N419UA

Part: ACCUMULATOR — UNKNOWN (GRN HYD SYS) · airframe 89,811 hrs · 35,749 cycles

ECAM CAUTION MESSAGE - G RSVR LO LVL MESSAGE INOP - HYD INFORMATION UPDATE: MARKED FOR SDR REPORTING, MANHOURS AND GROUND TIME UPDATED. REMOVED AND REPLACED GREEN HYD ACCUMULATOR. DID NOT PERFORM LEAK CHECK. PARTS USED: 40-0592-3-1245,QTY :1 00-0594-3-1415,QTY :1 31-2912-9-9001,QTY :1 40-0595-3-0708,QTY :1 40-0595-3-1983,QTY :1 1537119,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1537119 SN OFF 1483 IPC REFERENCE # 29-11-03-05A ACCUMULATOR, HY OFF 31-2912-9-9001 6707 ON 0000 ACCUMULATOR, HY OFF 31-2912-9-9001 6707 ON 31-2912-9-9001 0190. SERVICED ACCUMULATOR WITH NITROGEN AND PREFORMED LEAK CHECK, LEAK CHECK GOOD IAW AMM 29-11-42-400-001-A.

Part: RADOME — DAMAGED (NOSE) · airframe 87,350 hrs · 34,568 cycles

LIGHTNING STRIKE REPORTED LIGHTNING STRIKE NOSE CONEAPPROX 2000FT ON DEPCLIMB PHASE SYS OK. CREW REPORTS ONE LIGHTING BOLT STRUCK ON LH SIDE OF NOSE RADOME. PRELIM CHECK FOUND ONE BURNT SPOT ON RADOME LH SIDE, WILL NEED FURTHER INSPECTION. CREW STATE CANNOT TELL IF INSTRUMENTS BLINK AS THEY WERE TOTALLY BLIND BY THE LIGHT FOR ABOUT 10 SECOND. ALL INSTRUMENTS INCLUDING WEATHER RADAR OPS NML. ON THE TURN AROUND TO SFO. CREW STATES THAT IT WAS HAILING WHEN THE LIGHTING HIT. INSPECTION POST LIGHTNING STRIKE AT ZONE 1 NOSE RADOME FOUND BURN MARK FROM LIGHTNING ENTRANCE AT 9 O'CLOCK POS. RADOME REPLACEMENT ACOMPLISHED. REMOVED DAMAGED BASE PLATE. PERFORMED RESISTANCE CHECK OF RH WING TIP LOWER STATIC DISCHARGER.

Part: NONE — NONE (DOOR 2 RIGHT) · airframe 87,009 hrs · 34,405 cycles

LEVEL 1 CHRONIC - DOOR 2 RIGHT DOES NOT INDICATE ARMED ON DOOR/OXY PAGE WITH DOOR LOCKED AND ARMED. PLEASE T/S PER TSM 52-13-00-810-805-A. IF FAULT CANNOT BE DUPLICATED AND NO OTHER ISSUES ARE FOUND, PLEASE REPLACE PROX SW 7WN2. REPORT ALL FINDINGS AND ACTION TAKEN IS SIGN-OFF. THANK YOU. DENLM MERCIER. CARRIED BY ELB FAULT NOT CONFIRMED WITH DOOR 2R CLOSED, LOCKED AND ARMED. REPLACED PROX SWITCH 7WN2, REF AMM 52-73-11. OP CHK NML, REF AMM GROUND SIGNAL AT PIN A/C OF SWITCH 7WN2 GOOD. WIRE CHECK B/T 52-73-00. CONN 7WN2-A AND IND LIGHT 3WN2 PIN A/B TO H IS GOOD, REF TSM 52-13-00-810-805-A, FAULT ISOLATION STEP 4A1D AND ASM 52-73-01.

Part: NONE — UNSERVICEABLE (ELAC 2) · airframe 86,917 hrs · 34,362 cycles

F/CTL ALTN LAW REPORTED. NO PRESENT FAULTS POST FLIGHT REPORT FAULTS ALT LAW ELAC 2 IR DATA DISAGREE PERFORMED EFCS 1&2 NO FAULTS PERFORMED IR INTERFACE TEST NO FAULTS AFS TEST NO FAULTS REMOVED AND REPLACED ELAC 2 OPS TEST GOOD NO FAULTS IAW AMM 27-93-34-000-001-A ROTABLE PARTS CHANGE WAS INDICATED - TT # 1917116 SN OFF 1257 COMPUTER, ELEV/ OFF 31-2793-9-0031 1257 ON 31-2793-9-0031 1493

Part: FRAME — CRACKED (FR16) · airframe 86,245 hrs · 34,036 cycles

WHILE ACCOMPLISHING RE-INSPECTION OF HOLES #6, #A, #B, #C, AND #D COMMON TO THE LH FR16 DOUBLE JOGGLE AREA PER ECRA 5311-02437 REV A, CRACKS WERE NOTED IN HOLE #6 IN THE FRAME LAYER ONLY. NR: 9298294 INSPECTIONS AT LH FR16 UPPER DOUBLE JOGGLE AREA FRAME SPLICING ECRA 5311-02834 ON OR BEFORE THE AIRCRAFT REACHES 112,036 TOTAL BETWEEN DOOR STOPS 5 AND 6 PER PART 2 OF THE LATEST REVISION OF AIRCRAFT FLIGHT CYCLES. PERFORMED INTERIM REPAIR IAW ECRA 5311-02834 BY SPLICING IN SERVICEABLE FRAME SEGMENT @ LH FR16. ACCOMPLISH INITIAL APPROVED PER ECRA 5311-02834. ACCOMPLISH INITIAL INSPECTIONS AT TOMC-APPROVAL FROM SC1ELBYC COMMENT LH FR16 UPPER DOUBLE JOGGLE AREA FRAME SPLICING BETWEEN DOOR STOPS 5 AND 6 PER PART 2 OF THE LATEST REVISION OF ECRA 5311-02834 ON OR BEFORE THE AIRCRAFT REACHES 112,036 TOTAL AIRCRAFT FLIGHTCYCLES QC REVIEWED QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: PROFILE — CRACKED (RH AFT O/W EMER) · airframe 86,245 hrs · 34,036 cycles

RH AFT O/W EMERG EXIT LH LOAD TRANSMITTING PROFILE HAS A CRACK. GENERATED BY N078625 ON HAECO LCQ NR 9298273/34273 REMOVED AND REPLACED RH AFT O/W EMERG EXIT LH LOAD TRANSMITTING PROFILE IAW A320 SRM 51-72-11-911-001 ACMP BY MECH V918284 INSP BY V892442

Part: PROFILE — CRACKED (RH FWD O/W EMER) · airframe 86,245 hrs · 34,036 cycles

RH FWD O/W EMERG EXIT LH LOAD TRANSMITTING PROFILE HAS A CRACK. GENERATED BY N078625 ON HAECO LCQ NR 9298274/34274 REMOVED AND REPLACED RH FWD O/W EMERG EXIT LOAD TRANSMITTING PRO FILE IAW A320 SRM 51-72-11-911-001. ACMP BY MECH V918284 INSP BY V892442

Part: PROFILE — CRACKED (LH EMER EXIT) · airframe 86,245 hrs · 34,036 cycles

LH AFT O/W EMERGENCY EXIT LH LOAD TRANSMITTING PROFILE HAS A CRACK. GENERATED BY N078625 ON HAECO LCQ NR 9298272/34272 REMOVED AND REPLACED LH AFT O/W EMERG EXIT LH LOAD TRANSMITTING PROFILE IAW A320 SRM 51-72-11-911-001. ACMP BY MECH V918284 INSP BY V892442

Part: BLOCKER DOOR — DEPARTED (LH T/R) · airframe 85,525 hrs · 33,705 cycles

PDA 1 REF LOG PAGE 7855130: THIS ITEM CREATED TO FLAG FOUND ON ARRIVAL PART DEPARTED ACFT. THRUST REVERSER BLOCKER DOOR APPROXIMATELY 8 BY 12 INCHES METAL APPROXIMATELY 1 POUND MISSING FROM AIRCRAFT. REMOVED LH REVERSER FROM #2 ENGINE REF AMM78-32-01-000-010-A. ADD EMP:U101085,U377901,U377654 INSTALLED #2 L/H REVERSER REF 78-32-01-400-010-A. COMPLETED UP TO STEP M. CONTINUE ON WITH STEP N FOR T/R BLEED AND OPERATIONAL CHECK. ADD EMP:U375676,U375853,U376766 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1134725 SN OFF 1001 IPC REFERENCE # 78-30-00-81A

Part: FUEL CAP — MISSING (NA) · airframe 84,762 hrs · 33,337 cycles

PDA 2 - NO REMARKS ENTERED FOUND FUEL CAP MISSING ORDERED AND REPLACED FUEL CAP INSTALLED NEW FUEL CAP ROTABLE PARTS CHANGE WAS INDICATED - TT # 1937348 SN OFF 6619 CAP, COUPLING R OFF 31-2825-9-0001 6619 ON 31-2825-9-0001 0237

Part: CAP — MISSING (FUEL CELL) · airframe 83,758 hrs · 32,886 cycles

PDA 2 FUELER REPORTS MISSING FUEL CAP AND FUEL POINT RECEPTACLE. PHOTO ADDED.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 83,691 hrs · 32,858 cycles

ON DESCENT AT APPROX 20000 FEET CABIN ALT BEGAN TO CLIMB. GOT CA B PRSAFETY VALVE OPEN ECAM PFR SHOWED NO COORELATED FAILURE MESSAGES.PERFORMED CPC TESTS NO FAULTS NOTED. #2 PER AMM 21-31-00-710-002-A. BOTH CONTROLLERS PASSED WITH NO FAULTS. ALSO NEITHER CONTROLLER HAD ANY FAULTS ON LAST LEG PERFORMED CABIN PRESSURE CONTROLLER TESTS ON BOTH CPC #1 AND CPC ADD EMP:N REPORT OR PREVIOUS LEGS REPORT. SUSPECT OUTFLOW VALVE OPENED DURING FLIGHT BELOW DELTA P = 8.5 PSI (POSITIVE PRESSURE RELIEF) PERFORMED TSM 21-31-00-810-808-A FOR OPEN SAFETY VALVES, CHECKED ATTACHED) UNABLE TO VERIFY THAT SAFETY VALVES (6HL OR 7HL) POSITION OF VALVE (CLOSED), PULLED ECS REPORT 19 (SEE PIC FOR PRECAUTIONARY REASON REPLACED SAFETY VALVE 6HL REF 21-31-52 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1059285 SN OFF 2202 AS STATED ABOVE TESTS ON BOTH CPC''S REVEALED NO FAULTS AND PFR STATUS MESSAGES SHOWED NO ASSOCIATED FAILURE MESSAGES....WITH PRECAUTIONARY REASONS REPLACED OUTFLOW VALVE REF MM 21-31-51-400-001-A. RAN PRESSURE CONTROL TEST REF MM ADD EMP:U094578 INCOMPLETE DATA FROM ECS 19 ( SEE PREVIOUS UPDATE) AND FOR IPC REFERENCE # 21-31-51 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1994195 SN OFF 5713 21-31-00-710-002,003 SYSTEM CHECKS OK. PART ENTRY TT 1059285 ON S/N OFF 8202 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1059285 SN OFF 8202 VALVE, SAFETY O OFF 31-2131-9-0001 8202 ON 31-2131-9-0001 5567

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 83,456 hrs · 32,754 cycles

CABIN EMERGENCY LIGHTS OPERATIONAL CHECK: - GIVES MESSAGE OF "ESPU BATTERY EMER R". RESET EMER EXIT LIGHT BREAKERS NO HELP. REPLACED BATTERY PACK REF AMM 33-51-38-000-002-A & AMP; 33-51-38-400-002-A OPS CHECKED OK. INSPECTED REF AMM 33-51-38-000-002-A AND 33-51-38-400-002A OPS CHECK GOOD.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 82,578 hrs · 32,345 cycles

CRACK INDICATION (ROTO-HFEC) FASTNER HOLE AT FR24+8, STGR37L REMOVED AND REPLACED STRINGER 37L REPAIRSECTION FROM FR24-24+8 ELIMINATING FASTNER HOLE WITH CRACK INDICATION IAW A320 SRM53-00-13-300-001 AND SRI53-00-13-205-001 TABLE 2 INSPECTION THRESHOLD FROM TIME OF DL/REPAIR EMBODIMENT 60000FC/120000FH PLEASE REFERENCE CLOSE LP 4758390 APPROVED TO CARRY REF SRM53-00-13-300-001/ SRI53-00-13-205-001 INSPECTION TO BE ACCOMPLISHED 60,000 FC''S/120,000 FHRS FROM REPAIR EMBODIMENT TOMC-APPROVAL FROM SC1ELBYC COMMENT REVIEWED RECORDS UPDATE QC REVIEWED T/A: 60K FC OR 120K FH..................JQ

Part: SOLENOID VALVE — MALFUNCTIONED (7TH STAGE) · airframe 77,801 hrs · 30,201 cycles

LOW SPEED ABORT OF THE TAKEOFF AT 100KTS, DUE TO HIGH EGT ON THE NR 2 ENGINE. EEC REPLACED PRIOR TO LEG FOR SAME FAULT. MAINTENANCE REPLACED ALL BLEED SOLENOIDS 7A, B, C. D AND TMA SOLENOIDS. OPS CHECKED FOUND NORMAL IAW HIGH POWER ENGINE RUN.

Part: STRINGER — CORRODED (FRAMES 30-31) · airframe 76,489 hrs · 29,615 cycles

FWD CARGO STRINGER 42L DOUBLER CORRODED BETWEEN FRAMES 30 - 31. REMOVED AND REPLACED THE STRINGER DOUBLER .

Part: STRINGER — CORRODED (FRAMES 30-31) · airframe 76,489 hrs · 29,615 cycles

FWD CARGO CORRODED STRINGER DOUBLERS BETWEEN FR30/31 STGR 41LT REMOVED AND REPLACED THE STRINGER DOUBLER. INSTALLED A NEW DOUBLER.

Part: STRINGER — CORRODED (FRAMES 30-31) · airframe 76,489 hrs · 29,615 cycles

FWD CARGO , STRINGER 43L DOUBLER CORRODED BETWEEN FRAMES 30 - 31. REMOVED AND REPLACED THE DOUBLER.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 76,489 hrs · 29,615 cycles

BOTH OVERWING EXIT HATCH ESPU BATTERIES ARE DISCHARGED. REMOVED AND REPLACED THE BATTERIES IAW AMM 3 3-51-38-000-0002-A, 33-51-38-400-002-A, AND PERFORMED AN OPS TESTED IAW AMM 33-51-38-710-052-A. NO DEFECT FOUND.

Part: CLEAT — CORRODED (FRAME 28) · airframe 76,489 hrs · 29,615 cycles

CORROSION ON THE CLEATS. REMOVED AND REPLACED THE CLEATS AT FRAME 28 IAW SRM 51-25-00, 51-26-00, 51-72-11-911-001, 51-21-11-00, 51-28-11-911-004, AND DWG D53230399.

Part: STRINGER — CORRODED (FRAME 25) · airframe 76,489 hrs · 29,615 cycles

FWD CARGO HAS A CORRODED STRINGER 43L FWD OF FRAME 25. REMOVED, FABRICATED, LOCATED, AND DRILLED A STRINGER DOUBLER AND INSTALLED IAW SRM 51-42-11-001-2F, 53-00-13-300-001, 51- 25-00-001, 51-21-11, 51-23-11, NTM 51-10-17, 51-28-11-911-004, AND 51-10-01.

Part: STRINGER — CORRODED (FRAMES 25-26) · airframe 76,489 hrs · 29,615 cycles

FWD CARGO HAS A CORRODED STRINGER 41L DOUBLER BETWEEN FRAMES 25 - 26. REMOVED, FABRICATED, LOCATED AND DRILLED A NEW DOUBLER, AND INSTALLED IAW SRM 51-42-11-0012F, 53-00-13-300-001, 51-25-00-001, 51-21-11, 51-23-11, NTM 51-10-17, 51-2 8-11-911-004, AND 51-10-01.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 76,489 hrs · 29,615 cycles

WHILE REMOVING STR 31R AT FR67, SPLICE CONNECTOR SECTION FOUND TO BE CORRODED REMOVED CONNECTOR SPLICE SECTION AND FASTENERS AT FR67 STR 31R AND FABRICATED CONNECTOR SPLICE SECTION, MATCH DRILLED AND INSTALLED. RESTORED SURFACE PROTECTION IAW SRM 51-42-11-001 2.E, DWG D53480046, SRM 51-21-11-001, 51-23-11-001, 51-72-11-911-002 .

Part: SKIN — CORRODED (FUSELAGE) · airframe 76,489 hrs · 29,615 cycles

FUSELAGE EXTERNAL SURFACE AROUND VOR CABLE (4RSB) AT CONNECTION TO FIN 7102VC IS CORRODED. ACCOMPLISHED ALL STEPS OF ECRA 5341-01113.

Part: FRAME — CORRODED (FRM 16) · airframe 76,489 hrs · 29,615 cycles

L1 DOOR SILL FWD. GIRT BAR FITTING AT FRAME 16 HAS CORROSION. ACCOMPLISHED ALL STEPS OF ECRA 5311-01896.

Part: DOOR SILL — CORRODED (R1 DOORWAY) · airframe 76,489 hrs · 29,615 cycles

R1 DOOR SILL AFT OF AFT GIRT BAR FITTING ON FRAME 20 HAS CORROSION. ACCOMPLISHED ALL STEPS OF ECRA 5311-01890 PART 1.

Part: SKIN — CORRODED (FUSELAGE) · airframe 76,489 hrs · 29,615 cycles

FUSELAGE EXTERNAL SURFACE AROUND VOR HARNESS (4RSA) CONNECTION AT FIN 7113VC IS CORRODED. ACCOMPLISHED ECRA 5341-01113.

Part: STRINGER — CORRODED · airframe 76,489 hrs · 29,615 cycles

STR 38L TO 42R FROM FRAME 57 TO 58 HAS CORROSION. REMOVED 6 FASTENERS AT STR 41C AND 3 FASTENERS AT STR43L BETWEEN FR57 . REMOVED GUSSET PLATE AT FR58 AT STR 42L-43L, BLENDED CORROSION AT STR 41L AND STR 43L FR57 TO FR58. UT THICKNESS AND ROTOPROBE PERFORMED, NO CRACKS NOTED. STRINGER 43L FOUND TO BE OUT OF LIMITS BETWEEN FR54 AND FR60. REMOVED AND REPLACED STR 43L AT FR54 TO FR 58 INSTALLED REPAIR ANGLE AND RESTORED PROTECTIVE IAW A320 SRM 51-42-11-001 SRM 51-74-00-001, CRM 51- 21-11-001, SRM 51-23-11-00; ARM 53-00-13-300-002, NTM 51-10-04.

Part: STRINGER — CORRODED (FRAMES 54-60) · airframe 76,489 hrs · 29,615 cycles

FRAMES 54 TO 60, STRINGER 43L WAS FOUND CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 5142-11-001, SRM 51-44-11-001, SRM 51-21-11-001, SRM 51-23-11-001, NTM 51-10-01, DWG D53470656, AND ER5100R01017

Part: STRINGER — CORRODED (FRAMES 56-57) · airframe 76,489 hrs · 29,615 cycles

STRINGER 42R, FRAMES 56 TO 57 CORRODED. BLENDED THE CORROSION AND FOUND TO OUT OF LIMITS. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-11-001, 51-74-00-001, 53 -00-13-300-002, 51-21-11-001,51-23-11-001, NTM 51-10-01, AND NTM 51-10-04.

Part: STRINGER — CORRODED (FRAMES 54-60) · airframe 76,489 hrs · 29,615 cycles

STRINGER 43R, FRAMES 54 TO 60 CORRODED. BLENDED AREA THICKNESS AND ROTOPROBE PERFORMED, NO CRACKS NOTED. FOUND STRINGER 43L FOUND TO BE OUT OF LIMITS. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-42-11-001, SRM 51-74-00-001, SRM 53-00-13-300-002, SRM 51-21-11-001, SRM 51-23-11-001, NTM 51-10-01, AND NTM 51-10-01.

Part: FLOOR SUPPORT — CORRODED (FRAMES 65-66) · airframe 76,489 hrs · 29,615 cycles

AFT CARGO FLOOR SUPPORT, FRAMES 65 TO 66 HAS CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11-001, SRM 51-74-00-001, SRM 53-00-13-300-002, SRM 51-21-11-001, SRM 51-23-11-001, NTM 51-10-01, AND NTM 51-10-01.

Part: DOOR SILL — CORRODED (L2 DOOR) · airframe 76,489 hrs · 29,615 cycles

L2 DOOR SILL CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-72-11-911-001 AND SRM 51-75-12-911-003.

Part: FITTING — CORRODED (FRAME 68) · airframe 76,489 hrs · 29,615 cycles

AFTER REMOVAL OF THE L2 DOOR SILL, CORROSION WAS FOUND ON FRAME 68 FLOORBEAM TO FRAME CONNECTION FITTING. REMOVED AND REPLACED THE FITTING IAW SRM 51-72-11-911-001.

Part: SUPPORT BRACKET — CORRODED (FRAMES 69-70) · airframe 76,489 hrs · 29,615 cycles

CORROSION FOUND ON THE RT SHEAR PLATE SUPPORT BRACKET FRAMES 69 - 70. REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-72-11-911-001.

Part: FITTING — CORRODED (THRESHOLD) · airframe 76,489 hrs · 29,615 cycles

DURING CORROSION REMOVAL ON FWD FACE OF FRAME 20, CORROSION WAS FOUND ON THE LOWER AFT CORNER FITTING OF THE R1 DOOR. REMOVED & REPLACED THE THRESHOLD FITTING IAW SRM 51- 72-11-911-001. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-13-300-PB201, AND 51-73-00-001

Part: LAMP — NO TEST (EMERGENCY LIGHT) · airframe 76,228 hrs · 29,472 cycles

EPSU DISPLAYED DURING EMERGENCY LIGHT TEST. REPLACED THE LAMPS IAW MM 33-51-15. OPS TESTED OK.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 76,228 hrs · 29,472 cycles

EPSU DISPLAYED AFTER EMERGENCY LIGHT TEST. TESTED AFT LEFT EPSU. TEST INDICATED A FAULT. REPLACED THE BATTERY PACK IAW AMM 25-23-45-000-003-A, CHECKED OK.

Part: LINE — TORN (CABIN) · airframe 76,139 hrs · 29,424 cycles

OVERWING EMERG EXIT LIFE LINE GAB TORN. REPLACED LIFE LINE . ALL OK.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 75,986 hrs · 29,339 cycles

EMERGENCY LIGHTS TEST MESSAGE, BATTERY EMERGENCY LIGHT, REPLACED THE MID LEFT BATTERY IAW MM 33-51-38. BATTERY CHECKED GOOD.

Part: ALTIMETER — READS HIGH (STANDBY) · airframe 75,065 hrs · 28,922 cycles

STBY ALTIMETER READS 900 FT HIGH AT FL310. REPLACED STBY ALTIMETER IAW AMM 31-21-22.

Part: POWER SUPPLY — FAULTED (CABIN) · airframe 74,238 hrs · 28,574 cycles

LT EMERGENCY LIGHT UNIT FAULT. REPLACED EMER LT POWER SUPPLY AT LT OVERWING EMER EXT POS. OPS C HECK AND SELF TEST ARE GOOD REF AMM 33-51-38.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 74,238 hrs · 28,574 cycles

EMERGENCY LIGHT BATTERY LEFT AFT FAULT REMOVED AND REPLACED LEFT AFT EMERGENCY BATTERY PACK REF AMM 33-51-38. OPS CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 73,674 hrs · 28,320 cycles

EMERGENCY LIGHT SYS TEST FAILED ON 2SVC SYS TEST DOOR 1L ESCAPE SLIDE LIGHTING IS INOP BROKEN WIRE BETWEEN CON N 2871VC PIN B AND 2819VC PIN K, OF DOOR 1L WIRE HARENESS. 2871V C IS BEHIND DOOR SLIDE AND 2819VC IS BEHIND FWD LAV. REPAIRED BROKEN GROUND WIRE AT DOOR 1L HINGE AREA, CHKS GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 71,783 hrs · 27,445 cycles

SEAT 2B EMER LIGHT ASSEMBLY BROKEN. REPLACED EMER LIGHT ASSEMBLY IN SEAT SIDE PANEL IAW AMM 33-51-18. EMER LIGHT TESTED OK IAW AMM 33-51-00-710-001.

Part: STOP FITTING — GOUGED (FUSELAGE) · airframe 68,387 hrs · 26,009 cycles

R2 DOOR CUT OUT FRAME 68 DOOR STOP FITTING NR 2, ALL 4 ATTACH HOLES HAVE GOUGES. REAMED UPPER INBD & OTBD TO .263 INCHES, LOWER INBD TO .26 3 INCHES, LOWER OTBD .265 INCHES. REPAIRED IAW SRM 53-41-12 PAR 5 D.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,387 hrs · 26,009 cycles

R2 DOOR CUT OUT FRAME 66 DOOR STOP FITTING NR 6 LOWER INBD HOLE IS CRACKED IN THE WEB AT 2 O'CLOCK POSITION. REAMED HOLE TO .268 INCHES. REPAIRED IAW SRM 53-41-1 2 PAR 5 D.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 68,387 hrs · 26,009 cycles

R2 DOOR CUT OUT FRAME 68 DOOR STOP FITTING NR 5 LOWER INBD HOLE IS OUT OF ROUND IN THE FRAME WEB. REAMED TO .265 INCHES. REPAIRED IAW SRM 53-41-12 PAR 5 D.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 68,387 hrs · 26,009 cycles

R2 DOOR CUT OUT FRAME 66 RT DOOR STOP FITTING NR 5 UPPER INBD HOLE IS CRACKED IN THE WEB AT 2 O'CLOCK POSITION. REAMED TO .278 INCHES & REPAIRED IAW SRM 53-41-12 PAR 5 D.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 65,862 hrs · 25,008 cycles

PASSENGER SEAT OVERHEAD 02 MASK FELL AT 2E & 2F. REQUIRES MASK DROP AMM35- 23-00-710-001.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 65,246 hrs · 24,759 cycles

AIRCRAFT REJECTED TAKEOFF AT 100 KTS DUE TO AFT CARGO DOOR INDICATION.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 65,182 hrs · 24,740 cycles

VENT AVIONICS SYS FAULT. RESET BREAKERS D05 D06 Y1 7 FAULT CLEARED.

Part: COMPUTER — FAULTED (NR 1 ELAC) · airframe 64,907 hrs · 24,637 cycles

ELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. GOT ECAM WHEN NR 1 GENERATOR CAME ONLINE. CYCLED ELAC 1 IAW FM. ACCOMPLISH CHRONIC REVIEW. ITEM ROLLED FORWARD. ELAC 1 PITCH FAULT. IAW DF 2793A.

Part: SERVO CONTROL — UNKNOWN (LT ELEVATOR) · airframe 64,905 hrs · 24,636 cycles

IAW CH8798 REQ LT ELEV SERVO CTRL 34-CE-1 REPLACEMENT. R & R LT ELEV SERVO CTRL 34-CE-1 IAW AMM 27-34-51-400-001-A UP TO INCLUDING STEP 4F2.

Part: COMPUTER — FAULTY (NR 1) · airframe 64,768 hrs · 24,588 cycles

SEC 1 ECAM MSG SHOWN. REPLACED COMPUTER. REPLACED SEC 1 COMPUTER IAW MM & ACCOMPLISHED OPERATIONS CHECK IAW MM, CHECKED OK. CORRECT OPERATIONS CHECK IAW TO 27-94-00-710-002-A

Part: APU — LEAKING (APU BAY) · airframe 64,659 hrs · 24,547 cycles

STRONG PUNGENT ODOR THROUGHOUT CABIN, MAKING CABIN CREW NAUSEOUS. REPLACED APU FOR OIL INTERNAL LEAKAGE.

Part: COOLING FAN — FAULTY (APU) · airframe 64,659 hrs · 24,547 cycles

OIL SMELL IN CABIN IAW TSM 49-00-00-810-921-A12, FOUND OIL CONTAMINATION IN APU PMG & COOLING FAN ASSEMBLY. REPLACED APU PMG & COOLING FAN ASSEMBLY IAW MM.

Part: CLAMP — MISSING (ENTERTAIN SYS) · airframe 64,659 hrs · 24,547 cycles

WORKING WITH SMC 6, INSTALLING CLAMPS FOUND HARDWARE MISSING 2 CLAMPS MS21919WDG3 & 1 CLAMP MS21919WDG IAW IPC 23-32-01-01 CLAMPS LOOSE. ALSO NEED .010 SAFETY WIRE FOR COAX CONNECTION TO BROADBAND BASE TX & RX CONNECTORS. STARTED REMOVAL OF GCS ANTENNA & RADOME. COMPLETED THRU STEP 2 C 2H IAW AMM SUPPLEMENT 23-32-01 DOCUMENT 10T140R109. RADOME HARDWARE PLACED IN FOAM GUIDE WITH RADOME ON LIFT PLANESIDE. ANTENNA HARDWARE & CLAMP HARDWARE DISASSEMBLED & PLACED ON A - C ADAPTER PLATE. INSTALLED NEW CLAMPS & SAFE TIED BOTH COAX CONNECTORS TO BROADBAND BASE TX & RX IAW IPC 23-32-01. SECURED OTHER LOOSE CLAMPS ALONG COAX CABLES.

Part: COMPUTER — FAULTY (NR 2 ELAC) · airframe 64,648 hrs · 24,542 cycles

FLIGHT CONTROL ELEV SERVO FAULT DURING FLIGHT CONTROL CHECK ON TAXI OUT. REPLACED ELAC 2 IAW AMM 27-93-34 ACP CAT III TEST FULL AUTO LAND CAPABLE.

Part: CHECK VALVE — LEAKING (RT WING) · airframe 64,616 hrs · 24,527 cycles

FUEL DRIPPING FROM RT WING. REPLACED RT WING SURGE TANK DRAIN VLV. AFTER REPLACING WATER DRAIN VLV SURGE TANK STILL FILLING WITH FUEL THROUGH SCAVENGE JET PUMP SUCTION LINE. CHECK VLV AT RIB 22 LEAKING, REPLACED CHECK VLV, CHECKED GOOD.

Part: CONTROL UNIT — FAULTED (NR 1) · airframe 64,175 hrs · 24,374 cycles

UNABLE TO SELECT HEADING WHILE IN NAV MODE. REPLACED CONROL UNIT PER AMM. PERFORMED CAT III PER AMM 22-97-00. OPS CHECKED GOOD.

Part: MOUNT BRACKET — BROKEN (CRASH AXE) · airframe 63,887 hrs · 24,261 cycles

COCKPIT CRASH AXE HAS A BROKEN SADDLE MOUNTING BRACKET. INSTALLED NEW BRACKET.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,749 hrs · 24,205 cycles

ACCOMPLISHED BLEND OUT OF LIGHTING STRIKE FOUND IN THE UNPAINTED AREA SURROUNDING THE PILOTS STATIC PORTS ON THE RT SIDE NEAR FR24 TO AVO2262 AND SRM 51-73-00. NEED TO ACCOMPLISH HFEC INSPECTION IAW AVO2262 AND CONTACT ENGINEERING WHEN COMPLETE. ACP HFEC INSP BOTH SIDES, NO CRACKS INDICATED.

Part: SKIN — DENTED (FUSELAGE) · airframe 63,743 hrs · 24,203 cycles

DENT FOUND FWD OF L1 DOOR AT FRAME 12 APPROX .046 DEEP. REMOVED FASTENERS CUT OUT FUSELAGE SKIN AT FRAME 12 IAW SRM 53-00-11, FIG 213, FABRICATED REPAIR DOUBLER & INSTALLED IAW SRM 53-00-11, FIG 213.

Part: LENS — DISLODGED (R1 DOOR) · airframe 63,717 hrs · 24,193 cycles

R1 DOOR CABIN PRESSURE LIGHT COVER FELL OFF. SECURED LENS COVER.

Part: HANDSET — MALFUNCTIONED (L2 DOOR) · airframe 63,464 hrs · 24,091 cycles

AFT F/A HANDSET MAKING NOISE. REPLACED HANDSET AT L2 DOOR. OPS CHECKED OK.

Part: SEAL — MISSING (PANEL) · airframe 63,087 hrs · 23,946 cycles

PRESSURE LEAK AROUND 22A EXIT WINDOW. DEBRIEFED CABIN CREW AND FLIGHT CREW, FLIGHT CREW REPORTED NO PRESSURIZATION LOSS, CABIN CREW STATED THERE WAS NO AIR NOISE (LEAK) BUT A SLIGHT HUM. REMOVED HATCH AT SEAT 21A. ACCOMPLISHED VISUAL INSPECTION NO DEFECTS NOTED, CLEAN AND LUBE SEAL PRECAUTIONARY, REINSTALLED HATCH REF AMM 52-21-11-000-001-A. FOUND PANEL 191BT FWD UPPER 101062 CORNER 1" OF SEAL MISSING. TAPED AREA IAW AMM MT53-004. DL1468 CREATED TO MONITOR. VISUAL INSP NO DEFECTS NOTED.

Part: COMPUTER — FAULTY (SLAT SYSTEM) · airframe 63,072 hrs · 23,940 cycles

SLAT SYSTEM 2 FAULT. ATTEMPTED RESET NO-JOY. REPLACED NR 2 SFCC IAW MM 27-51-34.

Part: CONNECTOR — UNSECURE (LAVATORY) · airframe 62,812 hrs · 23,837 cycles

LAVATORY TOILET BOWL FLUSH SYSTEM INOPERATIVE AT FWD CAB LT LAV. SECURED LOOSE CONNECTOR AT FCU. OPERATIONAL CHECK NORMAL.

Part: ACOUSTIC PANEL — DAMAGED (NR 2 ENGINE) · airframe 62,808 hrs · 23,836 cycles

ACOUSTICAL PNL ON INLETOF ENG 2 MISSING A CHUNK AT THE 6 O'CLOCK POSITION. FAN CASE ATTRITION LINER HAS MISSING MATERIAL AT 6 O'CLOCK POSITION TOP LAYER MEASURING 2"X 1.750" NEEDS TO BE REPAIRED WITHIN 20 CYCLES. RPR- :REPAIRED ATTRITION LINER AT 6 O'CLOCK POSITION IAW MT 72-017.

Part: LIFE VEST — UNSECURE (CABNI) · airframe 62,339 hrs · 23,649 cycles

PAX FROM SEVERAL SEAT ROWS ARE HOLDING THE LIFE VEST FROM THEIR SEAT. RE-SECURED LIFE VESTS.

Part: SLIDING WINDOW — FAULTY (COCKPIT) · airframe 61,875 hrs · 23,467 cycles

FIRST OFFICER'S SLIDING WINDOW HEATING INOP. CREW COMMENTS: ECAM ON TAXI OUT SAYS ANTI-ICE R WINDOW. SAMC TEXT: CFDS SHOWS F-O FIX LATERAL WINDOW INOP. RESISTANCE OF FIXED LATERAL WINDOW IS HIGH. WILL NEED WINDOW REPLACED. R&R FO'S FIXED LATERAL WINDOW PER MM.

Part: TRUNNION — SHEARED (R1 DOOR) · airframe 62,149 hrs · 23,197 cycles

TRUNNION ASSY FOUND SHEARED AT LOWER END ON R1 DOOR. COMPLETED INSTALLED SPRING ROD. OPS OF DOOR NORMAL.

Part: TARGET — LOOSE (L1 DOOR) · airframe 61,144 hrs · 23,153 cycles

DOOR 1L IND NOT ARMED ON DOOR-OXY PAGE WITH DOOR HANDLE IN ARMED POS. FOUND PROX SWITCH 4WN1 TARGET LOCK NUT AND LOCKING TAB NOT INSTALLED. FOUND PARTS LOOSE IN DOOR. ADJUSTED TARGET AND INSTALLED TARGET NUT AND LOCKING TAB-WASHER PER AMM. OPERATIONAL TEST GOOD. INDICATIONS ON DOOR PAGE OKAY.

Part: TRANSFORMER — FAILED (STATIC INVERTER) · airframe 60,767 hrs · 22,999 cycles

STATIC INVERTER IS FAILED TEST. REPLACED NR 2 TRANSFORMER RECTIFIER PER AMM, OPS CHECK GOOD.

Part: WINDSHIELD — FAULTY (COCKPIT) · airframe 60,685 hrs · 22,965 cycles

RIGHT WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN. - ANTI ICE. STILL FAILS WINDSHIELD SENSOR. REMOVED JUMPER & WINDOW BACK TO ORIGINAL CONFIG. SUSPECT WINDSHIELD CHANGE. RESET WHC NR 2 C/B'S AND BOTH C-P ON WHC NR 2. ACP OPERATIONAL TEST OF WHC NR 2 REF MM. ALL GND TESTS GOOD. RE-OPENED FOR: FAULT REOCCURED. INSTALLED NEW WINDSHIELD PER MM.

Part: COMPUTER — FAULTY (RUDDER) · airframe 60,475 hrs · 22,884 cycles

DUE TO RUDDER UNCOMMANDED MOVEMENT, REPLACED BOTH FAC1 AND FAC 2. REPLACED FAC 1 AND FAC2 COMPUTERS.

Part: COMPUTER — MALFUNCTIONED (NR 2 ELAC) · airframe 60,427 hrs · 22,863 cycles

ELAC 2 FAULT TRIGGERS PRIORITY LEFT AURAL WARNING AND ALL AMBER INDICATIONS ON F-CTL. REPLACED ELAC 2 PER AMM, CHECKED NORMAL.

Part: OXYGEN MASK — DETACHED (OXYGEN BOTTLE) · airframe 60,330 hrs · 22,828 cycles

O2 BOTTLE ABV SEAT 37E, MASK IS NOT ATTACHED. REPLACED O2 BOTTLE.

Part: WINDSHIELD — DEFECTIVE (COCKPIT) · airframe 59,849 hrs · 22,637 cycles

L WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN. ANTI ICE, REPLACED CAPTAINS WINDSHIELD. REPLACED WINDOW HEAT CONTROLLER 2DG1, COMPLETED OPERATIONAL TEST OF THE WINDSHIELD ANTI-ICING AND DEFOGGING. OPS CHECKS GOOD.

Part: WIRE — SHORTED (PITOT HEAT) · airframe 59,631 hrs · 22,540 cycles

STBY PITOT DISPLAYED ON UPPER ECAM SCREEN. ANTI ICE STANDBY PITOT RIGHT AFTER TO WENT OUT 20 SECS LATER. REPLACED SHORTED WIRE IN CONDUIT 25GA REF PTT 6312001. PERFORMED TEST OF PHC3 IAW A320 MM 30-31-00. SYSTEM OP CHECKED GOOD. LGC1U PHC3 INTERFACE CORRECTED ON E4355I.

Part: WIRE — SHORTED (NLG SENSOR) · airframe 59,631 hrs · 22,540 cycles

NOSE LANDING GEAR DID NOT RETRACT ON FIRST ATTEMPT. SECOND ATTEMPT NORMAL. ASSOCIATED STANBY PITOT DISPLAYED ON ECAM. 25GAM SENSOR FAULTED ON CFDS. REPLACED SHORTED WIRES IN CONDUIT TO 25GA NLG SENSOR PER ESPM 20-33-11 AND AWM 32-21-03. ACCOMPLISHED OP CHECK PER MM 32-69-00 AND ACCOMPLISHED TEN SUCCESSFUL GEAR SWINGS, NO FAULTS FOUND REF NRE4355I.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,609 hrs · 22,532 cycles

AFT PIT HAS CORROSION ON STR 43L BETWEEN FR 52 + 60. REPLACED FACTORY STRINGER SECTION ON NR #E8396E.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,609 hrs · 22,532 cycles

AFT PIT HAS CORROSION ON STR 42L, BETWEEN FR 53 - 60. MAJOR REPAIR. INSTALLED STRINGER REPAIR PER SRM ON NR #E8395E BY #395958 AND INSPECTED. PER SRI 53-00-13-2-001-00 TABLE 209, MUST REINSPECT AT 60000C OR 75000T FROM REPAIR EMBODIMENT. CURRENT PTC 22532 AND PTT 59609. REINSPECT AT 60000C OR 75 000T FROM REPAIR EMBODIMENT PER SRI. RII ACCOMPLISHED ON NON ROUTINE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,609 hrs · 22,532 cycles

FWD CARGO PIT STRINGER 41R, BETWEEN FR 31 + 32, PREVIOUS REPAIR AND STRINGER CORRODED. THIS ITEM REPAIRED, SEE CF9077. SAME STR REPAIRED WITH NEW SECTION OF STR 41R. THE SRI IS ALSO COVERED. THE 2 STR LOCATIONS RPR WITH ONE RPR. N-R E8399E, E8398E BETWEEN FR 30 - 32.

Part: CLEAT — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 59,609 hrs · 22,532 cycles

FWD PIT, FR 33, STR 44L TO 38L CLEATS HAVE CORR. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED CLEATS, FAB NEW CLEATS. INSTALL NEW CLEATS. 1. 5EA CLEATS REPLACED. N-R E8777E.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,609 hrs · 22,532 cycles

FWD PIT, FR 31, STR 42R-41R CLEAT HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW CLEAT. FABRICATED PER SRM. INSTALLED REF SRM N-R E8778E.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,609 hrs · 22,532 cycles

FWD CARGO PIT STRINGER 41R, BETWEEN FR 30 + 31, PREVIOUS REPAIR IS CORRODED. REMOVED DAMAGED SECTION OF STR 41R, BETWEEN FR 30 AND 32. INSTALLED NEW SECTION STR AND SPLICES. THIS RPR REQUIRES REINSP 60,000 CYC AFTER EMBODIMENT. CURRENT PTC 22532. REINSP REF SRI TABLE 203. 60,000 CYC AFTER EMBODIMENT OF RPR. ACCOMPLISH RII INSPECTION OF AMIS ITEM 6092218 :REINSP REF SRI 53-21-13 TABLE 203. 60,000 CYC AFTER EMBODIMENT OF RPR.

Part: DOOR SEAL — CONTAMINATED (OVERWING EXIT) · airframe 62,443 hrs · 23,696 cycles

REF LOG 3, PRESSURIZED AIRCRAFT AND FOUND LEFT AFT OVERWING HATCH LEAK, BOTTOM OF HATCH OPENING. REMOVED AFT LEFT HATCH PER AMM, CLEANED HEAVY RESIDUE FROM SEAL AND HATCH OPENING. RE-INSTALLED PER AMM. OK FOR SERVICE.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 59,385 hrs · 22,438 cycles

FLOOR IN FIRST CLASS CABIN IS SOFT AND SPONGY. REPLACED FLOORBOARD.

Part: BUTTON — MISSING (CABIN) · airframe 59,264 hrs · 22,386 cycles

DURING TEST OF EMERGENCY O2, FOUND PULL OUT TEST BUTTON MISSING FROM OVHD PNL OF SEAT 24FED. PART ON ORDER & PNL HANGING DOWN FOR ACCESS. RPL'D BUTTON.

Part: CONE — CRACKED (NR 2 ENGINE) · airframe 59,264 hrs · 22,386 cycles

CRACK IN NR 2 ENG EXHAUST CONE. REPLACED REF MM.

Part: PANEL — UNSECURE (EMERGENCY EXIT) · airframe 58,467 hrs · 22,051 cycles

RT AFT EMER EXIT DISPLAYED ON UPPER ECAM SCREEN - DOOR. CREW COMMENTS: INTERIOR PANEL FELL OFF AND TRIGGERED ECAM. SECURED INTERIOR PANEL FOR RT EMER EXIT, NO MESSAGE DISPLAYED ON ECAM.

Part: SOLENOID — DAMAGED (COMPRESSOR DUCT) · airframe 58,437 hrs · 22,041 cycles

NR 2 ENGINE COMPRESSOR DUCT DAMAGE IN AREA OF 10TH STAGE COMP BLEED VALVE, AND EXPANDED ECM DATA FLT 9921-23 CRZ CELL E354 CH B FAULT. REPLACED 10TH STAGE SOLENOID, CHECKED OKAY.

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 57,816 hrs · 21,769 cycles

NR 1 ENG BIRD STRIKE. NR 1 FEC, STG 6 HPT 60% AIRFOIL MISSING. SUBSEQUENT WRITEUP FOR REMOVAL ACCT HPC STAGE 6 AIRFOIL DAMAGE. NR 1 ENG NOSE COWL 1 & 6 O'CLOCK APPEARS TO HAVE GONE INTO ENGINE AND LT WING PANEL 521AB NEAR FUSELAGE. BIRD STRIKE INSPECTION COMPLETED. ELEVATOR DELAM WITHIN LIMITS FOR 'C' CHECK. STARTING TO REMOVE ENGINE. ALSO HAVE PIT HYD LEAK. ENG REMOVED.

Part: FASTENER — MISSING (NR 1 ENG EXHAUST) · airframe 57,620 hrs · 21,677 cycles

NR 1 ENGINE HAS 1 RIVET MISSING AFT INSIDE TAIL CONE AT LOWER SUPPORT. MISSING RIVET IS LOCATED AT THE 11 :00 POSITION AFT LOOKING FORWARD.

Part: LIGHT — BROKEN (CABIN) · airframe 56,938 hrs · 21,395 cycles

LT SEAT ROW 11 EMERGENCY LIGHT ASSY IS BROKEN. REPLACED EMERGENCY LIGHT ASSY IAW AMM, OP CHECK GOOD IAW AMM ON NR V0325.

Part: SEAT — UNSERVICEABLE (CAPTAIN'S) · airframe 56,633 hrs · 21,260 cycles

CAPTAIN SEAT UNUSEABLE. PEDESTAL COMES COMPLETELY OUT OF BASE. R & R CAPT SEAT IAW AMM 25-11-51, OPS CHECKED NORMAL.

Part: SKIN — CRACKED (MLG DOOR) · airframe 56,091 hrs · 20,993 cycles

CRACK FOUND ON RT MLG DOOR. FOUND LESS THAN 1-4 INCH LENGTH CRACK ON RT GEAR DOOR FWD OUTER SKIN. NO WATER DAMAGE FOUND AND NO DAMAGE UNDER SKIN. SPEED TAPE AREA. AREA IS UPPER TOP SKIN OF RT GEAR DOOR WHEN DOOR IS UP POSITION. RECHECK TAPE AFTER EVERY DEPARTURE. TAPE SECURE.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 55,973 hrs · 20,926 cycles

FOUND APPROX 3 INCH X 4 INCH GASH ON THE LWR SIDE OF THE LT HORIZ STAB L/E. DAMAGE IS APPROX 6 INCHES FROM L/E. STOP DRILLED THE CRACK ON BOTH ENDS, AND SPEED TAPE AREA TO PROTECT FROM WATER INGRESSION. R & R DAMAGED HORIZONTAL STAB FIXED L/E OTBD SECTION.

Part: PANEL — MISINSTALLED (LAVATORY) · airframe 55,017 hrs · 20,444 cycles

AFT LAV PANEL IS INADEQUATE. FBO MECHANIC STATED THAT PANEL APPEARS TO BE INSTALLED UPSIDE DOWN, WHICH WOULD CAUSE BUTTON TO BE IN WRONG POSITION. PANEL WAS REPLACED WITH THE CORRECT PANEL. NOW THE FLUSH TOUCH BUTTON IS VISIBLE AT THE UPPER LT CORNER.

Part: FAN — FAILED (RECIRCULATION) · airframe 53,737 hrs · 19,848 cycles

BURNING ODOR THROUGHOUT CABIN & FLT DECK AT CRUISE ALTITUDE TWICE FOR APPROX 30 SECS. CONTINUOUS TRACE ODOR REMAINS. SEEMS TO GET WORSE WHEN CABIN TEMP IS ADJUSTED. LT RECIRCULATION FAN INDICATING AMBER ON COND PAGE A SHORT TIME AFTER SMELL WAS NOTICED. PFR GRIPES RECIRCULATION FAN 1 15H G FAILED. OPENED CARGO PIT INSPECTED RECIRCULATION FAN AREA, ALL NORMAL. VERIFIED RECIRCULATION FAN NOT OPERATING. DEF IAW MEL. REPLACED LT RECIRCULATION FAN AND CHECK VALVE REF MM. OP CHECK OK. REPLACED LT RECIRCULATION FAN FILTER DUE TO RECIRCULATION FAN FAILURE AND APPEARS TO BE CLOGGED. ALSO RT RECIRCULATION APPEARS TO BE JUST AS CLOGGED. REPLACED LT AND RT RECIRCULATION FILTERS, SYS TESTS OK.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 53,674 hrs · 19,813 cycles

CIDS FAILS SELF TEST IAW 3SVC. TROUBLE SHOT DOWN TO 2 OVERWING EXIT LIGHTS ON LT SIDE OF ACFT ARE INOP. UNABLE TO GET SCREWS OUT. BULB PCN 560-2375, TO BE REPLACED AT FIRST MAINT OPPORTUNITY. R& R POWER SUPPLY. CONTINUED TO TROUBLE SHOT SYS. FOUND DAMAGED WIRE AT STA 2979 LT IN CABIN. FROM CONNECTOR 7260VC10 TO SEATS. REPAIRED DAMAGED WIRES, CIDS RESET. SYS TESTS OK.

Part: FLAP — DAMAGED (RT WING) · airframe 53,306 hrs · 19,623 cycles

RIGHT O/B FLAP DAMAGED. REPAIR ACP'D ON C CHECK PACKAGE. TEST FLIGHT SUCCESSFUL FOR FLAP CHANGE.

Part: OXYGEN SYSTEM — LEAKING (CAPTAIN'S) · airframe 52,963 hrs · 19,450 cycles

CAPT O2 BOX EXTENDED TO FAR TEST BUTTON WILL NOT ENGAGE PIN FOR VALVE. R & R CAPT'S OXYGEN BOX. OPS CHECKED GOOD. NO DROP IN PSI NOTED.

Part: MICROPHONE — FAULTY (OXYGEN MASK) · airframe 52,963 hrs · 19,450 cycles

FO'S OXYGEN MASK MICROPHONE IS INOPERATIVE. REPLACED O2 MASK. OP CHECKS GOOD.

Part: FITTING — CORRODED (GIRT BAR) · airframe 52,685 hrs · 19,306 cycles

LT AFT ENTRY DOOR AND RT AFT SERVICE DOOR AFT AND FWD GIRT BAR FLOOR FITTING MOUNTING PLATE FOUND CORRODED. REMOVED AND REPLACED GIRT BAR MOUNTING FITTING. CHECKED ADJUSTMENT OF GIRT BAR FITTING.

Part: LIGHT — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,685 hrs · 19,306 cycles

RT AFT LWR EMERGENCY EXIT LITE INOP AT DOOR 2R. TROUBLESHOT AFT EMERGENCY LIGHT. REPLACED MOLEX PIN IN EXIT LIGHT CONNECTOR. ACP OPS CHECK OF EMERGENCY LIGHTING SYS. OPS CHECKED NORMAL.

Part: HANDLE — OUT OF POSITION (AFT CARGO DOOR) · airframe 52,167 hrs · 19,041 cycles

AFT CARGO ECAM MSG, RTFL. FOUND CARGO DOOR HANDLE NOT FLUSH WITH DOOR EXTERIOR. STOWING HANDLE MADE ECAM WARNING GO AWAY. OPERATED HANDLE SEVERAL TIMES, LIGHT CAME ON EACH TIME HANDLE NOT STOWED, WENT OUT WHEN HANDLE STOWED. SAMC CONTROLLER AND MANAGER CONCUR THAT THE AIRPLANE CAN BE RELEASED BACK TO SERVICE.

Part: PROBE — MALFUNCTIONED (TAT) · airframe 51,908 hrs · 18,937 cycles

AC ABRUPTLY PITCHED DOWN ON APPROACH TO DIA ON AP2, 1500 FT ALT AC PITCHED NOSE DOWN APPROX 5 DEG, 2300 FT PER MIN DESCENT RATE. DISCONNECTED AP AND LANDED NORMALLY. ITEM HAS HISTORY WHICH SHOWS PHC 1 REPLACED. PFR SHOWED THE INTERMITTANT ECAM WITH FAILURE MSG "CHECK TAT PHC1 SUPPLY". NEEDS MORE T/S. REPLACED CAPT'S TAT PROBE. CYC FMGC CB. ACP AUTO LAND TEST. OPS CHECKS OKAY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,879 hrs · 18,923 cycles

EMERGENCY LIGHT TEST FAILED COMM FWD L, EMER R. REPLACED BATTERY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,879 hrs · 18,923 cycles

EMERGENCY LIGHT TEST FAILED COMM EMER L, AFT L. REPLACED BATTERY PACK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,879 hrs · 18,923 cycles

EMERGENCY LIGHT TEST FAILED BATTERY FWD L. REPLACED 10LW BATTERY PACK.

Part: SENSOR — INTERMITTENT (FUEL CONTROL) · airframe 50,728 hrs · 18,436 cycles

N1 INDICATION PROBLEM. RTFL, N1 MODE GOES INOP EVERY FEW SECONDS. ENGINE PARAMETERS NORMAL. REPLACED P2-T2 SENSOR 4014 KS. REPLACED P2-T2 RELAY BOX, OPS CHECK OKAY.

Part: WIRE — BROKEN (CABIN) · airframe 49,055 hrs · 17,730 cycles

EMERGENCY EXIT LIGHTING INOP SEAT ROWS 12, 13 AND 14. BROKEN WIRE FOUND AT 13ABC. REPAIRED BROKEN WIRE. OP CHECKS GOOD.

Part: COVER — MISSING (CABIN) · airframe 49,055 hrs · 17,730 cycles

THE 6ABC EMERGENCY EXIT PATH LIGHT COVER MISSING. REPLACED LENS COVER FOR SEAT 6C EMERGENCY EXIT PATH LIGHT.

Part: HYDRAULIC SYSTEM — FAILED · airframe 48,379 hrs · 17,463 cycles

YELLOW HYD SYSTEM FAILURE. FLIGHT DIVERTED.

Part: BATTERY — FAULTY (CABIN) · airframe 47,744 hrs · 17,240 cycles

CIDS BIT BATTERY FWD L. EPSU FAILURE. REPLACED EPSU.

Part: HOSE — BROKEN (EVAC SLIDE)

HOSE BROKE DURING INFLATION. HOSE DID NOT SWIVEL DURING INFLATION CAUSING HOSE TO BREAK. REPLACED HOSE.

Part: OXYGEN SYSTEM — READS LOW (CREW) · airframe 46,830 hrs · 16,928 cycles

CREW O2 LOW. SUPPLEMENTAL DATA UPDATE CAUSE, UNKNOWN. SERVICED CREW O2, NO LEAKS WERE NOTED.

Part: COMPUTER — FAULTY (NR 1 ELAC) · airframe 46,482 hrs · 16,787 cycles

ELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. DISCREET OUTPUTS OUT OF CALIBRATION. REPLACED ELAC NR 1, ALL OPS CHECKS PERFORMED SATIFACTORY.

Part: EPSU — FAILED (CABIN) · airframe 46,203 hrs · 16,675 cycles

EMERGENCY LIGHTS TEST FAILED, FAULTS AFT LEFT BATTERY. EPSU FAILURE. REPLACED AFT LEFT EPSU, OPS CHECKED NORMAL.

Part: GIRT BAR — OBSTRUCTED (DOOR 1R) · airframe 45,879 hrs · 16,550 cycles

FOUND DOOR 1R WILL NOT DISARM. SPRAYED ICE RELEASE ON GIRT BAR ARMS. MECHANISM IS WORKING NOW. SHOULD PREVENT FURTHER FREEZE UP AS WELL.

Part: COMPUTER — FAULTY (NR 1 ELAC) · airframe 45,373 hrs · 16,381 cycles

AILERON SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. FOUND NR 1 ELAC FAULT CAUSING AIL SERVO FAULT DISPLAY. REPLACED NR 1 ELAC. OPS CHECK OK, NO REPEATS.

Part: THRUST REVERSER — DAMAGED (NR 2) · airframe 44,880 hrs · 16,191 cycles

NR 2 T/R SLEEVE DAMAGED DUE TO CONTACT WITH FUELING TRUCK. REVERSER REPLACED.

Part: FIRE BOTTLE — DISCHARGED (APU) · airframe 44,596 hrs · 16,077 cycles

APU FIRE BOTTLE DISCHARGE LIGHT ILLUMINATED ON OVERHEAD PANEL. 09-07-07 INADVERTANT DISCHARGE ON APU FIRE BOTTLE CAUSED INDICATION. REPLACED FIRE BOTTLE AND SQUIB, RESET INDICATION.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,766 hrs · 15,396 cycles

LEFT AFT BELLY FAIRING SUPPORT STRUCTURE ANGLE CRACKED AT ATTACH TO FUSELAGE SKIN BELOW KEELBEAM AT FRAME 46. MAJOR REPAIR ACCOMPLISHED: REPLACED DAMAGE SECTION OF ANGLE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,766 hrs · 15,396 cycles

RIGHT AFT BELLY FAIRING SUPPORT STRUCTURE ANGLE CRACKED AT ATTACH TO FUSELAGE SKIN BELOW KEEL BEAM AT FRAME 46. MAJOR REPAIR ACCOMPLISHED: REPLACED DAMAGE SECTION OF ANGLE.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 41,490 hrs · 14,926 cycles

EMERGENCY LIGHT TEST FAULTED UNIT FWD L. REPLACED DOOR 1L EPSU. OPS CHECK OK.

Part: VALVE — UNSERVICEABLE (SLIDE) · airframe 41,431 hrs · 14,902 cycles

LOW PRESSURE ON CYLINDER. REPLACED SLIDE 2R. PERFORMED INSPECTION OF NR 2R DOOR SLIDE. CHECKS GOOD. THE BALL SEAT WAS LEAKING THERE WAS A CUT MARK ON THE BALL SEAT. REPLACED BALL SEAT.

Part: BATTERY — FAULTY (EMERGENCY LIGHTS) · airframe 41,120 hrs · 14,787 cycles

EMERGENCY LIGHT TESTS FAULTS AFT L BATT. REPLACED BATTERY, TEST OK.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 40,852 hrs · 14,688 cycles

SYSTEM FAILED 3 SERVICE EMERGENCY CHECK. FAULT SHOWS COMM FWD L, EMER L, COMM AFT L. TRIED RESETTING SYSTEM, NO HELP.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,493 hrs · 13,820 cycles

EMERGENCY LIGHT TEST FAILS -AFT LT BATTERY FAULT- MSG SHOWN.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHT) · airframe 37,930 hrs · 13,632 cycles

FWD LEFT EMERGENCY POWER SUPPLY UNIT FAILED TEST DURING EMERGENCY LIGHT TEST. PSU REPLACED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,689 hrs · 13,542 cycles

FWD LEFT POWER SUPPLY UNIT AND BATTERY FOR EMERGENCY LIGHT INOP. REPLACED FWD LEFT POWER SUPPLY UNIT WITH BATTERY.

Part: STRAP — CORRODED (BTWN FR 33 & FR) · airframe 36,937 hrs · 13,272 cycles

PREVIOUS STRAP BETWEEN FS 33 AND FS 34 ON STRINGER 42R IS CORRODED.

Part: SKIN — DENTED (RT FUSELAGE AFT) · airframe 36,937 hrs · 13,272 cycles

RT FUSELAGE DENTED AFT OF FS 64 AT STR 20R. MAJOR REPAIR TO ADD DOUBLER OVER SKIN.

Part: FAN — FAILED (E/E BAY) · airframe 36,545 hrs · 13,146 cycles

BOTH AVIONICS BLOWER AND EXTRACT FANS BECAME INOPERATIVE. PFR SHOWS ECAM VENT AVIONICS SYS FAULT WITH ASSOCIATED FAILURE MSG NO AEVC DATA. TSM SHOWS POSSIBLE COMPUTER FAULT 10HQ. REPLACED AEVC AND BITE TEST CHECKS GOOD. NO FAILURES OR FAULTS NOTED.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 34,133 hrs · 12,301 cycles

UNABLE TO PRESSURIZE THE CABIN. REPLACED FAULTY SKIN AIR OUTLET VALVE.

Part: DOOR FRAME — DEFORMED (E/E BAY) · airframe 33,262 hrs · 11,984 cycles

FWD LOWER E AND E DOOR FWD FRAME SECTION AND CENTER INTERCOSTAL JUST FWD OF DOOR HANDLE DEFORMED DUE TO IMPACT WITH TOW BAR. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FRAME AND INTERCOSTAL REPLACED.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 33,262 hrs · 11,984 cycles

AFT PIT STR 43L EXFOLIATED FROM FR 53 TO 59. SPLICED IN NEW STRINGER SECTION.

Part: DOOR — OPEN (RT WING) · airframe 33,260 hrs · 11,983 cycles

DURING CLIMB CREW WAS UNABLE TO RETRACT FLAPS/SLATS. FUEL DOOR WAS FOUND OPEN AND BENT AROUND WING FIXED L/E PREVENTING SLAT FROM RETRACTING FULLY. FUEL DOOR REPLACED. LEADING EDGE REPAIRED. SLAT REPLACED.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 30,086 hrs · 10,803 cycles

LIGHTNING STRIKE DAMAGE AT FRAME 24, 3 INCHES BELOW STRINGER 36L. MAJOR REPAIR ACCOMPLISHED. INSTALLED SOLID FASTENER.

Part: ODOR — DETECTED (GALLEY) · airframe 29,912 hrs · 10,737 cycles

FLIGHT DIVERTED DUE TO REPORTS OF BURNING SMELL IN AFT GALLEY AREA. BURNED GUM WAS FOUND ON HOT PLATE. CLEANED HOT PLATE.

Part: SWITCH — FAILED (HYD SYSTEM) · airframe 20,712 hrs · 7,252 cycles

B-HYDRAULIC PUMP LOW PRESSURE INDICATION. *S/D* REPLACED PRESS SWITCH FOR BLUE ELECTRIC PUMP.

Part: A/C PACK — CLOGGED (REHEATER) · airframe 20,293 hrs · 7,112 cycles

COULD NOT CONTROL CABIN AND COCKPIT TEMPERATURE. *S/D* REPLACED NR 1 PACK REHEATER. OPERATIONAL AND LEAK CHECK NORMAL.

Part: ACM — LEAKING (ACM BAY) · airframe 20,236 hrs · 7,093 cycles

UNABLE TO COOL THE CABIN. *S/D* THE AIR CYCLE MACHINE AND VARIOUS PACK BLEED DUCT SEALS WERE LEAKING CAUSING POOR PERFORMANCE OF THE LEFT HAND AIR CONDITIONING PACK. THE AIR CYCLE MACHINE (10HM1) WAS CHANGED ALONG WITH THE FLOW CONTROL VALVE (11HB).

Part: UNKNOWN — ODOR (CABIN)

STRONG SULFUR ODOR IN CABIN, SOME PASSENGER NAUSEA. UNABLE TO FIND OUT THROUGH FF WHAT IS ACTUALLY ON AIRCRAFT. NO HAZMAT LISTED IN DCLR/DPWM. HOWEVER, CAPTAIN HAS HAZMAT FORM FOR DRY ICE TO CHILL MEDICAL SPECIMENS. ODOR SUBSIDING ON RETURN TO LAX WITH CABIN FANS OFF, BOTH PACKS ON HIGH. *S/D* INSPECTED LAVATORY LINE FROM FORWARD LAVATORY TO WING. NO DEFECTS OR LEAKS. INSPECTED RECIRCULATION FILTERS FOUND CLEAN. RAN BOTH ENGINES USING ENGINE BLEEDS, RAN BOTH PACKS NO SMELLS NOTED WITH CABIN CLOSED. UNABLE TO DUPLICATE GRIPE. NO HISTORY NOTED.

Part: FWC — MALFUNCTIONED (E&E COMP)

F/O PITOT, TAT PROBES AND AUTO THROTTLE APPEAR ON STATUS PAGE ACCOMPANIED BY STALL WARNING AND AUDIBLE OVERSPEED WARNING SPURIOUSLY AT FL 370, MACH .79 TO .80. FOR LAST 40 TO 50 MINS OF FLIGHT STALL WARNING AND OVERSPEED CONTINUOUSLY. *S/D* FAULT COULD NOT BE DUPLICATED ON GROUND TESTS. ALL FLIGHT COMPUTERS WERE RESET AND AIRCRAFT RETURNED TO SERVICE. FWC 2 DID FAULT ON FOLLOWING TRIP. THE FWC WAS RESET AND AIRCRAFT HAS OPERATED NORMALLY WITHOUT FAULTING.

Part: RAM AIR TURB — FAILED (AUX POWER)

RAT FAILED AUX HYD SYS OPS TEST. *S/D* DURING FUNCTIONAL CHECK OF RAT USING GROUND TEST UNIT, RAM AIR TURBINE FAILED CHECK. REPLACED RAT PER AMM AND OPS CHECKED NORMAL.

Part: HANDLE — OUT OF ADJUST (CARGO DOOR)

RAMP REPORTED AFT CARGO PIT DOOR HANDLE DIFFICULT TO STOW. FOUND HOUSING ASSY (ITEM 180 IPC 52 31 21 PG3B 0) CRACKED.

Part: METERING UNIT — LEAKING (NR 1 ENGINE)

NR 1 ENGINE FUEL DRAINMAST IS LEAKING FUEL FROM THE FMU PORT IN A STEADY STREAM DURING ENGINE RUN. FUEL METERING UNIT LEAKING FROM DRAIN MAST. NOT A NEW PROBLEM. MRR NOT REQUIRED. COA IN PROCESS TO REDUCE FUEL LEAKS.

Part: RETRACT MECH — MALFUNCTIONED (LANDING GEAR)

ON CLIMBOUT, GEAR DID NOT FULLY RETRACT. CYCLED GEAR, CAME UP OK BUT GOT LGCIU FAULT WITH ASSOCIATED ECAM WARNING.

Part: PFD — MALFUNCTIONED (LT COCKPIT)

CAPTAIN'S PFD INTERMITTENTLY NOT VISIBLE. *S/D* SYSTEM TESTED GOOD NOTHING WAS REPLACED.

Part: FAN — FAILED (E & E COMPT)

HIGH PITCH VIBRATION UNDER FLIGHT DECK FLOOR. ACRID SMOKE SMELL AND ECAM MESSAGE FOR AVIONICS BLOWER FAULT. SWITCHED TO OVERRIDE POSITION. VIBRATION AND SMOKE CLEARED. *S/D* VIBRATION WAS CAUSED BY THE AVIONICS COOLING FAN. VIBRATION AND SMOKE CLEARED AFTER COOLING FAN REPLACEMENT.

Part: PITOT PROBE — BLOCKED (FWD FUSELAGE)

INDICATED AIRSPEED FLUCTUATED +/- 100 KNOTS DURING DESCENT BETWEEN FL240AND FL230. AUTOPILOT DISENGAGED AND AIRCRAFT REVERTED TO ALTERNATE LAW. PITOT PROBE PARTIAL BLOCKAGE. BOTH PITOT PROBES REPLACED AND AIR DATA SYSTEM CHECKED. AIRBUS TECHNICAL FOLLOW-UP (TFU) 34.10.00.001 INDICATES THE POTENTIAL FOR ENVIRONMENTAL CONDITIONS THAT MAY EXCEED THE CERTIFICATION BASIS OF PITOT PROBE (P/N 50620-10). REDESIGNED PROBES (P/N C16195AA) HAVE REPLACED THE OLD INVENTORY AND ARE BEING INSTALLED ON AIRBUS AIRCRAFT ON AN ATTRITION BASIS.

Part: PRESSURIZATION — MALFUNCTIONED (CABIN)

AFTER TAKEOFF, RECEIVED AN ECAM CABIN PRESSURE SYSTEM NR 1 AND NR 2 FAULT. MANUAL MODE BACKUP WAS INOPERATIVE. RETURNED TO FIELD AND LANDED OVERWEIGHT.