N479UA

Part: CHECK VALVE — FAULTED (HYD SYS) · airframe 69,711 hrs · 30,535 cycles

HYD Y RSVR OVHT ECAM REPORTED BY FLIGHT CREW VIA ARINC TO DISPATCH, CREW C/W QRH AND SHUTOFF HYD Y ENG 2 PUMP. CREW REPORTED THAT THEY HAD NOT RUN THE YELLOW ELECTRIC PUMP. ONLY EDP WAS USED DURING OVERHEAT. OVER HEAT MSG WENT AWAY IN FLIGHT AFTER TURNING OFF THE EDP ACCOMPLISHED TSM 29-13-00-810-802-A NO MESSAGES AND NO FAULTS NOTED. REMOVED AND REPLACED Y CHECK VALVE FOUND IN PART OPEN POSITION(PHOTO ATTACHED) STEP 4(E)1&2. AND AMM 29-24-21-400-001 NO FAULTS NOTED, OPS CHECK NORMAL AND NO LEAKS NOTED.

Part: COVER — CRACKED (ZONE 800) · airframe 69,407 hrs · 30,379 cycles

FA ADVISED DOOR 2R SLIDE COVER HAS 2 INCH CRACKED. REPLACED DR 2R SLIDE BUSTLE, REF AMM 25-62-44-400-802-A.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 68,615 hrs · 29,976 cycles

CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - BATTERY FAULT AT FWD L EMERGENCY POWER SUPPLY UNIT REMOVED AND REPLACE BATTERY REF AMM 33-51-38-000/400-002-A OPS CHECK GOOD

Part: SKIN — DENTED (ZONE 500) · airframe 68,342 hrs · 29,844 cycles

L/H WING SLAT #3 L/E HAS DENT DOT 43-035

Part: STRINGER — CORRODED (ZONE 100) · airframe 68,342 hrs · 29,844 cycles

CA3NB-05-3-6025) DOT 210-60 AFT CABIN UNDER FLOOR COMPARTMENT FR 66 STGR 41 HAS CORROSION.()

Part: PANEL — MISSING (AFT PANEL 486AR) · airframe 64,600 hrs · 28,089 cycles

PDA 3 #2 ENGINE PHLON OUTBD AFT PANEL 486AR IS MISSING ONE EA SCREW INSTALLED MISSING SCREW ON PANEL 486AR, #2 ENGINE OUTBD PYLON. REF AMM 54-53-11

Part: PANEL — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,101 hrs · 27,351 cycles

EMERGENCY EXIT LTS ILLUMINATED IN CABIN REPLACED AFT LIGHT PANEL PER TASK 23-73-13-400-001-A - OPSCHECK NORMAL

Part: ENGINE — FIRE (E2) · airframe 62,550 hrs · 27,091 cycles

DURING HIGH POWER RUN OBSERVED #2 ENGINE FIRE WARNING INDICATION ALONG WITH CONTROL TOWER VISUAL CONFIRMATION. SHUTOFF FUEL CONTROL LEVER AND DEPLOYED #2 ENGINE FIRE SWITCH. CRANKED ENGINE UNTIL FIRE WARNING EXTINGUISHED. FIRE BOTTLES WERE NOT DEPLOYED. VISUALLY INSPECTED #2 ENGINE FOR FIRE CAUSE. SUSPECT FAULTY VSV UPDATED PICTURES ACTUATOR. TOO MUCH DAMAGE TO CONFIRM.

Part: PRIORITY VALVE — LEAKING (ENG #2) · airframe 62,097 hrs · 26,881 cycles

HYD Y ENG 2 PUMP LO PRECAM.YELLOW HYD SYSTEM LOST ALL FLUID DURING CRUISE. LEAK FOUND AT PRIORITY VALVE YELLOW SYS. R AND R YELLOW PRIORITY VALVE LEAK TEST IS GOOD NO DEFECT NOTICE AT THIS TIME. ADD EMP:U102061 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1124690 SN OFF 5120 IPC REFERENCE # 29-13-33 VALVE, HYDRAULI OFF 31-2910-9-9001 5120 ON 31-2910-9-9001 1300

Part: RELAY — ODOR (NA) · airframe 61,370 hrs · 26,550 cycles

FLIGHT CREW REPORTED TO HMC SMOKE IN THE COCKPIT UPDATING TO REFLECT SDR ITEM DEBREIFED CREW AND FOUND C/B E8 ON 49VU TRIPPED.. REF AWM 31-68-04 ,31-68-05,31-68-06,31-68-07,,31-61-07..FOUND TESTS PASSED.EIS DMC SWITCHING CKS NORMAL..CIRCUIT BRKR STAYS RELAY BOX20WT1 SHOWING BURN MARKS AND HEAT DISCOLORED...REPLACED SET...NO ABNORMAL INDICATIONS AND NO SMELL OR SIGNS OF RELAY BOX 20WT1...OPS CKED DMC1,2 AND 3..REF MM SMOKE..GVI OF SOCKTES AND WIRES GOING TO RELAY 20WT1 SHOWED NO 31-63-34..PERFORMED TEST OF EIS SYSTEM PER MM 31-60-00 AND ALL SIGNS OF DAMAGE

Part: POWER SUPPLY — INOPERATIVE (L/H OVER WING (1) · airframe 61,325 hrs · 26,529 cycles

PASSENEGER SEAT ROWS 10, 11 AND 38 EMERGENCY LIGHTS FAIL TO ILLU MINATE PER HAECO LCQ NON ROUTINE 9298752/36752 GENERATED BY V061 627. TROUBLESHOT IAW A320 AWM 35-51-06 & 35-51-08. REMOVED & REPLACED AND 33-51-00-710-001-A. PERFORMED BY MECH V920292 INSPECTED BY V CONNECTOR 7260VC10 IAW A320 AWM 33-51-08. REMOVED & REPLACED EP 892285 SU 11WL IAW A320 AMM 33-51-38-000-001-A AND 33-51-400-001-A. OPS TEST OF EMERGENCY LIGHTS GOOD IAW A320 AMM 33-51-00-710-000-A ROTABLE PARTS INFO ROTABLE PARTS CHANGE WAS INDICATED - TT # 1211558 SN OFF 4812 POWER SUPPLY, C OFF 31-3350-9-9001 4812 ON 31-3350-9-9001 2894

Part: BATTERY PACK — WEAK (13WL) · airframe 61,325 hrs · 26,529 cycles

13WL FAILS CAPACITY CHECK A3NB-33-3-6013 PER HAECO LCQ NON ROUTI NE 9298024/36024 GENERATED BY V039706

Part: STRINGER — CORRODED (FR34) · airframe 61,325 hrs · 26,529 cycles

FWD CARGO FR34 STR41 RT STRINGER HAS CORROSION (A3NB-05-3-6013) GENERATED AT HAECO LCQ PER NONROUTINE 9298365 (36365) BY N078592 REMOVED AND REPLACED STR 34 FR30-35 L/H IAW A320 SRM 51-72-11-91 1-001 PERFORMED BY:V061616 INSP BY:V919150

Part: INTERCOSTAL — CRACKED (FR 16) · airframe 61,325 hrs · 26,529 cycles

R1 FR16 DOOR STOP #1 HAS CRACK INDICATION IN LOWER IB HOLE, APPE ARS TO BE IN FRAME LAYER AT 5 O''CLOCK. GENERATED BY V892444 PER NR 9298275/36275 INSPECTIONS AT RH FR16 AT DOOR STOP FITTING #1 HOLE#3 AND #4 PER REACHES 38,829 TOTAL ACFT FC.PERFORM REPEAT INSP AT INTERVALS NO ALL WORK ACCOMPLISHED ON HAECO NR 9298275. PART 2 OF LATEST REV OF ECRA 5311-02764 ON OR BEFORE THE ACFT T TO EXCEED 12,300 FC THEREAFTER.IAW ECRA 5311-02764 PART 1.2. ACCOMPLISHED INTERIM REPAIR AT R1 FR16 DOOR STOP FITTING #1 IAW ECRA 5311-02764 PART 1.1. DIP GENERATED TO ACCOMPLISH INITIAL OK TO CARRY PER ECRA 5311-02764, ACP INITIAL INSP AT R/H FR16 AT TOMC-APPROVAL FROM SC1ELBYC COMMENT DOOR STOP FITTING #1 HOLE #3 & #4 PER PART 2 OF LATEST REV OF ECRA 5311-02764 ON OR BEFORE THE A/C REACHES 38829 TOTAL F/C''S. PER FORM REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 12300 F/C''S THERE AFTER. QC REVIEWED QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: SKIN — CRACKED (FR35) · airframe 61,325 hrs · 26,529 cycles

FR 35 STR 30 LH CRACK INDICATIONS NOTED IN FASTENER HOLE #2 FRAM E,AFT SKIN FWD SKIN LAYERS AND HOLE #3 FRAME LAYER ONLY. 5331-02848 PART 1.1. ACCOMPLISH PERMANENT REPAIR AT LH FR 35 STR BEFORE 16AUG2022. ALL WORK ACCOMPLISHED ON HAECO NR 9298178 AND 30 HOLES PER PART 3 OF LATEST REVISION OF ECRA 5331-02848 ON OR 9298179. ACCOMPLISHED INTERIM REPAIR AT FR 35 STR30LH HOLE#2 FRAME ,AFT S KIN AND FWD SKIN LAYERS AND HOLE#3 FRAME LAYER ONLY IAW ECRA OK TO CARRY PER ECRA 5331-02848, ACP PERMANENT REPAIR @ L/H FR TOMC-APPROVAL FROM SC1ELBYC COMMENT 35 STR30 HOLES PER PART 3 OF THE LATEST REV OF ECRA 5331-02848 ON OR BEFORE 16AUG22. QC REVIEWED QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: INTERCOSTAL — CRACKED (L1 DOOR FR16) · airframe 61,325 hrs · 26,529 cycles

L1 FR 16 DOOR STOP #1 HAS CRACK INDICATION IN LOWER IB HOLE, APP EARS TO BE IN INTERCOASTAL LAYER AT 3 O''CLOCK. SUPPORT TASK GENE RATED BY:V892444 AT HAECO LCQ PER NR:9298272 (36272) PERFORMED INTERCOASTAL REPLACEMENT AT L1 FR16, STOP FITTING #1 IAW EA5311-02164-001 & REPAIR DWG R53113118 PERFORMED BY:061616 INSP BY:V919150.

Part: STRINGER — CORRODED (STR40LFR57) · airframe 61,325 hrs · 26,529 cycles

AFT CARGO BILGE STRINGER 40 LEFT CORRODED AT FR57.A3NB-12-3-6020 GENERATED BY:V892285 AT HAECO LCQ PER NR:9298690 (36690) REMOVED AND REPLACED STR40 L/H FR47-57 IAW A320 SRM 51-72-11-911 -001 PERFORMED BY:V061630 INSPECTED BY:V061334

Part: INTERCOSTAL — CRACKED (L1 DOOR FR16) · airframe 61,325 hrs · 26,529 cycles

L1 FR 16 DOOR STOP #7 HAS CRACK INDICATION IN UPPER IB HOLE, APP EARS TO BE INTERCOASTAL LAYER AT 4 O''CLOCK. SUPPORT TASK. GENERA TED BY V892444 AT HAECO LCQ PER NR:9298273 (36273). PERFORMED INTERCOASTAL REPLACEMENT REPAIR AT L1 FR16, STOP FITTI NG #7. IAW EA5311-02164 & REPAIR DWG R53113118 PERFORMED BY :061 616 INSP BY:V919150

Part: PLATE — CORRODED (FR52A-56) · airframe 61,325 hrs · 26,529 cycles

AFT CARGO PIT R/H DOOR SILL SUPPORT BOX BETWEEN FR52A-56, HAS CO RROOSION ON UPPER SURFACE.A3NB-05-3-6023. GENERATED BY V919150 A T HAECO LCQ PER NR:9298328 (36328) REMOVED 7 REPLACED AFT CARGO PIT R/H DOOR SILL SUPPORT FR52A-56 IAW A320 SRM 51-72-11 PERFORMED BY:052030 INSP BY:V061334

Part: INTERCOSTAL — CRACKED (R1 DOOR FR16) · airframe 61,325 hrs · 26,529 cycles

R1 FR16 DOOR STOP #7, HAS CRACK INDICATION IN UPPER IB HOLE AT 5 O''CLOCK. GENERATED BY:V892444 AY HAECO LCQ PER NR:9298276 (3627 6) SUPPORT TASK.. PERFORMED INTERCOASTAL REPLACEMENT REPAIR AT R1 FR 16, STOP FITT ING #7 IAW EA 5311-02164.002 & REPAIR DWG R53113118. REPAIR CODE AD PERFORMED BY:V061616 INSP BY:V919150

Part: STRINGER — CORRODED (STR42FR57) · airframe 61,325 hrs · 26,529 cycles

AFT CARGO BILGE STRINGER 42 LEFT CORRODED AT FR57.A3NB-12-3-6020 GENERATED BY:V892285 AT HAECO LCQ PER NR:9298691 (36691) REMOVED AND REPLACED STR42 L/H AT FR57 IAW A320 SRM 51-72-11-911 -001.PERFORMED BY V061765,INSPECTED BY: V061334.

Part: PLATE — CORRODED (FR25-28) · airframe 61,325 hrs · 26,529 cycles

FWD CARGO DOOR SILL WEBB FR25 TO FR28 HAS SPOTS OF CORROSION. G ENERATED BY:N075892 @HAECO LCQ PER NON ROUTINE 9298330(36330) A3 NB-53-3-6105.

Part: OUTFLOW VALVE — FAULTED (CABIN PRESSURE) · airframe 58,525 hrs · 25,271 cycles

FLIGHT CREW REPORTED AVIONICS VENT SKIN VALVE FAULT ALONG WITH BLOWER FAULT. TOMC UPDATE- PRECAUTIONARY REMOVE AND REPLACE 22HQ SKIN AIR OUTLET VLV. REF TSM TASK 21-26-00-810-84-A, TESTED AEVC ON MCDU, TESTED OK, LAST LEG REPORT, SKIN AIR OUTLET V 22HQ AND ISOL V 24HQ. REMOVED SKIN AIR OUTLET VALVE REF AMM 21-26-53. INSTALLED NEW SKIN AIR OUTLET VALVE REFERENCE AMM 21-26-53-400-001-A. ALSO PREFORMED OPS CHECK REFERENCE AMM 21-26-00-710-001-A. OPS CHECK GOOD. REPLACED DEFECTIVE PART.

Part: EPSU — FAULTY (CABIN) · airframe 57,577 hrs · 24,867 cycles

MIDDLE OVERHEAD EMERGENCY LIGHT INTERMITTENTLY TURNS ON UNCOMMAN DED A3NB-33-3-6012 PER NR 9290608 T/S MIDDLE OVERHEAD EMERGENCY LIGHTS AND FOUND LT EPSU (11WL) TO BE BAD REMOVED AND REPLACED LT EPSU (11WL) IAW AMM 33-51-34-000-001-A AND 33-51-38-400-001-A OP CHECK GOOD IAW AMM 33-51-38-974-005-0B POSITION LEFT CENTER (LC) WORK ACCOMPLISHED. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1082648 SN OFF 3236 POWER SUPPLY, C OFF 31-3350-9-9001 3236 ON 31-3350-9-9001 4812.

Part: SHEAR PLATE — NOT REPORTED (FUSELAGE) · airframe 57,577 hrs · 24,867 cycles

RT AFT SHEAR PLATE @FR 68-69 A3NB-53-3-6222 PER NR 92 90327 REMOVED AND REPLACED SHEAR PLATE @FR 68-69 IAW A320 51-42-11 PER NR 9290327 WORK ACCOMPLISHED.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 57,577 hrs · 24,867 cycles

EVIDENCE OF CORROSION L-2 DOOR SILL I/B OF AFT GIRT PLATE A3NB-5 3-3-6222 PER NR 9290355. REPAIRED AREA ON L2 DOOR SILL I/B OF AFT GIRT PLATE IAW SRM 51-42-11 AND 53-41-14-300-001 THIS IS A CATEGORY A REPAIR NO REINSPECT REQUIRED PER NR 9290355.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 57,577 hrs · 24,867 cycles

EVIDENCE OF CORROSION AT FWD AND AFT I/B SIDE OF R-2 DOOR SILL A 3NB-53-3-6222 PER NR 9290351. REMOVED AND REPLACED R2 DOOR SILL IAW SRM 51-72-11-911-001 PER NR 9290351.

Part: COVER — CRACKED (OVERWING EXIT) · airframe 53,791 hrs · 23,208 cycles

RIGHT OVERWING EMER EXIT SLIDE COVER CRACKED. REPLACED RIGHT OVERWING SLIDE PER AMM25-62-42-400. ALL OPS CKS GOOD.

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 53,584 hrs · 23,111 cycles

EMERGENCY EXIT LIGHTS WILL NOT EXTINGUISH. RESET NO SMOKING LIGHTS TO ON POSITION

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,415 hrs · 23,040 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EPSU AND BATTERY REF AMM 33-51-38. OPS CHECK GOOD. OK FOR SVC.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 53,300 hrs · 22,982 cycles

RIGHT EMER LIGHT POWER SUPPLY FAILED SYSTEM TEST DURING 2 SERVICE CHECK. REPLACED RH EPSU REF AMM 33-51-38 OPS CHK OK

Part: OVEN — CONTAMINATED (GALLEY) · airframe 51,697 hrs · 22,260 cycles

F/A REPORTED AFT GALLEY OVEN R42 BURNT SMELL AND PLASTIC MELTED TO FAN GUARD. MELTED PLASTIC FOUND AT OVEN FAN GRILL. REMOVED PLASTIC, OPS CHECK GOOD. NO MORE SMELL.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,661 hrs · 20,106 cycles

AFT CARGO, STRINGER 43L IS CORRODED, BETWEEN FRAME 58 - 59. R & R STRINGER 43L IAW SRM 51-42-11.

Part: SKIN — DAMAGED (LT WING) · airframe 41,411 hrs · 17,983 cycles

LT WING FUEL PANEL LANDING 540MB HAS FOUR EACH SCREW HOLES GOUGED. REWORKED HOLES & INSTALLED BUSHINGS IAW SRM 57-27-11 FIG 102 & 57-21-11 FG 201.

Part: SKIN — DAMAGED (RT WING) · airframe 41,411 hrs · 17,983 cycles

RT WING FUEL TANK PANEL 640MB LANDING HAS ONE HOLE DAMAGED. REWORKED HOLES & INSTALLED BUSHINGS IAW SRM 57-27-11 FIG 102 & 57-21-11 FG 201.

Part: FITTING — CORRODED (FUSELAGE) · airframe 41,411 hrs · 17,983 cycles

R2 DOOR AFT FRAME 68 & STRINGER 23 HAS CORROSION. REMOVED CORROSION & FABRICATED REPAIR FITTING & INSTALLED IAW SRM 53-41-12 FG 202.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,411 hrs · 17,983 cycles

R2 DOOR AFT FRAME 68 & STATION 23 HAS CORROSION. REMOVED CORROSION, FABRICATED REPAIR FITTING & INSTALLED IAW SRM 53-41-12 FG 202.

Part: SKIN — GOUGED (LT WING) · airframe 41,411 hrs · 17,983 cycles

LT WING FUEL PANEL LANDING 540 MB HAS FOUR EACH SCREW HOLES GOUGED. HOLES REWORKED & BUSHING INSTALLED IAW A320 SRM 57-27-11 FIG 102 & 57-21-11 FG 201.

Part: SKIN — GOUGED (RT WING) · airframe 41,411 hrs · 17,983 cycles

RT WING FUEL TANK PANEL 640MB LANDING HAS ONE HOLE DAMAGED. HOLE REWORKED & BUSHING INSTALLED IAW A320 SRM 57-27-11 FIG 102 & 57-21-11 FG 201.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 41,411 hrs · 17,983 cycles

LT AVIONICS COMPARTMENT NLG DOG HOUSE CROSS BEAM FRAME 16 HAS ELONGATED SLOT ATTACH HOLE. REWORKED HOLE LT SIDE NLG COMPARTMENT BETWEEN LT AVIONICS DOOR & DOG HOUSE FAME 16. REAMED ELONGATED HOLE, FABRICATED & INSTALLED INSERT & REPAIRED WASHERS IAW ECRA 5310-05993, REO 374002 & AIRBUS TDP1S2095202014. ACP HFEC IAW NTM 51-10-08 PB6, NO DEFECTS NOTED.

Part: SILL — CORRODED (FUSELAGE) · airframe 41,411 hrs · 17,983 cycles

R2 DOOR SILL HAS CORROSION AT FRAME 66, REPLACED R2 DOOR SILL.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,411 hrs · 17,983 cycles

STRINGER 41R, FRAME 58 - 64 HAS CORROSION. REPLACED STRINGER IAW SRM 51-42-11 ON TIMCO NR 39450.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,411 hrs · 17,983 cycles

CORROSION PRESENT AT L2 DOOR SILL FWD GIRT BAR ATTACH POINT FRAME 66. R & R L2 DOOR SILL PN D534800420601 IAW A320 SRM 51-42-11 PG 7, PARA 5 & 6 & PG 25 PARA 7.

Part: STRUCTURE — GOUGED (FUSELAGE) · airframe 41,411 hrs · 17,983 cycles

REPAIRED MED R1 FWD GIRT BAR FITTING AREA GOUGE IN TWO PLACES IAW SRM 53-11-14 FIG 108. ACP HFEC IAW NTM'S 51-10-01 PB 6 & 51-10-04 PB 4, NO DISCREPANCIES. FABRICATED & INSTALLED TWO EACH REPAIR WASHERS FWD INBD & OTBD HOLES IAW SRM 53-11-14 FIG 108.

Part: FITTING — CORRODED (FUSELAGE) · airframe 41,411 hrs · 17,983 cycles

REPAIRED R1 DOOR SILL FWD GIRT BAR FITTING AFT TWO EACH HOLES CORROSION IAW SRM 53-11-14 FIG 108. ACCOMPLISHED HFEC ROTARY SCAN ON HOLES IAW NTM 51-10-01 PB 6, NO INDICATION NOTED.

Part: FITTING — CORRODED (FUSELAGE) · airframe 41,411 hrs · 17,983 cycles

REPAIRED L1 DOOR SILL FWD GIRT BAR FITTING FWD OTBD HOLE CORROSION IAW SRM 53-11-14 FIG 108. ACP HFEC ROTARY SCAN ON HOLE IAW NTM 51-10-01 PB 6, NO INDICATION NOTED.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,411 hrs · 17,983 cycles

REPAIRED L1 DOOR SILL FWD GIRT BAR FITTING TWO EACH AFT HOLES CORROSION IAW SRM 53-11-14 FIG 108. ACP HFEC ROTARY SCAN ON HOLES IAW NTM 51-10-01 PB 6, NO INDICATION NOTED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 41,062 hrs · 17,855 cycles

DURING TEST ITEM 31 OF JIC 4-2020 FAILED BATTERY CAPACITY TEST. MESSAGE DISPLAYED AS FOLLOWS EPSU BAT CAP FWD L, EMER R EMER L, AFT L. TEST COMPLETION AT "CIDS" SHOWS BATTERY FAULT AT "EMERG PWR SUPPLY UNIT". 10WL LOCATED ABOVE CEILING DOOR FWD LT. REPLACED POWER SUPPLY IAW AMM 33-51-38 & BATTERY, TESTED OK.

Part: GENERATOR — FAULTY (APU) · airframe 40,939 hrs · 17,806 cycles

APU ELEC NOT AVAILABLE, PNEUMATICS OK. REPLACED APU GEN IAW MM. RAN APU, OPERATIONS CHECKED GOOD.

Part: CRADLE — DEFECTIVE (FIRE BOTTLE) · airframe 40,842 hrs · 17,761 cycles

AFT HALON EXTINGUISHER CRADLE STRAP WILL NOT FASTEN CLOSED. REPLACED CRADLE.

Part: COMPUTER — FAULTY (NR 1 ELAC) · airframe 40,765 hrs · 17,726 cycles

ELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. CONFIRMED NR 2 ELAC COMPUTER IS BAD. SWAPPED BOX INTO THE NR 1 ELAC POSITION & MEL NR 1 ELAC SYSTEM INOPERATIVE. ACFT DOWNGRADED TO CAT 1. SN OF NR 1 ELAC IS 1039, SN OF NR 2 ELAC IS 5084. ALL DDPG IAW DF0980. REPLACED ELAC 1 IAW MM 27-93-34 & ACCOMPLISHED TEST IAW 27-93-00,TESTED OK, NO FAULTS & NO MESSAGES. ACCOMPLISHED LAND CAT 3 CAPABILITY TEST, TESTED OK. ACFT BACK TO CAT 3 STATUS, PLACARD REMOVED.

Part: COMPUTER — FAILED (NR 1) · airframe 40,768 hrs · 17,727 cycles

CAP MAP NOT AVAILABLE ON ND. REPLACED FMGC 1 IAW AMM 22-83-34, OPS CHECKED GOOD. LAND TEST IAW AMM22-97-710 TEST PASSED.

Part: CYLINDER — LACK OF LUBE (NLG STEERING) · airframe 40,360 hrs · 17,587 cycles

LOUD CONSISTENT GRINDING NOISE FROM NOSE WHEEL STEERING IN ALL LT TURNS WITH ABOUT 10. LUBED NLG STEERING CYL IAW AMM, OPERATIONS CHECKED GOOD.

Part: ACCESS PANEL — DAMAGED (CARGO DOOR) · airframe 39,996 hrs · 17,445 cycles

RAMP REPORTS THE AFT CARGO DOOR DAMAGE TO THE AFT LOWER ACCESS COVER PANEL 826AR. COMPLIED WITH CDL REMOVED AFT LOWER ACCESS COVER PANEL. OK :REPLACED AFT CARGO LOWER ACCESS PANEL.

Part: OXYGEN MASK — MISSING (CABIN) · airframe 39,430 hrs · 17,219 cycles

BOTH O2 BOTTLES MISSING MASK IN FIRST CLASS. DEF DUE TO TIME. MOVED ONE BOTTLE FROM REAR TO FIRST CLASS FOR MEL. SO ONE IN COACH AND ONE IN FIRST CLASS DEF. REPLACED 2EA OXYGEN MASKS IN FWD AFT LOCATIONS, OK TO CONTINUE.

Part: SCREW — LOOSE (FUSELAGE) · airframe 39,107 hrs · 17,090 cycles

RAMP LEAD REPORTED A LOOSE SCREW ON V-STA P. SECURED SCREW.

Part: VALVE — LEAKING (LT WING) · airframe 38,868 hrs · 16,990 cycles

FUEL DRIPPING FROM LEFT WING OUTBOARD DRAIN. REPLACED OUTER VALVE, NO LEAKS NOTED.

Part: PLATE — CRACKED (DOOR 1L COVER) · airframe 38,563 hrs · 16,871 cycles

DOOR 1L DOES NOT CLOSE FLUSH, UPPER LEFT TOP. FOUND UPPER FWD CORNER COVER PLATE CRACKED 2 INCH IN LENGTH. STOPPED DRILLED AND APPLIED HIGH SPEED TAPE PER SRM 52-10-00. 1L DOOR COVER PLATE CRACKED.

Part: FLOORBOARD — DENTED (CARGO BAY) · airframe 38,539 hrs · 16,861 cycles

AFT CARGO BAY ONE FOOT FWD OR CARGO DOOR, FOUR INCH DENT IN FLOORBOARD. REPAIRED IAW SRM 53-02-00.

Part: UNKNOWN — VIBRATION (WING) · airframe 38,050 hrs · 16,661 cycles

CREW REPORTS VIBRATION. VIBRATION STARTED WHEN GEAR WAS PUT DOWN, FULL FLAPS. VIBRATION REMAINED UNTIL TOUCHDOWN. ACCOMPLISHED MT 27-005, NO MIGRATION NOTED VERIFIED UPPER AND LOWER KINK AND CUSHION SEAL ARE OK. NO DEFECT NOTED ON GENERAL VISUAL FLAP INSPECTION.

Part: TAIL CONE — CRACKED (NR 1 ENGINE) · airframe 37,882 hrs · 16,589 cycles

NR 1 ENGINE TAIL CONE IS CRACKED AT 3 AND 7 O`CLOCK POSITIONS. CRACKS APPROXIMATELY 3-5 INCHES LONG. CRACKS AT 3 AND 7 O'CLOCK ARE FROM PREVIOUS WELDED AREAS AND TRUE MEASUREMENTS OF SEVERAL CRACKS RANGE FROM .5 TO 1.5 INCHES. ALL WITHIN ZONE 1 AND OK FOR SERVICE AS PER REF MM 78-11-12-601. NO FURTHER MAINTENANCE ACTION NEEDED.

Part: SWITCH — DEFECTIVE (COCKPIT) · airframe 37,701 hrs · 16,520 cycles

CAP SIDESTICK PTT STICKS CAUSING STUCK MIC. TROUBLESHOT, FOUND CAPTAIN PUSH TO TALK SWITCH BAD REPLACED, OP CHECKS GOOD.

Part: FAIRING — DENTED (FUSELAGE) · airframe 36,966 hrs · 16,207 cycles

DENT IN FORWARD MOST END OF MAIN BODY FAIRING ON LEFT SIDE OF ACFT. DAMAGE IS 2 IN BY 1 IN AND 0.03125 IN DEEP. DENT IS 15 INCHES FROM TOP OF FAIRING AND 1 INCH 3 INCHES FROM TRAILING EDGE. REF ECRA5325-01001 NO UNDERLYING CRACKS OR LOOSE FASTENERS AND EXTERNAL PAINT INTACT. AREA INTERIM REPAIRED WITH SPEED TAPE AND TO BE RECHECKED DAILY. DENTED PANEL IS OF METAL AND IS RIVETED ONTO THE FUSELAGE, WILL HAVE TO REMOVE WING TO BODY FAIRING TO GET TO DENTED PANEL. DRESSED DENT REF SRM 51-73-00 PARA 7A(3) PER ECRA 5325-01001. NEED NDI FOR CRACKS. ACCOMPLISHED HFEC INSP OF DENT ON BOTH INNER AND OUTER, NO CRACKS FOUND AT THIS TIME. SECURED PANEL

Part: COMPUTER — FAULTY (COCKPIT) · airframe 36,704 hrs · 16,095 cycles

WX RADAR FAULTY, FLIGHT DIVERTED. DUE TO REPEATED C-B RESETS, REPLACE AEVC PER AMM. (PCN 482-9059). REPLACED AEVC, OPS CHECKS GOOD. REPLACE AEVC FILTER. WEATHER RADAR SYSTEM OPS CHECK GOOD.

Part: STOWAGE BOX — DEFECTIVE (COCKPIT) · airframe 36,039 hrs · 15,828 cycles

ON TAXI IN - CREW O2 PRESS WENT TO ZERO. REPLACED FIRST OFF O2 STOWAGE BOX ASSY PER AMM, OPS CHECKS NORMAL.

Part: SPRING — UNSECURE (NLG DOWNLOCK) · airframe 35,856 hrs · 15,747 cycles

BOTH NOSE GEAR DOWNLOCK SPRINGS ARE NOT PROPERLY SEATED IN GROVE LWR FITTING. REPLACED BOTH LEFT AND RIGHT NOSE LANDING GEAR LOCK SPRINGS, ACFT OK TO CONTINUE.

Part: PLATE — CORRODED (FUSELAGE) · airframe 33,052 hrs · 14,619 cycles

CORROSION ON SILL PLATE AT DOOR 2R BETWEEN FRAMES 66 AND 68 AT FLOOR LEVEL. MAJOR REPAIR. INSTALLED REPAIR AT FR 68 PER SRM53-41-14 ON NR D3700Y.

Part: RAM AIR TURB — LACK OF LUBE (HYDRAULIC SYS) · airframe 31,885 hrs · 14,145 cycles

FOUND RAT OIL LEVEL DRY DURING RAT CHECK. RAT REMOVED, INSTALLING NEW RAT. REPLACED RAT. MADE SMC 12 AND SMC 13 TO COVER OPS CHECKS.

Part: SHADE — DAMAGED (EMERGENCY EXIT) · airframe 31,885 hrs · 14,145 cycles

11F EMERGENCY EXIT WINDOW SHADE DAMAGED. SHADE REMOVED. REQUIRES EXIT HATCH REMOVAL AND RE-INSTALLATION. REMOVED AND REPLACED LINER AND WINDW SHADE. SHADE BINDS, NEW SHADE ORDERED. RT EXIT HATCH REMOVED. REPLACED SHADE, RE-INSTALLED HATCH.

Part: FEEDER CABLE — DAMAGED (NR 2 GCU) · airframe 30,547 hrs · 13,576 cycles

FLIGHT AUGMENTATION COMPUTER 2 INOP - AUTO FLT. IN CRUISE GOT FAC 2 FAULT RESET IAW ECAM. REPLACED SWITCH 3XU2, REPLACED NR 2 GCU, GENERATED WRITE UP FOR OPS CK AFTER REPLACEMENT OF NR 2 PYLON GEN HARNESS. REPLACED IDG AND REPLACED FEEDER CABLE.

Part: WASHER — OUT OF TOLERANCE (OXYGEN SYSTEM) · airframe 29,723 hrs · 13,224 cycles

VERIFIED NR O2 LEAK AT LT SIDE CAPTAIN'S. SECOND OBSERVER O2 MASKS CHANGED OUT FROM AC 4101 DOWN TO LT SIDE FLOOR LEVEL T-FITTING. CHANGED OUT CAPT'S AND SECOND OBSERVER'S STOWAGE BOX 5774HM, 10RN1 COPPER RING CONICAL WASHER. TIGHTENED AND LEAK CHECKED.

Part: MICROPHONE — INOPERATIVE (OXYGEN MASK) · airframe 29,680 hrs · 13,203 cycles

CAPTAIN'S OXYGEN MASK MICROPHONE IS INOPERATIVE. SWAPPED CAPT. O2 MASK BOX WITH 2ND OBS. MASK BOX THAT DOES NOT USE O2 MIC. NO NEED TO REPLACE 2ND OBS MASK BOX. REPLACED IAW MM.

Part: APU — FAULTY (APU BAY) · airframe 29,326 hrs · 13,061 cycles

AFTER PACKS WERE TURNED ON ACFT HAD A FOUL SMELL. DURING PACK BURNOUT FOUND APU TO BE THE SOURCE OF OIL SMELL IN ACFT CABIN. AFTER APU SHUTDOWN, THEN RE-START SMELL CAME BACK. RECOMMEND REPLACING CABIN RECIRC FILTERS DUE TO POSSIBLE CONTAMINATION.-DURING PACK BURNOUT FOUND APU TO BE THE SOURCE OF OIL SMELL IN ACFT CABIN. AFTER APU SHUTDOWN, THEN RE-START SMELL CAME BACK. REPLACED IAW TOD.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 29,199 hrs · 13,009 cycles

CABIN EMERGENCY EXIT LIGHT TEST GIVES 'EPSU INTERNAL LOAD FWD LEFT' FAULT. REPLACED BATTERY AND POWER SUPPLY. SYSTEM TESTS OKAY.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 28,541 hrs · 12,736 cycles

DOOR 1L ASSIST BOTTLE PRESSURE LOW. SERVICED ASSIST CYL.

Part: BOTTLE — UNDERSERVICED (L1 DOOR ASSIST) · airframe 27,287 hrs · 12,165 cycles

DOOR 1L ASSIST BOTTLE PRESSURE LOW, REPORTED BY F/A. SERVICED BOTTLE PRESSURE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,311 hrs · 10,658 cycles

SEAT 18 EMERGENCY LIGHT IS INOP. REPLACED EMERGENCY LIGHT ON SEAT ROW END CAP AT POSITION 18C, OPS NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 24,311 hrs · 10,658 cycles

SEAT MOUNTED EMERGENCY LIGHTS AT ROW 10 AND 11 LEFT HAVE BROKEN WIRES. LIGHTS ARE OVERWING EXIT-NOT DEFERRABLE. REPLACED UNDER SEAT CABLE P/N 565-2099 ON BOTH ROWS REF IPC 33-51-09, ALL EMERGENCY LIGHTS ALL ROWS OPS NORMAL.

Part: POWER SUPPLY — UNKNOWN (CABIN) · airframe 22,781 hrs · 9,911 cycles

EPSU INT LOAD FWD L FOUND ON 3SVC CHECK.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 20,266 hrs · 8,772 cycles

FIRST OBSERVERS SEAT QUICK O2 MASK INOP BOX ASSY NEEDS CHANGED. *S/D* REPLACED FIRST OBS O2 STOW BOX ASSY.

Part: OXYGEN MASK — NO TEST (CAPTAIN'S) · airframe 20,060 hrs · 8,672 cycles

CAPTS O2 MASK WILL NOT TEST. FOUND FAULTY MASK & LEAKING HARNESS. REPLACED MASK.

Part: RADAR — INOPERATIVE (WX SYS) · airframe 19,994 hrs · 8,644 cycles

RTFL DUE TO INOPERATIVE WEATHER RADAR. [08-24-07] REPLACED WX RADAR PN 622-5137-601. NO REPEATS SINCE 7/16/07.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 19,974 hrs · 8,635 cycles

LAV SMOKE DETECTOR FAULT. LAV SMOKE DETECTOR FAULTY. REPLACED LAV SMOKE DETECTOR. OPS CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 18,436 hrs · 7,940 cycles

FLIGHT ATTENDANT ADVISES BOTTLE PRESSURE AT DOOR 1L READS LOW. REPLACED DOOR 1L DOOR-DAMPER AND EMERGENCY-OPERATION CYLINDER. COMPLETE INSPECTION OF REPLACED BOTTLE.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 16,621 hrs · 7,135 cycles

RETURNED TO FIELD DUE TO NR 1 ENG COMPRESSOR STALL.

Part: LIGHT — FAULTY (CABIN) · airframe 13,628 hrs · 5,796 cycles

EMERGENCY EXIT LIGHT TEST DOES NOT PASS. REPLACED BATTERY.

Part: BLEED VALVE — FAILED (ENGINE) · airframe 8,777 hrs · 3,467 cycles

RETURNED TO FIELD DUE TO FAILED BLEED VALVE. FAN AIR VALVE CONTROL THERMOSTAT FAILED. REPLACED FAN AIR VALVE CONTROL THERMOSTAT. OPERATIONS CHECK NORMAL.

Part: CONNECTOR — DAMAGED (FWD CARGO DOOR) · airframe 8,756 hrs · 3,453 cycles

FWD CARGO DOOR OPEN INDICATION ON TAKEOFF. *S/D* REPAIRED DAMAGED CONNECTOR BACKSHELL ON DOOR WARNING SENSOR.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 8,284 hrs · 3,245 cycles

AFT RT, LWR DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED CONNECTOR. CHECKS OK.

Part: DISK — BURST (CENTER TANK) · airframe 2,907 hrs · 1,176 cycles

RETURN TO FIELD WITH A FUEL IMBALANCE PROBLEM. OVER PRESSURE BURST DISC BETWEEN THE LEFT INNER WING FUEL TANK AND THE CENTER FUEL TANK RUPTURED. FUEL TRANSFERRED FROM THE LEFT WING TO THE CENTER CAUSING AN IMBALANCE BETWEEN THE INNER WING TANKS.