N628AW

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 73,719 hrs · 33,035 cycles

EMERGENCY LIGHTS DO NOT TEST CORRECTLY L1 & R1 DOOR. REMOVED AND REPLACED POWER SUPPLY 10WL PER 33-51-38-000-001. SYSTEM OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 73,719 hrs · 33,035 cycles

EMERGENCY LIGHTS DO NOT TEST CORRECTLY L1 AND R1 DOOR. REMOVED AND REPLACED POWER SUPPLY PER AMM 33-51-38 - OPS CHECKED GOOD.

Part: SIGN — CRACKED (CABIN) · airframe 73,228 hrs · 32,793 cycles

THE 2L EXIT SIGN CRACKED. REMOVED & REPLACED 2L EXIT SIGN.

Part: LENS — DETACHED (CABIN) · airframe 72,989 hrs · 32,685 cycles

EXIT PATH LIGHTING LENS COVER OFF LEFT SIDE LAST ROW. REPLACED EMERGENCY LIGHT LENS ROW 26 LEFT.

Part: LENS — MISSING (CABIN) · airframe 72,976 hrs · 32,679 cycles

EMERGENCY LIGHT LENS MISSING NEAR ROW 25ABC FLOORING. INSTALLED LENS AT ROW 25ABC.

Part: WIRE — BROKEN (COCKPIT) · airframe 72,351 hrs · 32,361 cycles

BC1 CHECK - FORWARD LEFT WINDSCREEN EMERGENCY LIGHT WIRES BROKEN. REPAIRED FORWARD LEFT WINDSCREEN EMERGENCY LIGHT WIRES IAW A320 ESPM 20-48-25. OPS CHECK GOOD IAW A320 AMM 33-51-00-710-001A.

Part: WIRE — BROKEN (CABIN) · airframe 72,351 hrs · 32,361 cycles

BC1 CHECK - NR 1 LEFT AND NR 3 LEFT EMERGENCY LIGHT WIRES BROKEN. REPAIRED NR 1 LEFT AND NR 3 LEFT EMERGENCY LIGHT WIRES IAW A320 AMM 33-51-19-0401 AND AIRBUS ESPM 20-43-13. OPS CHECK GOOD IAW A320 AMM 33-51-00-710-001A.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 72,351 hrs · 32,361 cycles

BC1 CHECK - WATER INGRESS ON UPPER SURFACE OF LEFT ELEVATOR AT ZONE 1 AND ZONE 3. REPAIRED UPPER SURFACE OF LEFT ELEVATOR AT ZONE 1 AND ZONE 3 IAW A320 SRM 55-21-11 AND 55-20-00.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 72,351 hrs · 32,361 cycles

BC1 CHECK - WATER INGRESS ON UPPER SURFACE OF RIGHT ELEVATOR AT ZONE 1 AND ZONE 5. REPAIRED UPPER SURFACE OF RIGHT ELEVATOR AT ZONE 1 AND ZONE 5 IAW A320 SRM 55-21-11, PARAGRAPH D & E.

Part: BRACKET — BROKEN (SLIDE COVER) · airframe 71,419 hrs · 31,901 cycles

SLIDE BUSTLE DOOR 2R NEEDS TO BE REFITTED. FOUND LATCHING BRACKET BROKEN. REPAIRED SLIDE COVER DOOR R2 IAW STRUCTURAL REPAIR MANUAL 51-42-11.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 71,349 hrs · 31,868 cycles

AFT FLIGHT ATTENDANT SWIVEL SEAT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY AFT SWIVEL JUMPSEAT. OPS CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 71,185 hrs · 31,796 cycles

LENS MISSING FROM EMERGENCY SEAT MOUNTED LIGHT ROW 11L. INSTALLED LENS ON SEAT MOUNTED EMERGENCY LIGHT ROW 11L.

Part: LIGHT — BROKEN (CABIN) · airframe 71,042 hrs · 31,730 cycles

SMALL EMERGENCY LIGHT AT EDGE OF FORWARD BULKHEAD BROKEN. REPLACED FORWARD WINDSCREEN EMERGENCY LIGHT ASSEMBLY.

Part: TRANSDUCER — FAILED (NR 1 ENGINE) · airframe 70,846 hrs · 31,645 cycles

AFTER TAKEOFF PRIOR TO 1000', ENGINE NR 1 SURGED TWICE AND SELF-RECOVERED WITH NORMAL INDICATIONS. ON LANDING ROLLOUT, RECEIVED ECAM MESSAGES FOR ENG 1 COMPRESSOR VANE AND FADEC MX. TWO SUBSEQUENT EVENTS FOR NR 1 ENGINE SURGE ON TAKEOFF ON 1/3/12 AND 1/4/12. REMOVED AND REPLACED THE VARIABLE STATOR VANE ACTUATOR. VENDOR INDICATED LVDT (LINEAR VARIABLE DIFFERENTIAL TRANSDUCER) FAILED ON INCOMING TEST. REPAIRED AS REQUIRED.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 70,127 hrs · 31,321 cycles

RIGHT SIDE OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND RE-INSTALLED BAYONET CONNECTOR - OPERATIONAL CHECK NORMAL IAW AIRBUS MAINTENANCE MANUAL 33-51-16.

Part: SPRING — BROKEN (GIRT BAR) · airframe 70,092 hrs · 31,306 cycles

CABIN DOOR 2L ARMED INDICATION INTERMITTENT. MAINTENANCE REPLACED BROKEN SPRING IN AFT GIRT BAR FLOOR FITTING.

Part: WIRE — LOOSE (CABIN) · airframe 70,056 hrs · 31,288 cycles

EMERGENCY LIGHT WIRING IS HANGING LOOSE UNDER SEAT ROW 11L. MAINTENANCE SECURED LIGHT WIRING FOR SEAT 11L - OPERATIONAL CHECK NORMAL.

Part: CONTAINER — BROKEN (CABIN) · airframe 69,915 hrs · 31,220 cycles

SEAT ROW 12L PASSENGER EMERGENCY O2 PANEL WILL NOT LATCH - SEAT ROW 18R PASSENGER EMERGENCY O2 PANEL TEST BUTTON IS BROKEN. MAINTENANCE REPLACED PASSENGER EMERGENCY O2 CONTAINERS AT SEAT ROWS 12L & 18R IAW AIRBUS MAINTENANCE MANUAL 35-21-41-401.

Part: CONTROL UNIT — MALFUNCTIONED (CABIN) · airframe 69,176 hrs · 30,883 cycles

LAS - EEL - EMERGENCY EXIT LIGHT TEST FAULTS 'AFT L'. RESET 'AFT L' POWER CONTROL UNIT, OPERATIONAL CHECK GOOD.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF RIGHT LOAD TRANSMITTIG PROFILE OF THE FORWARD RIGHT EMERGENCY EXIT (843) AT CENTRAL FUSELAGE. REPLACED LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE FORWARD RIGHT EMERGENCY EXIT (843) AT CENTRAL FUSELAGE IAW EA 133172.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE LEFT AFT EMERGENCY EXIT (834) AT CENTRAL FUSELAGE. REPLACED LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE LEFT AFT EMERGENCY EXIT (834) AT CENTRAL FUSELAGE IAW EA 133172.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE FORWARD LEFT EMERGENCY EXIT (833) AT CENTRAL FUSELAGE. REPLACED LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE FORWARD RIGHT EMERGENCY EXIT (833) AT CENTRAL FUSELAGE IAW EA 133172.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF LEFT LOAD TRANSMITTING PROFILE OF THE LEFT AFT EMERGENCY EXIT (834) AT CENTER FUSELAGE. REPLACED LOWER FLANGE OF LEFT LOAD TRANSMITTING PROFILE OF THE LEFT AFT EMERGENCY EXIT (834) AT CENTER FUSELAGE IAW EA 133172.

Part: SILL — CORRODED (FUSELAGE) · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - CORROSION ON LOWER SILL AROUND GIRT BAR FITTING AT FR 66, S23L. REPAIRED LOWER SILL AROUND GIRT BAR FITTING AT FR 66, S23L IAW EA 133170.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - CRACK ON FLOORBEAM BETWEEN FR46 TO FR47, -Y254. REPAIRED FLOORBEAM BETWEEN FR46 TO FR47, -Y254 IAW EA 133198.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF LEFT LOAD TRANSMITTING PROFILE OF THE FORWARD LEFT EMERGENCY EXIT (833) AT CENTRAL FUSELAGE. REPLACED LOWER FLANGE OF LEFT LOAD TRANSMITTING PROFILE OF THE FORWARD LEFT EMERGENCY EXIT (833) AT CENTRAL FUSELAGE IAW EA 133172.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE RIGHT AFT EMERGENCY EXIT (844) AT CENTRAL FUSELAGE. REPLACED LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE RIGHT AFT EMERGENCY EXIT (844) AT CENTRAL FUSELAGE IAW EA 133172.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF LEFT LOAD TRANSMITTING PROFILE OF THE FORWARD RIGHT EMERGENCY EXIT (843) AT CENTRAL FUSELAGE. REPLACED LOWER FLANGE OF LEFT LOAD TRANSMITTING PROFILE OF THE FORWARD RIGHT EMERGENCY EXIT (843) AT CENTRAL FUSELAGE IAW EA 133172.

Part: SILL — CORRODED (FUSELAGE) · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - CORROSION ON LOWER SILL AROUND GIRT BAR FITTING AT FR 68, S23R. REPAIRED LOWER SILL AROUND GIRT BAR FITTING AT FR 68, S23R IAW EA 133170.

Part: SKIN — CORRODED (FUSELAGE) · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON INTERNAL SKIN AT FR58 + 15 INCHES BETWEEN S43R & S44R AFT CARGO COMPARTMENT. REPAIRED INTERNAL SKIN AT FR58 + 15 INCHES BETWEEN S43R & S44R IAW EA 133191.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - CRACK ON UPPER FLANGE OF FRAME 25 AT LEVEL S31L FWD C.C. REPAIRED UPPER FRAME FLANGE AT FR25, S31L IAW A320 SRM 53-00-12.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON ANGLE AT FR71 CUTOUT ACCESS DOOR 312AR BETWEEN S27R TO S30R TAIL SECTION AFT FUSELAGE. REPLACED ANGLE AT FR71 CUTOUT ACCESS DOOR 312AR BETWEEN S27R TO S30R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53571500.

Part: SLIDE RAFT — FAULTY (PAX DOOR) · airframe 67,645 hrs · 30,185 cycles

SAL - EES - S5 CHECK - PASSENGER CREW DOOR 841 SLIDE RAFT WAS OVER INFLATED. REPLACED SLIDE RAFT AT PASSENGER CREW DOOR 841 IAW TASK CARD 26C84152006.

Part: SLIDE RAFT — FAULTY (PAX DOOR) · airframe 67,645 hrs · 30,185 cycles

SAL - EES - S5 CHECK - PASSENGER CREW DOOR 842 SLIDE RAFT WAS OVER INFLATED. REPLACED SLIDE RAFT AT PASSENGER CREW DOOR 842 IAW TASK CARD 26C84252006.

Part: SLIDE RAFT — FAULTY (PAX DOOR) · airframe 67,645 hrs · 30,185 cycles

SAL - EES - S5 CHECK - PASSENGER CREW DOOR 832 SLIDE RAFT WAS OVER INFLATED. REPLACED SLIDE RAFT AT PASSENGER CREW DOOR 832 IAW TASK CARD 26C83252008.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR30 BETWEEN S39L TO S40L. REPLACED CLEAT AT FR30 BETWEEN S39L TO S40L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231212.

Part: SHEAR PIN — CORRODED (ENGINE MOUNT) · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 - CORROSION WAS FOUND BETWEEN RIB 4 AND RIB 5 ON INNER PIN, LOCATED AT LEFT UPPER FROM LINK PIN ASSY OF AFT ENGINE MOUNT (ENGINE NR 1). REPLACED INNER PIN BETWEEN RIB 4 AND RIB 5 LOCATED AT LEFT UPPER FROM LINK PIN ASSY OF AFT ENGINE MOUNT (ENGINE NR 1) IAW A320 AMM 71-22-11.

Part: SHEAR PIN — CORRODED (ENGINE MOUNT) · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 - CORROSION WAS FOUND BETWEEN RIB 4 AND RIB 5 ON INNER PIN, LOCATED AT RIGHT MIDDLE FROM LINK PIN ASSY OF AFT ENGINE MOUNT (ENGINE NR 1). REPLACED INNER PIN BETWEEN RIB 4 AND RIB 5 LOCATED AT RIGHT MIDDLE FROM LINK PIN ASSY OF AFT ENGINE MOUNT (ENGINE NR 1) IAW A320 AMM 71-22-11.

Part: STIFFENER — CRACKED (HORIZ STAB) · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - CRACKS FRONT SPAR OF LEADING EDGE OF LEFT HORIZONTAL STABILIZER INTERNAL AREA OF ACCESS PANEL 331AB. REPAIRED STIFFENER BETWEEN RIB 4 TO RIB 5 OF LEADING EDGE OF LEFT HORIZONTAL STABILIZER INTERNAL AREA IAW EA 133177 & A320 SRM 51-77-12.

Part: SHEAR PIN — CORRODED (ENGINE MOUNT) · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 - CORROSION WAS FOUND BETWEEN RIB 4 AND RIB 5 ON INNER PIN, LOCATED AT LEFT MIDDLE FROM LINK PIN ASSY OF AFT ENGINE MOUNT (ENGINE NR 1). REPLACED INNER PIN BETWEEN RIB 4 AND RIB 5 LOCATED AT LEFT MIDDLE FROM LINK PIN ASSY OF AFT ENGINE MOUNT (ENGINE NR 1) IAW A320 AMM 71-22-11.

Part: HINGE PIN — CORRODED (ENGINE MOUNT) · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON INNER HINGE PIN FOR LEFT AFT NR 1 ENGINE MOUNT AT PYLON STA 684. REPLACED LEFT AFT NR 1 ENGINE MOUNT AT PYLON STA 684 IAW A320 AMM 71-22-11.

Part: SHEAR PIN — CORRODED (ENGINE MOUNT) · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 - CORROSION WAS FOUND BETWEEN WS 3758 TO WS 4067, BETWEEN RIB 7 AND RIB 8 ON INNER PIN, LOCATED AT RIGHT LOWER FROM LINK PIN ASSY OF AFT ENGINE MOUNT (ENGINE NR 1). REPLACED INNER PIN BETWEEN WING STATION 3758 TO 4067, BETWEEN RIB 7 AND RIB 8 LOCATED AT RIGHT LOWER FROM LINK PIN ASSY OF AFT ENGINE MOUNT (ENGINE NR 1) IAW A320 AMM 71-22-11.

Part: HINGE PIN — CORRODED (ENGINE MOUNT) · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON INNER HINGE PIN FOR RIGHT AFT NR 1 ENGINE MOUNT AT PYLON STA 684. REPLACED RIGHT AFT NR 1 ENGINE MOUNT AT PYLON STA 684 IAW A320 AMM 71-22-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM AT FR 65 + 5 INCH, + Y1215. REPLACED FLOORBEAM AT FR 65 + 5 INCH, + Y1215 IAW A320 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - CORROSION FOUND AROUND NUT PLATE OF LOWER SILL RT SIDE LOCATED FR67+9 INCH. REPAIRED LOWER SILL RT SIDE LOCATED FR67+9 INCH IAW A320 SRM 53-41-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - CORROSION ON SEAT TRACK LOCATED AT FR 34 + 9 INCHES -Y1292. REPAIRED SEAT TRACK LOCATED AT FR 34 + 9 INCHES -Y1292 IAW A320 SRM 53-21-15.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - CORROSION ON RIGHT WING FUEL PANEL 640RB BETWEEN RIB 21 AND RIB 22, WS 11664 - WS 11198. REPLACED RIGHT WING FUEL PANEL 640RB BETWEEN RIB 21 AND RIB 22, WS 11664 - WS 11198 IAW A320 SRM 57-27-11.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - CORROSION ON RIGHT WING FUEL PANEL 640MB BETWEEN RIB 17 AND RIB 18, WS 9704 - WS 9235. REPLACED RIGHT WING FUEL PANEL 640MB BETWEEN RIB 17 AND RIB 18, WS 9704 - WS 9235 IAW TASK CARD 26C60057091.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - CORROSION ON SEAT TRACK LOCATED AT FR 29+6 INCHES -Y1292. REPAIRED SEAT TRACK LOCATED AT FR 29+6 INCHES -Y1292 IAW A320 SRM 53-00-15 FIG 201.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - CRACK ON SHEAR PLATE AT FR 68 - FR 69, S23R. REPLACED SHEAR PLATE AT FR 68 - FR 69, S23R IAW A320 SRM 51-72-11.

Part: FITTING — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - LEVEL 2 CORROSION ON THE NR 1 PYLON LOWER SPIGOT FITTING. REPLACED THE NR 1 PYLON LOWER SPIGOT FITTING IAW EA 133205.

Part: FITTING — CORRODED (NR 2 PYLON) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - LEVEL 2 CORROSION ON THE NR 2 PYLON LOWER SPIGOT FITTING. REPLACED THE NR 2 PYLON LOWER SPIGOT FITTING IAW EA 133205.

Part: ACCESS PANEL — DELAMINATED (VERTICAL STAB) · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - VERTICAL STABILIZER ACCESS PANEL 327AL HAS AREA OF DELAMINATION. REPAIRED VERTICAL STABILIZER ACCESS PANEL 327A IAW EA 133199.

Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION 2 INNER HINGE PINS OF NR 2 SPOILER AT WS 6132, RIB 11. REPLACED INNER HINGE PINS OF NR 2 SPOILER AT WS6132, RIB 11 IAW A320 AMM 27-64-42.

Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON 2 INNER HINGE PINS OF LEFT WING NR 5 SPOILER. REPLACED INNER HINGE PINS OF LEFT WING NR 5 SPOILER IAW A320 AMM 27-64-45.

Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON 2 INNER HINGE PINS OF RIGHT WING NR 2 SPOILER BETWEEN WS 613 TO WS 670. REPLACED INNER HINGE PINS OF RIGHT WING NR 2 SPOILER BETWEEN WS 613 TO WS 670 IAW TASK CARD 26C68327003.

Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON 2 INNER HINGE PINS OF RIGHT WING NR 1 SPOILER AT WS 3758. REPLACED INNER HINGE PINS OF RIGHT WING NR 1 SPOILER AT WS 3758 IAW A320 AMM 27-64-41.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 - LEVEL 2 EXFOLIATION CORROSION ON STRINGER BETWEEN FR12 AND FR13, STR 34L. REPLACED STRINGER BETWEEN FR12 AND FR13, STR 34L IAW A320 SRM 51-72-11.

Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON 2 INNER HINGE PINS OF RIGHT WING NR 5 SPOILER. REPLACED INNER HINGE PINS OF RIGHT WING NR 5 SPOILER IAW TASK CARD 26C68627003.

Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON 2 INNER HINGE PINS OF RIGHT WING NR 3 SPOILER BETWEEN WS 7792 TO WS 8268. REPLACED INNER HINGE PINS OF RIGHT WING NR 3 SPOILER BETWEEN WS 7792 TO WS 8268 IAW A320 AMM 27-64-43.

Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON 2 INNER HINGE PINS OF RIGHT WING NR 4 SPOILER. REPLACED INNER HINGE PINS OF RIGHT WING NR 4 SPOILER IAW TASK CARD 26C68527003.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SHEAR TIE AT FR28 BETWEEN S40R TO S41R. REPLACED SHEAR TIE AT FR28 BETWEEN S40R TO S41R IAW A320 SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON CLEAT AT FR33 BETWEEN S41L TO S42L. REPLACED CLEAT AT FR33 BETWEEN S41L TO S42L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231212.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - LEVEL 2 GALVANIC CORROSION ON FWD CARGO COMPARTMENT CLEAT AT FR 29, S43L - S43R. REPLACED FWD CARGO COMPARTMENT CLEAT AT FR 29, S43L - S43R IAW A320 SRM 51-72-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON CLEAT (SHEAR TIE) AT FR32 BETWEEN S41R TO S42R. REPLACED CLEAT (SHEAR TIE) AT FR32 BETWEEN S41R TO S42R IAW A320 SRM 51-72-11.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON STRINGER TIE CLIP AT FR 33, S41L - S42L. REPLACED STRINGER TIE CLIP AT FR 33, S41L - S42L IAW A320 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 676,450 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE AT FR 69 - FR 70, S23L. REPLACED SHEAR PLATE AT FR 69 - FR 70, S23L IAW EA 133241.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 FILIFORM CORROSION ON SHEAR TIE AT FR32, S43R. REPLACED SHEAR TIE AT FR32, S43R IAW A320 SRM 51-72-11, 51-42-11 AND DWG D53231582.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - LEVEL 2 FILIFORM CORROSION ON STRINGER AT FR 27 + 11", S42L. REPAIRED STRINGER AT FR 27 + 11", S42L IAW A320 SRM 53-00-13.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON CLEAT AT FR33 BETWEEN S41R TO S42R. REPLACED CLEAT AT FR33 BETWEEN S41R TO S42R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231582.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - CORROSION ON STRINGER AT FR 58 + 19", S42L. REPAIRED STRINGER AT FR 58 + 19", S42L IAW A320 SRM 53-00-13.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - LEVEL 2 GALVANIC CORROSION ON FWD CARGO COMPARTMENT CLEAT AT FR 32, S42L- S43L. REPLACED FWD CARGO COMPARTMENT CLEAT AT FR 32, S42L- S43L IAW A320 SRM 51-72-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON CLEAT (SHEAR TIE) AT FR29 BETWEEN S40R TO S41R. REPLACED CLEAT (SHEAR TIE) AT FR29 BETWEEN S40R TO S41R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231582.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON SHEAR TIE AT FR34 BETWEEN S41R TO S42R. REPLACED SHEAR TIE AT FR34 BETWEEN S41R TO S42R IAW A320 SRM 51-72-11.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON CLEAT (SHEAR TIE) AT FR33 BETWEEN S42R TO S43R. REPLACED CLEAT (SHEAR TIE) AT FR33 BETWEEN S42R TO S43R IAW A320 SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON CLEAT AT FR30 BETWEEN S41L TO S42L. REPLACED CLEAT AT FR30 BETWEEN S41L TO S42L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231212.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - LEVEL 2 FILIFORM CORROSION ON STRINGER AT FR 31 + 10", S41R. REPAIRED STRINGER AT FR 31 + 10", S41R IAW A320 SRM 53-00-13.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON CLEAT AT FR30 BETWEEN S40L TO S41L. REPLACED CLEAT AT FR30 BETWEEN S40L TO S41L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231212.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 FILIFORM CORROSION ON CLEAT (SHEAR TIE) AT FR31 BETWEEN S40R TO S41R. REPLACED CLEAT (SHEAR TIE) AT FR31 BETWEEN S40R TO S41R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231582.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - RIGHT AFT EMERGENCY EXIT DOOR SEGMENT ANGLE CRACKED BETWEEN BEAM 1 AND BEAM 3. REPLACED RIGHT AFT EMERGENCY EXIT DOOR SEGMENT ANGLE CRACKED BETWEEN BEAM 1 AND BEAM 3 IAW EA 133172.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON CLEAT (SHEAR TIE) AT FR30 BETWEEN S40R TO S41R. REPLACED CLEAT (SHEAR TIE) AT FR30 BETWEEN S40R TO S41R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231582.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - LEVEL 2 GALVANIC CORROSION ON FWD CARGO COMPARTMENT CLEAT AT FR 31, S40R- S41R. REPLACED FWD CARGO COMPARTMENT CLEAT AT FR 31, S40R- S41R IAW A320 SRM 51-72-11.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - CRACK IN WEB BETWEEN FR8 TO FR11, Y765. REPLACED WEB BETWEEN FR8 TO FR11, Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53113219.

Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - LEVEL 2 GALVANIC CORROSION ON THE LEFT WING SPOILER NR 4 INNER HINGE PINS. REPLACED THE LEFT WING SPOILER NR 4 INNER HINGE PINS IAW A320 AMM 27-64-44.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - CRACKED AREA ON UPPER ATTACHMENT FITTING AT LEFT SLIDING WINDOW POST CUTOUT AT FR4. REPLACED UPPER ATTACHMENT FITTING AT LEFT SLIDING WINDOW POST CUTOUT AT FR4 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53111278.

Part: SILL — CORRODED (FUSELAGE) · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - CORROSION ON THE R2 DOOR LOWER SILL AT FR 66, S23R. REPAIRED HE R2 DOOR LOWER SILL AT FR 66, S23R IAW EA 133170.

Part: SILL — CORRODED (FUSELAGE) · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - CORROSION ON THE L2 DOOR LOWER SILL AT FR 68, S23L. REPAIRED THE L2 DOOR LOWER SILL AT FR 68, S23L IAW EA 133170.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - CRACK ON FLOOR WEB BETWEEN FR8 TO FR11, -Y765. EPLACED FLOOR WEB BETWEEN FR8 TO FR11, -Y765 IAW A320 SRM 51-72-11.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - CRACKED FLOOR SUPPORT AT FR 28 + 15 INCH, -Y254. REPAIRED FLOOR SUPPORT AT FR 28 + 15", -Y254 IAW A320 SRM 53-21-14.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - CRACK IN UPPER FLANGE OF FLOOR SUPPORT AT FR29 + 7 INCHES, Y254. REPAIRED FLOOR SUPPORT AT FR29 + 7 INCHES, Y254 IAW A320 SRM 53-21-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 FILIFORM CORROSION ON SUPPORT FLOOR BEAM BETWEEN FR19 + 7 INCHES TO FR20, -Y1292. REPLACED SUPPORT FLOOR BEAM BETWEEN FR19 + 7 INCHES TO FR20, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112089.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SUPPORT FLOORBEAM BETWEEN FR18 + 5 INCHES TO FR20, -Y765. REPLACED SUPPORT FLOOR BEAM BETWEEN FR18 + 5 INCHES TO FR20, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112089.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - MAJOR REPAIR - S5 CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE AT FR 69 - FR 70, S23R. REPLACED SHEAR PLATE AT FR 69 - FR 70, S23R IAW EA 133241.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR47 + 5 INCHES TO FR64, -Y765. REPAIRED SEAT TRACK BETWEEN FR47 + 5 INCHES TO FR64, -Y765 IAW A320 SRM 53-41-15 & 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,465 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK AT FR20, -Y765. REPLACED SEAT TRACK AT FR20, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112726.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR45, Y765. REPLACED SEAT TRACK AT FR45, Y765 IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR67 + 19 INCHES, Y1155. REPLACED FLOORBEAM AT FR67 + 19 INCHES, Y1155 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR47 TO FR64, -Y1292. REPAIRED SEAT TRACK BETWEEN FR47 TO FR64, -Y1292 IAW A320 SRM 53-41-15.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - DELAMINATION ON UPPER SURFACE OF FLOOR PANEL 232FF BETWEEN FR20 TO FR24, S23R. REPLACED FLOOR PANEL BOARD 232FF BETWEEN FR20 TO FR24, S23R IAW A320 SRM 53-12-00.

Part: DAMPER — OUT OF ADJUST (PAX DOOR) · airframe 67,645 hrs · 30,185 cycles

SAL - EES - S5 CHECK - PASSENGER CREW DOOR 841 DOOR DAMPER AND EMERGENCY CYLINDER PERCUSSION BELLCRANK FINGER REQUIRES ADJUSTMENT. ADJUSTED PASSENGER CREW DOOR 841 DOOR DAMPER AND EMERGENCY CYLINDER PERCUSSION BELLCRANK FINGER IAW A320 AMM 52-11-14-820-002.

Part: DAMPER — OUT OF ADJUST (PAX DOOR) · airframe 67,645 hrs · 30,185 cycles

SAL - EES - S5 CHECK - PASSENGER CREW DOOR 831 DOOR DAMPER AND EMERGENCY CYLINDER PERCUSSION BELLCRANK FINGER REQUIRES ADJUSTMENT. ADJUSTED PASSENGER CREW DOOR 831 DOOR DAMPER AND EMERGENCY CYLINDER PERCUSSION BELLCRANK FINGER IAW A320 AMM 52-11-14-820-002.

Part: FLOORBOARD — DELAMINATED (FUSELAGE) · airframe 67,645 hrs · 30,185 cycles

SAL - S5 - MAJOR REPAIR - DELAMINATION ON UPPER SURFACE OF FLOORBOARD 222CF BETWEEN FR12 TO FR16, S23R. REPLACED FLOORBOARD 222CF BETWEEN FR12 TO FR16, S23R IAW A320 SRM 53-12-00.

Part: WIRE — DAMAGED (CABIN) · airframe 67,635 hrs · 30,182 cycles

FLT 347 - PHX - EEL - EMERGENCY EXIT LIGHT INOPERATIVE AT 1L (WIRE BROKEN UNDER SEAT 1C). MAINTENANCE REPAIRED WIRE IAW ELECTRICAL STANDARD PRACTICES MANUAL 20-48-25.

Part: EPSU — INOPERATIVE (CABIN) · airframe 67,559 hrs · 30,147 cycles

FLT 73 - SEA - EEL - EMERGENCY POWER SUPPLY UNIT (EPSU) 12WL WILL NOT TEST. MAINTENANCE REMOVED AND REPLACED EPSU 12WL IAW AIRBUS MAINTENANCE MANUAL 33-51-38.

Part: ESCAPE ROPE — MISSING (CABIN) · airframe 66,881 hrs · 29,843 cycles

FLT 71 - PHX - SEA - EMERGENCY EQUIPMENT - OVERWING ESCAPE LIFE LINE MISSING AIRCRAFT RIGHT. INSTALLED OVERWING ESCAPE LIFE LINE.

Part: SERVO VALVE — FAULTY (BRAKE SYSTEM) · airframe 66,340 hrs · 29,601 cycles

FLT 9 PHX - ORD - EMERGENCY LANDING - CREW RECEIVED ECAM MESSAGES "BRAKES AUTO BRK FAULT" AND "INOP SYS NORM BRK AUTO BRK". AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. FAULTS WERE PRESENT IN CRUISE, ON DESCENT, APPROACH, LANDING AND TAXI IN. MAINTENANCE REPLACED THE NORMAL BRAKE SERVO VALVE 16GG IAW AIRBUS MAINTENANCE MANUAL 32-42-48-000-001.

Part: BATTERY — DISCHARGED (CABIN) · airframe 66,160 hrs · 29,522 cycles

FLT 460 LAS - EEL - FLASHLIGHT FOR AFT FLIGHT ATTENDANT JUMPSEAT (FWD-FACING) INOPERATIVE. MAINTENANCE REPLACED BATTERY FOR AFT F/A FLASHLIGHT.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 65,720 hrs · 29,326 cycles

FLT 128 - PVR - EEL - FLIGHT ATTENDANT REPORTS FORWARD FLASHLIGHT FAILS PREFLIGHT BATTERY TEST. MAINTENANCE REMOVED AND REPLACED BATTERY. OPERATIONAL CHECK GOOD.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 64,268 hrs · 28,682 cycles

FLT 79 - EXT LOAD FAULT AT RT OVERWING EMERGENCY LT POWER SUPPLY. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY.

Part: BATTERY PACK — DEFECTIVE (EMERGENCY LIGHTS) · airframe 64,261 hrs · 28,680 cycles

FLT 371 - PHX - EEL - AFT EMERGENCY EXIT LIGHTS OVER CENTER AISLE & OVER BOTH AFT DOORS FLICKER & MAKE AN AUDIBLE CLICKING SOUND. ALSO ON ECAM DOOR PAGE BOTH AFT DOOR SLIDE LIGHTS FLICKER ON AND OFF. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-51-38.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 64,127 hrs · 28,621 cycles

FLT 612 - ATL - EMERGENCY EGRESS SYSTEM - PASSENGER ENTRY (L1) DOOR EMERGENCY CYLINDER / ACCUMULATOR LOW. MAINTENANCE SERVICED L1 DOOR EMERGENCY CYLINDER / ACCUMULATOR AS PER AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 64,024 hrs · 28,577 cycles

FLT 335 - PHX - EMERGENCY EGRESS SYSTEM - L1 DOOR ASSIST BOTTLE PRESSURE LOW. MAINTENANCE SERVICED DOOR ASSIST BOTTLE.

Part: LENS — MISSING (CABIN) · airframe 63,999 hrs · 28,566 cycles

FLT 7 - PHX - EEL - L2 DOOR EMERGENCY LIGHT COVER LOWER MISSING. MAINTENANCE REPLACED COVER AS REQUIRED.

Part: LENS — MISSING (CABIN) · airframe 63,841 hrs · 28,497 cycles

FLT 73 - SEA - EEL - SEAT MOUNTED EMERGENCY FLOOR PROXIMITY LIGHT LENS MISSING AT ROWS 13L & 17L. MAINTENANCE INSTALLED LENS ON FLOOR PROXIMITY LIGHTS AT ROWS 13L & 17L.

Part: WIRE — DAMAGED (CABIN) · airframe 63,841 hrs · 28,497 cycles

FLT 73 - SEA - EEL - SEAT MOUNTED FLOOR PROXIMITY LIGHT AT ROW 1L INOPERATIVE. MAINTENANCE REPAIRED WIRES FOR SEAT MOUNTED PROXIMITY LIGHT AT ROW 11 IAW ELECTRICAL STANDARD PRACTICES MANUAL 20-48-11.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 63,479 hrs · 28,337 cycles

FLT 29 - ORD - EEL - FORWARD FLIGHT ATTENDANT'S FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED THE FORWARD FLIGHT ATTENDANT'S FLASHLIGHT BATTERY AS REQUIRED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 63,376 hrs · 28,295 cycles

FLT 123 - PHX - EEL - FORWARD FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,332 hrs · 28,274 cycles

SAL - C7 - EEL - NR 6190502 - LOW BATTERY IN ESPU LEFT HAND FORWARD GALLEY AREA. REPLACED BATTERY IN ESPU LEFT HAND FORWARD GALLEY AREA IAW A320 AMM 33-51-38.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 63,332 hrs · 28,274 cycles

SAL - C7 - MAJOR REPAIR - ESPU IS INOP IN GALLEY AREA. REPLACED EPSU FORWARD LEFT IN GALLEY AREA IAW A320 AMM 33-51-38.

Part: DAMPER — DAMAGED (L2 DOOR) · airframe 63,332 hrs · 28,279 cycles

SAL - C7 - EES - NR 6198392 - HARD IMPACT WHEN OPEN & CLOSE L2 PASSENGER / CREW DOOR. REPLACED DOOR DAMPER CYLINDER AT L2 DOOR IAW A320 AMM 52-13-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,332 hrs · 28,274 cycles

SAL - C7 - MAJOR REPAIR - NR 6198867 - CORROSION ON SEAT TRACK BETWEEN FR41 TO FR47, Y1292. REPLACED SEAT TRACK BETWEEN FR41 TO FR47, Y1292 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,332 hrs · 28,274 cycles

SAL - C7 - MAJOR REPAIR - NR 6167027 - CORROSION ON SEAT TRACK BETWEEN FR41 TO FR47, -Y1292. REPLACED SEAT TRACK BETWEEN FR41 TO FR47, -Y1292 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,332 hrs · 28,274 cycles

SAL - C7 - MAJOR REPAIR - NR 6195664 - CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, -Y1292. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, -Y1292 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,332 hrs · 28,274 cycles

SAL - C7 - MAJOR REPAIR - NR 6166102 - CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, Y1292. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, Y1292 IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,332 hrs · 28,274 cycles

SAL - C7 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR47 TO FR64, Y765. REPAIRED SEAT TRACK BETWEEN FR47 TO FR64, Y765 IAW A320 SRM 53-00-15.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 63,332 hrs · 28,274 cycles

SAL - C7 - MAJOR REPAIR - NR 6191236 - CORROSION ON SHEAR PLATE WEB BETWEEN FR48 TO FR49, S38L. REPAIRED SHEAR PLATE WEB BETWEEN FR48 TO FR49, S38L IAW US AIRWAYS EA 132444.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 63,332 hrs · 28,274 cycles

SAL - C7 - MAJOR REPAIR - NR 6191227 - CRACK ON PRESSURE PANEL AT FR36, Y1292. REPAIRED PRESSURE PANEL AT FR36, Y1292 IAW US AIRWAYS ENGINEERING CARD M2C53306.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 63,332 hrs · 28,274 cycles

SAL - C7 - MAJOR REPAIR - NR 6191226 - CRACK ON PRESSURE PANEL AT FR36, -Y756. REPAIRED PRESSURE PANEL AT FR36, -Y756 IAW US AIRWAYS ENGINEERING CARD M2C53307.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,332 hrs · 28,274 cycles

SAL - C7 - MAJOR REPAIR - NR 6191212 - CORROSION ON SEAT TRACK AT FR33 + 16 INCHES, Y765. REPAIRED SEAT TRACK AT FR33 + 16 INCHES, Y765 IAW A320 SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,332 hrs · 28,274 cycles

SAL - C7 - MAJOR REPAIR - NR 6191213 - CORROSION ON SEAT TRACK BETWEEN FR31 T0 FR35, Y1292. REPAIRED SEAT TRACK BETWEEN FR31 T0 FR35, Y1292 IAW A320 SRM 53-21-15.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 63,332 hrs · 28,274 cycles

SAL - C7 - EES - LOW PRESSURE AT L-1 DOOR DAMPER EMERGENCY OPERATIONAL CYLINDER. PERFORMED CHARGING OF L-1 DOOR DAMPER EMERGENCY OPERATIONAL CYLINDER IAW A320 AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 63,323 hrs · 28,274 cycles

SAL - C7 - EES - LOW PRESSURE IN R-1 DOOR DAMPER EMERGENCY OPERATIONAL CYLINDER. PERFORMED CHARGING OF R-1 DOOR DAMPER EMERGENCY OPERATIONAL CYLINDER IAW A320 AMM 52-10-00-614-001.

Part: COVER — CRACKED (FUSELAGE) · airframe 63,332 hrs · 28,274 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: SILL — CORRODED (FUSELAGE) · airframe 63,332 hrs · 28,274 cycles

SAL - C7 - MAJOR REPAIR - NR 6190560 - GALVANIC CORROSION ON LOWER SILL OF R-2 DOOR BETWEEN FR66 TO FR68, -Y1732. REPAIRED LOWER SILL OF R2 DOOR BETWEEN FR66 TO FR68, -Y1732 IAW A320 SRM 53-41-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,332 hrs · 28,274 cycles

SAL - C7 - MAJOR REPAIR - NR 6166099 - CORROSION ON SEAT TRACK BETWEEN FR35 TO FR36, Y1292. REPLACED SEAT TRACK BETWEEN FR35 TO FR36, Y1292 IAW A320 SRM 51-72-11.

Part: BEARING — EXCESS PLAY (RUDDER) · airframe 63,332 hrs · 28,274 cycles

SAL - C7 - MAJOR REPAIR - NR 6198958 - EXCESSIVE PLAY ON BEARING OF NR 2 RUDDER HINGE FITTING. REPLACED NR 2 RUDDER HINGE FITTING IAW A320 AMM 55-36-41.

Part: HINGE — WORN (RUDDER) · airframe 63,332 hrs · 28,274 cycles

SAL - MAJOR REPAIR - C7 CHECK - RUDDER HINGE NR 5 HAS EXCESSIVE PLAY AT HORIZONTAL STABILIZER STATION RIB 7. REPLACED RUDDER HINGE NR 5 AT HORIZONTAL STABILIZER STATION RIB 7 IAW A320 AMM 55-36-41.

Part: HINGE — WORN (RUDDER) · airframe 63,332 hrs · 28,274 cycles

SAL - MAJOR REPAIR - C7 CHECK - RUDDER HINGE NR 1 HAS EXCESSIVE PLAY AT HORIZONTAL STABILIZER STATION RIB 2. REPLACED RUDDER HINGE NR 1 AT HORIZONTAL STABILIZER STATION RIB 2 IAW A320 AMM 55-36-41.

Part: HINGE — WORN (RUDDER) · airframe 63,332 hrs · 28,274 cycles

SAL - MAJOR REPAIR - C7 CHECK - RUDDER HINGE NR 4 HAS EXCESSIVE PLAY AT HORIZONTAL STABILIZER STATION RIB 6. REPLACED RUDDER HINGE NR 4 AT HORIZONTAL STABILIZER STATION RIB 6 IAW A320 AMM 55-36-41.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 63,142 hrs · 28,190 cycles

FLT 2039 - PHX - LAS - EMERGENCY LIGHTS - EMERGENCY LIGHT FAILED TEST (RIGHT EMERGENCY POWER SUPPLY UNIT). REMOVED AND REPLACED RIGHT EMERGENCY POWER SUPPLY UNIT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,332 hrs · 28,274 cycles

SAL - C7 - MAJOR REPAIR - NR 6191067 - GALVANIC CORROSION ON FLOORBEAM ASSEMBLY BETWEEN FR65 TO FR67, Y920. REPLACED FLOORBEAM ASSEMBLY BETWEEN FR65 TO FR67, Y920 IAW A320 SRM 51-72-11.

Part: SENSOR — FAULTY (CABIN) · airframe 62,920 hrs · 28,079 cycles

FLT 245, A BURNING ODOR WAS REPORTEDLY COMING FROM GASPER VENTS AT ROWS 20-23 AIRCRAFT RIGHT DURING FLIGHT. CREW DIVERTED TO ELP. AN INSPECTION OF PASSENGER SERVICE UNITS AND DEU'S (DECODER/ENCODER UNIT) WAS PERFORMED WITH NO FAULTS FOUND. AIRCRAFT WAS MAINTENANCE FERRIED TO PHX. MAINTENANCE REPLACED TEMP SENSOR IAW MM 21-61-12.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 62,658 hrs · 27,950 cycles

PHX - OVERNIGHT - MAJOR REPAIR - EXFOLIATION CORROSION ON INTERNAL DOUBLER OF RIGHT LAV SYSTEM VACUUM GENERATOR EXHAUST PORT. REPAIRED INTERNAL DOUBLER AND FUSELAGE SKIN IAW A320 SRM 53-41-11.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 62,478 hrs · 27,860 cycles

EMERGENCY EQUIPMENT - L-1 DOOR ASSIST BOTTLE LOW PRESSURE. MX SERVICED DOOR ASSIST BOTTLE.

Part: DEU — FAULTY (CABIN) · airframe 62,423 hrs · 27,831 cycles

LOG PAGE 8299898 FLT NR 335 PHX-SJD BURNING SMELL FLIGHT ATTENDANT ADVISED LIGHTS AT EMERGENCY EXIT ROW FLICKERING WITH SPEAKER BREAKING SQUELCH. RESET CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS) PER QRH. 10 MINUTES LATER FLIGHT ATTENDANT ADVISED THERE WAS AN ELECTRICAL SMOKE ODOR PRESENT FROM EMERGENCY EXIT ROW FORWARD TO GALLEY. MX FOUND DEU 'A' FAULTING AND HEAT DISCOLORATION WAS NOTICED. R&R DEU 'A' 200RH11. OPS CHECK WAS GOOD.

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 62,034 hrs · 27,658 cycles

LOG PAGE 4377534 FLT NR 612 PHX-ATL EEL FORWARD CABIN SEVERAL EMERGENCY EXIT LIGHTS INOPERATIVE. MX R&R THE FORWARD EMERGENCY LIGHT BATTERY. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 61,288 hrs · 27,302 cycles

FLT 616 SEA-PHX - EMERG EQUIP - OUTBOARD EMERGENCY FLASHLIGHT BLINKING SLOW. MAINTENANCE REMOVED AND REPLACED THE OUTBOARD EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECK GOOD. (S)

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 58,325 hrs · 25,961 cycles

PHX - EEL - LOG 4160010 - FWD EMERGENCY LIGHT TEST FAILED. MX REPLACED THE 10W POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 58,325 hrs · 25,961 cycles

PHX - EEL - LOG 4121217 - EMERGENCY EXIT LIGHT TEST FAILED. MX REPLACED THE LT EPSU. OPERATIONAL TEST WAS GOOD.

Part: FITTING — WORN (ZONE 300) · airframe 58,301 hrs · 25,951 cycles

SAL - MAJOR REPAIR - C-06 CHECK - NR 5985591, RUDDER HINGE NR 2 FITTING HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 1926 / RIB 4. REPLACED RUDDER HINGE NR 2 FITTING, VERTICAL STABILIZER STATION 1926/RIB 4 IAW A320 AMM 55-36-41.

Part: FITTING — CORRODED (ZONE 100) · airframe 58,301 hrs · 25,951 cycles

SAL - MAJOR REPAIR - C-06 CHECK - NR 5985459, CORROSION ON CENTER FITTING IN R1 DOOR THRESHOLD SILL AREA, BS 709/FR16 - BS 808/FR 20, -Z 520. REPLACED CENTER FITTING IN R1 DOOR THRESHOLD SILL AREA, BS 709/FR16 - BS 808/FR 20, -Z 520 IAW A320 ARM 51-72-11.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 58,301 hrs · 25,951 cycles

SAL - MAJOR REPAIR - C-6 CHECK - CORROSION ON CABIN SEAT TRACK, BS 1590/FR 36 - BS 1810 / FR 41, +Y765. REPLACED CABIN SEAT TRACK, BS 1590/FR 36 - BS 1810/FR 41, +Y765 IAW A320 SRM 51-72-11.

Part: SILL — CRACKED (ZONE 100) · airframe 58,301 hrs · 25,951 cycles

SAL - MAJOR REPAIR - C-06 CHECK - NR 5985310, CORROSION ON BULK CARGO DOOR LOWER SILL, BS 2830/FR 60 - BS 2936/FR 62, -Y630 TO -Y680. REPAIRED BULK CARGO DOOR LOWER SILL, BS 2830/FR 60 - BS 2936/FR 62, -Y630 TO -Y680 IAW A320 SRM 53-41-49 FIGURE 203.

Part: FITTING — WORN (LT MLG DOOR) · airframe 58,301 hrs · 25,951 cycles

SAL - MAJOR REPAIR - C-06 CHECK - NR 5985453, WEAR ON FORWARD SUPPORT FITTING OF LT MAIN LANDING GEAR DOOR, BS 1869/FR 42, S-41L. REPLACED FORWARD SUPPORT FITTING OF LT MAIN LANDING GEAR DOOR, BS 1869/FR 42, S-41L IAW A320 SRM 51-72-11, PAGE 1.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 56,227 hrs · 25,060 cycles

PHX - EEL - AFT LT EMERGENCY LT CHARGER INOP, 3 RED FAULT. REMOVED AND REPLACED AFT LT EMERGENCY BATTERY CHARGER. OPS CK GOOD

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 53,530 hrs · 23,890 cycles

LAX - EEL - DURING OVERNIGHT MAINTENANCE THE RT EPSU FAILED TEST AT PTP. MAINTENANCE REMOVED AND REPLACED THE RT EPSU IAW AIRBUS MM 33-51-38. OPERATIONAL CHECKS WERE GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,493 hrs · 23,876 cycles

PHX - EEL - DURING OVERNIGHT INSPECTIONS MAINTENANCE REPORTED THAT THE EMERGENCY LIGHTS AT ROWS 9R, 11R, 13L, 17L, 21L AND AFT ENTRY DOORS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE MID CABIN RT EPSU AND THE AFT LEFT OVERHEAD EPSU IAW AMWEST TASK CARD R1C33303 AND A1C33302. OPERATIONAL CHECKS WERE GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 53,493 hrs · 23,876 cycles

PHX - EEL - DURING OVERNIGHT MAINTENANCE DISCOVERED THE EMERGENCY EXIT LIGHTS FAILED OPERATIONAL TEST, MESSAGE "COMM AFT L". MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNIT, 13WL, IAW AIRBUS 320 AMM 33-51-38. OPERATIONAL CHECKS WERE GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,399 hrs · 23,835 cycles

PHX - EEL - DURING OVERNIGHT MAINTENANCE DISCOVERED THE EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 18 TO ROW 26. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY POWER SUPPLY IAW AIRBUS 320 MM 33-51-38-991-001. OPERATIONAL CHECKS WERE GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,399 hrs · 23,835 cycles

DURING OVERNIGHT MAINTENANCE LIGHT TEST FAILED. MAINTENANCE REMOVED AND REPLACED THE AFT POWER SUPPLY. OPERATIONAL TESTS WERE GOOD. VENDOR REPLACED RELAYS RL405 AND RL406. THE UNIT WAS REPAIRED AND TESTED IAW CMM 33-51-09 REV 2

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 53,334 hrs · 23,808 cycles

DURING INSTALLATION OF PASSENGER SEATS EMERGENCY LIGHTS FAILED SYSTEM TEST. MAINTENANCE REMOVED AND REPLACED THE LEFT AFT EMERGENCY POWER SUPPLY. ALSO REPLACED THE RT EMERGENCY DOOR POWER SUPPLY. WORK WAS PERFORMED IAW AIRBUS 320 AMM 33-51-38. OPERATIONAL TEST WERE GOOD IAW AIRBUS 320 AMM 33-51-00. VENDOR CONFIRMED FAULT. VENDOR REPLACED FUSE F2. VENDOR REPAIRED AND TESTED UNIT IAW CMM 33-51-12 REV 2

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 53,334 hrs · 23,808 cycles

SAL - DURING C05 CHECK DISCOVERED DELAMINATED FLOOR PANEL NR 151GF AND PROTECTIVE DOUBLER DISBONDED IN AFT CARGO COMPARTMENT. MAINTENANCE REMOVED FLOOR PANEL NR 151GF AND INSTALLED FABRICATED FLOOR PANEL IAW IRM 9701. NEW PROTECTIVE DOUBLER WAS BONDED TO SURFACE OF FLOOR PANEL 151GF IAW AMERICA WEST AIRLINES TASKCARD M2M53305.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 53,334 hrs · 23,808 cycles

SAL - DURING C 5 CHECK DISCOVERED AFT AVIONIC COMPARTMENT FRAME SUPPORT CRACKED, 1.2 INCHES, BETWEEN FS 22 AND FS 23 AT Y1110. MAINTENANCE REMOVED SUPPORT WEB AND INSTALLED NEW WEB BETWEEN FS 22 AND FS 23 AT Y1110 IAW AIRBUS 320 SRM 51-72-11.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 53,099 hrs · 23,715 cycles

DURING TAKEOFF ROLL RECEIVED AVIONICS SKIN AIR VALVE FAULT & AN ECAM MESSAGE STATING NOT TO CLIMB ABOVE 10,000 FT. RETURNED & LANDED WITHOUT EVENT. MX R & R SKIN AIR OUTLET VALVE, 22HQ, IAW MM . OPS CHK GOOD. TEARDOWN CONFIRMS FAULT. ON ENTRY TEST, VALVE FAILED TO SHUTOFF DUE TO ELEC STOP OPEN. VALVE TRAVELED UNTIL STOPS CONTACTED & ACT TORQUE LIMITER SLIPPED. ACT NOISY DURING OPS. AFTER DIASSEMBLY, ELEC STOP SWITCH FOUND NOT DEPRESSED DOWN ENOUGH FOR PROPER CONTACT. ACT TRAVELED UNTIL STOPS CONTACTED. REPLACED CONSUMABLES, IDLE GEAR & OVERHAULED ACT. UNIT CLEANED, SWITCH ADJUSTED, IDLE GEAR REPLACED & ACTUATOR TESTED IAW CMM.

Part: FUEL CONTROL — MALFUNCTIONED (APU) · airframe 52,888 hrs · 23,628 cycles

DURING GROUND HANDLING OPERATIONS, WAS REPORTED THAT THERE WAS AN APU TAIL PIPE FIRE AFTER SHUTDOWN. T-HANDLE WAS PULLED, BOTTLE WAS NOT BLOWN. MAINTENANCE INSPECTED THE APU AND TAILPIPE. REMOVED AND REPLACED THE APU FUEL FLOW DIVIDER AND THE APU FUEL CONTROL IAW AIRBUS 320 MM 49-32-11 & 12. OPERATIONAL CHECKS WERE GOOD. VENDOR TEAR DOWN REPORT DID NOT CONFIRM FAILURE. UNIT WAS FOUND TO HAVE HAD A PACKING SMASHED OUT AND WEDGED BETWEEN ROTOR AND OIL SEAL, BUT CUSTOMER CONFIRMED REMOVAL REASON WAS MARKED NO. UNIT WAS REPAIRED AND RECERTIFIED IAW CMM 49-30-97 REV. 07.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 52,416 hrs · 23,428 cycles

EEL-DURING OVERNIGHT INSPECTION DISCOVERED THE EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 24L INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CONNECTOR PLUG FOR THE EMERGENCY LIGHT ASSEMBLY AT ROW 24L IAW MM. OPERATIONAL CHECKS WERE GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY EXIT) · airframe 49,374 hrs · 22,124 cycles

ORD - EMERGENCY EXIT LIGHT INOPERATIVE AT AFT OVERWING EXIT, RIGHT SIDE WALL MOUNTED. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AT RIGHT AFT OVERWING EXIT; OPERATIONAL CHECK WAS GOOD.

Part: CONTROL UNIT — FAULTY (NR 1) · airframe 48,854 hrs · 21,906 cycles

ON SHORT FINAL AFTER MLG SELECTED DOWN, RECEIVED NLG STEERING FAULT, ABORTED APPROACH & FLEW BY TOWER. CYCLED ANTI-SKID & NLG STEERING SWITCH & FAULT CLEARED, DECLARED EMERGENCY & LANDED WITHOUT FURTHER EVENT. MX TROUBLESHOT SYS, BITE CODES INDICATED INTERNAL FAULT IN MLG CONTROL INTERFACE UNIT NR 1. R/R LGCIU NR 1 (D197) IAW AMM, OPS CHECK GOOD. FUNCTIONAL TEST OF LGCIU COULD NOT DUPLICATE REASON FOR REMOVAL, UNIT WAS INSPECTED AND SUBJECTED TO EXTENSIVE TESTING PER CMM, RETURNED TO SERVICE AS NFF.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK, CORROSION WAS FOUND ON AFT SIDE OF AFT CARGO COMPARTMENT FLOOR PANEL 151AF. MAINTENANCE REMOVED CORRODED AFT CARGO FLOOR PANEL 151AF; FABRICATED A NEW REPLACEMENT FLOOR PANEL; INSTALLED REPAIR PART IAW A320 SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 48,382 hrs · 21,725 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK A 6 INCH CRACK WAS FOUND IN FLOOR PANEL 221AF. MAINTENANCE REMOVED CRACKED FLOOR PANEL FROM FS 12 TO FS 16 AND -Y81 TO -Y512; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG B5D53610125AND A320 SRM 53-02-00, FIG. 209.

Part: DAMPER — LEAKING (L-1 DOOR) · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK, THE L-1 DOOR ASSIST DAMPER PRESSURE WAS LOW. MAINTENANCE REMOVED L-1 DOOR ASSIST DAMPER PERCUSSION MECHANISM AND REPLACED TWO EACH PACKINGS. REINSTALLED L-1 DOOR ASSIST DAMPER IAW A320 AMM 52-10-00, LEAK AND OPERATIONAL CHECK WAS GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK, FOUND BROKEN EMERGENCY ESCAPE PATH LIGHT WIRES AT SEAT ROWS 5, 7, 13, AND 24 LEFT. MAINTENANCE REPAIRED BROKEN EMERGENCY ESCAPE PATH LIGHT WIRES AT SEAT ROWS 5, 7, 13, AND 24 LT, OPERATIONAL CHECK WAS GOOD.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL FORWARD PLATE, AT FORWARD INBOARD EDGE FS 53. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL FORWARD PLATE AT FS 53; FABRICATED A NEW REPLACEMENT PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 2, 3, 8, & 12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND IN 8 PLACES ON LEFT CABIN SEAT TRACK Y765 BETWEEN FS 41 AND FS 47. MAINTENANCE REMOVED CORRODED SECTION LT CABIN SEAT TRACK Y765 FROM FS 41 TO FS 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND IN 8 PLACES ON RT CABIN SEAT TRACK Y1292 BETWEEN FR 41 AND FR 47. MAINTENANCE REMOVED CORRODED SECTION RT CABIN SEAT TRACK Y1292 FROM FR 41 TO FR 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND IN 6 PLACES ON RT CABIN SEAT TRACK Y765 BETWEEN FS 36 AND FS 41. MAINTENANCE REMOVED CORRODED SECTION RT CABIN SEAT TRACK Y765 FROM FR 36 TO FR 41; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 12-18.

Part: PLATE — CORRODED (FUSELAGE) · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK, CORROSION WAS FOUND IN 7 PLACES ON FORWARD CARGO COMPARTMENT DOOR SILL PLATE BETWEEN FS 25 AND FS 28. MAINTENANCE REMOVED CORRODED FORWARD CARGO COMPARTMENT DOOR SILL PLATE FROM FS 25 TO FS 28; FABRICATED A NEW REPLACEMENT PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND IN 5 PLACES ON LT CABIN SEAT TRACK Y1292 BETWEEN FS 36 AND FS 41. MAINTENANCE REMOVED CORRODED SECTION LT CABIN SEAT TRACK Y1292 FROM FS 36 TO FS 41; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-42-11.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FORWARD CARGO COMPARTMENT SILL WEB BETWEEN FS 26 AND FS 27. MAINTENANCE REMOVED CORRODED FORWARD CARGO COMPARTMENT SILL WEB FROM FS 24 TO FS 28; FABRICATED A NEW REPLACEMENT SECTION OF WEB; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND IN 8 PLACES ON LT CABIN SEAT TRACK Y1292 BETWEEN FS 41 AND FS 47. MAINTENANCE REMOVED CORRODED SECTION LT CABIN SEAT TRACK Y1292 FROM FS 41 TO FS 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: WEB — CORRODED (FUSELAGE) · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK, CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL WEB (SHEET COVER) BETWEEN FS 52 AND FS 56. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT DOOR SILL WEB FROM FS 52 TO FS 56; FABRICATED A NEW REPLACEMENT SECTION OF WEB; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 2 & 3.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND IN 8 PLACES ON RT CABIN SEAT TRACK Y765 BETWEEN FS 41 AND FS 47. MAINTENANCE REMOVED CORRODED SECTION RT CABIN SEAT TRACK Y765 FROM FS 41 TO FS 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND IN 5 PLACES ON RT CABIN SEAT TRACK Y1292 BETWEEN FR 36 AND FR 41. MAINTENANCE REMOVED CORRODED SECTION RT CABIN SEAT TRACK Y1292 FROM FR 36 TO FR 41; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW SRM 51-42-11.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT SPLICE PLATE (GUSSET) AT LOWER AFT CORNER OF DOOR CUTOUT FS 62. MAINTENANCE REMOVED CORRODED PLATE GUSSET Y1492 RT, FS 62; FABRICATED A NEW REPLACEMENT PLATE GUSSET; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y1292 RT BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CORRODED BEAM Y1292 RT FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW SRM 51-42-11, FIG. 9-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y1292 RT BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CORRODED BEAM Y1292 RT FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 9-12.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT AT FR 66. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK, GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT AFT SHEAR PLATE BETWEEN FS 69 AND FS 70, OUTBOARD OF BEAM Y1292. MAINTENANCE REMOVED CORRODED RT AFT SHEAR PLATE FROM FS 69 TO FS 70, AT Y1292; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 2, 3, & 11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT BETWEEN FS 16 AND FS 20. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 RT FROM FS 16 TO FS 20; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 53-11-14, FIG 102.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON OB SEAT TRACK Y1292 RT FROM FR 20 TO THE AFT SIDE OF FR 23. MAINTENANCE REMOVED CORRODED SEAT TRACK Y1292 RT FROM FR 20 TO FR 23; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW SRM 51-42-11, FIG. 11-18.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF L-2 DOOR SILL AT Y1350 BETWEEN FR 66 AND FR 68. MAINTENANCE CUTOUT DAMAGE IN L-2 DOOR SILL AT Y1350 FROM FS 66 TO FS 68; FABRICATED A REPAIR ANGLE, FILLER, AND PLATE; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14, FIG. 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT Y254 RT BETWEEN FS 16 AND FS 20. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOOR SUPPORT Y254 RT FROM FS 16 TO FS 20; FABRICATED A NEW REPLACEMENT SECTION OF FLOOR SUPPORT AND 4 EACH SPLICE ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14, 202.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF LT AFT SHEAR PLATE, OB OF Y1292, BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED CORRODED LT AFT SHEAR PLATE AT Y1292 FROM FR 69 TO FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON RT IB SEAT TRACK Y765 FROM FR 20 TO THE AFT SIDE OF FR 23. MAINTENANCE REMOVED CORRODED SEAT TRACK Y765 RT FROM FR 20 TO FR 23; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW SRM 51-72-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK, FOUND CORROSION ON L-2 DOOR ENTRY WAY FLOOR PANEL 221FF. MAINTENANCE REMOVED AND REPLACED L-2 DOOR ENTRY WAY FLOOR PANEL 221FF IAW T/C C1D25306.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT OUTBOARD WEB Y1698 BETWEEN FS 20 AND FS 21. MAINTENANCE REMOVED CORRODED SECTION OF RT OUTBOARD WEB Y1698 FROM FS 20 TO FS 21; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER OB EDGE OF R-2 DOOR LOWER CENTER SCUFF PLATE SHAPE SILL AT Y1546, BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED SECTION R-2 DOOR LOWER CENTER SCUFF PLATE SHAPE SILL AT Y1546, FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT SECTION OF SHAPE SILL; INSTALLED REPAIR PART IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (CORRODED) · corrosion level 2 · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT BETWEEN FS 68 AND FS 69. MAINTENANCE REMOVED CORRODED SECTION BEAM Y1292 LT FROM FS 68 TO FS 69; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 48,382 hrs · 21,725 cycles

MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON CORNER OF AFT CARGO COMPARTMENT FLOOR PANEL 161AF UNDER PADDING. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT FLOOR PANEL 161AF, FABRICATED A NEW REPLACEMENT FLOOR PANEL, INSTALLED PANEL IAW A320 SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 48,382 hrs · 21,725 cycles

DURING C-04 CHECK, FOUND R-1 DOOR ENTRY FLOOR PANEL DELAMINATED. MAINTENANCE REMOVED AND REPLACED R-1 DOOR ENTRY FLOOR PANEL IAW T/C C1D25306.

Part: EPSU — FAILED (ZONE 263) · airframe 47,979 hrs · 21,544 cycles

FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHTS IN AFT GALLEY WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT GALLEY EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM WAS GOOD.

Part: ROD END — DETACHED (NLG) · airframe 45,656 hrs · 20,591 cycles

AFTER TAKEOFF, NLG FAILED TO RETRACT, CYCLED MLG TO DOWN POSITION & GEAR INDICATED DOWN & LOCKED. TURNED BACK & LANDED WITHOUT EVENT. MAINT FOUND NLG RETRACT ACTUATOR PISTON ROD END HAD SEPARATED FROM BEARING. R & R NLG RETRACT ACTUATOR IAW AMM 32-31-22, CYCLED GEAR SEVERAL TIMES WITH NO FAULTS NOTED. INVESTIGATION OF NLG RETRACT ACTUATOR FOUND PISTON ROD END BORE ELONGATED WHICH IS BELIEVED TO HAVE BEEN CAUSED BY FORCES APPLIED DURING RETRACTION & EXTENSION. CONTINUED OPERATION IN THIS CONDITION CAUSED BEARING THAT ALSO HAD INDICATIONS OF EQUAL DISTORTION TO MIGRATE OUT OF ROD END BORE. OTHER FINDINGS INDICATED THAT THE SWAGING OF THE BEARING WAS INADEQUATE & BEARING HOUSING MATERIAL MAY NOT BE ABLE TO WIT

Part: OVERHEAT LOOP — FAULTY (NR 1 PYLON) · airframe 44,973 hrs · 20,319 cycles

PHX - ABORTED TAKEOFF - FLT 0567 - ON APPLICATION OF TOGA POWER FOR BLEEDS OFF TAKEOFF AT PHX EN ROUTE FOR MCO, RECEIVED ECAM MESSAGES FOR ENGINE NR 1 BLEED LEAK FOLLOWED BY APU BLEED FAULT & AIR PACK NR 1 FAULT. REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE PERFORMED BLEED MONITOR COMPUTER BITE TEST THAT FAULTED NR 1 ENGINE PYLON LOOP. FOLLOWED TSM 36-22-15 AND REPLACED NR 1 PYLON OVERHEAT SENSING ELEMENT (1HF1). REPLACED APU LOAD CONTROL VALVE IAW AMM 49-51-51, APU BLEED FAULT STILL EXISTS, REPLACED APU BLEED SWITCH IN FLIGHT DECK AND SYSTEM OPERATION CHECK WAS NORMAL. PART NAME; SWITCH, MFG; ECE L'EQUIPEMENT, P/N; 2FCC2FEA0B01263, CONDITION; LOOSE

Part: RIB — CRACKED (NR 1 PYLON) · airframe 44,459 hrs · 20,113 cycles

DURING C-03 CHECK A 1.5 INCH CRACK WAS FOUND ON NR 1 PYLON LOWER AFT FIXED FAIRING RIB 14. MAINTENANCE REMOVED CRACKED NR 1 PYLON LOWER AFT FIXED FAIRING RIB; FABRICATED A NEW REPLACEMENT RIB; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG. 7-12, 10, 12, AND 22, FIG 2, 3, &. 8, AND SRM 51-44-11, PG. 1 AND 4, FIG. 1.

Part: DAMPER — FAILED (PAX DOOR) · airframe 44,459 hrs · 20,113 cycles

DURING C-03 CHECK THE L-2 DOOR ASSIST DAMPER CYLINDER FAILED FUNCTIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR DAMPER CYLINDER IAW AMM SUBTASKS 52-13-14-020-050-0 & 52-13-14-420-051-0. ADJUSTED AND SERVICED IAW SUBTASK 52-13-14-820-050-0 & 52-13-14-200-001; OPERATIONAL CHECK GOOD IAW SUBTASK 52-13-14-210-060-0. VENDOR FUNCTIONAL CHECK OF DAMPER CYLINDER S/N 101 CONFIRMED FAILURE OF UNIT. REAR CUP WAS FOUND RUSTED & PITTED, FRONT CUP WAS FOUND LOW ON FLUID, AND DETERIORATED SEALS WERE FOUND ON THE PERCUSSION AND BOTTLE ASSEMBLY, REPLACED ALL DAMAGED PARTS AND COMPLIED WITH SERVICE BULLETINS FE174-52-1, 2, & 3R1 CHANGING PART NUMBER TO FE174-0011.

Part: CONNECTOR — DAMAGED (SEAT ROW 26 LT) · airframe 44,459 hrs · 20,113 cycles

MCN - EEL - DURING C-03 CHECK FOUND A DAMAGED RECEPTACLE AND CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT. MAINTENANCE REMOVED AND REPLACED RECEPTACLE AND CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT, OPERATIONAL CHECK WAS GOOD.

Part: PANEL — CRACKED (NR 1 NACELLE) · airframe 44,459 hrs · 20,113 cycles

DURING C-03 CHECK 2 EACH 1/4 INCHES CRACKS WERE FOUND ON NR 1 ENGINE PYLON PANEL (413DL) ON INBOARD SIDE. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK IS CONTAINED; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW A320 SRM 54-52-12, PG. 221-225, AND SRM 51-42-11, PG. 8-10, & 12.

Part: SKIN — CORRODED (NR 1 PYLON) · airframe 44,459 hrs · 50,495 cycles

DURING C-03 CHECK CORROSION WAS FOUND ON NR 1 PYLON TRAILING EDGE FAIRING INBOARD SKIN, PYLON STA 8370 TO 9278. MAINTENANCE REMOVED CORROSION ON NR 1 PYLON TRAILING EDGE FAIRING INBOARD SKIN AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED DAMAGED SKIN PYLON STA 8370 TO 9278; UPON FURTHER INSPECTION FOUND CRACKED LOWER RIB; REMOVED CRACKED RIB; FABRICATED NEW REPLACEMENT SKIN AND LOWER RIB; INSTALLED REPAIR PARTS IAW A320 SRM 51-42-11 PG 7-12, FIG 2.

Part: RESERVOIR — BROKEN (ESCAPE SLIDE) · airframe 62,039 hrs · 50,495 cycles

DURING C-03 CHECK THE LT OVER WING ESCAPE SLIDE RESERVOIR INFLATION CABLE CONNECTOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE RESERVOIR ASSEMBLY, OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,358 hrs · 18,927 cycles

LAS - EEL - EMERGENCY LIGHT BATTERY FAILED TEST AT FLIGHT ATTENDANT PANEL AND EMERGENCY POWER SUPPLY UNIT 11WL. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY AT EMERGENCY POWER SUPPLY UNIT 11WL. OPERATIONAL TEST WAS GOOD.

Part: O-RING — LEAKING (ZONE 140) · corrosion level 0 · airframe 40,712 hrs · 18,671 cycles

PHX - AIR TURN BACK - FLT 0175 - EN ROUTE FROM PHX TO MEX IN CRUISE ECAM INDICATION FOR GREEN HYDRAULIC SYSTEM LOW LEVEL FOLLOWED BY ECAM HYDRAULIC LEVEL IN AMBER. ON RETURN TO PHX TURNED ON GREEN PUMP / PTU AUTO PER ECAM INSTRUCTIONS AND RECOVERED NORMAL PRESSURE. LOWERED LANDING GEAR AND RECOVERED 1/2 OF HYDRAULIC QUANTITY, NO FURTHER HYDRAULIC LOSS. LANDED SAFELY AT PHX, AIRCRAFT TOWED TO GATE. MAINTENANCE FOUND HYDRAULIC LEAK AT SLAT POWER CONTROL UNIT ON R/H SIDE LOWER FLEX LINE UNION. REPLACED O-RINGS ON FLEX LINE UNIONS. OPERATIONAL AND LEAK CHECK WAS GOOD PER 27-84-00-710-001. PART NAME; O-RING, MFG; NATIONAL AEROSPACE STANDARDS (NAS), P/N; NAS1612-6, COND; LEAKING, LOC; ZONE 140.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 40,221 hrs · 18,485 cycles

LAS - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE LT FORWARD EMERGENCY FLASHLIGHT WAS NOT BLINKING. MAINTENANCE REPLACED THE LT FORWARD EMERGENCY FLASHLIGHT.

Part: HYDRAULIC LINE — BURST (NLG) · airframe 39,469 hrs · 18,193 cycles

ON FINAL TURN INTO PHX WHEN LANDING GEAR WAS EXTENDED ECAM INDICATED A LOSS OF GREEN SYSTEM HYDRAULIC PRESSURE. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED UNEVENTFULLY WITH ALTERNATE HYDRAULIC SYSTEM OPERATING NORMALLY. NOSE WHEEL STEERING INOPERATIVE AFTER LANDING AND AIRCRAFT REQUIRED TOW TO GATE. MAINTENANCE FOUND THE LT MAIN LANDING GEAR DOOR RETRACT ACTUATOR FLEX LINE HAD BURST. REMOVED AND REPLACED THE LT MAIN LANDING GEAR DOOR RETRACT FLEX LINE. MAINTENANCE ALSO FOLLOWED PROCEDURES FOR POSSIBLE PUMP CAVITATION AMM 29-00-00-280-006 AND REMOVED AND REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW AMM 29-13-51-401.

Part: HOUSING — BROKEN (SEAT ROW 7 L/H) · airframe 39,379 hrs · 18,162 cycles

PHX - EEL - "C" - DURING INSPECTION EMERGENCY ESCAPE LIGHT WAS FOUND BROKEN AT SEAT ROW 7 L/H. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE LIGHT HOUSING AT SEAT ROW 7, OPERATIONAL CHECK WAS GOOD.

Part: CONTROLLER — FAILED (AUTOPILOT SYS) · airframe 37,878 hrs · 17,538 cycles

PHX- ABORTED TAKEOFF - FLT 239 - ON TAKEOFF ROLL CREW HAD NO INDICATION OF TOGA AND ABORTED THE TAKEOFF AT 70 KTS AND RETURNED TO THE GATE. MAINTENANCE TROUBLESHOT AND REPLACED THE FLIGHT CONTROL UNIT PER AMM 22-81-12-401, SYSTEM CHECKS WERE GOOD. NO FURTHER DISCREPANCIES HAVE BEEN REPORTED.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 37,046 hrs · 17,208 cycles

DTW - unscheduled landing - 6/7/01 - FLT 55 - en route from JFK to LAS the First Officer's NR 1 window outer pane cracked and the aircraft diverted to DTW making an uneventful landing. window changed and aircraft returned to service.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 36,462 hrs · 16,985 cycles

PHX - EMERGENCY LANDING - 4/10/01 - EN ROUTE FROM ORD TO PHX THE FLIGHT CREW GOT AN ECAM WARNING AND CAUTION LIGHT FOR THE GREEN HYD SYSTEM RESERVOIR OVERHEAT. THE CREW CALLED AN EMERGENCY LANDING; THE CREW CYCLED THE GREEN HYD SYSTEM SWITCH AND THE GREEN SYSTEM FUNCTIONED NORMALLY AND THE WARNINGS CLEARED AS WELL. AN UNEVENTFUL LANDING. MAINTENANCE PERFORMED HYDRAULIC INTERNAL LEAK CHECK WHICH CHECKED GOOD. PERFORMED CONTINUITY CHECK THAT CHECKED GOOD. THE GREEN HYD SYSTEM LOW PRESS AND HIGH PRESS FILTERS WERE REMOVED AND REPLACED. NO DEBRIS WAS FOUND IN EITHER FILTER.

Part: FMU — FAILED (NR 2 ENGINE) · airframe 36,370 hrs · 16,950 cycles

SEA - ABORTED TAKEOFF - 4/2/01 - NR 2 ENGINE FLAMEOUT. ON TAKEOFF AFTER SETTING TAKEOFF POWER AND ABOUT 60 KTS THERE WAS A SURGE ON NR 2 ENGINE AND IT SHUT DOWN; THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. THE POST FLIGHT REPORT FAULTED THE NR 2 ENGINE FUEL METERING UNIT (FMU); MAINTENANCE PERFORMED BITE CHECKS ON THE NR 2 ENGINE FADEC & EEC W/ NO FAULTS REPORTED. MAINTENANCE REPLACED THE NR 2 ENGINE FMU IAW AWA TASK CARD RSM71304; ENGINE RUNS AND FUNCTIONAL CHECKS WERE GOOD.

Part: ELEVATOR — DAMAGED (RT ELEVATOR) · airframe 3,614 hrs · 16,876 cycles

ON REMOVAL OF RT ELEVATOR ABNORMAL SHEAR LOAD NOTED ON ELEVATOR ATTACH BOLTS AND ELEVATOR HINGE BEARINGS FOUND TO BE MISALIGNED. COMPLIED WITH AWA ER 26-5552-01054-DL2; ELEVATOR REPLACED IAW AMM 27-34-41-401.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 3,614 hrs · 16,876 cycles

NR 4 SEAT TRACK AT FR 20 CORRODED, -0Y1292 -Z500. FABED SEAT TRACK IAW DWG D53112092; INSTALLED IAW SRM 53-11-14.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 3,614 hrs · 16,876 cycles

NR 3 SEAT TRACK AT FR 20 CORRODED, -Y765-Z500. FABED SEAT TRACK IAW DWG D53112092; INSTALLED IAW SRM 53-11-14.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 35,804 hrs · 16,734 cycles

SEVERAL EMERGENCY LIGHTS INOP WITH EMERGENCY LIGHTS ACTIVATED. REPLACED POWER SUPPLY; OPS CHECKED GOOD

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 35,196 hrs · 16,513 cycles

EMERGENCY LANDING, BLUE SYS HYDRAULIC PRESS WENT TO ZERO PSI. REMOVED AND REPLACED BLUE SYS HYD PUMP.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 32,997 hrs · 15,364 cycles

C-CHECK, PREVIOUS REPAIRS TO THE LOWER SKIN SURFACE OF THE RIGHT I/B FLAP DISBONDING. REPAIRED IAW A320 SRM 51-77-11, 57-52-00 PARA 8N STEP 4, 57-52-00 PARA 8Q FIG 213 SHEET 3 AND AWA ER 26-5752-00266JSZ.

Part: FLOOR SUPPORT — CORRODED (Y254LH FR20-17)

CORROSION AROUND A NUT HOLES B/T FR 20-17. FABRICATED AND INSTALLED FLOOR SUPPORT PER DWG NR D53112087 AND SRM 51-42-00, SRM 51-72-00.

Part: TRACK — CORRODED (Y189 RH FR20)

FLOOR PANEL SUPPORT RT 189 FR 20 CORRODED. FABRICATED NEW PART PER DWG D 53112613200. INSTALLED PER SRM 51-72-11, AND SRM 51-42-11.

Part: SUPPORT — CORRODED (Y1732RH FR 65-66)

CORROSION RT FLOOR SUPPORT Y1732 BTWN FR 65-66, CORROSION AROUND CLIP. NUT HOLES (TOP AND BOTTOM). REPLACED BEAM AS PER DWG NR D534772075001 AND INSTALLED IAW A-320 SRM 51-72-11.

Part: SUPPORT — CORRODED (BS 765)

CORROSION LEFT AND RIGHT FLOOR SUPPORT Y765 RT BETWEEN FRAMES 66 AND 68, CORROSION AROUND CLIP NUT (TOP AND BOTTOM). REPAIRED RT FLOOR SUPPORT AT FR 68 Y 765 AS PER ER 26-5341-99294-EYI. PRIMED AND PAINTED AS PER SRM 51-75-17-2. REMOVED AND REPLACED DAMAGED LT FLOOR SUPPORT, FABRICATED REPLACEMENTS AND INSTALLED AS PER SRM 51-74-00.

Part: SEAT TRACK — CORRODED (BS 1292)

RT INBD AND OUTBD SEAT TRACKS Y-1292 CORRODED AT FRAME 20. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACKS RT INBD AND OUTBD Y 1292 AS PER DWG NR 53112092205 AND 206 RESPECTIVELY.

Part: SUPPORT FLOOR — CORRODED (Y1292RH @FR66)

CORROSION ON RT FLOOR SUPPORT Y1292 RT AT FR 66. FABRICATED FLOOR SUPPORT PER DWG NR D 53472090 AND INSTALLED AS PER SRM 51-42-11.

Part: SERVO — FAILED (NLG STEERING)

EMERGENCY LANDING, NOSE LANDING GEAR NOT CENTERED UPON LANDING. UPON LANDING IN CMH, ACFT LANDED WITH THE NOSE GEAR 90 DEG FROM CENTERLINE AXIS. LEFT AND RIGHT NOSE WHEEL TIRE ASSEMBLIES DAMAGED. REMOVED AND REPLACED STEERING SERVO CONTROL, REMOVED AND REPLACED LEFT AND RIGHT NOSE WHEEL TIRE ASSEMBLIES. PERFORMED DETAILED VISUAL INSPECTION OF NOSE LANDING GEAR. CHECKED BARREL/DRAG STRUT CONNECTION. ALL INSPECTIONS CHECK GOOD.

Part: RELAY — FAILED (RAM AIR TURBINE)

RAM AIR TURBINE DEPLOYED ON ITS OWN ON CLIMBOUT. FOUND BOTH RELAYS 17XE AND 18 XE BAD, REPLACED BOTH. PERFORMED RAT AUTO DEPLOYMENT AND INSPECTION PER AWA TASK CARD NR F2C29301, STEP 3, FUNCTION TEST GOOD.

Part: CONNECTOR — DISCONNECTED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 26 EMERGENCY LIGHT INOPERATIVE. RESECURED CONNECTOR TO SIDE WALL. OPS CHECK OK.

Part: O-RINGS — FAILED (BOBBIN ASSY)

CMH - FLT 2031 - AIR TURN BACK DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. FOUND 2 HYDRAULIC LEAKS IN MAIN LANDING GEAR WHEEL WELL. BOTH LEAKS WERE ON THE GREEN HYDRAULIC SYSTEM MANIFOLD. REPLACD O-RINGS ON BOBBIN ASSEMBLY OF GREEN SYSTEM 3-2 WAY VALVE (CENTER MAIN WHEEL WELL). LEAK CHECKS GOOD. SERVICED AS REQUIRED. (M)

Part: WIRE — CUT (CABIN)

LAS - FLT 2085 - DURING ROUTINE MAINTENANCE CHECK, FOUND L-1 DOOR BULKHEAD EMERGENCY EXIT LIGHT INOP. FOUND BULKHEAD/SIDEWALL WIRES CUT. SPLICED TOGETHER. OPS CHECK GOOD. (M)

Part: ACTUATOR — MALFUNCTIONED (RT TE FLAP)

PHX - FLT 2247 - WHEN FLAPS FULL ARE SELECTED ON APPROACH, A HEAVY VIBRATION IS FELT THROUGHOUT THE AIRFRAME. PERFORMED VISUAL INSPECTION PER 27-54-00. NO DEFECTS NOTED AT THIS TIME AND RAN FLAP. NO VIBRATION NOTED AND VISUAL INSPECTION WHILE FLAP MOVED, NO DEFECT. OK FOR SERVICE. AIRCRAFT VIBRATION FELT WHEN FLAPS SELECTED FULL IN AIRSPEED RANGE 140-170 KIAS. REMOVED AND REPLACED NR 1 RIGHT FLAP ACTUATOR IAW 27-54-49, PG 401-421. OPS CHECK GOOD. AIRCRAFT SHAKES NOTICEABLE AT FLAPS FULL POSITION (TEST FLT). REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR ASSEMBLY PER AMM 27-54-49, PGS 401-408. OPS CHECK GOOD. TEST FLT COMPLETED. NO ABNORMAL VIBRATION NOTED BY MAINTENANCE. REFERENCE AWXA960406.

Part: ACTUATOR — MALFUNCTIONED (RT TE FLAP)

PHX - FLT 2247 - WHEN FLAPS FULL ARE SELECTED ON APPROACH, A HEAVY VIBRATION IS FELT THROUGHOUT THE AIRFRAME. PERFORMED VISUAL INSPECTION PER 27-54-00. NO DEFECTS NOTED AT THIS TIME AND RAN FLAP. NO VIBRATION NOTED AND VISUAL INSPECTION WHILE FLAP MOVED, NO DEFECT. OK FOR SERVICE. AIRCRAFT VIBRATION FELT WHEN FLAPS SELECTED FULL IN AIRSPEED RANGE 140-170 KIAS. REMOVED AND REPLACED NR 1 RIGHT FLAP ACTUATOR IAW 27-54-49, PG 401-421. OPS CHECK GOOD. AIRCRAFT SHAKES NOTICEABLE AT FLAPS FULL POSITION (TEST FLT). REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR ASSEMBLY PER AMM 27-54-49, PGS 401-408. OPS CHECK GOOD. TEST FLT COMPLETED. NO ABNORMAL VIBRATION NOTED BY MAINTENANCE. (M)

Part: SEAL — FAILED (LT WING ROOT)

LAS - FLT 0146 - ABORTED TAKEOFF. LOW SPEED REJECT FOR AIR LEAK AT LEFT WING. LEAK CHECKED, BLED SYSTEM, AND FOUND BAD SEAL AT SLIP JOINT JUST INBOARD OF WING ROOT. REPLACED SEAL. LEAK CHECK GOOD. (X)

Part: BLEED VALVE — MALFUNCTIONED (NR 1)

CMH - FLT 0266 - BOTH NR 1 AND NR 2 BLEED VALVES FAILED IN-FLIGHT. EMERGENCY DESCENT. ALL CABIN OXYGEN MASKS DROPPED. PERFORMED BLEED SYSTEM INSPECTION ON BOTH ENGINES PER SIL 36-034 AND RAN ENGINES. NO DEFECTS NOTED. REPLACED ALL OXYGEN MASKS EXCEPT ALL LAVS, ROWS 12, 21, 24, AND 25 RIGHT TO 10 AND 17 LEFT. NR 2 BLEED WAS ON MEL 36-11-07, WHEN PILOT INADVERTENTLY SELECTED ENGINE ANTI-ICE WITHOUT TURNING 1 PACK OFF, THUS CAUSING BLEED FAILURE. (X)

Part: SEAT TRACK — CORRODED (BS 265)

PHX - DURING SCHEDULED C4 INSPECTION, FOUND SEAT TRACK ON RAIL AT 265 BETWEEN FRAME 20 AND FRAME 21 CORRODED. REPAIRED PER SRM 51-72-11. (M)

Part: RAIL — CORRODED (FR 20)

PHX - DURING SCHEDULED C4 INSPECTION, FOUND RAIL AT MINUS 254 FRAME 20 CORRODED. REPAIRED PER SRM 53-11-14. (M)

Part: HANDLE CASTING — CRACKED (FWD CARGO DOOR)

PHX - DURING SCHEDULED C4 CHECK, FOUND FORWARD CARGO DOOR HANDLE MOUNTING CASTING CRACKED. REMOVED AND REPLACED CASTING PER SRM 51-72-11. (M)

Part: SEAT TRACK — CORRODED (FR 20)

PHX - DURING SCHEDULED C4 INSPECTION, FOUND SEAT TRACK ON RAIL AT MINUS 1292 BETWEEN FRAME 20 AND FRAME 21 CORRODED. REPAIRED PER SRM 51-72-11. (M)

Part: SKIN — DAMAGED (FRAME 60-61)

PHX - DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN DAMAGED BETWEEN FRAME 60 AND FRAME 61, INBOARD OF STRINGER 43 RT. FABRICATED FILLER/DOUBLER REPAIR PER SRM 53-00-11. (M)

Part: RAIL — CORRODED (FR 16)

PHX - DURING SCHEDULED C4 INSPECTION, FOUND RAIL AT MINUS 1292 BETWEEN FRAME 16 AND FRAME 20 CORRODED. REPAIRED PER SRM 51-72-11. (M)