N475UA

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 70,028 hrs · 30,819 cycles

FOUND AFT EMERGENCY LIGHT INOPERATIVE, SEAT 27 ABC. R & R THE EMERGENCY LIGHT ASSY IAW AMM 33-51-19-000-002-A, & 33-51-19-400-002-A. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 70,028 hrs · 30,819 cycles

FOUND SEAT 30ABC EMERGENCY LIGHT INOPERATIVE. R & R ROW 30 EMERGENCY LIGHT ASSY IAW AMM 33-51-19-000-002-A, & AMM 33-51-19-400-002-A. OPS CHECKS GOOD.

Part: LIGHT — BROKEN (ZONE 200) · airframe 70,028 hrs · 30,819 cycles

FOUND ROW 32 EMERGENCY SEAT LIGHT BROKEN OFF. R & R THE EMERGENCY LIGHT ASSY IAW AMM 33-51-19-000-002-A, & AMM 33-51-19-400-002-A. OPS CHECKED GOOD.

Part: LIGHT — BROKEN (ZONE 200) · airframe 70,028 hrs · 30,819 cycles

FOUND FWD EMERGENCY LIGHT INOPERATIVE, SEAT 25 ABC. R & R THE EMERGENCY LIGHT ASSY IAW AMM 33-51-19-000-002-A, & 33-51-19-400-002-A. OPS CHECKED GOOD.

Part: POWER SUPPLY — FAULTED (ZONE 200) · airframe 69,915 hrs · 30,767 cycles

AFT EMERGENCY LIGHTS WOULD RANDOMLY FLICKER ON & OFF. R&E CHANGING BATTERY AND CHARGER AT THIS TIME. ACFT INBOUND CREW REPORTED THAT AFT EMERGECY LIGHT WOULD BLINK OFF & ON, & THEN BACK OFF AT ABOUT THE TIME OF DISARMING THE DOORS DID NOT SEE ANY BLINKING DURING FLIGHT. EPLACED 13WL EPSU AND BATTERY REF AMM

Part: WIRE SPLICE — DAMAGED (ZONE 200) · airframe 68,906 hrs · 30,237 cycles

PROCEDURE - AFTER DOING CABIN EMERGENCY LIGHTING TEST, FAULT INDICATED EPSU INT LOAD EMER L. EMERGENCY LIGHTS INOP FROM SEAT ROW 26- 28. BITE TEST EMER L PWR SUPPLY, SHOWED SHORT IN LIGHTING SYSTEM. AT ROW 27ABC, FOUND DAMAGED SPLICE AT FLOOR-TO-SEAT CONNECTOR. REMOVED SPLICES & REPINNED MATE-N-LOK CONNECTOR. REF ESPM 20-48-14-01. EMERGENCY LIGHTING SYSTEM OPS CK'D NORMAL.

Part: LIGHT — NO DISCREPANCY (ZONE 200) · airframe 68,719 hrs · 30,141 cycles

REMOVED RH EMERGENCY EXIT PATH TO FOM IN REF TO AMM TASK 52-21-11-000-001-A. FOLLOWED RSC IN REF TO GMM 02-30-25. INSTALLED RH AFT OVERWING HATCH IN REF TO AMM TASK 52-21-11-400-001-A.

Part: SLIDE — NO DISCREPANCY (ZONE 800) · airframe 68,281 hrs · 29,905 cycles

RQST INSPECTION OF DOOR 2L SLIDE PX INSPECTED DOOR 2L SLIDE PRESSURE GUAGE, PRESSURE IN LIMITS. REF AMM 25-62-00/601

Part: FUEL CAP — MISSING (REFUEL COUPLING) · airframe 65,643 hrs · 28,662 cycles

PDA 2 CHS REPORTED MISSING FUEL CAP POST FLIGHT 1573. FUEL CAP CDL''D. NOTIFIED BUY STATION OPS FUEL CAP MISSING. DEFERRED PER CDL, VERIFIED NO LEAKS, INSTALLED INOP STICKER ADJ TO REG NUMBER IN COCKPIT. REPLACED REFUEL/DEFUEL COUPLING CAP PER A320 AMM 28-25-41.

Part: SKIN — DAMAGED (RH WING SLAT) · airframe 65,591 hrs · 28,635 cycles

UPON OKAY TO CLOSE, FOUND RIGHT WING SLAT NO.3, HAS DAMAGE TO THE I/B TRAILING EDGE. REPAIRED RIGHT WING SLAT NO.3 I/B TRAILING EDGE AS PER REF A320 SRM 57-44-21-300-001 FIG 2 PG8. INSPECTED PER SRM 57-44-21 SEE AMES NON ROUTINE FOR WORK ACCOMPLISHED.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 65,591 hrs · 28,635 cycles

DURING OPS TEST OF CABIN EMERGENCY LIGHTS EPSU ARME/ON EMER R&L FAILS ON PTP PANEL.REF TO PEMCO R 15100.0020 REMOVED AND REPLACED EPSU11WR AND 12WL. OPS CHECK GOOD IAW A320 AMM33-51-38. REMOVED AND REPLACED EPSU 11WL (BAD FROM STOCK) AN 12WL. OPS CHE CK GOOD. IAW A320 AMM 33-51-38.

Part: UNKNOWN — MISSING (LEFT WING) · airframe 64,213 hrs · 27,982 cycles

PDA 2 SCREW MISSING FROM LEFT WING RUB STRIP SCREW WAS CLASS 2PDA

Part: ENGINE — SLOW (NR 2) · airframe 64,025 hrs · 27,889 cycles

ON T/O ROLL..THR LEVERS SET TO FLX SETTING..ENG1 WENT TO PROPER EPR 1.46..ENG 2 WENT TO..CONT. . PERFORMED TEST 11 HIGH POWER ASSURANCE TEST ON #2 ENG. ALL ENGINE PARAMETERS WITHIN LIMITS REF AMM 71-00-00-710-013C. A/C OKAY FOR SERVICE. ADD EMP:U246551

Part: BATTERY PACK — NO TEST (AFT EPSU BATTERY) · airframe 62,568 hrs · 27,197 cycles

CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - MOST AFT EPSU BAT FAILED TEST REMOVED AND REPLACED EPSU BAT, OPS TST GOOD.

Part: INTERCOSTAL — CRACKED (FR16LH) · airframe 60,107 hrs · 26,009 cycles

(AD 2019-20-10) FR 16 LH DOOR STOP #7 FITTING FRAME HOLES UPPER AND LOWER I/B HOLES HAVE CRACK INDICATIONS. HOLES CIRCLED IN RED . REPAIR BEFORE NEXT FLIGHT PER EA 5311-02164. () TRANSFERRED TO ELB 809638, REF THIS LOG FOR WORK ACCOMPLISHED

Part: FRAME — CRACKED (LHFR35STR30) · airframe 60,107 hrs · 26,009 cycles

(AD2016-14-03) (WORK TRANSFERRED FROM NR''S 0020546, 0020547, 002 0547) DURING ROTO PROBE INSPECTION OF LH FR35 STRG 30. CRACK IND ICATIONS NOTED IN IN HOLES #1, #2 & #3. () ERROR IN DISCREPANCY GENERATED NEW ELB 8082931 FOR REPAIR

Part: FRAME — CRACKED (FR35STR30) · airframe 60,107 hrs · 26,009 cycles

(AD2016-14-03) DURING ROTO PROBE OF FRAME 35 STRG 30 FOUND DAMAG E INDICATION IN HOLE #2 AND #1 PERFORM AN INSPECTION PER PART 2 OF LATEST REVISION OF ECRA 5310 -07982"REF VT MAE NRC 0020638 FOR WORK PERFORMED. REPAIRED DAMAGE HOLES AT FR35 STRG 30 ASS PER ECRA 5310-07982, G ENERATING DIP PER STAEP 8 OF ECRA FOR "ON OR BEFORE AUG 10, 2022 ADD DIP 53-DIP DISCREPANCY NOT WRITTEN UP TO INCLUDE ALL DAMAGED HOLES. CANNOT IDENTIFY AIRCRAFT DAMAGE ON AN ECRA, MUST BE IN LOGBOOK. (HOLES 5, 9, 18). DOES NOT CONTAIN THE STATEMENT "INTERIM REPAIR ACP''D PER PART 1 OF ECRA.....". CONTAINS A CURSE WORD. L/P WRITTEN WITH ERRORS, GENERATED NEW ELB 8082404

Part: PLATE — CORRODED (LH O/B MAINTANK) · airframe 60,107 hrs · 26,009 cycles

(SUPPORT TASK) FOUND CORROSION ON TOP OF LH OUTBOARD MAIN TANK ( BETWEEN LH LONGERON Y1292 AND LH BULKHEAD) FORWARD OF FRAME 42 N EXT TO APU FUEL PUMP. () ACCOMPLISHED REPAIR OF LH O/B MAIN TANK PER FINAL EA 320-5711-13 -A2789 AND UAL EC/RA 5711-01168. ACCOMPLISHED BY EMP#V933438 AT BFM ST AEROSPACE MOBILE. NR#0020386

Part: INTERCOSTAL — CRACKED (FR16RH) · airframe 60,107 hrs · 26,009 cycles

(AD 2019-20-10) FR16 RH DOOR STOP FITTING FRAME HOLES, FITTING # 7 UPPER AND LOWER I/B HOLES HAVE CRACK INDICATIONS. HOLES CIRCLE D IN RED. REPAIR BEFORE NEXT FLIGHT PER EA 5311-02164.() TRANSFERRED TO ELB 809638, REF THIS LOG FOR WORK ACCOMPLISHED

Part: INTERCOSTAL — CRACKED (FR16) · airframe 60,107 hrs · 26,009 cycles

(AD 2019-20-10) FR 16 RH DOOR STOP FITTING FRAME HOLES. FITTING #1, LOWER I/B HOLE HAS CRACK INDICATIONS. HOLE CIRCLED IN RED. R EPAIR BEFORE NEXT FLIGHT PER EA 5311-02164. () TRANSFERRED TO ELB 809638, REF THIS LOG FOR WORK ACCOMPLISHED

Part: FRAME — CRACKED (RH FR16) · airframe 60,107 hrs · 26,009 cycles

(AD2020-20-05) WORK TRANSFERRED FROM 0020428, 0020429) DURING RO TO PROBE OF RH FR16 DOUBLE JOGGLE CRACK INDICATION NOTED IN HBOL ES #7 & #A. DAMAGE INDICATIONS ALSO NOTED IN HOLES #4 & #19. ALL 4 INDICATIONS NOTED ON 1ST & 2ND LAYER LOOKING O/B. REPAIRED RH FR16 DOUBLE JOGGLE IN 7,A,4 BY OVERFSIZING IAW EC/RA 5311-02763, HOLE #4 FOUND TO BE FALSE INDICATIONS AFTER CLEANIN G. ACCOMPLISHED BY

Part: FRAME — CRACKED (FR35-36) · airframe 60,107 hrs · 26,009 cycles

(AD 2018-06-04) R/H SIDE PRESSURE PANEL BTWN FR35-FR36 HAS 1 HOL E OUTSIDE THE ALLOWABLE CUT-OUT AREA THAT HAS A CRACK INDICATION DOT 07-183" CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS AND REPA IR BEFORE NEXT FLIGHT. TRANFERED ALL MX ACTIONS TO LP8088915

Part: FRAME — CRACKED (PRESSURE PANEL) · airframe 60,107 hrs · 26,009 cycles

(AD 2018-06-04) LH SIDE 4 FASTENERS HOLES ON THE PRESSURE PANEL OUTSIDE THE ALLOWABLE CUTOUT AREA HAVE CRACK INDICATIONS AND THE MIDDLE HOLE ON THE O/B BRACKET UNDER THE PRESSURE PANEL IS DAMAG ED DOTS 07-182 "CONTACT. TRANFERED ALL MX ACTIONS TO LP8088915

Part: NONE — CRACKED (FR68) · airframe 60,107 hrs · 26,009 cycles

(SUPPORT TASK) LH AFT DOOR FR68 DOOR STOP FITTING #1 I/B LOWER H OLE HAS A CRACK INDICATION, HOLE IS CIRCLED IN BLACK, NEEDS TOBE REPAIRED BEFORE NEXT FLIGHT. () NOTED IAW NTM 51-10-01, INSTALLED FREEZE PLUG. REINSTALLED #1 FROM TIME OF ADL/REPAIR EMBODIMENT 37900 FC (FH NOT RELEVANT) METHOD HFEC (REFER TO NTM 51-10-08) IAW SRI 53-41-12-205-010. DOOR FITTING IAW SRM 52-13-31-400-002-A. INSPECTION THRESHOLD SUBSEQUENT INSP AT INTERVALS 5300 FC (FH NOT RELEVANT) INSP REF VT MAE NRC 0020526 FOR WORK PERFORMED. REPAIRED LH AFT FR 68 DOORSTOP FITTING #1 I/B LOWER (D1), IAW SRM 53-41-12-300-011. HOLE REAMED FINAL TO 0.6920" NO CRACKS OK TO CARRY PER SRI 53-41-12-205-010, REQUIRES INSPECTION 37900 TOMC-APPROVAL FROM SC1ELBYC COMMENT F/C''S FROM REPAIR EMBODIMENT, F/H''S NOT RELEVANT. SUBSEQUENT INSPECTIONS REQUIRED AT INTERVALS OF 5300 F/C''S, F/H''S NOT RELEVANT. RECORDS UPDATE QC REVIEWED QC REVIEWED INIT: 37,900 F/C FROM REPAIR EMBODIMENT WILL ITO TO RIR (-4416) RIR: EVERY 5,300 F/C.............LT

Part: TANK — CORRODED (FR 42 LONGERON Y) · airframe 60,107 hrs · 26,009 cycles

(SUPPORT TASK) FOUND CORROSION ON TOP OF LH OUTBOARD MAIN TANK ( BETWEEN LH LONGERON Y1292 AND LH BULKHEAD) FORWARD OF FRAME 42 N EXT TO APU FUEL PUMP. () ACCOMPLISHED REPAIR OF LH O/B MAIN TANK PER FINAL EA 320-5711-13 -A2789 AND UAL EC/RA 5711-01168. ACCOMPLISHED BY AT BFM ST AEROSPACE MOBILE. NR#0020386

Part: STRINGER — CORRODED (FR54-55S24L) · airframe 60,107 hrs · 26,009 cycles

A3NB-53-3-6186 AFT CARGO BILGE AREA FR54 TO FR55 S42L HAVE CORRO SION DOT 42-036 () FOUND TO BE OUT OF LIMITS IAW SRM 53-41-13-283-002 FIG 001 SHT 53-00-13-300-001 FIG 001 SHEET 02. REQUIRES INSPECTIONS PER SRI EMBODIMENT, SUBSEQUENT INSPECTION AND METHOD TBD. REF VT AEROSPA 01 REMOVED DAMAGE AND SPLICED IN NEW SECTION OF STGR IAW SRM 53-00-13-205-001 TABLE 004 AT 60000 FC / 120000 FH FROM REPAIR CE NRC 0020416 FOR WORK PERFORMED. REMOVED CORROSION ON STR42L FR 54 TO FR 55 IAW SRM 51-74-00. L=3.50" W=2" D=0.021" ORG MATERIAL 0.110" REMAINING 0.089" OK TO CARRY PER SRI 53-00-13-205-001, REQUIRES INSPECTION AT TOMC-APPROVAL FROM SC1ELBYC COMMENT 60000 F/C''S OR 120000 F/H''S FROM REPAIR EMBODIMENT, WHICHEVER OCCURS FIRST. SUBSEQUENT INSPECTIONS TBD. QC REVIEWED QC REVIEWED T/A : 60000 FC/ 120000 FH..........AP/U366012 AFT CARGO FR54 & FR55 STR 42L FOUNDED OUT OF LIMITS IAW SRM 53-4 1-13-283-002. REPAIRED IAW SRM 53-00-13-300-001. ACCOMPLISHED B Y V933438 AT BFM ST AEROSPACE MOBILE. NR#0020416 REOPEN BFM U296760 22FEB22 FOR: CLOSED IN ERROR IF SRM 53-00-13-300-002 WAS ACP''D, THEN REPETITIVE INSPS PER SRI 53-00-13-205-002 ARE REQUIRED. RECORDS UPDATE - AP

Part: INTERCOSTAL — DAMAGED (FR66) · airframe 60,107 hrs · 26,009 cycles

(A3NB-53-4-0033) DURING ROTO INSPECTION OF RH FR66 STGR12 GUSSET PLATE. REJECTABLE DAMAGE WAS NOTED IN BOTTOM HOLE DUE TO MECHAN ICAL DAMAGE IN ALL LAYERS WITH OVER 75% SH. CIRCLED IN RED.() DURING ROTO INSPECTION OF RH FR66 STGR 12 GUSET PLATE REJECTABLE MOBILE NR#0020727. DAMAGE WAS NOTED IN BOTTOM HOLE DUE TO MECHANICAL DAMAGE IN ALL LAYERS WITH OVER 75% SH. REMOVED AND REPLACED GUSSET PLATE IAW S RM 51-42-00/001. ACCOMPLISHED BY EMP#V936054 AT BFM ST AEROSPACE

Part: CROSSBEAM — CRACKED (FR20) · airframe 60,107 hrs · 26,009 cycles

(AD 2018-14-09) LH FR20 CROSSBEAM HAS CRACK INDICATIONS ON H17, H18,H23, H25 AND H26 FASTENER HOLES, REPAIR LH FR20 CROSSBEAM BE FORE NEXT FLIGHT PER STEP 8. CIRCLED IN RED. () REPAIRED LBH FR20 CROSSBEAM HOLES H17, H18, H25 & H26 BY OVER SI ZED COLDWORKING IAW R DWG R53112926 & EC/RA 5310-07977. ACCOMPLI SHED BY EMP#V933868 AT BFM ST AEROSPACE MOBILE NR#0020559

Part: CROSSBEAM — CRACKED (FR20) · airframe 60,107 hrs · 26,009 cycles

(AD 2018-14-09) LH FR20 CROSSBEAM HAS CRACK INDICATIONS ON H17, H18,H23, H25 AND H26 FASTENER HOLES, REPAIR LH FR20 CROSSBEAM BE FORE NEXT FLIGHT PER STEP 8. CIRCLED IN RED. () REPAIRED LBH FR20 CROSSBEAM HOLES H17, H18, H25 & H26 BY OVER SI ZED COLDWORKING IAW R DWG R53112926 & EC/RA 5310-07977. ACCOMPLI SHED BY EMP#V933868 AT BFM ST AEROSPACE MOBILE NR#0020559

Part: FITTING — CRACKED (FR 43) · airframe 60,107 hrs · 26,009 cycles

(AD2020-18-06) DURING ROTO INSPECTION OF THE FRAME FOOT AT FR43 LH SIDE CRACK INDICATION WAS NOTED AT FASTENER HOLE. REPAIR BEFO RE NEXT FLIGHT.

Part: STRINGER — CORRODED (FR56-57) · airframe 60,107 hrs · 26,009 cycles

A3NB-53-3-6186 AFT CARGO BILGE AREA STRINGER FR56 TO FR57 S43L H AVE CORROSION DOT 42-037 () REMOVED AND INSTALLED NEW COUPLING AND STRINGER IAW SRM 51-42-11 -00. ACCOMPLISHED BY EMP#V934344 AT BFM ST AEROSPACE MOBILE. NR #0020417.

Part: FLOOR SUPPORT — CORRODED (FR69-70 STR23R) · airframe 60,107 hrs · 26,009 cycles

(SUPPORT TASK) AFT CABIN SUPPORT FRAME BETWEEN FR69-FR70 STGR23R IS CORRODED. () REMOVED AFT CABIN SUPPORT IAW SRM 51-42-11 LOCATED AND DRILLED N EW PART IAW SRM 51-44-11 INSTALLED NEW PART IAW SRM 51-42-11 RES TORED SURFACE PROTECTION IAW SRM 51-23-11. ACCOMPLISHED BY EMP#V 934718 AT BFM ST AEROSPACE MOBILE. NR#V934718

Part: HINGE FITTING — CRACKED (#4 HINGE FITTIN) · airframe 60,107 hrs · 26,009 cycles

(A3NB-55-3-6005) RH HORIZONTAL #4 HINGE FITTING UPPER BONDING PL ATE CRACKED () REMOVED DAMAGE BONDING STRAP IAW SRM 51-42-11 FABRICATED NEW BON W 20-28-00. ACCOMPLISHED BY EMP#V934718 AT BFM ST AEROSPACE MOBI . DING STRAP MATERIAL P/N 2024T3050 BATCH#0003832165 DRAWING D9248 LE. NR#0020556 81 RESTORE SURFACE PROTECTION IAW SRM 51-23-11 INSTALLED NEW BON DING STRAP IAW SRM 51-42-11 BONDING STRAP TEST 0.08 MILLIOHMS IA

Part: FRAME — CRACKED (FR68) · airframe 60,107 hrs · 26,009 cycles

L/H AFT FR 68 DOORSTOP FITTING #1 I/B LOWER (D1) HAS CRACK INDIC ATION NOTED IN HOLE IAW NTM 51-10-01 PT6. INSTALLED FREEZE PLUG AND WASHERS. REINSTA SHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 24500 FC (FH NOT RELEVA ETHOD NTM 51-10-08 AND ROTO TEST REF TO AMM 53-41-00. IAW SRI 53 LLED #1 DOOR FITTING IAW SRM 52-13-31-400-002-A. INSPECTION THRE NT) SUBSEQUENT INSP AT INTERVALS 10700 (FH NOT RELEVANT), INSP M -41-12-205-009. REFF VT MAE NRC 0020529 FOR WORK PERFORMED. REPAIRED L/H AFT FR 68 DOORSTOP FITTING #1 I/B LOWER (D1), IAW S RM 53-41-12-300-10. HOLE REAMED FINAL TO 0.403" NO CRACKS NOTED ADD EMP:U354480 OK TO CARRY PER SRI 53-41-12-205-009, REQUIRES INSPECTION AT TOMC-APPROVAL FROM SC1ELBYC COMMENT 24500 F/C''S FROM REPAIR EMBODIMENT, F/H''S NOT RELEVANT. SUBSEQUENT INSPECTIONS EVERY 10700 F/C''S, F/H''S NOT RELEVANT. TOMC APPROVED : QC REVIEWED TOMC APPROVED : QC REVIEWED INIT : 24500 FC INIT WILL ITO TO RIR (-4386) RIR : 10700 FC.................AP/U366012 RECORDS UPDATE - AP CORRECTION TO DISCREPANCY AS NOT L/H SHOULD STATE R/H.

Part: FRAME — CRACKED (FR68) · airframe 60,107 hrs · 26,009 cycles

L/H AFT FR 68 DOORSTOP FITTING #3 O/B LOWER (D1) HAS CRACK INDIC ATION NOTED IN HOLE. IAW NTM 51-10-01 PT6. INSTALLED FREEZE PLUG AND WASHERS. REINSTA SHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 24500 FC (FH NOT RELEVA ETHOD NTM 51-10-08 AND ROTO TEST REF TO AMM 53-41-00. IAW SRI 5 LLED #3 DOOR FITTING IAW SRM 52-13-31-400-002-A. INSPECTION THRE NT) SUBSEQUENT INSP AT INTERVALS 10700 (FH NOT RELEVANT), INSP M -41-12-205-009. REFF VT MAE NRC 0020529 FOR WORK PERFORMED. REPAIRED L/H AFT FR 68 DOORSTOP FITTING #3 O/B LOWER (D1), IAW S RM 53-41-12-300-10. HOLE REAMED FINAL TO 0.421" NO CRACKS NOTED ADD EMP:U354480 OK TO CARRY PER SRI 53-41-12-205-009, REQUIRES INSPECTION AT TOMC-APPROVAL FROM SC1ELBYC COMMENT 24500 F/C''S FROM REPAIR EMBODIMENT, F/H''S NOT RELEVANT. SUBSEQUENT INSPECTIONS EVERY 10700 F/C''S, F/H''S NOT RELEVANT. TOMC APPROVED : QC REVIEWED TOMC APPROVED : QC REVIEWED INIT : 24500 FC INIT WILL ITO TO RIR ( 4384) RIR : 10700 FC..................AP/U366012 RECORDS UPDATE - AP

Part: STOP FITTING — CRACKED (LH AFT DOOR FR 6) · airframe 60,107 hrs · 26,009 cycles

LH AFT DOOR FR68 DOOR STOP FITTING #3 O/B TOP HOLE HAS A CRACK I NDICATION HOLE IS CIRCLED IN BLACK. NEEDS TO BE REPAIRED. L/H AFT DOOR FITTING FR68 LOWER I/B HOLE REAMED TO 0.391 NO CRAC OVED FOR ACCESS) IAW SRM 51-42-11. ACCOMPLISHED BY EMP#V934344 A K INDICATION NOTED IAW NTM 51-10-01 PT6 REPAIRED IAW SRM 53-41-1 T BFM ST AEROSPACE MOBILE. NR#0020527 2-300-010 FINAL DIM 0.4210 INSTALLED FREEZE PLUG AND WASHER ON T R#T21/159 2638/T21/1592637 REINSTALLED DOOR STOP FITTING #3 (REM

Part: STOP FITTING — CRACKED (RH AFT DOOR FR 6) · airframe 60,107 hrs · 26,009 cycles

RH AFT DOOR FR68 DOOR STOP FITTING #1 I/B LOWER HOLE HAS A CRACK INDICATION, HOLE IS CIRCLED IN BLACK. NEEDS TO BE REPAIRED BEFOR E FURTHER FLIGHT () L/H AFT DOOR STOP FITTING FR68 LOWER I/B HOLE REAMED TO 0.391 NO #1 (REMOVED FOR ACCESS) IAW SRM 51-42-11. ACCOMPLISHED BY EMP#V9 CRACK INDICATION NOTED IAW NTM 51-10-01 PT6. REPAIRED IAW SRM 5 34344 AT BFM ST AEROSPACE MOBILE. NR#0020529 3-41-12-300-10 FINAL DIM. 0.403. INSTALLED FREEZE PLUG AND WASHE R ON TR#T21/1592639/TR#T21/1592636 REINSTALLED DOOR STOP FITTING

Part: BONDING PLATE — CRACKED (RH HOR STAB #4 H) · airframe 60,107 hrs · 26,009 cycles

(A3NB-55-3-6005) RH HORIZONTAL #4 HINGE FITTING UPPER BONDING PL ATE CRACKED () REMOVED DAMAGE BONDING STRAP IAW SRM 51-42-11 FABRICATED NEW BON W 20-28-00. ACCOMPLISHED BY EMP#V934718 AT BFM ST AEROSPACE MOBI . DING STRAP MATERIAL P/N 2024T3050 BATCH#0003832165 DRAWING D9248 LE. NR#0020556 81 RESTORE SURFACE PROTECTION IAW SRM 51-23-11 INSTALLED NEW BON DING STRAP IAW SRM 51-42-11 BONDING STRAP TEST 0.08 MILLIOHMS IA

Part: GUSSET — DAMAGED (RH FR68) · airframe 60,107 hrs · 26,009 cycles

(A3NB-53-4-0033) DURING ROTO INSPECTION OF GUSSET PLATE RH FR68 STGR14 REJECTABLE DAMGE NOTED IN LWR TWO HOLES & STGR16 UPER AND LAST TWO LWR HOLES DUE TO MECHANICAL DAMAGE IN ALL LAYERS WITH OVER 75% SH. CIRCLED IN. DURING ROTO INSPECTION OF GUSSET PLATE RH FR68 STGR 14 REJECTABLE LISHED BY EMP#V936054 AT BFM ST AEROSPACE MOBILE. NR#0020728 DAMGE NOTED IN LWR TWO HOLES & STGR 16 UPPER AND LAST TWO LWR HO LES DUE TO MECHANICAL DAMAGE IN ALL LAYERS WITH OVER 75% SH. REM OVED AND REPLACED GUSSET PLATE (2EA) IAW SRM 51-42-00/001 ACCOMP

Part: FRAME — CRACKED (RH FWD EMR EXIT) · airframe 60,107 hrs · 26,009 cycles

A3NB-53-3-6132 RH FWD EMREGENCY EXIT DOOR RH I/B BEAM FRAME CRAC KED DOT 42-055. () PERFORMED HFEC SURFACE INSPECTION ON DOOR WITH SERIAL NO VH4011 BY EMP#V936054 AT BFM AEROSPACE MOBILE NR#0020651. IAW NTM 51-10-08. CRACK INDICATIONS NOTED AROUND FASTENERS REMOV ED AND REPLACED NEW BEAM FRAME IAW SRM 51-42-11/001. PN#D5227902 620551. RESTORED PAINT AS NEEDED IAW SRM 51-75-12. ACCOMPLISHED

Part: SHEAR TIE — CORRODED (STR40R-42R) · airframe 60,107 hrs · 26,009 cycles

(A3NB-5321-1-2706) 2EA SHEAR TIES/CLEATS FR30 STR40R-42R ARE COR RODED (REPLACE SHEAR TIES/CLEATS) REMOVED AND REPLACED (2EA) SHEAR TIES ON FR30 STGR 40R TO 42R IA W A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V928493 AT BFM ST AEROS PACE MOBILE NR#0020647

Part: FRAME — CRACKED (FR43) · airframe 60,107 hrs · 26,009 cycles

(AD2020-18-06) DURING ROTO INSPECTION OF THE FRAME FOOT AT FR43 RH SIDE. CRACK INDICATION WAS NOTED AT FASTENER HOLE. REPAIR NEF ORE NEXT FLIGHT. () REPAIRED RH FR43 RH IAW UAL EA 5330-06692 OPT 1 & R DWG R5337023 3. ACCOMPLISHED BY EMP#V935774 AT BFM ST AEROSPACE MOBILE NR#002 0370.

Part: SHEAR TIE — CORRODED (FR33) · airframe 60,107 hrs · 26,009 cycles

(A3NB-5321-1-2706) 2EA SHEAR TIES/CLEATS FR33 STR40R-42R ARE COR RODED (REPLACE SHEARTIES/CLEATS.) REMOVED AND REPLACED (2E) SHEARTIES ON FR33 STGR 40R TO 42R IAW A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V928493 AT BFM ST AEROSPA CE MOBILE. NR#0020645

Part: SHEAR TIE — CORRODED (FR31) · airframe 60,107 hrs · 26,009 cycles

(A3NB-5321-1-2706) 2EA SHEAR TIES/CLEATS FR31 STR 40R-42R ARE CORRODED (REPLACE SHEAR TIES/CLEATS.) REMOVED AND REPLACED (2EA) SHEAR TIES ON FR 31 STRG 40R TO 42R I AW A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V928493 AT BFM ST AERO SPACE MOBILE. NR#0020646

Part: BRACKET — CORRODED (FR33) · airframe 60,107 hrs · 26,009 cycles

(A3NB-05-3-6013) FWD CARGO COMPT: FR33 BETWEEN STR42 LH AND STR4 2 RH HAS CORROSION EVIDENCE. DOT 61-081. REMOVED SHEAR TIE FR33 BETWEEN STR43CL AND REPLACED BY SHEAR TIE 3. FABRICATED ON VTMAE TRAVELER#T21/1592356, INSTALLED NEW SHEAR TI E P/N UAD5323039920000 IAW A320 SRM 51-42-11, RESTORED SURFACE. ACCOMPLISHED BY EMP#V935832 AT BFM ST AEROSPACE MOBILE NR#002039

Part: FLOOR SUPPORT — CORRODED (FR70) · airframe 60,107 hrs · 26,009 cycles

A3NB-53-3-6279 AFT GALLEY FLOOR SUPPORT BEAM Y765 AT FR70 HAVE CORROSION DOT 42-019 EVALUATED AFT GALLEY FLOOR SUPPORT BEAM Y765 AT FR70 WITH CORROS ION OUT OF LIMITS DIM L=1.782, W=1.516, REMAIN THICKNESS 0.3, RE MOVED AND REPLACED FOR NEW BEAM IAW SRM 51-42-11. ACCOMPLISHED B Y EMP#V936054 AT BFM ST AEROSPACE MOBILE. NR#0020351

Part: SEAT TRACK — CORRODED (FR19-20) · airframe 60,107 hrs · 26,009 cycles

(A3NB-53-3-6038) FLOOR MAIN CABIN SEAT TRACK OUTBOARD RH BETWEEN FR 19 AND FR 20 HAS CORROSION. DOT 61-071 () EVALUATED SEAT TRACK Y-1292 OUTBOARD RH BETWEEN FR19 AND FR20 WI 936040 AT BFM ST AEROSPACE MOBILE. NR#0020359. TH CORROSION ON HARD POINT AREA AND WAS FOUND WITHOUT LIMITS IAW A320 SRM 53-00-15-283-002. REMOVED AND INSTALLED SEAT TRACK Y-1 292 IAW SRM 51-72-11 AND SRM 51-47-11/001. ACCOMPLISHED BY EMP#V

Part: FRAME — CRACKED (RH FWD EMER EXIT) · airframe 60,107 hrs · 26,009 cycles

A3NB-53-3-6132 RH FWD EMREGENCY EXIT DOOR RH I/B BEAM FRAME CRAC KED DOT 42-055. () PERFORMED HFEC SURFACE INSPECTION ON DOOR WITH SERIAL NO VH4011 BY EMP#V936054 AT BFM AEROSPACE MOBILE NR#0020651. IAW NTM 51-10-08. CRACK INDICATIONS NOTED AROUND FASTENERS REMOV ED AND REPLACED NEW BEAM FRAME IAW SRM 51-42-11/001. PN#D5227902 620551. RESTORED PAINT AS NEEDED IAW SRM 51-75-12. ACCOMPLISHED

Part: FRAME — CRACKED (RH FWD EMEREXIT) · airframe 60,107 hrs · 26,009 cycles

A3NB-53-3-6132 RH FWD EMERGENCY EXIT DOOR LH I/B BEAM FRAM CRACK ED DOT 42-054 () RH FWD EMERGENCY EXIT DOOR LH I/B REMOVED ANGLE CRACKED IAW SRM 51-42-11/001 AND INSTALLED NEW ANGLE IAW SRM 51-42-11/001 PN#D52 237902620451 BATCH#0003892709 PAINTED AS NEED IAW SRM 51-75-12. ACCOMPLISHED BY EMP#V936636 AT BFM ST AEROSPACE MOB NR#0020650

Part: FRAME — CRACKED (FR43 RH) · airframe 60,107 hrs · 26,009 cycles

(AD2020-18-06) DURING ROTO INSPECTION OF THE FRAME FOOT AT FR43 RH SIDE. CRACK INDICATION WAS NOTED AT FASTENER HOLE. REPAIR NEF ORE NEXT FLIGHT. () REPAIRED RH FR43 RH IAW UAL EA 5330-06692 OPT 1 & R DWG R5337023 3. ACCOMPLISHED BY EMP#V935774 AT BFM ST AEROSPACE MOBILE NR#002 0370.

Part: GUSSET — DAMAGED (RHFR68STR14) · airframe 60,107 hrs · 26,009 cycles

(A3NB-53-4-0033) DURING ROTO INSPECTION OF GUSSET PLATE RH FR68 STGR14 REJECTABLE DAMGE NOTED IN LWR TWO HOLES & STGR16 UPER AND LAST TWO LWR HOLES DUE TO MECHANICAL DAMAGE IN ALL LAYERS WITH OVER 75% SH. CIRCLED IN. DURING ROTO INSPECTION OF GUSSET PLAE RH FR68 STGR 14 REJECTABLE LISHED BY EMP#V936054 AT BFM ST AEROSPACE MOBILE. NR#0020728 DAMGE NOTED IN LWR TWO HOLES & STGR 16 UPPER AND LAST TWO LWR HO LES DUE TO MECHANICAL DAMAGE IN ALL LAYERS WITH OVER 75% SH. REM OVED AND REPLACED GUSSET PLATE (2EA) IAW SRM 51-42-00/001 ACCOMP

Part: GUSSET — DAMAGED (FR66STR12) · airframe 60,107 hrs · 26,009 cycles

(A3NB-53-4-0033) DURING ROTO INSPECTION OF RH FR66 STGR12 GUSSET PLATE. REJECTABLE DAMAGE WAS NOTED IN BOTTOM HOLE DUE TO MECHAN ICAL DAMAGE IN ALL LAYERS WITH OVER 75% SH. CIRCLED IN RED.() DURING ROTO INSPECTION OF RH FR66 STGR 12 GUSET PLATE REJECTABLE MOBILE NR#0020727. DAMAGE WAS NOTED IN BOTTOM HOLE DUE TO MECHANICAL DAMAGE IN ALL LAYERS WITH OVER 75% SH. REMOVED AND REPLACED GUSSET PLATE IAW S RM 51-42-00/001. ACCOMPLISHED BY EMP#V936054 AT BFM ST AEROSPACE

Part: SHEAR TIE — CORRODED (FR33STR40-42R) · airframe 60,107 hrs · 26,009 cycles

(A3NB-5321-1-2706) 2EA SHEAR TIES/CLEATS FR33 STR40R-42R ARE COR RODED (REPLACE SHEARTIES/CLEATS.) REMOVED AND REPLACED (2E) SHEARTIES ON FR33 STGR 40R TO 42R IAW A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V928493 AT BFM ST AEROSPA CE MOBILE. NR#0020645

Part: SHEAR TIE — CORRODED (FR30STR40-42R) · airframe 60,107 hrs · 26,009 cycles

(A3NB-5321-1-2706) 2EA SHEAR TIES/CLEATS FR30 STR40R-42R ARE COR RODED (REPLACE SHEAR TIES/CLEATS) REMOVED AND REPLACED (2EA) SHEAR TIES ON FR30 STGR 40R TO 42R IA W A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V928493 AT BFM ST AEROS PACE MOBILE NR#0020647

Part: SHEAR TIE — CORRODED (FR31STR40R-42R) · airframe 60,107 hrs · 26,009 cycles

(A3NB-5321-1-2706) 2EA SHEAR TIES/CLEATS FR31 STR 40R-42R ARE CO RRODED (REPLACE SHEAR TIES/CLEATS.) REMOVED AND REPLACED (2EA) SHEAR TIES ON FR 31 STRG 40R TO 42R I AW A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V928493 AT BFM ST AERO SPACE MOBILE. NR#0020646

Part: SHEAR TIE — CORRODED (FR 33STR42LHRH) · airframe 60,107 hrs · 26,009 cycles

(A3NB-05-3-6013) FWD CARGO COMPT: FR33 BETWEEN STR42 LH AND STR4 2 RH HAS CORROSION EVIDENCE. DOT 61-081. REMOVED SHEAR TIE FR33 BETWEEN STR43CL AND REPLACED BY SHEAR TIE 3. FABRICATED ON VTMAE TRAVELER#T21/1592356, INSTALLED NEW SHEAR TI E P/N UAD5323039920000 IAW A320 SRM 51-42-11, RESTORED SURFACE. ACCOMPLISHED BY EMP#V935832 AT BFM ST AEROSPACE MOBILE NR#002039

Part: SEAT TRACK — CORRODED (FR19,20) · airframe 60,107 hrs · 26,009 cycles

(A3NB-53-3-6038) FLOOR MAIN CABIN SEAT TRACK OUTBOARD RH BETWEEN FR 19 AND FR 20 HAS CORROSION. DOT 61-071 () EVALUATED SEAT TRACK Y-1292 OUTBOARD RH BETWEEN FR19 AND FR20 WI 936040 AT BFM ST AEROSPACE MOBILE. NR#0020359. TH CORROSION ON HARD POINT AREA AND WAS FOUND WITHOUT LIMITS IAW A320 SRM 53-00-15-283-002. REMOVED AND INSTALLED SEAT TRACK Y-1 292 IAW SRM 51-72-11 AND SRM 51-47-11/001. ACCOMPLISHED BY EMP#V

Part: BEAM — CORRODED (Y765) · airframe 60,107 hrs · 26,009 cycles

A3NB-53-3-6279 AFT GALLEY FLOOR SUPPORT BEAM Y765 AT FR70 HAVE C ORROSION DOT 42-019 EVALUATED AFT GALLEY FLOOR SUPPORT BEAM Y765 AT FR70 WITH CORROS ION OUT OF LIMITS DIM L=1.782, W=1.516, REMAIN THICKNESS 0.3, RE MOVED AND REPLACED FOR NEW BEAM IAW SRM 51-42-11. ACCOMPLISHED B Y EMP#V936054 AT BFM ST AEROSPACE MOBILE. NR#0020351

Part: FRAME — CORRODED (FR69-70) · airframe 60,107 hrs · 26,009 cycles

(SUPPORT TASK) AFT CABIN SUPPORT FRAME BETWEEN FR69-FR70 STGR23R IS CORRODED. () REMOVED AFT CABIN SUPPORT IAW SRM 51-42-11 LOCATED AND DRILLED N EW PART IAW SRM 51-44-11 INSTALLED NEW PART IAW SRM 51-42-11 RES TORED SURFACE PROTECTION IAW SRM 51-23-11. ACCOMPLISHED BY EMP#V 934718 AT BFM ST AEROSPACE MOBILE. NR#V934718

Part: SKIN — CONTAMINATED (LT ELEVATOR) · airframe 56,004 hrs · 24,236 cycles

LH UPPER SURFACE, FOUND FLUID ENTRAPMENT AT 22 INCHES FROM I/B E DGE AND 5.5 INCHES FROM TRAILING EDGE. DEFECT IS 5"X3.5" IN SIZE PER HAECO LCQ NR 9292260 GENERATED BY V916887 A3NB-55-4-6016 UPON EVAL OF LH ELEVATOR UPPER SURFACE 22 IN FROM I/B 5.5 IN FROM T/E DUE TO CLOSE DISTANCE JOINED 3 EA REPAIRS I NTO 1. NR 22259/9292259 & 22258/9292258 TOTAL SIZE 28..5 IN. ZON E 3 APPLIED STRUCTURAL REPAIR IAW A320 SRM 55-21-11-300-010 CATE GORY A REPAIR AT HAECO LCQ ON HANGAR NR 9292260 SUPERVISOR V061767 RII INSP C/W BY LC-32 V077953

Part: SKIN — CONTAMINATED (LT ELEVATOR) · airframe 56,004 hrs · 24,236 cycles

LH UPPER SURFACE, FOUND FLUID ENTRAPMENT AT 18.5 INCHES FROM I/B EDGE AND 6.25 INCHES FROM TRAILING EDGE. DEFECT IS 4.75"X4" IN SIZE AD RELATED TASK 2017-22-03 PER HAECO LCQ NR 9292259 GENERAT ED BY V916887 A3NB-55-4-6016 UPON EVALUATION OF LEFT ELEVATOR UPPER SKIN 18.5 IN FROM I/B 6.25 IN FROM T/E ZONE 3 DUE TO CLOSE DISTANCE JOINED 3 EA REPAIRS INTO 1 STRUCTURAL REPAIR NR 22258/9292258 & 22260/ 9292260 TOTAL SIZEE 28.5 IN. APPLIED STRUCTURAL REPAIR IAW A320 SRM 55-21-11-300-010 CATEGORY A REPAIR AT HAECO LCQ ON HANGAR NR V061744 9292259 BY MECH V080675 SUPERVISOR V061767 RII INSP C/W BY LC-23

Part: SKIN — CONTAMINATED (LT ELEVATOR) · airframe 56,004 hrs · 24,236 cycles

LH UPPER SURFACE, FOUND FLUID ENTRAPMENT AT 19.75 INCHES FROM I/ B EDGE AND 3.5 INCHES FROM TRAILING EDGE. DEFECT IS 2"X1.5" IN S IZE AD RELATED TASK 2017-22-03 PER HAECO LCQ NR 9292258 GENERATE D BY V916887 UPON EVAL OF LEFT ELEVATOR UPPER SURFACE 19.75 IN FROM I/B 3.5 I N FROM T/E ZONE 3 DUE TO CLOSE DISTANCE JOINED 3 EA REPAIRS INTO 1. NR 22260/9292260 & 22259/9292259 TOTAL SIZE 28.5 IN. APPLIED STRUCTURAL REPAIR IAW A320 SRM 55-21-11-300-010 CATEGORY A REPA IR AT HAECO LCQ ON HANGAR NR 9292258 SUPERVISOR V061767 RII INSP C/W BY LC-32 V077953

Part: BATTERY — FAILED (CABIN) · airframe 51,877 hrs · 22,372 cycles

EMER EXIT BATTERY AT LT OVERWING EXIT FAILED CAPACITY CHECK. REPLACED BATTERY REF AMM 33-51-38 OPS CHECKED OK.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHT) · airframe 49,869 hrs · 21,496 cycles

EPSU BATTERY FWD LIGHT FAULT ON PTP. REPLACED THE EMERGENCY LIGHT BATTERY . OPS CHECKED NORMAL.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHT) · airframe 49,869 hrs · 21,496 cycles

EPSU UNIT EMEREMERGENCY LIGHT FAULT ON PTP. REPLACED EMERGENCY LIGHT BATTERY AT 21D. OPS CHECKED NORMAL.

Part: SLAT — DENTED (RT WING) · airframe 45,425 hrs · 19,539 cycles

RIGHT WING NR 1 SLAT HAS A DENT APPROX 3" WIDE X 2" TALL, CHORD WISE X .025" DEPTH. DENT IS APPROX 25" IN FROM OTBD SIDE OF SLAT. REMOVED EXISTING REPAIR, CUT OUT DAMAGE & INSTALLED REPAIR PARTS IAW SRM 57-54-00 REPAIR 5G.

Part: INLET BULLET — DAMAGED (NR 2 ENGINE) · airframe 41,255 hrs · 17,876 cycles

NR 2 ENG RUBBER SPINNER CAP MISSING. R & R INLET CONE ON NR 2 ENG.

Part: VALVE — FAULTY (PARKING BRAKE) · airframe 41,006 hrs · 17,787 cycles

AFTER LANDING ON TAXI, PARKING BRAKE WOULD NOT RELEASE. TRIPLE INDICATOR SHOWING 3000 PSI LT & RT REGARDLESS OF PARKING BRAKE SWITCH POSITION. REPLACED PARKING BRAKE VLV IAW AMM, OPERATION & LEAK CHECKED GOOD.

Part: HANDSET — DEFECTIVE (CABIN) · airframe 40,888 hrs · 17,742 cycles

AFT CABIN HANDSET INOPERATIVE. CAN TRANSMIT, BUT NOT RECEIVE. TROUBLE SHOT & FOUND AFT ATTENDANTS HANDSET BAD, MFG ST3100-23-10, PCN 582-0042, PARTS 582-0042 & ST3100-23-10U3 HANDSET.

Part: AMU — FAULTY (NR 2) · airframe 40,885 hrs · 17,740 cycles

THE FWD & AFT FLIGHT ATTENDANT INTERPHONE HAS HIGH STATIC & WHEN THE FWD FLIGHT ATTENDANT TRIES TO TRANSMIT THE TRANSMISSION SHORTS TO THE PA SYSTEM. SWAPPING HANDSETS BETWEEN THE FWD & AFT CABIN, NO HELP. RESETTING THE AMU IS NO HELP. REPLACED AMU, BOTH HANDSET HARNESSES & FWD CRADLE. OPERATIONS CHECKED GOOD IAW AMM.

Part: STRINGER — CORRODED (42 LEFT) · corrosion level 2 · airframe 40,508 hrs · 17,599 cycles

CORROSION FOUND ON STRINGER 42L BETWEEN FRAMES 63-64 IN AFT CARGO. R & R STRINGER IAW SRM 51-42-11.

Part: SKIN — CORRODED (LT WING) · airframe 40,508 hrs · 17,599 cycles

LT WING TANK PLATE LANDING AT 540PB HAS CORROSION IN FASTENER HOLE THAT IS OUT OF LIMITS. REAMED, BUSHED & INSTALLED BRIDGE PLATE IAW SRM 57-21-11 FIG 202.

Part: SILL — CORRODED (FUSELAGE) · airframe 40,508 hrs · 17,599 cycles

R2 DOOR SILL CORRODED AT FR68. REPLACED R2 DOOR SILL IAW SRM 51-42-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,508 hrs · 17,599 cycles

L2 DOOR SILL HAS CORROSION AT FR 68-69. INSTALLED REPAIR ANGLE IAW SRM 53-41-14 FIG 201 PRINCIPLE 5.

Part: SKIN — DENTED (NR 2 NACELLE) · airframe 40,508 hrs · 17,599 cycles

NR 2 ENG INLET COWL UPPER INBD LIP EXTERIOR SKIN HAS DENT 2 O'CLOCK. MEASURE DENT NR 2 ENG INLET COWL UPPER LIP AT 2 O'CLOCK WITH DEPTH GAGE TLC 2815 .023" & 8.0" TO NEAREST RIVET SRM 54-10-00 FIG 101 DENT REQ INSP 6000FH, 4500 FC, R 20 MONTHS SRM 54-10-00 FIG101 NR 45445.

Part: STRAP — DEFECTIVE (L1 DOOR) · airframe 40,461 hrs · 17,580 cycles

YELLOW & BLACK STRAP AT DOOR 1L WILL NOT STOW. REPLACED SAFETY BARRIER STRAP AT DOOR 1L.

Part: MICROPHONE — INOPERATIVE (OXYGEN MASK) · airframe 40,072 hrs · 17,423 cycles

CAPTAIN'S OXYGEN MASK MICROPHONE IS INOPERATIVE. AMU IAW MM 23-51-34 AND CF DS TEST OK AND BOTH MASKS FUNCTION NORMAL.

Part: CONTROL BOX — FAILED (NLG) · airframe 39,973 hrs · 17,386 cycles

ON TAXI ACFT TRACKS LEFT AND REQUIRES 5-8 DEGREES RT NOSE TILLER. BSCU SHOWS FAILED ON PFR. REPLACEED BSCU IAW AMM 32-42-34. R & R BSCU BOX IAW AMM 32-42-34-000-001 A AND 32-42-34-400-001-A. OPS CHECKED NORMAL.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 39,916 hrs · 17,362 cycles

RIGHT WINDSHIELD ANTI-ICE DISPLAYED ON UPPER ECAM SCREEN. REPLACED WINDSHIELD IAW MM.

Part: UNKNOWN — UNKNOWN (WINDSHIELD HEAT) · airframe 39,666 hrs · 17,263 cycles

FIRST OFFICER`S SLIDING WINDOW HEAT INOPERATIVE. TEST WINDSHIELD HEAT CONTROLLER, NO PROBLEMS FOUND.

Part: WINDSHIELD — LEAKING (COCKPIT) · airframe 39,402 hrs · 17,150 cycles

VERY LOUD WIND NOISE ON RT SIDE AFT WINDOW. EXTERNAL SEAL AFT EDGE COMING OFF. REPLACED NR 3 RT FIXED WINDOW, OP'S TEST ANTI-ICING AND DEFOGGING, TESTED GOOD.

Part: WIRE — SHORTED (EMERGENCY LIGHT) · airframe 39,325 hrs · 17,122 cycles

EMERGENCY LIGHTS FAIL TEST. EPSU INT EMERGENCY LIGHT AND EPSU EXT LOAD EMERGENCY LIGHT. REPAIRED WIRE SHORTED TO GROUND AT SEAT ROW 30 IAW SWP CH 20. EMERGENCY LIGHTS TEST SATISFACTORY IAW AMM 33-51-00.

Part: WIRE — SHORTED (MICROPHONE) · airframe 39,244 hrs · 17,088 cycles

CAPTAIN'S OXYGEN MASK MICROPHONE IS INOPERATIVE. FOUND MICROPHONE WIRE IS INTERMITTENT IN O2 BOX. WHEN WIGGLED, COMMS IS INTERMITTENT. REPLACED CAPTAIN'S OXYGEN MASK STOWAGE BOX REF AMM35-12-41-00-0-001 A. CHECKS OK REF AMM 35-12-41-710-001A.

Part: APU — MALFUNCTIONED · airframe 38,984 hrs · 16,988 cycles

BCL 1 FAULT, FLT DIVERTED. REPLACED APU.

Part: INDICATOR — DETACHED (L1 SLIDE ARM) · airframe 38,907 hrs · 16,961 cycles

L1 DOOR SLIDE ARM INDICATOR DETACHED. ATTACHED INDICATOR TO DOOR, CHECKED OKAY.

Part: SEAL — BROKEN (GALLEY) · airframe 38,879 hrs · 16,948 cycles

AFT GALLEY WATER EXT HAS BROKEN SEAL. REPLACED SEAL.

Part: MICROPHONE — INOPERATIVE (OXYGEN MASK) · airframe 38,623 hrs · 16,850 cycles

CAPTAIN'S OXYGEN MASK MICROPHONE IS INOPERATIVE. REPLACED WITH SECOND OBSERVER. OPS CHECKS NORMAL.

Part: SEAL — PEELING (WINDOW) · airframe 38,600 hrs · 16,843 cycles

OUTSIDE WEATHER STRIPPING ON F/O REAR SIDE WINDOW PEELING BACK CAUSING LOUD WIND NOISE RESEALED AFT DAMAGED SECTION WITH SEA3750-21 REF MT 56-001. ALSO REF AMM 56-11-11.

Part: UNKNOWN — VIBRATION (TE FLAPS) · airframe 38,217 hrs · 16,700 cycles

ABNORMAL EXCESSIVE VIBRATION WITH FLAPS FULL SELECTED 140 KTS. LOWERED FLAPS AND SLATS TO PERFORM VISUAL INSP. NO DEFECTS NOTED AND FLAPS AND SLATS SECURE. DID FIND ICE ACCUMULATION AND REQUESTED DE-ICE.

Part: WIRE — CHAFED (EMERGENCY LIGHTS) · airframe 37,847 hrs · 16,555 cycles

L2 DOOR EMERGENCY LIGHT WIRES CHAFED. FOUND NO BROKEN STRANDS. REPAIRED CHAFED WIRES.

Part: PAN — CRACKED (LAVATORY) · airframe 37,847 hrs · 16,555 cycles

DOOR 2L FWD LAV FLOOR PAN IS CRACKED. INSPECTED AFT FWD LAV FLOOR PAN SENT PHOTOS TO FOR DISPOSITION AND PARTS. APPLIED CLEAR VINYL FLOOR TAPE OVER AFFECTED AREA. VERIFIED PAN IS CRACKED. REMOVED FLOOR FOUND DAMAGED MEMBRANE. REPLACED FLOOR PAN.

Part: UNKNOWN — MALFUNCTIONED (STEERING SYS) · airframe 37,070 hrs · 16,241 cycles

NOSE WHEEL STEERING PULLING RIGHT AND REQUIRES RUDDER TRIM TO TRACK STRAIGHT. STRAIGHT TRACKING REQUIRED RUDDER TRIM (UNITS LEFT OR RIGHT) TO BE SET AT: CREW COMMENTS: 4.5-ACCOMPLISHED TSM32-51-00- 201 REVIEW OF AMSDIS AND PFR. NO FAULT HISTORY NOTED. ACCOMPLISHED TSM 32-51-00-810-823 NO FAULTS NOTED EITHER. REPLACED NLG TIRES PRECAUTIONARY REF AMM.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 37,035 hrs · 16,227 cycles

CABIN EMERGENCY LIGHT TEST FAILS WITH MSG EPSU INTERNAL FAULT LEFT. REPLACED OVERWING POWER SUPPLY AND BATTERY.

Part: TIRE — VIBRATION (NLG) · airframe 36,688 hrs · 16,073 cycles

EXCESSIVE MODERATE VIBRATION FROM THE NOSE GEAR ON TAKEOFF UNTIL GEAR FULLY RETRACTED. REMOVED & REPLACED BOTH NOSE GEAR TIRE ASSEMBLIES.

Part: GROUND STUD — LOOSE (DOOR WARNING) · airframe 36,399 hrs · 15,966 cycles

RIGHT FWD CABIN DOOR ECAM ILLUMINATED 4 TIMES DURING DESCENT. DOOR OPS NORMAL. FOUND GROUND STUD 2050VN LOOSE CAUSING INTERMITTENT ECAM DOOR WARNING FAULT. SECURED GROUND WIRE, FWD RT DOOR INDICATION CHECKS NORMAL.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 36,289 hrs · 15,925 cycles

FIRST OFFICERS OXYGEN HARNESS FAILS TO INFLATE AND IS LEAKING. REPLACED 2ND OBSERVER MASK ASSY.

Part: ANALYZER — DEFECTIVE (VIBRATION SYS) · airframe 36,196 hrs · 15,882 cycles

ENGINE 1 VIBRATION N1 INDICATION ENGINE 1 INOP ON ENGINE ECAM SYSTEM PAGE - ENGINE. ACCOMPLISHED EG7182, FOUND 121.8 OHMS RESISTANCE BETWEEN PINS 7 AND 8 OF TERMINAL BLOCK 4 000VS, REF TASK77-30-00-810-821-A. SPEED SENSOR IS FAULTING, NEEDS ENG CHANGE.

Part: BRACKET — LOOSE (CABIN) · airframe 35,292 hrs · 15,517 cycles

AFT CABIN FLOOR MOUNTED FIRE EXTINGUISHER LOOSE IN BRACKET. INSTALLED NEW BRACKET.

Part: LINE — MISSING (EMERGENCY EVAC) · airframe 35,077 hrs · 15,441 cycles

1 EA EMER EVAC LINE. EMER EVAC LINE.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 35,068 hrs · 15,436 cycles

OVERWING EXIT EMERGENCY LIGHT BATTERY POWER SUPPLY HAS A BATTERY FAULT. REPLACED BATTERY PACK, NO HELP. REPLACED POWER SUPPLY 110WL2 AND INSTALLED NEW BATTERY TEST GOOD, NO FAULTS.

Part: WARNING LIGHT — ILLUMINATED (RAT) · airframe 34,792 hrs · 15,322 cycles

RAT FAULT DISPLAYED ON UPPER ECAM SCREEN. RAT AND EMERGENCY GENERATOR FAULT LIGHT ON PROGRAM TEXT: WORK WITH LM2730. SEE PTT 7922001 FOR BCL 1 REPLACEMENT.

Part: COMPUTER — FAULTY (NR 1) · airframe 34,075 hrs · 15,030 cycles

CLASS II MAINT MSG F-CTL DISPLAYED LOWER ECAM. REPLACED SEC 1. OP CHECKED PER MM.

Part: COMPUTER — FAULTY (ELAC 2) · airframe 34,061 hrs · 15,024 cycles

REPLACED ELAC 2 PER MM. OPS NORMAL.

Part: EXTINGUISHER — DISCHARGED (AFT) · airframe 33,976 hrs · 14,989 cycles

AFT FIRE EXTINGUISHER AGENT LEVEL LOW. REMOVED AFT HALON BOTTLE.

Part: PROXIMITY SWITCH — OUT OF ADJUST (PAX DOOR) · airframe 33,928 hrs · 14,965 cycles

RT FWD CABIN DOOR DISPLAYED ON UPPER ECAM SCREEN. REPEATED CHRONIC DOOR ECAM. ALL POSSIBLE PARTS HAVE BEEN CHANGED AT LEAST ONCE SUSPECT POSSIBLE RIGGING OF HANDLE OR HOOK PROX SENSOR. TOMC-FLAMINI ADJUSTED PROX SW 11WV1, REPLACED RELAY 12WN ACP HAND OVER HAND OF ALL WIRING HARNESS WITH PROX SWITCHES BYPASSED. VERIFIED ADJ OF DOOR LOCKS, LATCHING AND GIRT. REF MM 52-11-00 52-71-00 DOOR OPS AND IND NORMAL.

Part: OXYGEN MASK — MALFUNCTIONED (CABIN) · airframe 32,705 hrs · 14,456 cycles

O2 MASKS DEPLOYED AT ROW 26ABC. MASK STOWED, SEAT NOT TO BE OCCUPIED. ACCOMPLISHED REPACK OF O2 MASKS AT ROW 26ABC PER MM & ACCOMPLISHED MANUAL MASK RELEASE OPS CHECK PER MM. OPS CHECKED NORMAL. REPAIRED MASK REPACKED MASK.

Part: BRAKE SYS — MALFUNCTIONED (MLG) · airframe 32,694 hrs · 14,452 cycles

CAPTAIN BRAKE PEDALS HAVE NO ARTIFICIAL FEEL TAKES LESS THAN 5 POUNDS OF PRESSURE ALL THE FOUND AIR IN MASTER CYL, BLEED LOW PRESS SYS OF ALT BRAKES PER MM, OP CHECK GOOD.

Part: MASK — BROKEN (SAFETY EQUIPMENT) · airframe 31,616 hrs · 14,009 cycles

F/A O2 DEMO MASK BROKEN. REPLACED MASK.

Part: SHADE — TORN (COCKPIT WINDOW) · airframe 31,315 hrs · 13,869 cycles

F/O SLIDING WINDOW SHADE TORN. WINDOW REMOVED AND REPLACED F/O'S SLIDING WINDOW SHADE. TRANSFERRING PANE AND NEW SEAL. ALSO WORKING NR2 B PYLON LOOP. REPLACED METAL CONDUIT FOR F/O SLIDING WINDOW. REPLACED F/O SLIDING WINDOW PANEL (2RH) IAW MM.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 29,426 hrs · 13,080 cycles

EMERGENCY LIGHT TEST FAILS. REPLACED FWD LT BATTERY, TESTED GOOD.

Part: BATTERY — FAILED (CABIN) · airframe 28,486 hrs · 12,674 cycles

LEFT BATTERY PACK FOR EMERGENCY LIGHTS FAILED TEST. REPLACED BATTERY AND POWER SUPPLY.

Part: GAUGE — OUT OF POSITION (R1 DOOR SLIDE) · airframe 28,366 hrs · 12,634 cycles

DOOR 1R SLIDE PRESSURE GAUGE NOT VISIBLE. SECURED SLIDE PRESSURE GAUGE LENS. GAUGE NOW VISIBLE.

Part: CONNECTOR — UNSECURE (MID PWR SUPPLY) · airframe 27,538 hrs · 12,250 cycles

EMERGENCY LIGHT CHECK. EPSU BATT. EMERGENCY LH CAME ON DURING TEST. SUPPLEMENTAL DATA UPDATE SECURED CONNECTOR AT LEFT MID PWR SUPPLY, OPS CK OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,439 hrs · 11,157 cycles

SEAT MOUNTED EEL LIGHT OUT AT 1C, 5C, 11C. RELAMPED.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT) · airframe 17,505 hrs · 7,552 cycles

FOUND EPSU BAT EMERGENCY R AND EPSU COM FWD L MESSAGE DISPLAYED. REPLACED BATTERY PACK. ACCOMPLISHED EMERGENCY LIGHT TEST, OPS CHECKED NORMAL.

Part: BATTERY — UNSECURE (CABIN) · airframe 17,258 hrs · 7,433 cycles

FOUND EMERGENCY LIGHT TEST FAILS WITH L FWD EPSU FAIL AND RIGHT SLIDE EMERGENCY FAIL MESSAGES. REAPPLIED SYSTEM POWER AND CHECKED CHARGING UNITS AND BATTERIES. ALL OK. RESEATED BATTERIES ON CHARGING UNITS. EMERGENCY LIGHTING CHECKS OK.

Part: LIGHT — NO TEST (CABIN) · airframe 15,301 hrs · 6,544 cycles

EMERGENCY LIGHT TEST FAILS PER 3SVC.

Part: LINK ASSY — BENT (MLG) · airframe 8,595 hrs · 3,370 cycles

FLIGHT DIVERTED DUE TO PROBLEM WITH THE LANDING GEAR. FOUND LINK ON PROXIMITY SENSOR ASSEMBLY BENT. STRAIGHTENED LINK AND PERFORMED OPERATIONAL CHECK OF GEAR RETRACTION. OPERATIONS CHECK NORMAL.

Part: COMPUTER — MALFUNCTIONED (CABIN PRESSURE) · airframe 5,977 hrs · 2,361 cycles

DIVERSION DUE TO LOSS OF CABIN PRESSURE. AIRCRAFT EXPERIENCED DUAL BLEED SYSTEM FAILURE - LT BLEED LEAK & ENG 2 BLEED FAULT. THE BLEED MANAGEMENT COMPUTER WAS REPLACED FOR THE REPORTED BLEED LEAK (NO LEAKS WERE FOUND) AND THE FAN AIR THERMOSTAT WAS REPLACED FOR THE NR 2 BLEED SYSTEM FAULT.

Part: FIRE BOTTLE — UNSERVICEABLE (CARGO BAY) · airframe 2,294 hrs · 901 cycles

CREW REPORTS ECAM MESSAGE INDICATES A FIRE BOTTLE DISCHARGE. REPLACED CARGO FIRE BOTTLE DUE TO LOW PRESSURE INDICATION.

Part: SKIN — DENTED (FUSELAGE) · airframe 1,803 hrs · 695 cycles

DENT FOUND AT AIRCRAFT ARRIVAL. DENT LOCATED ABOUT 20 INCHES ABOVE AVIONICS EQUIPMENT AIR INLET AND 9 INCHES AFT OF FRAME 20. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.

Part: SIGN — INOPERATIVE (CABIN) · airframe 34,669 hrs · 42,723 cycles

SEA - FORWARD EXIT DOOR EXIT LIGHT FOUND INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.