N725UW

Part: O-RING — LEAKING (ZONE 100) · airframe 67,787 hrs · 40,773 cycles

AIRCRAFT WAS GROUNDED: YELLOW HYD SYS RSV LOW. AIR INTERRUPTED BACK TO PHL. NO EMERGENCY DECLARED. THE AIRCRAFT WAS NOT OVERWEIGHT FOR LANDING. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BAD O-RING/FITTING CRACKED AT ALT BRAKE DISTRIBUTION DUALVALVE. REPLACED FITTING AND O-RING PER AMM 32-43-14.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 66,263 hrs · 39,795 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHTS AT SEAT 23C NOT TURNING ON PER A-CHECK INSPECTION. REMOVED AND REPLACED SEATS 23C EMERGENCY LIGHTS PER AMM 33-51-18.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 66,263 hrs · 39,795 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHTS AT SEAT 22C NOT TURNING ON PER A-CHECK INSPECTION. REMOVED AND REPLACED SEATS 22C EMERGENCY LIGHTS PER AMM 33-51-18.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 66,263 hrs · 39,795 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHTS AT SEAT 27C NOT TURNING ON PER A-CHECK INSPECTION. REMOVED AND REPLACED SEATS 27C EMERGENCY LIGHTS PER AMM 33-51-18.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 66,163 hrs · 39,738 cycles

AIRCRAFT WAS NOT GROUNDED: R2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.

Part: O-RING — DAMAGED (HYD SYSTEM) · airframe 64,968 hrs · 38,933 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INTO ORD DUE TO THE FLIGHT CREW REPORTING A YELLOW HYDRAULIC SYSTEM RESERVOIR LOW LEVEL ECAM MESSAGE DURING FLIGHT. AIRCRAFT LANDED SAFELY AT ORD WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE PTU MANIFOLD QUICK DISCONNECT FITTING O-RING DAMAGED AND LEAKING HYDRAULIC FLUID. REPLACED O-RING AND ACCOMPLISHED A SATISFACTORY LEAK CHECK PER AMM 29-13-15.

Part: IDG — FAULTED (NR 1 GENERATOR) · airframe 64,012 hrs · 38,307 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW: AFTER TAKE OFF #1 GENERATOR FAULT. DISPLAYED AND THE #1 GENERATOR WOULD NOT RE-SET. THE FLIGHT CREW ALSO REPORTED RECIEVING A LOW OIL PRESSURE ECAM FOR THE #1 IDG AND THEY DISCONNECTED THE IDG. THE AIRCRAFT LANDED SAFELY AT DFW AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE REPLACED THE #1 ENGINE IDG AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER AMM 24-21-51.

Part: BATTERY — FAULTED (EMERGENCY LIGHTS) · airframe 63,995 hrs · 38,297 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT TEST ON PTP FAULTS EMERGENCY POWER SUPPLY UNIT BATTERY FORWARD AND AFT LEFT. REMOVED AND REPLACED THE FORWARD (AALA202404080297) AND AFT EMERGENCY LIGHT BATTERIES.

Part: BATTERY — FAULTED (EMERGENCY LIGHTS) · airframe 63,995 hrs · 38,297 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT TEST ON PTP FAULTS EMERGENCY POWER SUPPLY UNIT BATTERY FORWARD AND AFT LEFT. REMOVED AND REPLACED THE FORWARD AND AFT (AALA202404080403) EMERGENCY LIGHT BATTERIES.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 63,995 hrs · 38,297 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT AFT DOOR ASSIST BOTTLE PRESSURE LOW 1500 PSI AT 65 DEGREES. SERVICED RIGHT AFT DOOR ASSIST BOTTLE PRESSURE TO CORRECT PRESSURE.

Part: LATCH — DISENGAGED (ZONE 800 - DOORS) · airframe 63,255 hrs · 37,870 cycles

AIRCRAFT WAS NOT GROUNDED: 1L FWD ENTRY DOOR HOLD OPEN LATCH NOT ENGAGING. MAINTENANCED CLEANED AND LUBED 1L FWD ENTY DOOR HOLD OPEN LATCH MECHANISM. LATCH ENGAGING NORMAL, REF GPM 17.11.4.

Part: DAMPER — LOW PRESSURE (ZONE 800 - DOORS) · airframe 63,029 hrs · 37,737 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: DOOR 2L BOTTLE ASSIST BOTTLE PRESSURE LOW. PERFORMED CHARGING PRESSURE DOOR 2L BOTTLE.

Part: FITTING — NONE (ZONE 200 - FUSE) · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 2 AT Y0 NEEDS TO BE REPLACED AS PART OF THE MAJOR REPAIR BEING ACCOMPLISHED ON EA 347153 AND REPAIR INSTRUCTION R53112919004 ISSUE F. MAINTENANCE REPLACED CONTINUITY FITTING PER EA 347153 AND REPAIR INSTRUCTION R53112919004 ISSUE F.

Part: SEAL DEPRESSOR — CRACKED (ZONE 200 - FUSE) · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND AFT PASSENGER / CREW DOOR CUTOUT UPPER PLATE / SEAL DEPRESSOR CRACKED AT FR 67 AND S8L. REPLACED UPPER PLATE / SEAL DEPRESSOR PER SRM 51-42-11.

Part: HANDLE — CRACKED (ZONE 200 - FUSE) · airframe 63,029 hrs · 37,737 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK RIGHT HAND SLIDING WINDOW HANDLE CRACKED. REPLACED HANDLE PER CMM 56-12-12.

Part: HANDLE — CRACKED (ZONE 200 - FUSE) · airframe 63,029 hrs · 37,737 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK LEFT HAND SLIDING WINDOW HANDLE CRACKED. REPLACED HANDLE PER CMM 56-12-12.

Part: BOLT — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #9 LOWER BOLT BETWEEN WS 10201 AND WS 10729, BETWEEN RIBS 19 AND 20. REPLACED BOLT PER AMM 27-84-65.

Part: BOLT — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #7 UPPER BOLT BETWEEN WS 7316 AND WS 7792, BETWEEN RIBS 13 AND 14. REPLACED BOLT PER AMM 27-84-63.

Part: DAMPER — NO TEST (ZONE 800 - DOORS) · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: PASSENGER CREW DOOR 832 DOOR DOOR DAMPER AND EMERGENCY OPERATION CYLINDER FAILED DAMPING FUNCTIONAL TEST. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-13-14. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: GAUGE — GLAZED (ZONE 800 - DOORS) · airframe 63,029 hrs · 37,736 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE GUAGE IS GLAZED. **SUPPLEMENTAL REPORT FOR AALA202308292564: REPLACED DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14.** (CLOSED)

Part: GAUGE — GLAZED (ZONE 800 - DOORS) · airframe 63,029 hrs · 37,736 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 DAMPER AND OPERATIONAL OPERATION CYLINDER PRESSURE GUAGE IS GLAZED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: DAMPER — NO TEST (ZONE 800 - DOORS) · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: PASSENGER CREW DOOR 842 DAMPER AND EMERGENCY OPERATION CYLINDER FAILED DAMPING FUNTIONAL CHECK. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-13-14 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: STRINGER — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER BETWEEN FR 56 AND FR 57 AT S43L. REPAIRED STRINGER PER SRM 53-41-13-283-002.

Part: FITTING — NONE (ZONE 200 - FUSE) · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: AS PART OF THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK WINDSHIELD FRAMING THE LEFT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 2 AT Y0 NEEDS TO REPLACED PER EA 347153 AND REPAIR INSTRUCTION R53112919004 ISSUE F. REPLACED LEFT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 2 AT Y0 NEEDS TO REPALCED PER EA 347153 AND REPAIR INSTRUCTION R53112919004 ISSUE F.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 - STABS) · airframe 63,028 hrs · 37,736 cycles

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

Part: FLOORBEAM — CORRODED (ZONE 100 - FUSE) · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CABIN FLOOR BEAM INOARD SPLICE HAS ELONGATED / WORN HOLE AT FR 24 AND +Y1292. REPLACED SPLICE PER SRM 51-72-11.

Part: FLOORBEAM — WORN (ZONE 100 - FUSE) · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CABIN FLOOR BEAM OUTBOARD SPLICE HAS ELONGATED / WORN HOLE AT FR 24 AND +Y1292. REPLACED SPLICE PER SRM 51-72-11.

Part: SPLICE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM INBOARD SPLICE COUPLING AT FR 64 AND -Y765. REPLACED SPLICE COUPLING PER SRM 51-72-11.

Part: FITTING — CRACKED (ZONE 800 - DOORS) · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED LEFT HAND MAIN LANDING GEAR DOOR FORWARD FITTING. REPLACED FITTING PER CMM 52-81-18.

Part: STRINGER — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING DRY BAY STRINGER 3 BETWEEN RIB 5 AND RIB 6. REPAIRED STRINGER PER EA 348171.

Part: SEAT TRACK — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR SEAT TRACK AT FR 20 AND -Y765. REPLACED SEAT TRACK PER SRM 51-42-11-801.

Part: FLOOR SUPPORT — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM BETWEEN FR 12 AND FR 24 AT -Y254. REPLACED FLOOR BEAM PER SRM 51-42-11-801.

Part: SEAT TRACK — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN BEAM-SEAT TRACK AT FR 16 AND +Y1292. REPLACED BEAM-SEAT TRACK PER SRM 51-72-11.

Part: SEAT TRACK — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR SEAT TRACK BETWEEN FR 20 AND FR 21 AT -Y1292. REPLACED SEAT TRACK PER SRM 51-42-11-801.

Part: FRAME — CRACKED (ZONE 200 - FUSE) · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME WEB AFT FACE UPEER RADII AT FR 68 AT S8L. REPAIRED FRAME PER EA 347592.

Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK ON SHEAR PLATE BETWEEN FR 69 AND FR 70 AT STR 23L. REPLACED SHEAR PLATE PER SRM 51-42-11-801.

Part: WINDOW FRAME — CRACKED (ZONE 200 - FUSE) · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND WINDSHIELD FRAME CENTER LOWER POST ATTACHMENT LOWER RADIUS AT FR 2. REPAIRED FRAME PER EA 347153.

Part: WINDOW FRAME — CRACKED (ZONE 200 - FUSE) · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED LEFT HAND WINDSHIELD FRAME CENTER LOWER POST ATTACHMENT UPPER TENSION BOLT AT FR 2. REPAIRED FRAME PER EA 347153.

Part: FLOOR SUPPORT — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR LONGITUDINAL BEAM BETWEEN FR 64 AND FR 65 AT -Y465. REPLACED LONGITUDINAL BEAM PER SRM 51-72-11.

Part: SEAT TRACK — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM-SEAT TRACK AT FR 66 AND +Y765. REPLACED BEM-SEAT TRACK PER SRM 51-72-11.

Part: FLOORBEAM — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM AT FR 66 AND +Y1292. REPLACED FLOOR BEAM PER SRM 51-72-11.

Part: WINDOW FRAME — CRACKED (ZONE 200 - FUSE) · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND WINDSHIELD FRAME CENTER LOWER POST ATTACHMENT UPPER TENSION BOLT AT FR 2. REPAIRED FRAME PER EA 347153.

Part: SEAT TRACK — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM-SEAT TRACK AT FR 66 AND -Y765. REPLACED BEAM-SEAT TRACK PER SRM 51-72-11.

Part: CHANNEL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT ANTENNA SUPPORT CHANNEL BETWEEN FR 59 AND FR 60, BETWEEN S42L AND S43L. REPLACED CHANNEL PER SRM 51-42-11.

Part: FRAME — CRACKED (ZONE 200 - FUSE) · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME WEB HORIZONTAL FLANGE AT FR 68 AND S22L. REPAIRED FRAME PER EA 347443.

Part: FITTING — CRACKED (WINDOW FRAME) · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING LOWER FRONT FITTING LEFT HAND SIDE OUTBOARD END IS CRACKED AT FR 4, FROM Y0 TO Y511. REPLACED FITTING PER EA 347614.

Part: SKIN — CORRODED (ZONE 500 - LH WI) · airframe 63,028 hrs · 37,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TOP SKIN FROM RIB 18 TO RIB 19. EVALUATED BLENDED AREA LOCATED REAR SPAR TOP SKIN LOWER SURFACE BTW RIB 18 TO RIB 19 ON LEFT WING AND FOUND WITHIN LIMITS IAW SRM 57-21-11-283-026 PARAGRAPH 2 A SHEET 07 FIGURE 005.

Part: GIRT BAR — LACK OF LUBE (ZONE 800 - DOORS) · airframe 61,560 hrs · 36,848 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR DIFFICULT TO ARM., VERY RESISTANT TO MOVEMENT AND MUST BE SMASHED DOWN TO INDICATE ARMED ON FLIGHT DECK DOOR PAGE MAINTENANCE REMOVED DEBRIS FROM FLOOR GIRT BAR RECEPTICLES AND LUBED GIRT BAR AS REQUIRED.. DOOR ARMS OK WITH NORMAL FORCE REQUIRED PER AMM 52-11-00-820-001-A.

Part: DETECTOR — DEFECTIVE (ZONE 800 - DOORS) · airframe 60,617 hrs · 36,222 cycles

AIRCRAFT WAS NOT GROUNDED: 2L SLIDE INDICATION FLICKERS, FLIGHT ATTENDANT VERIFIED SLIDE IS ARMED. MAINTENANCE REPLACED ARMING HANDLE PROXIMITY DETECTOR 17WV1I PER AMM 52-71-11 A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: COMPUTER — INOPERATIVE (FLT MANAGEMENT) · airframe 57,179 hrs · 34,289 cycles

AIRCRAFT WAS GROUNDED: AFTER TAKEOFF, AUTO THRUST ECAM-AUTO THRUST TEMPORARILY INOPERATIVE THEN RESET AND ABLE TO RE-ENGAGE. AIR INTERRUPT ACCOUNT OF #1 FLIGHT MANAGEMENT AND GUIDANCE COMPUTER/#2 DME INOPERATIVE AND 32 DME ID FLASHING INTERMITTENTLY. ON APPROACH, VLS DISPLAYED 8KTS HIGHER THAN COMPUTED BY FLIGHT MANAGEMENT AND GUIDANCE COMPUTER. REPLACED #1 FLIGHT MANAGEMENT AND GUIDANCE COMPUTER CHECKS. OK FOR SERVICE PER AMM 22-83-34.

Part: GIRT BAR — LACK OF LUBE (DOOR) · airframe 56,660 hrs · 33,993 cycles

AIRCRAFT WAS NOT GROUNDED: SLIDE WILL NOT STAY ARMED. CLEANED GIRT BAR RECEPTICAL LATCHES AND LUBED.

Part: APU — LEAKING (APU BAY) · airframe 54,140 hrs · 32,320 cycles

AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS SMOKE SMELL IN A/C CABIN. MAINTENANCE ACCOMPLISHED CARD 26L0002101 ODOR CARD FOUND APU TO BE AT FAULT. REPLACED APU IAW JOB CARD 26L31049003.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 53,475 hrs · 31,907 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS WHILE ACCOMPLISHING CARD 26L00025011 INSTALL OF SLIDE PACK, TEST FOR EMER SYS FAULT EPSU INT LEFT, COULD NOT RESET. REPLACED LEFT EPSU AND BATTERY, REPLACED FWD EPSU BATTERY IAW AMM 33-51-38. OPS TEST OK IAW AMM 33-51-00. (SEE SDR # AALA201907059028)

Part: BATTERY — DISCHARGED (CABIN) · airframe 53,475 hrs · 31,907 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS WHILE ACCOMPLISHING CARD 26L00025011 INSTALL OF SLIDE PACK, TEST FOR EMER SYS FAULT EPSU INT LEFT, COULD NOT RESET. REPLACED LEFT EPSU AND BATTERY, REPLACED FWD EPSU BATTERY IAW AMM 33-51-38. OPS TEST OK IAW AMM 33-51-00. (SEE SDR # AALA201907059023)

Part: SLIDE RAFT — SWOLLEN (L1 DOOR) · airframe 53,475 hrs · 31,907 cycles

AIRCRAFT WAS GROUNDED: FA REPORTS THAT DOOR L1 VERY DIFFICULT TO DELATCH AND CLOSE. MAINTENANCE REPORTS SLIDE HAS SWELLED TO THE POINT THE GUST LOCK NO LONGER LOCKS. REMOVED AND REPLACED L1 SLIDE/RAFT ASSEMBLY IAW CARD 26L00025011. DOOR OPS CHECK GOOD.

Part: ADIRU — FAULTED (NR 1) · airframe 53,425 hrs · 31,877 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS DURING DESCENT, ONE TIME FOR ABOUT A SECOND, BOTH CAPT AND FO PFD AIRSPEED AND ALTITUDE FLUCTUATED WILDLY THEN RETURNED TO NORMAL. STATUS MSG THEN SHOWED CAT I ONLY. MAINTENANCE POST FLT REVIEW FOUND ADIRU1 INTERMITTENT FAULT. ACCOMPLISHED SYSTEM TEST OF ADIRU1 IAW AMM 34-13-00. ACCOMPLISHED OPERATIONAL TEST OF LAND CAT III SYSTEM IAW AMM 22-97-00. ALL TESTS PASSED.

Part: BOLT — EXCESS PLAY (PAX DOOR) · airframe 53,277 hrs · 31,782 cycles

AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS DOOR 2 HARD TO MOVE AND MAKES GRINDING NOISE. UPPER AND LOWER PIVOT BOLTS HAS PLAY. LUBRICATED UPPER AND LOWER HINGE BOLT AND ATTACH FITTINGS. NO PLAY IN THE BOLTS NOTED DURING FUNCTIONAL CHECK OF DOOR SUSPENSION IAW AMM 52-10-00-720-001.

Part: COMPUTER — FAULTY (FUEL SYSTEM) · airframe 53,134 hrs · 31,693 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS FUEL L OUTER XFER OPEN R OUTER XFER OPEN ON ECAM INOP SYS L CELL VALVE R CELL VALVE INDICATION OCCURRED ON DESCENT. MAINTENANCE REMOVED AND REPLACED FQIC IAW AMM 28-42-34. OPS CHECK GOOD.

Part: PIN — CORRODED (LT MLG) · airframe 51,506 hrs · 30,702 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT MAIN LANDING GEAR AFT ATTACHMENT PINTLE PIN. REPLACED PINTLE PIN PER TASK CARD 26T00032001.

Part: LENS — DETACHED (EMERGENCY EXIT) · airframe 50,619 hrs · 30,130 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY DOOR SLIDE LENS FELL OFF. RESECURED EMERGENCY EXIT DOOR SLIDE LENS. CHECKS OK PER AMM 33-50-00.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 49,885 hrs · 29,683 cycles

AIRCRAFT WAS NOT GROUNDED. FORWARD FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT DOES NOT TEST. REMOVED AND REPLACED BATTERY.

Part: SLIDE — INOPERATIVE (L1 DOOR) · airframe 49,295 hrs · 29,333 cycles

AIRCRAFT WAS GROUNDED. L1 DOOR SLIDE WILL NOT ARM. REPLACED L1 DOOR SLIDE PER JOB CARD NO 26L00025011.

Part: LENS — MISSING (CABIN) · airframe 49,035 hrs · 29,152 cycles

L2 DOOR AREA LIGHT LENS COVER MISSING. RE-INSTALLED L2 DOOR LIGHT LENS.

Part: SEAT TRACK — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 48,842 hrs · 29,004 cycles

CORROSION ON LEFT SIDE OF THE SEAT TRACK AT Y765, BETWEEN FRAMES 64 AND 66. REPLACED THE SEAT TRACK IAW SRM 51-72-11, SRM 51-42-11, SRM 51-75-12, AND DRAWING D53472000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · airframe 48,842 hrs · 29,004 cycles

CORROSION ON AFT SECTION OF THE FLOOR SUPPORT AT -Y1162.5, BETWEEN FRAMES 68 AND 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DRAWINGS D53480019, AND D53474180.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,842 hrs · 29,004 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT SECTION OF FLOORBEAM AT -Y1162.5 JUST FORWARD OF FR 68. REPLACED SPLICE PER SRM 51-72-11, AND DRAWINGS D53480019 AND D53474180.

Part: ELEVATOR — DELAMINATED (LEFT) · airframe 48,842 hrs · 29,004 cycles

LEFT HAND ELEVATOR IS DELAMINATED BEYOND SERVICEABLE LIMITS. REPLACED LEFT HAND ELEVATOR PER JOB CARD 26L30027001.

Part: FITTING — CRACKED (FRAMES 1-2) · airframe 48,842 hrs · 29,004 cycles

CRACK ON NOSE FUSELAGE WINDSHIELD FRAME LT CONTINUITY FITTING, BL 0, BETWEEN FRAMES 1 AND 2. REPAIRED THE CONTINUITY FITTING IAW EA 272404.

Part: FLOORBEAM — CORRODED (FRAME 16) · airframe 48,842 hrs · 29,004 cycles

CORROSION ON FLOORBEAM AT LBL 11 AND FRAME 16. REPLACED THE FLOORBEAM IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 64-66) · airframe 48,842 hrs · 29,004 cycles

CORROSION FOUND ON THE SEAT TRACK AT LBL 49.5, BETWEEN FRAMES 64 AND 66. REPLACED THE SEAT TRACK IAW SRM 51-42-11.

Part: SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 48,842 hrs · 29,004 cycles

CORROSION FOUND ON THE RIGHT AFT SUPPORT PLATE AT -Y1732 AND STRINGER 23R, BETWEEN FRAMES 66 AND 68. REPLACED SUPPORT PLATE IAW SRM 51-72-11 AND DRAWING 534805000.

Part: PRESSURE SWITCH — FAILED (FUEL BOOST) · airframe 47,754 hrs · 28,343 cycles

FUEL BOOST PUMP INOPERATIVE. REMOVED AND REPLACE THE BOOST PUMP PRESSURE SWITCH.

Part: PROXIMITY SENSOR — FAULTED (MLG) · airframe 47,118 hrs · 27,922 cycles

AFTER TAKE OFF, ECAM MESSAGE, LANDING GEAR CONTROL INTERFACE UNIT 2, FAULT. NO EMERGENCY WAS DECLARED AND NORMAL LANDING WAS MADE. AIRCRAFT WAS GROUNDED. REPLACED PROXIMITY SENSOR (29GA) IAW AMM 32-31-00.

Part: WINDOW SHADE — INOPERATIVE (CABIN) · airframe 46,625 hrs · 27,566 cycles

AIRCRAFT WAS NOT GROUNDED. WINDOW SHADE AT EMERGENCY EXIT ROW 14 WILL NOT OPEN. REPLACED WINDOW SHADE PER AMM 25-23-47.

Part: LIGHT — LOOSE (CABIN) · airframe 46,434 hrs · 27,435 cycles

AIRCRAFT WAS NOT GROUNDED, EMERGENCY EXIT LIGHT ON FORWARD LT CLOSET HAS COME LOOSE. SECURED EMERGENCY EXIT LIGHT.

Part: LENS — MISSING (ZONE 200) · airframe 46,350 hrs · 27,381 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 33-51-18.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 45,090 hrs · 26,618 cycles

AIRCRAFT IN BASE MX. RT SIDE BOX BEAM UPPER FLANGE, HAS CRACK INDICATIONS, AT THE AFT TWO HOLES AT FRAME 43 & -Y1622. REPAIRED BOX BEAM IAW EO 5315Y066.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 45,090 hrs · 26,618 cycles

AIRCRAFT IN BASE MX. LT SIDE BOX BEAM, UPPER FLANGE FWD & AFT HOLES HAVE CRACK INDICATION AT FRAME 43 & Y1622. REPAIRED IAW EO 5315Y066.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 42,664 hrs · 25,111 cycles

EMERGENCY LIGHTS EPSU BATTERY FAULT ON CIDS PANEL. REPLACED EPSU 11WL BATTERY.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 41,807 hrs · 24,600 cycles

DELAMINATION ON AFT CARGO FLOOR PANEL 151VG AT FRAME 53 BETWEEN STRINGER 35L TO 35R, Z-150. REPLACED AFT CARGO FLOOR PANEL 151VG IAW AMM 53-42-14 PB 401.

Part: SLIDE RAFT — DEFECTIVE (L1 DOOR) · airframe 41,520 hrs · 24,415 cycles

C11 CHECK L1 SLIDE & RAFT HITTING FUSELAGE WHEN LOCKED IN THE FULL OPEN POSITION. INSTALLED NEW L1 SLIDE & RAFT IAW JOB CARD 26L00025011.

Part: SLIDE — DEFECTIVE (R2 DOOR) · airframe 41,520 hrs · 24,415 cycles

C11 CHECK R2 SLIDE DECORATIVE COVER CONTACTING FUSELAGE WITH DOOR LOCKED IN FULLY OPEN POSITION. INSTALLED NEW AFT SLIDE RAFT IAW JOB CARD 26L00025011.

Part: POWER SUPPLY — FAULTED (CABIN) · airframe 41,327 hrs · 24,292 cycles

DURING SCHEDULED TIME CHANGE OF LT ESCAPE SLIDE OFF WING RAMP, MX REPORTED A FAULT DURING OPERATIONS CHECK OF EMER LIGHT SYS. R & R LT EPSU IAW AMM 33-51-38-000-001-A & 33-51-38-400-001-A.

Part: BUSHING — CORRODED (RUDDER) · airframe 41,231 hrs · 24,207 cycles

RON RUDDER NR 7 BEARING BUSHING PITTED, HINGE BEARING. INSTALLED SERVICEABLE BUSHING IAW AMM 55-36-41.

Part: BUSHING — CORRODED (RUDDER) · airframe 41,231 hrs · 24,207 cycles

RON RUDDER NR 1 BEARING, BUSHING PITTED. INSTALLED SERVICEABLE BUSHING FOR RUDDER NR 1 POS BEARING IAW AMM 55-36-41.

Part: BOLT — PEELING (RUDDER) · airframe 41,231 hrs · 24,207 cycles

RON RUDDER NR 4 BEARING, BOLT PLATING PEELING. INSTALLED SERVICEABLE BOLT FOR NR 4 POS RUDDER ATTACH BOLT IAW AMM 55-36-41.

Part: BUSHING — CORRODED (RUDDER)

RON RUDDER NR 3 BEARING, BUSHING PITTED. INSTALLED SERVICEABLE BUSHING AT RUDDER NR 3 BEARING POS IAW AMM 55-36-41.

Part: HINGE — DAMAGED (HYDRAULIC DOOR) · airframe 40,942 hrs · 24,037 cycles

CLIMBING OUT SPEED 300 KNOTS, ALT BETWEEN 14000'-25000', CREW REPORTED A STRONG VIBRATION. FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. COMPLIED WITH TSM TASK 05-50-00-810-801-A, 27-30-00-810-850-A, 32-20-00-810-803-A, 52-13-00-810-826-A & 53-35-00-810-801-A. FOUND BLUE HYD ACCESS PANEL TWEAKED. REPLACED PANEL HINGES.

Part: DOOR — OUT OF SEQUENCE (CABIN) · airframe 40,674 hrs · 23,882 cycles

THE 1L DOOR SLIDE ARMED BUT STILL INDICATING OPEN. PINNED DOOR BLOW & SLIDE. SEQUENCED DOOR & ARM MECHANISM. DOOR ARMS, OPENS & CLOSES PROPERLY.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 40,285 hrs · 23,671 cycles

THE L1 CABIN DOOR HARD TO CLOSE. LUBED AS NEEDED. OK FOR SERVICE IAW AMM 52-10-00.

Part: UNKNOWN — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 39,870 hrs · 23,367 cycles

CREW REPORTED THE OVERWING EXIT, ACFT LT, EMERGENCY EXIT LIGHT ON AS WELL AS OVERHEAD DURING FLIGHT. PERFORMED CIDS RESET & TEST. OPERATIONS & TEST NORMAL. ALL EMERGENCY LIGHTS OPERATIONS TEST NORMAL ON GND IAW AMM 33-51-00-710-001-A.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 39,616 hrs · 23,192 cycles

THE AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT LED INOPERATIVE. REPLACED BATTERY IN AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT, CHECKED OK.

Part: RESERVOIR — LOW PRESSURE (EVAC SLIDE) · airframe 39,557 hrs · 23,145 cycles

CREW REPORTED A CIDS CAUTION ILLUMINATED. THE RT OVERWING SLIDE RESERVOIR LOW. REPLACED RT OFF WING SLIDE INFLATION RESERVOIR IAW AMM 25-62-46-400-001A. CIDS PANEL CHECKED OK.

Part: TRANSDUCER — FAULTY (ZONE 200) · airframe 39,456 hrs · 23,092 cycles

EN ROUTE FROM PHL TO UVF, CREW REPORTED AN ECAM. F/CTL AILERON SERVO FAULT. FLIGHT RETURNED TO FIELD AT PHL & LANDED WITHOUT INCIDENT. RECEIVED CFDS POST FLIGHT REPORTS. LAST LEG, ELAC 1 OR INPUT OF LT PEDALS TRANSDUCER UNIT 25CE1 FAULTS. TROUBLESHOOTING IAW TSM TASK 27-10-00-810-801-A. R & R LT PEDAL TRANSDUCER UNIT 25CE1 IAW AMM 27-92-15-000-001-A & 27-92-15-400-001-A. GND CHECKS SATISFACTORY. REVIEWED FINDINGS WITH MOC. NO FURTHER FAULTS INDICATED AT THIS TIME.

Part: COVER — BROKEN (CABIN) · airframe 39,210 hrs · 22,934 cycles

CREW REPORTED THE EXIT SIGN FLOOR LEVEL PLASTIC COVER BROKEN, REPLACED COVER.

Part: GARLOCK SEAL — LEAKING (NR 1 ENGINE) · airframe 38,295 hrs · 22,286 cycles

DURING CRUISE, ENROUTE, CREW REPORTED THE LT ENGINE OIL QTY DROPPED TO ZERO. OIL PRESSURE AND TEMPERATURE WAS NORMAL. FLIGHT DIVERTED AND LANDED WITHOUT INCIDENT. MX FOUND THE NR 1 ENGINE IDG GARLOCK SEAL LEAKING. REMOVED IDG AND REPLACED GARLOCK SEAL. REINSTALLED NR 1 IDG. LEAK AND OPS CHECKED OK.

Part: BUSHING — ELONGATED (RT MLG) · airframe 38,264 hrs · 22,269 cycles

RIGHT MLG ACTUATOR BRACKET BUSHING IS OUT OF ROUND. CLEANED AND MACHINED BUSHING IAW EA 205242.

Part: LENS — MISSING (CABIN) · airframe 37,776 hrs · 21,900 cycles

CREW REPORTED 1C EXIT ROW COVER MISSING. MAINTENANCE INSTALLED MISSING LENS AT ROW 1C. OPS CHECK OK.

Part: ACCESS PANEL — OUT OF ADJUST (EVAC RAFT) · airframe 37,234 hrs · 21,555 cycles

MAINTENANCE REPORTED THE FORWARD ENTRY RAFT ACCESS PANEL HARD TO OPEN AND CLOSE. MAINTENANCE REMOVED SHIM FROM HINGE. OPS CHECK NORMAL.

Part: MEGAPHONE — INTERMITTENT (CABIN) · airframe 36,041 hrs · 20,746 cycles

AFT MEGAPHONE INTERMITTENT. REMOVED AND REPLACED AFT MEGAPHONE.

Part: SLIDE RAFT — FAULTY (L2 DOOR)

2S CHECK - BAD FROM STOCK L2 DOOR SLIDE/RAFT FAILS CIDS CHECK. REPLACED L2 DOOR SLIDE/RAFT IAW JOB CARD 26L00025011.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 33,694 hrs · 19,166 cycles

2S CHECK - AFT EMERGENCY LIGHT POWER UNIT HAS UNIT FAULT. REPLACED EMERGENCY POWER SUPPLY UNIT IAW A319 AMM 33-51-38-000-002 & 33-51-38-400-002.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LAV 'A' FLIGHT ATTENDANT SEAT FLASHLIGHT & BRACKET BROKEN. RECEIVED LAV 'A' FLIGHT ATTENDANT SEAT FLASHLIGHT & BRACKET ASSEMBLY. OPS CHECKS GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR68, Y512. REPLACED FLOORBEAM AT FR68, Y512 IAW A319 SRM 53-00-14 & 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR64, -Y512. REPLACED FLOORBEAM AT FR64, -Y512 IAW A319 SRM 53-00-14, 51-42-11 & 51-49-00.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON CORNER SEAL SHAPE FITTING AT FR68, -Y1417. REPLACED CORNER SEAL SHAPE FITTING IAW A319 SRM 51-42-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON R-2 DOOR SILL PLATE AT FR68, -Y1237. REPLACED R-2 DOOR SILL PLATE AT FR68, -Y1237 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR67+6 INCHES BETWEEN Y1162 TO Y1292. REPLACED FLOORBEAM AT FR67+6 INCHES BETWEEN Y1162 TO Y1292 IAW A319 SRM 53-00-14 FIG 102 & 51-49-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR14 TO FR24, -Y81. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y81 IAW A319 SRM 53-11-15 & 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR18 TO FR23, Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y1292 IAW A319 SRM 53-11-15 & 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR19 TO FR24, -Y765. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y765 IAW A319 SRM 51-42-11 & 51-72-11.

Part: PLATE — CORRODED (FUSELAGE) · airframe 33,694 hrs · 19,166 cycles

2S CHECK - CORROSION ON AFT CARGO COVER SHEET (SILL PLATE) BETWEEN FR55 TO FR59. REPLACED AFT CARGO COVER SHEET (SILL PLATE) IAW A319 SRM 51-42-11.

Part: HINGE PIN — CORRODED (NR 5 SPOILER) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 FILIFORM CORROSION ON LEFT WING NR 5 SPOILER OUTBOARD HINGE PIN AT WING RIB 20+11 INCHES. REPLACED LEFT WING NR 5 SPOILER OUTBOARD HINGE PIN IAW A319 AMM 27-64-44-400-001.

Part: HINGE PIN — CORRODED (NR 5 SPOILER) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 FILIFORM CORROSION ON LEFT WING NR 5 SPOILER INBOARD HINGE PIN AT WING RIB 20+1 INCHES. REPLACED LEFT WING NR 5 SPOILER INBOARD HINGE PIN IAW A319 AMM 27-64-44-400-001.

Part: HINGE PIN — CORRODED (LT AILERON) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 FILIFORM CORROSION ON LEFT AILERON NR 5 HINGE PIN AT WING RIB 26+1 INCH. REPLACED LEFT AILERON NR 5 HINGE PIN IAW A319 AMM 27-14-41-400-001.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR67, -Y465. REPLACED FLOORBEAM AT FR67, -Y465 IAW A319 SRM 51-42-11 & 51-49-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64+10 INCHES & FR66, Y1292. REPLACED FLOORBEAM BETWEEN FR64+10 INCHES & FR66, Y1292 IAW A319 SRM 53-00-14 & 51-49-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT RAIL BEAM ASSEMBLY BETWEEN FR64 TO FR66, -Y1292. REPLACED SEAT RAIL BEAM ASSEMBLY BETWEEN FR64 TO FR66, -Y1292 IAW A319 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR70, -Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR70, -Y1292 IAW A319 SRM 51-42-11.

Part: HINGE PIN — CORRODED (NR 3 SPOILER) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 FILIFORM CORROSION ON LEFT WING NR 3 SPOILER INBOARD HINGE PIN AT WING RIB 14+4 INCHES. REPLACED LEFT WING NR 3 SPOILER INBOARD HINGE PIN IAW A319 AMM 27-64-44-400-001.

Part: PANEL — CORRODED (LT WING) · airframe 33,694 hrs · 19,166 cycles

2S CHECK - COUNTERSINKS IN LEFT WING FUEL PANEL 540JB CORRODED & PITTED BETWEEN WS7792 TO WS8268. REPLACED LEFT WING FUEL PANEL 540JB IAW A319 SRM 51-42-11.

Part: PANEL — CORRODED (LT WING) · airframe 33,694 hrs · 19,166 cycles

2S CHECK - COUNTERSINKS IN LEFT WING FUEL PANEL 540LB CORRODED & PITTED BETWEEN WS 8744 TO WS 9235. REPLACED LEFT WING FUEL PANEL 540LB IAW A319 SRM 51-42-11.

Part: PANEL — CORRODED (LT WING) · airframe 33,694 hrs · 19,166 cycles

2S CHECK - COUNTERSINKS IN LEFT WING FUEL PANEL 540MB CORRODED & PITTED BETWEEN WS9235 TO WS9704. REPLACED LEFT WING FUEL PANEL 540MB IAW A319 SRM 51-42-11.

Part: PANEL — CORRODED (LT WING) · airframe 33,694 hrs · 19,166 cycles

2S CHECK - COUNTERSINKS IN LEFT WING FUEL PANEL 550AB CORRODED & PITTED BETWEEN WS11664 TO WS12277. REPLACED LEFT WING FUEL PANEL 550AB IAW A319 SRM 51-42-11.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON PLATE AT AFT END OF DUMMY RAIL AT FR16, -Y1379. REPLACED PLATE AT AFT END OF DUMMY RAIL AT FR16, -Y1379 IAW A319 SRM 51-42-11 FIG 3, 8.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON DUMMY RAIL AT FR14, Y503. REPLACED DUMMY RAIL AT FR14, Y503 IAW A319 SRM 51-42-11.

Part: PANEL — CORRODED (RT WING) · airframe 33,694 hrs · 19,166 cycles

2S CHECK - COUNTERSINKS IN RIGHT WING FUEL PANEL 640LB CORRODED & PITTED BETWEEN WS9235 TO WS9704. REPLACED RIGHT WING FUEL PANEL 640LB IAW A319 SRM 51-42-11.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 FILIFORM CORROSION ON RIGHT SIDE WEB PLATE AT FR21, -Y1743. REPAIRED RIGHT SIDE WEB PLATE AT FR21, -Y1743 IAW A319 SRM 51-72-11.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON DUMMY RAIL BETWEEN FR12 TO FR14, -Y81. REPLACED DUMMY RAIL BETWEEN FR12 TO FR14, -Y81 IAW A319 SRM 51-72-11 & 53-11-14.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BETWEEN FR12 TO FR24, Y254. REPLACED FLOOR SUPPORT BETWEEN FR12 TO FR24, Y254 IAW A319 SRM 51-74-00 FIG 1 & 51-72-11.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON DUMMY RAIL BETWEEN FR20 TO FR24, -Y189. REPLACED DUMMY RAIL BETWEEN FR20 TO FR24, -Y189 IAW A319 SRM 51-72-11 & 51-42-11.

Part: HINGE PIN — CORRODED (NR 4 SPOILER) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 FILIFORM CORROSION ON RIGHT WING NR 4 SPOILER INBOARD HINGE PIN AT WING RIB 17+4 INCHES. REPLACED RIGHT WING NR 4 SPOILER INBOARD HINGE PIN IAW A319 AMM 27-64-44-400-00.

Part: HINGE PIN — CORRODED (NR 2 SPOILER) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 FILIFORM CORROSION ON LEFT WING NR 2 SPOILER OUTBOARD HINGE PIN AT WING RIB 11 +20 INCHES. REPLACED LEFT WING NR 2 SPOILER OUTBOARD HINGE PIN IAW A319 AMM 27-64-42-400-001.

Part: HINGE PIN — CORRODED (NR 1 SPOILER) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 FILIFORM CORROSION ON LEFT WING NR 1 SPOILER INBOARD HINGE PIN AT WING RIB 6+15 INCHES. REPLACED LEFT WING NR 1 SPOILER INBOARD HINGE PIN IAW A319 AMM 27-64-41-400-001.

Part: HINGE PIN — CORRODED (NR 4 SPOILER) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 FILIFORM CORROSION ON RIGHT WING NR 4 SPOILER OUTBOARD HINGE PIN AT WING RIB 17+14.5 INCHES. REPLACED RIGHT WING NR 4 SPOILER OUTBOARD HINGE PIN IAW A319 AMM 27-64-44-400-001.

Part: HINGE PIN — CORRODED (NR 1 SPOILER) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 FILIFORM CORROSION ON LEFT WING NR 1 SPOILER OUTBOARD HINGE PIN AT WING RIB 6+25 INCHES. REPLACED LEFT WING NR 1 SPOILER OUTBOARD HINGE PIN IAW A319 AMM 27-64-41-400-001.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, Y1162. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, Y1162 IAW A319 SRM 53-00-14 FIG 102 & 51-49-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR70, Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR70, Y765 IAW A319 SRM 51-42-11 & 51-49-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON BEAM SEAT RAIL ASSEMBLY AT FR66, -Y765. REPLACED BEAM SEAT RAIL ASSEMBLY BETWEEN FR64 TO FR66, -Y765 IAW A319 SRM 51-42-11 & 51-49-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, Y765 IAW A319 SRM 51-42-11 & 51-49-00.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHAPE SILL PROFILE BETWEEN FR66+7 INCHES TO FR68 - 5 INCHES, Y1882. REPLACED SHAPE SILL PROFILE BETWEEN FR66+7 INCHES TO FR68 - 5 INCHES, Y1882 IAW A319 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, -Y1162. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, -Y1162 IAW A319 SRM 51-74-00.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,694 hrs · 19,166 cycles

2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON LEFT SHEAR PLATE BETWEEN FR69 TO FR70, Y1162. REPLACED LEFT SHEAR PLATE BETWEEN FR69 TO FR70, Y1162 IAW A319 SRM 51-72-11.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 33,694 hrs · 19,166 cycles

2S CHECK - CRACK IN CABIN FLOOR PANEL BETWEEN FR12 TO FR16 & BETWEEN -Y30 TO -Y1640. REPLACED CABIN FLOOR PANEL BETWEEN FR12 TO FR16 & BETWEEN -Y30 TO -Y1640 IAW A319 AMM 53-12-12-400-001.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 33,694 hrs · 19,166 cycles

2S CHECK - AREA OF WATER INGRESS ON UPPER SURFACE OF RIGHT ELEVATOR APPROX 39 INCHES FROM INBOARD END. REPAIRED RIGHT ELEVATOR UPPER SURFACE IAW A319 SRM 55-22-11 PARA G, FIG 207.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 33,694 hrs · 19,166 cycles

2S CHECK - AREA OF WATER INGRESS ON UPPER SURFACE OF RIGHT ELEVATOR APPROX 107 INCHES FROM INBOARD END. REPAIRED RIGHT ELEVATOR UPPER SURFACE IAW A319 SRM 55-21-11 PARA G, FIG 207.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 33,694 hrs · 19,166 cycles

2S CHECK - AREA OF WATER INGRESS ON UPPER SURFACE OF RIGHT ELEVATOR APPROX 22 INCHES FROM INBOARD END IN 2 PLACES. REPAIRED RIGHT ELEVATOR UPPER SURFACE IAW A319 SRM 55-22-11 PARA G, FIG 207.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 33,694 hrs · 19,166 cycles

2S CHECK - AREA OF WATER INGRESS/DELAMINATION ON UPPER SURFACE OF LEFT ELEVATOR APPROX 117 INCHES FROM INBOARD END. REPAIRED LEFT ELEVATOR UPPER SURFACE IAW A319 SRM 55-21-11 PARA N, FIG 214.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 33,694 hrs · 19,166 cycles

2S CHECK - AREA OF WATER INGRESS ON UPPER SURFACE OF RIGHT ELEVATOR APPROX 89 INCHES FROM INBOARD END. REPAIRED RIGHT ELEVATOR UPPER SURFACE IAW A319 SRM 55-22-11 PARA G, FIG 207.

Part: SKIN — SATURATED (RT ELEVATOR) · airframe 33,694 hrs · 19,166 cycles

2S CHECK - AREA OF WATER INGRESS ON UPPER SURFACE OF RIGHT ELEVATOR APPROX 148 INCHES FROM INBOARD END. REPAIRED RIGHT ELEVATOR UPPER SURFACE IAW A319 SRM 55-21-11 PARA G, FIG 207.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 33,694 hrs · 19,166 cycles

2S CHECK - CRACK IN CABIN FLOOR PANEL BETWEEN FR36 TO FR42 & BETWEEN Y254 TO Y765. REPLACED CABIN FLOOR PANEL BETWEEN FR36 TO FR42 & BETWEEN Y254 TO Y765 IAW A319 AMM 53-32-12-400-002.

Part: FLAP — DELAMINATED (RT WING) · airframe 33,694 hrs · 19,166 cycles

2S CHECK - DELAMINATION ON RIGHT OUTBOARD AFT FLAP TRAILING EDGE APPROX 66 INCHES FROM INBOARD END & 4 INCHES FROM TRAILING EDGE. REPLACED RIGHT OUTBOARD AFT FLAP ASSEMBLY IAW EA 130684, A319 AMM 27-54-62.

Part: LENS — MISSING (CABIN) · airframe 27,804 hrs · 15,699 cycles

FLT 1181 - DTW-CLT - EMERGENCY LIGHTS - EMERGENCY EXIT LIGHT COVER MISSING ON SEAT 10C. BULBS ARE OPERATING NORMAL. REMOVED AND REPLACED LENS ON EMERGENCY LIGHT ON ROW 10C.

Part: CHILLER — FAULTY (GALLEY) · airframe 36,559 hrs · 5,214 cycles

FLT 1177-LGA-CLT- BURNING ODOR - FORWARD CHILLER HAS A BURNING ODOR. TURNED CHILLER OFF AND ODOR DISSIPATED. MAINTENANCE REMOVED AND REPLACED FORWARD CHILLER. OPERATIONAL CHECK WAS GOOD. (S)

Part: DECODER — FAILED (CABIN) · airframe 26,043 hrs · 14,609 cycles

PIT-CII-EEL- EMERGENCY LIGHT BIT TEST FAILS. REPLACED FORWARD DECODER/ENCODER UNIT-B. (A)

Part: EPSU — FAILED (ZONE 200)

TPA - FWD EMERGENCY LIGHT POWER UNIT FAILED. MAINTENANCE REPLACED FWD POWER SUPPLY, OPS OK.

Part: EPSU — FAILED (EMERGENCY LIGHTS)

TPA - FWD EMERGENCY LIGHT POWER UNIT FAILED. MAINTENANCE REPLACED FWD POWER SUPPLY, OPS OK.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

TPA - ROW 19 A/B/C SEAT MOUNTED EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PLACED THE AIRCRAFT ON MEL. MAINTENANCE RELAMPED THE EMERGENCY LIGHT ON ROW 19 A/B/C. OPERATIONALLY CHECKS OK.

Part: FAN — OVERHEATED (AVIONICS BAY)

SJU FLT 1037, EN ROUTE PHL TO SJU. DURING THE OPERATION OF THE AIRCRAFT, A BURNING ODOR WAS DETECTED IN THE FLIGHT DECK. AN ECAM WARNING OF BLOWER FAULT WAS GENERATED AROUND THE SAME TIME. THE CREW FOLLOWED PROCEDURES FOR THE WARNING AND COMPLETED THE FLIGHT WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE AVIONICS VENT BLOWER SYSTEM ON MEL. MAINTENANCE REPLACED THE EXTRACT FAN AS THE FINAL CORRECTIVE ACTION.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 1 · airframe 17,750 hrs · 17,750 cycles

FOUND CORROSION Y 1500 AND FRAME 6. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER, DEFECT SIZE: 2 SQ IN.

Part: SENSOR — FAULTY (NR 1 ENGINE)

PIT FLT 268 ON CLIMB OUT FROM PIT, AT FL160, CREW REPORTED THE NR 1 ENGINE AGENT ONE DISCHARGE LIGHT ILLUMINATED. FLIGHT ATTENDANT REPORTED FLAMES OUT THE REAR OF THE ENGINE WHILE A DEADHEAD PILOT REPORTED EXCESSIVE VIBRATION. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT PIT. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. MAINTENANCE PERFORMED BOROSCOPE INSPECTION OF NR 1 ENGINE. NO DEFECTS NOTED. ACCOMPLISHED TROUBLESHOOTING TASK 73-00-00-02 AND REPLACED NR 1 ENGINE T3 SENSOR PER MM 77-23-10-04. RAN ENGINES AT VARIOUS POWER SETTINGS. ALL OPERATIONS NORMAL. ALSO, REMOVED AND REPLACED NR 1 ENGINE AGENT ONE DISCHARGE BOTTLE. OPS CHECK GOOD.

Part: FLOORBEAM — CORRODED (FR 66) · airframe 17,750 hrs · 17,750 cycles

CORROSION FLOORBEAM FR 66 -Y1500. INSTALLED DOUBLER PER SRM 53-41-14 REPAIR 6. DEFECT SIZE: 1.5 X .75 INCH.

Part: ODOR — DETECTED (CABIN)

ENROUTE PIT-IAH. DURING FLIGHT, NOTICED OILY ODOR AT MID-CABIN. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE OPERATED THE AIR CONDITIONING PACKS WITH THE APU. NO ODOR DETECTED. CHECKED APU AREA. NO OIL DRAINAGE NOTED. FOUND AIRCRAFT OK FOR SERVICE.

Part: EPSU — WILL NOT TEST (EMERGENCY LIGHT)

DCA - ESPU FAILED SELF-TEST. MAINTENANCE REPLACED THE LEFT (11LWA) EMREGENCY LIGHT EPSU. (M)

Part: SLIDE — DEFECTIVE (AFT ENTRY DOOR)

CLT - THE RIGHT SIDE AFT ENTRY DOOR SLIDE COVER WOULD NOT REMAIN INSTALLED. MAINTENANCE REPLACED THE RIGHT SIDE AFT ENTRY DOOR ESCAPE SLIDE, THEN INSTALLED COVER. OK FOR SERVICE. (M)

Part: SLIDE — MALFUNCTIONED (CABIN)

NO EMERGENCY LIGHTS DID NOT ILLUMINATE ON THE AFT RIGHT SLIDE WHEN THE SLIDE WAS DEPLOYED FOR AN OPERATIONAL CHECK. MAINTENANCE REPLACED THE ESCAPE SLIDE. OPERATIONALLY CHECKED EMERGENCY LIGHTS SYSTEM. OK FOR SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

CLT - THE EMERGENCY LIGHT TEST INDICATED A 'L FWD LT' FAULT. MAINTENANCE REPLACED THE BATTERY PACK FOR THE LEFT FORWARD LIGHT. OPERATIONALLY CHECKED AND TESTED OK. (M)

Part: FAN — OVERHEATED (E/E BAY)

STL - FLT 163 - EN ROUTE PHL-PHX - WHILE IN CRUISE AT FL350, A VIBRATION WAS FELT IN THE COCKPIT AREA, FOLLOWED LATER BY AN ELECTRICAL ODOR. WHEN THE ODOR BECAME PRESENT, THE CREW PUT ON THEIR OXYGEN MASKS AND THE FLIGHT DIVERTED TO STL, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AVIONICS FAN. OPS CHECKED NORMAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SFO - FOUND ROW 8 SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPS CHECKS NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

PIT - FOUND THE EMERGENCY LIGHTS FAILED TEST. MAINTENANCE REPLACED THE BATTERY PACK ON AFT EMERGENCY POWER SUPPLY UNIT, OPS CHECKED OK. (X)