N624AW

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 78,728 hrs · 35,976 cycles

EMERGENCY LIGHT RT SIDE OVERWING INOPERATIVE. REPLACED EMER POWER SUPPLY UNIT 11WL IAW TROUBLESHOOTING TASK 33-51-00-810-806A. OPERATIONS CHECKED OK.

Part: COOLING FAN — CONTAMINATED (APU) · airframe 78,447 hrs · 35,805 cycles

EXTREMELY STRONG ODOR IN FLIGHT DECK & CABIN. COMPLAINTS OF STINGING EYES & NAUSEA FROM BOTH PAXS & CREW. REPLACED FAN ASSEMBLY FOR APU. OPERATIONS & LEAK CHECKED OK IAW AMM 49-52-51-000-001A.

Part: ACTUATOR — LEAKING (APU) · airframe 78,447 hrs · 35,805 cycles

EXTREMELY STRONG ODOR IN FLIGHT DECK & CABIN. COMPLAINTS OF STINGING EYES & NAUSEOUS FROM BOTH PAXS & CREW. ACCOMPLISHED JOB CARD 26L31049009 & 26L00021004. REPLACED APU VARIABLE INLET GUIDE VANE ACTUATOR IAW AMM 49-23-51. APU CHECKED GOOD, NO ODORS NOTED. THIS SDR SUBMITTED IN CONJUNCTION WITH LOG 2014111900001 FOR MULTIPLE PARTS CHANGES.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 78,276 hrs · 35,680 cycles

CLASS II SMOKE DETECTOR CONTROL UNIT MX FAULT. ACCOMPLISHED TROUBLE SHOOTING MANUAL TASK 26-17-00-810-802-A, NO FAULTS NOTED. REPLACED LT AFT LAVATORY SMOKE DETECTOR IAW AMM TASK 26-17-00-810-802-A & AMM 26-17-15 PB 401.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 78,276 hrs · 35,680 cycles

SEAT MOUNTED EMER EXIT LIGHTS INOPERATIVE LT & RT SIDES AT EMER EXIT HATCHES. REPLACED EMER POWER SUPPLY UNIT 12WL IAW AMM 33-51-38. OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 78,246 hrs · 35,659 cycles

ROWS 9R, 11R, 11L & 13L EMER EXIT PATH SEAT LIGHTS INOPERATIVE. REPLACED RT EPSU.

Part: O-RING — DAMAGED (APU) · airframe 77,383 hrs · 35,120 cycles

LONG EXTENDED DECENT AT IDLE POWER DIRTY SOCK SMELL BELOW 10,000 FT, CONTINUED THROUGH DECENT & APPROACH. REPLACED APU TURBINE CAVITY VENT O RING IAW AMM 49-91-53 & WASHED APU IAW AMM 49-20-00. NO LEAKS FOUND IAW LOG PAGE 8557047.

Part: APU — OVERSERVICED (APU BAY) · airframe 77,379 hrs · 35,117 cycles

DIRTY SOCK SMELL IN FWD CABIN ON DESCENT. FOUND OIL AT APU AIR INLET IAW NR 3060271. CLEANUP & DECONTAMINATION ACCOMPLISHED IAW NOTED WORK CARDS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,320 hrs · 35,092 cycles

CABIN EMER LIGHT TEST FAILS. LT AFT BATTERY FAULT. REPLACED BATTERY PACK FOR AFT LT ESPU. CABIN EMER LIGHTS TESTED OK IAW AMM 33-51-38.

Part: DIAPHRAGM — DAMAGED (R1 DOOR) · airframe 77,286 hrs · 35,078 cycles

DOOR R1 ASSIST BOTTLE DEPLETED. REPLACED ASSIST BOTTLE DIAPHRAGM & SERVICED. OK FOR SERVICE IAW FIG EAC CMM 52-22-17.

Part: ATTACH FITTING — BROKEN (EVAC SLIDE) · airframe 77,286 hrs · 35,078 cycles

FOUND DOOR R1 SLIDE ATTACHMENT CLIP BROKEN. REPLACED DOOR R1 SLIDE IAW JOB CARD 26L00025011.

Part: WIRE — BROKEN (CABIN) · airframe 76,994 hrs · 34,939 cycles

C2 CHECK EMERGENCY LIGHTS AT CABIN SEATS 1, 3, & 7 ARE INOPERATIVE. PERFORMED TROUBLE SHOOTING IAW FIM 33-51-00 FOUND BROKEN WIRE ON SEAT 3 IN SEAT HARNESS. ACCOMPLISHED REPAIR ON IN SEAT HARNESS BROKEN WIRE IAW ESPM 20-43-10. OPERATIONS CHECKED GOOD IAW AMM 33-51-00.

Part: SIGN — BROKEN (CABIN) · airframe 76,814 hrs · 34,868 cycles

DOOR L1 EMERGENCY EXIT SIGN BROKEN. REPLACED EMERGENCY EXIT SIGN AT DOOR L1 IAW AMM 33-51-16-0401.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 76,714 hrs · 34,816 cycles

EXIT SIGN AT DOOR 2R DOES NOT ILLUMINATE. RESEATED EXIT SIGN AT DOOR 2R.

Part: INLET — CONTAMINATED (APU) · airframe 76,663 hrs · 34,796 cycles

AFTER DEPARTURE FROM YVR COCKPIT & CABIN HAD OILY AIR SMELL FOR A SHORT TIME THEN WENT AWAY. LATER DURING CRUISE FLIGHT ATTENDANT`S REPORTS THE SMELL HAS RETURNED. APU INLET WASH COMPLETED IAW JOB CARD 26L00021004 & 26L00021001, NO ODOR.

Part: LENS — MISSING (CABIN) · airframe 76,258 hrs · 34,618 cycles

EMERGENCY AISLE LIGHT LENS IS MISSING AT ROW 7 LT. REPLACED EMERGENCY AISLE LIGHT LENS MISSING AT ROW 7 LT.

Part: UNKNOWN — ODOR (CABIN) · airframe 76,011 hrs · 34,505 cycles

OIL SMELL ON ACFT SHUT DOWN CABIN ODOR REPORT US-0137 COMPLETE & FAXED TO MOC. ACCOMPLISHED WORK CARD 26L00021001 WITH NO ODOR NOTED, ACFT OK FOR SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 76,011 hrs · 34,505 cycles

STRONG OIL SMELL IN ACFT CREW REPORTING BURNING IN NOSE, THROAT & HEADACHE. COMPLIED WITH JOB CARDS 26L00021001, 26L00021002 & 26L00021004 WITH NO OIL SMELL NOTED IAW NR 3054008.

Part: SMOKE DETECTOR — FAULTED (LAVATORY) · airframe 75,879 hrs · 34,443 cycles

CREW REPORTED A SMOKE DETECTOR FAULT. R & R LAVATORY D SMOKE DETECTOR IAW AMM 26-17-15-401PB, OPERATIONS CHECKED GOOD.

Part: LANYARD — OUT OF POSITION (L1 DOOR SLIDE) · airframe 75,460 hrs · 34,247 cycles

F/A REPORTED L1 DOOR WAS NOT SHUTTING LIKE THE OTHER DOORS. MAINTENANCE REPOSITIONED SLIDE LANYARD FROM AFT GIRT BAR. OPS CHECK GOOD.

Part: DIRECTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,423 hrs · 34,226 cycles

CABIN SIGNS AND EMERGENCY LIGHTS FLASHING NO CHIMES OR CALLS ARE WORKING AND PA INOPERATIVE. TRIED CIDS RESET BUT UNSSUCESSFUL. REMOVED CIDS 2 DIRECTOR AND INSTALLED IN CIDS 1 POSITION AND INSTALLED NEW CIDS DIRECTOR IN POSITION NR 2.

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 75,296 hrs · 34,172 cycles

EXIT LENS COVER KNOCKED OFF SEAT 1C. INSTALLED LENS AT SEAT 1C.

Part: LENS — MISSING (CABIN) · airframe 74,448 hrs · 33,763 cycles

LENS COVER IS MISSING FROM EMERGENCY LIGHTING ASSY AT SEAT 7L. INSTALLED NEW LENS TO EMERGENCY LIGHTING ASSY AT SEAT 7L.

Part: LENS — MISSING (CABIN) · airframe 74,402 hrs · 33,743 cycles

EMERGENCY LIGHT LENS MISSING AT SEAT 18L. INSTALLED NEW EMERGENCY LIGHT LENS AT SEAT 18L.

Part: RESERVOIR — LOW PRESSURE (EVAC SLIDE) · airframe 74,254 hrs · 33,674 cycles

CIDS CAUTION LIGHT LT, SLIDE PRESSURE LOW. R & R LEFT OVER WING SLIDE BOTTLE RESERVOIR IAW AMM 25-62-46-00-001-A.

Part: MODULE — INOPERATIVE (CABIN) · airframe 73,596 hrs · 33,368 cycles

EMERGENCY PATH LIGHTING AT SEAT ROW 24 LEFT INOPERATIVE. REPLACED EMERGENCY PATH LIGHT MODULE IN ACCORDANCE WITH AIRBUS MAINTENANCE MANUAL 33-51-19 AT SEAT ROW 24 LEFT.

Part: LENS — MISSING (CABIN) · airframe 73,051 hrs · 33,104 cycles

EMERGENCY AISLE LIGHT LENS IS MISSING AT ROW 24L. INSTALLED EMERGENCY AISLE LIGHT LENS AT ROW 24L.

Part: LENS — MISSING (CABIN) · airframe 71,734 hrs · 32,437 cycles

EMERGENCY SEAT MOUNTED AISLE LIGHT LENS MISSING AT ROW 11DEF. INSTALLED RED LENS ON AISLE SEAT MOUNTED LIGHT AS REQUIRED.

Part: LENS — MISSING (CABIN) · airframe 71,641 hrs · 32,390 cycles

RIGHT FORWARD OVERWING EXIT WALL LIGHT LENS MISSING. REPLACED RIGHT FORWARD OVERWING EXIT WALL LIGHT LENS.

Part: LENS — BROKEN (CABIN) · airframe 70,714 hrs · 31,944 cycles

THE 1L EMERGENCY EXIT FLOOR COVER BROKE. MAINTENANCE REPLACED L1 DOOR EXIT LENS.

Part: EXTINGUISHER — UNSERVICEABLE (COCKPIT) · airframe 69,885 hrs · 31,544 cycles

FLIGHT DECK FIRE EXTINGUISHER PIN MISSING. REMOVED AND REPLACED FLIGHT DECK FIRE EXTINGHISHER.

Part: STRAP — OUT OF POSITION (R2 DOOR) · airframe 69,433 hrs · 31,340 cycles

FLIGHT ATTENDANT REPORTED A LOUD HUMMING NOISE COMING FROM DOOR 2-R. MAINTENANCE FOUND DOOR SLIDE RETAINING STRAP CLOSED IN DOOR - REMOVED AND STOWED STRAP.

Part: LENS — MISSING (CABIN) · airframe 69,243 hrs · 31,250 cycles

EMERGENCY LIGHT LENS MISSING 26L. INSTALLED NEW EMERGENCY LIGHT LENS AT 26L.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 69,203 hrs · 31,231 cycles

AFT RIGHT FLIGHT ATTENDANT FLASHLIGHT NOT FLASHING. REMOVED AND REPLACED FLASHLIGHT AT AFT RIGHT. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 68,965 hrs · 31,112 cycles

MAINTENANCE REPORTED LEFT AFT EMERGENCY LIGHT BATTERY FAULT. REPLACED BATTERY AS REQUIRED.

Part: LEVER — OUT OF ADJUST (R2 DOOR) · airframe 67,604 hrs · 30,489 cycles

FLT 21 - PHX - EES - R2 DOOR ASSIST BOTTLE PERCUSSION MECHANISM KNURLED NUT IS NOT PROPERLY ENGAGED IN DETENT ON STRIKER LEVER. MAINTENANCE REMOVED SAFETY WIRE, ADJUSTED STRIKER LEVER AND RE-SAFTIED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 67,397 hrs · 30,401 cycles

FLT 94 - PHX - EEL - L2 DOOR EMERGENCY LIGHT POWER SUPPLY FAILS BATTERY DURING SLIDE REPLACEMENT. MAINTENANCE REPLACED L2 DOOR POWER SUPPLY BATTERY.

Part: POWER SUPPLY — DEFECTIVE (CABIN) · airframe 67,162 hrs · 30,292 cycles

FLT 596 - PHX - EEL - AIRCRAFT RIGHT, MID-CABIN EMERGENCY LIGHTS FLASHING. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY UNIT IAW AIRBUS MAINTENANCE MANUAL 33-51-38.

Part: DOOR — CRACKED (EMERGENCY EXIT) · airframe 67,058 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - CRACK ON RIGHT AFT EMERGENCY EXIT DOOR 844 BETWEEN FR40 TO FR41 & BETWEEN S14R TO S21R. REPLACED RIGHT AFT EMERGENCY EXIT DOOR 844 IAW JOB CARD 26C83352006 & A320 SRM 52-21-11.

Part: WEB — CORRODED (FUSELAGE) · airframe 67,085 hrs · 30,257 cycles

SAL - MAJOR REPAIR - S5 CHECK - CORROSION ON WEB LOCATED BETWEEN FR33 TO FR34, S38R. REPLACED WEB LOCATED BETWEEN FR33 TO FR34, S38R IAW A320 SRM 51-72-11.

Part: PIN — CORRODED (NR 2 ENG MOUNT) · airframe 67,085 hrs · 30,257 cycles

MAJOR REPAIR - S5 CHECK - CORROSION ON SOLID PIN AFT ENGINE MOUNT LOWER OUTBOARD POSITION ENG 2. REPLACED SOLID PIN AFT ENGINE MOUNT LOWER OUTBOARD POSITION ENG 2 IAW A320 AMM 71-22-11.

Part: PIN — CORRODED (ENGINE MOUNT) · airframe 67,085 hrs · 30,257 cycles

SAL - MAJOR REPAIR - S5 CHECK - CORROSION ON SOLID PIN AFT ENGINE MOUNT LOWER CENTER POSITION ENGINE NR 2. REPLACED SOLID PIN AFT ENGINE MOUNT LOWER CENTER POSITION ENGINE NR 2 IAW A320 AMM 71-22-11.

Part: PIN — CORRODED (ENGINE MOUNT) · airframe 67,085 hrs · 30,257 cycles

SAL - MAJOR REPAIR - S5 CHECK - CORROSION ON SOLID PIN AFT ENGINE MOUNT LOWER INBOARD POSITION ENGINE NR 2. REPLACED SOLID PIN AFT ENGINE MOUNT LOWER INBOARD POSITION ENGINE NR 2 IAW A320 AMM 71-22-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 261DF BETWEEN FR66 TO FR68 & BETWEEN -Y765 TO -Y765. REPLACED FLOOR PANEL 261DF BETWEEN FR66 TO FR68 & BETWEEN -Y765 TO -Y765 IAW A320 SRM 53-02-00 & IRM 9701 REV G.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,085 hrs · 30,257 cycles

SAL -MAJOR REPAIR - S5 CHECK - CRACKED WEB LOCATED Y765 BTW FR 8 TO FR 11 IN COCKPIT. REPLACED WEB LOCATED Y765 BETWEEN FR 8 TO FR 11 IN COCKPIT IAW A320 SRM 51-72-11.

Part: ATTACH FITTING — CORRODED (PYLON) · airframe 67,085 hrs · 30,257 cycles

SAL - MAJOR REPAIR - S5 CHECK - CORROSION ON THE RIGHT WING TO PYLON AFT ATTACH FITTING AT RIB 10. REPLACED THE RIGHT WING TO PYLON AFT ATTACH FITTING AT RIB 10 IAW TASK CARD 26C40054026.

Part: PIN — CORRODED (ENGINE MOUNT) · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON PIN OF NR 2 ENGINE AFT ENGINE MOUNT LOWER OUTBOARD POSITION BETWEEN PYLON STA 6465 TO STA 7063 & BETWEEN RIB 3 TO RIB 5. REPLACED PIN OF NR 2 ENGINE AFT ENGINE MOUNT LOWER OUTBOARD POSITION IAW A320 AMM 71-22-11-0401.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,085 hrs · 30,257 cycles

S5 - MAJOR REPAIR - LEVEL 2 CORROSION ON SEAT TRACK AT FR25, -Y1292. REPAIRED SEAT TRACK AT FR27 + 10 INCHES, -Y1292 IAW SRM 53-21-15 & AIRBUS DRAWING D53112812.

Part: FITTING — CORRODED (LT PYLON) · corrosion level 2 · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON LEFT PYLON SPIGOT FITTING BORE BETWEEN LEFT PYLON STA 6465 TO STA063. REPLACED LEFT PYLON SPIGOT FITTING BETWEEN LEFT PYLON STA 6465 TO STA 063 IAW A320 SRM 54-51-12.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 67,085 hrs · 30,257 cycles

SAL - MAJOR REPAIR - S5 CHECK - CABIN FLOOR PANEL 251LF HAS DELAMINATION. REPLACED CABIN FLOOR PANEL 251LF.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 670,805 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON SHEAR PLATE BETWEEN FR58 TO FR59, S38L. REPLACED SHEAR PLATE BETWEEN FR58 TO FR59, S38L IAW A320 SRM 51-72-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,085 hrs · 30,257 cycles

S5 CHECK- MAJOR REPAIR - CORROSION ON SHEAR TIE CLEAT AT FR31 BETWEEN S40R TO S41R. REPLACED SHEAR TIE CLEAT AT FR31 BETWEEN S40R TO S41R IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON FLOORBEAM BETWEEN FR56 TO FR57, S44. REPLACED FLOORBEAM BETWEEN FR56 TO FR57, S44 IAW A320 SRM 51-72-11 & AIRBUS DRAWING 53470001.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,085 hrs · 30,257 cycles

S5 CHECK - MAJOR REPAIR - CORROSION ON CROSSBEAM AT FR33 BETWEEN S38L TO S38R. REPLACED CROSSBEAM AT FR33 BETWEEN S38L TO S38R IAW SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON SHEAR PLATE WEB BETWEEN FR54 TO FR55, S38L. REPLACED SHEAR PLATE WEB BETWEEN FR54 TO FR55, S38L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53470320.

Part: FITTING — CORRODED (FUSELAGE) · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON AFT LOWER CORNER FITTING OF L-1 DOOR AT FR20, S23L. REPLACED AFT LOWER CORNER FITTING OF L-1 DOOR AT FR20, S23L IAW A320 SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,085 hrs · 30,257 cycles

S5 - MAJOR REPAIR - LEVEL 2 CORROSION ON CLEAT AT FR31 BETWEEN S41R TO S42R. REPLACED CLEAT AT FR31 BETWEEN S41R TO S42R IAW SRM 51-72-11 & DRAWING D53231582.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - CRACK ON WEB OF FLOOR STRUCTURE AT FR6, Y869. REPAIRED WEB OF FLOOR STRUCTURE AT FR6, Y869 IAW EA 133257.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON STRINGER BETWEEN FR28 TO FR28 + 19 INCHES, S40L. REPAIRED STRINGER BETWEEN FR28 TO FR28 + 19 INCHES, S40L IAW A320 SRM 53-21-13.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,085 hrs · 30,257 cycles

S5 CHECK - MAJOR REPAIR - CORROSION ON CLEAT AT FR28 BETWEEN S42R TO S43R. REPLACED CLEAT AT FR28 BETWEEN S42R TO S43R IAW SRM 51-72-11.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - CRACK IN WEB AT FR14 BETWEEN S1R TO S1L. REPLACED WEB AT FR14 BETWEEN S1R TO S1L IAW A320 SRM 51-72-11.

Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON NR 3 SPOILER INNER HINGE PIN AT LEFT WING STA 7792, RIB 14. REPLACED NR 3 SPOILER INNER HINGE PIN AT LEFT WING STA 7792, RIB 14 IAW A320 AMM 27-64-43.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - CRACK ON FITTING AT FR24A BETWEEN S34L TO S35L. REPLACED FITTING AT FR24A BETWEEN S34L TO S35L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53911160.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON CORNER FITTING AT FR20, S23R. REPLACED CORNER FITTING AT FR20, S23R IAW A320 SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FORWARD LOWER CORNER FITTING OF R-1 DOOR CUTOUT AT FR16, S23R. REPLACED FORWARD LOWER CORNER FITTING OF R-1 DOOR CUTOUT AT FR16, S23R IAW A320 SRM 51-72-11 & EA 133272.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 67,085 hrs · 30,257 cycles

SAL - MAJOR REPAIR - S5 CHECK - CABIN FLOOR PANEL 242FF HAS DELAMINATION. REPLACED CABIN FLOOR PANEL 242FF.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 232DF BETWEEN FR20 TO FR24, S23R & BETWEEN -Y765 TO -Y254. REPLACED FLOOR PANEL 232DF BETWEEN FR20 TO FR24, S23R & BETWEEN -Y765 TO -Y254 IAW A320 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 67,085 hrs · 30,257 cycles

SAL - MAJOR REPAIR - S5 CHECK - CABIN FLOOR PANEL 242GF HAS DELAMINATION. REPLACED CABIN FLOOR PANEL 242GF.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,085 hrs · 30,254 cycles

SAL - S5 - MAJOR REPAIR - 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 D53110876.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - CRACK ON RIGHT SEGMENT ANGLE AT EMERGENCY EXIT HATCH 843 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3. PERFORMED ENGINEERING ORDER MODIFICATION 5210Y228 ON RIGHT LOAD TRANSMITTING PROFILE AT EMERGENCY EXIT HATCH 843 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 67,085 hrs · 30,257 cycles

SAL - MAJOR REPAIR - S5 CHECK - CABIN FLOOR PANEL 241EF HAS DELAMINATION. REPLACED CABIN FLOOR PANEL 241EF.

Part: STRUCTURE — CORRODED (EMERGENCY EXIT) · corrosion level 2 · airframe 67,085 hrs · 30,257 cycles

S5 - MAJOR REPAIR - LEVEL 2 CORROSION ON RIGHT AFT EMERGENCY EXIT HATCH LOWER LEFT CURVED EDGE BETWEEN FR40 TO FR41 BEAM 4. REPLACED RIGHT AFT EMERGENCY EXIT HATCH LOWER LEFT CURVED EDGE BETWEEN FR40 TO FR41 BEAM IAW SRM 51-72-11 & DRAWING D52279028204.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 67,085 hrs · 30,257 cycles

SAL - MAJOR REPAIR - S5 CHECK - CABIN FLOOR PANEL 251RF HAS DELAMINATION. REPLACED CABIN FLOOR PANEL 251RF.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - CRACK ON LEFT SEGMENT ANGLE AT EMERGENCY EXIT HATCH 843 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3. PERFORMED ENGINEERING ORDER MODIFICATION 5210Y228 ON LEFT SEGMENT ANGLE AT EMERGENCY EXIT HATCH 843 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - CRACK ON LEFT SEGMENT ANGLE AT EMERGENCY EXIT HATCH 834 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. PERFORMED ENGINEERING ORDER MODIFICATION 5210Y228 ON LEFT SEGMENT ANGLE AT EMERGENCY EXIT HATCH 834 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY BETWEEN FR12 TO FR16, -Y81. REPLACED RAIL DUMMY BETWEEN FR12 TO FR16, -Y81 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112619.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - DELAMINATION ON SURFACE OF FLOOR PANEL 261NF BETWEEN FR64 TO FR66, -Y765 TO Y765. REPLACED FLOOR PANEL 261NF BETWEEN FR64 TO FR66, -Y765 TO Y765 IAW A320 SRM 53-02-00 & MCGILL IRM 9701 REV G.

Part: STRUCTURE — CORRODED (EMERGENCY EXIT) · corrosion level 2 · airframe 67,085 hrs · 30,257 cycles

S5 CHECK - MAJOR REPAIR - LEVEL 2 CORROSION ON LEFT AFT EMERGENCY EXIT HATCH LOWER RIGHT CURVED EDGE BETWEEN FR40 TO FR41 BEAM 4. REPLACED LEFT AFT EMERGENCY EXIT HATCH LOWER RIGHT CURVED EDGE BETWEEN FR40 TO FR41 BEAM 4 IAW 51-72-11 & DRAWING D2279010.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - CRACK ON LEFT LOAD TRANSMITTING PROFILE AT EMERGENCY EXIT HATCH 844. PERFORMED ENGINEERING ORDER MODIFICATION 5210Y228 ON LEFT LOAD TRANSMITTING PROFILE AT EMERGENCY EXIT HATCH 844.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - CRACK ON LEFT SEGMENT ANGLE AT EMERGENCY EXIT HATCH 833 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3. PERFORMED ENGINEERING ORDER MODIFICATION 5210Y228 ON LEFT SEGMENT ANGLE AT EMERGENCY EXIT HATCH 833 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - CRACK ON RIGHT LOAD TRANSMITTING PROFILE AT EMERGENCY EXIT HATCH 844. PERFORMED ENGINEERING ORDER MODIFICATION 5210Y228 ON RIGHT LOAD TRANSMITTING PROFILE AT EMERGENCY EXIT HATCH 844.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - CRACK ON RIGHT SEGMENT ANGLE AT EMERGENCY EXIT HATCH 833 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3. PERFORMED ENGINEERING ORDER MODIFICATION 5210Y228 ON RIGHT SEGMENT ANGLE AT EMERGENCY EXIT HATCH 833 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3.

Part: BEAM — CRACKED (EMERGENCY EXIT) · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - CRACK ON LEFT SEGMENT BEAM AT EMERGENCY EXIT HATCH 834 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. PERFORMED ENGINEERING ORDER MODIFICATION 5210Y228 ON LEFT SEGMENT BEAM AT EMERGENCY EXIT HATCH 834 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,085 hrs · 30,257 cycles

S5 CHECK- MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR20, -Y765. REPLACED SEAT TRACK AT FR20, -Y765 IAW A320 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 INTERGRANULAR CORROSION ON LOWER DOOR SILL OF R-2 DOOR CUTOUT AT FR68, S23R. REPAIRED LOWER DOOR SILL OF R-2 DOOR CUTOUT AT FR68, S23R IAW EA 133246.

Part: SLIDE RAFT — DEFECTIVE (PAX DOOR) · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - EES - OVER INFLATED SLIDE RAFT PACK ASSEMBLY AT PASSENGER CREW DOOR 831. REPLACED SLIDE RAFT PACK ASSEMBLY AT PASSENGER CREW DOOR 831 IAW JOB CARD 26C83152008.

Part: SLIDE RAFT — DEFECTIVE (PAX DOOR) · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - OVER INFLATE SLIDE RAFT PACK ASSEMBLY AT PASSENGER / CREW DOOR 842. REPLACED SLIDE RAFT PACK ASSEMBLY AT PASSENGER / CREW DOOR 84 IAW A320 AMM 25-62-44.

Part: EPSU — FAILED (CABIN) · airframe 66,775 hrs · 30,115 cycles

FLT 342-LAS - EEL - FORWARD EMERGENCY POWER SUPPLY UNIT (10WL) FAILED TEST PER T/C 26C00033004. MAINTENANCE REMOVED AND REPLACED FORWARD EPSU 10WL.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 66,705 hrs · 30,087 cycles

FLT 9245 - PHX - EEL - FOUND BROKEN WIRE AT EMERGENCY LIGHT ROW 11 LEFT. MAINTENANCE INSTALLED NEW SEAT HARNESS ROW 11 LEFT IAW AIRBUS MAINTENANCE MANUAL 33-51-19.

Part: PIN — CRACKED (NLG) · airframe 67,085 hrs · 30,257 cycles

SAL - S5 - MAJOR REPAIR - CRACKS ON NOSE LANDING GEAR TORQUE LINKS CENTER HINGE PIN BETWEEN FR16 TO FR20 & BETWEEN S41L TO S41R. REPLACED NOSE LANDING GEAR TORQUE LINKS CENTER HINGE PIN IAW EA 133294.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 66,082 hrs · 29,815 cycles

FLT 614 - ODOR IN CABIN. REMOVED AND REPLACED APU. OPERATIONAL AND LEAK CHECK GOOD. VENDOR REPORT INDICATED NO IMMEDIATE INDICATION OF OIL CONTAMINATION IN BLEED SYSTEM OR ISSUES WITH LOAD COMPRESSOR SEAL DURING BOROSCOPE. UNIT WAS STEAM CLEANED AND RETURNED TO SERVICE.

Part: B-NUT — LOOSE (HYDRAULIC SYS) · airframe 65,951 hrs · 29,755 cycles

FLT 128 - PHX - CABIN ODOR - PASSENGERS COMPLAINED OF DIRTY-SOCK SMELL THROUGHOUT CABIN. ODOR ALSO IN FLIGHT DECK. MAINTENANCE FOUND A LEAK AT THE YELLOW HYDRAULIC QUICK DISCONNECT PANEL. TORQUED YELLOW QUICK DISCONNECT SUPPLY SIDE B-NUT BEHIND QD PANEL IAW AIRBUS MAINTENANCE MANUAL 20-21-12.

Part: LENS — BROKEN (CABIN) · airframe 65,355 hrs · 29,492 cycles

FLT 324 PHX - EEL - EMERGENCY EXIT LIGHT COVER ON BULKHEAD ACROSS FROM 1 FLIGHT ATTENDANT JUMP SEAT BROKEN. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT LENS.

Part: LENS — OUT OF POSITION (CABIN) · airframe 64,699 hrs · 29,205 cycles

FLT 29 - LAX - EEL - EMERGENCY EXIT LIGHT COVER AT SEAT 11D FELL OFF. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT COVER AT SEAT 11D.

Part: LENS — MISSING (CABIN) · airframe 64,398 hrs · 29,070 cycles

FLT 122 - PHX - EEL - EMERGENCY PATHWAY LIGHT LENS MISSING SEAT 9C. MAINTENANCE INSTALLED NEW LIGHT LENS SEAT 9C.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 64,194 hrs · 28,976 cycles

FLT 342 - LAS - EEL - AFT EMERGENCY POWER SUPPLY (EMERGENCY EXIT LIGHTS) FAULTS INTERNAL LOADS. MAINTENANCE REMOVED AND REPLACED AFT EMERGENCY POWER SUPPLY.

Part: EPSU — DISCHARGED (CABIN) · airframe 64,134 hrs · 28,950 cycles

FLT 614 - PHX - ATL - EMERGENCY LIGHTS - SEVERAL EMERGENCY LIGHTS IN AFT CABIN AREA INOPERATIVE ON TEST. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (EPSU) IN AFT CABIN PER AMM 33-51-38. OPERATIONAL TEST WAS GOOD.

Part: LENS — MISSING (R2 DOOR) · airframe 64,101 hrs · 28,936 cycles

FLT 457 - PHX - EMERGENCY EGRESS SYSTEM - "SLIDE ARMED" LIGHT COVER MISSING DOOR 2R. MAINTENANCE INSTALLED SLIDE ARMED LENS COVER AT DOOR 2R.

Part: FILTER — CONTAMINATED (AC BAY) · airframe 63,430 hrs · 28,620 cycles

FLT 7 - PHX - CABIN ODOR - FLIGHT ATTENDANT REPORTED "STINKY SOCK" SMELL DURING DESCENT - APU NEVER STARTED. MAINTENANCE COMPLIED WITH STAGE 3 BORESCOPE ON BOTH ENGINES AND NO OIL WAS PRESENT. FOUND APU OIL OVERSERVICED AND INLET WET WITH OIL. DRAINED RESERVOIR TO FULL MARK AND CLEANED APU. REMOVED AND REPLACED BOTH OZONE FILTERS.

Part: FILTER — CONTAMINATED (CABIN) · airframe 63,430 hrs · 28,620 cycles

FLT 7 - PHX - CABIN ODOR - FLIGHT ATTENDANT REPORTED "STINKY SOCK" SMELL DURING DESCENT - APU NEVER STARTED. MAINTENANCE COMPLIED WITH STAGE 3 BORESCOPE ON BOTH ENGINES AND NO OIL WAS PRESENT. FOUND APU OIL OVER SERVICED AND INLET WET WITH OIL. DRAINED RESERVOIR TO FULL MARK AND CLEANED APU. REMOVED AND REPLACED BOTH OZONE FILTERS.

Part: CONTROL UNIT — FAULTED (CABIN) · airframe 63,287 hrs · 28,557 cycles

A-CK PHX - EEL - AFT EMERGENCY LIGHT CONTROL UNIT FAULTS. MAINTENANCE REPLACED AFT EMERGENCY LIGHT CONTROL UNIT PER AIRBUS MAINTENANCE MANUAL 33-51-38.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 63,287 hrs · 28,557 cycles

A-CK PHX - EEL - AFT EMERGENCY LIGHT CONTROL UNIT FAULTS INTERIOR & EXTERIOR LIGHTS. MAINTENANCE REPLACED AFT EMERGENCY LIGHT POWER SUPPLY & BATTERY PER AIRBUS MAINTENANCE MANUAL 33-51-38.

Part: BATTERY — DISCHARGED (CABIN) · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - EEL - NR 6194862 - LOW BATTERY OF EPSU ALONG PASSENGER CABIN AT FORWARD UTILITY AREA. REPLACED EPSU BATTERY ALONG PASSENGER CABIN AT FORWARD UTILITY AREA IAW A320 AMM 33-51-38.

Part: BATTERY — DISCHARGED (CABIN) · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - EEL - NR 6194862 - LOW BATTERY OF EPSU ALONG PASSENGER CABIN AT AFT UTILITY AREA. REPLACED EPSU BATTERY ALONG PASSENGER CABIN AT AFT UTILITY AREA IAW A320 AMM 33-51-38.

Part: SKIN PANEL — CONTAMINATED (ELEVATOR) · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - NR 6205727, 6205726, 6205728 & 6206177 - TRAPPED WATER AT SEVERAL LOCATIONS IN LEFT HAND ELEVATOR UPPER SKIN PANEL. REPLACED LEFT HAND ELEVATOR IAW A320 AMM 27-34-41.

Part: BATTERY — DISCHARGED (CABIN) · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - EEL - NR 6194862 - LOW BATTERY OF EPSU ALONG PASSENGER CABIN AT RIGHT HAND EMERGENCY EXIT DOOR. REPLACED EPSU BATTERY ALONG PASSENGER CABIN AT RIGHT HAND EMERGENCY EXIT DOOR IAW A320 AMM 33-51-38.

Part: BATTERY — DISCHARGED (CABIN) · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - EEL - NR 6194862 - LOW BATTERY OF EPSU ALONG PASSENGER CABIN AT LEFT HAND EMERGENCY EXIT DOOR. REPLACED EPSU BATTERY ALONG PASSENGER CABIN AT LEFT HAND EMERGENCY EXIT DOOR IAW A320 AMM 33-51-38.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - NR 6205979 - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66+ 5 INCHES TO FR67 + 17 INCHES, -Y1162. REPLACED FLOORBEAM BETWEEN FR66+ 5 INCHES TO FR67 + 17 INCHES, -Y1162 IAW A320 SRM 51-72-11. THIS DISCREPANCY IS DETERMINED TO BE LEVEL 2 CORROSION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR20 TO FR24, Y765. REPLACED SEAT TRACK BETWEEN FR20 TO FR24, Y765 IAW A320 SRM 51-72-11.

Part: STRUCTURE — CRACKED (ZONE 100) · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - CRACK ON TRAY AT FR68 TO FR69, Y1732. REPLACED TRAY AT FR68 TO FR69, Y1732 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR34, -Y765. REPAIRED SEAT TRACK AT FR34, -Y765 IAW A320 SRM 53-00-15.

Part: PLATE — CORRODED (FUSELAGE) · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - CORROSION ON LOWER SILL PLATE AT BULK CARGO DOOR AT FR62, S38R. REPAIRED LOWER SILL PLATE AT BULK CARGO DOOR AT FR62, S38R IAW A320 SRM 53-41-49.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - NR 6205978 - LEVEL 2 GALVANIC CORROSION R-2 LOWER DOOR SILL BETWEEN FR66 TO FR67, -Y1732. REPLACED R-2 LOWER DOOR SILL BETWEEN FR66 TO FR67, -Y1732 IAW A320 SRM 53-41-14. THIS DISCREPANCY IS DETERMINED TO BE LEVEL 2 CORROSION.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON WEB SUPPORT BETWEEN FR69 TO FR70, -Y765. REPLACED WEB SUPPORT BETWEEN FR69 TO FR70 IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 TO FR67, Y1195. REPLACED FLOORBEAM BETWEEN FR66 TO FR67,Y1195 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 +5 INCHES TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66 +5 INCHES TO FR70, -Y765 IAW A320 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - NR 6205971 - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, Y1732. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, Y1732 IAW A320 SRM 51-72-11. THIS DISCREPANCY IS DETERMINED TO BE LEVEL 2 CORROSION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR20 TO FR23, -Y189. REPLACED FLOORBEAM BETWEEN FR20 TO FR23, -Y189 IAW SRM 51-72-11. THIS DISCREPANCY IS DETERMINED TO BE LEVEL 2 CORROSION.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - NR 6069928 - CRACK IN FLOOR FORWARD PRESSURE PANEL AT FR36, -Y1292. REPAIRED FLOOR FORWARD PRESSURE PANEL AT FR36, -Y1292 IAW US AIRWAYS ENGINEERING CARD M2C53307.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - NR 6205974 - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, -Y1732. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, -Y1732 IAW A320 SRM 51-72-11. THIS DISCREPANCY IS DETERMINED TO BE LEVEL 2 CORROSION. ADDED ''LEVEL 2'' TO DISCREPANCY AND MARKED CORROSION LEVEL INDICATOR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR20 TO FR24, -Y1292. REPLACED SEAT TRACK BETWEEN FR20 TO FR24, -Y1292 IAW A320 SRM 51-72-11.

Part: SKIN — CONTAMINATED (ELEVATOR) · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - TRAPPED WATER DETECTED IN RIGHT ELEVATOR UPPER SKIN. REPAIRED RIGHT ELEVATOR UPPER SKIN IAW A320 SRM 51-77-13.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,904 hrs · 34,096 cycles

SAL - C7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67 TO FR69, Y1165. REPLACED FLOORBEAM BETWEEN FR67 TO FR69, Y1165 IAW SRM 51-72-11.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 62,990 hrs · 25,431 cycles

SAL - C7 - MAJOR REPAIR - NR 6069929 - CRACK AT PRESSURE PANEL AT FR36, Y1292. REPAIRED PRESSURE PANEL AT FR36, Y1292 IAW US AIRWAYS ENGINEERING CARD M2C53306.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - NR 6069841 & 6077472 - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR20 TO FR24, -Y765. REPLACED SEAT TRACK BETWEEN FR20 TO FR24, -Y765 IAW A320 SRM 51-72-11. THIS DISCREPANCY IS DETERMINED TO BE LEVEL 2 CORROSION.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - CORROSION ON WEB AT FR20 TO FR21, -Y1584. REPLACED WEB AT FR20 TO FR21, -Y1584 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - LEVEL 2 CORROSION ON SEAT BEAM RAIL BETWEEN FR64 TO FR66, Y765. REPLACED SEAT BEAM RAIL BETWEEN FR64 TO FR66, Y765 IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SUPPORT FLOOR STRUCTURE BETWEEN FR16 TO FR20, -Y1292. REPLACED SUPPORT FLOOR STRUCTURE IAW SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LOWER SILL OF R-2 DOOR AT FR68 , -Y1732. REPAIRED LOWER SILL OF R-2 DOOR AT FR68 , -Y1732 IAW SRM 53-41-14.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,990 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FRAME SUPPORT BETWEEN FR69 TO FR70, Y1732. REPLACED FRAME SUPPORT BETWEEN FR69 TO FR70, Y1732 IAW SRM 51-72-11.

Part: TRAY — CRACKED (FUSELAGE) · airframe 62,990 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - CRACK ON COVER SHEET TRAY BETWEEN FR68 TO FR69, -Y1732. REPLACED COVER SHEET TRAY BETWEEN FR68 TO FR69, -Y1732 IAW A320 SRM 51-72-11.

Part: RIB — CRACKED (RT NACELLE) · airframe 29,906 hrs · 28,431 cycles

SAL - C7 - MAJOR REPAIR - CRACK ON RIGHT PYLON AFT FIXED FAIRING ON RIB 14 AT INTERNAL AREA LOWER SIDE. REPLACED RIGHT PYLON AFT FIXED FAIRING RIB 14 IAW A320 SRM 51-72-11.

Part: INTAKE — DIRTY (APU) · airframe 62,987 hrs · 28,430 cycles

FLT 351 - PHX - ODOR - PILOT REPORTED APU BLEED PRODUCES VERY STRONG NOXIOUS ODOR. MAINTENANCE PERFORMED APU AIR INTAKE CLEAN AND OPERATIONAL CHECK WAS GOOD WITH NO SMELL NOTED.

Part: SLIDE RAFT — DEFECTIVE (L1 DOOR) · airframe 62,610 hrs · 28,262 cycles

FLT 117 - PHX - EMERGENCY EGRESS SYSTEM - CANNOT INSERT LOCKOUT PIN ON L1 DOOR SLIDE. MAINTENANCE REMOVED AND REPLACED THE L1 DOOR SLIDE.

Part: BLEED VALVE — FAULTY (NR 1 ENGINE) · airframe 62,520 hrs · 28,219 cycles

FLT 79 - PHX-SEA - RETURN TO FIELD - NR 1 ENGINE COMPRESSOR STALLED AFTER ROTATION. ENGINE 1 EGT 611+HIGH FUEL FLOW+HIGH OIL PRESS 301 PSI+. AFTER REDUCING POWER (LEVELED FLIGHT) ENGINE PARAMETERS WERE NORMAL. CREW ELECTED TO RETURN TO PHX AND NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE 7C BLEED VALVE.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 62,171 hrs · 28,067 cycles

FLT 117 - ATL-PHX - EMERGENCY EQUIPMENT - L-2 DOOR DAMPER CYLINDER OUT OF LIMITS. SERVICED L-2 DOOR DAMPER CYLINDER PER AIRBUS MAINTENANCE MANUAL 52-10-00.

Part: CYLINDER — LOW PRESSURE (PAX DOOR) · airframe 62,171 hrs · 28,067 cycles

FLT 117 - ATL-PHX - EMERGENCY EQUIPMENT - LEFT AFT PASSENGER DOOR EMERGENCY CYLINDER PRESSURE LOW. SERVICED LEFT AFT PASSENGER DOOR EMERGENCY CYLINDER AS REQUIRED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,949 hrs · 27,952 cycles

FLT NR 123 MKE-PHX - EMERGENCY LIGHT - A/C RT MID EMERGENCY LIGHT FAILED TEST. MX R&R A/C RT MID EMERGENCY BATTERY. OPS CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 61,775 hrs · 27,871 cycles

FLT 296 LAS-SEA - EMERGENCY EQUIPMENT - L2 DOOR ASSIST BOTTLE REQUIRES SERVICING. MAINTENANCE SERVICED L2 DOOR ASSIST BOTTLE PER AIRBUS MAINTENANCE MANUAL 52-10-00-614.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 61,477 hrs · 27,730 cycles

FLT 614 - PHX-ATL - EEL - EMERGENCY LIGHTS INOP 26-L, 22-L, 15-L, 7-L AND 3-L SEAT ENDS. MAINTENANCE REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT POWER SUPPLY UNIT. OPERATIONAL CHECK WAS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,448 hrs · 26,801 cycles

FLT 43 - PHX - EEL - EMERGENCY LIGHTS WILL NOT PASS TEST AT FLIGHT ATTENDANT PANEL. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT 10WL. SYSTEM TEST OK.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 58,170 hrs · 26,253 cycles

SAL - EEL - C6 CHECK - ROW 10 EMERGENCY LIGHTS DID NOT ILLUMINATE DURING OPERATIONAL TEST. REPLACED AND FUNCTIONAL CHECKED MIDDLE POWER SUPPLY IAW A320 AMM 33-51-00.

Part: FITTING — CORRODED (FUSELAGE) · airframe 58,170 hrs · 26,253 cycles

SAL - MAJOR REPAIR - C-6 CHECK - CORROSION ON FWD CORNER FITTING OF LEFT AFT PASSENGER CREW DOOR AT BS 3158+3"/ FR 66 + 3", S23L. REPLACED FWD CORNER FITTING OF LEFT AFT PASSENGER CREW DOOR AT BS 3158+3"/ FR 66 + 3", S23L IAW A320 SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · airframe 58,170 hrs · 26,253 cycles

SAL - MAJOR REPAIR - C-6 CHECK - CORROSION ON AFT CORNER FITTING OF LEFT AFT PASSENGER CREW DOOR AT BS 3257/ FR 68. REPLACED AFT CORNER FITTING OF LEFT AFT PASSENGER CREW DOOR AT BS 3257/ FR 68 IAW A320 SRM 51-72-11.

Part: FITTING — CORRODED (ZONE 200) · airframe 58,170 hrs · 26,253 cycles

SAL - MAJOR REPAIR - C6 CHECK - CORROSION ON THE R2 DOOR CUTOUT LOWER SILL CENTER SHAPE SILL FITTING, BS 3158 / FR 66 - BS 3257 / FR 68. REPLACED THE R2 DOOR CUTOUT LOWER SILL CENTER SHAPE SILL FITTING, BS 3158 / FR 66 - BS 3257 / FR 68 IAW A320 SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 58,170 hrs · 26,253 cycles

SAL - MAJOR REPAIR - C-6 CHECK - DELAMINATION ON CABIN FLOOR PANEL 241JF , BS 1869/FR42 - BS 2136/FR47, -Y254 - Y254. REPLACED CABIN FLOOR PANEL 241JF, BS 1869/FR42 - BS 2136/FR47, -Y254 - Y254 IAW A320 SRM 53-02-00 TABLE 103 AND IRM 9701 REV F.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 55,342 hrs · 24,942 cycles

PHX - EEL - EMERGENCY EXIT LIGHTS TEST FAILS-INT. LOADS EMERG. L, AND COMM EMERG L. MX REMOVED AND REPLACED THE LEFT MID EMERGENCY POWER SUPPLY UNIT IAW MM 33-51-38PB401. OPS CHECK WAS GOOD.

Part: PUMP — LEAKING (NR 1 ENGINE) · airframe 53,972 hrs · 24,333 cycles

PHX - EL - FLT - 057 - WHILE EN ROUTE TO PHX, THE CREW DISCOVERED THAT THE GREEN HYDRAULIC SYSTEM QUANTITY WAS INDICATING ZERO. INBOUND TO PHX THE CREW DECLARED AN EMERGENCY. THE PASSENGERS DID NOT BRACE. THE LANDING WAS UNEVENTFUL. THE FIRE DEPARTMENT EXAMINED THE BRAKES AND NO DISCREPANCIES WERE NOTED. THE AIRCRAFT WAS TOWED FROM THE RUNWAY TO THE GATE. UPON INSPECTION OF THE NR 1 ENGINE, IT WAS DISCOVERED THAT THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP WAS LEAKING. MAINTENANCE REPLACED THE NR 1 EDP. OPERATIONAL/LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BEAM — CRACKED (ZONE 500)

SAL - DURING C5 CHECK DISCOVERED CRACK ON SUPPORT ANGLE LOCATED AT THE TRAILING EDGE BETWEEN RIB 23 AND RIB 24 OF THE LEFT WING. MAINTENANCE REMOVED AND REPLACED THE BEAM ASSEMBLY ON THE TRAILING EDGE OF THE LT WING RIB 23 TO RIB 24 IAW AIRBUS 320 SRM 51-72-11.

Part: NUT — CORRODED (LT MLG) · airframe 53,072 hrs · 23,932 cycles

SAL - DURING C5 CHECK DISCOVERED CORROSION IN LT MLG FWD BEARING PINTLE PIN RETAINING NUT. MAINTENANCE REMOVED AND REPLACED RETAINING NUT IAW SRM 57-26-13 PAGES 229 TO 232.

Part: NUT — CORRODED (RT MLG) · airframe 53,072 hrs · 23,932 cycles

SAL - DURING C5 CHECK DISCOVERED CORROSION IN THE FORWARD BEARING PINTLE PIN RETAINING NUT ON THE RT MLG. MAINTENANCE REMOVED AND REPLACED THE FORWARD BEARING PINTLE PIN RETAINING NUT ON THE RT MLG IAW AIRBUS 320 SRM 57-26-13 PAGES 224 TO 232.

Part: FLOOR PANEL — BROKEN (FUSELAGE) · airframe 53,072 hrs · 23,932 cycles

SAL - DURING C5 CHECK MAINTENANCE DISCOVERED FLOOR PANEL 241AF CRACKED 15 INCHES. MAINTENANCE REMOVED, FABRICATED AND INSTALLED FABRICATED FLOOR PANEL 241KF IAW IRM 9701 REV. F AND AIRBUS 320 SRM 53-02-00 TABLE 3.

Part: SUPPORT FITTING — DAMAGED (ZONE 500) · airframe 53,072 hrs · 23,932 cycles

SAL - DURING C5 CHECK DISCOVERED ELONGATE HOLE ON THE FRAME SUPPORT FITTING OF THE LT AILERON AT RIB 23. MAINTENANCE REMOVED AND INSTALLED NEW FRAME SUPPORT FITTING ON THE LT AILERON AT RIB 23 IAW AIRBUS 320 SRM 51-72-11.

Part: CHANNEL — CRACKED (ZONE 500) · airframe 53,072 hrs · 23,932 cycles

SAL - DURING C5 CHECK DISCOVERED CRACK ON TRAILING EDGE (T/E) CHANNEL ON THE LT WING, T/E AILERON. MAINTENANCE REMOVED AND INSTALLED NEW T/E CHANNEL ON THE LT WING, T/E AILERON IAW AIRBUS 320 SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 53,072 hrs · 23,932 cycles

SAL - DURING C5 CHECK MAINTENANCE DISCOVERED FLOOR PANEL 251RF DELAMINATED. MAINTENANCE REMOVED, FABRICATED AND INSTALLED FABRICATED FLOOR PANEL 251RF IAW IRM 9701 REV F AND AIRBUS 320 SRM 53-02-00 TABLE 3.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 53,072 hrs · 23,932 cycles

SAL - DURING C5 CHECK MAINTENANCE DISCOVERED FLOOR PANEL 231KF DELAMINATED. MAINTENANCE REMOVED, FABRICATED AND INSTALLED FABRICATED FLOOR PANEL 231KF IAW IRM 9701 REV. F AND AIRBUS 320 SRM 53-02-00 TABLE 3.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 53,072 hrs · 23,932 cycles

SAL - DURING C5 CHECK MAINTENANCE DISCOVERED FLOOR PANEL 231RF DELAMINATED. MAINTENANCE REMOVED, FABRICATED AND INSTALLED FABRICATED FLOOR PANEL 231RF IAW IRM 9701 REV F AND AIRBUS 320 SRM 53-02-00 TABLE 3.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 50,478 hrs · 22,842 cycles

PHX - EES - DURING 4-DAY CHECK WHILE REMOVING GIRT BAR FROM THE L1 DOOR, THE SLIDE DROPPED OUT OF THE BOTTOM. MAINTENANCE REMOVE AND REPLACED THE L1 DOOR SLIDE IAW AMERICA WEST AIRLINES TASK CARD R1C25304. VENDOR FOUND NO FAULTS WITH SLIDE. UNIT WAS OVERHAULED IAW CMM 25-61-20 REV. 9.

Part: WIRE — BROKEN (CABIN) · airframe 49,458 hrs · 22,412 cycles

SEA - EEL - DURING FUNCTIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM-A BROKEN WIRE WAS FOUND AT THE WALL CONNECTOR FOR THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 17 LT. MAINTENANCE REPINNED THE EMERGENCY ESCAPE PATH LIGHT WIRE TO THE WALL CONNECTOR AT SEAT ROW 17 LT, OPERATIONAL CHECK WAS GOOD.

Part: ENGINE — FAILED (NR 1) · airframe 49,458 hrs · 22,412 cycles

ON TAKEOFF AT SEA EN ROUTE FOR PHX AFTER APPLYING TAKEOFF THRUST FLIGHT CREW HEARD A LOUD BANG ON LT SIDE OF AIRCRAFT FOLLOWED BY A BURNING ODOR, REJECTED TAKEOFF AT 20 KTS, ANOTHER AIRCRAFT REPORTED SEEING FIRE COMING OUT OF THE NR 1 ENGINE, FIRE FIGHTERS RESPONDED AND FOUND NO EVIDENCE OF FIRE. MAINTENANCE INSPECTED THE NR 1 ENGINE AND FOUND METAL IN THE TAILPIPE, ENGINE WILL BE REPLACED. MX R & R NR 1 ENGINE IAW T/C R5M71302, ENGINE RUN OPERATIONAL CHECK WAS GOOD. TEAR DOWN REPORTS CONFIRMS REASON FOR REMOVAL. MTU ATTRIBUTES THE COMPRESSOR STALL TO A STAGE 4 BLADE TEARING OFF.

Part: CONTROL UNIT — FAULTY (BRAKE/STEERING) · airframe 48,499 hrs · 22,015 cycles

ON LANDING, RECEIVED ECAM MESSAGE "BRAKING/STEERING CONTROL UNIT (BSCU) FAULT CH. 2 INCHES, WHEN CLEARING RUNWAY BRAKES LOCKED UP MOMENTARILY. MAINTENANCE REMOVED AND REPLACED THE BSCU IAW AMM 32-42-34-04, OPERATIONAL CHECK WAS GOOD. COULD NOT DUPLICATE REASON FOR REMOVAL, UNIT WAS TESTED PER CMM 32-47-27, REV. 11 WITH NO FAULTS FOUND.

Part: SLIDE — FAULTY (L-2 DOOR) · airframe 47,937 hrs · 21,767 cycles

PHX - EEL / EES - FLT 0005 - DURING FLIGHT, EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 13, 17, 19, AND 24 ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR SLIDE ASSEMBLY IAW T/C R1C25304, OPERATIONAL CHECK OF EMERGENCY LIGHTING AND SLIDE WAS GOOD.

Part: EPSU — FAULTY (ZONE 242) · airframe 47,854 hrs · 21,733 cycles

LAS - EEL - DURING 8-DAY CHECK EMERGENCY EXIT LIGHT TEST FAULTED FOR RT EXTERNAL. MAINTENANCE REMOVED AND REPLACED RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — DISCHARGED (ZONE 241) · airframe 47,808 hrs · 21,711 cycles

SAL - EEL - DURING C-04 CHECK THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 13 LT, 17 LT, 19 LT, 24 LT AND 26 LT DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK A 2 X 7 INCH AREA OF DELAMINATION WAS FOUND ON FLOOR PANEL 222CF. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 222CF IAW A320 SRM 53-02-00 FIG 209.

Part: WEB — CRACKED (FUSELAGE) · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK A 2 INCH CRACK WAS FOUND IN WEB TRAY LT SIDE OF FUSELAGE BETWEEN FR 68 AND FR 69, WL Z240. MAINTENANCE REMOVED CRACKED WEB TRAY ON LT SIDE FROM FR 68 TO FR 69. FABRICATED A NEW REPLACEMENT TRAY; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT OUTBOARD SEAT TRACK BETWEEN FR 44 AND FR 45. MAINTENANCE REMOVED CORRODED LT OUTBOARD SEAT TRACK FROM FR 44 TO FR 45; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

DURING C-04 CHECK, CORROSION WAS FOUND ON RT OUTBOARD SEAT TRACK BETWEEN FS 44 AND FS 45. MAINTENANCE REMOVED CORRODED RT OUTBOARD SEAT TRACK FROM FS 44 TO FS 45; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT OUTBOARD SEAT TRACK BETWEEN FR 42 AND FR 43. MAINTENANCE REMOVED CORRODED LT OUTBOARD SEAT TRACK FROM FR 42 TO FR 43; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

DURING C-04 CHECK, CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BETWEEN FS 38 AND FS 39. MAINTENANCE REMOVED CORRODED RT INBOARD SEAT TRACK FROM FS 38 TO FS 39; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND RT INBOARD SEAT TRACK BETWEEN FR 44 AND FR 45. MAINTENANCE REMOVED CORRODED RT INBOARD SEAT TRACK FROM FR 44 TO FR 45; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOORBEAM -Y48 RT AT FR 65+23 INCHES. MAINTENANCE REMOVED CORRODED FLOORBEAM -Y48 RT FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

DURING C-04 CHECK FRETTING CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BETWEEN FR 46 AND FR 47. MAINTENANCE REMOVED CORRODED RT INBOARD SEAT TRACK FROM FR 46 TO FR 47; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON LONGITUDINAL FLOORBEAM -Y765 RT BETWEEN FR 19 AND FR 20. MAINTENANCE REMOVED CORRODED LONGITUDINAL FLOORBEAM -Y765 RT FROM FR 19 TO FR 20; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 53-11-14 FIG 104.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT INBOARD SEAT TRACK BETWEEN FR 42 AND FR 43. MAINTENANCE REMOVED CORRODED LT INBOARD SEAT TRACK FROM FR 42 TO FR 43; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT OUTBOARD SEAT TRACK BETWEEN FR 38 AND FR 39. MAINTENANCE REMOVED CORRODED LT OUTBOARD SEAT TRACK FROM FR 38 TO FR 39; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND LT OUTBOARD SEAT TRACK BETWEEN FR 46 AND FR 47. MAINTENANCE REMOVED CORRODED LT OUTBOARD SEAT TRACK FROM FR 46 TO FR 47; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT INBOARD SEAT TRACK BETWEEN FR 35 AND FR 36. MAINTENANCE REMOVED CORRODED LT INBOARD SEAT TRACK FROM FR 35 TO FR 36; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

DURING C-04 CHECK, CORROSION WAS FOUND ON RT OUTBOARD SEAT TRACK BETWEEN FS 42 AND FS 43. MAINTENANCE REMOVED CORRODED RT OUTBOARD SEAT TRACK FROM FS 42 TO FS 43; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT OUTBOARD SEAT TRACK BETWEEN FR 43 AND FR 44. MAINTENANCE REMOVED CORRODED LT OUTBOARD SEAT TRACK FROM FR 43 TO FR 44; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

DURING C-04 CHECK, CORROSION WAS FOUND ON RT OUTBOARD SEAT TRACK BETWEEN FS 45 AND FS 46. MAINTENANCE REMOVED CORRODED RT OUTBOARD SEAT TRACK FROM FS 45 TO FS 46; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

DURING C-04 CHECK, CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BETWEEN FS 39 AND FS 40. MAINTENANCE REMOVED CORRODED RT INBOARD SEAT TRACK FROM FS 39 TO FS 40; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

DURING C-04 CHECK, CORROSION WAS FOUND ON RT OUTBOARD SEAT TRACK BETWEEN FS 42 AND FS 43. MAINTENANCE REMOVED CORRODED RT OUTBOARD SEAT TRACK FROM FS 42 TO FS 43; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT INBOARD SEAT TRACK BETWEEN FR 44 AND FR 45. MAINTENANCE REMOVED CORRODED LT INBOARD SEAT TRACK FROM FR 44 TO FR 45; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR PANEL PLATE AT FR 66, -Y60 RT. MAINTENANCE REMOVED CORRODED PANEL PLATE AT FR 66, -Y60 RT; FABRICATED A NEW REPLACEMENT PANEL PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT OUTBOARD SEAT TRACK BETWEEN FR 45 AND FR 46. MAINTENANCE REMOVED CORRODED LT OUTBOARD SEAT TRACK FROM FR 45 TO FR 46; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

DURING C-04 CHECK, FRETTING CORROSION WAS FOUND ON RT OUTBOARD SEAT TRACK BETWEEN FS 46 AND FS 47. MAINTENANCE REMOVED CORRODED RT OUTBOARD SEAT TRACK FROM FS 43 TO FS 44; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

DURING C-04 CHECK, CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BETWEEN FS 43 AND FS 44. MAINTENANCE REMOVED CORRODED RT INBOARD SEAT TRACK FROM FS 43 TO FS 44; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT INBOARD SEAT TRACK BETWEEN FR 43 AND FR 44. MAINTENANCE REMOVED CORRODED LT INBOARD SEAT TRACK FROM FR 43 TO FR 44; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

DURING C-04 CHECK, CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BETWEEN FS 35 AND FS 36. MAINTENANCE REMOVED CORRODED RT INBOARD SEAT TRACK FROM FS 35 TO FS 36; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

DURING C-04 CHECK, CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BETWEEN FS 41 AND FS 42. MAINTENANCE REMOVED CORRODED RT INBOARD SEAT TRACK FROM FS 41 TO FS 42; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: FLOOR SUPPORT — WORN (FUSELAGE) · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK LONGITUDINAL FLOORBEAM (FLOOR SUPPORT) Y254 LT WAS FOUND WITH WORN HOLES BETWEEN FR 12 AND FR 14. MAINTENANCE REMOVED WORN FLOOR SUPPORT Y254 LT FROM FR 12 TO FR 14. FABRICATED A NEW REPLACEMENT SECTION OF FLOOR SUPPORT AND 4 EACH ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14 FIG 202.

Part: FLOOR PANEL — CORRODED (PAX CABIN) · corrosion level 2

DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON PASSENGER CABIN FLOOR PANEL 222FF. MAINTENANCE BLENDED OUT CORROSION ON PASSENGER CABIN FLOOR PANEL 222FF; FABRICATED A DOUBLER; INSTALLED REPAIR PART IAW ER 26-5312-00151-BA1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOORBEAM Y38 LT AT FR 66+6 INCH. MAINTENANCE REMOVED CORRODED FLOORBEAM Y38 LT FROM FR 65 TO FR 67; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON FLOORBEAM Y20 LT AT FR 66+6 INCHES. MAINTENANCE REMOVED CORRODED FLOORBEAM Y20 LT AT FR 66+6 INCHES; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 53-00-14 FIG 207.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON GIRT BAR FLOOR PLATE AT R-2 DOOR ENTRY WAY FR 68. MAINTENANCE REMOVED CORRODED GIRT BAR FLOOR PLATE AT FR 68; INSTALLED NEW REPLACEMENT FLOOR PLATE IAW T/C C1D25310.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON LONGITUDINAL FLOOR SUPPORT WEB Y1584 LT BETWEEN FR 20 AND FR 21. MAINTENANCE REMOVED CORRODED LONGITUDINAL FLOOR SUPPORT WEB Y1584 LT FROM FR 20 TO FR 21; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 7.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM -Y48 RT AT FR 68. MAINTENANCE REMOVED CORRODED FLOORBEAM -Y48 RT AT FR 68; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOORBEAM -Y48 RT AT FR 67+11 INCHES. MAINTENANCE REMOVED CORRODED FLOORBEAM -Y48 RT AT FR 67+11 INCHES; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOORBEAM -Y48 RT AT FR 66. MAINTENANCE REMOVED CORRODED FLOORBEAM -Y48 RT FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON STRINGER 39 LT IN FORWARD CARGO COMPARTMENT AT FR 34. MAINTENANCE CUT OUT DAMAGED AREA OF STRINGER 39 LT AT FR 34; FABRICATED A COUPLING; INSTALLED REPAIR PART IAW A320 SRM 53-00-13 FIG 201.

Part: BEAM — CORRODED (CARGO DOOR SILL) · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND AT FASTENER HOLES ON LOWER SILL BEAM OF BULK CARGO DOOR BETWEEN FR 60 AND FR 62, STR 38 RT. MAINTENANCE CUT OUT DAMAGE IN SILL BEAM FROM FR 60 TO FR 62, STR 38 RT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-49, FIG 203.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON SKIN IN FORWARD CARGO COMPARTMENT BETWEEN STR 39 LT AND STR 42 LT, FS 33 AND FS 34. MAINTENANCE CUTOUT DAMAGE IN SKIN BETWEEN STR 39 LT AND STR 42 LT, FS 33 AND FS 34; FABRICATED A DOUBLER; INSTALLED REPAIR PART IAW A320 SRM 53-00-11, FIG 220.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,808 hrs · 21,711 cycles

SAL - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON STRINGER 41 LT IN FORWARD CARGO COMPARTMENT BETWEEN FR 33 AND FR 34. MAINTENANCE REMOVED CORROSION ON STRINGER 41 LT BETWEEN FR 33 AND FR 34. FABRICATED A REPAIR ANGLE AND SHIMS, AND INSTALLED REPAIR PARTS IAW A320 SRM 53-21-34 FIG 202.

Part: CONTROL UNIT — MALFUNCTIONED (ZONE 120) · airframe 46,335 hrs · 21,077 cycles

PHL - DIVERSION - FLT 0419 - DURING CLIMBOUT FROM BDL EN ROUTE FOR PHX RECEIVED CLASS 1 ECAM MESSAGE FOR FORWARD AND AFT CARGO SMOKE FOLLOWED BY FORWARD & AFT SMOKE DETECTOR FAULTS, ALSO RECEIVED LAVATORY SMOKE DETECTOR FAULT, DIVERTED TO PHL. MAINTENANCE REMOVED AND REPLACED SMOKE DETECTOR CONTROL UNIT (10WQ) IAW AMM 26-17-34-04, OPERATIONAL CHECK WAS GOOD. FUNCTIONAL TEST OF SMOKE DETECTOR CONTROL UNIT COULD NOT DUPLICATE REASON FOR REMOVAL. UNIT WAS TESTED IAW CMM 26-17-34 AND RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (ZONE 900 - LAVAT) · airframe 46,066 hrs · 20,963 cycles

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

Part: WIRE — BROKEN (SEAT ROW 3 LT) · airframe 44,920 hrs · 20,497 cycles

DURING 4-DAY CHECK 2 EACH EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROW 3 LT WERE FOUND INOPERATIVE. MAINTENANCE DISCOVERED A BROKEN WIRE STRAND GOING TO THE LIGHT HOUSING AT SEAT ROW 3 LT, REPAIRED BROKEN WIRE, OPERATIONAL CHECK WAS GOOD.

Part: PROFILE — CRACKED (ZONE 480) · airframe 43,527 hrs · 11,924 cycles

DURING C-03 CHECK A .5 INCH CRACK WAS FOUND ON INBOARD UPPER ANGLE (PROFILE) AT ATTACH SCREW HOLE JUST AFT OF RIB 7 ON THE NR 2 PYLON. MAINTENANCE CUT OUT CRACKED AREA OF ANGLE JUST AFT OF RIB 7 ON THE NR 2 PYLON; FABRICATED A REPAIR SPLICE AND FILLER; INSTALLED REPAIR PART IAW A320 SRM 54-52-12 PG 215-217, & 220, FIG 203.

Part: ATTACH ANGLE — CRACKED (LT PYLON) · airframe 43,527 hrs · 19,924 cycles

DURING C-03 CHECK A .5 INCH CRACK WAS FOUND ON LT PYLON PANEL ATTACH ANGLE AT INBOARD SIDE, AFT OF RIB 7. MAINTENANCE CUT OUT DAMAGE ON LT PYLON PANEL ATTACH ANGLE AT INBOARD SIDE, AFT OF RIB 7; FABRICATED A FILLER AND SPLICE; INSTALLED REPAIR PARTS IAW A320 SRM 54-52-12, PG 216-218.

Part: ATTACH ANGLE — CRACKED (ZONE 480) · airframe 43,527 hrs · 11,924 cycles

MCN - MAJOR REPAIR - DURING C-03 CHECK A .5 INCH CRACK WAS FOUND ON RT PYLON UPPER ATTACH ANGLE AT SCREW HOLE FORWARD OF RIB 8. MAINTENANCE CUT OUT DAMAGE ON RT PYLON ATTACH ANGLE FORWARD OF RIB 8; FABRICATED A FILLER AND SPLICE; INSTALLED REPAIR PARTS IAW A320 SRM 54-52-12 PG 215-220 FIG 2.

Part: RIB — CRACKED (NR 1 PYLON) · airframe 43,527 hrs · 19,924 cycles

DURING C-03 CHECK A .125 INCH CRACK WAS FOUND ON NR 1 PYLON RIB, 4TH LOWER RIB FROM UPPER DRAIN LINE CLEARANCE HOLE, OUTBOARD EDGE IN AFT FIXED FAIRING. MAINTENANCE REMOVED CRACKED RIB; FABRICATED A NEW REPLACEMENT RIB; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 8-12 & 21-22, FIG 2, 3 & 8.

Part: PANEL — DELAMINATED (FAIRING) · airframe 43,527 hrs · 11,924 cycles

DURING C-03 CHECK THE LOWER CENTER BELLY FAIRING (191BB) WAS FOUND DELAMINATED ALONG THE FORWARD LOWER EDGE AT THE RT AFT OUTBOARD CORNER, FR 34. MAINTENANCE REMOVED AND REPLACED THE LOWER CENTER BELLY FAIRING (191BB) IAW A320 AMM SUBTASK 53-35-13-020-052-AO & 53-35-13-420-051-AO.

Part: ACTUATOR — LOOSE (VARI STATOR VANE) · airframe 43,417 hrs · 19,877 cycles

TEARDOWN REPORT OF ENG IDENTIFIED HIGH INTERNAL LEAKAGE AT VSV ACT ALONG WITH SLOW PISTON VELOCITY. TEARDOWN REVEALED THAT CONTROL SERVO VALVE & SEAL WERE WORN BEYOND LIMITS & CAUSED INTERNAL LEAKAGE AT VSV ACT. FAILURE MODE & EFFECTS ANALYSIS CONSIDER THIS A MAJOR FAILURE & WOULD RESULT IN CSV TO M

Part: BATTERY — DISCHARGED (ZONES 220, 260) · airframe 42,142 hrs · 19,382 cycles

LAX - EMERGENCY EQUIPMENT - DURING ROUTINE MX INSPECTION MAINTENANCE DISCOVERED THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT DISCHARGED/INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE FORWARD FLIGHT ATTENDANT POSITION, OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — DISCHARGED (ZONE 241) · airframe 41,428 hrs · 19,111 cycles

SEA - EEL - DURING INSPECTION, THE EMERGENCY ESCAPE LIGHT SYSTEM TEST FAILED AT PROGRAMMING AND TEST PANEL. MAINTENANCE REMOVED AND REPLACED THE LT OVER WING EMERGENCY POWER SUPPLY UNIT (11WL); OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — DISCHARGED (ZONE 263) · airframe 41,297 hrs · 19,063 cycles

DURING INSPECTION THE EMERGENCY LIGHT SYSTEM FAILED TEST. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL TEST WAS GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 40,795 hrs · 18,865 cycles

PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THAT THE EMERGENCY FLASHLIGHT AT THE AFT FLIGHT ATTENDANT SEAT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT AT THE AFT FLIGHT ATTENDANT SEAT.

Part: BALLAST — DEFECTIVE (SEAT ROW 17 L/H) · corrosion level 0 · airframe 40,708 hrs · 18,836 cycles

PHX - BURNING SMELL - FLT 0534 - EN ROUTE FROM SAN TO PHX AN ACRID BURNING SMELL WAS NOTICED IN PROXIMITY OF SEAT ROW 17 L/H. MAINTENANCE FOUND CEILING LIGHT BALLAST BAD ABOVE SEAT ROW 17 L/H, REPLACED CEILING LIGHT BALLAST ASSEMBLY IAW AMM 33-21-09, OPERATIONAL CHECK WAS GOOD.

Part: WIRE — BROKEN (SEAT ROW 2) · airframe 40,154 hrs · 18,620 cycles

FLT 0683 - EMERGENCY AISLE LIGHTS INOPERATIVE SEAT ROWS 1 & 2. MAINTENANCE REPAIRED BROKEN WIRE UNDER SEAT ROW 2, OPERATIONAL CHECK GOOD.

Part: DAMPENER — LEAKING (L1 DOOR) · airframe 38,954 hrs · 18,153 cycles

YWG - DOOR SYSTEM - C - DURING C-02 CHECK DOOR ASSIST CYLINDER FOR THE L1 DOOR WAS FOUND TO HAVE NO DAMPENING ACTION. MAINTENANCE REMOVED, REPLACED, AND RIGGED THE L1 DOOR DAMPER ASSIST CYLINDER IAW AMM 52-11-14-052, OPERATIONAL CHECK WAS GOOD.

Part: DAMPENER — LEAKING (R2 DOOR) · airframe 38,954 hrs · 18,153 cycles

YWG - DOOR SYSTEM - C - DURING C-02 CHECK DOOR ASSIST CYLINDER FOR THE R2 DOOR WAS FOUND TO HAVE NO DAMPENING ACTION. MAINTENANCE REMOVED, REPLACED, AND RIGGED THE R2 DOOR DAMPER ASSIST CYLINDER IAW AMM 52-11-14-052, OPERATIONAL CHECK WAS GOOD.

Part: DAMPENER — LEAKING (L2 DOOR) · airframe 38,954 hrs · 18,153 cycles

YWG - DOOR SYSTEM - C - DURING C-02 CHECK DOOR ASSIST CYLINDER FOR THE L2 DOOR WAS FOUND TO HAVE NO DAMPENING ACTION. MAINTENANCE REMOVED, REPLACED AND RIGGED THE L2 DOOR DAMPER ASSIST CYLINDER IAW AMM 52-11-14-052, OPERATIONAL CHECK WAS GOOD.

Part: FITTING — WORN (STA 35306 FR 74) · airframe 38,954 hrs · 18,153 cycles

YWG - MAJOR REPAIR - "C" - DURING C-02 INSPECTION CENTER JOINT FITTINGS FOR THE TRIMMABLE HORIZONTAL STABILIZER ACTUATOR WERE FOUND WORN BEYOND DRAWING LIMITATIONS. L/H DIMENSIONS RANGE FROM 2.4746' TO 2.4751", R/H SIDE DIMENSIONS RANGE FROM 2.6007" TO 2.6009". MAINTENANCE REMOVED AND REWORKED CENTER JOINT FITTING FIXED BEARING AND SLIDING BEARING PER AWA ER 26-5511-02060-ES2.

Part: WEB — CRACKED (FUSELAGE) · airframe 38,735 hrs · 17,974 cycles

YWG - MAJOR REPAIR - C - DURING C-02 CHECK A CRACK WAS FOUND ON LT OUTBOARD WEB BELOW THE AFT GALLEY, FR 68-69.

Part: PRESSURE SWITCH — FAILED (HYD PUMP) · airframe 33,777 hrs · 16,011 cycles

DECLARED EMERGENCY, ON SHORT FINAL ECAM MESSAGE DISPLAYED GREEN HYD ENG PUMP LOW PRESSURE. T/S GREEN HYDRAULIC SYS, FOUND LOW PRESSURE SWITCH AT FAULT. REMOVED AND REPLACED EDP LOW PRESS SWITCH AND SECURED LOOSE CANNON PLUG.

Part: PRESSURE SWITCH — FAILED (HYD PUMP) · airframe 33,626 hrs · 15,958 cycles

AIR TURNBACK, EMERGENCY DECLARED. LOST NR 1 AND NR 2 HYD PUMP ON DOWNWIND WHEN FLAPS WERE SELECTED (AC WENT TO DIRECT LAW). REMOVED AND REPLACED NR 1 AND NR 2 ENGINE PUMP PRESSURE SWITCHES IAW MM 29-32-12, OPS CHECK GOOD.

Part: BRACKET — WORN (MLG)

EMERGENCY LANDING - LGCIU 1AND 2 FAULTED. RESET CIRCUIT BREAKERS, NO HELP. MANUALLY EXTENDED GEAR MLG FOR LANDING. REMOVED AND REPLACED WORN TARGET SUPPORT PER AMM 32-21-27-991.

Part: POWER SUPPLY — INOP (CABIN)

OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY AND OPS GOOD.

Part: SKIN — CORRODED (L2 DOORWAY)

FEW SPOTS CORROSION AFT OF L2 DOOR AREA NR 5066917 CORROSION REMOVAL BEYOND LIMITS. FABRICATED ANGLE DOUBLER AS PER ER 32-53-17-05.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHT OVER LEFT OVERWING EXIT REPORTED OUT OR INTERMITTEN. RESET SYSTEM, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS ON LT AND RT OVERWING MARKER LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK ON RT OVERWING PANEL ASSEMBLY, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT LENS AT ROW 7L BROKEN. EMERGENCY LIGHTS AT ROW 3L AND 11L INOP. REMOVED AND REPLACED LIGHT UNIT. REMOVED AND REPLACED BATTERY PACK AT ROW 11L AND ROW 11R.

Part: NAV DISPLAY — INOPERATIVE (NR 1)

CAPTAIN'S NAV DISPLAY WENT BLANK ON BOTTOM OF SCREEN AND SQUIGGLES ON TOP HALF. SMELLED HOT, TURNED OFF FOR DURATION OF FLIGHT. REMOVED AND REPLACED NR 1 NAV DISPLAY PER MM 31-63-22, OPS NORMAL.

Part: AIR RELEASE VLV — INOPERATIVE (RT WING)

AFTER TAKEOFF, TOWER REPORTED FUEL VENTING FROM RIGHT WING. WHILE INVESTIGATING PROBLEM, APPROXIMATELY 2,900 LBS OF CENTER TANK FUEL DISAPPEARED WITHIN 8 MINUTES. FOUND AIR RELEASE VALVE BAD IN RIGHT WING. REMOVED AND REPLACED AIR RELEASE VALVE PER MM 28-21-41, OPS CHECK GOOD.

Part: FLT AUG COMPUTER — INOPERATIVE (NR 1)

RUDDER TRAVEL LIMIT CLASS 1 WARNING IN FLIGHT, BOTH 1 AND 2. UNABLE TO CLEAR BY TURNING FACS 1 AND 2 OFF AND ON. REPLACED NR 1 FAC, TEST NORMAL.

Part: PACK — MALFUNCTIONED (NR 2)

NUMBER 2 PACK OVERHEAT, CABIN FILLED WITH BURNING SMELL. SMELL WENT AWAY AS TEMPERATURE DECREASED. RAN NR 2 PACK FOR 10 MINUTES AT DIFFERENT SETTINGS WITHOUT FAULT.

Part: FUSE — MISSING (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND BOTH RIGHT EMERGENCY OVERWING EXIT HANDLE COVER LIGHTS INOP. FOUND MISSING FUSE ON BATTERY PACK AND INSTALLED NEW ONE. OPS CHECK GOOD.

Part: PACK INLET ACT — INOPERATIVE (NR 2 PACK)

STRONG SMELL OF SMOKE IN CABIN ASSOCIATED WITH NR 2 PACK FAILURE. REMOVED AND REPLACED NR 2 PACK INLET ACTUATOR PER AMM, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

PHX - FLT 2050 - AFT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK ABOVE L-2 DOOR. OPERATIONS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

PHX - FLT 146 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS AT ROWS 13, 17, 19, 24, AFT GALLEY AREA AND L-2 AND R-2 DOORS FAILED EMERGENCY BATTERY TEST. REMOVED AND REPLACED BATTERY PACK. REMOVED AND REPLACED BATTERY CHARGER. OPERATIONS CHECKED GOOD. (M)

Part: BATTERY CHARGER — INOP (CABIN)

PHX - FLT 146 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS AT ROWS 13, 17, 19, 24, AFT GALLEY AREA AND L-2 AND R-2 DOORS FAILED BATTERY TEST. REMOVED AND REPLACED BATTERY PACK. REMOVED AND REPLACED BATTERY CHARGER. OPERATIONS CHECK GOOD. REFERENCE AWXA960558.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

PHX - FLT 2051 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INOP AT SEATS 13, 17, 19 AND 24. BULLNOSE LIGHTS INOP AT ROW 19 AND 2. ALL SIGNS INOP IN AFT GALLEY. SYSTEM TEST FAILS LEFT AFT UNIT. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT. (M)

Part: SLIDE — MALFUNCTIONED (R-2 DOOR)

LAX/PHX - FLT 2274 - R-2 DOOR SLIDE INADVERTENTLY DEPLOYED, BUT DID NOT INFLATE IN LAX. INSTALLED R-2 DOOR SLIDE PER CARD R1C25304. PART TOTAL CYCLES, 7,527. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

LAS - FLT 2609 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP OVERWING. REPLACED BATTERY PACK OVERWING LEFT SIDE IAW, AMM 33-51-38, TEST OK. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

LAS - FLT 2609 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE, OVERWING. REPLACED BATTERY PACK OVERWING, LEFT SIDE. TEST OK. (X)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DTW - FLT 0058 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTING ROW 9 AND ROW 11 A/C LEFT, INOPERATIVE. SWAPPED EMERGENCY LIGHT OVER-WING EXIT DOOR POWER SUPPLIES PER 33-51-38. REMOVED POWER FROM A/C. POWER UP A/C EMERGENCY LIGHT SYSTEM, OPERATIONS CHECK GOOD. LEFT S/N - 433. RIGHT S/N - 1551. (X)

Part: SEAT TRACK — CORRODED (BS 1292)

PAE - FLT 7809 - DURING ROUTINE SCHEDULED C-5 MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK -1292, Z-540, FR 20. REMOVED AND REPLACED SEAT TRACK AT Y-1292, Z-540, FR 20 TO FR 24 PER SRM 51-72-11 AND 51-42-21. (M)

Part: RAIL — CORRODED (BS 1292)

PAE - FLT 7809 - DURING ROUTINE SCHEDULED C-5 MAINTENANCE CHECK, FOUND CORROSION ON DUMMY RAIL -1292, FR 20 THROUGH FR 16, Z-540. REPAIRED DUMMY RAIL IAW SRM 53-11-41. (M)

Part: RAIL — CORRODED (BS 1292)

PAE - FLT 7809 - DURING ROUTINE SCHEDULED C-5 MAINTENANCE CHECK, FOUND CORROSION ON DUMMY RAIL AT Y 1292, FR 20 THROUGH FR 18, Z-540. REMOVED AND REPLACED DUMMY RAIL FR 16 THROUGH FR 20, Y 1292, Z -540, IAW SRM 51-72-11, SRM 53-11-14. (M)

Part: BEAM — CORRODED (BS 1800)

DURING ROUTINE SCHEDULED C-5 MAINTENANCE CHECK, FOUND CORROSION ON THRESHOLD SUPPORT BEAM FR 68, Y 1800, LEFT Z -540 'MARKED'. BLENDED CORROSION 2 INCH BY 1 INCH BY .035 INCH ORIGINAL THICKNESS OF .071 FOUND OUT OF LIMITS PER MM 53-00-14. FABRICATED REPAIR AND INSTALLED PER SRM 53-00-14. (M)

Part: RAIL — CORRODED (BS 254)

PAE - FLT 7809 - DURING ROUTINE SCHEDULED C-5 MAINTENANCE CHECK, FOUND CORROSION ON DUMMY RAIL Y=254, FR 21 THROUGH FR 16, Z -540. REMOVED, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-11-14. (M)

Part: RAIL — CORRODED (BS 254)

PAE - FLT 7809 - DURING ROUTINE SCHEDULED C-5 MAINTENANCE CHECK, FOUND CORROSION ON DUMMY RAIL Y=-254, FR 20 THOUGH FR 16. REMOVED, FABRICATED AND INSTALLED REPAIR PER SRM 53-11-14. (M)

Part: ELAC — FAILED (NR 1)

PHX - FLT 845 - ABORTED TAKEOFF, ELAC PITCH TRIM FAULT. REMOVED AND REPLACED ELEVATOR AILERON COMPUTER. (M)

Part: COMPUTER — FAILED (E/E BAY)

PHX/CMH - FLT NR 266 - ABORTED TAKEOFF, AVIONICS SKIN VALVE FAULT ON TAKEOFF ROLL. REMOVED AND REPLACED AVIONICS VENT COMPUTER. (M)

Part: HANDLE — OUT OF ADJUST (CARGO DOOR)

FLT NR 657 - SNA - ABORTED TAKEOFF, AFT CARGO DOOR ECAM WARNING. FOUND CARGO DOOR HANDLE BEING PUSHED OUT OF PROX SWITCH RANGE, PERFORMED PER 32-52-30-06. HANDLE NOW CLOSES NORMALLY WITH NO INTERFERENCE AND INDICATION IS NORMAL. (M)

Part: VALVE — LEAKING (PARKING BRAKE)

EN ROUTE FROM DFW TO PHX, ECAM INDICATED YELLOW SYSTEM HYDRAULIC QUANTITY LOW. CREW SHUT YELLOW SYSTEM DOWN AND CONTINUED TO PHX, LANDING UNEVENTFULLY. MAINTENANCE FOUND PARKING BRAKE VALVE LEAKING. MAINTENANCE REMOVED AND REPLACED VALVE. OPS CHECKED PER AMM 32-43-00. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LOCK PIN — LOOSE (NR 1 ENGINE)

PHX-YVR - FLT NR 815 - AIR TURNBACK DUE TO NR 1 ENGINE BLEED FAULT. BLEED WENT TO OVERHEAT CONDITION TWO MINUTES AFTER SELECTED ON. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND SAFETY WIRE BROKEN AND LOCK PIN BACKED OUT OF FAN AIR VALVE. REINSTALLED PIN AND SAFETIED. RAN ENGINE, TEMPERATURE 185 DEGREES CELSIUS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: EEL BATT PACK — DISCHARGED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, LT MID OVERWING EMERGENCY EXIT LIGHT BATTERY PACK FAULTED. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (Z)

Part: RUDDER PEDALS — STIFF (RT COCKPIT)

ORD - FLT 701 - AFTER A/P DISCONNECT AT 1000 FEET ON DESCENT, THE FO'S RUDDER PEDAL INPUT REQUIRED EXCESSIVE FORCE. NO RUDDER PEDAL INPUT DEFECTS FROM CAPT'S SIDE. ACFT LANDED WITHOUT INCIDENT. MX COMPLIED WITH ER 32 27 21 02, INSTALLATION OF NEW LEVER IN THE RUDDER ARTIFICIAL FEEL AND TRIM UNIT. OPS CHECK OK. ACFT RETURNED TO SERVICE. (W)

Part: KEY WASHER — BROKEN TAB (NLG DOOR ACT)

PHX - DURING FLEET INSPECTION DUE TO OTHER FAILURES NOTED, FOUND KEY WASHER TANGS PROPERLY SECURED, BUT KEY PORTION OF LOCK WASHER DEFECTIVE ALLOWING ROTATION OF NUT ON NOSE LANDING GEAR DOOR ACTUATOR LOWER ATTACHMENT FITTING BOLT. THE KEY PORTION OF THE LOCK WASHER IS NOT VISIBLE WITHOUT REMOVING THE NUT. REMOVED AND REPLACED LOCK WASHER PER AMM 32 32 16 PP 404 407. AIRCRAFT RETURNED TO SERVICE. (X)