N113UW

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 42,721 hrs · 19,389 cycles

FLASHLIGHT AT L2 INOPERATIVE. REPLACED BATTERY.

Part: COVER — BROKEN (CABIN) · airframe 42,037 hrs · 19,012 cycles

CLEAR EXIT LIGHT COVER BROKEN, 2R DOOR. REINSTALLED COVER FOR EXIT LIGHT AT 2R DOOR.

Part: LENS — MISSING (CABIN) · airframe 41,862 hrs · 18,919 cycles

EXIT ROW LIGHTING ON SEAT 1A IS INOPERATIVE. REPLACED LENS COVER AT SEAT 1A, EMERGENCY LIGHTS OPERATES NORMALLY.

Part: LENS — MISSING (CABIN) · airframe 41,754 hrs · 18,855 cycles

EMERGENCY LIGHT COVERS MISSING 1C & 3C. REPLACED LENS COVERS ON SEATS 1C AND 3C.

Part: LENS — MISSING (CABIN) · airframe 41,313 hrs · 18,643 cycles

FIRST CLASS SEAT 3AC MISSING EMERGENCY LIGHT LENS. INSTALLED LENS ON FIRST CLASS SEAT 3AC. OPERATIONAL CHECK GOOD.

Part: LENS — BROKEN (CABIN) · airframe 41,103 hrs · 18,543 cycles

SEAT 1C FLOOR EXIT LIGHT COVER BROKEN OFF. INSTALLED NEW LENS COVER ON SEAT 3C.

Part: AIR DATA MODULE — FAULTY (NR 4) · airframe 39,170 hrs · 17,546 cycles

CAPTAIN REPORTED NO AIRSPEED INDICATION ON TAKEOFF ROLL. REJECTED TAKEOFF AT 80 KTS. REMOVED AND REPLACED NR 4 AIR DATA MODULE IAW AIRBUS MAINTENANCE MANUAL 34-11-17-0401.

Part: AIR DATA MODULE — FAULTY (NR 8) · airframe 39,170 hrs · 17,546 cycles

CAPTAIN REPORTED NO AIRSPEED INDICATION ON TAKEOFF ROLL. REJECTED TAKEOFF AT 80 KTS. REMOVED AND REPLACED NR 8 AIR DATA MODULE IAW AIRBUS MAINTENANCE MANUAL 34-11-17-0401.

Part: PITOT TUBE — FAULTY (PITOT/STATIC SYS) · airframe 39,170 hrs · 17,546 cycles

CAPTAIN REPORTED NO AIRSPEED INDICATION ON TAKEOFF ROLL. REJECTED TAKEOFF AT 80 KTS. REMOVED AND REPLACED CAPTAIN'S PITOT PROBE IAW AIRBUS MAINTENANCE MANUAL 34-11-15. ALSO REFERENCE SDR'S USAA2012091800002 & USAA2012091800003.

Part: PLUG — LOOSE (APU) · airframe 38,986 hrs · 17,444 cycles

UPON ARRIVAL AT GATE, TWO FLIGHT ATTENDANTS REPORTED FUMES DESCRIBED AS SCORCHING AND/OR VOMIT SMELL, AND SUFFERED BURNING / RED EYES, HEADACHE AND THROAT ISSUES. MAINTENANCE FOUND LOOSE PLUG ON APU GENERATOR - TIGHTENED PLUG AND LEAK CHECKED WITH NO LEAKS NOTED. REPLACED HEPA FILTERS AND PERFORMED ECS DECONTAMINATION.

Part: LENS — BROKEN (CABIN) · airframe 37,685 hrs · 16,793 cycles

EMERGENCY LIGHT LENS COVER BROKEN 11L. REMOVED AND REPLACED EMERGENCY LIGHT LENS 11L.

Part: RESERVOIR — FAILED (EVAC SLIDE) · airframe 37,478 hrs · 16,684 cycles

2S CHECK, DURING OPERATIONAL TEST OF THE INFLATION RESERVOIR UTILIZING THE CIDS A FAILURE MESSAGE WAS RECIEVED FOR THE LEFT UNIT. REMOVED AND REPLACED THE LEFT INFLATION RESERVOIR IAW A320 AMM 25-62-46.

Part: SLIDE RAFT — DEFECTIVE (DOOR) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - OVER INFLATED SLIDE/RAFT AT DOOR 831. REPACKED SLIDE RAFT IAW A320 CMM 25-61-20 PAGE 309 SEC DISASSEMBLY AND FOLDING PROCEDURE P 11921.

Part: DAMPER — WEAK (DOOR) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - DURING OPERATIONAL TEST DAMPING FUNCTION, BUFFER IMPACT HARD ON AIRCRAFT STRUCTURE AT DOOR 831. REPLACED DOOR-DAMPER & EMERGENCY OPERATION CYLINDER AT DOOR 831 IAW A320 AMM 52-11-14-400-001 & EA 133889. CHECKED ADJUSTMENT IAW A320 AMM 52-11-14-820-002, ADJUSTMENT OK.

Part: SETSCREW — OUT OF ADJUST (DOOR) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - OUT OF ADJUSTMENT RIGGING POINT OF REDUCER SHAFT BELLCRANK (UP POSITION) AT DOOR 831. PERFORMED ADJUSTMENT OF RIGGING POINT OF REDUCER SHAFT BELLCRANK (UP POSITION) AT DOOR 831, ADJUSTMENT IS OK IAW A320 AMM 52-11-21-400-001 PROCEDURE 8(G) STEP 20 THRU 25.

Part: SLIDE RAFT — DEFECTIVE (DOOR) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - OVER INFLATED SLIDE/RAFT AT DOOR 832. REPACKED SLIDE/RAFT AT DOOR 832 IAW A320 CMM 25-61-20 PAGE 309 SEC. DISASSEMBLY & FOLDING PROCEDURE P-11915.

Part: BUSHING — WORN (DOOR) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - EXCESSIVE PLAY IN UPPER CONNECTION LINK AT DOOR 832. REPLACED BUSHINGS IN UPPER CONNECTION LINK AT DOOR 832 IAW A320 AMM 52-10-00-915-001 PAR 4 STEP A, B. ADJUSTMENT CHECK IAW AMM 52-13-21-400-001 STEP J, ADJUSTMENT IS OK.

Part: DAMPER — DAMAGED (DOOR) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - DURING OPERATIONAL TEST DAMPING FUNCTION BUFFER IMPACT HARD ON AIRCRAFT STRUCTURE AT DOOR 842. REPLACED DOOR DAMPER AND EMERGENCY-OPERATION CYLINDER AT DOOR 842 IAW A320 AMM 52-13-14. CHECKED THE ADJUSTMENTS & FOUND GOOD.

Part: STRIKER — OUT OF ADJUST (DOOR) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - OUT ADJUSTMENT AT DIMENSION 'B' BETWEEN FINGER & STRIKER LEVER AT DOOR 841. PERFORMED ADJUSTMENT DIMENSION "B" (J1) BETWEEN FINGER & STRIKER LEVER OF THE DOOR DAMPER & EMERGENCY OPERATION CYLINDER AT DOOR 841, ADJUSTMENT IS OK IAW AMM 52-11-14-820-002.

Part: SLIDING WINDOW — BROKEN (COCKPIT) · airframe 37,475 hrs · 16,633 cycles

2S CHECK - BROKEN FRAME ON SLIDING WINDOW PANEL CAPTAINS SIDE. REPLACED SLIDING WINDOW PANE AT CAPTAINS SIDE IAW AMM 56-12-11. OPERATIONAL TEST OF THE WINDSHIELD ANTI-ICING & DEFOGGING GOOD IAW A320 AMM 30-42-00-710-001.

Part: STRIKER — OUT OF ADJUST (DOOR) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - DOOR 831 IS OUT ADJUSTMENT AT DIMENSION B BETWEEN FINGER AND STRIKER LEVER AT DOOR 831. PERFORMED ADJUSTMENT AT DIMENSION B BETWEEN FINGER AND STRIKER LEVER AT DOOR 831 IAW AMM 52-11-14-820-002 PAR 4 ITEM A, STEP (1),. ADJUSTMENT GOOD.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - CORROSION ON CONNECTING SECTION AT FR68, -Y1162. REPLACED CONNECTING SECTION AT FR68, -Y1162 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53474250.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR27 TO FR29, -Y765. REPLACED SEAT TRACK BETWEEN FR27 TO FR29, -Y765 IAW A320 SRM 53-21-15.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING FUEL ACCESS PANEL 540JB BETWEEN WS 7792 TO WS 8268, BETWEEN RIB 14 TO RIB 15. REPLACED LEFT WING FUEL ACCESS PANEL 540JB IAW JOB CARD 26C54057007.

Part: STRUT — CORRODED (RT WING) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - CORROSION ON INTERCONNECT STRUT BETWEEN WS 375 TO WS 551 & BETWEEN RIB 7 TO RIB 10. REPLACED INTERCONNECT STRUT BETWEEN WS 375 TO WS 551 & BETWEEN RIB 7 TO RIB 10 IAW A320 AMM 27-51-44.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING FUEL ACCESS PANEL 540KB BETWEEN WS 8268 TO WS 8744, BETWEEN RIB 15 TO RIB 16. REPLACED LEFT WING FUEL ACCESS PANEL 540KB IAW JOB CARD 26C54057007.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - MULTIPLE CRACKS IN SEGMENT ANGLE OF EMERGENCY EXIT DOOR 844 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. ACCOMPLISHED MODIFICATION ON EMERGENCY EXIT HATCH DOOR 844 IAW EO 5210Y228.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - MULTIPLE CRACKS IN SEGMENT ANGLE OF EMERGENCY EXIT DOOR 834 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. ACCOMPLISHED MODIFICATION ON EMERGENCY EXIT HATCH DOOR 834 IAW EO 5210Y228.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - MULTIPLE CRACKS IN SEGMENT ANGLE OF EMERGENCY EXIT DOOR 843 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3. ACCOMPLISHED MODIFICATION ON EMERGENCY EXIT HATCH DOOR 843 IAW EO 5210Y228.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - MULTIPLE CRACKS ON SEGMENT ANGLE OF EMERGENCY EXIT DOOR 833 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3. REPLACED SEGMENT ANGLE OF EMERGENCY EXIT DOOR 833 IAW EO 5210Y228.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SUPPORT FRAME BETWEEN FR69 TO FR70, S23L. REPLACED SUPPORT FRAME BETWEEN FR69 TO FR70, S23L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53474180.

Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING NR 1 SPOILER CENTER HINGE PIN. REPLACED LEFT WING NR 1 SPOILER CENTER HINGE PIN IAW A320 AMM 27-64-41-400-001.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 212EF BETWEEN FR6 TO FR12 & BETWEEN -Y254 TO -Y765. REPLACED FLOOR PANEL 212EF IAW A320 SRM 53-12-00 & IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 232EF BETWEEN FR20 TO FR24 & BETWEEN -Y1242 TO -Y765. REPLACED FLOOR PANEL 232EF IAW A320 53-12-00 AND MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 262BF BETWEEN FR64 TO FR66, BETWEEN -Y1732 TO Y765. REPLACED FLOOR PANEL 262BF IAW A320 SRM 53-12-00 AND MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 232FF BETWEEN FR20 TO FR24 & BETWEEN -Y1732 TO -Y1292. REPLACED FLOOR PANEL 232FF IAW A320 SRM 53-12-00 & IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 37,475 hrs · 16,683 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 261QF BETWEEN FR64 TO FR66 & BETWEEN -Y765 TO Y765. REPLACED FLOOR PANEL 261QF IAW A320 SRM 53-02-00 & IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 261PF BETWEEN FR68 TO FR70 & BETWEEN Y1242 TO -Y1242. REPLACED FLOOR PANEL 261PF IAW A320 SRM 53-12-00 & IRM 9701 REV G.

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON INTERNAL AREA OF LOWER CURVED EDGE OF EMERGENCY EXIT DOOR 844 AT FR39, BEAM 4. REPLACED LOWER CURVED EDGE OF INTERNAL AREA OF EMERGENCY EXIT DOOR 844 BETWEEN FR40 TO FR41, BEAM 4 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D52279010.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - CORROSION ON FLOOR PANEL NR 222FF BETWEEN FR16 TO FR20, S23R, -Y1732. REPLACED FLOOR PANEL NR 222FF IAW A320 AMM 53-12-12-400-001 & JOB CARD 26C22053014.

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER CURVED EDGE OF EMERGENCY EXIT DOOR 844 BETWEEN FR40 TO FR41, BEAM 4. REPLACED LOWER CURVED EDGE OF EMERGENCY EXIT DOOR 844 BETWEEN FR40 TO FR41, BEAM 4 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D52279010.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 222CF BETWEEN FR16 TO FR20, Y-1732 TO -Y254. REPLACED FLOOR PANEL 222CF IAW A320 SRM 53-12-00 AND MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 231CF BETWEEN FR20 TO FR24 & BETWEEN Y765 TO Y254. REPLACED FLOOR PANEL 231CF IAW A320 SRM 53-12-00 & IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 221DF BETWEEN FR16 TO FR20 & BETWEEN Y254 TO -Y254. REPLACED FLOOR PANEL 221DF IAW A320 SRM 53-12-00 & IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 37,475 hrs · 16,683 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 221PF BETWEEN FR12 TO FR16 & BETWEEN Y1292 TO Y254. REPLACED FLOOR PANEL 221PF IAW A320 SRM 53-12-00 & IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 231BF BETWEEN FR20 TO FR24 & BETWEEN -Y254 TO Y254. REPLACED FLOOR PANEL 231BF IAW A320 SRM 53-12-00 & IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 232DF BETWEEN FR20 TO FR24, BETWEEN -Y765 TO -Y254. REPLACED FLOOR PANEL 232DF IAW TYPICAL REPAIR 320-2528-10-0011 & A320 AMM 53-12-12-400-001.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL 221EF BETWEEN FR16 TO FR20 & BETWEEN Y1292 TO Y254. REPLACED FLOOR PANEL 221EF IAW A320 SRM 53-12-00 AND MCGILL IRM 9701 REV G.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - CORROSION ON FLOOR PANEL 262FF AT FR66 TO FR68, S20L, -Y1732. REPLACED FLOOR PANEL 262FF IAW A320 SRM 53-42-12 & 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 37,475 hrs · 16,683 cycles

S2 CHECK - DELAMINATION ON FLOOR PANEL 261BF BETWEEN FR64 TO FR66 & BETWEEN Y765 TO Y1732. REPLACED FLOOR PANEL 261BF IAW A320 SRM 53-02-00 & IRM 9701 REV G.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - CORROSION ON FLOOR PANEL 221FF BETWEEN FR16 TO FR20, S23L, Y1732. REPLACED FLOOR PANEL 221FF IAW A320 AMM 53-12-12-400-001 & JOB CARD 26C22053014.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR70, -Y160. REPLACED FLOORBEAM BETWEEN FR68 TO FR70, -Y160 IAW A320 SRM 51-72-11 AND AIRBUS DRAWINGS D53472780, D53474250.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING AT L1 DOOR ENTRANCE BETWEEN FR66+5 INCHES TO FR67+17 INCHES, S23L. REPLACED CENTER FITTING AT L1 DOOR ENTRANCE BETWEEN FR66+5 INCHES TO FR67+17 INCHES, S23L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53480048.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK, CORROSION ON R2 DOOR CUT OUT LOWER SILL AT FR 66 + 5" AND S23R. REPLACED R2 DOOR CUT OUT LOWER SILL AT FR 66 + 5" AND S23R IAW EA 133888.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING BETWEEN FR16+5 INCHES TO FR19+5 INCHES, S23R. REPLACED CENTER FITTING BETWEEN FR16+5 INCHES TO FR19+5 INCHES, S23R IAW A320 SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING BETWEEN FR16+5 INCHES TO FR19+5 INCHES S23L. REPLACED CENTER FITTING BETWEEN FR16+5 INCHES TO FR19+5 INCHES S23L IAW A320 SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON CORNER FITTING AT FR68, S23L. REPLACED CORNER FITTING AT FR68, S23L IAW A320 SRM 51-72-11 AND AIRBUS DRAWING D53480505.

Part: COUPLING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING AT FR66, S23L. REPLACED COUPLING AT FR66, S23L IAW A320 SRM 51-72-11, AIRBUS DRAWING 53480505 AND EA 133887.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL BETWEEN FR66 TO FR68, S23L. REPLACED LOWER SILL BETWEEN FR66 TO FR68, S23L IAW A320 SRM 51-72-11, AIRBUS DRAWING 53480505 AND EA 133887.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHAPE SILL BETWEEN FR66 TO FR68, S23R. REPLACED SHAPE SILL BETWEEN FR66 TO FR68, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWING 53480505.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON CORNER FITTING AT FR66, S23R. REPLACED CORNER FITTING AT FR66, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWING 53480505.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON CORNER FITTING AT FR68, S23R. REPLACED CORNER FITTING AT FR68, S23R IAW A320 SRM 51-72-11, 51-42-11 AND AIRBUS DRAWING D53480505.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16 INCHES, -Y1200. REPLACED FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16 INCHES, -Y1200 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472780.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY AT FR16, -Y81. REPLACED RAIL DUMMY AT FR16, -Y81 IAW A320 SRM 51-72-11 & DRAWING D53112828.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, S23L, Y1292. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, S23L, Y1292 IAW A320 SRM 51-72-11 AND AIRBUS DRAWING D53112812.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66+5 INCHES, Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66+5 INCHES, Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472815.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SUPPORT FLOOR BETWEEN FR16 TO FR20, -Y254. REPLACED SUPPORT FLOOR BETWEEN FR16 TO FR20, -Y254 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53110920.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM FR64 TO FR67+10 INCHES, -Y464.8. REPLACED FLOORBEAM FR64 TO FR67+10 INCHES, -Y464.8 IAW A320 SRM 53-72-11& AIRBUS DRAWING D53472816.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR66, -Y765. REPLACED SEAT TRACK BETWEEN FR27 TO FR29, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472815.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR44 TO FR47, -Y1292. REPLACED SEAT TRACK BETWEEN FR44 TO FR47, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53371000.

Part: COUPLING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING LEFT UPPER SIDE AT FR67+16 INCHES, -Y1162. REPLACED COUPLING LEFT UPPER SIDE AT FR67+16 INCHES, -Y1162 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472780.

Part: HINGE FITTING — EXCESS PLAY (VERTICAL STAB) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - EXCESSIVE PLAY ON NR 7 HINGE ARM FITTING AT VERTICAL STAB STA 5605 RIB 11. REPLACED NR 7 HINGE ARM FITTING IAW A320 SRM 51-72-11 & AMM 55-36-41.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR20, -Y765. REPLACED SEAT TRACK AT FR20, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112812 & D53110984.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR68, Y765. REPLACED FLOORBEAM AT FR68, Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472780.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, -Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472780.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON TRACK FLOOR SUPPORT BETWEEN FR20 TO FR23, -Y189. REPLACED TRACK FLOOR SUPPORT BETWEEN FR20 TO FR23, -Y189 IAW A320 SRM A320 51-72-11, AIRBUS DRAWING D53111406 & EA 133853.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66+5 INCHES, Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66+5 INCHES, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472815.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR68, Y765. REPLACED FLOORBEAM AT FR68, Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472780.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE AT FR69 PLUS 5 INCHES, S23R. REPLACED SHEAR PLATE AT FR69 PLUS 5 INCHES, S23R IAW A320 SRM 51-72-11, AIRBUS DRAWING 53480505 AND TYPICAL REPAIR 320-2528-10-0011.

Part: COVER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON JOINT COVER AT FR14, -Y81. REPLACED JOINT COVER AT FR14, -Y81 IAW A320 SRM 51-72-11 AND AIRBUS DRAWING D53112829.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR66, -Y765. REPLACED FLOORBEAM AT FR66, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472816.

Part: COUPLING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

S2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SPLICE (COUPLING) AT FR67+16 INCHES, Y1167. REPLACED SPLICE (COUPLING) AT FR67+16 INCHES, Y1167 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472780.

Part: HINGE FITTING — EXCESS PLAY (VERTICAL STAB) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - EXCESSIVE PLAY ON NR 2 HINGE ARM FITTING AT VERTICAL STAB STA 1926 RIB 4. REPLACED NR 2 HINGE ARM FITTING IAW A320 SRM 51-72-11 & AMM 55-36-41.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, -Y1292. REPLACED SEAT TRACK BETWEEN FR24 TO FR35, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231730.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, Y254. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, Y254 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112816.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SUPPORT BEAM TRACK BETWEEN FR20 TO FR23, -Y1584. REPLACED SUPPORT BEAM TRACK BETWEEN FR20 TO FR23, -Y1584 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53111463 & D53111473.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR65+20 INCHES, -Y1732. REPLACED FLOORBEAM AT FR65+20 INCHES, -Y1732 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53474250 & D53472750.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR64 TO FR66+5 INCHES, -Y1292. REPLACED SEAT RAIL BETWEEN FR64 TO FR66+5 INCHES, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472816.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM ASSEMBLY BETWEEN FR56 TO FR66, S23L, Y1732. REPLACED FLOORBEAM ASSEMBLY BETWEEN FR56 TO FR66, S23L, Y1732 IAW A320 SRM 51-72-11, 51-42-11 & AIRBUS DRAWING D53474250.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON WEB BETWEEN FR20 TO FR21, -Y1600. REPLACED WEB BETWEEN FR20 TO FR21, -Y1600 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53114392.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23L. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23L IAW A320 SRM 51-72-11 AND AIRBUS DRAWING 53480505.

Part: COUPLING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON COUPLING LEFT UPPER SIDE AT FR66+5 INCHES, -Y1200. REPLACED COUPLING LEFT UPPER SIDE AT FR66+5 INCHES, -Y1200 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472816.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67+16 INCHES TO FR69, -Y1162. REPLACED FLOORBEAM BETWEEN FR67+16 INCHES TO FR69, -Y1162 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472780.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, S23L, -Y1292. SEAT TRACK BETWEEN FR12 TO FR24, S23L, -Y1292 IAW A320 SRM 51-72-11 AND AIRBUS DRAWING D53112812.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16 INCHES. REPLACED FLOORBEAM BETWEEN FR66+5 INCHES TO FR67+16 INCHES IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472815.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67+16 INCHES TO FR69+4 INCHES, Y1167. REPLACED FLOORBEAM BETWEEN FR67+16 INCHES TO FR69+4 INCHES, Y1167 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472780.

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL PROFILE BETWEEN FR58 TO FR59, S44L. REPLACED LONGITUDINAL PROFILE BETWEEN FR58 TO FR59, S44L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53470340 & D53470014.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, Y765. REPLACED SEAT TRACK BETWEEN FR24 TO FR35, Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231730.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT BEAM RAIL BETWEEN FR64 & FR61+12 INCHES, S23R, -Y765. REPAIRED SEAT BEAM RAIL BETWEEN FR64 & FR61+12 INCHES, S23R, -Y765 IAW A320 SRM 53-41-15 FIG 202, 51-42-11 & AIRBUS DRAWING D53472815.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - CORROSION ON CARGO FORCE PROFILE SUPPORT AT FR65, S44. REPLACED CARGO FORCE PROFILE SUPPORT AT FR65, S44 IAW A320 SRM 51-72-11 AND AIRBUS DRAWING D53474160.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL AT FR47+12 INCHES, Y1292. REPLACED SEAT RAIL AT FR47+12 INCHES, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472770/D53470080/D53472831.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR42, Y765. REPLACED SEAT TRACK AT FR42, Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53371000.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT BEAM RAIL BETWEEN FR64 & FR61+12 INCHES, Y765. REPAIRED SEAT BEAM RAIL BETWEEN FR64 & FR61+12 INCHES, Y765 IAW A320 SRM 53-41-15 FIG 202, 51-42-11 & AIRBUS DRAWING D53472770 & D53472831.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,475 hrs · 16,683 cycles

S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR42 TO FR46, Y1292. REPLACED SEAT TRACK BETWEEN FR42 TO FR46, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53371000.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LIQUID INGRESS ON LEFT ELEVATOR UPPER SKIN BETWEEN HORIZONTAL STAB STA 342 TO STA 404, BETWEEN RIB 9 TO RIB 10, APPROX 5 INCHES FORM LEADING EDGE. REPAIRED LEFT ELEVATOR UPPER SKIN BETWEEN HORIZONTAL STAB STA 342 TO STA 404, BETWEEN RIB 9 TO RIB 10, APPROX 5 INCHES FORM LEADING EDGE IAW A320 SRM 55-21-11 PARA 5E.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL151DF BETWEEN FR49 TO FR53, BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL151DF IAW A320 SRM 53-02-00 AND IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - DELAMINATION ON FLOOR PANEL151GF BETWEEN FR52 TO FR56, BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL151GF IAW A320 SRM 53-02-00 AND IRM 9701 REV G.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 37,475 hrs · 16,683 cycles

2S CHECK - LIQUID INGRESS ON RIGHT ELEVATOR BETWEEN HORIZONTAL STABILIZER STATION 181 TO STA227, BETWEEN RIB 5 TO RIB 6, APPROX 11 INCHES FROM LEADING EDGE. REPAIRED RIGHT ELEVATOR BETWEEN HORIZONTAL STABILIZER STATION 181 TO STA 227, BETWEEN RIB 5 TO RIB 6, APPROX 11 INCHES FROM LEADING EDGE IAW A320 SRM 55-21-11.

Part: MODULE — LEAKING (CABIN) · airframe 37,469 hrs · 16,681 cycles

FLIGHT ATTENDANTS REPORTED A DIRTY SOCK ODOR AND SYMPTOMS OF NAUSEA AND DIZZINESS. MAINTENANCE FOUND OIL LEAK ON OIL LUBE MODULE. REMOVED AND REPLACED IAW MM 49-91-45.

Part: RELEASE PIN — OBSTRUCTED (EVAC SLIDE) · airframe 37,208 hrs · 16,546 cycles

UPON PREFLIGHT, CAPTAIN FOUND A/C LEFT ESCAPE SLIDE RELEASE PINS PAINTED OVER. MAINTENANCE CLEANED PAINT OFF THREE LEFT OVERWING SLIDE COMPARTMENT DOOR RELEASE PINS.

Part: MEGAPHONE — MISSING (CABIN) · airframe 37,166 hrs · 16,525 cycles

AFT MEGAPHONE MISSING. MAINTENANCE INSTALLED MEGAPHONE IN AFT POSITION.

Part: LENS — MISSING (CABIN) · airframe 36,987 hrs · 16,435 cycles

EMERGENCY LIGHT LENS COVER MISSING AT ROW 10A. MAINTENANCE INSTALLED LENS COVER AT ROW 10A.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 36,433 hrs · 16,198 cycles

LAS - EEL - FIRST CLASS FLIGHT ATTENDANT'S EMERGENCY FLASHLIGHT NEEDS BATTERY REPLACEMENT. MAINTENANCE REPLACED FIRST CLASS EMERGENCY FLASHLIGHT BATTERY AS REQUIRED & ADDED SECURITY STRAP.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 35,669 hrs · 15,847 cycles

FLT 1559-PHL - EEL - AFT BREAKAWAY FLASHLIGHT NOT BLINKING. MAINTENANCE REMOVED AND REPLACED AFT EMERGENCY FLASHLIGHT BATTERY PACK.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 35,548 hrs · 15,788 cycles

MX - LAX - EEL - AFT EMERGENCY POWER SUPPLY UNIT FAILED DURING TEST. MAINTENANCE REMOVED AND REPLACED EPSU.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 34,795 hrs · 15,419 cycles

FLT 1822 - CLT- BOS - EMERGENCY LANDING - CAPTAIN'S FRONT WINDSHIELD CRACKED IN FLIGHT. DECLARED EMERGENCY. REPLACED CAPTAIN'S WINDSHIELD PER J/C 26L21056001. REMOVED AND REPLACED LEFT WINDOW HEAT COMPUTER PER AMM 30-42-34. OPERATIONAL CHECK WAS GOOD.

Part: COMPUTER — FAULTY (WINDOW HEAT) · airframe 34,795 hrs · 15,419 cycles

LOGPAGE:7325990 - FLT#1822- CLT-BOS - EMERGENCY LANDING - CAPTAIN'S FRONT WINDSHIELD CRACKED IN FLIGHT. DECLARED EMERGENCY. REPLACED CAPTAIN'S WINDSHIELD PER J/C 26L21056001. REMOVED AND REPLACED LEFT WINDOW HEAT COMPUTER PER AMM 30-42-34. OPERATIONAL CHECK WAS GOOD.

Part: LENS — MISSING (CABIN) · airframe 34,486 hrs · 15,251 cycles

FLT 1564 - PHL - EEL - EMERGENCY EXIT ROW 10 SEAT F - EMERGENCY LIGHT COVER MISSING. MAINTENANCE REPLACED LIGHT COVER AS REQUIRED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 34,171 hrs · 15,103 cycles

RON/PIT - EEL - FORWARD LEFT EMERGENCY POWER SUPPLY UNIT HAS "BATTERY FAULT" AND "UNIT FAULT" DISPLAYED. MAINTENANCE REMOVED AND REPLACED THE FORWARD LEFT EMERGENCY POWER SUPPLY UNIT AND BATTERY.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 33,221 hrs · 14,621 cycles

FLT 1850 - BDL - EES - R2 AND L2 DOOR DAMPERS NEED TO BE SERVICED. MAINTENANCE SERVICED R2 DOOR DAMPER IAW AIRBUS MAINTENANCE MANUAL 52-10-00.

Part: DAMPER — LOW PRESSURE (L2 DOOR) · airframe 33,221 hrs · 14,621 cycles

FLT 1850 - BDL - EES - R2 AND L2 DOOR DAMPERS NEED TO BE SERVICED. MAINTENANCE SERVICED L2 DOOR DAMPER IAW AIRBUS MAINTENANCE MANUAL 52-10-00.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 31,653 hrs · 13,844 cycles

FLT 1583 - PHL - EEL - AFT EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED THE AFT EMERGENCY FLASHLIGHT.

Part: DIRECTOR — DEFECTIVE (CABIN) · airframe 30,636 hrs · 13,423 cycles

LOG PAGE 8260166 - FLT 1800-CLT - EEL - EMERGENCY EXIT LIGHTS ARE INOP IN NORMAL CONFIGURATION. MAINTENANCE REPLACED DEFECTIVE CIDS DIRECTOR IAW AIRBUS MAINTENANCE MANUAL 23-73-34.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 29,901 hrs · 13,105 cycles

FLT 1723 - FLL - EEL - SEAT 29 ABC FLOOR PROXIMITY LIGHT INOPERATIVE. MAINTENANCE REPAIRED CONNECTOR. OPERATIONAL CHECK NORMAL.

Part: LANYARD — MISROUTED (ESCAPE SLIDE) · airframe 28,648 hrs · 12,583 cycles

PIT A12 EES LT AFT DOOR HAS IMPROPER ROUTING OF WHITE AND YELLOW LANYARDS ON ESCAPE SLIDE RAFT. PIT. RE-ROUTED LANYARDS ON LT AFT DOOR IAW US AIRWAYS JOB CARD 26L00025011.

Part: LANYARD — MISROUTED (ESCAPE SLIDE) · airframe 28,468 hrs · 12,583 cycles

PIT A12 EES LT FORWARD DOOR HAS IMPROPER ROUTING OF WHITE AND YELLOW LANYARDS ON ESCAPE SLIDE RAFT. REPLACED LT FORWARD DOOR SLIDE RAFT. IAW US AIRWAYS JOB CARD 26L00025011.

Part: ACTUATOR — FAILED (VSV) · airframe 27,124 hrs · 11,980 cycles

FLT 1490 - CLT-LGA - RTF - CREW REPORTED TWO AUDIBLE COMPRESSOR STALLS ON THE NR 1 ENGINE ON TAKEOFF. THE AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE VARIABLE STATOR VANE ACTUATOR. ACCELERATION CHECK AND POWER ASSURANCE RUNS WERE GOOD. (S)

Part: A/C PACK — DETACHED (EVAC SLIDE) · airframe 27,124 hrs · 11,980 cycles

A-9 CK LAX - EES - R-2 SLIDE RAFT FWD COVER ASSEMBLY STRAP IS DETACHED FROM THE SLIDE ASSEMBLY. MAINTENANCE REMOVED AND REPLACED THE R-2 SLIDE/RAFT.

Part: ENGINE — SMOKE (NR 1)

SAN FLT 883 EN-ROUTE LAS TO SAN - CREW SHUT DOWN THE NUMBER TWO ENGINE AFTER A REPORT FROM ANOTHER FLIGHT ABOUT A TRAIL OF SMOKE COMING FROM THE ENGINE. THE ENGINE HAD ALSO JUST BEGUN TO HAVE HIGH LEVELS OF VIBRATION. MAINTENANCE ACTION PENDING (OPEN).

Part: ACTUATOR — LEAKING (ZONE 400)

PIT FLT 914 EN ROUTE, SFO TO PHL. DURING IN-FLIGHT CHECKS, IT WAS DETERMINED THAT THE AIRCRAFT HAD BURNED 4,000 LBS OF FUEL MORE THAN EXPECTED. A FUEL LEAK FROM THE RIGHT SIDE FUEL SYSTEM WAS SUSPECTED. THE FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ISOLATED THE LEAK TO THE NUMBER TWO ENGINE, OUTBOARD, VARIABLE STATOR VANE (VSV) ACTUATOR. THE VSV ACTUATOR WAS REPLACED. SYSTEM OPERATIONALLY AND LEAK CHECKS OK.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

RIC - MAINTENANCE REPORTED THE LOW LEVEL EMERGENCY LIGHTS AT ROW 23 INOPERATIVE. MAINTENANCE RESEATED THE QUICK-DISCONNECT PLUG BENEATH THE SEAT. OPERATIONAL CHECK GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 18,972 hrs · 18,972 cycles

Y129L AT C-18 CORRODED. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-42-11; DEFECT SIZE: .5 X .5 X .070 INCH DEEP.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 1 · airframe 18,972 hrs · 18,972 cycles

FOUND CORROSION Y-254 FRAME C-16 TO C-18. FAB'D AND INSTALLED TOP FILLER AND TWO ANGLE DOUBLERS PER SRM 53-00-14; CORROSION LEVEL 1; TASK JA-220-53500 DEFECT SIZE: 4" X 3".

Part: FLOORBEAM — CORRODED (FR 66) · corrosion level 1 · airframe 18,972 hrs · 18,972 cycles

FOUND CORROSION FS 66 Y765. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 1-1/2" X 1-1/2".

Part: FLOOR SUPPORT — CORRODED (Y1292 C64-66) · corrosion level 1 · airframe 18,972 hrs · 18,972 cycles

FOUND CORROSION FLOOR SUPPORT Y1292 C64-66. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-42-11; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 2 SQ IN.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 1 · airframe 18,972 hrs · 18,972 cycles

CORROSION Y1292-Y1162 BETWEEN FR C66-C68. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-42-11; CORR LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 1 INCH DIA.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 1 · airframe 18,972 hrs · 18,972 cycles

FOUND CORROSION RT SHEAR WEB BETWEEN FS 69 AND 70 - Y1200. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-00; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 1" DIA.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 1 · airframe 18,972 hrs · 18,972 cycles

FOUND OVAL CORROSION TOP OF SHEAR WEB, BETWEEN C69 & 70 AT Y1200. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-43-00; CORROSION LEVEL 1; TASK JA-260-53500-12, DEFECT SIZE: 2".

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 1 · airframe 18,972 hrs · 18,972 cycles

FR 64-69 AT -Y1292 CORRODED. REPLACED BEAMS PER SRM 51-72-11; CORR LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 2 X 1, 3 X .5, 2 X 1.5 INCH

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 1 · airframe 18,972 hrs · 18,972 cycles

OVAL SURFACE, TOP & BOTTOM, BETWEEN C69-70 AT Y1200 CORRODED. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-43-00; CORR LEVEL 1; TASK JA-260-53500-14, DEFECT SIZE: 3 INCH.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 1 · airframe 18,972 hrs · 18,972 cycles

Y765 AT CROSSBEAM C-68 CORRODED. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11; CORR LEVEL 1; TASK JA-160-53500. DEFECT SIZE: 1 INCH DIA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 1 · airframe 18,972 hrs · 18,972 cycles

Y254, BETWEEN C-16 & C-22 CORRODED. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11; CORR LEVEL 1; TASK JA-220-53500. DEFECT SIZE: 4 X 3 INCH.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 1 · airframe 18,972 hrs · 18,972 cycles

Y1400 AT C66 CORRODED. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-42-11; CORR LEVEL 1; TASK JA-260-53500. DEFECT SIZE: 1 INCH DIA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 1 · airframe 18,972 hrs · 18,972 cycles

CORROSION Y1162 BETWEEN C68-69. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-42-11; CORR LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 1 INCH DIA.

Part: FITTING — CORRODED (DOOR SILL) · corrosion level 1 · airframe 18,972 hrs · 18,972 cycles

FOUND CORROSION AFT SVC DOOR SILL BEAM AT C66 AND Y1400. INSTALLED DOUBLERS PER SRM 53-41-14; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 1/2" X 1-1/2" LONG.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 1 · airframe 18,972 hrs · 18,972 cycles

FRAME C-14-C16 Y505 CORRODED. REPLACED BEAM PER SRM 51-72-11; CORR LEVEL 1; TASK JA-220-53500, DEFECT SIZE: 1 X .5 INCH, 1.5 X 1 INCH.

Part: HMU — FAILED (NR 2 ENGINE)

WHILE AT FL 360, THE NR 2 ENGINE GENERATOR FAILED, FOLLOWED BY THE NR 2 ENGINE. THE FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE HMU AND ECU FOR TROUBLESHOOTING. ALSO, REPLACED THE NR 2 ENGINE ALTERNATOR ROTOR AND STATOR DUE TO RUB MARKS ON THE STATOR. OPERATIONALLY CHECKS OK.

Part: SLIDE — DAMAGED (PASSENGER CABIN)

BOS - DURING A SLIDE TIME CHANGE, THE REPLACEMENT SLIDE WAS FOUND DEFECTIVE FROM STOCK WITH LANYARDS FOR THE GIRT BARS TORN IN HALF. THE SLIDE WAS NOT INSTALLED. MAINTENANCE RETURNED THE SLIDE FOR REPAIR. THE SLIDE TIME CHANGE OCCURRED THREE DAYS LATER WITH A SERVICEABLE SLIDE.

Part: SLIDE — DAMAGED (LEFT)

PIT - THE AFT LEFT REPLACEMENT SLIDE WAS FOUND SEPARATED FROM ITS BACKING PLATE. MAINTENANCE INSTALLED THE AFT LEFT SLIDE/RAFT TO THE BACKING PLATE AND THEN BACK ONTO THE AIRCRAFT. OK FOR SERVICE.

Part: CONTROLLER — FAILED (WINDSHIELD HEAT)

PHX - FLT 1011 EN-ROUTE, PHL - PHX, DURING FLIGHT, THE FIRST OFFICER'S WINDSCREEN STARTED TO ARC AND DELAMINATE. THE CREW PULLED THE WINDSHIELD HEAT CIRCUIT BREAKER. THE FLIGHT CONTINUED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE F/O WINDSHIELD AND WINDOW HEAT CONTROLLER. OK FOR SERVICE.

Part: CABLE — BROKEN (AFT CARGO BAY)

THE LEFT OVERWING SLIDE BOTTLE CABLE WAS FOUND BROKEN. MAINTENANCE REPLACED THE LT OVERWING SLIDE BOTTLE ASSEMBLY. OK FOR SERVICE. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

TPA - AN EMERGENCY LIGHTS FAULT FOR THE LEFT SIDE WAS RECEIVED DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED AN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED OK. (M)

Part: LIGHT — INOPERATIVE (CABIN)

TPA - THE EMERGENCY LIGHTS FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE SECURED LOOSE CONNECTOR ON R-1 DOOR EMERGENCY ESCAPE SLIDE. OPERATIONALLY CHECKED OK. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

DCA - THE EMERGENCY LIGHT SYSTEM FAILED TEST. MAINTENANCE REPLACED AN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M)