 CENTER TANK FUEL PUMP. REPLACED THE CENTER TANK NR 1 FUEL PUMP IAW MM 28-21-51.

Part: LIGHT — INOPERATIVE (SEAT 9C) · airframe 59,422 hrs · 25,716 cycles

BLUE EMERGENCY LIGHT INOPERATIVE ON SEAT 9C. REPLACED THE EMERGENCY LIGHT.

Part: DOOR FRAME — CRACKED · airframe 58,749 hrs · 25,374 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CRACKED L1 DOOR FRAME 16 NR 1 DOOR STOP FITTING BOTTOM INBOARD HOLE AT S24L. REPAIRED DOOR FRAME PER SRM 51-73-12 AND EA 274070.

Part: PLATE — WORN (RT WING) · airframe 58,749 hrs · 25,374 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. SURFACE WEAR ON RIGHT WING UNDER PYLON FIXED FAIRING BOTTOM WING SKIN PANEL NR 3, PYLON LINE REINFORCING PLATE. REMOVED AND REPLACED PLATE PER SRM 57-21-11.

Part: FLOORBEAM — CORRODED (FRAME 66) · corrosion level 2 · airframe 58,749 hrs · 25,374 cycles

CORROSION ON THE FLOORBEAM AT FRAME 66, Y1292, Z-500. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11 AND SRM 51-72-11.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 58,749 hrs · 25,374 cycles

DELAMINATION FOUND ON THE RIGHT ELEVATOR UPPER SKIN, 16 INCHES FROM TRAILING EDGE AND 68 INCHES FROM INBOARD END. REPAIRED THE ELEVATOR SKIN IAW SRM 55-21-11-300-004.

Part: SKIN — CONTAMINATED (RT ELEVATOR) · airframe 58,749 hrs · 25,374 cycles

WATER INGRESS INDICATION ON RIGHT ELEVATOR UPPER SKIN 20 INCH FROM AFT EDGE AND 101 FROM OUTBOARD EDGE. REPAIRED ELEVATOR IAW SRM 55-21-11-300-005.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 58,749 hrs · 25,374 cycles

CORROSION ON AFT CABIN FLOOR SUPPORT BETWEEN FRAMES 64 AND 70, Y765, Z-500. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11.

Part: MOUNT — CORRODED (R2 DOOR GIRT BAR) · corrosion level 2 · airframe 58,749 hrs · 25,374 cycles

CORROSION ON THE R2 DOOR SILL FORWARD GIRT BAR MOUNT AREA AT FRAME 66, Y-1400. REPAIRED DOOR GIRT BAR MOUNT IAW SRM 53-41-14.

Part: FLOORBEAM — CORRODED (FRAME 16) · corrosion level 2 · airframe 58,749 hrs · 25,374 cycles

CORROSION ON CABIN FLOORBEAM AT FRAME 16, Y1292, Z-500. REMOVED AND REPLACED FLOORBEAM IAW SRM 53-11-14 AND DRAWING D5311281300251.

Part: FLOORBEAM — CORRODED (FRAME 66) · corrosion level 2 · airframe 58,749 hrs · 25,374 cycles

CORROSION FOUND ON THE AFT CABIN FLOORBEAM AT FRAME 66, Y-765, Z-500. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-72-11.

Part: FITTING — CORRODED (FRAME 69) · corrosion level 2 · airframe 58,749 hrs · 25,374 cycles

CORROSION ON THE L2 DOOR SILL FITTING AT FRAME 69, Y1732. REMOVED AND REPLACED THE DOOR SILL FITTING IAW SRM 51-72-11, AND SRM 51-42-11.

Part: BEAM — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 58,749 hrs · 25,374 cycles

CORROSION ON AFT CABIN LEFT Z BEAM FROM FRAMES 66 TO 68, Y1292, Z-500. REMOVED AND REPLACED THE BEAM IAW SRM 51-42-11 AND SRM 51-72-11.

Part: DOOR SILL — CORRODED (FRAME 68) · corrosion level 2 · airframe 58,749 hrs · 25,374 cycles

CORROSION ON THE L2 DOOR SILL PLATE AT FRAME 68, Y1400, Z-500. REMOVED AND REPLACED THE DOOR SILL PLATE IAW SRM 51-72-11, SRM 51-42-11, SRM 51-75-12, AND DRAWING D53480505.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · corrosion level 2 · airframe 58,749 hrs · 25,374 cycles

CORROSION ON THE AFT CABIN FLOOR SUPPORT BETWEEN FRAMES 66 AND 70, Y-765, Z-500. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, SRM 51-42-11, AND SRM 53-21-14.

Part: BEAM — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 58,749 hrs · 25,374 cycles

CORROSION ON AFT CABIN LEFT Z BEAM BETWEEN FRAMES 64 AND 66, Y1292, Z-500. REMOVED AND REPLACED THE BEAM IAW SRM 51-42-11, AND SRM 51-72-11.

Part: BEAM — CORRODED (FRAME 66-68) · corrosion level 2 · airframe 58,749 hrs · 25,374 cycles

CORROSION ON RIGHT Z BEAM BETWEEN FRAMES 66 AND 68, Y-1162.5, Z-500. REMOVED AND REPLACED THE BEAM IAW SRM 51-42-11, SRM 53-41-14, AND DRAWING 53472780000.

Part: BEAM — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 58,749 hrs · 25,374 cycles

CORROSION ON AFT CABIN RIGHT Z BEAM BETWEEN FRAMES 64 AND 66, Y-1292, Z-500. REMOVED AND REPLACED THE BEAM IAW SRM 51-42-11 AND SRM 53-00-14.

Part: FITTING — CORRODED (FRAME 20) · corrosion level 2 · airframe 58,749 hrs · 25,374 cycles

CORROSION ON R2 DOOR SILL AFT CORNER SHAPE FITTING AT FRAME 20, Y-1584, Z-500. REMOVED AND REPLACED THE FITTING IAW SRM 51-42-11.

Part: FRAME — CRACKED (FRM 35) · airframe 58,749 hrs · 25,374 cycles

CRACK INDICATIONS ON FRAME 35, STRINGER 30R, BOTTOM AFT FASTENER HOLES. REPAIRED THE FRAME IAW EA 273448.

Part: FRAME — CRACKED (FRM 35) · airframe 58,749 hrs · 25,374 cycles

CRACK INDICATIONS ON FRAME 35, STRINGER 30L, BOTTOM AFT FASTENER HOLE. REPAIRED THE FRAME IAW EA 273447, AND SRM 51-21-00

Part: OUTLET — BURNED (CABIN) · airframe 58,539 hrs · 25,283 cycles

NR 1 FLIGHT ATTENDANT REPORTED A SMELL IN FIRST CLASS DESCENDING THROUGH 10,000 FT. FOUND BURNT POWER PORT AT 1C. REPLACED POWER PORT AT SEAT 1C IAW AMM 25-21-11.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 58,345 hrs · 25,171 cycles

CABIN EMERGENCY LIGHTS INOPERATIVE AT ROWS 24 AND 25. REPAIRED THE WIRING AT POWER CONNECTOR FOR ROWS 24 & 25 IAW ESPM.

Part: PUMP — WARNING MESSAGE (RT FUEL) · airframe 58,255 hrs · 25,130 cycles

RT FUEL PUMP FAULT FOR LOW PRESSURE. FAULT ACTIVATED, AFTER 1 MINUTE WENT OFF. PUMP DID CYCLE OFF THEN ON. FUEL TEMP WAS ABNORMALLY COLD COMPARED TO OTHER TANKS. REPLACED THE NR 2 FUEL LEVEL SENSING CONTROL UNIT AS APRECAUTION IAW MM 28-46034, AND 28-46-00. OPS CHECKED GOOD.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 58,098 hrs · 25,059 cycles

EMERGENCY LIGHT LENS AT SEAT 26C DETACHED.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 57,513 hrs · 24,728 cycles

FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED THE LENS.

Part: GIRT BAR — OBSTRUCTED (R2 DOOR) · airframe 57,355 hrs · 24,637 cycles

AFT R2 DOOR SLIDE DOES NOT SHOW ARMED ON ECAM SYSTEM DISPLAY. FLIGHT ATTENDANT REPORTS THAT ARMING LEVER FEELS LIKE IT POPS UP WHEN ARMING. FOUND TRASH ON GIRT BAR ASSEMBLY. CLEARED GIRT BAR AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: MECHANISM — SEIZED (DOOR ARMING) · airframe 57,207 hrs · 24,548 cycles

L1 DOOR WILL NOT ARM. REMOVED DEBRIS AND LUBRICATED ARMING MECHANISM, DOOR ARMS AND OPERATES NORMALLY.

Part: APU — LEAKING (ZONE 100) · airframe 56,354 hrs · 24,114 cycles

AIRCRAFT WAS GROUNDED. STRONG DIRTY SOCK SMELL THROUGHOUT CABIN WHEN APU BLEED TURNED ON. MAINTENANCE FOUND APU LEAKING INTERNALLY. REPLACED APU PER JOB CARDS 26L00201001, 26L00021002 AND 26L00021004.

Part: FITTING — OUT OF ADJUST (R2 DOOR GIRT BAR) · airframe 55,622 hrs · 23,731 cycles

R2 DOOR DISARMS INFLIGHT BY ITSELF. AIRCRAFT GROUNDED. ADJUSTED R2 DOOR GIRT BAR FITTING CLEARANCE IAW AMM 52-13-22 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: GIRT BAR — OBSTRUCTED (PAX DOOR) · airframe 55,345 hrs · 23,587 cycles

TWICE DURING FLIGHT AT CRUISE ALTITUDE, (FL350) CONTINUOUS LIGHT TURBULANCE, THE AFT RIGHT CABIN DOOR HANDLE MOVED ENOUGH TO DISARM THE SLIDE. ACCOMPLISHED TSM 52-13-00-800-804-A AND COULDN'T REPRODUCE FAULT. REMOVED DEBRIS & TAPE FROM UNDER GIRT BAR/ GIRT BAR CLIPS. PERFORMED A SATISFACTORY OPERATIONAL CHECK OF THE DOOR WARNING SYSTEM PER AMM 52-71-00-710-001-A.

Part: LENS — LOOSE (CABIN) · airframe 54,384 hrs · 23,081 cycles

AIRCRAFT WAS NOT GNDED. DOOR 2L EXIT PATH LIGHT UNDER EXIT SIGN HAS BLUE TAPE ON IT. SECURED LENS & OPERATIONAL CHECKED GOOD.

Part: BEAM — CRACKED (FUSELAGE) · airframe 53,360 hrs · 22,540 cycles

RIGHT SIDE BOX BEAM, AFT FASTENER HOLE, UPPER FLANGE CRACKED AT FRAME 43 & -Y1622. REPAIRED IAW EO 5315Y066.

Part: BEAM — CRACKED (FUSELAGE) · airframe 53,360 hrs · 22,540 cycles

LEFT SIDE BOX BEAM, AFT FASTENER HOLE, UPPER FLANGE CRACKED AT FRAME 43 & Y1622. REPAIRED IAW EO 5315Y066.

Part: GIRT BAR — DEFECTIVE (R1 DOOR) · airframe 51,708 hrs · 21,577 cycles

GIRT BAR ON R1 DOOR MISSING INDICATOR. REPLACED GIRT BAR IAW AMM 25-62-44-000-002A.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 51,466 hrs · 21,462 cycles

C11 CHECK, RT WING FUEL PANEL 640JB LOCATED BETWEEN RIB 14 & 15, STRINGER 8 & 11 HAS CORROSION & WEAR ON SEVERAL COUNTERSINK FASTENER HOLES. FUEL PANEL WAS REPLACED IAW TASK CARD 26T60057033.

Part: SCREW — LOOSE (RUDDER PEDAL) · airframe 48,986 hrs · 20,053 cycles

CREW REPORTED RUDDER PEDALS FELT JAMMED, FREED UP AFTER LANDING. FOUND LOOSE SCREW LOCATED AT CAPTAIN'S RUDDER PANEL, SECURED SAME. CYCLED RUDDER PEDALS. NO DISCREPANCIES NOTED.

Part: COFFEEMAKER — SPARKS (GALLEY) · airframe 47,561 hrs · 19,466 cycles

F/A REPORTS THAT THE NR 1 AFT COFFEEMAKER SPARKS AND POPS. MAINTENANCE R & R NR 1 AFT COFFEEMAKER IAW AMM 25-35-15.

Part: THRESHOLD — DIRTY (R2 DOOR) · airframe 47,553 hrs · 19,462 cycles

R2 DOOR WILL NOT OPEN. CLEANED DEBIS FROM THRESHOLD.

Part: KNOB — BROKEN (SEAT) · airframe 46,737 hrs · 19,081 cycles

CREW REPORTED THE CAPTAIN'S ELECTRIC SEAT KNOB TO SLIDE FWD AND BACK, BROKEN. MX REINSTALLED CONTROL KNOB ON CAPTAIN'S FORWARD/AFT SWITCH. REF ESPM 20-45.

Part: O-RING — LEAKING (APU OIL SYS) · airframe 46,133 hrs · 18,808 cycles

CREW COMPLAINED OF A CABIN ODOR ISSUE (DIRTY SOCK ODOR) WHEN THE APU WAS STARTED, BEFORE BOARDING OF FLIGHT. MX FOUND SMALL LEAK OF OIL FROM APU OIL SCAVENGE FILTER HOUSING. REPLACED TWO O-RINGS. LEAK CHECKED OK. ALSO, REPLACED FWD CARGO SELECTOR VALVE FOR SUSPECT LEAK. ACCOMPLISHED DECONTAMINATION. NO ODOR NOTED AFTER REPAIRS.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 45,089 hrs · 18,338 cycles

CREW REPORTED EXIT SIGN 1R INOPERATIVE. MAINTENANCE RESECURED EXIT SIGN COVER AT 1R. OPS CHECK GOOD.

Part: LENS — MISSING (CABIN) · airframe 44,839 hrs · 18,232 cycles

MAINTENANCE REPORTED THE EMERGENCY LIGHT LENS MISSING AT ROW 22 LEFT. MAINTENANCE REPLACED MISSING EMERGENCY LIGHT LENS AT ROW 22 LEFT.

Part: WIRE HARNESS — INOPERATIVE (CABIN) · airframe 44,766 hrs · 18,203 cycles

EMERGENCY PATH LIGHT AT ROW 22L INOPERATIVE. REMOVED AND REPLACED SEAT HARNESS IAW AIRBUS MAINTENANCE MANUAL 33-51-19.

Part: WIRE HARNESS — FAULTY (CABIN) · airframe 44,760 hrs · 18,198 cycles

MAINTENANCE REPORTED THE EMERGENCY PATH LIGHT AT ROW 22L IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED SEAT HARNESS. REFERENCE AMM 33-51-19, PB 401. OPS GOOD PER AMM 33-51-00-710-001A.

Part: WIRE — DAMAGED (CABIN) · airframe 42,249 hrs · 17,076 cycles

SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE 10R. REPAIRED WIRING SEAT MOUNTED EMERGENCY LIGHT 10. OPS CHECKED GOOD.

Part: WIRE — DAMAGED (CABIN) · airframe 42,249 hrs · 17,076 cycles

SEAT MOUNTED EMERGENCY LIGHT ON 8R INOPERATIVE. REPAIRED WIRING SEAT MOUNT EMERGENCY LIGHT 8R. OPS CHECKED GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,348 hrs · 16,672 cycles

S2 CHECK - CORROSION ON SEAT TRACK BETWEEN FR47 TO FR58, Y1292. REPLACED SEAT TRACK BETWEEN FR47 TO FR58, Y1292 IAW A319 SRM 53-41-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,348 hrs · 16,672 cycles

S2 CHECK - CORROSION ON SEAT TRACK AT FR55, -Y1292. REPLACED SEAT TRACK AT FR55, -Y1292 IAW A319 SRM 53-41-15, FIG 101 & SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,348 hrs · 16,672 cycles

S2 CHECK - CORROSION ON SEAT TRACK LUG AT FR58, -Y765. REPLACED SEAT TRACK AT FR58, -Y765 IAW A319 SRM 51-42-11 & 53-41-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,348 hrs · 16,672 cycles

S2 CHECK - CORROSION ON SEAT TRACK AT FR56, -Y1292. REPLACED SEAT TRACK AT FR56, -Y1292 IAW A319 SRM 53-41-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,348 hrs · 16,672 cycles

S2 CHECK - CORROSION ON SEAT TRACK BETWEEN FR53 TO FR54, -Y1292. REPLACED SEAT TRACK BETWEEN FR53 TO FR54, -Y1292 IAW A319 SRM 53-41-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,348 hrs · 16,672 cycles

S2 CHECK - CORROSION ON SEAT TRACK AT FR52, -Y1292. REPLACED SEAT TRACK AT FR52, -Y1292 IAW A319 SRM 53-41-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,348 hrs · 16,672 cycles

S2 CHECK - CORROSION ON SEAT TRACK BETWEEN FR56 TO FR57, -Y1292. REPLACED SEAT TRACK BETWEEN FR56 TO FR57, -Y1292 IAW A319 SRM 53-41-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,348 hrs · 16,672 cycles

2S CHECK - CORROSION ON SEAT TRACK BETWEEN FR44 AND FR45, -Y1292. REPLACED SEAT TRACK BETWEEN FR44 AND FR45, -Y1292 IAW A319 SRM 53-31-15, 51-42-11, 51-44-11, 51-46-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 41,348 hrs · 16,672 cycles

2S CHECK - CORROSION ON FLOOR PANEL 262FF BETWEEN FR66 TO FR68 & BETWEEN -Y1292 TO -Y 1753. REPLACED FLOOR PANEL 262FF IAW A319 SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 41,348 hrs · 16,672 cycles

2S CHECK - DELAMINATION ON CABIN FLOOR PANEL BETWEEN FR66 TO FR68, Y1292. REPAIRED CABIN FLOOR PANEL BETWEEN FR66 TO FR68, Y1292 IAW A319 SRM 53-02-00.

Part: FLOOR PANEL — DEBONDED (CARGO BAY) · airframe 41,348 hrs · 16,672 cycles

2S CHECK - DISBONDED AFT CARGO FLOOR PANEL 151DE BETWEEN FR56 TO FR58, BETWEEN S35L TO S38L. REPLACED AFT CARGO FLOOR PANEL 151DE IAW A319 SRM 53-02-00 FIGURE 209.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 41,348 hrs · 16,672 cycles

2S CHECK - CRACK ON CABIN FLOOR PANEL 222CF BETWEEN FR16 TO FR20, -Y765. REPLACED CABIN FLOOR PANEL 222CF IAW A319 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 41,348 hrs · 16,672 cycles

2S CHECK - DELAMINATION ON AFT CARGO FLOOR PANEL 161FF BETWEEN FR63 TO FR65, BETWEEN S31L TO S35L. REPLACED AFT CARGO FLOOR PANEL 161FF IAW A319 SRM 53-02-00 FIGURE 209.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 41,348 hrs · 16,672 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 221DF BETWEEN FR20 TO FR24, Y0. REPLACED FLOOR PANEL 221DF IAW A319 SRM 53-02-00 FIGURE 209.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 41,348 hrs · 16,672 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 231BF BETWEEN FR24 TO FR25, Y=0. REPLACED FLOOR PANEL 231BF IAW A319 SRM 53-02-00 FIGURE 209.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 41,348 hrs · 16,672 cycles

2S CHECK - DELAMINATION ON FORWARD CARGO FLOOR PANEL 131CF BETWEEN FR24 TO FR28, BETWEEN S31L TO S35L. REPLACED CARGO FLOOR PANEL 131CF IAW A319 SRM 53-02-00 FIGURE 209.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 41,348 hrs · 16,672 cycles

S2 CHECK - DELAMINATION CARGO FLOOR PANEL 151UG BETWEEN FR47 TO FR53, S38L. REPLACED FLOOR PANEL 151UG IAW A319 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 41,348 hrs · 16,672 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 222EF BETWEEN FR20 T0 FR24, -Y765. REPLACED FLOOR PANEL 222EF IAW A319 SRM 53-02-00 FIGURE 209.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 41,348 hrs · 16,672 cycles

S2 CHECK - DELAMINATION CARGO FLOOR PANEL 161DF BETWEEN FR63 TO FR65 & BETWEEN S38L TO S38R. REPLACED FLOOR PANEL 161DF IAW A319 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 41,348 hrs · 16,672 cycles

S2 CHECK - DELAMINATION CARGO FLOOR PANEL 131CG BETWEEN FR28 TO FR53 & BETWEEN S38L S38R. REPLACED FLOOR PANEL 131CG IAW A319 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 41,348 hrs · 16,672 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 251JF BETWEEN FR51 TO FR54, BETWEEN Y1292 TO Y1732. REPLACED FLOOR PANEL 251JF IAW A319 SRM 53-02-00 FIGURE 209.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 41,348 hrs · 16,672 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 252JG BETWEEN FR62 TO FR64, BETWEEN -Y1292 TO -Y1732. REPLACED FLOOR PANEL 252JG IAW A319 SRM 53-02-00 FIGURE 209.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 41,348 hrs · 16,672 cycles

S2 CHECK - CRACK ON FLOOR PANEL 262BG BETWEEN FR64 TO FR66, BETWEEN -Y254 TO -Y1732. REPLACED FLOOR PANEL 262BG IAW A319 SRM 53-02-00 FIGURE 209.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 41,348 hrs · 16,672 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 252HG BETWEEN FR59 TO FR62, -Y1292 TO -Y1732. REPLACED FLOOR PANEL 252HG IAW A319 SRM 53-02-00 FIGURE 209.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,348 hrs · 16,672 cycles

S2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON DOOR SILL AT FR68, Y1975. REPAIRED DOOR SILL AT FR68, Y1975 IAW A319 SRM 53-41-14, 51-21-11 & NTM 51-00-19 P 6.

Part: CONTROL UNIT — MALFUNCTIONED (GROUNG POWER) · airframe 40,377 hrs · 16,237 cycles

YYC-PHX - BURNING SMELL - SMOKE AND ELECTRICAL BURNING SMELL IN COCKPIT. FOUND CIRCUIT BREAKER AB7 GROUND POWER PROTECTION TRIPPED. INSPECTED MAIN E&E BAY, BATTERY BAY, CIRCUIT BREAKER PANELS, AND FORWARD E&E BAY. FOUND BURNING SMELL FROM GPCU. REMOVED AND REPLACED GROUND POWER CONROL UNIT (GPCU) PER AMM 24-41-34-000-001. RESET CIRCUIT BREAKER AB7. PERFORMED TEST OF THE GPCU PER M/M 24-41-00-740-002. OPERATIONAL CHECK GOOD.

Part: WIRE — CHAFED (CABIN) · airframe 40,091 hrs · 16,101 cycles

BOS - EEL - EMERGENCY LIGHTS IN FORWARD ENTRY WAY INOPERATIVE. MAINTENANCE FOUND AND REPAIRED CHAFING WIRE ON SEAT 1 A/C.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,585 hrs · 15,882 cycles

FLT 339 - SJD-PHX - EMERGENCY LIGHTS - EMERGENCY PATH LIGHT AT ROW 14 INOPERATIVE. RE-TERMINATED 7260VC6 REF. ASM 33-51-00.

Part: TRAY — CRACKED (FUSELAGE) · airframe 39,294 hrs · 15,763 cycles

MCN - C11 - MAJOR REPAIR - CRACK ON TRAY BETWEEN FR66 TO FR68, -Z240 BETWEEN Y1865 TO Y1732. REPLACED TRAY BETWEEN FR66 TO FR68, -Z240 BETWEEN Y1865 TO Y1732 IAW A319 SRM 51-42-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 39,294 hrs · 15,763 cycles

MCN - C11 - MAJOR REPAIR - CORROSION ON FLOOR PANEL 222FF BETWEEN FR20 TO FR24, -Z240 & BETWEEN -Y1037 TO -Y1379. REPLACED FLOOR PANEL 222FF BETWEEN FR20 TO FR24, -Z240 & BETWEEN -Y1037 TO -Y1379.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 39,294 hrs · 15,763 cycles

MCN - C11 - MAJOR REPAIR - CRACK ON SHEAR PLATE BETWEEN FR69 TO FR70, -Z240, -Y1260. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, -Z240, -Y1260 IAW A319 SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,294 hrs · 15,763 cycles

MCN - C11 - MAJOR REPAIR - CORROSION ON SEAT RAIL BEAM BETWEEN FR65 TO FR66, -Z240, -Y1292. REPLACED SEAT RAIL BEAM BETWEEN FR65 TO FR66, -Z240, -Y1292 IAW A319 51-49-00.

Part: FITTING — CORRODED (FUSELAGE) · airframe 39,294 hrs · 15,763 cycles

MCN - C11 - MAJOR REPAIR - CORROSION ON ANGLE FITTING AT FR20, -Z240, -Y1292. REPLACED ANGLE FITTING AT FR20, -Z240, -Y1292 IAW A319 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,294 hrs · 15,763 cycles

MCN - C11 - MAJOR REPAIR - CORROSION ON LONGITUDINAL FLOORBEAM BETWEEN FR67 TO FR68, -Z240, -Y1292. REPLACED LONGITUDINAL FLOORBEAM BETWEEN FR67 TO FR68, -Z240, -Y1292 IAW A319 SRM 53-41-14 & 51-49-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,294 hrs · 15,763 cycles

MCN - C11 - MAJOR REPAIR - CORROSION ON LONGITUDINAL FLOORBEAM BETWEEN FR68 TO FR69, -Z240, -Y1292. REPLACED LONGITUDINAL FLOORBEAM BETWEEN FR68 TO FR69, -Z240, -Y1292 IAW A319 SRM 51-49-00.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 37,353 hrs · 14,897 cycles

FLT 80 - PHL - EEL - FLIGHT ATTENDANT REPORTED AFT JUMPSEAT FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT F/A JUMPSEAT FLASHLIGHT BATTERY IAW AIRBUS MAINTENANCE MANUAL 25-65-00.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 35,310 hrs · 14,017 cycles

FLT 321 - ORD - EEL - EMERGENCY LIGHTS AT DOOR 1L & 1R INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY UNIT 10WL AND BATTERY PACK.

Part: EPSU — DISCHARGED (CABIN) · airframe 35,052 hrs · 13,900 cycles

FLT 34 - SLC-PHX - EMERGENCY LIGHTS - EMERGENCY LIGHT SYSTEM AT CIDS PANEL FAILED TEST. REMOVED AND REPLACED FORWARD LEFT EMERGENCY POWER SUPPLY UNIT (EPSU) IAW AMM33-51-38. SYSTEM TESTED GOOD.

Part: DOOR — OBSTRUCTED (L2) · airframe 34,484 hrs · 13,619 cycles

FLT 426 - SEA - PHX - EMERGENCY EQUIPMENT - L2 DOOR SLIDE WILL NOT ARM. REMOVED (FOD) FOREIGN OBJECT DEBRIS FROM L2 DOOR ENTRY AREA, DOOR ARMS NORMAL.

Part: ACTUATOR — FAULTY (ZONE 400) · airframe 34,275 hrs · 13,505 cycles

FLT 204 - OAK-OAK - ABORTED TAKEOFF - ENGINE NR 2 COMPRESSOR VANE FAULT ON TAKEOFF. REJECTED TAKEOFF AT +/- 85 KNOTS. REMOVED AND REPLACED ENGINE NR 2 VSV ACTUATOR PER JOBCARD R5M75303. OPERATIONAL CHECK WAS GOOD.

Part: SWITCH — FAULTY (COCKPIT) · airframe 34,106 hrs · 13,423 cycles

FLT 48 - DCA-LAS - EMERGENCY LIGHTS - FLIGHT ATTENDANT REPORTED EMERGENCY EXIT LIGHTS IN CABIN CAME ON AND WERE FLASHING THEN STAYED ON IN SPITE, FLIGHT DECK SWITCH IN ARMED POSITION. RECYCLE SWITCH TO OFF TWICE BEFORE LIGHTS WOULD STAY OFF IN ARMED POSITION. REMOVED AND REPLACED EMERGENCY LIGHTS SWITCH 4WL. OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 33,626 hrs · 13,228 cycles

FLT 248 - SJC-PHX - EMERGENCY LIGHTS - AFT LEFT POWER SUPPLY FOR EMERGENCY EXIT LIGHTS FAILS TEST ON CIDS. REMOVED AND REPLACED AFT LEFT POWER SUPPLY FOR EMERGENCY LIGHT SYSTEM PER AIRCRAFT MAINTENANCE MANUAL 33-51-38. OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 31,956 hrs · 12,476 cycles

LOGPAGE 8349619 FLT NR 548 LAS-PHX EMERGENCY LIGHT FORWARD FLIGHT ATTENDANT FLASHLIGHT RED LIGHT IS NOT BLINKING. R&R FLASHLIGHT BATTERY IN FORWARD FLIGHT ATTENDANT FLASHLIGHT. OPS CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 30,225 hrs · 11,767 cycles

SAL - EMERGENCY EQUIPMENT - BC6 CHECK - FORWARD FLIGHT ATTENDANTS RIGHT FLASHLIGHT BATTERY LOW. REPLACED THE BATTERY IN THE FORWARD FLIGHT ATTENDANTS RIGHT FLASHLIGHT.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 30,225 hrs · 11,767 cycles

SAL - EMERGENCY EQUIPMENT - BC6 CHECK - FORWARD FLIGHT ATTENDANTS LEFT FLASHLIGHT BATTERY LOW. REPLACED THE BATTERY IN THE FORWARD FLIGHT ATTENDANTS LEFT FLASHLIGHT.

Part: VALVE — FAILED (A/C PACK) · airframe 26,933 hrs · 10,450 cycles

PHL - CREW REPORTED, DURING CLIMB TO F250 PACK 2 TRIPPED. TEMP 32 DEG C ZONE OUTPUT 92 DEG F, PACK FLOW STAYED IN THE LO POSITION. MX REMOVED AND REPLACED NR 2 PACK FLOW CONTROL VALVE PER AMM 21-51-51- 401, OPS/LEAK CHECK WAS GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 25,351 hrs · 9,773 cycles

PHX - EEL - AT MID CABIN, EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED EPSU. OPS CHECK WAS GOOD.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 25,212 hrs · 9,703 cycles

LAS - FWD GALLEY EMERGENCY LIGHTS INOP WITH C/BS H05 AND H06 PULLED. REPLACED BATTERY ASSY ON LEFT FWD EPSU PER MM 33-51-38. OPS CHECK WAS GOOD.

Part: SMOKE DETECTOR — FALSE INDICATION (CARGO BAY) · airframe 24,682 hrs · 9,479 cycles

LAS - FFW - THE PILOT REPORTED A LAV SMOKE AND A CARGO DETECTION FAULT ON THE UPPER ECAM. MAINTENANCE REPLACED LAV (E) AND (D) FILTERS. MAINTENANCE ALSO REPLACED THE FORWARD CARGO DETECTOR (1WH), OPS CHECK WAS GOOD.

Part: SERVO CONTROL — FAILED (LT ELEVATOR) · airframe 23,137 hrs · 8,838 cycles

PHX - VIBRATION - CREW REPORTED AIRFRAME VIBRATION DURING CLIMB AND CRUISE. MAINTENANCE PERFORMED ELEVATOR AND RUDDER FREE PLAY CHECKS IAW AWA TASK CARD I6B27301 AND F6C55302. FOUND THE LEFT BLUE ELEVATOR FREE PLAY IN EXCESS OF .200, WAS AT .220. MAINTENANCE REMOVED AND REPLACED THE LT BLUE ELEVATOR SERVO CONTROL IAW AIRBUS MM 27-34-51-00 AND TASK CARD F6C55302.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,648 hrs · 7,104 cycles

SAL - MAJOR REPAIR - DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM -Y1292 AT FS 66+3". MAINTENANCE REMOVED CORRODED FLOORBEAM -Y1292 FROM FS 64" TO FS 66+5", FABRICATED A NEW REPLACEMENT FLOORBEAM, INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,648 hrs · 7,104 cycles

SAL - MAJOR REPAIR - DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1190 AT FS 68. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1190 FROM FS 67 -5" TO FS 68 +3". FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 18,648 hrs · 7,104 cycles

SAL - MAJOR REPAIR - DURING BC-4 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOOR PANEL AT L-2 DOOR ENTRANCE. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL AT L-2 DOOR ENTRY WAY IAW T/C R1C25306.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,648 hrs · 7,104 cycles

SAL - MAJOR REPAIR - DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1292 AT FR 68 -3". MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 FROM FS 68 -3" TO FS 69. FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 18,648 hrs · 7,104 cycles

SAL - MAJOR REPAIR - DURING BC-4 CHECK FOUND EXFOLIATION CORROSION ON FLOORBEAM Y1292 AT FR 66+3 INCHES. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM Y1292 FROM FR 66+3 INCHES TO FR 64; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,648 hrs · 7,104 cycles

SAL - MAJOR REPAIR - DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1292 AT FS 67+3". MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 FROM FS 67+3" TO FS 68, FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,648 hrs · 7,104 cycles

SAL - MAJOR REPAIR - DURING BC-4 CHECK FOUND EXFOLIATION CORROSION ON UPPER FLANGE OF DUMMY RAIL -Y254 AT FR 20. MAINTENANCE CUT OUT DAMAGE IN UPPER FLANGE OF DUMMY RAIL -Y254 AT FR 20, FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14 FIG 201.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 18,648 hrs · 7,104 cycles

SAL - MAJOR REPAIR - DURING BC-4 CHECK FOUND FLOOR PANEL 251RF DELAMINATED. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 251RF IAW A319 SRM 53-02-00 FIG 209.

Part: RESERVOIR — LEAKING (RT OVERWING) · airframe 13,343 hrs · 5,313 cycles

DURING INSPECTION THE RT OVER WING EMERGENCY EVACUATION SLIDE BOTTLE WAS FOUND TO HAVE LOW PRESSURE. MAINTENANCE REMOVED AND REPLACED THE RT OVER WING EMERGENCY EVACUATION SLIDE BOTTLE IAW AMM 25-62-46-000-001, OPERATIONAL CHECK WAS GOOD. VENDOR TEARDOWN OF R/H OVER WING EMERGENCY EVACUATION SLIDE BOTTLE S/N 4733 CONFIRMED FAILURE OF UNIT. UNIT WAS FOUND TO HAVE LOW PRESSURE DUE TO A LEAK, REPAIRED LEAK AND PERFORMED LEAK CHECK. MAINTENANCE ACCOMPLISHED IAW CMM 25-65-17, REV. 8.

Part: ADC — DEFECTIVE (E/E BAY) · airframe 12,119 hrs · 4,824 cycles

ON CLIMBOUT, EN ROUTE WHLE SELECTING FLAPS UP THE CAPTAINS PRIMARY FLIGHT DISPLAY INDICATED A BROKEN POLE OF 230 KTS, AND THE OVERSPEED WARNING HORN WOULD GIVE A CONTINUOUS ALARM IF THE AIRSPEED EXCEEDED 230 KTS. TURNED BACK TO RDU AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 AIR DATA INERTIAL REFERENCE UNIT (ADIRU) IAW AWA T/C R2A34304, OPERATIONAL CHECK WAS GOOD. VENDOR EVALUATION TEST OF ADIRU S/N 2891 WAS NFF, TEST CONDUCTED IAW CMM TP1011, REV 22.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 11,371 hrs · 4,566 cycles

FLIGHT CREW REPORTED THE AFT RT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT HAS A LOW BATTERY. MAINTENANCE REMOVED AND REPLACED THE AFT RT EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 11,167 hrs · 4,487 cycles

FLIGHT CREW REPORTED THE LT FORWARD GALLEY HAND HELD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT FORWARD GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.

Part: BRAKE ASSY — INOPERATIVE (MAIN) · airframe 10,693 hrs · 4,309 cycles

WHILE TAXING TO GATE, ARRIVING, BRAKES WERE GRABBING AND RELEASING ALMOST UNCONTROLLABLY. MAINTENANCE PERFORMED A BITE CHECK ON BRAKE STEERING CONTROL UNIT (BSCU) 1 AND 2 AND FOUND NO FAULTS. RESET BSCU 1 AND 2 IAW AMM 32-42-00-810-912. BRAKING FUNCTIONS NORMAL DURING MAINTENANCE TAXI. NO GRABBING FELT IN A/C OR RUDDER PEDALS. SUBSEQUENT TROUBLESHOOTING REVEALED THAT ALL 4 BRAKES WERE BLED OF AIR IAW TROUBLE SHOOTING MANUAL AMM 32-42-00-810-912.

Part: CABLE — MALADJUSTMENT (ZONE 844 - DOORS) · corrosion level 0 · airframe 9,517 hrs · 3,875 cycles

MCN - EMERGENCY ESCAPE SYSTEM - DURING B-02 CHECK THE L/H OVER WING EMERGENCY ESCAPE EXIT RELEASE CABLE FAILED TEST. MAINTENANCE ADJUSTED FLEXIBLE CONTROL CABLE ASSEMBLY IAW AMM 25-62-43-420-050, STEP A(9) B, AND STEP 11; TEST WAS GOOD IAW AWA T/C F1C52303.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 8,775 hrs · 3,588 cycles

DURING INSPECTION THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT (12WL) AND BATTERY PACK AT RT OVERWING DOOR IAW AMM 33-51-38-000-001, OPERATIONAL CHECK WAS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 7,641 hrs · 3,129 cycles

SAN - EEL - C - DURING INSPECTION RT OVERWING EMERGENCY EXIT LIGHT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT RT OVERWING EMERGENCY EXIT LIGHT, OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 6,918 hrs · 2,839 cycles

LAX - EEL - C - EMERGENCY LIGHTS AT OVERWING EXITS INOP 11WL AND 12WL. MAINTENANCE REMOVED AND REPLACED BATTERIES AT POWER SUPPLIES 11WL AND 12WL IAW T/C R1C3301.

Part: COMPUTER — UNRELIABLE (E/E BAY) · airframe 6,518 hrs · 2,671 cycles

PHX - ABORTED TAKEOFF - FLT 231 -C- ON TAKEOFF ROLL AT 90 KTS FLIGHT CREW OBSERVED ECAM MESSAGE ALT LAW AND NO AIRSPEED INDICATION ON PFD NR 2 AND THE TAKEOFF WAS REJECTED. MAINTENANCE TROUBLESHOT AND REPLACED THE NR 2 ADIRU. AFTER ALIGNING THE ADIRU BITE CHECKS WERE GOOD. MAINTENANCE ALSO RAN THE NR 2 PITOT SYSTEM TO 150 KTS WITH TEST SET AND NR 2 AIRSPEED INDICATIONS WERE NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. TEAR-DOWN REPORT INDICATES A THERMAL CALIBRATION PERFORMED AND TESTED. NO OTHER DEFECTS NOTED ON THIS UNIT.