N466UA

Part: BATTERY — FAULTED (ZONE 200) · airframe 75,731 hrs · 31,325 cycles

BITE FAULT: EPSU BATTERY EMER R REPLACED EPSU BATTERY AT POSITION BATT. EMER R IAW AMM 33-51-38, OPS TEST GOOD.

Part: BATTERY — FAULTED (ZONE 200) · airframe 75,731 hrs · 31,325 cycles

BITE FAULT: AFT L REPLACED EPSU BATTERY AT POSITION AFT L IAW AMM 33-51-38, OPS TEST GOOD .

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 75,590 hrs · 31,257 cycles

RIGHT FWD DOOR EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. MOUNTING ON BASE OF LIGHT ALSO BROKEN. REMOVED AND REPLACED EXIT LIGHT IAW AMM 33-51-13. OPS CHECKED GOOD.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 75,555 hrs · 31,236 cycles

PROCEDURE - TEST FAILED WITH MSG "EPSU COMM FWD L" SEE PIC ABOVE SHOULD READ EMERGENCY LIGHTING TEST PROCEDURE- PERFORMED TSM 33-51-00, FOUND EPSU COMM FWD LEFT FAULT. TESTED EPSU 10WL REF STEP 4B-1A NO EPSU LED'S CAME ON. REPLACED EPSU 10WL REF AMM 33-51-38. OPS CHECK GOOD.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 75,517 hrs · 31,215 cycles

OPERATIONAL CHECK OF THE EMERGENCY POWER SUPPLY UNITS BY BITE-CHECK EMERGENCY LIGHTS FAIL TEST AT CIDS PANEL. FAULT EPSU INT LOAD FWD L ATA 33-51-38. CYCLED BREAKERS NO HELP. REMOVED CEILING PANEL AT DOOR 1 LEFT. DID TEST OF LIGHTING BOX FAULTING INTERIOR LIGHTS. FOUND EVERY LIGHT THAT IS CONTROLLED BY THE FWD EMERGENCY LIGHT POWER SUPPLY TO BE WORKING PROPERLY BUT FAULT CODE IS STILL PRESENT DURING THE TEST. REMOVED AND REPLACED THE FWD ESPU (10WL) IAW AMM TASK 33-51-38-000-001-A AND TASK 33-51-38-400-001-A. TRANSFERRED THE BATTERY TO THE NEW ESPU. OPS CHECKS GOOD. NO FAULTS.

Part: LIGHT — FAULTED (ZONE 200) · airframe 75,417 hrs · 31,163 cycles

EMERGENCY EXIT LIGHTS REMAIN ILLUMINATED IN ALL MODES. POWERED DOWN AIRCRAFT COMPLETELY FOR 3 MINUTES. POWERED BACK UP, CYCLED NO SMOKING LIGHTS SWITCH AND SEAT BELT LIGHT SWITCH PER TROUBLESHOOTING MANUAL (TSM) 33-51-00-810-881-A. EMERGENCY LIGHTS STAYED OFF IN "ARM" MODE AND "OFF"MODE. OPS CK GOOD.

Part: WIRE HARNESS — DETACHED (ZONE 200) · airframe 74,339 hrs · 30,625 cycles

EMERGENCY EXIT PATHWAY LIGHT INOP AT SEAT 21C. FOUND EMERGENCY EXIT PATHWAY LIGHT HARNESS DETACHED AT JUNCTION OF SEAT 21A. REATTACHED HARNESS. OPS CHECKED GOOD.

Part: TRANSMITTER — FAULTY (OIL QTY) · airframe 73,897 hrs · 30,405 cycles

RIGHT ENG OIL QTY DROPPED EXTREMELY LOW THEN 0 AND ECAM ENG WRN REQUESTING MEL 7931B FOR OIL INDICATION ON THE #2 ENGINE INOP VERFIED OIL SERVICE IS FULL AND THERE IS NO OIL LEAKAGE, CONFIRMED WITH CREW OIL PRESSURE AND TEMP. WAS GOOD #2 ENGINE OIL QTY INDICATION INOP. NUMBER 2 ENGINE ECAM OIL QUANITY INDICATION INOPERATIVE. ENG OIL QTY FULL. NO LEAKS NOTED. R&R #2 ENGINE OIL QUANTITY TRANSMITTER OPS AND LEAK CHK GOOD.AMM 79-31-15.

Part: BATTERY — DISCHARGED (ZONE 800) · airframe 73,850 hrs · 30,379 cycles

OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - EPSU BITE FAIL UNIT EMER R SEE PHOTO. LOCATION R/H OVERWING EXIT. SLAVED NEW EPSU AT R/H EMERGENCY OVERWING EXIT, REF AMM 33-51-38-400-001-A. NO GO. RE-INSTALLED EPSU REF AMM 33-51-38-400-001-A. SWAPPED BATTERY FROM L/H SIDE REF AMM 33-51-38-400-002-A. BITE TEST ON EPSU SYSTEM OK. RE-INSTALLED BATTERY TO L/H SIDE. INSTALLED NEW BATTERY REF AMM 33-51-38-400-002-A. EPSU BITE CHECKPARTS USED: 18-3351-3-0001,QTY :1

Part: CONTROL SERVO — FAULTED (NLG) · airframe 73,796 hrs · 30,363 cycles

ECAM WHEEL N/W STRG FAUL T IN CRUISE FL340 T/S PER TSM REF. 32-51-00-810-826-A, REMOVED AND REPLACED N/W STEERING SERVO CTL PER AMM REF. 32-51-51-000-001-A, FOUND CONNECTOR CLOCKED DIFFERENT. ADDED ROTABLE PARTS CHANGE INFORMATION. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1355076 SN OFF 9100 CONTROL, SERVOC OFF 31-3252-9-0001 9100 ON 31-3252-9-0001 0449 REMOVED NLG ELECTRICAL HARNESS 2M REFER AMM 32-21-43-000-003-A SLAVED REPLACEMENT NLG ELECTRICAL HARNESS 2M USE AMM 32-21-43-400-003-A FOR INSTALLATION NEEDS OP CHECK AND ALL BOLTS STILL NEEDS TO BE TIGHTENED N/W STEERING SERVO CTL OPS CHECK STILL NEEDED REFER AMM 32-51-51-400-001-A PARA SUBTASK D FINISHED INSTLLING NLG 2M HARNESS REF AMM 32-21-43-400-003-A. BITE TESTS OK. PREFORMED STEERING OPC FOR THE NOSE WHEEL STEERING CONTROL 6GC REF AMM 32-51-00-720-003-A. TEST FAILS. NO STEERING MOVEMENT AND WHEEL NW STRG FAULT MESSAGE ON UPPER ECAM. BSCU BITE GIVES MESSAGE STEERING ELECTRO-HYD MODULE 6GC. REQUIRES FURTHER T/S. REMOVED AND REPLACED N/W STEERING SERVO-CONTROL PER AMM REF. 32-51-51-400-001-A, ACCOMPLISHED FUNCTIONAL TEST PER AMM REF. 32-51-00-720-003-A ALL TESTS PASSED, NO FAULTS DISPLAYED ON ECAM, NO LEAKS NOTED. OK FOR SERVICE.PARTS USED: ,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1326947 SN OFF 0449 CONTROL, SERVOC OFF 31-3252-9-0001 0449 ON 31-3252-9-0001 1312

Part: FRAME — CRACKED (FR 35) · airframe 71,415 hrs · 29,268 cycles

AT C-CHECK IN BFM, DURING INSPECTION OF FWD FACE OF FR 35 LH SIDE BTWN STRG 30 AND STRG 31 WAS FOUND CRACK. REPAIR ACCOMPLISHED IAW ECRA 5331-02600 ON VTMAE N/R 81943. THE LATEST REVISION OF EC/RA 5331-02600. PLANNING TO CONTACT ENGINEERING AFTER APRIL 14, 2024, BUT BEFORE MAY 14, 2024 FOR PART 3 PERMANENT REPAIR AT FR35 STGR 30LH PER REF ECRA 5331-02600 PART 1A INTERIM RPR, STEP 3. DIP INITIATED TOMC-APPROVAL FROM SC1ELBYC COMMENT TO READ AS FOLLOWS.PLANNING TO CONTACT ENGINEERING AFTER APRIL 14, 2024, BUT BEFORE MAY 14, 2024 FOR PART 3 PERMANENT REPAIR AT FR35 STGR 30LH PER THE LATEST REVISION OF EC/RA 5331-02600. REPAIR HAS BEEN ACCOMPLISHED PER ECRA 5331-02600 REV C WITHOUT QC DEVIATIONS. ORIGINAL DISCREPANY FOUND ON VTMAE NON-ROUTINE 81967 AND LP 4456199.

Part: SHOCK ABSORBER — UNKNOWN (MLG) · airframe 71,415 hrs · 29,268 cycles

RIGHT MAIN LANDING GEAR REQUIRES SHOCK ABSORBER PRESSURE CHECK DUE TO FULL STRUT SERVICING, AFTER FIVE (5) LANDINGS BUT NOT TO EXCEED TWENTY (20) LANDINGS AFTER THE FIRST SUBSEQUENT FLIGHT. 20 LANDINGS PER AMM 12-14-32-614-003-A. REF. GMM 05-30-15. INITIATED DIP TO ACCOMPLISH RIGHT MLG SHOCK ABSORBER CHARGE PRESSURE AND "H" DIMENSION AFTER 5 LANDINGS, BUT NOT TO EXCEED OK TO DIP RH MLG SHOCK ABSORBER PRESSURE CHECK PER AMM TOMC-APPROVAL FROM SC1ELBYC COMMENT 12-14-32-614-003-A. "CHECK SHOCK STRUT PRESSURE AND "H" DIMENSION AFTER 5 LANDINGS, BUT NOT TO EXCEED 20 LANDINGS." TOMC APPROVED : QC REVIEWED RECORDS UPDATE TOMC APPROVED : QC REVIEWED T/A: >5 <20 FC...KJB

Part: SKIN — CORRODED (#2 PYLON) · airframe 71,415 hrs · 29,268 cycles

#2 PYLON AFT FIXED FAIRING SKIN HAS CORROSION ON OTBD SIDE. REPLACED SKIN PANEL AT AFT FIXED FAIRING #2 IAW A-32O SRM 51-72- 11 AND INSTALLED IAW SRM 51-42-11 AND DRAWING D54510054, RECEIVE D SKIN PANEL P/N= D54530052522100, B/N= 0004191346. EMP: V936039 WC: 81854 STA: ST ENG BFM INSPECTED IAW SRM 51-72-11 AND DWG 54510054. INSTALLATION SERVIC ABLE AND CORRECT.

Part: SENSOR — FAULTY (ENG 1) · airframe 68,044 hrs · 27,622 cycles

**RTBL** LOW SPEED RTO ENGINE 1 ACCELERATION ABNORMAL TROUBLESHOOT NO FAILURE MESSAGES ON MAINTENANCE POST FLIGHT REPORT AFFILIATED WITH NUMBER 1 ENGINE. GROUND SCANNING AND LAST LEG REPORT SHOWS NO FAULT. SCHEDULED MAINTENANCE REPORT HAS P2 T2/ ADIRS1/2/EEC1. ATA CHAPTER 73-22-11. PROBES MAY NEED R&R ENGINE 1 P2/T2 SENSOR IAW AMM 73-22-11. REF TO L/P 9267290 FOR OPS CK.

Part: CONNECTOR — UNSAFETIED (LH ENGINE) · airframe 66,385 hrs · 26,872 cycles

*EMERGENCY DECLARED* ENGINE 1 H.O.C. DUE TO 10 QTS OF OIL ADDED. RUN ENGINE AT IDLE FOR 5 MINUTES ENGINE REQUIRES EXTERNAL INSPECTION FOR OIL LEAKS, IF NONE FOUND CONTACT TOMC EMC FOR FURTHER INSTRUCTIONS.. LOCKED FOR TROUBLESHOOTING UNLOCKED LOGPAGE TO DOCUMENT THE CORRECTIVE ACTION THAT WAS ACCOMPLISHED. ADDED A PICTURE OF THE OIL TUBE CONNECTION THAT WAS FOUND UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V900886 71-00-00-710-045-A. LEAKING. PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. INVESTIGATE THE MAC RELATED WORK ORDER 000000003033106 AND PRTR SOURCE OF THE OIL LEAK. CARREON, DANIEL (V900886). OIL TUBE CONNECTION UNDER THE THRUST REVERSER COWLING WAS FOUND LEAKING (SEE ATTACHED IMAGE). THE B-NUT WAS NOT SAFETY WIRED AND WAS SEVERAL TURNS LOOSE. TIGHTENED THE B-NUT AND SECURED THE CONNECTION WITH SAFETY WIRE. ACCOMPLISHED A DRY MOTOR LEAK CHECK PER AMM TASK CARREON, DANIEL (V900886). OIL TUBE CONNECTION UNDER THE THRUST ACCOMPLISHED A DRY MOTOR LEAK CHECK PER AMM TASK REVERSER COWLING WAS FOUND LEAKING (SEE ATTACHED IMAGE). THE 71-00-00-710-045-A. B-NUT WAS NOT SAFETY WIRED AND WAS SEVERAL TURNS LOOSE. TIGHTENED THE B-NUT AND SECURED THE CONNECTION WITH SAFETY WIRE. ADD EMP:V900886

Part: INTERCOSTAL — CRACKED (FR16) · airframe 66,250 hrs · 26,810 cycles

R/H FR 16 DOORSTOP FITTING #7 HAS CRACK INDICATION NOTED IN HOLE #1 & #3 TO READ AS FOLLOWS: "ACCOMPLISH INSPECTION REQUIREMENTS PER PART AFT REACHES 39,510 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAAT INSPE R." REFF VT MAE NRC 0020970 FOR WORK PERFORMED. 2A OF LATEST REVISION OF EC/RA 5311-02713 ON OR BEFORE THE AIRCR CTIONS AT INTERVALS NOT TO EXCEED 12,700 FLIGHT CYCLES THEREAFTE REPAIRED R/H FR 16 DOORSTOP # 7 HOLES #1 & #3 IAW PART 1 - INTER IM REPAIR OF ECRA 5311-02713. STEP 1.A. STEP 3 REQUIRES DTA DIP ADD EMP:U354480 APPROVED TO CARRY REF ECRA 5311-02713 STEP 1.3 ACCOMPLISH TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTION REQUIREMENTS PER PART 2A OF LATEST REVISION OF ECRA 5311-02713 ON OR BEFORE THE AIRCRAFT REACHES 39,510 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 12,700 FLIGHT CYCLES QC QC REVIEWED. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: INTERCOSTAL — CORRODED (FR20) · airframe 66,250 hrs · 26,810 cycles

L/H FR 20 DOORSTOP FITTING #7 HAS CRACK INDICATION NOTED IN HOLE #3 AS FOLLOWS: "ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2B OF L AS FOLLOWS: "ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2B OF L CHES 40,010 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTIONS A VT MAE NRC 0020972 FOR WORK PERFORMED. ATEST REVISION OF EC/RA 5311-02713 ON OR BEFORE THE ATEST REVISION OF EC/RA 5311-02713 ON OR BEFORE THE AIRCRAFT REA T INTERVALS NOT TO EXCEED 13,200 FLIGHT CYCLES THEREAFTER." REFF REPAIRED L/H FR 20 DOORSTOP # 7 HOLE #3 IAW PART 1 -INTERIM REPA REPAIRED L/H FR 20 DOORSTOP # 7 HOLE #3 IAW PART 1 -INTERIM REPA IR OF ECRA 5311-02713. STEP 1.E. STEP 4 REQUIRES DTA DIP TO READ IR OF ECRA 5311-02713. STEP 1.E. STEP 4 REQUIRES DTA DIP TO READ ADD EMP:U354480 ADD EMP:U354480 APPROVED TO CARRY REF ECRA 5311-02713 SECTION 1.4 TO ACCOMPLISH TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTION REQUIREMENTS PER PART 2A OF LATEST REVISION OF ECRA 5311-02713 ON OR BEFORE THE AIRCRAFT REACHES 40,010 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 13,200 FLIGHT CYCLES THEREAFTER. DIP 53-DIP ITEM REJECTED. QC QC REVIEWED. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: FITTING — CRACKED (FR66) · airframe 66,250 hrs · 26,810 cycles

WHILE AT VT AREOSOACE BFM DURING C-1 CHECK REF NR0021094 ROTO PROBE OF RH FR66 #5 DOOR STOP FITTING HOLE D1 FOUND CRACK INDICA TION. PLUG & WASHER IAW SRM 53-73-12-001. RE-INSTALLED DOORSTOP FITTIN EMBODIMENT 33000FC (FH NOT RELAVENT) SUBSEQUENT INSP AT INTERVAL 51-10-08 & ROTOTEST REF AMM 53-41-00 IAW SRI 53-41-12-205-009 G #5 IAW SRM 51-42-11. INSP THRESHOLD FROM TIME OF ADL REPAIR S OF 10700FC (FH NOT RELAVENT) INSP METHOD HFEC REF TO NTM WORK ACCOMPLISHED ON VT NR0021094 REAMED HOLE D1 TO .394" IAW SRM53-41-12-300-010 FINAL DIM .421" NO CRACK NOTED IAW NTM 51-10-01 PT6. FABBED & INSTALLED FREEZE REF SRI 53-41-12-205-009 INSPECT THRESHOLD FROM TIME OF TOMC-APPROVAL FROM SC1ELBYC COMMENT ADL/REPAIR EMBODIMENT 33000 FC (FH NOT RELEVANT) SUBSEQUENT INSPECTION AT INTERVALS 10700 FC (FH NOT REVELANT) INSPECTION METHOD NTM 51-10-08 (REF AMM 53-41-00) APPLICABLE TO FR66. TOMC APPROVES DIP. QC REVIEWED QC REVIEWED RECORDS UPDATE RECORDS UPDATE INIT: 33,000 FC (FROM REPAIR EMBODIMENT) WILL ITO TO RIR(-4301) RIR: INTERVALS 10,700 FC...LN/U253409

Part: NONE — CRACKED (FR16) · airframe 66,250 hrs · 26,810 cycles

L/H FR 16 DOORSTOP FITTING #7 HAS CRACK INDICATION NOTED IN HOLE #1 & #3 READ AS FOLLOWS: "ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2A AFT REACHES 39,510 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPEC " REFF VT MAE NRC 0020933 FOR WORK PERFORMED. 2A OF LATEST REVISION OF EC/RA 5311-02713 ON OR BEFORE THE AIRCR TIONS AT INTERVALS NOT TO EXCEED 12,700 FLIGHT CYCLES THEREAFTER REPAIRED L/H FR 16 DOORSTOP # 7 HOLE 1 & #3 IAW PART 1 - INTERIM REPAIR OF ECRA 5311-02713. STEP 1.A. STEP 3 REQUIRES DTA DIP TO ADD EMP:U354480 APPROVED TO CARRY REF ECRA 5311-02713 STEP 1.3 ACCOMPLISH TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTION REQUIREMENTS PER PART 2A OF THE LATEST REVISION OF ECRA 5311-02713 ON OR BEFORE THE AIRCRAFT REACHES 39,510 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 12,700 FLIGHT CYCLES THEREAFTER. QC QC REVIEWED. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: NONE — CRACKED (FR16) · airframe 66,250 hrs · 26,810 cycles

R/H FR 16 DOORSTOP FITTING #1 HAS CRACK INDICATION NOTED IN HOLE #3 D AS FOLLOWS: "ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2A OF ACHES 39,510 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTIONS VT MAE NRC 0020971 FOR WORK PERFORMED. LATEST REVISION OF EC/RA 5311-02713 ON OR BEFORE THE AIRCRAFT RE AT INTERVALS NOT TO EXCEED 12,700 FLIGHT CYCLES THEREAFTER." REF REPAIRED R/H FR 16 DOORSTOP # 1 HOLE #3 IAW PART 1 - INTERIM REP AIR OF ECRA 5311-02713. STEP 1.B. STEP 3 REQUIRES DTA DIP TO REA ADD EMP:U354480 APPROVED TO CARRY REF ECRA 5311-02713 STEP 1.3 ACCOMPLISH TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTION REQUIREMENTS PER PART 2A OF LATEST REVISION OF ECRA 5311-02713 ON OR BEFORE THE AIRCAFT REACHES 39,510 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 12,700 FLIGHT CYCLES THEREAFTER. QC QC REVIEWED. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: NONE — NONE (AFT CARGO) · airframe 66,250 hrs · 26,810 cycles

(A3NB-21-3-6032) WATER FOUND COMING FROM LAV DRAINS BETWEEN FR 8 THRU FR21.() ACCOMPLISHED ECRA 2011-01000 "SPILLAGE WAS ONLY POTABLE WATER" E MP# V936637 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOB ILE AT BFM ON NR# 0021202.

Part: NONE — CRACKED (FR20) · airframe 66,250 hrs · 26,810 cycles

L/H FR 20 DOORSTOP FITTING #1 HAS CRACK INDICATION NOTED IN HOLE #1 & #3 READ AS FOLLOWS: "ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2B REACHES 40,010 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTION FF VT MAE NRC 0020973 FOR WORK PERFORMED. OF LATEST REVISION OF EC/RA 5311-02713 ON OR BEFORE THE AIRCRAFT AT INTERVALS NOT TO EXCEED 13,200 FLIGHT CYCLES THEREAFTER. " RE REPAIRED L/H FR 20 DOORSTOP # 1 HOLE 1 & #3 IAW PART 1 - INTERIM REPAIR OF ECRA 5311-02713. STEP 1.D. STEP 3 REQUIRES DTA DIP TO ADD EMP:U354480 APPROVED TO CARRY REF ECRA 5311-02713 PART 1.4 , ACCOMPLISH TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTION REQUIREMENTS PER PART 2B OF THE LATEST REVISION REF ECRA 5311-02713 ON OR BEFORE AIRCRAFT REACHES 40,010 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 13,200 FLIGHT CYCLES THEREAFTER. CORRECTION REPAIR DIP IS STEP 4 NOT 3 QC QC REVIEWED. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: STOP FITTING — CRACKED (FRM 66) · airframe 66,250 hrs · 26,810 cycles

RH-FR66, DOOR STOP #1, LOWER INBOARD HOLE HAS CRACK INDICTION.() SUPPORT TASK AD 2018-03-12. R/H FR66 #1 LOWER I/B HOLE. REPAIED AND REAMED IAW SRM 53-41-12- ATTACHED EMP# V934344 WORK ACCOMPLISHED AT ST ENGINEERING AEROSP 300-10. ORG REAMED .394 FINAL DIA. .421 NO CRACK NOTED IAW NTM 5 ACE OF MOBILE AT BFM ON NR# 0021093 1-10-01 PT6. FABRICATED AND INSTALLED FREEZE PLUG AND WASHED IAW SRM 53-73-12-001. REINSTALLED DOOR STOP FITTING #1 FORM 44-0008

Part: STOP FITTING — CRACKED (FRM 66) · airframe 66,250 hrs · 26,810 cycles

RH-FR66, DOOR STOP #5, LOWER INBOARD HOLE HAS CRACK INDICATION.( ) SUPPORT TASK AD 2018-03-12 R/H FR66 #5 DOOR STOP LOWER HOLE. REPAIRED AND REAMED IAW SRM 53 44-0008 ATTACHED EMP# V934344 WORK ACCOMPLISHED AT ST ENGINEERIN -41-12-300-10. ORG. REAMED .394 FIN DIA. .421 NO CRACK NOTED IAW G AEROSPACE OF MOBILE AT BFM ON NR# 0021094. NTM 51-10-01 PT 6 FABRICATED AND INSTALLED FREEZE PLUG AND WASH ER IAW SRM 53-73-12-001. REINSTALLED DOOR STOP FITTING #5. FORM

Part: STOP FITTING — CRACKED (FRM 68) · airframe 66,250 hrs · 26,810 cycles

RH-FR68, DOOR STOP #6, LOWER INBOARD HOLE HAS CRACK INDICATION.( ) SUPPORT TASK AD 2018-03-12. R/H FR68 #6 DOOR STOP LOWER I/B HOLE REPAIRED AND REAMED IAW SRM FORM 44-0008 ATTACHED EMP# V934344 WORK ACCOMPLISHED AT ST ENGIN 53-41-12-300-10 ORG. REAMED .394 FINAL DIA. .421 NO CRACK NOTED EERING AEROSPACE OF MOBILE AT BFM ON NR# 0021088 . IAW NTM 51-10-01-PT6. FABRICATED AND INSTALLED FREEZE PLUG AND WASHER IAW SRM 53-73-12-001. REINSTALLED DOOR STOP FITTING #6

Part: STOP FITTING — CRACKED (FRM 66) · airframe 66,250 hrs · 26,810 cycles

RH-FR66, DOOR STOP #4, UPPER INBOARD HOLE HAS CRACK INDICATION.( ) SUPPORT TASK AD 2018-03-12 R/H FR66 #4 DOOR STOP UPPER I/B HOLE. REPAIRED AND REAMED IAW SR FORM 44-0008 ATTACHED. EMP# V934344 WORK ACCOMPLISHED AT ST ENGI M 53-41-12-300-10. ORG. REAMED .394 FINAL DIA, .421 NO CRACK NOT NEERING AEROSPACE OF MOBILE AT BFM ON NR# 0021096 ED IAW NTM 51-10-01 PT6. FABRICATED AND INSTALLED FREEZE PLUG AN D WASHER IAW SRM 53-73-12-001. REINSTALLED DOOR STOP FITTING #4

Part: DRAIN — LEAKING (LAVATORY) · airframe 66,250 hrs · 26,810 cycles

WITHIN 36 MONTHS, ACCOMPLISH ECRA 2011-01000, CARGO COMPARTMENT SPILL SECTION 2.C. SUPPLEMENTAL INSPECTION,IN THE AREA FROM BODY STATION 8 TO BODY STATION 21 BETWEEN STRINGERS 10 AND STRINGER 12. THE AREA FROM BODY STATION 8 TO BODY STATION 21 BETWEEN STRINGERS 10 AND STRINGER 12. ACCOMPLISH ECRA 2011-01000, CARGO COMPARTMENT SPILL SECTION 2.C. SUPPLEMENTAL INSPECTION WATER FOUND COMING FROM LAV DRAINS BETWEEN FR 8 THRU FR 21. DIP 20-DIP DIP CAN BE SIGNED OFF AFTER SUPPLEMENTAL INSPECTION ACCOMPLISHED SEE STEP 19B OF ECRA 2011-01000

Part: STOP FITTING — CRACKED (FRM 66) · airframe 66,250 hrs · 26,810 cycles

RH- FR66, DOOR STOP #6, LOWER INBOARD HOLE HAS CRACK INDICATION. () SUPPORT TASK AD 2018-03-12 R/H FR66 #6DOOR STOP LOWER I/B HOLE. REPAIRED AND REAMED IAW SRM FORM 44-0008 ATTACHED. EMP# V934344 WORK ACCOMPLISHED AT ST ENGI 53-14-12-300-10. ORG. REAMED .394 FINAL DIA .421 NO CRACK NOTED NEERING AEROSPACE OF MOBILE AT BFM ON NR# 0021095 IAW NTM 51-10-01-PT6. FABRICATED AND INSTALLED FREEZE PLUG AND WASHER IAW SRM 53-73-12-001. REINSTALLED DOOR STOP FITTING #6

Part: DRAIN LINE — CRACKED (#2 ENGINE) · airframe 66,218 hrs · 26,793 cycles

#2 ENG DRAIN MAST HAS DRAIN LINE( A.C.O.C) CRACKED THRU TUBE OVER 180 DEGREES. LOCATED A BRAZED AREA. UPDATE TO SDR. REMOVED #2 ENGINE DRAIN MAST AND REPLACED IT WITH A NEW ONE

Part: PUMP — FAILED (NR 2 ENGINE) · airframe 63,558 hrs · 25,592 cycles

Y ENG 2 PUMP LO PR DISPLAYED ON UPPER ECAM SCREEN. HYD APPEARED AT CRUISE FL350 PARTS UPDATE INSTALL KIT. REPLACED CASE DRAIN FILTER, THRUST REVERSER HCU FILTER AND HP FILTER, NO PARTICLES FOUND. REMOVED AND REPLACED NR 2 ENG HYD PUMP, IAW 29-13-51. OPS CK GOOD, OK FOR RETURN TO SERVICE. ROTABLE PARTS CHANGE WAS INDICATED - TT NR 1177475 SN OFF 6260 PUMP, HYDRAULIC OFF 31-2914-9-9003 6260 ON 31-2914-9-9003 4070.

Part: FRAME — CRACKED (FRM 33) · airframe 62,482 hrs · 25,134 cycles

FR35 AND 10 CM, AT STR30 L/H SIDE, HOLE NO. 2 HAS A CRACK INDICA TION ON HAECO LCQ REF 9298240 SPEC A3NB-53-3-6315. ACCOMPLISHED INTERIM REPAIR PER EC/RA 5331-02600. ACCOMPLISH PERMANENT REPAIR AT HOLE 2 FR 35 STR 30LH PER PART 3 OF EC/RA ON OR BEFORE 30JUL2020 BUT BEFORE 15JUL2020 FOR PERM. REPAIR INTERIM REPAIR PERFORMED PER ECRA 5331-02600 PART 1. NO PART 2 R EQUIRED, AND PART 3 TBD BY EG."ACCOMPLISH A PERMANENT REPAIR AT HOLE #2 FR35 STRG30LH PER PART 3 OF ECRA 5331-02600 ON OR BEFORE 30JUL2020. PLANNING TO CONTACT ENGINEERING AFTER 30JUN2020 BUT BEFORE 15JUL2020 FOR THE PERMANENT REPAIR.

Part: DOOR FRAME — CORRODED (FRAMES 52-56) · airframe 62,482 hrs · 25,134 cycles

AFT CARGO COMPARTMENT DOOR CUTOUT, BOX BEAM UPPER SKIN, FR 52.5- 56 STGR 39R-41R, MULTIPLE AREAS OF CORROSION - {A3NB-53-4-6179} - REMOVED AND REPLACED AFT CARGO COMPARTMENT DOOR CUTOUT BOX BEAM UPPER SKIN AT FR52.5-56 STR 39R-41R IAW A320 SRM 51-72-11-911-00 1.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,482 hrs · 25,134 cycles

LAV EXHAUST VENT EXTERIOR SKIN HAS CORROSION AT LOWER SURFACE AN D AROUND THE EDGE (EA 5100-02750 REV. A). BLEND CORRODED AREA LAV VENT EXHAUST. FOUND TO BE BEYOND ALLOWAB LE LIMITS AND REPAIRED AREA IAW A320 SRM 53-41-11-300-004 FIG 00 1 PG 1-6. ORG THICKNESS .063 MATERIAL REMAINING .048 A MATERIAL LOSS OF 21% A320 SRM 51-74-00-801.

Part: DOOR FRAME — CORRODED (FRAME 68) · airframe 62,482 hrs · 25,134 cycles

AFT CABIN DOOR CUTOUT FR68 ST22L-23L FWD FACE HAS CORROSION PER HAECO LCQ NR LP 9299010 CORROSION FOUND OUT OF LIMITS AROUND ANCHOR NUT AT FR 68 STRG 22 L-23L.ACCOMPLISHED REPAIR IAW SRM 53-41-12-300-002 PARAGRAPH 2 F IG 001.REQUIRES DETAILED VISUAL INSPECTION AT 18,500 FC/FH NOT RELEVANT WITH SUBSEQUENT INSP AT INTERVALS OF 18,500 FC/FH NOT R ELEVANT FROM REPAIR EMBODIMENT IAW SRI 53-41-12-205-003 PARAGRAP H 2 TABLE 002.ALL WORK ACCOMPLISHED ON HAECO NR 9299010. DIP APPROVED PER SRM 53-41-12-300-002 REQUIRES RE INSPECTION AT 18500FC FROM TIME OF REPAIR EMBODIMENT. AND SUBSEQUENT INSPECTIONS EVERY 18500 FC / FH NOT RELEVANT INSPECTION METHOD IS DVI .

Part: SHEAR TIE — NOT REPORTED (FRAME 3) · airframe 62,482 hrs · 25,134 cycles

REMOVED AND REPLACED CLEAT AT FR 3 STR 39R-40R IAW A320 SRM 51-7 2-11-911-001-A PARA 2 (D) - REMOVED AND REPLACED CLEAT AT FR 3 STR 39R-40R IAW A320 SRM 51-7 2-11-911-001-A PG 2 (D)-

Part: INTERCOSTAL — CORRODED (NOT REPORTED) · airframe 62,482 hrs · 25,134 cycles

REMOVED AND REPLACED CORRODED INTERCOSTAL IAW A320 SRM 51-72-11- 911-001. REMOVED AND REPLACED CORRODED INTERCOSTAL IAW A320 SRM 51-72-11- 911-001.

Part: DOOR SILL — CORRODED (FRAME 66 -68) · airframe 62,482 hrs · 25,134 cycles

L-2 DOOR SILL HAS SEVERAL AREAS OF CORROSION PRESENT ON FWD AND AFT SURFACES. REMOVED AND REPLACED L-2 DOOR SILL IN AFT CABIN BETWEEN FRAME 66 TO FRAME 68 AT STRINGER 23L IAW SRM 51-72-11-911-001 PARA D.

Part: FITTING — CORRODED (L2 DOOR SILL) · airframe 62,482 hrs · 25,134 cycles

L2 DOOR CUTOUT LOWER FWD CORNER FITTING HAD CORROSION ON THE SURFACE. REMOVED AND REPLACED AFT CABIN L2 DOOR SILL LOWER FWD CORNER FITTING AT FRAME 66, STRINGER 23L IAW SRM 51-72-11-911-001, PARAGRAPH 20.

Part: FITTING — CORRODED (FRAME 68) · airframe 62,482 hrs · 25,134 cycles

L-2 PASS/CREW DOOR CUTOUT LWR AFT CORNER FITTING HAS CORROSION O N SURFACE. REMOVED AND REPLACED AFT CABIN L-2 DOOR SILL LOWER AFT CORNER FI TTING AT FRAME 68 AT STRINGER 23L IAW SRM 51-72-11-911-001 PARA 2D

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,482 hrs · 25,134 cycles

RMLG DOOR ACTUATOR KEEL BEAM FITTING AFT SECTION UPPER SURFACE P RODUCED A CRACK INDICATION DURING HFEC INSPECTION EA 5330-04821 AD 2015-02-14 PER HAECO LCQ NR 9298541 GENERATED REMOVED AND REPLACED RMLG DOOR ACTUATOR KEEL BEAM FITTING AFT IA W A320 SRM 51-72-11-911-001 WORK ACCOMPLISHED INSPECT ED

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 62,482 hrs · 25,134 cycles

R/H AFT CABIN SHEAR PLATE AND FRAME SUPPORT STRUCTURE LOCATED BE NEATH FLOOR BOARDS BETWEEN FR 69-70 HAS CORROSION PRESENT ON BOT H SURFACES SUPPORT TASK PER HAECO LCQ NR 9294809 GENERATED REMOVED AND REPLACED R/H AFT CABIN SHEAT PLATE BETWEEN FR69-FR70 IAW A320 SRM 51-72-11-911 AND FOR FRAME SUPPORT JOB WILL BE ACC OMPLISHED ON HAECO OP #40900 AND UNITED LOGPAGE 9298900 WORK ACC OMPLISHED INSPECTED

Part: FITTING — CORRODED (FUSELAGE) · airframe 62,482 hrs · 25,134 cycles

R2 DOOR AT FR68 AFT CORNER FITTING HAS CORROSION PER HAECO LCQ N R LP 9299034 GENERATED REMOVED CORROSION FROM R2 DOOR AFT CORNER FITTING IAW A320 SRM 5 1-74-00-801 PARA 5.A4 FOUND TO BE OUT OF LIMITS WITH .140IN MATE RIAL LOSS FROM EDGE OF FITTING LEAVING INSUFFICANT EDGE DISTANCE AT FASTENER HOLE IAW A320 SRM 51-47-00-801 PA 2.A 1 REMOVED AND REPLACED IAW A320 SRM 51-72-11 PERFORMED

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,482 hrs · 25,134 cycles

RH AFT SHEAR PLATE SUPPORT HAS CORROSION ON UPPER SURFACE UNDER SHEAR PLATE SUPPORT TASK PER HAECO LCQ NR 9298900 GENERATED REMOVED AND REPLACED R/H AFT SHEAR PLATE SUPPORT IAW A320 SRM 51 -72-11-911-001 WORK ACCOMPLISHED INSPECTED

Part: STRINGER — CORRODED (FRAMES 55-58) · airframe 62,482 hrs · 25,134 cycles

AFT CARGO PITT ON STGR 42 BTWEEN FRAMES 55 TO FRAME 58 STGR IS C ORRODED SEE DOT DD01 (A3NB-05-3-6026) . REMOVED AND REPLACED WITH NEW STRINGER 42L FROM FR53 TO FR60 ON AFT CARGO COMPARTMENT IAW A320 SRM 51-42-11-801 AND 51-22-11-911 -001.

Part: SHEAR PLATE — CORRODED (FRAMES 69-70) · airframe 62,482 hrs · 25,134 cycles

L/H AFT CABIN SHEAR PLATE LOCATED BENEATH FLOOR BOARDS BETWEEN F R69-70 HAS CORROSION PRESENT ON SURFACE. REMOVED AND REPLACED SHEAR PLATE AT LH AFT CABIN LOCATED BENEATH FLOOR BOARD BETWEEN FR69-FR70 IAW A320 SRM 51-72-11-911-001.

Part: BOTTLE — DEFECTIVE (EVAC SLIDE) · airframe 56,705 hrs · 22,546 cycles

SLIDE BOTTLE EMER L MESSAGE ON POSTTEST FLT. R&R SLIDE RESERVOIR EMERG OVER WING LT IAW AMM 25-62-46-000-001-A.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 55,977 hrs · 22,199 cycles

EMERGENCY LIGHT BATTERY FAILED A BITE CHECK. REPLACED THE BATTERY PACK. SYSTEM CHECKED OK. VERIFIED BITE TEST, SYSTEM CHECKED OK.

Part: SLAT — OBSTRUCTED (NR 3) · airframe 55,271 hrs · 21,889 cycles

ECAM FOR F/CTL SLATS FAULT APPEARED AFTER TAKEOFF. EMERGENCY DECLARED. FOUND FUEL DOOR CAUGHT IN BETWEEN SLAT NR 3 AND WING. REMOVED AND REPLACED RIGHT WING SLAT NR 3 IAW MM-27-84-65-000-001-A AND DOOR ASSY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,164 hrs · 21,401 cycles

DURING EMERGENCY LIGHT TEST, AN EPSU UNIT MESSAGE DISPLAYED. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD IAW AMM 33-51-39.

Part: LENS — DEFECTIVE (CABIN) · airframe 53,474 hrs · 21,097 cycles

EMERGENCY PATH LIGHT AT ROW 2B INOP. REPLACED LENS CAP AND CHECKED LIGHT OK.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 47,549 hrs · 18,509 cycles

DIVERT TO PIT DUE LT REVERSER LIGHT EN ROUTE. ECAM FAULT ENG 2 REVERSER IAW AMM 78-31-00-710-041-A FOR CFDS OPERATIONAL TEST OF REVERSER. REVERSER FAULT CLEARED AT ENG SHUTDOWN ON ARRIVAL. ACCOMPLISHED OPERATIONAL REVERSER CHECK VIA CFDS. BOTH A & B CHANNELS RETURNED NO FAULTS. PRECAUTIONARY CLEANED LVDT ACTUATOR CONNECTORS & ACCOMPLISHED CFDS CHECKED AGAIN FOLLOWED BY ENG RUN OPERATIONAL CHECK WITH NO FAULTS RETURNING.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,159 hrs · 18,340 cycles

R2 DOOR SILL HAS CORROSION AT FRAME 68 AT PREVIOUS REPAIR. REPLACED DOOR SILL IAW SRM 51-42-11.

Part: SMOKE WARNING — FALSE INDICATION (COCKPIT) · airframe 45,178 hrs · 17,580 cycles

AVIONICS SMOKE ECAM MESSAGE DISPLAYED AFTER STARTING FIRST ENG. REMAINED AFTER SECOND ENG STARTED. SHUTDOWN ENGS & RETURNED TO GATE. RESET AEVC SYSTEM, NO FAULTS FOUND, AEVC TESTED OK. RAN BOTH ENGS, NO MESSAGE OR FAULTS. NO SMOKE NOTED IN AVIONICS OR CARGO COMPARTMENTS.

Part: HOSE — LEAKING (THRUST REVERSER) · airframe 44,350 hrs · 17,253 cycles

FLUID DRIPPING UNDER NR 2 ENG. REPLACED NR 2 ENG INBD THRUST REVERSER CROSSOVER HOSE IAW AMM. PERFORMED OPERATIONAL TEST OF THE THRUST REVERSER IAW AMM 78-31-00- 710-041-A13. NO LEAKS & OPERATIONS CHECKED NORMAL.

Part: CONTROL CABLE — BROKEN (RUDDER PEDAL) · airframe 44,216 hrs · 17,203 cycles

FIRST OFFICER`S RUDDER PEDALS WILL NOT LOCK IN POSITION. FOUND CABLE BROKEN FROM RUDDER PEDAL ADJUSTER MECHANISM. REPLACED CABLE IAW AMM, OPERATIONS CHECKED GOOD.

Part: HANDSET — INTERMITTENT (L1) · airframe 44,154 hrs · 17,183 cycles

1L HANDSET INTERMITTENT. REPLACED HANDSET AT 1L, OPERATION NORMAL.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 44,134 hrs · 17,174 cycles

HYD FLUID COMING DRAIN HOLE FWD OF RADAR ALT IN FRONT OF MAIN GEAR. FLUID COMING FROM BROKEN LINE, WHICH WAS REPAIRED, CLEANED UP LEAKING HYD FLUID.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 44,134 hrs · 17,174 cycles

BELOW FWD CARGO PIT'S J-S DRIVE MOTOR, BILGE AREA, FOUND "DOOR CLOSE PRESS" HYD LINE FOAMING & DRIPPING AT SUPPORT CLAMP, YELLOW SYS. PERFORMED RYNLOCK REPAIR ON THE HYD LINE IAW GPM 1-0-13-028 & AMM 20-23-11-300-007A. INSTALLED REPAIRED HYD LINE, LEAK CHECKED GOOD IAW AMM 20-23-11-911-001A.

Part: BOOT — MISINSTALLED (SIDE STICK) · airframe 43,020 hrs · 16,754 cycles

CAPTAIN`S SIDE STICK BOOT INSTALLED INCORRECTLY. REMOVED PINCHED SECTION OF SIDE STICK BOOT, ITEM OK FOR SERVICE.

Part: COMPUTER — FAILED (NR 1 & 2 ELAC) · airframe 42,761 hrs · 16,648 cycles

SIDE STICK PRIORITY DISPLAYED ON UPPER ECAM SCREEN. REPLACED ELAC1 & ELAC 2 IAW AMM 27-93-34, RETURNED ACFT TO FULL CAT III CAPABILITY AFS AND LAND VERIFICATION TESTS NORMAL, IAW AMM 22-96-00 AND 22-97-00.

Part: GUST LOCK — INOPERATIVE (L1 DOOR) · airframe 42,332 hrs · 16,475 cycles

L1 DOOR WILL NOT LOCK OPEN. REPLACED THE L1 DOOR STAY MECHANISM IAW AMM.

Part: COMPUTER — FAULTY (NR 1) · airframe 42,316 hrs · 16,467 cycles

PFR SHOWS "GPSW FLP MODE PB SW (7WZ)-SFFC1( 21CV)-GPWC(1WZ) 34-48-08" "SFCC1-2(21CV-22CV)-ADIRU2(1FP2) AOA I NPUT A & B 27-51-34" AND "SFCC1 21CV 27-51-34". PERFORMED GPWS, ADR2, SFC C2 BITES - NO FAULTS. RAN FLAPS NO MSGS. INSTALLED NEW SFCC 1 AND FINAL OPS CHECK SAT AS PER MM AND ASM.

Part: COMPUTER — FAULTY (NR 1) · airframe 42,315 hrs · 16,466 cycles

F-CTL FLAP SYS 1 FAULT ECAM. REPLACED NR 1 SFCC REF AMM 27-51-34-000-001-A.

Part: ACTUATOR — FAULTY (APU) · airframe 42,303 hrs · 16,461 cycles

APU FUEL SHUTOFF VALVE SHOWS AMBER IN TRANSITON LOWER ECAM FUEL PAGE. APU SYSTEM TO BE DEFERRED IN COMPLIANCE WITH MEL CARD 49060. APU FUEL SHUTOFF VALVE SHOWS AMBER IN TRANSITION LOWER ECAM FUEL PAGE. APU SHUTOFF VALVE INOP. REMOVED AND REPLACED APU LP ACT ASSY, NO HELP. ACTUATOR BELIEVED TO BE BAD OUT OF STOCK. REPLACED ACTUATOR, OPS CHECK GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 42,277 hrs · 16,451 cycles

DENT ON CROWN SKIN BETWEEN FR 84-85 S5R, D=.066, ON STR 5R AND FR84, BETWEEN DENTS 11.00. FABRICATED REPAIR AND INSTALLED IAW SRM 53-51-11 FIG 203. MAJOR REPAIR.

Part: FRAME — GOUGED (CARGO BAY) · airframe 42,277 hrs · 16,451 cycles

AFT CARGO BAY LEFT FRAME GOUGED AT FR 59, S36L. REPAIRED FRAME IAW SRM 53-00-12 FIG 201.

Part: CONTROL UNIT — NO TEST (RT AILERONS) · airframe 42,277 hrs · 16,451 cycles

RIGHT AILERON FAILS FREE PLAY CHECK. REMOVED AND REPLACED BOTH INBD AND OTBD RIGHT AILERON SERVOS CONTROL UNITS IAW AMM, OPS CHECKED GOOD IAW AMM. FREE PLAY CHECKED GOOD.

Part: SKIN — DENTED (FUSELAGE CROWN) · airframe 42,277 hrs · 16,451 cycles

DENT ON CROWN SKIN BETWEEN FR 48-49 S9L. INSTALLED REPAIR IAW SRM 53-00-11 FIG 204.

Part: HOLDER — INOPERATIVE (MICROPHONE) · airframe 41,789 hrs · 16,256 cycles

MICROPHONE HOLDER INOPERATIVE AT DOOR 1L.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 41,503 hrs · 16,154 cycles

DURING EMERGENCY LIGHTING TEST. MESSAGE 'EPSU BATTERY AFT DISPLAYED'. INSTALLED NEW BATTERY PACK AT 13WL AND FINAL OPS CHECK SATISFACTORY 33-51-38.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 41,334 hrs · 16,086 cycles

THE 1L DOOR ASSIST GAUGE IS LOW. SERVICED DOOR 1L ASSIST BOTTLE PER AMM.

Part: TRANSMITTER — LEAKING (FUEL SYSTEM) · airframe 41,111 hrs · 15,990 cycles

LEFT ENGINE FF XMITER LEAKING APROX 20 DROPS PER MIN AT IDLE. REPLACED FF TRANSMITTER PER AMM. LEAK CHECK AND OPS CHECK NORMAL.

Part: PACKING — NOT SEATED (NR 1 ENGINE) · airframe 41,092 hrs · 15,980 cycles

CREW REPORTS NR 1 ENGINE APPEARS TO HAVE OIL DRIP. FOUND OIL DRIP FROM OIL TANK SCUPPER DRAIN. FOUND PACKING ON OIL CAP PARTIALLY UNSEATED. SECURED PACKING AND CLOSED OIL TANK CAP. CLOSED FAN COWL PER MM 71-13-00-410-010. CLEANED COWLING.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 40,880 hrs · 15,882 cycles

EMERGENCY LIGHTS TEST PER 3 SVC WILL NOT PASS, GIVES MESSAGE EPSU BATTERY EMER R. REPLACED BATTERY PACK.

Part: COMPUTER — FAULTY (ELAC) · airframe 40,822 hrs · 15,858 cycles

ELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. ON SHUTDOWN. REPLACED ELAC COMPUTER. LAND VERIFY PASSED. AIRCRAFT REMAINS FULLY CAPABLE.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 40,716 hrs · 15,809 cycles

DOOR 1L EMERGENCY ASSIST BOTTLE PSI LOW. SERVICED DOOR 1L EMERGENCY ASSIST BOTTLE PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 40,592 hrs · 15,754 cycles

CABIN EMERGENCY LIGHTING CHECK FAILED, EPSU INT LOAD EMER L- DISPLAYED. REPLACED LEFT OVERWING EXIT LIGHT EPSU BATTERY. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,333 hrs · 15,653 cycles

EMERGENCY LIGHT TEST DOES NOT PASS, GIVES MESSAGE EPSU BATTERY EMER R MESSAGE AND NO GREEN LIGHT. CYCLED AIRCRAFT POWER TO RESET CIDS SYSTEM, TEST NOW NORMAL. SYSTEM OK MESSAGE DISPLAYED.

Part: OXYGEN MASK — DEFECTIVE (COCKPIT) · airframe 40,041 hrs · 15,532 cycles

CAPTAINS O2 MASK DEFECTIVE. REMOVED AND REPLACED O2 MASK, OPS GOOD.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 39,613 hrs · 15,349 cycles

HAD CABIN PRESSURIZATION FAULT DESCENDED TO 10,000 FT, OUTFLOW VLV FULL OPEN, MASK DID NOT DEPLOY. REPLACED BOTH CABIN PRESS CONTROLLERS AND PERFORMED ALL TESTS AS REQUIRED PER MM AND 05-53-00. NO FAULTS NOTED A-C OKAY FOR SERVICE.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 39,613 hrs · 15,349 cycles

CABIN PRESSURIZATION FAULT, DESCENDED TO 10,000 FT, OUTFLOW VALVE FULL OPEN, MASK DID NOT DEPLOY.

Part: SMOKE DETECTOR — FAULTED (LAVATORY) · airframe 39,227 hrs · 15,175 cycles

SMOKE LAVATORY DETECTOR FAULT. REPLACED THE LAV 'A' SMOKE DETECTOR, OPS CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SMOKE DETECTION) · airframe 38,143 hrs · 14,705 cycles

LAVATORY AND CARGO SMOKE DETECTION FAULT ECAM. SYSTEM RESET, NO HELP. REPLACED SDCU PER MM.

Part: FAIRING — UNSECURE (LT WING TE FLAP) · airframe 38,078 hrs · 14,679 cycles

FOUND LEFT WING INBD FLAP TRACK FAIRING LATERAL MOVEMENT OUT OF LIMITS. LATERAL MOVEMENT MEASURES (.562 INCHES) LIMIT IS .449 INCHES. REMOVED PANEL 531AT DISCONNECTED CONTROL AND SIDESTAY RODS MOVEABLE FLAP TRACK FAIRING LOWERED AND HELD UP IN POSITION WITH STRING. REBUSHED FLAP TRACK FAIRING I.A.W. AMM, SECURED FAIRING.

Part: BUSHING — WORN (LT WING TE FLAP) · airframe 38,078 hrs · 14,679 cycles

FOUND LEFT WING OUTBD FLAP TRACK FAIRING (NR 4) LATERAL MOVEMENT OUT OF LIMITS PER MM. LATERAL MOVEMENT MEASURES (.375 INCHES) LIMIT IS .158 INCHES. REMOVED PANEL 533AT DISCONNECTED CONTROL AND SIDESTAY RODS MOVABLE FLAP TRACK FAIRING LOWERED AND HELD UP IN POSTION WITH STRING. REPLACED BUSHINGS IAW AMM. SECURED FAIRING.

Part: BUSHING — WORN (RT WING TE FLAP) · airframe 38,078 hrs · 14,679 cycles

FOUND RIGHT WING OUTBD FLAP TRACK FAIRING LATERAL MOVEMENT OUT OF LIMITS PER MM. LATERAL MOVEMENT MEASURES (.250 INCHES) LIMIT IS .158 INCHES. REMOVED PANEL 633 AT DISCONNECTED CONTROL AND SIDESTAY RODS MOVEABLE FLAP TRACK FAIRING LOWERED AND HELD UP IN POSTION WITH STRING. REPLACED PHONOLIC FACED BUSHINGS IN SIDE-LOAD STAY. REASSEMBLED SIDESTAY & CONTROL RODS. SECURED FAIRING.

Part: BUSHING — WORN (RT WING TE FLAP) · airframe 38,078 hrs · 14,679 cycles

FOUND RIGHT WING NR 3 FLAP TRACK FAIRING LATERAL MOVEMENT OUT OF LIMITS PER MM. LATERAL MOVEMENT MEASURES (.230 INCHES) LIMIT IS .189 INCHES. REMOVED PANEL 632AT DISCONNECTED CONTROL AND SIDESTAY RODS MOVABLE FLAP TRACK FAIRING LOWERED AND HELD UP IN POSITION WITH STRING. REPLACED PHONOLIC FACED BUSHINGS IN SIDE LOAD STAY. REASSEMBLE SIDESTAY & CONTROL ROD. SECURED NR 3 FLAP FAIRING.

Part: FAIRING — UNSECURE (LT WING TE FLAP) · airframe 38,078 hrs · 14,679 cycles

FOUND LEFT WING NR 3 FLAP TRACK FAIRING LATERAL MOVEMENT OUT OF LIMITS PER MM. LATERAL MOVEMENT MEASURES (.437 INCHES) LIMIT IS .189 INCHES. REMOVED PANEL 532 AT DISCONNECTED CONTROL AND SIDESTAY RODS MOVABLE FLAP TRACK FAIRING LOWERED AND HELD UP IN POSITION WITH STRING. REBUSHED FLAP TRACK FAIRING I.A.W. AMM. SECURED FAIRING.

Part: PUMP — FAILED (NR 1 ENGINE) · airframe 37,702 hrs · 14,514 cycles

NR 1 ENG HYD PUMP FAILURE, RTFL.

Part: CONTROL VALVE — FAULTY (PARKING BRAKE) · airframe 37,554 hrs · 14,431 cycles

CREW REPORTS ACFT NEEDS EXTRA POWER TO GET ROLLING FROM STILL AND WHEN ADVANCING TO TAKEOFF POWER THE ACFT WAS LAGGING IN ACCELERATION. CREW FURTHER REPORTS THE RIGHT GEAR BRAKE TEMPS ARE 100+ DEGREES HIGHER THAN THE LEFT. TROUBLESHOT PER TSM 32-45- 00-810-806. REPLACED PARKING BRAKE CONTROL VALVE (72GG) PER AMM 32-45-51.

Part: SERVO CONTROL — MALFUNCTIONED (NLG STEERING) · airframe 37,249 hrs · 14,304 cycles

N-W STR FAULT DISPLAYED. SAMC TEXT: CONTACT SAMC, REF TSM 32-51-00 TASK 836. REPLACE NWS SERVO VALVE 6GC. REMOVED & REPLACED NOSE STEERING SERVO CONTROL, OPS GOOD.

Part: TUBE — CRACKED (HYDRAULIC SYS) · airframe 37,212 hrs · 14,285 cycles

BLUE HYD SYSTEM - FOUND HYD MOTOR LEAKING IN FWD LT SIDE OF WHEEL WELL LEAKING FLUID. FOUND BLUE RESERVOIR EMPTY. SLAT POWER CONTROL UNIT LEFT HYDRAULIC MOTOR LEAKING AT OUTBD AFT TRANSFER TUBE. REPLACED HYDRAULIC MOTOR. NO HELP, STILL LEAKING AT OTBD AFT TRANSFER TUBE. OTBD AFT TRANSFER TUBE IS CRACKED AT 6 O'CLOCK. ON ORDER OSTF #J6093. RMV'D HYD MOTOR AND VALVE BLOCK ASSY TO GAIN ACCESS ON REPLACEMENT OF THE CRACK TRANSFER TUBE. RMV'D & REPLACED CRACKED TRANSFER TUBE, REINSTALLED HYD MOTOR & VLV BLOCK ASSEMBLY. OPS CHECKED GOOD, NO LEAKS NOTED.

Part: UNKNOWN — DAMAGED · airframe 37,016 hrs · 14,193 cycles

HAIL DAMAGE DUE TO HAIL STORM.

Part: CONTAINER — CRACKED (LT OVERWING) · airframe 36,625 hrs · 14,031 cycles

LT OVER WING SLIDE ASSY HAS DELAM AND CRACK ALONG T/E FLANGE OF CONTAINER HOUSING. REPLACED LT OFF WING SLIDE.

Part: SKIN — CRACKED (NR 1) · airframe 34,999 hrs · 13,286 cycles

NR 1 ENGINE INLET COWL LIP SKIN HAS 7 INCH CRACK IN AREA K1. REPLACED NOSE COWL ASSY PER MM, OP CHECKS NORMAL ON ENGINE RUN.

Part: COMPUTER — FAULTY (NR 2 ELAC) · airframe 34,484 hrs · 13,026 cycles

ELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. ELAC NR 2 ECAM HAD SHARP SMOKE ODOR THAT IS GONE. TURNED OFF ELAC NR 2. DID NOT ATTEMPT A RESET DUE CONFIRMED SMOKE ODOR IN ELAC NR 2. REPLACED ELAC NR 2. ACCOMPLISHED ELAC OPERATIONAL TEST, AFS TEST AND LAND CAT III TEST. ALL TESTS PASS.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 32,390 hrs · 12,104 cycles

EMERGENCY LIGHT AT SEAT 2A & 2B INOPERATIVE. WORK ACP ON SMB W-U K3627F BY 93983 FOUND PIN IN CONNECTOR BELOW SEAT NOT ENGAGED- REPAIRED. ACP OPS CHECK.

Part: SHEAR PIN — BROKEN (AFT PAX DOOR) · airframe 32,390 hrs · 12,104 cycles

LT AFT ENTRY DOOR DAMPER AND EMERGENCY OPERATION CYCLE SHEAR PIN IS BROKEN. SHEAR PIN REPLACED AT SMB, SAFETY PIN REMOVAL AND ARMING DOOR TO BE ACCOMPLISHED ON JIC SEQ NO 441.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 31,477 hrs · 11,644 cycles

DURING 3 SVC CHECKED CABIN EMERGENCY LIGHTS. TEST FAILED WITH MSG EPSU L. REPLACED EPSU DOOR 2 LEFT. SYS CHECKED NORMAL.

Part: BATTERY — FAULTY (CABIN) · airframe 30,768 hrs · 11,342 cycles

EPSU BAT FWD L MESSAGE DISPLAYED AFTER TEST. REPLACED BATTERY, OKAY.

Part: MICROPHONE — FAULTY (OXYGEN MASK) · airframe 30,698 hrs · 11,318 cycles

CAPTAIN'S OXYGEN MIC WILL NOT TRANSMIT. REPLACED MASK, NO HELP. FOUND MASK STOWAGE BOX MIC LEAD BROKEN. REPLACED STOWAGE BOX, OPS CHECK OKAY. REPLACED STOWAGE BOX.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,861 hrs · 10,972 cycles

AISLE SEAT EEL LIGHTS ARE INOP AT SEAT 7 AND 15A. REPLACED LIGHT ASSY, OPS CHECKED GOOD.

Part: CONTROL UNIT — FAILED (NR 2) · airframe 28,888 hrs · 10,573 cycles

LGCIU2 REVERSER FAULT. FLIGHT DIVERTED. REPLACED LGCIU 2 AND REINSTALLED FLIGHT CONTROL UNIT AFTER TROUBLESHOOTING.

Part: MICROPHONE — FAULTY (OXYGEN MASK) · airframe 28,254 hrs · 10,325 cycles

CAPT OXYGEN MASK MIKE IS WEAK, UNREADABLE ACCORDING TO ATC. REPLACED O2 MASK.

Part: SMOKE WARNING — ACTIVATED (E&E BAY) · airframe 26,565 hrs · 9,700 cycles

AVIONICS SMOKE/ECAM. RTFL.

Part: UNKNOWN — SMOKE (CABIN) · airframe 26,043 hrs · 9,517 cycles

AVIONICS SMOKE DISPLAYED ON UPPER ECAM SCREEN, SMOKE CREW COMMENTS, AVIONICS SMOKE ECAM. S/O BLOWERS ETC. RESET, ECAM GONE, BUT WE STILL ODOR OF FAINT SMOKE. AVIONICS SMOKE ECAM. S-OBLOWERS ETC. RESET. ECAM GONE. BUT WE STILL SMELL FAINT SMOKE. INSPECTED AVIONICS AREAS, RAN BLOWER & EXTRACT FANS, NO SMOKE OR ANY OTHER DEFECTS NOTED. ACPD BITE CHK OF SDCU & AEVC, NO FAULTS.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 23,725 hrs · 8,708 cycles

OVERHEAD EMERGENCY LIGHT ABOVE ROWS 18-19 INOP. *S/D* LOOSE PIN IN CONNECTOR. SECURED LOOSE PIN -J- IN TERM BLOCK 7222VT. SYSTEM OPS OK.

Part: COMPUTER — FAULTED (NR 1) · airframe 23,538 hrs · 8,644 cycles

ELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. F-CTL CREW COMMENTS: ATTEMPTED 2 RESETS, NO JOY. 10-11-07 FOUND ELAC NR 1 FAULTED. REPLACED ELAC NR 1.

Part: ENGINE — VIBRATION (NR 1) · airframe 21,061 hrs · 7,784 cycles

LANDED UNDER AMBER ALERT DUE TO NR 1 ENGINE VIBRATION. HPC STAGES 3 AND 6 WERE BORESCOPED AND DAMAGE WAS FOUND "BEYOND ALL LIMITS". LATER RECEIVED VERBAL CONFIRMATION THAT THE DAMAGE WAS AT STAGE 3. REPLACED NR 1 ENGINE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 19,319 hrs · 7,155 cycles

FOUND EMERGENCY LIGHTS TEST FAILED. FAULTING EPSU BATTERY FWD LEFT. REPLACED BATTERY PACK AT FWD LEFT POSITION. TEST PASSED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,028 hrs · 6,669 cycles

EMERGENCY LIGHTS AT SEATS 12 & 17 A,B,C HAVE ONE BULB INOP. RELAMPED. OPS CHECKED GOOD.

Part: WIRE HARNESS — FAILED (NR 1 BRAKE) · airframe 11,248 hrs · 4,223 cycles

DURING FLIGHT RECEIVED LOST NR 1 BRAKE SYSTEM ECAM MSG. PRECAUTIONARY LANDING. AIRCRAFT TOWED TO GATE & THE PROBLEM WAS ADDRESSED. ON SUBSEQUENT FLIGHT THE SAME SCENARIO OCCURRED. WIRING HARNESS FAILED DUE TO SHORT TO GROUND FROM FRETTING. REPLACED WIRING HARNESS. OPERATIONS CHECK NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 921 hrs · 312 cycles

AFT FUSELAGE SKIN DAMAGED FROM STRINGER 40R TO STRINGER 41R. THIS IS CLASSIFIED AS A MAJOR REPAIR. *S/D* THE DAMAGED AREA WAS CUT OUT AND REPAIRED BY THE INSTALLATION OF A FILLER AND ONE EXTERNAL DOUBLER. AN INSPECTION WAS PERFORMED AND THE REPAIR WAS APPROVED.