N428UA

Part: AUTOBRAKE SYS — NO TEST (ZONE 700) · airframe 92,065 hrs · 36,671 cycles

BRAKES AUTO BRK FAULT AFTER GEAR EXTENTION TEST RESULTS PERFORMED BITE CHECK-BITE TEST OF BSCU NORMAL BRAKING TEST PER AMM TASK 32-46-00-740-005-A. NO FAULTS FOUND ON BSCU CHANNELS 1 OR 2. NO FAULT HISTORY IN THE PAST 90 DAYS IN SCEPTRE. NO CURRENT FAULTS ON ECAM. A/C OK TO CONTINUE.

Part: ENGINE — VIBRATION (NR 2) · airframe 91,722 hrs · 36,483 cycles

ENG 2 N1 VIB INDICATION ON MEL TOMC APPROVES MEL 7700G FOR ENG 2 N1 VIB TURNS YELLOW X OCCASIONALY. REPLACED EVMU IAW MM77-32-34/401 , IPC REF 77-32-34-01A NO HELP STATUS MESSAGE NEED FURTHER T/S. ADJUST AND TEST IAW MM UNIT, ENGINE VI OFF 31-7731-9-0001 0564 ON 31-7731-9-0001 0375 UNIT, ENGINE VI OFF 31-7731-9-0001 0564 ON 0000 32-34-710-041 A NEED FURTHER T/S. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1369085 SN OFF 0564.

Part: FUEL CAP — MISSING (REFUEL COUPLING) · airframe 89,978 hrs · 35,659 cycles

PDA 2 FUEL CAP WAS FOUND MISSING PRIOR TO REFUELING FUEL CAP WAS CONFIRMED LEFT ON TRUCK IN IAD PRIOR TO FLIGHT 1262-02 COMPLIED WITH GMM. REPLACED FUEL/DEFUEL COUPLING CAP IAW AMM 28-25-41-400-005-A, OK FOR SVC.

Part: PROXIMITY SENSOR — FAULTY (MLG) · airframe 88,968 hrs · 35,210 cycles

L/G NOT UPLOCKEDWITH SHOCK ABSORBERFAULT DURING DEBREIF PILOT STATED IT WAS THE NLG SHOCK ABSORBER FAULT. ADDING POST FLIGHT REPORT REMOVED UNSERVICEABLE PROX SENSOR 24GA AND INSTALLED SERVICEABLE RECOMMEND FOLLOWING TSM 32-31-00-810-868-A SUSPECT SENSOR 24GA OR 25GA, REQUIRES LGCIU BITE CHECK TO ONE PER AMM 32-31-73-400-005-A OPS CHECKS AND BITE CHECKS GOOD. CONFIRM SEALANT REQUIRED ON NUTS AND SCREW ENDS. ADD EMP:U172529,U167026,U381122 FOUND FLIGHT/GROUND SENSING BRACKET WITH EXCESSIVE PLAY. DISCOVERED BOLT THAT SECURES CASING TO PIN ON STRUT WAS MISSING. PICTURES ATTACHED SHOWING POSITION HELD IN MOST FWD/AFT POSITION. T/S PER TSM 32-31-00-810-868A NLG SCHOCK ABSORBER (LG WILL NOT RETRACT).FOUND NO SET SCREW AT FITTING LEG ASSY CAUSING EXCESSIV E PLAY.REPLACED PROX SENSORS 24GA & 25GA.STRUT DIMENSION GOOD. PERFORMED GEAR SWING ALL OPERATIONAL CHECKS GOOD.

Part: WINDOW FRAME — CRACKED (FRNT WINDSHIELD) · airframe 88,685 hrs · 35,081 cycles

FLIGHT DECK LOWER NODE R/H AND L/H I/B HOLES HAVE CRACK INDICATIONS. ACCOMPLISHED INTERIM REPAIR OF THE FRONT WINDSHIELD FRAME AND CONTINUITY FITTINGS PER ECRA 5311-03068 REV- PT1, QC INTERIM REPAIR PERFORMED PER PART 1 OF ECRA 5311-03068. PER PART 1 STEP 3-FOR THE FRONT WINDSHIELD FRAME AND CONTINUITY FITTINGS, PLANNING TO CONTACT ENGINEERING AFTER 63,681 TOTAL AIRCRAFT FLIGHT CYCLES BUT BEFORE 64,681 TOTAL AIRCRAFT FLIGHT CYCLES FOR THE ECRA 5311-03068 PART 2 INSPECTION REQUIREMENTS. (CURRENT PTC 35081) TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED. INSPS OF THE FRONT WINDSHIELD FRAMES AND CONTINUITY FITTINGS PER PART 2 OFTHE LATEST REVISION OF ECRA 5311-03068 ON OR BEFORE THE AC REACHES 65681 TOTAL AIRCRAFT FLIGHT CYCLES ACCOMPLISHED INTERIM REPAIR OF THE FRONT WINDSHIELD FRAME AND CONTINUITY FITTINGS PER ECRA 5311-03068 REV-, PT1 QC INTERIM REPAIR PERFORMED PER PART 1 OF ECRA 5311-03068. PER PART 1 STEP 2.

Part: WINDOW FRAME — DAMAGED (FRNT WINDSHIELD) · airframe 88,685 hrs · 35,081 cycles

FRONT WINDSHIELD FRAME AND CONTINUITY FITTING HAVE REJECTABLE INDICATIONS "ACCOMPLISH INITIAL INSPS OF THE FRONT WINDSHIELD FRAMES OF ECRA 5311-03068 ON OR BEFORE THE AC REACHES 65681 TOTAL AND CONTINUITY FITTINGS PER PART 2 OFTHE LATEST REVISION AIRCRAFT FLIGHT CYCLES ACCOMPLISHED INTERIM REPAIR OF THE FRONT WINDSHIELD FRAME AND CONTINUITY FITTINGS PER ECRA 5311-03068 REV-, PT1 INTERIM REPAIR PERFORMED PER PART 1 OF ECRA 5311-03068. PER PART TOMC-APPROVAL FROM SC1ELBYC COMMENT 1 STEP 2-ACCOMPLISH INITIAL INSPECTIONS OF THE FRONT WINDSHIELD FRAMES AND CONTINUITY FITTINGS PER PART 2 OF THE LATEST REVISION OF ECRA 5311-03068 ON OR BEFORE THE AIRCRAFT REACHES 65,681 TOTAL AIRCRAFT FLIGHT CYCLES. PART 2 RECHECK IS TBD BY EG. QC RECORDS UPDATE ...HC QC REVIEWED. T/A : 65,681 TAFC ....HC/U389717

Part: PANEL — CRACKED (RH FR35-36) · airframe 88,685 hrs · 35,081 cycles

LOG PAGE FOR NEW DTA DIP REQUIREMENTS PER ECRA 5311-02197 REV D PT 1B REFERANCE LOG PAGE #3786677 "FOR RH FR35-36 PRESSURE PANEL, HOLES #A1- #A28, PLANNING AC FH''S (WHICHEVER COMES FIRST), BUT BEFORE 61707 TOTAL AC TO CONTACT ENG''ING AFTER 60707 TOTAL AC FH''S OR 141152 TOTAL ACCOMP''D INTERIM REPAIR OF THE FR36RH PRESSURE HOLES AS PER ECRA 5311-02197 REV. D, PT 1B OK TO DIP PER ECRA 5311-02197D. FOR RH FR35-36 PRESSURE PANEL, TOMC-APPROVAL FROM SC1ELBYC COMMENT HOLES #A1- #A28, PLANNING TO CONTACT ENGINEERING AFTER 60,707 TOTAL AIRCRAFT FLIGHT CYCLES OR 141,152 TOTAL AIRCRAFT FLIGHT HOURS (WHICHEVER COMES FIRST), BUT BEFORE61,707 TOTAL AIRCRAFT FLIGHT CYCLES OR 142,152 TOTAL AIRCRAFT FLIGHT HOURS (WHICHEVER COMES FIRST), FOR THE PART 2 INSPECTION REQUIREMENTS. QC QC REVIEW INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: UNKNOWN — CRACKED

5 CRACKS NOT CONTAINED WITHIN AREA A1. OUT OF SUBTASK 72-50-00-230-071 ACCEPTANCE LIMITS. LIFE LIMITED PART (LLP) TO BE RETIRED WITH 12565 CYCLES SINCE NEW (LLP LIMIT IS 20000 CYCLES)

Part: FUEL CAP — MISSING (FUEL PANEL) · airframe 88,112 hrs · 34,822 cycles

FUELER REPORTS FUEL CAP MISSING. INSTALLED FUEL CAP.

Part: COUPLING — UNKNOWN (REFUEL) · airframe 88,086 hrs · 34,813 cycles

PDA 2 REF LP 4548150 - ON ARRIVAL, FUELER REPORTS FUEL CAP MISSING. REFER LP# 4548160 UPDATE INFO...ACCOMPLISHED ACFT WINGS AND FUSELAGE VISUAL INSPECTION. NO DAMEGE FOUND. OK TO CONTINUE.

Part: LIGHT — INOPERATIVE (AFT EMER BATTERY) · airframe 86,206 hrs · 33,863 cycles

CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - AFT EMERGENCY BATTERY FAILED CAP TEST REMOVED AND REPLACED AFT EMERGENCY BATTERY. OPS CHECK GOOD

Part: RELAY — INOPERATIVE (OTHER) · airframe 86,182 hrs · 33,850 cycles

AUTO FLT ''A-THR OFF''DISPLAYED ON UPPER ECAM SCREEN. AUTO THRUST FAIL TROUBLESHOT PER TSM 22-31-00-810-812-A. PERFORMED GROUND SCAN OF THE AFS AND REPLACED RELAYS 17CA1, 17CA2, 18CA1, 18CA2, 5CA1, AND 5CA2. ENG 2 EEC WAS ALSO REPLACED FOR ANOTHER PROBLEM, SEE LOGPAGE 9258776 FOR REPLACEMENT. NEEDS ANOTHER AFS GROUND SCAN. PERFORMED GOUND SCAN PER AMM 27-96-00-740-001A ,OP CK ,NO FAULTS FOUND.

Part: LIGHT — FAILED (L1) · airframe 84,578 hrs · 33,140 cycles

EPSU EXT LOAD FWD L ON FORWARD PANEL DURING EMERGENCY LIGHT TEST. REF 33-51-38.

Part: PACKING — LEAKING (PTU) · airframe 83,183 hrs · 32,505 cycles

HYD Y QTY LOW...SYSTEM NORM B4 T/O LOST FLUID AT ALTITUDE PER CAPTAIN YELLOW HYDRAULIC SYSTEM RAN WITH 0 QTY. INSPECTED MLG WHEEL WELL AND FOUND YELLOW SYSTEM PRIORITY MANIFOLD ASSY (3015GM) MISTING HYD FLUID. REF IPC 29-13-15-02A SUSPECT ITEM 40 AND 10. IPC PAPERWORK IN FLIGHT DECK. TORQUE UNION ON PTU MANIFOLD YELLOW HYD SYSTEM. REPLACED PACKING, O-RING. LEAK CHECKED ITEM 46 AND 47 NO LEAKS DETECTED, FOUND ITEM 10 LEAKING IPC 29-13-15-02A SHEET 1, REPLACED O RING ITEM 40 AND REPLACED ITEM 10 REF AMM 29-13-15 OPS GOOD NO LEAKS NOTED. AND REPLACED # 2 ENGINE HYDRAULIC CASE DRAIN FILTER PER TSM NO LEAKS DETECTED. ADD EMP:177154

Part: HYDRAULIC LINE — LEAKING (LT MLG) · airframe 79,871 hrs · 31,046 cycles

HYDRAULIC QUANTITY LOW LEFT OR GREEN SYSTEM SHOWING 4.5 LITRESIN FLIGHT FL350 FOUND EVIDENCE OF HYD LEAK ON LOWER FUSELAGE JUST BEHIND THE GEARWHEEL PREVIOUS UPDATE NO HELP WILL NEED TO START TROUBLESHOOTING FOUND LEFT MLG HOSE LEAKING. R/R HOSE LEAK AND OPS CHECK GOOD

Part: ROLLER — LACK OF LUBE (TE FLAP) · airframe 79,010 hrs · 30,637 cycles

FLAPS LOCKED - ALIGNMENT FAULT DISPLAYED ON UPPER EC AM SCREEN. - F-CTL PLEASE WORK FAULTS IAW TSM 27-51-00-810-818-A. TOMC SMITH 847-700-9980 CONTACT TOMC 847-700-9980 UNLOCKED FOR AVIONICS UPDATE, TOMC SMITH SFCC BITE , NO CURRENT FAULT FOUND. ON LAST LEG REPORT(POST FLIGHT) FOUND " CHECK LT DRIVE INTEGRITY" 27-51-00. CONTINUED WITH TSM 27-51-00-810-818A SEE NOTE STEP3 A. CONTINUED WITH GVI FOR ELECTRICAL HARDWARE ON FLAP INTERCONNECTING STRUT. LOOKED AT CONNECTORS, AND HARNESS, SENSORS, NO DAMAGE NOTED. CYCLED FLAPS SEVERAL TIMES NO DUPLICATED FAULT FOUND. LOG PAGE LOCKED BY TOMC OK TO UNLOCK TOMC SMITH DURING VISUAL INSPECTION, FOUND LT FLAP CARRIAGE ROLLERS REQUIRED ADDITIONAL GREASE. LUBRICATED LT CARRIAGE ROLLERS AS REQUIRED. REF AMM 12-22-27

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 78,952 hrs · 30,607 cycles

AFT PIT FR56-57 STR 38R INTERCOSTAL TOP SURFACE CORROSION A3NB-5 3-4-5179 PER NON ROUTNE 9293340 REMOVED AND REPLACED CORRODED INTERCOSTAL AT FR56-57 STR38R IAW CRA 5341-01175.

Part: SKIN — DENTED (FUSELAGE) · airframe 78,952 hrs · 30,607 cycles

FUSELAGE EXTERIOR SKIN LOWER LOBE FR25-26 STR 41-43 RT SKIN DENTED A3NB-53-3-6105 PER NON ROUTINE 9293391 DISCREPANT LOCATION SHOULD READ FR25-26, STR 42R-43R. ACCOMPLISHED INTERIM REPAIR PER ECRA 5331-02415 PART 1. ACCOMPLISH THE INITIAL INSPECTION REQUIREMENTS PER PART 2 OF ECRA 5331-02415 ON OR BEFORE THE AIRCRAFT REACHES 77807 TOTAL AIRCRAFT FLIGHT CYCLES. PLANNING TO CONTACT ENGINEERING AFTER 75807 BUT BEFORE 76807 FOR THE INSPECTION REQUIREMENTS. CURRENT FC 30607. T REPAIR: THE ACCOMPLISHED REPAIR IS CONSIDERED PERMANENT BEFORE THE AIRCRAFT REACHES THE NOTED THRESHOLD. PART 3 PERMANEN PART 2 INSPECTION REQUIREMENTS: TO BE DETERMINED BY ENGINEERING PROVIDED THAT THE STATED INSPECTION REQUIREMENTS ARE COMPLIED WITH. PER ECRA 5331-02415. MUST ACCOMPLISH THE INITIAL INSPECTION REQUIREMENTS PER PART 2 OF ECRA 5331-02415 ON OR BEFORE THE AIRCRAFT REACHES 77,807 TOTAL AIRCRAFT FLIGHT CYCLES. PLANNING TO CONTACT ENGINEERING AFTER 75,807 BUT BEFORE 76,807 FOR THE INSPECTION REQUIREMENTS. OK TO DIP INTERIM RPR ON FUSELAGE DENTS AT FR25-26; STR41-43 RH TOMC-APPROVAL FROM SC1ELBYC COMMENT REVIEWED QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 78,952 hrs · 30,607 cycles

DURING INSPECTION AND MODIFICATION PER EA 5330-05216 OP2 AT LT PRESSURE PANEL AT FR35-36 HOLES SHOWN FIGURE 1 WERE FOUND WITH CRACK INDICATIONS DAMAGE IS BEYOND EA LIMITS PER NON ROUTINE 9293540 ACCOMPLISHED INTERIM REPAIR AT LH PRESSURE PANEL FR 35-36 HOLES IAW ECRA 5311-02199 PART 1 STEP 1. ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF ECRA 5311-02199 ON OR BEFORE 05JAN2020. PLANNING TO CONTACT ENGINEERING AFTER 15DEC2019 BUT BEFORE 25DEC2019 FOR PERMANENT REPAIR. ALL WORK ACCOMPLISHED ON NR 9293540. APPROVED TO CARRY REF ECRA 5311-02199 PERMANENT REPAIR TO BE ACCOMPLISHED ON OR BEFORE 05JAN20, PLANNING TO CONTACT ENGINEERING AFTER 15DEC19 BUT BEFORE 25DEC19. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEW QC REVIEW INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 78,952 hrs · 30,607 cycles

DURING INSPECTION AND MODIFICATION PER EA 5330-05216 OP3 AT RT PRESSURE PANEL AT FR35-36 HOLES SHOWN IN FIGURE 1 WERE FOUND WITH CRACK INDICATIONS DAMAGE IS BEYOND EA LIMITS PER NON ROUTINE 9293541 ACCOMPLISHED REPAIR AT RT PRESSURE PANEL AT FR 35-36 HOLES IAW ECRA 5311-02197 PART 1 STEP 1. ACCOMPLISH A PERMANENT REPAIR PER P ART 3 OF ECRA 5311-02197 ON OR BEFORE 03JAN2020. PLANNING TO CONTACT ENGINEERING AFTER 13DEC2019 BUT BEFORE 23DEC 2019 FOR PERMANENT REPAIR. ALL WORK ACCOMPLISHED ON NR 9293541. APPROVED TO CARRY REF ECRA 5311-02197 PERMANENT REPAIR TO BE ACCOMPLISHED ON OR BEFORE 03JAN20, PLANNING TO CONTACT ENGINEERING AFTER 13DEC19 BUT BEFORE 23DEC19. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEW QC REVIEW INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT.

Part: PLATE — CORRODED (FUSELAGE) · airframe 78,952 hrs · 30,607 cycles

AFT CARGO PIT SKIN PLATE BETWEEN STRG 38R-39R IS CORRDED APPRX. 2" AFT FRAME 65 A3NB-53-3-6185 PER NON ROUTINE 9293158 ACCOMPLISHED REPAIR IAW ECRA 5331-02416 PART 1. ACCOMPLISH THE IN ITIAL INSPECTION REQUIREMENTS PER PART 2 OF ECRA 5331-02416 ON OR BEFORE THE AIRCRAFT REACHES 94,607 TOTAL AIRCRAFT FLIGHT CYCLES. PLANNING TO CONTACT ENGINEERING AFTER 92,607 FC BUT BEFORE 93, 607 FC FOR THE INSPECTION REQUIREMENTS.ALL WORK ACCOMPLISHED ON NR 3777990. APPROVED TO CARRY REF ECRA 5331-02416, ACCOMPLISH INITIAL INSPECTION ON OR BEFORE ACFT REACHES 94,607 TOTAL ACFT FLIGHT CYCLES. PLANNING TO CONTACT ENGINEERING AFTER 92,607 BUT BEFORE 93,607 FOR THE INSPECTION REQUIREMENTS . TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEW QC REVIEW INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT R

Part: KEELBEAM — DAMAGED (FUSELAGE) · airframe 78,952 hrs · 30,607 cycles

DURING ACCOMPLISHMENT OF FCD 5330-05575 REV D KEEL BEAM HOLES LABELED L2, L8, L21, L74, 10, R18 AND R19 WERE FOUND OUT OF ROUND ECRA 5311-02186 APPENDIX A DEFINES LOCATION AND DETAILS OF THE DISCREPANT HOLES PER NON ROUTINE 9293501 ACCOMPLISHED INTERIM REPAIR IAW ECRA 5311-02186. ACCOMPLISH A PER MANENT REPAIR ON THE KEELBEAM HOLES PER PART 3 OF ECRA 5311-021 86 ON OR BEFORE 01-JUL-2020, PLANNING TO CONTACT ENGINEERING AFTER 01-MAY-2020 BUT BEFORE 01-JUN-2020 FOR THE PERMANENT REPAI R.ALL WORK ACCOMPLISHED ON NR 9293501. APPROVED TO CARRY REF ECRA 5311-02186 PERMANENT REPAIR TO BE ACCOMPLISHED ON OR BEFORE 01JUL20. PLANNING TO CONTACT ENGINEERING AFTER 01MAY20 BUT BEFORE 01JUN20. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEW QC REVIEW INSPECTIONS CREATED BY AUTODIP PENDING A.

Part: SKIN — DENTED (FUSELAGE) · airframe 78,952 hrs · 30,607 cycles

REF LOG PAGE 3639919 DENT FOUND CREASE OUT OF LIMITS RE-EVALUATE DENT AND POSSIBLE CREASE BELOW LH PAX WINDOW 2 STA897+ FR23-24 STR21-22L PER NON ROUTINE 9293275 DENT FOUND TO BE OUT OF LIMITS PER SRM 53-11-11-283-001 AND SRM 53-11-11-283-012 DIA 02. ACCOMPLISHED LIMITED CUTOUT EXTERNAL REPAIR AT DAMAGED AREA IAW SRM 53-00-11-300-029 FIG. 01. THIS REPAIR IS CATEGORY B. IT IS NECESSARY TO INSPECT THIS REPAIR AT DEFINED INTERVALS PER SRI 53-00-11-205-017. INSPECTION LOCA TION IS ZONE A PER SRI 53-00-11-205-017 FIG. 01, SHT. 3. N TBD. INSPECTION METHOD TBD. CURRENT FC=30607, FH=78952:22. FC, 120000 FH WHICHEVER IS ACHIEVED FIRST. SUBSEQUENT INSPECTIO INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT IS 60000 CLEARED ORIGINATING LOG PAGE 3639919. OKAY TO DIP FOR 60,000 FC / 120.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 78,952 hrs · 30,607 cycles

CLEAT AT FR 65 STR 39R HAS CORROSION PER NR LP 9293324 REMOVED AND REPLACED CLEAT AT FR63 STR 39R IAW SRM 51-72-11 -911-001.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 78,952 hrs · 30,607 cycles

FWD CARGO FR32 CLEAT STR 40R-39R HAS CORROSION PER NR LP 9293169 REMOVED AND REPLACED FWD CARGO CLEAT AT FR32 STR 40R TO 39R IAW SRM 51-72-11-911-001.

Part: STRAP — CORRODED (FUSELAGE) · airframe 78,952 hrs · 30,607 cycles

FWD CARGO STRAP BELOW CLEAT AT FR29 ST41R-40R HAS CORROSION ON REF 9293149 SPEC A3NB-05-3-6013. REMOVED & REPLACED LOWER STRAP BELOW CLEAT AT FR29 ST 41R-40R IAW SRM 51-42-11 PARA E & SRM 51-72-11 PARA 3 & 4 AT ON HANGAR NR 9293149.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,952 hrs · 30,607 cycles

AFT CARGO FLOOR FR59 STR40R HAS CORROSION A3NB-53-4-6179 PER NON ROUTINE 9293045 REMOVED AND REPLACED STR 40R B/W FR58-63 IAW SRM 51-72-11-9 11-001 AND 51-42-11-001.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 78,952 hrs · 30,607 cycles

FWD CARGO CLEAT FR30 STR 42R-41R HAS CORROSION ON REF 9293153 SPEC A3NB-05-3-6013. REMOVED & REPLACED FWD CARGO CLEAT AT FR30 STR 42R TO 41R IAW SRM 51-72-11-911-001 AT ON HANGAR NR 9293153.

Part: SKIN — DENTED (FUSELAGE) · airframe 78,952 hrs · 30,607 cycles

LWR FUSELAGE EXTERIOR SKIN BETWEEN FR28-29 STR43R HAS DENT A3NB- 05-3-6003 PER NON ROUTINE 9292198 REPAIRED LWR FUSELAGE EXTERIOR SKIN B/W FR28-29R AT STR43R IAW SRM 53-00-11-300-042.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,952 hrs · 30,607 cycles

FWD PIT STR 39 FRAME 28-29 HAS SPOTS OF CORROSION. A3NB-53-3-61 05. NR 9293222 REPAIRED STR 39L BTW FRAMES 28 & 29 AT FWD PIT IAW SRM 53-00-13-300-001 FIG 1 SHEET 3 THIS REPAIR REQUIRES REINSPECT AT 60000FC OR 12000FH FROM REPAIR EMBODIMENT. SUBSEQUENT INSPECTION INTERVALS AND METHODS TBD IAW SRI 53-00-13-205-001 STEP 2 A 1 TABLE 2. OKAY TO CARRY FORWARD REPAIR AT STRINGER 39L BETWEEN FRAMES 28 - 29 IN FORWARD PIT PER SRM 53-00-13-300-001 FIG 1 SHEET 3. THIS REPAIR REQUIRES AN INSPECTION AT 60,000 FLIGHT CYCLES (FC) OR 120,000 FLIGHT HOURS (FH) FROM DATE OF AIRCRAFT FIRST FLIGHT. SUBSEQUENT REINSPECTION INTERVAL AND METHOD TO BE DETERMINED AT A LATER DATE PER SRI 53-11-13-205-001. MAJOR REPAIR NOTED DUE TO STRINGER SPLICE PER SRM 53-00-13-300-001. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED RECORDS UPDATE QC REVIEWED T/A: 60K TAFC OR 120K TAFH...SN

Part: CLEAT — CORRODED (FUSELAGE) · airframe 78,952 hrs · 30,607 cycles

FWD PIT HAS CORROSION CLEAT AT FR33 STR42L-43L A3NB-53-3-6112 PER HAECO LCQ NON ROUTINE 9293190 REMOVED AND REPLACED CLEAT IN FWD CARGO AT FR33 BETWEEN STR 42L- 43L IAW SRM 51-72-11-911-002 PARA 2.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,952 hrs · 30,607 cycles

FWD PIT BILGE AREA FR 29 STR 42-43R SKIN HAS DAMAGE HOLT AT CLEAT AREA PER NR 9293008 AND REPAIRED FWD PIT BILGE AREA AT FR29 STR 42-43R IAW SRM 53-0 0-11-300-043.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,952 hrs · 30,607 cycles

AFT CARGO FLOOR FR 56-57 STR 40 RT CORROSION. A3NB-53-4-6179, NR 9293053 REMOVED AND REPLACED AFT CARGO STR 40R FRAME 56-57 IAW SRM 51-72-11-911-001 & SRM 51-42-11-001.

Part: SKIN — DENTED (TAILCONE) · airframe 78,952 hrs · 30,607 cycles

2EA DENTS ON TOP OF TAIL CONE APPROX. 1FT LEFT OF RUDDER TRAILING EDGE TRIANGLE. A3NB-05-3-6072. NR 9292361 REPAIRED DENTED AREA BTEWEEN FR51 AND FR82 STR 2L AND 3L IAW SRM 53-51-11-300-002 FIG 01.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 78,952 hrs · 30,607 cycles

FWD PIT FR31 STR42-43LT CLEAT CORRODED A3NB-05-3-6013 PER NON ROUTINE 9293394 REMOVED AND REPLACED CLEAT IN FWD CARGO AT FRAM 31 BETWEEN STR 42L TO 43L IAW SRM 51-72-11-911-002 PARA 2.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 78,952 hrs · 30,607 cycles

FWD CARGO FR29 STR43L-42L CLEAT HAS CORROSION A3NB-05-3-6013 PER NON ROUTINE 9292919 REMOVED AND REPLACED CLEAT IN FWD CARGO AT FR 29 BETWEEN STR 42L TO 43L IAW SRM 51-72-11-911-002 PARA 2.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 78,952 hrs · 30,607 cycles

FWD PIT CLEAT FRAME 31 STR 42R-43R IS CORRODED A3NB-53-3-6105 PER NON ROUTINE 9293216 REMOVED AND REPLACED CLEAT IN FWD CARGO AT FR 31 BETWEEN ST 42R AND 43R IAW SRM 51-72-11-911-002 PARA 2.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 78,952 hrs · 30,607 cycles

FWD CARGO CLEAT FR30 ST43L-42L HAS CORROSION A3NB-05-3-6013 PER NON ROUTINE 9293157 REMOVED AND REPLACED CLEAT IN FWD CARGO AT FRAME 30 BETWEEN STRINGER 42L AND STRINGER 43L IAW SRM 51-72-11-911-002.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 78,952 hrs · 30,607 cycles

FWD CARGO FR29 ST43R-42R CLEAT HAS CORROSION A3NB-05-3-6013 PER NON ROUTINE 9292916 REMOVED AND REPLACED CLEAT AT FWD CARGO FR29 B/W STR43R-42R IAW SRM 51-72-11-911-001 AND SRM 51-42-11-001.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,952 hrs · 30,607 cycles

FWD CARGO STR 40R HAS CORROSION BETWEEN FR31-32 ON REF 9293168 SPEC A3NB-05-3-6013. REMOVED & REPLACED STR 40R AT FWD CARGO FR29-35 IAW SRM 51- 7-11-001 & SRM 51-42-11-001 AT ON HANGAR NR 9293168. MAINT PERFORMED RII INSP PERFORMED.

Part: STRINGER — CORRODED (FRAME 65) · airframe 78,952 hrs · 30,607 cycles

AFT CARGO PIT STRINGER 39R JUST AFT OF FRAME 65 IS CORRODED. REMOVED AND REPLACED AFT CARGO PIT STRINGER 39R IAW A320 51-72-1 1-911-001.

Part: NOT REPORTED — CORRODED (FRAME 59) · airframe 78,952 hrs · 30,607 cycles

AFT CARGO FLOOR FR59 STR43 RT CORRODED. REMOVED AND REPLACED STR43RT FR57-60 IAW SRM 51-42-11 AND S RM 51-72-11-911-001.

Part: CARGO TRACK — CORRODED (FRAME 65) · airframe 78,952 hrs · 30,607 cycles

AFT CARGO CLEAT HAS CORROSION AT FR 65 STR43LT. REMOVED AND REPLACED AFT CARGO CLEAT IAW SRM 51-42-11-001.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 78,952 hrs · 30,607 cycles

FWD CARGO FR32 CLEAT ST41R-40R HAS CORROSION A3NB-05-3-6013 PER HAECO LCQ NON ROUTINE 9293167 GENERATED BY N078625 REMOVED AND REPLACED CLEAT AT FRAME 32 BETWEEN STRINGER 40R TO S TRINGER 41R IAW A320 SRM 51-72-11-911-002.

Part: FLOOR SUPPORT — BENT (FRAME 54) · airframe 78,952 hrs · 30,607 cycles

AFT CARGO FLOOR FR54 STR43RT AND 43LT FLOOR SUPPORTS BENT A3NB-5 3-4-6179 . REMOVED AND REPLACED AFT CARGO FLOOR SUPPORT AT FR54 STR43R-STR4 3L IAW A320 SRM 51-42-11.

Part: SHEAR TIE — CORRODED (FRAME 33) · airframe 78,952 hrs · 30,607 cycles

FWD PIT HAS CORRODED CLEAT AT FR 33 STRG 40R-41R A3NB-53-3-6112 PER HAECO LCQ NON ROUTINE 9293187 GENERATED BY V078632 REMOVED AND REPLACED CLEAT AT FRAME 33 BETWEEN STINGER 40R T STR INGER 41R IAW A320 SM 51-72-11-911-002 PERFORMED BY MECH V892568 MECH V080285 INSP BY LC-04

Part: SHEAR TIE — CORRODED (FRAME 30) · airframe 78,952 hrs · 30,607 cycles

FWD CARGO CLEAT FR30 ST40R-41R HAS CORROSION A3NB-05-3-6013 PER HAECO LCQ NON ROUTINE 9293152 GENERATED BY N078625 REMOVED AND REPLACED CLEAT AT FRAME 30 BETWEEN STRINGER 40R TO S TRINGER 41R IAW A320 SRM 51-72-11-911-002 PERFORMED BY MECH V892 568 MECH V080285 INSP BY LC-04

Part: SHEAR TIE — CORRODED (FRAME 36) · airframe 78,952 hrs · 30,607 cycles

FWD CARGO FR26 STR43L-42L CLEAT HAS CORROSION A3NB-05-3-6013 PER HAECO LCQ NON ROUTINE 9292913 GENERATED BY N078625 REMOVED AND REPLACED CLEAT AT FRAME 26 BETWEEN STRINGER 43L AND 42L IAW A320 SRM 51-72-11-911-002 PERFORMED BY MECH V892568 MECH V080285 INSP BY LC-04

Part: INTERCOSTAL — CORRODED (FRAMES 58-59) · airframe 78,952 hrs · 30,607 cycles

UPON PROFILE PANEL REMOVAL FOUND CORROSION AT INTERCOSTAL TOP SURFACE ALSO INTERCOSTAL WEB BENT FR58-59 STR 38RT AT AFT PIT LOWE R LOBE INNER STRUCTURE. REMOVED & REPLACED THE INTEROSTAL IAW SRM 51 42-11 PARA E(4) &E(2) & SRM 51-72-11-911-001.

Part: INTERCOSTAL — CRACKED (FRAMES 52-53) · airframe 78,952 hrs · 30,607 cycles

AFT PIT FR 53-52 STR 38LT INTERCOSTAL TOP AFT EDGE CRACKED. REMOVED & REPLACED INTERCOSTAL AT FR53-52 STR 38L IAW A320 SRM 5 1-42-11 PARA E & SRM 51-72-11-911-001.

Part: STRINGER SPLICE — CORRODED (FRAME 28-30) · airframe 78,952 hrs · 30,607 cycles

FWD CARGO PIT STRINGER SPLICE 42R BETWEEN FRAMES 28 AND 30 WAS CORRODED. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-72-11-91 1-002 PARA 2.

Part: SHEAR TIE — CORRODED (FRAME 28) · airframe 78,952 hrs · 30,607 cycles

FWD CARGO SHEAR TIE FRAME 28, STRINGERS 41R-40R WAS CORRODED. REMOVED AND REPLACED IAW SRM 51-72-11-911-002, PARA 2.

Part: SHEAR TIE — CORRODED (FRAME 28) · airframe 78,952 hrs · 30,607 cycles

FWD CARGO CLEAT FRAME 28 STRINGERS 42R - 41R WAS CORRODED. REMOVED AND REPLACED THE CLEAT IN THE FWD CARGO BAY IAW SRM 51-72-11-911-001.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 78,952 hrs · 30,607 cycles

FWD PIT CLEAT FRAME 31 STRG 40R-41R IS CORRODED. REMOVED AND REPLACED CLEAT IAW SRM 51-72-11-911-002 PARAGRAP H 2.

Part: CLEAT — CORRODED (FRAME 29) · airframe 78,952 hrs · 30,607 cycles

FWD PIT CLEAT FRAME 29 STRG 38L-39L IS CORRODED A3NB-53-3-6105 P ER HAECO LCQ NON ROUTINE 9293213 GENERATED BY V078632 REMOVED AND REPLACED 1EA CORRODED CLEAT IN THE FWD CARGO COMP AT FR29 STR36L-38L IAW AIRBUS A320 SRM 51-72-11-911-001 PERFORMED BY V914965 MECH V080285 INSP BY LC-10

Part: CLEAT — CORRODED (FRAME 31) · airframe 78,952 hrs · 30,607 cycles

FWD PIT CLEAT FRAME 31 STRG 43L-44L IS CORRODED. REMOVED AND REPLACED 1EA CORRODED CLEAT IN THE FWD CARGO COMP. F R31 STR 43L-44L IAW AIRBUS A320 SRM 51-72-11-911-001.

Part: CLEAT — CORRODED (FRAME 31) · airframe 78,952 hrs · 30,607 cycles

FWD PIT CLEAT FRAME 31 STRG 41R-42R IS CORRODED. REMOVED AND REPLACED 1EA CLEAT @ FWD CARGO FR 31 STRG 41R-42R IA W A320 SRM 51-72-11-002.

Part: CLEAT — CORRODED (FRAME 32) · airframe 78,952 hrs · 30,607 cycles

FWD CARGO FR32 CLEAT ST41R-42R HAS CORROSION. REF HAECO LCQ NR 9 293166. GENERATED BY N078625. REMOVED AND REPLACED 1EA CORRODED CLEAT IN THE FWD CARGO COMP AT FR32 STR 41R-42R IAW AIRBUS A320 SRM 51-72-11-911-002. PERFORME D BY MECH V914965 AND INSP BY N078625. SDR ITEM.

Part: CLEAT — CORRODED (FRAME 30) · airframe 78,952 hrs · 30,607 cycles

FWD CARGO CLEAT FR30 ST44L-43L HAS CORROSION. REF HAECO LCQ NR 9 293156. GENERATED BY N078625 REMOVED AND REPLACED 1EA CORRODED CLEAT @ FWD CARGO FR30 STR. 44 L-43L IAW A320 SRM 51-72-11-911-002.

Part: CLEAT — CORRODED (FRAME 32) · airframe 78,952 hrs · 30,607 cycles

FWD CARGO FR32 CLEAT ST43R-42R HAS CORROSION. REMOVED AND REPLACED 1EA CORRODED CLEAT AT FR32 STR 42R-43R IAW AIRBUS A320 SRM 51-72-11-911-002.

Part: CLEAT — CORRODED (FRAME 33) · airframe 78,952 hrs · 30,607 cycles

FWD PIT HAS CORRODED CLEAT AT FR 33 STRG 41R-42R. REF HAECO LCQ NR 9293188. GENERATED BY V078632. REMOVED AND REPLACED 1EA CORRODED CLEAT @ FWD CARGO FR33 STR 41R -42R IAW A320 SRM 51-72-11-911-002.

Part: CARGO TRACK — CORRODED (FRAME 30) · airframe 78,952 hrs · 30,607 cycles

FWD CARGO CLEAT FR30 ST42R-43R HAS CORROSION A3NB-05-3-6013 PER HAECO LCQ NON ROUTINE 9293154 GENERATED BY N078625 REMOVED AND REPLACED CLEAT TO FORWARD CARGO AT FR30 BETWEEN STR 42R-43R IAW SRM 51-72-11-911-002 BY MECH V080285 INSP BY N078625 PER HANGAR NR 9293154 AT HAECO LCQ HMV VISIT.

Part: CARGO FITTING — CORRODED (FRAME 32) · airframe 78,952 hrs · 30,607 cycles

FWD PIT CLEAT FRAME 32 STRG 42L-43L IS CORRODED A3NB-53-3-6105 P ER HAECO LCQ NON ROUTINE 9293214 AND GENERATED BY V078632 REMOVED AND REPLACED CLEAT IN FORWARD CARGO AT FRAME 32 STR42L-4 3L IAW SRM 51-72-11-911-002 BY MECH V080285 INSP BY N075625 PER HANGAR NR 9293214 AT HAECO LCQ HMV VISIT.

Part: CARGO TRACK — CORRODED (FRAME 33) · airframe 78,952 hrs · 30,607 cycles

FWD PIT HAS CORRODED CLEAT AT FR 33 STRG 42R-43R A3NB-53-3-6112 PER HAECO LCQ NON ROUTINE 9293189 GENERATED BY V078632 REMOVED AND REPLACED CLEAT IN FORWARD CARGO AT FRAME 33 BETWEEN STRINGER 42R-43R IAW SRM 51-72-11-911-001 BY MECHV08285 INSP BY N078625 PER HANGAR NR9293189 AT HAECO LCQ HMV VISIT.

Part: CLEAT — CORRODED (FRAME 26) · airframe 78,952 hrs · 30,607 cycles

FWD CARGO FR26 ST43R-42R CLEAT HAS CORROSION. REF HAECO LCQ NR 9 292912 GENERATED BY N078625 REMOVED AND REPLACED FWD CARGO CLEAT AT FRAME 26 BETWEEN STR 42R STR 43R IAW A320 SRM 51-72-11-911-002 PARA 2.

Part: CLEAT — CORRODED (FRAME 29) · airframe 78,952 hrs · 30,607 cycles

FWD CARGO FR29 ST41L-42L CLEAT HAS CORROSION REF HAECO 9292920 G ENERATED N078625 REMOVED AND REPLACED FWD CARGO CLEAT AT FRAME 29 BETWEEN 41L TO STR 42L IAW A320 SRM 51-72-11-911-002 PARA 2.

Part: SKIN — CORRODED (FRAME 69) · airframe 78,952 hrs · 30,607 cycles

LAV EXHAUST VENT AFT FASTENER HOLE AT FUSELAGE EXTERIOR SKIN EXI STING DOUBLER HAS CORROSION FR 69 EA5100-02750 002 PER HAECO LCQ NON ROUTINE 9292341 GENERATED BY V061623 REMOVED AND REPLACED LAV EXHAUST VENT DOUBLER IAW A320 SRM53-41- 11-300-004 PERFORMED BY MECH V915153 INSP BY LC-10

Part: FITTING — CORRODED (FRAME 68) · airframe 78,952 hrs · 30,607 cycles

LH CABIN L2 DOOR SILL AFT CORNER FITTING HAS CORROSION AT STR23L FR68 SPEC NO. A3NB-53-3-6222 GEN BY V077960 PER HANGAR NR 929255 7 AT HAECO LCQ HMV VISIT. REMOVED AND REPLACED L2 DOOR SILL LH CABIN AFT CORNER FITTING ST R23L FR63 IAW SRM 51-42-11 BY MECH V914232 INSP BY LC-10 PER HAN GAR NR 9292557 AT HAECO LCQ HMV VISIT.

Part: FITTING — CORRODED (L2 DOOR GIRT BAR) · airframe 78,952 hrs · 30,607 cycles

AFT LH CABIN L2 DOOR SILL HAS CORROSION AROUND FASTENER HOLE AT FWD AND AFT GIRT BAR FITTING PER HANGAR NR 9292559 GEN BY V07796 0 AT HAECO LCQ HMV VISIT. REMOVED AND REPLACED AFT LH CABIN L2 DOOR SILL FR66-FR68 IAW SRM 51-42-11-001 AND SRM 51-72-11-911-001 BY MECH V914232 INSP BY LC-10 PER HANGAR NR 9292559 AT HAECO LCQ HMV VISIT.

Part: FITTING — CORRODED (FRAME 66) · airframe 78,952 hrs · 30,607 cycles

AFT LH CABIN L2 DOOR SILL FWD CORNER FITTING HAS CORROSION AT ST R 23L FR66 SPEC NO A3NB-3-6222 GEN BY V077960 PER HANGAR NR 9292 561 AT HAECO LCQ HMV VISIT. REMOVED AND REPLACED LH CABIN L2 DOOR SILL FWD CORNER FITTING ST R23L FR66 IAW SRM 51-42-11-001 BY MECH V904232 INSP BY LC-10 PER HANGAR NR 9292561 AT HAECO LCQ HMV VISIT.

Part: SUPPORT — CORRODED (STRINGER 23L) · airframe 78,952 hrs · 30,607 cycles

AFT L/H CABIN AFT LATERAL SHEAR WEB SUPPORT AT STR 23L HAS CORROSION ON UNDERSIDE AROUND DRAIN HOLE A3NB-53-3-6222. REMOVED AND REPLACED LH AFT SHEAR WEB SUPPORT IAW SRM 51-72 -11-911-00.

Part: FITTING — CORRODED (R2 DOOR FRAME) · airframe 78,952 hrs · 30,607 cycles

R2 DOOR SILL AFT CORNER FITTING HAS CORROSION. REMOVED AND REPLACED R2 DOOR SILL AFT CORNER FITTING FR68 RH SIDE IAW A320 SRM 51-72-11-911-001 PG 2 PAR 3, 4 SRM 51-42-11-001 P G 6 PAR E PG 7, 17, 18.

Part: DOOR SILL — CORRODED (R2 DOOR) · airframe 78,952 hrs · 30,607 cycles

R-2 DOOR SILL HAS CORROSION AROUND AFT NUTPLATE HOLES 2EA JUST F WD OF FR 68 PER HAECO LCQ NR 9292539. REMOVED AND REPLACED R2 DOOR SILL RH SIDE FR 66-68 IAW A320 SRM 51-72-11-911-001 PG 2 PAR 3 AND 4 SRM 51-42-11-001 PG 6 PAR E PG 7, 17, 18.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 78,467 hrs · 30,388 cycles

EMERGENCY LIGHT TEST FOR NR 2 SERVICE FAILS TEST WITH AFT LEFT UNIT FAULTIN. AFT CURTAIN ROD AND AFT PANEL AT DOOR 2 LT IS REMOVED FOR ACCESS REPLACED 13WL EXIT POWER UNIT...NO FAULTS...INSTALLED CURTAIN ROD ASSY AND CEILING PANEL ROTABLE PARTS CHANGE WAS INDICATED - TT # 1211891 SN OFF 4893 POWER SUPPLY, C OFF 31-3350-9-9001 4893 ON 31-3350-9-9001 8316.

Part: SLIDE — FAULTED (L1 DOOR) · airframe 74,582 hrs · 28,574 cycles

EPSU EXT LOAD FWD L (ATA 33-51-38) FAULT DURING TEST OF EMERGENCY LIGHTS OPERATIONAL CHECK (REF NR 2 SERVICE). REPLACED SLIDE /RAFT REF AMM 25-62-44-400-006A.

Part: BATTERY — DISCHARGED (CABIN) · airframe 74,520 hrs · 28,541 cycles

DOOR 1 LEFT EMERGENCY LIGHT CIDS MSG ON SIDS PANEL. R&R EMERGENCY BATTERY AND CONTROLLER.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 74,501 hrs · 28,532 cycles

WHEN PERFORMING EMERGENCY LIGHT CK FOR 2 SERVICE GOT MESSAGE EPSU FWD L. REPLACED ESPU AND BATTERY IN FWD POSITION REF 33-51-38 AMM. OPS CK GOOD.

Part: SLIDE — NO TEST (L1 DOOR LIGHT) · airframe 73,813 hrs · 28,227 cycles

EMERGENCY LIGHT TEST FAILED EXT LOAD FWD L. REMOVED AND REPLACED FWD LT SLIDE PACK ASSY IAW AMM 25-62-44-400 -006-A OPS PASSED

Part: CONNECTOR — FAILED (POSITION SENSOR) · airframe 73,398 hrs · 28,048 cycles

SMOKE ODOR IN AFT CABIN AROUND ROW 31 DURING TAKEOFF. REOCCURED DURING CRUISE. FOUND LANDING GEAR POSITION SENSOR AND CONNECTOR FAILED, GIVING FALSE INDICATION. ACFT WAS IN FLIGHT MODE WHICH LED TO EQUIPMENT COOLING DOORS TO REMAIN CLOSED DURING GROUND OPERATION WHICH POSSIBLY LED TO THE LT ELECTRICAL CIRCUIT BREAKER TRIP. PERFORMED AMM TASK 05-51-10-10 -200-801C1 NO ODOR PRESENT. OK TO CONTINUE.

Part: CIRCUIT BREAKER — TRIPPED (ESS BUSS) · airframe 73,398 hrs · 28,048 cycles

DC ESS BUSS SHED AT ROTATION. CIRCUIT BREAKER TRIPPED, LT ELEC BAY. EMERGENCY DECLARED. TROUBLESHOT IAW TSM 24-60-810-810A, IAW AMM 20-16-11, FOUND THE CIRCUIT BREAKER 1PH ON 10 6VU TRIPPED. RESET SAME TESTED ESS BUSS WITH NO FAULTS. OK FOR SERVICE.

Part: BATTERY — FAILED (CABIN) · airframe 72,276 hrs · 27,556 cycles

EMERGENCY EXIT LIGHT BATTERY 10WL FAILS CAPACITY CHECK. REPLACED BATTERY REF AMM 33-51-00-710-001-A01. OPS CHECKED OK

Part: BATTERY — FAILED (CABIN) · airframe 72,276 hrs · 27,556 cycles

EMERGENCY EXIT LIGHT BATTERY PACK 12WL FAILED CAPACITY CHECK. REPLACED BATTERY PACK 12WL REF AMM 33-51-00-710-001-01A. OPS CHECKED OK.L

Part: EPSU — INOPERATIVE (CABIN) · airframe 71,785 hrs · 27,327 cycles

AFT LEFT EMERG LIGHT FAILED. REPLACED AFT L EPSU.

Part: SWITCH — STICKING (EMERGENCY LIGHT) · airframe 71,335 hrs · 27,117 cycles

AFT ATTENDANT EMERGENCY LIGHT TEST SWITCH STICKS IN ON POSITION. REPLACED THE PANEL, GROUND TESTED, NO DEFECTS.

Part: CONTROL PANEL — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 71,335 hrs · 27,117 cycles

AFT ATTENDANT EMERGENCY LIGHT TEST SWITCH STICKS IN ON POSITION. REPLACED THE CONTROL PANEL . GROUND TEST OK, NO DEFECT NOTED IAW 23-00-00.

Part: LIGHT — INOPERATIVE (L1 DOOR SLIDE) · airframe 71,335 hrs · 27,117 cycles

EMERGENCY LIGHT TEST FAILED. REPLACED L1 SLIDE.

Part: SLIDE — FAULTED (L1 DOOR) · airframe 69,805 hrs · 26,436 cycles

EMERGENCY LIGHTS OPERATIONAL TEST FAILED SHOWING FAULT, EXT LOADS FWD L. REPLACED DOOR SLIDE AT 1L IAW AM 25-62-44-400-006. OPERATIONS CHECKED GOOD.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,321 hrs · 26,217 cycles

AFT CARGO STRINGER 41R, FRAME 58 - 63 SHOWS SIGNS OF CORROSION. R & R STRINGER 41R, FRAME 58 - 63 IN AFT CARGO. REMOVED & REINSTALLED CLEATS & FWD SPLICE FROM FRAME 58 - 63 IN AFT CARGO IAW SRM 51-42-11 PG 7 & P G 25 PARA 7 & SRM 51-42-11 PG 1 - 2 STEP 6 A.

Part: SLIDE — DEFECTIVE (CABIN) · airframe 68,859 hrs · 26,019 cycles

CABIN EMER LIGHT TEST FAILED. REPLACED FWD LT SLIDE, NO HELP. REPLACED RT FWD SLIDE, MSG CLEARED IAW AMM 25-62-44. DOOR ASSIST ACTUATORS REAMED.

Part: SLIDE — FAULTY (L1 DOOR) · airframe 67,745 hrs · 25,557 cycles

EXT LOADS FWD L, FAULT WHEN PERFORMING EMER LIGHTS TEST. REPLACED NR 1 LT EXIT DOOR SLIDE IAW AMM TASK 25-62-44-400-006-A. OPERATIONS CHECKED GOOD.

Part: SLIDE — DEFECTIVE (R1 DOOR) · airframe 66,998 hrs · 25,248 cycles

EMERGENCY LIGHTS OPERATIONAL TEST DOES NOT PASS DURING 2 SERVICE CHECK. MESSAGE ATA 33-51-38 EXT LOADS FWD LT. TRIED NEW EPSU, NO HELP IAW TSM31-51-00-810-808A. REPLACED DOOR 1R SLIDE ASSEMBLY IAW AMM-25-62-44-400-006-A. PERFORMED EMER LIGHT TEST, SYS OPERATED NORMALLY.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 66,534 hrs · 25,072 cycles

PACK 1 REG FAULT DISPLAYED ON UPPER ECAM SCREEN. DURING INITIAL CLIMB SYS APPEARED NORMAL. FAULT FOR NR 1 PACK NO LONGER DISPLAYED. NR 1 PACK RAM AIR DOOR CYCLES WITH PACKS ON.

Part: BATTERY — FAILED (CABIN) · airframe 66,131 hrs · 24,907 cycles

EMERGENCY TEST FAILS AT 2 SERVICE, FAILS EMER LT BATTERY. REPLACED LT BATTERY AT SEAT 21A IAW AMM 33-51-38. OPERATIONS CHECKED GOOD.

Part: BATTERY — FAULTED (CABIN) · airframe 65,656 hrs · 24,713 cycles

EXT LOADS FWD LT & BATTERY EMER LT FAULTS WHEN PERFORMING EMER LIGHTS TEST. AFTER RESETTING BREAKERS ONLY GETTING EXT LOAD FWD LT FAULT TRIED NEW POWER SUPPLY, NO HELP. REINSTALLED ORIGINAL, FAULT CLEARS WHEN SLIDE AT DOOR 1L CONNECTOR IS TESTED WITH TEST LAMP.

Part: SLIDE — FAULTED (R1 DOOR) · airframe 65,473 hrs · 24,637 cycles

EPSU 10WL DOOR 1R FAILED WITH EXTERIOR LIGHTS FAULT. REPLACED SLIDE ASSEMBLY DUE TO EXTERNAL LOAD FAULT DOOR 1R IAW 25-62-44.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 64,476 hrs · 24,247 cycles

CREW REPORTS 02 MASKS FELL AT ROW 12ABC. REPACK MASK ON ROW 12ABC IAW AMM 35-21-43 & CHECK 02 GEN AMM 35-21-42 DROP TEST ACP ON TASK CARD 4R3590171 SEQ 546.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 64,448 hrs · 24,237 cycles

CREW REPORTS 02 MASKS FELL AT ROW 12ABC. STOWED MASKS IAW MT 35- 003, DROP TEST TO BE COMPLIED WITH WITHIN 3 DAYS.

Part: MICROPHONE — INOPERATIVE (COCKPIT) · airframe 63,591 hrs · 23,912 cycles

HAND MICROPHONE 1 INOPERATIVE. REPLACED CAPTAIN`S HAND MIC, OPERATION CHECKED OKAY.

Part: CONNECTOR — LOOSE (SMOKE DETECTOR) · airframe 63,538 hrs · 23,894 cycles

FLIGHT ATTENDANT`S CIDS PANEL CAUTION ON. FOUND LAVATORY SMOKE SYSTEM FAULT. SECURED LOOSE CONNECTOR 7200VC BEHIND FWD LAVATORY A IAW WD 25-41-01. LAVATORY SMOKE SYS CHECKED OK IAW AMM TK 26-17-00-710-001 & 26-16-00-710-001.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 63,538 hrs · 23,894 cycles

IAW LOG 2 CIDS CAUTION LIGHT ON. FOUND SYS STATUS SHOWING LAVATORY SMOKE SYS FAIL WITH NO SDCU 1 & 2 DATA. REPLACED SDCU, NO HELP. REINSTALLED ORIGINAL UNIT. TROUBLESHOOTING DATA FAULTING FWD LAVATORY DETECTOR IAW MT 26-002.

Part: UNKNOWN — MALFUNCTIONED (SMOKE WARNING) · airframe 63,532 hrs · 23,893 cycles

AFT CARGO SMOKE TEST FAILED.

Part: HYDRAULIC LINE — LEAKING (CARGO BAY) · airframe 63,229 hrs · 23,773 cycles

HYD FLUID DRIPPING FROM AFT CARGO PIT CEILING, FWD END RT SIDE. YELLOW & GREEN SYSTEM RESERVOIRS AT REFILL. FOUND YELLOW SYS HYD LINE LEAKING JUST BELOW T FITTING IAW IPC 52-36-04-02C LINE-ITEM 170, PCN110-2740-PN-D291709020600. REPLACED SECTION OF LINE & SPLICED IAW GNMM1-0-13-028, OPERATED AFT CARGO DOOR SEVERAL TIMES, NO LEAKS.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 63,016 hrs · 23,698 cycles

PASSENGER SEAT OVERHEAD 02 MASK FELL AT 24ABC. PERFORMED MT 35-003 ALL PARTS LOOK NORMAL NEEDS MASK DROP TEST.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 63,006 hrs · 23,692 cycles

AFT LT EMERGENCY LIGHT BATTERY FAILED TEST. R & R EMERGENCY POWER SUPPLY BATTERY FOR 13-WL EPSU IAW AMM 33-51-38.

Part: ANTI-ICE SYSTEM — INOPERATIVE (COCKPIT) · airframe 62,955 hrs · 23,673 cycles

CAPTAIN'S SLIDING WINDOWS HEAT INOPERATIVE.

Part: FLUID — LEAKING · airframe 62,600 hrs · 23,537 cycles

CLEANED UP RED FLUID OFF THE BELLY FROM THE AFT CARGO DOOR TO THE REAR OF THE AIRCRAFT. FOUND RED-FLUID UNDER THS ACTUATOR, FLUID IS LEAKING OUT ACCESS PANEL BOTTOM OF TAIL & RUNNING FORWARD. CLEANED OFF RED FLUID FOUND NO LEAK OR TROUBLE. AUDIO CONTROL PANEL SERVICED & LEAK CHECKED.

Part: DEU — INOPERATIVE (CABIN) · airframe 62,573 hrs · 23,524 cycles

BOTH COCKPIT AND FORWARD F/A ARE UNABLE TO TALK TO F/A IN AFT OF ACFT VIA INTERCOM. AFT HANDSET INOPERATIVE, R & R DEU B POSITION 300-RH-1. DISCOUNTED ALL CONNECTORS AT AFT FA SEAT ASSY, RECONNECTED, OPS CHECKED NORMAL OF AFT AND FWD HANDSETS.

Part: BEARING — CRACKED (AFT CARGO DOOR) · airframe 62,452 hrs · 23,477 cycles

AT ARRIVAL FOUND AFT CARGO DOOR DAMAGED AT AND AROUND DOOR OPEN LEVER AND WAS UNABLE TO OPEN DOOR. FOUND BEARING ASSY CRACKED ITEM 140 IPC 52-32-21-03 ON AFT CARGO HANDLE ASSY. INSTALLED STOP SCREWS IN NEW HANDLE ASSY. BLENDED DENTED AREA TO REMOVE STRESS RISERS. ACCOMPLISHED HFEC. NO CRACK INDICATIONS NOTED.

Part: COMPUTER — FAILED (WINDSHIELD HEAT) · airframe 62,418 hrs · 23,461 cycles

RIGHT WINDSHIELD ANTI-ICE DISPLAYED ON UPPER ECAM SCREEN. LAST LEG REPORT SHOWS RT WINDSHIELD SENSOR. RT WINDOW HEAT COMPUTER IAW TSM 30-42-00. OPS NORMAL.

Part: SWITCH — MISSING (RADIO) · airframe 61,276 hrs · 23,009 cycles

COVER ON FIRST OFFICERS SIDE STICK RADIO SWITCH MISSING. REPLACE HANDGRIP PER MAINT TIP 23-012. INSTALLED NEW COVER.

Part: SERVO — FAULTED (LT AILERON) · airframe 60,954 hrs · 22,872 cycles

AILERON DAMPING TEST DOES NOT PASS TEST EFCS NR 1 & 2 IN DOWN FACTOR IN THE LEFT AILERON. REPLACED LEFT AILERON SERVO IAW AMM. PERFORMED OPERATIONAL & DAMPING TEST OF SERVO'S WORKS OK, ACFT RETURNED TO SERVICE.

Part: NUT — STRIPPED (COCKPIT DOOR) · airframe 60,255 hrs · 22,601 cycles

COCKPIT DOOR HARD TO LATCH. FOUND DOOR ADJUSTMENT NUT STRIPPED PREVENTING PROPER DOOR ADJUSTMENT. REPLACE WORN NUT AND ACCOMPLISHED ADJUSTMENT AND TEST OF DOOR PER AMM.

Part: DOOR — MISSING (COCKPIT) · airframe 60,173 hrs · 22,565 cycles

LEFT VEST DOOR FOR 2ND OBSERVER IN THE FLIGHT DECK IS MISSING. SEAT IS INOP, SHOULD HAVE COVER AND VEST. AC NOT ON COA LIST, NEED COVER AND VEST.

Part: OXYGEN BOTTLE — UNKNOWN (CREW O2) · airframe 60,139 hrs · 22,552 cycles

OXYGEN PRESSURE WENT FROM 870 TO 820 PSI OVER 2 1/2 HOURS WITH NO USE. SERVICED CREW O2 BOTTLE. OPS CHECKED GOOD, NO LEAKS NOTED.

Part: REGULATOR — LEAKING (COCKPIT) · airframe 60,135 hrs · 22,551 cycles

CREW OXYGEN SYSTEM LOW. FOUND FIRST OBSERVERS O2 REGULATOR LEAKING. BOX AND CRUSH GASKET HAVE BEEN REPLACED WITH NO LEAKS.

Part: HANDLE — UNSECURE (AFT CARGO DOOR) · airframe 59,829 hrs · 22,426 cycles

CARGO DOOR OPEN EICAS, RTFL. FOUND AFT CARGO DOOR NOT RECESSED AND FAIRED WITH CARGO DOOR SKIN. HANDLE WAS STICKING OUT THREE QUARTERS OF AN INCH. CYCLED DOOR AND SECURED DOOR HANDLE RECESSED FLUSHED TO DOOR SKIN. DOOR HANDLE FLAP DOES ENGAGE AND LOCKS HANDLE IN PLACE.

Part: CONTROL PANEL — FAULTY (FIRE WARNING) · airframe 59,572 hrs · 22,322 cycles

FOUND ENGINE AND APU FIRE PANEL 1WD CAUSE OF DISCHARGE LEGEND OF ENGINE 2 AGENT 1 INSTALLED PANEL PER AMM. NEED TO OP CHECK PER AMM(S) 26-22-00-710-004 26-22-00-710-001 26-12 -00-710-001, 26-21-00-720-001 & 26-21-00-720-005. OPS CHECKED GOOD. ENG 2 PANEL 1WD AND SQUIB 6WE2 REPLACED, OPS TEST GOOD.

Part: INDICATOR — STUCK (COCKPIT) · airframe 59,523 hrs · 22,299 cycles

PACK MAINT STS CLASS II MESSAGE DISPLAYED ON LOWER ECAM. PREV LEGS REPORTS SHOWS 21-51-51 'P1 FLOW CONT VALVE' 11HB MSG 7 TIMES IN THE LAST FEW DAYS. TROUBLESHOT IAW TSM 21-51-00-810-803-A, PERFORMED OP'S TEST OF PACK TEMP CONT SYSTEM IAW AMM 21-61-00-710-001, TEST PASSED. PERFORMED OPS TEST OF FLOW CONT & IND IAW AMM 21-51-00-710-002, PACK 1 FLOW INDICATOR APPEARS STUCK IN THE LO POS, WILL NOT MOVE AT ALL. LONG HISTORY OF THIS PROBLEM, INCLUDING MULTIPLE CHORNICS.

Part: BRACKET — BROKEN (COCKPIT) · airframe 59,469 hrs · 22,275 cycles

COCKPIT CRASH AXE INBOARD SADDLE CLIP-BRACKET BROKEN AND SECURING STRAP MISSING. REPLACED CLIP AND STRAP.

Part: OXYGEN MASK — NO TEST (SEAT 3 EF) · airframe 59,443 hrs · 22,263 cycles

DURING OXYGEN MASK MANUAL RELEASE CHECK, MASKS SEATS 3E AND F DID NOT DROP. REPACKED OXYGEN MASK ASSY AND OPS CHECKED MANUAL MASK RELEASE, OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,319 hrs · 22,206 cycles

EMERGENCY LIGHT TEST INDICATES 'BATTERY AFT LT'. REPLACED BATTERY PACK AND OPS CHECKED GOOD.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 59,319 hrs · 22,206 cycles

PAX SIDE AISLE EMERGENCY LIGHT LENS BROKEN. REPLACED EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 59,211 hrs · 22,159 cycles

TWO BROKEN WIRES ON WALL AFT OF DOOR 2R, EXIT LIGHT IDENTIFIER. REPAIRED WIRES PER ESPM 20-53-21, TYPE 1 REPAIR. OPS CHECKED NORMAL REF MM33-51 -00-710-002-C.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 59,211 hrs · 22,159 cycles

LT WHEEL WELL KEELBEAM SUPPORT ANGLE FOR FUSELAGE FAIRING IS CRACKED JUST AFT OF AFT DOOR HINGE AT FRAME 46.

Part: STRINGER — CORRODED (CARGO BAY) · corrosion level 2 · airframe 59,211 hrs · 22,159 cycles

AFT CARGO BAY STRINGER 31R IS CORRODED BETWEEN FR 64 AND 66. REPLACED STRINGER SECTION PER SRM.

Part: SUPPORT — CRACKED (RT MLG WW) · airframe 59,211 hrs · 22,159 cycles

RT WHEEL WELL KEELBEAM SUPPORT ANGLE FOR FUSELAGE FAIRING IS CRACKED JUST AFT OF AFT DOOR HINGE AT FRAME 46.

Part: SEAL — WORN (FAIRING) · airframe 58,754 hrs · 21,984 cycles

AIRFRAME VIBRATION, FL200 UP TO FL340, MORE NOTICEABLE IN CLIMB THAN LEVEL FLT. ACCOMPLISHED TSM CHART 05-50-00 PB201 AND INFORMATION FROM VIBRATION SURVEY SUGGESTS BELLY FAIRING SOURCE OF VIBRATION. TAPED BELLY FAIRING SEALS REF MT53-004. FOUND SEAL WORN ON PANEL 197BB REPLACED SEAL.

Part: SENSOR — FAULTY (PAX DOOR) · airframe 58,324 hrs · 21,802 cycles

ECAM IN FLIGHT. DOOR R AFT CABIN. LASTED 1 MINUTE. DOORS PAGE SHOWED OPEN. REPEAT GRIPE. REPLACED SENSOR 17WV2 & ADJUSTED PER MM, CHECKED GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (ROW 36) · airframe 58,212 hrs · 21,753 cycles

CREW REPORTED O2 MASK DEPLOYED AT ROW 36 DEF. STOWED MASK LATCH AND CLOSED NORMAL. ACCOMPLISHED 02 MASK DROP CHECK. IAW AMM.

Part: SEAT — DETACHED (CABIN) · airframe 58,097 hrs · 21,696 cycles

ROW 36 ABC DETACHED FROM FLOOR. SECURED SEAT ROW.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 58,058 hrs · 21,675 cycles

FLOOR SOFT IN AISLE BETWEEN ROW 35 & 36 BY FLIGHT ATTENDANT. AREA MEASURES 18' X 18' BETWEEN FRAME 61 AND 62. REPLACED CABIN FLOOR PANEL.

Part: SEAT — DEFECTIVE (COCKPIT) · airframe 57,613 hrs · 21,481 cycles

FIRST OFFICER SEAT, MANUAL HORIZONTAL ADJUSTMENT DEFECTIVE. REPLACED SEAT ASSY.

Part: PINION — FAILED (RUDDER PEDALS) · airframe 57,562 hrs · 21,461 cycles

CAPTAIN'S RUDDER PEDAL ADJUSTMENT INOPERATIVE. PEDALS DO NOT SPRING BACK FROM FULL FWD POS WITH HANDLE. REPLACED THE AIR PINTON, OPS CHECKED GOOD.

Part: FIRE WARNING — FALSE INDICATION (CARGO BAY) · airframe 57,284 hrs · 21,353 cycles

AT GATE HAD A FALSE INDICATION OF A AFT CARGO FIRE. CYCLED BREAKERS. BITE TESTED PER AMM. TESTED OKAY.

Part: ENGINE — VIBRATION (NR 2) · airframe 57,166 hrs · 21,299 cycles

CREW REPORT: NOTICEABLE LOUD ROAR AND VIBRATION ON NR 2 ENGINE THROUGHOUT FLIGHT SAMC TEXT: PER CREW. HIGHEST VIBRATION NR 2 ENGINE WAS 2.0. THROTTLES BROUGHT TO IDLE, VIBS DECREASED. FELT ON FLOOR. FBO TO ACCOMPLISH INLET AND EXHAUST CHECK PER MT 72-021 AND MCD CHECK PER A MM79-22-45 PG 601. REPORT FINDINGS TO SAMC-EMC. ACP'D A VISUAL FOD INSP OF NR 2 ENG PER MT72-021. NO DEFECTS NOTED. CHECKED ALL 5 CHIP DETECTORS REF MM 79-22-45. CD'S CLEAN. INSTALLED NEW PACKINGS AND INSTALLED CD'S.

Part: TOILET — DEFECTIVE (LAVATORY) · airframe 57,132 hrs · 21,281 cycles

LAVATORY TOILET BOWL OVERFLOWING AT AFT CABIN LT FWD LAV. INOP AFT FWD LAV. REPLACED AFT-FWD TOILET, OPS CHECK OK.

Part: SLIDE — FAULTY (L1 DOOR) · airframe 56,770 hrs · 21,118 cycles

EXT LOADS FWD L' FAULT WHEN PERFORMING EMERGENCY LIGHTS TEST. ORDERED SLIDE TO TROUBLESHOOT THE FAULTY SLIDE. NOT ABLE TO TROUBLESHOOT DUE TO WORK ON RT FWD DOOR. SLIDE IS IN LSR DROP. T/S EMG LIGHT TEST. DUAL SLIDE LIGHT FAILURES DOOR 1R AND 1L.

Part: LANYARD — DISLODGED (ESCAPE SLIDE) · airframe 55,944 hrs · 20,746 cycles

A CORD IS HANGING DOWN FROM SLIDE PACK AT DOOR 1R. RESTOWED CORD IN SLIDE PACK.

Part: LIGHT — NO TEST (L1 DOOR SLIDE) · airframe 55,226 hrs · 20,433 cycles

EMERGENCY LIGHT TEST FAILED MESSAGE EXT LOADS FWD L. TROUBLESHOT PER TSM. CONNECTED TESTING TOOL AT DOOR 1L TEST PASSED.

Part: B-NUT — LEAKING (FUEL LINE) · airframe 55,226 hrs · 20,433 cycles

UPON REMOVING OIL CAP TO SERVICE NR 2 ENG OIL FOUND VERY STRONG FUEL SMELL COMING FROM OIL TANK. ACP'D INSPECTION AND CHECK OF FUEL OIL COOLER, NO PROBLEMS NOTED. FOUND MAIN FUEL SUPPLY LINE B-NUT WITH SMALL SEEPAGE. TIGHTENED B-NUT AND IDLE LEAK CHECKED GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 18 DEF) · airframe 55,069 hrs · 20,362 cycles

OXYGEN MASKS DROPPED AT 18DEF. REPACKED MASKS PER AMM, DROP CHECK PER MM, OPS CHECK GOOD.

Part: WIRE — OUT OF POSITION (CABIN) · airframe 55,051 hrs · 20,354 cycles

CABIN EMERG LIGHTING CHECK RESULT SHOWED ATA 33-51-38 INT LOADS EMER L. FOUND EXT AND INT LIGHTS FLASHING ON 11W EPSU. TRIED NEW BATTERY AND EPSU NO HELP. 11W DISCONNECTED FROM AIRCRAFT. REPLACED EPSU 11W AND BATTERY PACK, NO HELP. FOUND WIRES BELOW SEAT ROW 15 UNDER SEAT TRACK. REPOSITIONED WIRES. CABIN EMERGENCY LIGHT TESTS NORMAL.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 55,000 hrs · 20,319 cycles

CABIN EMERGENCY LIGHT TEST FAILED ON 3 SERVICE. REPLACED POWER SUPPLY 110W L2. CABIN EMERGENCY LIGHT TEST PASSED, OPS CHECKED NORMAL.

Part: SLIDE — FAULTY (POS 1) · airframe 54,451 hrs · 20,052 cycles

EMERGENCY LIGHT TEST FAILS WITH "EXT LOADS FWD L" MESSAGE. INSTALLED TEST LIGHT FIXTURES ON BOTH FWD SLIDES TO GET TEST TO PASS. FWD EMERGENCY LIGHT POWER SUPPLY AND BATTERY REPLACED (PN 3214, SN 390), NO HELP. REPLACED SLIDES. OPS CHECKED NORMAL.

Part: WIRE — TRANSPOSED (WARNING LIGHT) · airframe 54,135 hrs · 19,916 cycles

NO SMOKING SIGN BURNED OUT OVER AFT FLT ATTENDANT JUMP SEAT. RELAMPED, NO HELP. FOUND WIRES TO TERMINALS 2 AND 3 TRANSPOSED. SWAPPED WIRES AND LIGHT CHECKS GOOD IN PROPER SEQUENCE.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 53,887 hrs · 19,794 cycles

LEFT MID EMERGENCY LIGHT BATTERY FAILS SELF TEST. REPLACED BATTERY, ALL SYS CHECKED OK.

Part: SLIDE — NO TEST (R1 DOOR) · airframe 53,124 hrs · 19,423 cycles

FAILS PTP TEST. FWD LT LOAD. CHANGED RT SLIDE. REPLACED RT FWD DOOR ESCAPE SLIDE. OPS ARE NORMAL.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 52,669 hrs · 19,223 cycles

LOST BLUE HYD SYSTEM ON DESCENT. DIVERSION FOR ADDITIONAL RUNWAY LENGTH. REPLACED HP FILTER & BLUE SYS ELECTRIC PUMP. OPS ARE GOOD.

Part: SLIDE — FAULTY (POSITION 1R) · airframe 52,140 hrs · 18,995 cycles

EXT LOADS FWD L MESSAGE ON CIDS PANEL AFTER EMERGENCY LIGHT TEST. T/S DETERMINED THAT SLIDE AT 1R IS CAUSING MSG. REPLACED 1R DOOR SLIDE. INSP SLIDE AT DOOR 1R, SLIDE SECURED ON DOOR, SLIDE PIN REMOVED AND STOWED, ASSIST BOTTLE REARMED AND SAFETIED, EMERG LIGHT TEST OK. ACFT RETURNED TO NORMAL.

Part: SLIDE — NO TEST (R1 DOOR) · airframe 51,426 hrs · 18,648 cycles

FOUND 1 RT MED SLIDE WOULD NOT PASS EMERGENCY LIGHT TEST. REMOVED AND REPLACED NR1 RT MED SLIDE ASSY, EMERGENCY LIGHTS CHK GOOD.

Part: THERMOSTAT — FAULTY (NR 1) · airframe 50,952 hrs · 18,417 cycles

BLEED AIR LOSS, FLT DIVERTED. RE-ACTIVATED NR 2 ENG PRV AND DE-ACTIVATED HP VALVE. REPLACED NR 1 ENG FAN AIR VALVE CONTROL THERMOSTAT. REPLACED SOLENOID. BLEED CHECK COMPLETED ALL RUNS COMPLETED SATISFACTORY. ACCOMPLISHED HEALTH CHECK FROM PAGE 1 TO 14 ALL CHECKS PASSED. ACCOMPLISHED ENG RUN OF NR 1 & NR 2 ENGS, RAN BOTH PACKS USING 1 ENG AT A TIME. PACKS OPERATED NORMAL, NO FLUX OR ABNORMALITIES NOTED.

Part: SLIDE — FAULTY (R1 DOOR) · airframe 50,943 hrs · 18,409 cycles

EMERGENCY LIGHT TEST FAIL TEST, MSG EXT LOAD FWD LEFT, BATTERY FWD LEFT, BATTERY AFT LEFT. REPLACED LEFT FWD EPSU BATTERY PACK AND LEFT AFT EPSU BATTERY PACK AND CLEARED THE BATTERY MSG'S. FOUND SLIDE AT DOOR 1R BAD FOR "EXT LOAD FWD LEFT" FAULT. NEEDS A SLIDE AT DOOR 1R. REPLACED LEFT FWD EPSU BATTERY PACK AND LEFT AFT EPSU BATTERY PACK AND CLEARED THE BATTERY MSG'S. FOUND SLIDE AT DOOR 1R BAD FOR "EXT LOAD FWD LEFT" FAULT. NEEDS A SLIDE AT DOOR 1R. REPLACED DOOR 1R SLIDE.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 50,596 hrs · 18,256 cycles

F-REPORTS EMERGENCY EXIT LIGHTS ON DOOR 1L, EMERGENCY LIGHTS TEST FAILURE MSG WAS "EPSU UNIT FWD L". REPLACED EPSU AT DOOR 1L. EMERGENCY LIGHTS NOW TEST OKAY.

Part: SENSOR — MALFUNCTIONED (COCKPIT) · airframe 50,473 hrs · 18,211 cycles

ABORTED TAKEOFF AT 100 KTS DUE TO CAPTS AIRSPEED INDICATION. PER POST FLIGHT REPORT, ADM -19 MESSAGE, AOA SENSOR 3FP2, AOA SENSOR 3FP3 DISAGREE. REPLACED CAPT ADM 19PF1 AND REPLACED NR 2 AOA 3PF2. ACP HIGH RANGE LEAK TEST, CHECKS OK. NO SPLIT ON AIRSPEED OR ALT.

Part: SLIDE — FAULTY (DOOR 1L) · airframe 50,470 hrs · 18,210 cycles

WHILE ACCOMPLISHING EMERGENCY LIGHTS TEST ON CIDS GOT MSG- EXT. LOADS FWD L. PERFORMED TEST OF LEFT FWD EPSU AND GOT A FAULT ON EXTERIOR LIGHTS. SUSPECT LT FWD ESCAPE SLIDE. MT33-001 IS HELPFUL FOR TS. ACCOMPLISHED TROUBLESHOOTING AND FOUND BOTH FWD DOOR SLIDES BAD. ONE SLIDE PLANESIDE AND ONE SLIDE ON AOG D1555. ACCMP'D REPLACEMENT OF DOOR 1R SLIDE & 1L SLIDE.ACCOMPLISHED RII INSPECTION OF DOOR 1LH AND DOOR 1RH. OPS CHECK NORMAL

Part: SLIDE — FAULTY (R1 DOOR) · airframe 49,592 hrs · 17,800 cycles

EMERGENCY LIGHT TEST FAILS, FAULT "EXT LOADS FWD R". TROUBLESHOOT SYSTEM FOUND DOOR 1R CAUSING EMERGENCY LIGHT FAILURE DURING TEST. REPLACED RT DOOR SLIDE ASSY. INSTALLATION AND OPS CHECKS GOOD, EMERGENCY LIGHT TESTS GOOD.

Part: LIGHT — INOPERATIVE (ESCAPE SLIDE) · airframe 49,240 hrs · 17,669 cycles

EMERGENCY LIGHT TEST FAULTING "EXT LOADS FWD L". DOOR 1L SLIDE LIGHTING FAULT ESTABLISHED. ACP EMERGENCY LIGHT TEST. FOUND NO FAULT. OPS CHK NORMAL.

Part: SLIDE — FAULTY (R1 DOOR) · airframe 48,379 hrs · 17,328 cycles

CIDS CLASS 1 FAULT FOR ESPU EXT LOAD FWD L MESSAGE AFTER OPERATION TEST OF EMERGENCY LIGHTING SYSTEM. REPLACED 1R FWD SLIDE. SYSTEM CHECKED NORMAL.

Part: SLIDE — FAULTY (L1 DOOR) · airframe 48,064 hrs · 17,198 cycles

EMERG LIGHT CK MESSAGE EXT LOADS FWD LT SLIDE LIGHTS INOP. REPLACED DOOR 1L SLIDE. EMERGENCY LIGHT CHECK PASSED.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 46,998 hrs · 16,770 cycles

EMERGENCY LIGHT TEST FAILED WITH MSG, EXTERNAL LOAD FWD LEFT. REPLACED PSU 10WL AND BATTERY, NO HELP. RE-INSTALLED ORIGINAL. SWAPPED L FWD AND R FWD SLIDES, ALSO NO HELP. RE-INSTALLED ORIGINAL. REPLACED DOOR 1LT SLIDE. CHECKS NORMAL. ALL EMERGENCY TEST FUNCTIONS NORMAL.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 45,426 hrs · 16,191 cycles

FLIGHT DIVERTED TO DUE TO YELLOW SYSTEM HYDRAULIC LOSS. PYLON HYD LINE WAS LEAKING AT RIB 5, REPLACED PYLON HYD LINE IN NR 2 PYLON. ALSO -REPLACE NR 1 ENG HYD FILTER DUE TO SYS RUN DRY.

Part: WIRE — SHORTED (DOOR 1L) · airframe 45,370 hrs · 16,175 cycles

3 SVC EMERGENCY LIGHT TEST FAILS. MED 1L SLIDE LIGHT NOT TESTING. FOUND SHORTED WIRE INSIDE ASSY SLIDE AT 1L. REPLACED DOOR SLIDE 1L.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 45,093 hrs · 16,077 cycles

DIVERTED DUE TO BURNING-ACRID SMELL IN AFT CABIN. BURNT BEARING IN LT RECIRC FAN. REPLACED LT RECIRC FAN, ALL TESTS WERE NORMAL, NO SMELL NOTED.

Part: SLIDE — SHORTED (EVAC SLIDE) · airframe 44,589 hrs · 15,901 cycles

EMERGENCY LIGHT SYSTEM TEST FAILS WITH CFDS MESSAGE EXT LOAD FWD LEFT. ELECTRICAL SHORT WITHIN FWD LEFT SLIDE ASSY. REPLACED SLIDE AT FWD LT DOOR. ALL CHECKS ARE NOW NORMAL.

Part: WIRE — SHORTED (EVAC SLIDE) · airframe 44,512 hrs · 15,871 cycles

CABIN EMERGENCY LIGHTS TEST FAILED EXT LOADS FWD L. WIRING SHORT IN SLIDE PACK. REPLACED SLIDE AT DOOR 1R. OPS CHECKED NORMALLY.

Part: COVER — MISSING (CABIN) · airframe 44,428 hrs · 15,839 cycles

SEATS 11C, 20C & 21C ARE MISSING THE EMERGENCY LIGHT LENS COVER. UNKNOWN PASSENGER DAMAGE. REPLACED LENS ON EMERGENCY LIGHTS ASSY AT ROW 11C, 20C, 21C. ALL LIGHTS OPERATIONAL.

Part: SLIDE — FAILED (L1 DOOR) · airframe 43,057 hrs · 15,360 cycles

DOOR 1L EMERGENCY SLIDE FAILS EMERGENCY LIGHT TEST. REPLACED DOOR 1L SLIDE PACK.

Part: SMOKE DETECTOR — FAULTY (FWD CARGO BAY) · airframe 42,413 hrs · 15,134 cycles

FWD CARGO COMPT SMOKE DETECTOR FAULT MESSAGE.

Part: SLIDE — FAULTY (L1 DOOR) · airframe 42,413 hrs · 15,134 cycles

EMERGENCY LIGHTS FAULTING EXTERNAL LOADS FWD LEFT.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 42,413 hrs · 15,134 cycles

WATER WASTE VENT OUTLET AT RIGHT FUSELAGE BETWEEN FR 68 & 69 HAS HEAVY CORROSION. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRICATED & INSTALLED DOUBLER REPAIR.

Part: BLADES — FAILED (NR 1 ENGINE) · airframe 41,912 hrs · 14,948 cycles

RTFL WITH NR 1 ENGINE SHUT DOWN. LOUD BAND HEARD ON CLIMBOUT. REPLACED NR 1 ENGINE. [06-26-07] ENGINE INGESTED COWLING ACOUSTIC PANELS DURING CLIMBOUT CAUSING DAMAGE TO A STAGE 3 COMPRESSOR BLADE.

Part: SLIDE — FAULTY (L1 DOOR) · airframe 41,667 hrs · 14,861 cycles

CABIN EMERGENCY LIGHTS CHECK SHOWS -ATA 33 -51-38 EXT LOADS FWD L- RE-SET CIDS, MESSAGE RE-APPEARED. REPLACED DOOR 1L ESCAPE SLIDE.

Part: UNKNOWN — VIBRATION · airframe 41,667 hrs · 14,861 cycles

DURING CLIMB-OUT, AIRCRAFT VIBRATION VARYING SPEEDS AND ALTITUDES. CRUISE SMOOTH. [SUP 06-06-07] REPLACED ALL THREE RUDDER ACTUATOR ROD ENDS.

Part: CONTROLLER — MALFUNCTIONED (NLG STEERING) · airframe 41,473 hrs · 14,794 cycles

NOSE WHEEL STEERING FAULT AT GEAR DOWN. [SUP 06-01-07] REPLACED NOSE WHEEL STEERING SERVO CONTROL 6GC.

Part: LIGHT — NO TEST (ESCAPE SLIDE) · airframe 40,729 hrs · 14,531 cycles

EMERGENCY LIGHT TEST FAILED LEFT FWD DOOR SLIDE. FAULT READS EXT LOAD FWD LEFT. REPLACED DOOR 1L SLIDE PACK. EMERGENCY LIGHT TEST OK.

Part: SLIDE — FAULTY (R1 DOOR) · airframe 40,519 hrs · 14,457 cycles

EMERGENCY LIGHT TEST PER 3SV HAS FAULT, EXT LOADS FWD L FAULT. REPLACED DOOR 1R SLIDE.

Part: SLIDE — FAULTY (L1 DOOR) · airframe 40,179 hrs · 14,336 cycles

EMERGENCY LIGHT TEST FAULTS EXT LOADS FWD LEFT. UNBOLTED SLIDE, CLEANED CONNECTOR, REINSTALLED SLIDE. TEST PASSED.

Part: LIGHT — FAULTY (ESCAPE SLIDE) · airframe 39,365 hrs · 14,040 cycles

ACFT FAILS CABIN EMERGENCY LIGHT CHECK. CIDS FAULTS 33-51-38 EXT FWD LT. REPLACED NR 1 LEFT SLIDE.

Part: SLIDE — FAILED (DOOR 1R) · airframe 38,508 hrs · 13,741 cycles

DOOR 1R SLIDE FAILS EXT LOADS TEST IN EMERGENCY LIGHTS TEST. REPLACED SLIDE 1R PER AMM 25-62-44.

Part: SLIDE — FAILED (CABIN) · airframe 37,965 hrs · 13,563 cycles

EXT LOADS FWD L, SHOWS ON PTP AFTER EMERGENCY SYSTEM TEST. REPLACED BOTH RIGHT HAND AND LEFT HAND FORWARD SLIDES. BOTH REMOVED SLIDES DID NOT RING-OUT CORRECTLY AT THE CONNECTOR. OPS TESTED NORMAL WITH NEW SLIDES.

Part: LIGHT — INOPERATIVE (DOOR 1L SLIDE) · airframe 37,440 hrs · 13,366 cycles

DOOR 1L SLIDE EMERGENCY LIGHTS INOPERATIVE. REPLACED SLIDE, NO HELP. CONNECTOR 2871VC. FOUND DAMAGED, REPLACED. REINSTALLED DOOR 1R SLIDE, PER AMM 25-62-44. OPS CHECKED LIGHTS GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SMOKE DETECTION) · airframe 37,371 hrs · 13,336 cycles

FWD CARGO PIT SMOKE WARNING ON FINAL. DISCHARGED AGENT 1 BOTTLE. ECAM WENT AWAY. FIRE DEPT ONSITE. TROULBESHOOTING PROCEDURES PERFORMED ON SMOKE DETECTION SYSTEM AND DISCOVERED SDCU CLASS II FAULT. REPLACED THE SDCU (10WQ) PCN:565-9019 PER AMM 26-17-34-401.

Part: LIGHT — NO TEST (DOOR 1L SLIDE) · airframe 36,077 hrs · 12,855 cycles

WHILE TESTING EMERGENCY LIGHTS FAULTED EXT LOADS FWD L HAD RED FAULT LIGHT EXT LOADS. WHILE PERFORMING THE AIRCRAFT EMERGENCY LIGHT TEST, SYSTEM MESSAGE POINTING TO FAULT IN FWD DOOR SLIDE ASSY. THE SLIDE WAS REPLACED SERVICEABLE ONE AND THE AIRCRAFT SYSTEM BECAME NORMAL. THE AIRBUS SLIDES HAVE LIGHT SYSTEM THAT CAN ONLY BE MAINTAINED IN THE SHOP. COMMON SLIDE LIGHT SYSTEM DEFECT IS BUSTED BULB OR BROKEN HARNESS. AS REQUIRED BY THE UALCMM FOR THE SLIDE, A SDR IS INITIATED BY THE OSV SHOP EVERYTIME A DEFECT IS FOUND DURING THE MAINTENANCE OF SLIDES.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 35,337 hrs · 12,582 cycles

NOSE GEAR WOULD NOT LOCK IN UP POSITION.

Part: LIGHT — FAILED (CABIN) · airframe 32,660 hrs · 11,586 cycles

EMERGENCY LIGHTS TEST FAIL, FAULTS EXT LOADS FWD LT. AMPERAGE READING ON RECEIPT 0.00. CHANGED LIGHTS. AMPERAGE READING WAS .870 (NORMAL) AFTER REPACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,807 hrs · 11,284 cycles

EMERGENCY LIGHT TEST FAULTED EXT LOADS FWD L. THE EPSU FAULTED. REPLACED POWER SUPPLY. OPERATIONS CHECK NORMAL.

Part: WIRE — SHORTED (SEAT 25B) · airframe 31,039 hrs · 11,001 cycles

ON FINAL APPROACH WIRES UNDER SEAT 25B SPARKED ELECTRICAL SMOKE. HALON FIRE EXTINGUISHER USED. CAUSE OF ELECTRICAL SPARK WAS IDENTIFIED TO ORIGINATE FROM THE SEAT-TO-SEAT CABLE, WHICH CONNECTS BOTH PES AND PSS DATA. THIS CABLE ALSO CARRIES 110 VAC. PER AIRCRAFT SAFETY, A CUSTOMER (ESCORTED IN PROTECTIVE CUSTODY) WAS KICKING THE SEAT IN FRONT OF HIM, CONTACTING THE SEAT-TO-SEAT CABLE RESULTING IN THIS INCIDENT. REPLACED THE SEAT-TO-SEAT CABLE AND PERFORM AN OPERATIONAL CHECK.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 21,874 hrs · 7,450 cycles

CABIN EMERGENCY LIGHT TEST FAILED. REPLACED DOOR 1 LEFT SLIDE AND EMERGENCY LIGHT SYSTEM POWER SUPPLY ASSEMBLY.

Part: UNKNOWN — ODOR (CABIN) · airframe 19,956 hrs · 6,825 cycles

CHEMICAL SMELL IN ENTIRE CABIN. *S/D* FOUND DEICING FLUID ON APU INLET DOOR AND INLET DUCT. CLEANED INLET DOOR, DUCT AND SURROUNDING AIRCRAFT SKIN. TEST RUN APU AND BOTH ENGINES, RAN BOTH AIR CONDITIONING PACKS, NO FURTHER ODOR NOTED.

Part: OVEN — CONTAMINATED (GALLEY) · airframe 18,586 hrs · 6,359 cycles

GALLEY OVEN SMOKING. *S/D* CLEANED SPILL IN THE OVEN (P/N: 2710-0001-01) AND PERFORMED AN OPERATIONAL CHECK. NO FURTHER FAULTS WERE FOUND.

Part: BOTTLE — DISCHARGED (DOOR ASSIST) · airframe 18,936 hrs · 6,477 cycles

DOOR 1 LEFT EMERGENCY ESCAPE RESERVOIR PRESSURE IS LOW. *S/D* SERVICED BOTTLE.

Part: LIGHT — INOP (CABIN)

WOULD NOT PASS EMERGENCY LIGHT TEST. *S/D* CAUSES CANNOT BE DETERMINED FROM THE WRITE-UP. EMER LIGHT BATTERY PACK, POWER SUPPLY UNIT AND SLIDE WERE REPLACED. EMERGENCY LIGHT TEST WAS THEN CHECKED OK. BUT SHOP FINDINGS REVEALED NO AMP READINGS ON LIGHT SYSTEM OF THE SLIDE.

Part: FAN — FAILED (COCKPIT)

DURING CRUISE, ELECTRICAL SMOKE SMELL IN COCKPIT WITH ECAM EXTRACT VENT FAULT AND VIBRATION FROM RT COCKPIT FLOOR. PUT EXTRACT VENT TO OVRHD, ODOR DISSIPATED, STILL HAD VIBRATION. CIRCUIT BREAKER PULLED FOR EXTRACT FAN, VIBRATION STOPPED.

Part: LIGHT — FAILED (CABIN)

EMERGENCY LIGHT SYSTEM FAILED TEST PER NR 2 SERVICE. *S/D* CHANGED P0WER SUPPLY AND BATTERY. ALSO, REPLACED SLIDE AND OPERATIONALLY CHECKED NORMAL.