N422UA

Part: ENGINE — VIBRATION (RIGHT) · airframe 90,208 hrs · 35,787 cycles

DURING CLIMB HIGHVIBRATION NUMBER 2 ENGN1 INDICATION 9.9 E2 PHOTOS ATTACHED UPDATING LOGPAGE TO REFLECT SDR. REPLACED #2 ENGINE. SEE JC 31-7100-9-0001 FOR APPLICABLE SIGNOFFS. ALL RII TASKS ACCOMPLISHED FOR E2 ENGINE CHANGE REF JC 31-7100-9-0001 AND RII GMM 09-25-05

Part: RESERVOIR — LOW (HYD SYSTEM) · airframe 88,394 hrs · 34,937 cycles

ECAM CAUTION MESSAGE - Y RSVR LO LVL MESSAGE INOP - HYD LEAK IS COMING OUT OF HP MANIFOLD ASS.GREEN/ YELLOW SYSTEM HYD. HP MANIFOLD GR./YE. ASS. IS LOCATED JUST FWD OF RH WHEEL WELL REMOVED #2 ENGINE EDP CASE DRAIN FOUND. PU WITHIN 30 SECONDS AFTER ECAM WARNING. FILTER, NO DEBRIS FOUND AND REPLACED FILTER PER MM29-13-43. ACCOMPLISHED CHECK OF THE FILTER DPI OF THE #2 ENGINE HCU OF THE REPLACED DAMAGED O-RING

Part: NONE — NONE (FR 25-27) · airframe 88,009 hrs · 34,733 cycles

ACCOMPLISH A PERMANENT REPAIR OF THE HOLES ON THE FWD CARGO COMP ARTMENT DOOR FR 25-27 FRAME FORK PER PART 3 OF THE LATEST REV OF ECRA 5230-02199 ON OR BEFORE THE AIRCRAFT REACHES 34,933 TOTAL AIRCRAFT FLIGHT CYCLES REQUEST DIP PER ECRA 5230-02199 FOR PERMANENT REPAIR OF FR25-27 FRAME FORKS PRIOR TO ACFT REACHED 34933 FLIGHT CYCLES. ACCOMPLISH A PERMANENT REPAIR OF THE HOLES ON THE FWD CARGO TOMC-APPROVAL FROM SC1ELBYC COMMENT COMPARTMENT DOOR FR25-27 FRAME FORK PER PART 3OF LATEST REVISION OF ECRA 5230-02199 ON OR BEFORE THE AIRCRAFT REACHES 34,933 TOTAL AIRCRAFT FLIGHT CYCLES QC REVIEWED QC REVIEWED T/A : 34933 TAFC........HC/U389717 RECORDS UPDATE....HC

Part: FITTING — NONE (FLANGE AT L20) · airframe 88,009 hrs · 34,733 cycles

UPON INSPECTION FOUND MATERIAL LOSS FROM FLANGE AT AND BELOW HOLE L20, ALSO MATERIAL LOSS FROM HEAD OF ADJACENT FASTENER L1 ON H AECO LCQ REF 9296325/36325 SUPPORT TASK FOR EC/RA 5311-02026. NR GENERATED BY V892444 REMOVED AND REPLACED L/H MLG DOOR ACTUATOR FWD FITTING IAW A320 SRM 51-42-11/001 AND SRM 51-44-11/001 AT HAECO LCQ ON HANGAR NR 9296325/36325 PERFORMED BY MECH V061619 RII INSP BY N078625

Part: NONE — NONE (FR 25- 27) · airframe 88,009 hrs · 34,733 cycles

REPAIR WAS ACCOMPLISHED ON THE FWD CARGO COMPARTMENT DOOR FR 25- 27 FRAME FORKS. PLANNING TO CONTACT ENGINEERING AFTER THE AIRCRA FT REACHES 34,833 TOTAL FLIGHT CYCLES BUT BEFORE 34,873 TOTAL AI RCRAFT FLIGHT CYCLES FOR THE ECRA 5230-02199 PART 3 PERMANENT RE PAIR INSTRUCTIONS. REF LOG PAGE 9524132 INTERIM REPAIR PER ECRA 5230-02199 PER PART 1.2 FOR DIP FOR INSP PRIOR TO ACFT REACHED 34933 PTC. REPAIR WAS ACCOMPLISHED ON THE FWD CARGO COMPARTMENT DOOR TOMC-APPROVAL FROM SC1ELBYC COMMENT FR25-27 FRAME FORKS. PLANNING TO CONTACT ENGINEERING AFTER THE AIRCRAFT REACHES 34,833 TOTAL AIRCRAFT FLIGHT CYCLES BUT BEFORE 34,873 TOTAL AIRCRAFT FLIGHT CYCLES FOR THE ECRA 5230-02199 PART 3 PERMANENT REPAIR INSTRUCTIONS AMENDMENT TO ABOVE TEXT. SHOULD READ "INTERIM REPAIR PER ECRA QC REVIEWED 5230-02199. PER PART 1.3 FOR DIP FOR PLANNING TO CONTACT ENGINEERING AFTER ACFT REACHED 34833PTC BUT BEFORE 34873 PTC. NOTE THIS IS A DTA DIP. QC REVIEWED T/A : PLN/ENG (>34833<34873 TAFC).......HC/U389717 RECORDS UPDATE....HC

Part: FRAME — CRACKED (LH FWD O/W EXT) · airframe 88,009 hrs · 34,733 cycles

LH FWD O/W EXIT FWD AND AFT FRAME SEGMENT HAVE SEVERAL CRACKS ON HAECO LCQ REF 9296327/36327 SPEC A3NB-52-4-6031. NR GENERATED B Y N078625 REMOVED & REPLACED L/H FWD O/W EXIT FWD AND AFT FRAME SEGMENT IA W A320 SRM 51-72-11-911-001 AT HAECO LCQ ON HANGAR NR 9296327/36 327 PERFORMED BY MECH V918284 RII INSP BY V892285

Part: FRAME — CRACKED (LH O/W EXT) · airframe 88,009 hrs · 34,733 cycles

LH AFT O/W EXIT FWD AND AFT FRAME SEGMENT HAVE SEVERAL CRACKS ON HAECO LCQ REF 929326/36326 SPEC A3NB-52-4-6031. NR GENERATED BY N078625 REMOVED & REPLACED L/H AFT O/W EXIT FWD AND AFT FRAME SEGMENT IA W A320 SRM 51-72-11-911-001 AT HAECO LCQ ON HANGAR NR 9296326/36 326 PERFORMED BY MECH V918284 RII INSP BY V892285

Part: NONE — CRACKED (RH AFT O/W EXIT) · airframe 88,009 hrs · 34,733 cycles

RH AFT O/W EXIT FWD AND AFT FRAME SEGMENTS HAVE SEVERAL CRACKS. GENERATED AT HAECO LCQ PER NR 9296329 (36329) BY N078625 {A3NB-5 2-4-6031} REMOVED AND REPLACED TWO EACH SEGMENTS IAW A320 SRM 51-72-11-911 -001- PG 1-2. ACP BY V918284 INSP BY V892442

Part: NONE — CRACKED (RH FWD O/W EXIT) · airframe 88,009 hrs · 34,733 cycles

RH FWD O/W EXIT FWD AND AFT FRAME SEGMENTS HAVE SEVERAL CRACKS. GENERATED AT HACEO LCQ PER NR 9296328 (38328) BY N078625. {A3NB- 52-4-6031} REMOVED AND REPLAED (2EA) SEGMENTS IAW A320 SRM 51-72-11-911-001 RESTORED STRUCTURE FINISH IAW A320 SRM 51-23-11/001 AND IAW A32 0 SRM 51-72-11-911-001. ACP BY V918284 INSP BY V892442.

Part: BATTERY — DISCHARGED (EEMRGENCY LIGHTS) · airframe 83,507 hrs · 32,620 cycles

FWD EMERGENCY EPSU BATTERY FAILS CAP CHECK 10CL-A3NB-33-3-6013-NR 9296399 GENERATED BY V061697, AT HAECO LCQ. REMOVED AND REPLACED THE EMERGENCY LIGHTS EPSU BATTERY PACK (10W L), IAW A319/320 M/M 33-51-38-000-002-A AND 33-51-38-400-002-A. OPERATIONS TEST OFF EPSU BY BITE CHECKS GOOD, IAW A319/320 M/M 33-51-00-7 10-001-A.

Part: SECU — MALFUNCTIONED (SPOILERS) · airframe 82,791 hrs · 32,283 cycles

F/CTL SPLR FAULT MESSNUMBER 3 SPOILER SHOWINUP ON BOTH WINGSFA V ERIFY DOWN T/S PER TSM TASK 27-60-00-810-830-A. REMOVED AND REPLACED SEC1 PER AMM 27-94-34. NO FAULTS FOUND. AIRCRAFT BACK TO SERVICE. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1059407 SN OFF 5139 SEE L/P 4628030 ADD EMP:U353205

Part: TARGET — OUT OF ADJUST (AFT CARGO DOOR) · airframe 80,292 hrs · 31,213 cycles

AFT CARGO DISPLAYED ON UPPER ECAM SCREEN. - DOOR AT 2000 FEET ON DEPARTURE. PRESSURIZATION NORMAL. PERFORMED WIRING CHECK AS PER AWM 31-54-46 CHECKED WIRES FROM LGCIU 1 PLUG AA 6E ,6F TO SENSOR 32WV . WIRING CHECKS GOOD ALSO MEGGED PAIR NO FAULTS FOUND .FOUND FLAPPER DOOR WITH PLAY CAUSING TARGET GAP TO MOVE . VERIFIED BY PUSHING ON CARGO DOOR FLAPPER AND INDICATION WOULD ALSO FLUCTUATE ,TARGET N DOOR WILL REQUIRE A RIG AS PER AMM 52-71-12-400-001A ADJUSTED AFT CARGO VENT DOOR IRW AMM 52-32-11-820-003-A, NO FIX. T/S AFT CARGO DOOR FOUND J1 TARGET TOO FAR FROM PROXIMITY SWITCH. ADJUSTED TARGET J1 IRW 52-71-00-820-003-A. OPS CHECKED GOOD, NO FURTHER DEFECTS NOTED AT THIS TIME. A/C OK TO CONTINUE.

Part: PROXIMITY SWITCH — BENT (AFT CARGO DOOR) · airframe 80,292 hrs · 31,213 cycles

AFT CARGO DOOR ECAM CAME ON SHORTLY AFTER LIFTOFF FROM SRQ FOUND DOOR PROX SWITCH MOUNTING SURFACE BENT. ADJUSTED PROX SWITCH FOR AFT CARGO DOOR. PER AMM 52-71-12. OPENED AND CLOSED DOOR SEVERAL TIMES. DOOR OPEN AND CLOSE INDICATION FUNCTIONS ARE NORMAL

Part: PROXIMITY SWITCH — FAILED (AFT CARGO DOOR) · airframe 80,258 hrs · 31,199 cycles

DOOR AFT CARGO ECAM IN FLIGHT AT ABOUT12000 FEET MSLNO LOSS OF P RESSURE REF TSM 32-31-00-810-886-A. AIRCRAFT FAULTED 32WV PROX SENSOR TA RGET POSITION- TOMC KROWN REQUEST MEL 5270D FOR AFT CARGO DOOR INDICATION INOP. ADD EMP:U232365 NOC DESK: 320 NAME: JOHN DATE: 24-APR-19- APPROVED FOR MEL 5270D VERIFIED CLOSED AND SECURE PRIOR TO FLIGHT. ADD EMP:U232365 C/W MEL 5270D. AFT CARGO DOOR ECAM INDICATION INOP. DOOR

Part: SKIN — DENTED (L2 DOOR) · airframe 78,949 hrs · 30,599 cycles

L-2 DOOR EXTERNAL SURFACE AFT LOWER CORNER HAS A DENT A3NB-06-3- 6001 GENERATED BY N078570 ON HAECO LCQ NR 23034 ON HAECO LCQ NR 9297034 ACCOMPLISHED DOUBLER REPAIR ON L2 DOOR AFT CORNER ZONE 800 STA 3237 TO STA 3257 STR 23 L. ORG DENT WAS L:1.5 X W: 2.9 X D.120. THIS REPAIR IS A CAT B AND WAS ACCOMPLISHED PER SRM 52-10-00-300 005 FIG 20103. THIS REPAIR REQUIRES REINSP AT THE FOLLOWING DEFINED INTERVALS 60,000 FC. FH NOT RELEVANT, SUBSEQUENT INSP TBD. METHOD TBD PER SRI 52-10-00-205. MATERIAL: DOUBLER 2024T3 THICKNESS.125. FILLER MATERIAL 2024T3 THICKNESS .100. OK TO DIP PER SRI. THIS RPR REQ REINSP AT THE FOLLOWING DEFINED INTERVALS 60,000 FC FROM RPR EMBODIMENT. SUBSEQ INSP TBD. METHOD TBD PER SRI. REF SRI 52-10-00-205-022. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: STRINGER — CORRODED (FRAMES 29-34) · airframe 78,949 hrs · 30,599 cycles

FWD CARGO FR 29-34 STGR 43L HAS CORROSION AROUND FASTENER HOLES. (SUPPORT TASK:FCD 5300-01440) PER HAECO LCQ REF. NO. 9297138. G ENERATED BY N078570. REPAIRED FWD CARGO FR29-34 STRINGER 43L CORROSION PER SRM53-21-1 3-283-001. REMOVED & REPLACED STRINGER SPLICE @ FR30-31 PER SRM5 1-72-11-911-001. STRINGER ORIG THICKNESS 0.079". REMOVED STRINGE R CORROSION BETWEEN FR32-33 (2 HOLES), 7TH FASTENER HOLE AFT OF FR32 D=0.010" BY 1.0"X 1.0" & 10TH FASTENER HOLE AFT OF FR32 D=0 .011" BY 1.0"X 1.0". WITHIN MAX ALLOW REWORK LIMIT PER SRM53-21- REA ON STR43L BETWEEN FR33&34 HIGH=0.089" LOW=0.082". THICKNESS R33-34, THICKNESS HIGH=0.089" LOW=0.082". THICKNESS OF BLENDED A 13-283-001 FIG 10102 SHT 1. REMOVED STRINGER CORROSION BETWEEN F OF BLENDED AREA ON STRG43L BETWEEN FR32&33 ON #5 HOLE AFT OF FR3 2 HIGH=0.090" LOW=0.088". THICKNESS OF BLENDED AREA ON STR43L BE TWEEN FR32&33 ON HOLE 7.5" AFT OF FR32 HIGH=0.089" LOW=0.087". B SPECTION AT 60,000 FC & 120,000 FH EHICHEVER OCCURS FIRST. SUBSE NCES. PRIMED & TOP COATED. SRM REQUIRES SRI53-21-13-205-001 REIN LENDED AREAS BETWEEN FR32-34 ON STR43L FOUND TO BE WITHIN TOLERA QUENT INSPECTION INTERVALS AND INSP METHODS TBD. HAECO NON ROUTI NE 23138. OK TO DIP PER SRM. REINSPECT PER SRI 53-21-13-205-001 AT 60000FC OR 120000FH WHICHEVER OCCURS FIRST. TOMC-APPROVAL FROM SC1ELBYC COMMENT TOMC APPROVED: QC REVIEWED TOMC APPROVED: QC REVIEWED RECORDS UPDATE OK TO DIP PER SRM. REINSPECT PER SRI 53-21-13-205-001 AT 60000FC O

Part: SKIN — DENTED (FRAME 23) · airframe 78,949 hrs · 30,599 cycles

FUSELAGE EXTERNAL SURFACE FR-23 STRG 23 DENT REQS FURTHER EVAL L OG #3534741 AT HAECO LCQ PER REF NO.9297300 BY MECH N078570 REMOVED DAMAGE & REPAIRED EXTERNAL SURFACE FR23 STRG23 PER SRM 5 3-00-11-300-029. NOMINAL SKIN THICKNESS 0.047". DOUBLER THICKNE SS 0.050". SRI 53-00-11-205-017 REQUIRES INSP THRESHOLD FROM TIM AIR OF 60,000 FC & 120,000 FH, SUBSEQUENT INSPS & INSP METHODS T BD. HAECO NR 23300. OKAY TO DIP INSPECTION THRESHOLD FROM TIME OF REPAIR EMBODIMENT FOR 60,000FC/120,000 FH SUBSEQUENT INSPECTIONS TBD REF SRI 53-00 -11-205-017. TOMC-APPROVAL FROM SC1ELBYC COMMENT TOMC APPROVED: QC REVIEWED TOMC APPROVED: QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: STOP FITTING — CRACKED (R1 DOOR FRAME) · airframe 78,949 hrs · 30,599 cycles

R-1 DOOR STOP FITTING #1 FRAME 20 INBOARD LOWER HOLE IS CRACKED IN FRAME WEB AT 6:00. REPAIRED R-1 FR20 IB LWR HOLE PER ECRA 5311-02033. HAECO NR 2266 6. ECRA REQUIRES DTA LOG PAGE TO ACP INIT INSPECTIONS PER PART2 OF ECRA 5311-02033 ON OR BEFORE ACFT REACHES 44,899 TTL ACFT FL T CYCLES. ACP REPEAT INSPS AT INTERVALS NOT TO EXCEED 14,300 ACF T FLT CYCLES, THEREAFTER. OKAY TO DIP TO ACCOMPLISH THE INITIAL INSPECTIONS PER PART 2 OF ECRA 5311-02033 ON OR BEOFRE AIRCRAFT REACHES 44899 TOTAL AIRCRA FT FLIGHT CYCLES.ACCOMPLISH THE REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 14,300 AIRCRAFT FLIGHT CYCLES, THEREAFTER REF ECRA 5311-02033. TOMC-APPROVAL FROM SC1ELBYC COMMENT TOMC APPROVED: QC REVIEWED TOMC APPROVED: QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: STOP FITTING — CRACKED (L1 DOOR FRAME) · airframe 78,949 hrs · 30,599 cycles

ROTO INSP SHOWED CRACK INDICATION AT L1 DOOR, FR16 STOP #7, INBD UPPER HOLE. HAECO NR 22652. REPAIRED LH FR 16 #7 INTERCOSTAL PER ECRA 5311-02033. PER PART 1 ITEM 2 OF ECRA DTA LOG PAGE REQUIRED TO ACP INITIAL INSPS PER PA RT 2 OF ECRA 5311-02033 ON OR BEFORE THE AIRCRAFT REACHES 44,899 TTL ACFT FLT CYCLES. ACCOMPLISH REPEAT INSPS AT INTERVALS NOT TO EXCEED 14,300 ACFT FLT CYCLES, THEREAFTER. OKAY TO DIP TO ACCOMPLISH THE INITIAL INSPECTIONS PER PART 2 OF ECRA 5311-02033 ON OR BEFORE AIRCRAFT REACHES 44899 TOTAL AIRCRA FT FLIGHT CYCLES.ACCOMPLISH THE REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 14,300 AIRCRAFT FLIGHT CYCLES, THEREAFTER REF ECRA 5311-02033. TOMC-APPROVAL FROM SC1ELBYC COMMENT TOMC APPROVED: QC REVIEWED TOMC APPROVED: QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: STOP FITTING — CRACKED (L1 DOOR) · airframe 78,949 hrs · 30,599 cycles

ROTO INSP SHOWED CRACK INDICATION AT L1 DOOR, FR16 STOP #7, INBD UPPER HOLE. HAECO NR 22652. REPAIRED LH FR 16 #7 INTERCOSTAL PER ECRA 5311-02033. PER PART 1 ITEM 2 OF ECRA DTA LOG PAGE REQUIRED TO ACP INITIAL INSPS PER PA RT 2 OF ECRA 5311-02033 ON OR BEFORE THE AIRCRAFT REACHES 44,899 TTL ACFT FLT CYCLES. ACCOMPLISH REPEAT INSPS AT INTERVALS NOT TO EXCEED 14,300 ACFT FLT CYCLES, THEREAFTER. OKAY TO DIP TO ACCOMPLISH THE INITIAL INSPECTIONS PER PART 2 OF ECRA 5311-02033 ON OR BEFORE AIRCRAFT REACHES 44899 TOTAL AIRCRA FT FLIGHT CYCLES.ACCOMPLISH THE REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 14,300 AIRCRAFT FLIGHT CYCLES, THEREAFTER REF ECRA 5311-02033. TOMC-APPROVAL FROM SC1ELBYC COMMENT TOMC APPROVED: QC REVIEWED TOMC APPROVED: QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: SKIN — DENTED (FRAME 23) · airframe 78,949 hrs · 30,599 cycles

FUSELAGE EXTERNAL SURFACE FR-23 STRG 23 DENT REQS FURTHER EVAL L OG #3534741 AT HAECO LCQ PER REF NO.9297300 BY MECH N078570 REMOVED DAMAGE & REPAIRED EXTERNAL SURFACE FR23 STRG23 PER SRM 5 3-00-11-300-029. NOMINAL SKIN THICKNESS 0.047". DOUBLER THICKNE SS 0.050". SRI 53-00-11-205-017 REQUIRES INSP THRESHOLD FROM TIM AIR OF 60,000 FC & 120,000 FH, SUBSEQUENT INSPS & INSP METHODS T BD. HAECO NR 23300. OKAY TO DIP INSPECTION THRESHOLD FROM TIME OF REPAIR EMBODIMENT FOR 60,000FC/120,000 FH SUBSEQUENT INSPECTIONS TBD REF SRI 53-00 -11-205-017. TOMC-APPROVAL FROM SC1ELBYC COMMENT TOMC APPROVED: QC REVIEWED TOMC APPROVED: QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: SKIN — CORRODED (L2 DOOR) · airframe 78,949 hrs · 30,599 cycles

L-2 DOOR SKIN INNER SURFACE LOWER FWD & AFT SECTIONS CORROSION A ROUND FASTENER HOLES (12 EA) ON HAECO LCQ REF 9297399 SPEC A3NB- 06-3-6001 GENERATED BY N078570

Part: SKIN — GOUGED (FRAMES 51-52) · airframe 78,949 hrs · 30,599 cycles

LOWER AFT FUSELAGE AT FR51-FR52, BETWEEN STR37R AND STR38R HAS A 0.40" GOUGE (A3NB-53-4-6229) PER HAECO LCQ NR 9296167. GENERATE D BY V923923. CUTOUT DAMAGED AREA AT FR50 STR38R TO STR 39R PER SRM53-00-11-30 0-013 PARA 2(A)(1)(C)&(D). FABRICATED & INSTALLED DOUBLER & FILL WE PER SAME SRM 2(A)(1)(G)-(K). TREATED, PRIMED & TOPCOATED. SRI 53-00-11-205-035 FOR SKIN THICKNESS 4MM REQUIRES INSP THRESHOLD FROM TIME OF REPAIR OF FC 19,400, FH 38,800 & STRUCTURAL MOD POI NT AFTER REPAIR OF FC 29,100, FH 58,200 & SUBSEQUENT INSPECTION & NTM 51-10-16. INTERVALS OF FC 3,700, FH 7,400, USING INSP METHODS NTM 51-10-15 OK TO DIP PER SRM. REQUIRES INSP THRESHOLD FROM TIME OF REPAIR OF 19400FC, 38800FH, & STRUCTURAL MOD POINT AFTER REPAIR OF 29100FH, 58200FH & SUBSEQUENT INSPECTION INTERVALS OF 3700FC, 7400FR

Part: STOP FITTING — CRACKED (FRAME 16) · airframe 78,949 hrs · 30,599 cycles

L-1 DOOR CUTOUT FRAME 16 STOP FITTING #1 OB HOLE IS CRACKED IN F RAME WEB AT 6:00. STEP REAMED FR16 #1 DOOR STOP FITTING UPPER OB HOLE TO CRACK FRE E CONDITION PER SRM51-44-11-001. PERFORMED REPAIR PER AIRBUS SB A320-53-1339/ALI53-11-03. R&R''D DOOR STOP FITTING & INTERCOSTAL PER SRM 51-72-11-911-001 PER ECRA 5311-02029. HAECO NR 22580. RII INSP C/W BY HAECO QC LC-31

Part: SKIN — DENTED (FRAME 62) · airframe 78,949 hrs · 30,599 cycles

FUSELAGE EXTERNAL SURFACE FR-62 STRG 41L,42L HAS DENT (A3NB-05-3 -6003) PER HAECO LCQ NR 9296352. GENERATED BY N078570. PERFORMED DAMAGE CUT-OUT, FABRICATED & INSTALLED DOUBLER & FILLE R PER SRM53-00-300-043 PARA 2(A)(1)(G-L)(N-O) & FIG 20144 SHEET 1. TREATED, PRIMED & TOP COATED. SRI53-00-11-205-017 REQUIRES IN SPECTION FROM TIME OF REPAIR AT FC 21,200 & FH 42,400. SUBSEQUEN T INSPECTIONS REQUIRED AT INTERVAL FC 2,200 & FH 4,400. INSP MET HOD ULTRASONIC/HFEC. NOMINAL SKIN THICKNESS 0.063" PER SRM 53-41-11-001 FIG 00108. DO UBLER THICKNESS 0.071". FILLER THICKNESS 0.063". FOR 21,200FC/42,400FH WITH SUBSEQUENT INSPECTION INTERVALS OF 2, 200FC/4,400 FH REF SRI 53-00-11-205-017. OKAY TO DIP INSPECTION THRESHOLD FROM TIME OF REPAIR EMBODIMENT TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED QC REVIEWED INSPECT

Part: SKIN — DENTED (FRAME 63) · airframe 78,949 hrs · 30,599 cycles

AFT FUSELAGE EXTERNAL SURFACE FR 63 STR 41L HAS A DENT - A3NB-05 -3-6003 - GENERATED BY N078570 AT HAECO LCQ PER N/R 9297297 REPAIRED AFT FUSELAGE SKIN AT FR63, STR 41L PER SRM 53-00-11-800 -004.REMOVED DOUBLER AND CLEAT AT FR63 STR41L-STR42L. FABBED & I NSTALLED DOUBLER & CLEAT PER SRM53-00-11-300-004 & SRM51-44-11- 001 & DWG D53470801. TREATED & PRIMED & TOP COATED. SRI REQUIRED AT INSP THRESHOLD FROM TIME OF REPAIR AT 24,600 FC, 49,200 FH & SUBSEQUENT INSPS AT INTERVAL OF 2,900 FC, 5,800 FH. INSP METHODS NTM51-10-15 & 16. NOMINAL SKIN THICKNESS 0.063". DOUBLER THICKNESS 0.071". FILLER THICKNESS 0.063". CLEAT THICKNESS 0.063". HAECO NR 23297. OKAY TO DIP INSPECTION THRESHOLD OF 24600FC/49200FH WITH SUBSEQUENT INSP

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

LT FR56 TO FR57 STR43 EVIDENCE OF CORROSION. REMOVED AND REPLACED CORRODED SECTION OF STRINGER 43 BETWEEN FR56 & FR57. SPLICED IN SECTION WITH 2 COUPLINGS PER SRM-53-00-13-3 00-001 PG 8. ALODINED, PRIMED & TOP COATED.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

FWD CARGO FR 26-34 STR 41L HAS CORROSION AROUND FASTENER HOLES. REMOVED CORROSION BY BLENDING IAW SRM 53-21-13-283-001. MATERIAL LOSS OF .003 FOUND TO BE WITHIN LIMITS IAW SRM 53-21-13-283-001. REMOVED AND REPLACED STRINGER SPLICE AT FR30-FR31 STR 41L IAW SRM 51-72-11-911-001.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

FWD CARGO FR28 BETWEEN 41R-42R CLEAT IS CORRODED. REMOVED, FABRICATED AND INSTALLED CLEAT IN FWD CARGO FR28 BTWN STR 41R-42R IAW DRAWING D53230537, SRM 51-26-00-001 AND 51-7 0-12-001. TREATED/PRIMED IAW SRM 51-21-A-001. TOPCOATED IAW SRM 51-75-12-0013C.

Part: FITTING — CORRODED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

UPON REMOVING AFT CARGO THRESHOLD FOUND FWD LWR CORNER FITTING H AS CORROSION. R&R AFT CARGO FWD LWR CORNER FITTING IAW SRM 51-42-11.

Part: FITTING — CORRODED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

UPON REMOVING AFT CARGO THRESHOLD FOUND AFT LWR CORNER FITTING H AS CORROSION. R&R AFT CARGO COMPARTMENT AFT CORNER FITTING AT FR56 ON RIGHT HAND SIDE IAW SRM 51-42-11-001.

Part: HINGE FITTING — DAMAGED (VERTICAL STAB) · airframe 78,949 hrs · 30,599 cycles

VERT STAB RUDDER HINGE FITTING 2, 4 AND 5 IS DAMAGED. R&R HINGE FITTINGS NR 2, NR 4 AND NR 5 ON VERTICAL STAB IAW SRM 55-36-41-000-001-A & AMM 55-36-41-400-001-A.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

FWD CARGO FR 31 BETWEEN STR 41R-42R CLEAT HAS CORROSION FCD 530 0-01440. R&R CLEAT AT FRAME 31 BTWN STR 41R-42R IAW SRM 51-42-11-001.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

FWD CARGO PIT RT SIDE INTERCOSTAL AT FR29-30, STR 38R HAS OUT OF ROUND AND DOUBLE DRILLED HOLES. R&R INTERCOSTAL AT FR29-FR30, STR38R IAW SRM 51-72-11-911-001 AND SRM 51-42-11-001 PARA 2E AND 2F.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

LT FR56 TO FR57 STR43 EVIDENCE OF CORROSION A3NB-53-4-6179 GENERATED ON NR 9296814 REMOVED AND REPLACED CORRODED SECTION OF STRINGER 43 BETWEEN FR5 6 & FR57. SPLICED IN SECTION WITH 2 COUPLINGS PER SRM-53-00-13-3 00-001 PG 8. ALODINED, PRIMED & TOP COATED. SRI-53-00-13-205-001 TABLE 30105 REQUIRES REINSPECT BEFORE 60,000 FC AND 120,000 FH A T INTERVALS TBD & INSP METHODS TO TBD.

Part: STOP FITTING — DAMAGED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

L2 DOOR FR68 NO.1 DOOR STOP LOWER I/B HOLE HAS A REJECTABLE INDI CATION AD RELATED TASK NO. 2018-03-12 SUPPORT TASK GENERATED ON NR 9296748 REAMED I/B HOLE TO .391 PER SRM 53-41-12-300-008 STEP 2A(F). HFEC ROTORY SCAN COMPLETED WITH NO RELEVANT INDICATIONS. COLD WORKED HOLE PER SRM 51-48-00-001 TABLE 00101. FINAL REAM SIZE .400 D OVER .2825 PER SRM 51-44-11-001 TABLE 00112. FREEZE PLUG FABRICATED ON NR 23186. INSTALLED FREEZE PLUG PER SRM 51-73-12-001 PAR. 4A. REAMED HOLE IN STOP FITTING TO 2N M 51-75-12-001 PARA. C. HFEC INSPECTED L2 DOOR FR 68 NR 1 STOP WEB & 53-41-12-300-010 PAR. 2(A). TREATED, PRIMED AND PAINTED PER SR (BOTH SIDES OF AFFECTED AREA) WITH NO REJECTABLE INDICATIONS. -009 AT 38500 FC FROM TIME OF REPAIR EMBODIMENT FH NOT RELEVANT. INSTALLED L2 DOOR NR 1 STOP FITTING AT FR 68 PER SRM 53-41-12-300- 010. THIS REPAIR REQUIRES AN SRI INSPECTION PER SRI 53-41-12-205 VANT. SUBSEQUENT INSPECTION INTERVALS REQUIRED AT 7700 FC. FH NOT RELE REPAIR WASHER FABRICATED ON NR 23186.

Part: STOP FITTING — DAMAGED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

R2 DOOR NR 4 STOP FITTING OTBD UPPER HOLE AT FR68 PRODUCES REJECTABLE INDICATIONS DURING RFHEC BOLT HOLE INSP AT LCQ PER REF NR 9296646. REPLACED DOOR R2 NR 4 STOP FITTING P/N D5348017920000. REAMED HOLE IN STOP FITTING TO 2ND OVER TO .2825 PER SRM 51-44-11-001 TABLE 00112 AND 53-41-12-300-010 PAR. 2(A). TREATED, PRIMED & PAINTED PER SRM 51-75--12-001. HFEC INSPECTED R2 DOOR FR 68 DOOR STOP NR 4 WEB (BOTH SIDES OF AFFECTED AREA), NO REJECTABLE INDICATIONS NOT ED PRIOR TO INSTALLATION. INSTALLED DOOR R2 NR 4 STOP FITTING PER SRM 58-41-12-300-010 PAR 2.

Part: STOP FITTING — DAMAGED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

R2 DOOR NR 1 STOP FITTING INBD LWR HOLE AT FR68 PRODUCES REJECTABLE INDICATIONS DURING RFHEC BOLT HOLE INSP. REPLACED DOOR R2 NR 1 STOP FITTING P/N D5348017920000. REAMED INBD LOWER HOLE TO 2ND OVER .2821 PER SRM 51-44-11-001 TABLE 00112 A ND SRM 53-41-12-300-010 PAR 2A. TREATED, PRIMED & PAINTED PER SRM 51-75-11-001 PAR 4C. HFEC INSPECTED R2 DOOR FR68 DOOR STOP NR 1 WEB (BOTH SIDES OF AFFECTED AREA) WITH NO REJECTABLE INDICATIONS. INSTALLED NR 1 STOP FITTING PER SRM 53-41-12-300-010.

Part: STOP FITTING — DAMAGED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

R2 DOOR NR 5 STOP FITTING OTBD UPPER HOLE AT FR68 PRODUCES REJECTABLE INDICATIONS DURING RFHEC BOLT HOLE INSPECTION AD 2018-03-1 2. REPLACED STOP FITTING P/N D5348017920000. REAMED HOLE IN STOP FITTING TO .2825 PER SRM 51-44-11-001 TABLE 00112 & SRM 53-41-12-3 00-010 PAR 2(A). TREATED, PRIMED & PAINTED PER SRM 51-75-12-001 PAR 4C. HFEC INSPECTED R2 DOOR FR 68 NR 5 DOOR STOP WEB(BOTH SIDES OF AFFECTED AREA) WITH NO REJECTABLE INDICATIONS. INSTALLED NR 5 STOP FITTING AT FR 68 PER SRM 53-41-12-300-010.

Part: STOP FITTING — DAMAGED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

R2 DOOR NR 6 STOP FITTING INBD LWR HOLE AT FR68 PRODUCES REJECTABLE INDICATIONS DURING RFHEC BOLT HOLE INSP PER REF NR 9296644. REPLACED R2 NR 6 DOOR STOP FITTING P/N D5348017920000. REAMED I/B LWR HOLE TO 2ND O/S .2825 PER SRM 51-44-11-001 TABLE 00112 AND 5 3-41-12-300-010 PAR 2(A). NEW STOP FITTING TREATED, PRIMED AND PAINTED PER SRM 51-75-12-001 PAR 4C. HFEC INSPECTED R2 DOOR FR 68 DOOR STOP NR 6 WEB(BOTH SIDES OF AFFECTED AREA)WITH NO REJECTABLE INDICATIONS. INSTALLED R2 NR 6 STOP FITTING AT FR68 PER SRM 53-41-12-300-010.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

FWD CARGO FR 28-34 STR 41R HAS CORROSION AROUND FASTENER HOLES. REMOVED AND REPLACED STR IAW SRM 51-72-11 FROM FR24-35 STR 41R.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

LT FR61 TO FR63 STR42 HAS EVIDENCE OF CORROSION (A3NB-53-4-6179). REMOVED AND REPLACED STRINGER 42L AT FR60 TO FR64 IAW SRM 51-72-11-911-001.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

(A3NB-53-4-6179) FR52A TO FR56 DOOR SILL HAS EVIDENCE OF CORROSI ON IN NUMEROUS AREAS, AND TORSION BOX COVER SHEET AT PER FREF NR 9296809 REMOVED AND REPLACED AFT CARGO COMPT TORSION BOX SHEET COVER BET WEEN FR52 AND FR56 IAW SRM 51-42-11-001 PARA E&F.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

(A3NB-53-4-6179) FR52A TO FR56 DOOR SILL HAS EVIDENCE OF CORROSION IN NUMEROUS AREAS, AND TORSION BOX COVER SHEET AT PER FREF NR 9296809 REMOVED AND REPLACED AFT CARGO COMPT TORSION BOX SHEET COVER BETWEEN FR52 AND FR56 IAW SRM 51-42-11-001 PARA E&F.

Part: CLEAT — DAMAGED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

FCD 5300-01440 - SFWD CARGO FR26 BTWN STR 43R-44 HAS ELONGATED FASTENER HOLES AND TOOLING MARKS, DOT Z163, SUPPORT TASK, REF. NR 9297130, REMOVED AND REPLACED CLEAT IN FWD CARGO AT FRAME 26 BTWN STR 43R-44 IAW SRM 51-42-11-001 2(E). WORK ACCOMPLISHED.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

FWD CARGO FR29 BETWEEN STR 42R-43R CLEAT HAS CORROSION. REMOVED AND REPLACED CLEAT IN FWD CARGO AT FRAME 29 BETWEEN STR 42R-43R IAW SRM 51-42-11-001 2(E).

Part: CLEAT — CORRODED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

FWD CARGO FR33 BETWEEN STR 41R-42R CLEAT HAS CORROSION, SUPPORT TASK FCD 5300-01440. REMOVED AND REPLACED CLEAT IN FWD CARGO AT FRAME 33 BETWEEN STR 41R-42R IAW SRM 51-42-11-001 2(E).

Part: CLEAT — CORRODED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

FWD CARGO FR30 BETWEEN STR 43L-44 CLEAT HAS CORROSION, SUPPORT TASK FCD 5300-01440. REMOVED AND REPLACED CLEAT IN FWD CARGO AT FRAME 30 BETWEEN STR 43L-44 IAW SRM 51-42-11-001 2(E).

Part: CLEAT — CORRODED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

FWD CARGO FR30 BETWEEN STR 42L-43L CLEAT HAS CORROSION, SUPPORT TASK FCD 5300-01440. REMOVED AND REPLACED CLEAT IN FWD CARGO AT FRAME 30 BETWEEN STR 42L-43L IAW SRM 51-42-11-001 2(E).

Part: CLEAT — CORRODED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

FWD CARGO FR28 BETWEEN STR 42R-43R CLEAT HAS CORROSION, SUPPORT TASK FCD 5300-01440. REMOVED AND REPLACED CLEAT IN FWD CARGO AT FRAME 28 BETWEEN STR 42R-43R IAW SRM 51-42-11-001 2(E).

Part: CLEAT — CORRODED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

FWD CARGO FR31 BETWEEN STR 43L-44 CLEAT HAS CORROSION, SUPPORT TASK FCD 5300-01440. REMOVED AND REPLACED CLEAT IN FWD CARGO AT FRAME 31 BETWEEN STR 43L-44 IAW SRM 51-42-11-001 2(E).

Part: CLEAT — CORRODED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

FWD CARGO FR32 BETWEEN STR 40L-41L CLEAT HAS CORROSION, SUPPORT TASK FCD 5300-01440. REMOVED AND REPLACED CLEAT IN FWD CARGO AT FRAME 32 BTWN STR 40L-41L IAW SRM 51-42-11-001 2(E).

Part: SKIN PANEL — CORRODED (RUDDER) · airframe 78,949 hrs · 30,599 cycles

RUDDER TIP RT SIDE HAS CORROSION AND HAS NUMEROUS EXPOSED MATERIAL ON FAIRING MOUNTING SURFACE, OFF ACFT PART. REMOVED DAMAGE FROM RUDDER TIP AND REPAIRED IAW SRM 55-44-0 0-300-012 FIG 20109. THIS REPAIR IS CONSIDERED MAJOR REPAIR IAW GMM 03-20-20 AND SRM 51-11-12 FIG 00127.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

FWD CARGO FR29 BETWEEN STR 43R-44 CLEAT HAS CORROSION, SUPPORT TASK FCD 5300-01440. REMOVED AND REPLACED CLEAT IN FWD CARGO AT FRAME 29 BETWEEN 43R-44 IAW SRM 51-42-11-001 2(E).

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

FR52-56 CARGO DOOR THRESHOLD SHEET HAS AREAS OF CORROSION A3NB-5 3-4-6179. REMOVED AND REPLACED AFT CARGO DOOR SILL THRESHOLD COVER SHEET BETWEEN FRAME 52 AND FRAME 56 IAW SRM 51-42-11-001.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

AFT CABIN RT LONGERON FR69-FR70 HAS EVIDENCE OF CORROSION. REMOVED AND REPLACED AFT CABIN RT LONGERON / FRAME SUPPORT WEB BETWEEN FR 69-70 IAW SRM 51-42-11-001.

Part: SKIN — DENTED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

FUSELAGE EXTERNAL SKIN FR9 STR 20L, 21L HAS DENT, A3NB-53-4-6068 - AD RELATED TASK - 2015-05-02. REPAIRED FUSELAGE EXTERNAL SKIN AT FR9, STR 20L-21L IAW SRM 53-00-11-300-011, FIG 20115, SH1.

Part: FITTING — CRACKED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

RT KEELBEAM FWD ACTUATOR FITTING HAS A CRACK INDICATION IN HOLR E. R&R RT KEELBEAM FWD ACTUATOR FITTING IAW SRM 51-42-11- 001, SRM 51-48-00-001, 51-44-11-001, AND 53-1158.

Part: GUSSET — DAMAGED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

SEVERAL FASTNER HOLES FOR R2 DOOR FR66 INNER CAP JOINT GUSSET PLATES AT STRINGERS 10,12,14, AND 16 ARE VISUALLY OUT OF ROUND AND ALSO NEED TO BE DE-BURRED. (DISCREPANT HOLES ARE MARKED) A3NB-5 3-3-6354 GENERATED BY V061690 ON LCQ REF NR 9296642 STEP REAMED HOLES TO ROUND AND TRUE CONDITION IAW SRM 51-44 -11-001 FABRICATED 1EA GUSSET PLATE FOR STR16 IAW SRM 53-41 -69-001 INSTALLED FR66 STR16 GUSSET PLATE IAW SRM 51-42-11- 001

Part: GUSSET — DAMAGED (FUSELAGE) · airframe 78,949 hrs · 30,599 cycles

SEVERAL FASTENER HOLES FOR R2 DOOR FR68 INNER CAP JOINT GUSSET PLATES AT STRINGERS 10,12,14,AND 16 ARE VISUALLY OUT OF ROUND AND ALSO NEED TO BE DE-BURRED. (DESCREPANT HOLES ARE MARKED) A3NB-5 3-3-6354 GENERATED BY V061690 ON LCQ REF NR 9296643 STEP REAMED HOLES TO A ROUND AND TRUE CONDITION IAW SRM 51- 44-11-001, FABRICATED 1EA GUSSET PLATE FOR STR16 IAW SRM 53 -41-69-001, INSTALLED FR68 STR16 GUSSET PLATE IAW SRM 51-42 -11-001

Part: FITTING — CORRODED (GIRT BAR) · airframe 78,949 hrs · 30,599 cycles

MAIN CABIN L2 DOOR AFT LOWER CORNER AT GIRT BAR FITTING LOWER SI DE HAS CORROSION AT FASTENER HOLE (A3NB-53-3-6299) PER LCQ REF. NR 9296571 (22571 REMOVED AND REPLACED AFT LOWER CORNER FITTING ON L2 DOOR CUTOUT IAW SRM 51-72-11-911-002 AND SRM 51-42-11.

Part: FITTING — CORRODED (GIRT BAR) · airframe 78,949 hrs · 30,599 cycles

MAIN CABIN L2 DOOR FWD LOWER CORNER AT GIRT BAR FITTING UPPER SIDE HAS CORROSION (A3NB-53-3-6299) PER LCQ REF. NR 9296570 (22570) GENERATED BY V923923. REMOVED AND REPLACED L2 DOOR FWD LOWER CORNER FITTING IAW S RM 51-72-11-911-002 AND A320 SRM 51-42-11.

Part: FITTING — CORRODED (GIRT BAR) · airframe 78,949 hrs · 30,599 cycles

MAIN CABIN L2 DOOR AFT LOWER CORNER AT GIRT BAR FITTING UPPER SI DE HAS CORROSION SPEC NR A3NB-53-3-6299 GEN BY V923923. RMVD & RPLD L2 DOOR SILL IAW SRM 51-72-11-911-002 AND SRM 51-42- 11 AT LCQ.

Part: PIN — CORRODED (OVRWG DOOR LATCH) · airframe 77,098 hrs · 29,778 cycles

LEFT FWD EMERGENCY OVERWING HATCH DOOR LWR LATCH PIN CORRODED. REPLACED THE LATCH PIN.

Part: TERMINAL — FAULTY (CABIN) · airframe 74,925 hrs · 28,790 cycles

STRONG ELECTRICAL SMELL REPORTED BY INFLIGHT CREW THEN COFFEE MAKER M41, CHILLER C41, AND HOTPLATE H41 WENT INOP. REMOVED AND REPLACED TERMINAL LUG ON WIRE 2533-9031-8 AT THE M41 C/B (9010ML4). REF IFM AWM 25-33-03.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 74,018 hrs · 28,400 cycles

EMERGENCY LIGHT TEST FAILED. MSG EPSU AFT L RESETS NO HELP. NEEDS POWER UNIT AND BATTERY RPL'D. EPSU BATTERY AND UNIT REF AMM 33-51-38 GRD TEST NORM NO DEFECTS NOTED.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 46,668 hrs · 20,174 cycles

CABIN EMERGENCY LIGHTS CAME ON FOR 8 MINUTES. OCCURRED SAME TIME AS CABIN PRESSURIZED. GROUND CHECKED NORMAL

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 72,484 hrs · 27,675 cycles

TEST FAIL MESSAGE, EMERGENCY LIGHT. REPLACED THE BATTERY AND EPSU, OPS TESTED OK

Part: HYDRAULIC SYSTEM — LOW (GREEN SYSTEM) · airframe 67,917 hrs · 25,761 cycles

HYDRAULIC GREEN SYS LOW LEVEL DISPLAYED ON UPPER ECAM SCREEN. SERVICED HYDRAULICS IAW AMM 29-31-00-710-001-A. TAXI RUN ACCOMPLISHED, ALL NORMAL.

Part: CHARGER — MALFUNCTIONED (CABIN) · airframe 67,900 hrs · 25,754 cycles

EMERGENCY LIGHT SYS FAILED TEST. FAULTS ATA 33-51-38 BATTERY FED LT. RESET FWD CHARGING UNIT & SYS TESTED GOOD IAW MM 33-51-00.

Part: INDICATION SYS — MALFUNCTIONED (HYDRAULIC SYS) · airframe 64,790 hrs · 24,544 cycles

BLUE HYD SYS SD DISP SHOWS GREEN PSI DOWN STREAM OF PUMP WITH PUMP OFF.

Part: RESERVOIR — FAULTY (HYDRUALIC SYS) · airframe 64,761 hrs · 24,532 cycles

HYDRAULIC SYSTEMS G, B & Y WILL NOT PRESSURIZE WITH APU. APU WITH BLEED ON IN BOOST MODE WITH PACKS ON OR OFF NO PRESSURIZATION. SYSTEMS PRESSURIZE NORMAL WITH NR 1 ENGINE BLEED. REPLACED RESERVOIR PRESSURIZATION UNIT IAW MM, OPERATIONS CHECKED & LEAK CHECKED GOOD.

Part: SEAL — DAMAGED (LT AILERON) · airframe 64,598 hrs · 24,479 cycles

LEFT WING AILERON INBD BOTTOM SEAL MISSING 5 0R 6 INCHES OF SEALANT. A 3 INCH SECTION OF LOWER BLADE SEAL MISSING, NEEDS A NEW LOWER BLADE SEAL.

Part: WIRE HARNESS — SHORTED (NLG) · airframe 64,090 hrs · 24,294 cycles

LGCIU 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. FOUND WIRE A1009 IN UPPER HARNESS 1M SHORTED TO GROUND. REPLACED NLG HARNESS 1M IAW AMM. ACP NOSE GEAR LANDING, TAXI, TURNOFF LIGHT CHECKED GOOD, ALSO ACP NOSE GEAR WHEEL STEERING OPERATIONS & LGCIU 1 & 2 BITE TESTED GOOD.

Part: EXTINGUISHER — LOW PRESSURE (LAVATORY) · airframe 63,594 hrs · 24,098 cycles

FWD AFT LAVATORY FIRE EXTINGUISHER BOTTLE LOW IN THE RED BAND.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 63,435 hrs · 24,034 cycles

MULTIPLE DENTS ON LEFT INBOARD TRAILING EDGE FLAP. DENTS FILLED AND CURED.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 60,990 hrs · 23,044 cycles

MULTIPLE DENTS ON LEFT OTBD T/E FLAP. FILLED DENTS.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 63,435 hrs · 24,034 cycles

MULTIPLE DENTS ON RT INBD T/E FLAP. ALL DENTS FILLED AND CURED.

Part: SEAL — MISSING (RT AILERON) · airframe 63,136 hrs · 23,923 cycles

RT WING AILERON INNER UPPER SEALS MISSING 3 OR 4 INCHES AND LOWER SEAL A COUPLE OF INCHES. REPLACED UPPER AND LOWER SEALS.

Part: B-NUT — LEAKING (HYD SYSTEM) · airframe 62,922 hrs · 23,832 cycles

HYDRAULIC FLUID LEAKING FROM LEFT MLG. PUDDLE UNDER THE GEAR. FOUND B-NUT LOOSE ON LOWER BRAKE SERVO VALVE. SECURED B-NUT, NO LEAKS NOTED.

Part: SEAT — LOOSE (CABIN) · airframe 62,881 hrs · 23,815 cycles

ENTIRE ROW 37 DEF IS LOOSE AND WIGGLES. FOUND FWD INBD FOOT LOOSE. TIGHTENED FOOT. SEAT ASSY SECURE.

Part: EXHAUST DUCT — DAMAGED (NR 2 ENGINE) · airframe 62,767 hrs · 23,772 cycles

NR 2 ENGINE EXHAUST LEFT INBOARD SIDE OF THE FAN AIR DUCT (C-DUCT) HAS SOME LOOSE MESH MATERIAL. AREA OF DELAMINATION IS NEAR OF TRAILING EDGE OF THE C-DUCT. SQUARE INCG AREA OF DELAM IS APPROX 24 SQUARE INCH PER MT 78-010. LOOSE MATERIAL HAS BEEN REMOVED, SPEED TAPE APPLIED.

Part: NOSE COWL — DAMAGED (POSIT 2) · airframe 62,552 hrs · 23,693 cycles

FOUND EVIDENCE OF BIRD STRIKE AT GATE, RT NOSE COWL. DAMAGED AND LEADING EDGE PYLON PANEL DAMAGED. RT ENG RING COWL AT 10:0 0 HAS A DENT 18 INCH BY 8 INCH. NO SKIN TEAR DENT ONLY. REMOVED NOSE-AIR INTAKE COWL PER AMM 71-11-11-0401. STARTED TO INSTALL ROBBED NOSE COWL (PCN 170-3428), MR71212-014. BOLTS STARTED BUT NOT (PARTIAL). REPLACED NOSE COWL PER MM.

Part: WIRE — EXPOSED (SEAT 21D) · airframe 62,492 hrs · 23,669 cycles

21D HAS WIRES STICKING OUT OF ARMREST. SECURED IN SEAT ARM CAB

Part: NOSE COWL — DENTED (NR 2 ENGINE) · airframe 62,295 hrs · 23,578 cycles

NR 2 ENGINE HAS A THREE INCH DENT ON NOSE COWL AT APPROXIMATELY THE SEVEN O'CLOCK. INLET DENT AT 5:00, IS MAJOR AXIS IS 3.5", MINOR AXIS 1.75" DEPTH 0.25" NO CRACKS NOTED AT LEADING EDGE LIP SKIN, IN ZONE K1 AND J. DENT IS BEYOND LIMITS SRM 54-10-00, PG 105-106. DAMAGED AREA WAS COLD WORKED AND DAMAGE DIMENSIONS WERE REDUCED TO: MAJOR AXIS 3", MINOR 1" K1,D=.015" J,D=.093. HFEC IS SATISFACTORY IAW ECRA 5410-01 716 PART 2, NO DISCREPANCIES NOTED.

Part: INDICATOR — MISSING (L2 DOOR) · airframe 62,212 hrs · 23,547 cycles

F/A CANNOT DETERMINE IF DOOR 2L IS ARMED. COCKPIT INDICATION IS NORMAL. FOUND 2L SLIDE VISUAL ARMED AND DISARMED INDICATOR MISSING.

Part: STOWAGE BOX — FAULTY (COCKPIT) · airframe 61,859 hrs · 23,394 cycles

CAPT OXYGEN MASK WILL NOT TEST. REPLACED CAPT'S O2 BOX, NO LEAKS TEST OKAY.

Part: ACTUATOR — FAULTY (CABIN TEMP) · airframe 61,739 hrs · 23,350 cycles

PACK 2 ALL ZONES TEMPS VERY WARM ON DESCENT PACK 1 CURRENTLY ON DF FOR FCV. FOUND AFT CABIN TEMP SENSOR FILTER BLOCKED CLEANED BOTH MID AND AFT FILTER. PERFORMED CABIN TEMP CONTROL TEST, FAILED P2 RAM AIR OUT ACTUATOR, OPEN RIGHT PACK PANEL, CLEANED CONNECTOR ON ACTUATOR FAULT BECAME INTERMITTENT - REMOVED AND REPLACED P2 RAM AIR OUT ACTUATOR PER AMM 21-61-52-400-001. OP'S CHECK GOOD AT THIS TIME.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 61,739 hrs · 23,350 cycles

O2 MASKS FELL AGAIN AT SEATS 31ABC WHILE PASSENGERS WHERE BEING LOADED. SEATS PLACARD DO NOT OCCUPY AND O2 COMPARTMENT TAPE AS REQUIRED. -RDF-T :SEATS NUMBER IS ACTUALLY 27ABC. SEAT IS PLACARD DO NOT OCCUPY. RE-STOWED MASK CORRECTLY IN PLACE, AND RELATCH PANEL. OK TO CONTINUE.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 61,725 hrs · 23,342 cycles

PASSENGER SEAT OVERHEAD 02 MASK FELL AT 23DEF. COMPLIED WITH MT-35-003 NEED TO ACP PROP TEST ON OR BEFORE 3 DAYS MAX REF MT-35-003. ACP DROP CHECK PER MM 35-23-00 OPS OK.

Part: COUPLING — FAULTY (LT MLG) · airframe 61,446 hrs · 23,227 cycles

LEFT MAIN GEAR HAS DISCONNECTED HYDRAULIC LINE BRAKE QUICK DISCONNECT COUPLING: IPC 32-11-12-03B ITEM 10: PCN 110-1909. REPLACED LEFT GEAR BRAKE AFT QUICK DISCONNECT LINE SECURED.

Part: CONTROLLER — FAULTY (CABIN) · airframe 61,440 hrs · 23,225 cycles

WARM AIR IS STILL SUPPLIED TO FORWARD CABIN WITH RESPECTIVE ZONE TEMP CONTR IN FULL COLD. CLEAN AND TEST TEMP SENSORS (21HK AND 22HK). REPLACED 8HK ZONE CONT PER AMM 21-63-34. GND TEST OKAY.

Part: SEAT — LOOSE (CABIN) · airframe 61,196 hrs · 23,128 cycles

THE 32ABC WHOLE ROW IS LOOSE AND IS A ROCKER. SECURED SEAT IN TRACK.

Part: IDG — FAULTY (NR 2) · airframe 60,998 hrs · 23,048 cycles

AFTER GEAR EXTENSION ON APPROACH ALL CABIN LIGHTS FLICKERED UNTIL LANDING. REPLACED NR 2 IDG. LEAK CHECKED OPS CHECKED, DISCONNECTED, RECONNECTED & RAN NR 2 ENGINE SECOND TIME. ALL CABIN LIGHTS ARE GOOD.

Part: FLAP — DENTED (RT WING) · airframe 60,990 hrs · 23,044 cycles

MULTIPLE DENTS ON RIGHT INBOARD TRAILING EDGE FLAP. FOUND 7 DENTS ON FLAP. ALL DENTS ARE LESS THAN .118\ DEEP AND AND LESS THAN 1.575\ IN WIDTH. PER SRM 57-52-00 PAGE 137 OK TO FLY FOR 1000 FC BEFORE REPAIR NECESSARY. TAP TEST ACCOMPLISHED NO DELAMINATION FOUND.

Part: FLAP — DENTED (LT WING) · airframe 60,990 hrs · 23,044 cycles

MULTIPLE DENTS ON LEFT OUTBOARD TRAILING EDGE FLAP. FOUND 18 DENTS ON FLAP. ALL DENTS ARE LESS THAN .118\ IN DEPTH AND LESS THAN 1.575\ IN WIDTH PER SRM 57-53-00 PAGE 129 OK TO FLY FOR 1000 FC BEFORE REPAIR NECESSARY. TAP TEST ACCOMPLISHED NO DELAMINATION FOUND.

Part: FLAP — DENTED (LT WING) · airframe 60,990 hrs · 23,044 cycles

MULTIPLE DENTS ON LEFT INBOARD TRAILING EDGE FLAP. FOUND 16 DENTS ON FLAP. ALL DENTS ARE LESS THAN .118\ DEEP AND LESS THAN 1.575\ IN WIDTH. PER SRM 57-52-00 PG 137 OK TO FLY FOR 1000 FC BEFORE REPAIR REQUIRED. ACCOMPLISHED TAP TEST NO DELAMINATION FOUND.

Part: B-NUT — LOOSE (PTU) · airframe 60,848 hrs · 22,985 cycles

HYDRAULIC FLUID ON UNDERSIDE OF FUSELAGE ON AFT SIDE OF LEFT MAIN GEAR DOOR. CLEANED AREA TIGHTENED B-NUT ON TOP OF PTU, NO LEAKS FOUND.

Part: EEC — FAULTY (NR 1 ENGINE) · airframe 60,809 hrs · 22,968 cycles

ENG 1 REV FAULT, FLIGHT DIVERTED. REVERSER FAULT DISPLAYED ON UPPER ECAM SCREEN. ENG 1 CK ROOT FAULT PER AMM ON MCDU WITH FADEC SW ON GET CELL FAULT ACRONYM AND REPORT. ACP MCDU REVIEW AND POST FLT, FOUND FADEC 1A CELL 4 =REVXCW, CELL 3=REVLFF, FOUND FADEC1B CELL 4 REVXCW, CELL 3 REVLF. REPLACED NR 1 ENG EEC DUE TO PFR SHOWING BOTH REV LVDT CH A&B EEC1 FAILURE MSG. RPL EEC REF MM AND INSTALL. REF MM73-22-34-400-010-B. OPS CHK OK. RAN NR 1ENG REF JRH TWICE AND OPS CHK THRU MCDU 123419. OPS CHK OK CAT III PERFORMED.

Part: SKIN — DENTED (FUSELAGE) · airframe 60,511 hrs · 22,838 cycles

SMALL BUMPS-DAMAGE ON BODY JUST FWD OF DOOR 2L, FR 69 AND 70 STRINGERS 15 AND 16, TWO SMALL DENTS 1 INCH BY 1 INCH APPROX .050 DEPTH DOES NOT INVOLVE STRINGERS OR RIVETS. DENT WITHIN ALLOWABLE DAMAGE LIMITS OF SRM 53-41-11 DIAGRAM 101 SH3. DETAILED VISUAL INSPECTION ACCOMPLISHED PER GMM 06-35-05. NO CRACKS DETECTED.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 60,020 hrs · 22,644 cycles

'Y' HYD SYSTEM PRESSURE LOSS, FLIGHT DIVERTED. FOUND LEAKING O-RING AT YELLOW PTU MANIFOLD CHECK VALVE, REPLACED. FOUND METAL IN NR 2 ENG PUMP HP FILTER, CHANGED HP FILTER, LP FILTER, CASE DR FILTER AND EDP PER AMM.

Part: PACKING — LEAKING (WATER TANK) · airframe 59,192 hrs · 22,284 cycles

DEPARTED LAX WITH WATER AT 100 PERCENT. 2HR INTO FLT WATER AT 0 AND ONLY AIR FROM FAUCET - TANK DRAINED INTO BELLY OF FWD CARGO PIT PAST WATER OUTLET PLUMBING PACKINGS. REPLACED PACKINGS REF IPC 38-11-03. SERVICED WITH WATER BEYOND ONE QUARTER TANK CAPACITY. NO LEAKS.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,161 hrs · 22,274 cycles

R-2 THRESHOLD SILL HAS DEEP CORROSION ON 3 EACH FASTENERS HOLES. REPLACED R2 DOOR SILL.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 59,161 hrs · 22,274 cycles

MAJOR REPAIR. INSTALL DOUBLER AT FORMER LT ANTENNA LOCATION PER 4079C AND SRM 53-00-11 FIG 238. INSTALLED DOUBLER REPAIR. MUST BE RE-INSPECTED AT 60000C FROM REPAIR EMBODIMENT. CURRENT PTC 22274.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 59,161 hrs · 22,274 cycles

FORMER VERIZON ANTENNA LOCATION HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. MUST BE RE-INSPECTED AT 59900C PER S RI 53-00-11 TABLE 246. CURRENT PTC 22274.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,161 hrs · 22,274 cycles

FUSELAGE SKIN CORROSION AT WASTE TANK VENT FR 69-70 RT SIDE. MAJOR REPAIR ACCOMPLISHED. MAINT TEXT: INSTALLED REPAIR PER SRM. REQUIRES RE-INSPECTION PER SRI. INSTALLED DOUBLER REPAIR PER SRM. INSPECT AT 53900 PER REPAIR EMBODIMENT. CURRENT PTC 22274.

Part: THRUST REVERSER — DEBONDED (NR 1 ENGINE) · airframe 58,608 hrs · 22,014 cycles

NR 1 ENG RT REV HALF FWD EDGE HAS DISBONDED FROM 6 O'CLOCK TO 11 O'CLOCK, SHEETMETAL UNDER BLOCKER DOORS HAS TORN BACK APPROX 4\ DEEP FROM FWD EDGE. REPLACED NR 1 ENG INBOARD REV HALF PER MM WITH UNIT ROBBED FROM AC 4628.

Part: RELAY — FAULTY (ELECTRICAL SYS) · airframe 57,814 hrs · 21,677 cycles

EMERGENCY GENERATOR FAILED THE EQ3333 TEST. REPLACED RELAYS 12XE AND 20. REPLACED NR 3 TR BAD FROM STOCK, RE-INSTALLED ORIGINAL. FOUND RELAY 17XE CONTACTS A2 TO A3 REMAINS OPEN WHEN DE-ENERGIZED. REPLACED RELAY 17XE - OPS CHECKS GOOD.

Part: COMPUTER — FAULTY (ELEVATOR SYS) · airframe 57,685 hrs · 21,613 cycles

ELAC2 ELAC FAULT. RESET OK. CHRONIC. REPLACED ELAC 2 AND CAT III AUTOLAND TEST PER MM. ALL TESTS OKAY.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 57,085 hrs · 21,354 cycles

FWD CARGO PIT DOOR HANDLE MOUNTING FITTING CRACKED AT FWD EDGE. ACCOMPLISHED HFEC 3EA CRACKS MARKED ENDS. REPAIRED PER UAL EVA 809-02.

Part: MECHANISM — FAULTY (CARGO DOOR) · airframe 57,010 hrs · 21,321 cycles

AFT CARGO DOOR HANDLE WILL NOT ROTATE TO CLOSE. SAMC TEXT: CONTACT SAMC, DOOR HANDLE CRACKED AT PIVOT AREA. REPLACE DOOR LOCK HANDLE PER MM. REMOVED AND INSTALLED NEW HANDLE MECHANISM D5237130100651 PER AMM. AFT CARGO DOOR HANDLE MECHANISM HAS SET SCREW MISSING (AN565FC1032H8, NUT PCN 750-5493 AND TAB WASHER 756-1119). INSTALLED A SCREW AND JAMB NUT AS AN INTERIM REPAIR AND ADJUSTED. PLACED PAC ORDER FOR SET SCREW ON V5608. 40 EA AN565FC1032 IN HB 1 OSTF C4513 MAY 27 11. 2EA PN AN565FC1032H OSTF C 5538 MOVED TO SFRJL. INSTALLED NEW SET SCREW, WASHER AND NUT. CHECKED RIG. OP CHECKS GOOD.

Part: SERVO VALVE — FAULTY (SPOILER) · airframe 56,769 hrs · 21,219 cycles

SPOILER FAULT DISPLAYED ON UPPER ECAM SCREEN. F-CTL CREW COMMENTS: NR 1 SPLR BOTH SIDES INDICATES AMBER RETRACTED. REPLACED SERVO VALVE FOR NR 1 SERVO CONTROL. OP CHECKS GOOD, NO LEAKS.

Part: OXYGEN MASK — OUT OF POSITION (CABIN) · airframe 56,549 hrs · 21,107 cycles

O2 MASK HANGING AT 11D. SEATS 12DEF INOP DUE TO O2 MASK DOWN AT SEAT 12D. ACP TEST PER MM. RAN TEST PER AMM. NO DEFECTS NOTED, RETURNED SEATS TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,337 hrs · 21,004 cycles

EMERGENCY LIGHT TEST FAILS, FAULTING FWD L INT LOADS AND FWD L EXT LOADS. REPLACED POWER SUPPLY AND BATTERY PER MM 33-51- 58. NO HELP. FOUND BAD LAMPS IN FWD ENTRY DOOR LIGHT 21WL. RELAMPED PER MM 33-51-11. TEST NORMAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,530 hrs · 20,617 cycles

DURING EMERGENCY LIGHT TEST FAULTING INT LOADS FWD LT AND FWD. EPSU FAULTING INTERIOR AND EXTERIOR LIGHTS AND BOTH ARE BLINKING. DOOR 1L ESCAPE SLIDE CAN ONLY BE USED DURING DAYLIGHT OPERATIONS DUE TO EMERGENCY LIGHT INOP. REPLACED 1L EPSU 10WL AND BATTERY. FOUND LIGHT BULB MESSAGE AT L2 DOOR. REPLACED BULB, TESTS OKAY.

Part: GROUNDING STRAP — LOOSE (GALLEY) · airframe 55,302 hrs · 20,516 cycles

ELECTRIC SHOCK FELT IN GALLEY WHEN ELEC PWR IS TRANSFERRED. ENTIRE GALLEY HAS BEEN HAS BEEN ELECTRICALLY DEACTIVATED. NO SHOCK NOTICED WHEN TRANSFERRING POWER. NEED TO CHECK THE GALLEY ELECTRICAL BONDING AND GROUNDING. FOUND POOR ELECTRICAL BONDING BETWEEN G1 COUNTERTOP AND AC STRUCTURE (114 KILOHMS). REMOVED OVENS AND FOUND LOOSE BONDING STRAP. SECURED STRAP AND CLEANED OVERHEAD GROUNDING CONNECTIONS AND SECURED 106589 OVERHEAD GROUNDS. REINSTALLED OVENS AND REACTIVATED GALLEYS G1 AND G2. RESISTANCE BETWEEN GALLEY BONDING POINTS, GALLEY COUNTER TOPS AND AIRCRAFT STRUCTURE ALL CHECKS WITHIN LIMITS.

Part: BEARING — MIGRATED (LT WING TE FLAP) · airframe 55,227 hrs · 20,479 cycles

LEFT INBD FLAP CARRIAGE SPHERICAL BUSHING IS MIGRATING OUT OF FITTING. REMOVED ECCENTRIC BUSHING & HARDWEAR. LT NR 1 FLAP TRACK CARRIAGE AFT END STOP PLATE REMOVED. STARTED REMOVING FLAP TRACK ATTACH BOLTS. COMPLETED REMOVAL AND REPLACEMENT OF BEARING.

Part: LIGHT — MALFUNCTIONED (LAVATORY) · airframe 55,134 hrs · 20,430 cycles

FOUND OVERHEAD PANEL CB H-7 POPPED, RESET & CB POPPED AGAIN, IT'S EMERGENCY LIGHT BREAKER. REPLACED DOME AND AUX LIGHT ASSY AT LAV 'A', OPS CHECKED OK.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 54,505 hrs · 20,137 cycles

CREW REPORTED EMERGENCY EXIT LIGHT ABOVE DOOR 2L INOP. PERFORM EMERGENCY LIGHT POWER SUPPLY TEST. FOUND CONNECTION ON BACK OF SIGN, LOOSE. SECURED, ACCOMPLISHED EMERGENCY LIGHT TEST, LIGHT OPS NORMALLY.

Part: WIRE — CHAFED (FIRE SUPPRESSION) · airframe 53,588 hrs · 19,720 cycles

ENG 2, AGENT 1, DISCHARGE LIGHT FLICKERS ON AND OFF. REPLACED CHAFED WIRES IN J -BOX IN ENG PYLON FROM BOTTLE PRESS SWITCH TO GROUND AND J-BOX DISC ALL GROUND TEST OK.

Part: PANEL — FAULTY (COCKPIT) · airframe 53,568 hrs · 19,714 cycles

NUMBER 2 ENGINE AGENT 1 DISCHARGE LIGHT IS FLASHING INTERMITTENTLY. NO ECAM MESSAGE. REPLACED ENGINE AND APU FIRE PANEL, OPS NORMAL.

Part: SERVO — OUT OF LIMITS (RUDDER) · airframe 53,387 hrs · 19,631 cycles

AIRFRAME SHUDDER/VIBRATION, RTFL CREW PLEASE COMPLETE VIBRATION REPORT LOCATED IN FLT DECK. FOUND RUDDER SERVO AND ROD END GREEN SYS OUT OF LIMITS. REPLACED. FOUND RUDDER RIG OUT OF LIMITS. RIGGED. REPLACED GREEN SYS YAW DAMPENER AND NR 1 FAC . FLUSHED GREEN SYS HYD.

Part: TOILET — FULL (AFT LAVATORY) · airframe 52,490 hrs · 19,164 cycles

DUE TO WATER LEAK FROM AFT LAV,CARPET IN AFT SECTION OF LAST ROW NEEDS TO BE CLEANED. FOUND TOILET BOWL FULL OF WATER, REMOVED WATER & CLEANED UP AFT LAV. SHUT OFF WATER VALVE & REMOVED AFT PANEL IN AFT PIT NO LEAK FOUND. RPL'D PANEL. ACTIVATED WATER SYS. REMOVED TOILET SHROUD AND CABINET DOORS AND CHECKED FOR LEAKS WITH NO FINDINGS. TOILET OPERATION NORMAL. FOUND COFFEEMAKER DRAIN PACKED WITH GROUNDS AND FULL OF WATER. CLEANED AND VERIFIED FLOW OUT DRAIN MAST. SHAMPOO AND CLEAN UP ACPD BY CLEANERS. OK FOR SVC.

Part: ACTUATOR — FAULTED (HYD SYSTEM) · airframe 52,328 hrs · 19,073 cycles

NR 2 ENG FIRE SHUTOFF VALVE FAILS TO CLOSE WITH FIRE SWITCH OUT. REPLACED NR 2 ENG HYD VALVE ACTUATOR, OPS CHECKS NORMAL.

Part: DAMPER — DEFECTIVE (L1 DOOR) · airframe 52,031 hrs · 18,928 cycles

NEED TO REPLACE THE 1L DOOR DAMPER AND EMERGENCY OPERATION CYLINDER DUE TO DOOR BINDING WHEN OPENED. REPLACED DAMPER.

Part: LIGHT — BROKEN (SEAT 22) · airframe 50,604 hrs · 18,310 cycles

EMERGENCY LIGHT AT SEAT 22 INOP. REPLACED LIGHT ASSY, OPS CHECKED OKAY.

Part: OVEN — DEFECTIVE (GALLEY) · airframe 50,066 hrs · 18,100 cycles

DIVERTED TO DEN DUE TO CIRCUIT BREAKER FOR AFT GALLEY TRIPPING OFF. AFT GALLEY TRIPPING OFF. FLIGHT DIVERTED. FOUND ON INSPECTION BRACKET THAT HOLDS BUS PLUG 9025ML4 PULLED OUT FROM WALL. SUSPECT IT IS THE CAUSE OF TRIPPED BREAKER. REPAIRED BRACKET FOR OVEN RECEPTICLE. STILL NEEDS OVEN REPLACEMENT. REPLACED OVEN ASSY, RAN OVEN FOR 30 MIN, BREAKER DID NOT TRIP.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 49,566 hrs · 17,892 cycles

F/O'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). REPLACED MASK AND STOW BIN.

Part: OXYGEN BOTTLE — LOW PRESSURE (COCKPIT) · airframe 49,508 hrs · 17,866 cycles

COCKPIT OXYGEN BOTTLE - LOW. SERVICED TO NORMAL, WAS 1240 PSI.

Part: UNKNOWN — ODOR (CABIN) · airframe 48,578 hrs · 17,481 cycles

NEAR ROW 6, ELECTRICAL ODOR AND HAZE REPORTED IN AREA. NEED TO INVESTIGATE FOR SOURCE. PERFORMED INSPECTION, FOUND NO EVIDENCE OF ELECTRICAL BURNING. REMOVED AND INSTALLED PANELS IN CABIN AROUND ROW SIX. PERFORMED INSPECTION. CKD CEILING AT ROWS 5-6-7, ALL NORMAL. FOUND NO EVIDENCE OF ELECTRICAL BURNING. NO OIL CONTAMINATION FOUND INSIDE OR OUTSIDE APU BLEED DUCTS, APU INLET, NO OIL LEAKS. RAN NR 1 & 2 ENGS ISOLATED WITH BLDS & ELECTRICS, ALL NORMAL. CHECKED ALL E&E COMPTS NO ABNORMALITIES, CHECKED ENG INLETS & EXHAUST, NO OIL PRESENT. CHECKED GEN TIE BREAKERS DURING SWITCH OVER WITH ENGS, ALL OK. INBOUND FLT CREW REPORTED NO ABNORMAL ODORS DURING PREV FLT. WILL CONTINUE TO MONITOR. NFF.

Part: BOTTLE — LOW (OXYGEN SYS) · airframe 48,107 hrs · 17,312 cycles

LARGE O2 BOTTLE AT 2R PRESS IS LOW.

Part: TRANSMITTER — FAULTY (NR 2 ENGINE) · airframe 47,415 hrs · 17,075 cycles

NR 2 ENG OIL QUANTITY LOW INDICATION, RTFL. INCORRECT INDICATION ISSUE. REPLACED NR 2 ENGINE OIL QUANTITY TRANSMITTER, ACCOMPLISHED ENGINE RUN. NO LEAKS NOTED.

Part: LANYARD — OUT OF POSITION (EVAC SLIDE) · airframe 46,961 hrs · 16,913 cycles

NO LANYARD VISIBLE ALL 4 DOOR SLIDES. REPOSITIONED LANYARD ON AL L SLIDES, OK FOR SERVICE.

Part: SMOKE DETECTOR — NO TEST (CARGO BAY) · airframe 46,030 hrs · 16,588 cycles

FAILED CARGO SMOKE TEST. IMPROPER TEST METHOD PER AMM. REPEATED TEST AND PASSED.

Part: BLADES — BENT (RAM AIR TURB) · airframe 45,906 hrs · 16,550 cycles

RAM AIR TURBINE BLADE BENT DURING RAT CHECK. ACCIDENTAL DAMAGE TO RAT BLADES. REPLACED THE RAT ASSY, ALL OPS CHECKS ACCOMLISHED.

Part: CONTROL PANEL — FAULTY (EMERGENCY LIGHTS) · airframe 45,004 hrs · 16,211 cycles

AFT ATTND PANEL, EMERGENCY LIGHT SWITCH IS INOP. SWITCH WILL NOT STAY ON. FOUND SWITCH IS FAULTY. REPLACED ATTEND PANEL CONTROL.

Part: FIRE LOOP — FAULTY (NR 2 ENGINE) · airframe 44,453 hrs · 15,997 cycles

ENG 2 FIRE LOOP -A- FAULT ECAM. NR 2 ENG PYLON LOOP A 3WD2 FAILS. REPLACED NR 2 ENG PYLON LOOP A 3WD2.

Part: OVEN — ODOR (RIGHT) · airframe 44,184 hrs · 15,900 cycles

AFT RIGHT OVEN HAS ELECTRICAL ODOR. ODOR WENT AWAY AFTER LANDING AND NEVER RETURNED. ALL VISUAL CHECKS OF COMPONENTS COMPLETED, NO UNUSUAL DEFECTS DEFECTS. NO REPEATS SINCE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 43,107 hrs · 15,525 cycles

EEL LIGHT TEST FAIL: -BATTERY FWD LT. REPLACED EEL LIGHT BATTERY AT DOOR 1L. TESTS NORMALLY NOW.

Part: LEVER — FAULTY (R2 DOOR) · airframe 42,417 hrs · 15,266 cycles

DOOR 2R ARM LEVER WON'T GO ALL THE WAY DOWN WHEN IN THE ARMED POSITION. [SUP 05-08-07] LOOSE EMERGENCY SLIDE COVER WAS INTERFERING WITH MOTION OF DOOR LEVER. FULL MOTION RESTORED AFTER SLIDE COVER WAS SECURED.

Part: STALL WARNING — ACTIVATED (COCKPIT) · airframe 42,320 hrs · 15,232 cycles

NR 1 ENG STALL DISPLAYED ON UPPER ECAM SCREEN DURING STEADY STATE CLIMB OR CRUISE. ENGINE NOT SHUTDOWN. PERFORMED FUNCTIONAL CHECK OF 7TH AND 10TH STAGE HPC VALVES. FOUND 7TH STAGE B AND C VALVES STUCK. REPLACED 7TH STAGE HPC. FADEC INTERROGATION REPORT REFLECTS VSV MECH BLD VLV LPC1 LATCHED. PERFORMED BORO INSPECTION OF HPC STG 3 AND 6 ON NR 1 ENGINE. NO DEFECTS NOTED.

Part: UNKNOWN — WARNING LIGHT (E/E BAY) · airframe 41,034 hrs · 14,762 cycles

AVIONICS SMOKE MESSAGE ON ECAM. INSPECTED AIRCRAFT, AVIONICS BAYS, NO SMOKE FOUND. NO DEFECTS NOTED ON AVIONICS SYSTEM. NO FAULTS FOUND ON CFDS. AVIONICS SMOKE DETECTOR CLEAN. REPLACED AVIONIC EQUIPMENT VENTILATION COMPUTER.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,717 hrs · 14,645 cycles

DURING CIDS CHECK GOT MESSAGE, ATA 33-51-38 BATTERY EMERGENCY LIGHT. REPLACED BATTERY ON EPSU AT MID CABIN. CHECKED OK.

Part: BOTTLE — DISCHARGED (DOOR 1R SLIDE) · airframe 37,712 hrs · 13,532 cycles

DOOR 1R ESCAPE SLIDE BOTTLE INDICATION OUT OF GREEN BAND. THE SLIDE (MR25611-1055) HAD BEEN REMOVED FROM ACFT 4622 WITH A WRITE-UP STATING THAT BOTTLE PRESS NEEDLE WAS IN "RED BAND". HOWEVER, THE SHOP INSPECTION REVEALED THAT THE BOTTLE WAS IN THE "GREEN BAND". TEMP HAD NOT STABILIZED BEFORE READING (AMM 26-62-00, PG-604). PERHAPS MECH DECISION TO REPLACE COULD BE DUE TO NOT ENOUGH GROUND TIME TO LET THE BOTTLE TEMP TO STABILIZE, AS INDICATED ON I & R TAG MECH COMMENT, "LOW PRESS PREVENT DELAY AT DEPARTURE."

Part: BATTERY PACK — INOPERATIVE (SEATS 1C-6C) · airframe 36,881 hrs · 13,227 cycles

SEATS 1C-6C FLOOR PROXIMITY EMERGENCY ESCAPE PATH SYSTEM LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK.

Part: INSERT — MISSING (EVAC SLIDE) · airframe 35,186 hrs · 12,610 cycles

LT OFFWING SLIDE, METAL INSERTS IN ENCLOSURE FOR MOUNTING STUDS ARE MISSING IN 4 HOLES, ALLOWING MOUNTING STUDS TO CRUSH ENCLOSURE AGAINST MOUNTING PLATE. INSERTS COULD GET FOULED UP AND GETTING LOST DURING ENCLOSURE REMOVAL AND/OR TRANSPORT. THE SHOP DOCUMENT (CE-40-25-61-01-JD AND OEM CMM) REQUIRE THE SHOP TO PROVIDE THESE EXPENDABLE HARDWARE. THE REPAIR LIMITS ARE ALSO SPECIFIED IN THE CMM.

Part: SKIN — DENTED (FUSELAGE) · airframe 34,248 hrs · 12,264 cycles

THREE DENTS ALONG RIGHT SIDE OF NOSE WHEEL OPENING FROM CONTACT WITH GROUND EQUIPMENT. DOUBLER AND TRIPLER INSTALLED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,666 hrs · 10,891 cycles

ROWS 21ABC AND 19ABC EEL LIGHTS ARE INOPERATIVE. REPLACED EEL LIGHTS.

Part: DAMPER — LEAKING (NR 1 YAW) · airframe 29,064 hrs · 10,263 cycles

LANDED UNDER AMBER ALERT DUE TO A GREEN HYDRAULIC SYSTEM INDICATION AND LOSS OF QUANTITY. YAW DAMPER NR 1 WAS FOUND LEAKING. UNIT WAS REPLACED.

Part: HEATER — FAILED (GALLEY WATER) · airframe 19,420 hrs · 6,742 cycles

CREW REPORTS SMOKE DETECTOR ALARM SOUNDING CONTINUOUSLY WITH NO ELECTRONIC CENTRALIZED AIRCRAFT MONITORING SMOKE WARNING. *S/D* REPLACED HOT WATER HEATER.

Part: VALVE — INTERMITTENT (PARKING BRAKE)

ON ARRIVAL TO MEX, CAPTAIN SET PARKING BRAKE AND IT FAILED. AIRCRAFT ROLLED ABOUT 20 FEET BEFORE CAPTAIN WAS ABLE TO APPLY BRAKES. AIRCRAFT CONTACTED JETWAY AT THE LEFT ENGINE COWL. *S/D* PERFORMED AN OPERATIONAL TEST OF THE PARKING BRAKE SYSTEM PER AMM TASK 32-45-00-710-001. FOUND PARKING BRAKE VALVE (72GG) TO BE INTERMITTENT. REPLACED VALVE AND OPS CHECK WAS NORMAL. TAXI TEST OF AIRCRAFT SHOWED BRAKE SYSTEM TO FUNCTION NORMALLY.

Part: STRUCTURE — VIBRATION (AIRFRAME)

AIRCRAFT EXPERIENCED EXCESSIVE LOW FREQUENCY VIBRATION DURING CLIMB. DIVERTED TO LAS. AMBER ALERT, OVERWEIGHT LANDING.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN)

LOST CABIN PRESSURE AT FL350. EXECUTED EMERGENCY DESCENT AND REGAINED CONTROL OF CABIN IN MANUAL MODE. *S/D* ELECTRONIC BOX NR 1 FAILED ON OUTFLOW VALVE DRIVING THE VALVE OPEN. REPLACED OUTFLOW VALVE AND OPERATIONALLY CHECKED NORMAL.