N630VA

Part: DOOR SILL — CORRODED (UNKNOWN) · corrosion level 2 · airframe 47,562 hrs · 15,607 cycles

L2 DOOR SILL FWD BLANKING PLATE ATTACH AREA AFT INBD NUTPLATE HOLE CORRODED GROUNDED - YES. ACCOMPLISHED SRM REPAIR TO DISCREPANT AREA IAW A320 SRM 53-41-14-300-001 REPAIR PRINCIPLE 11. REMOVED AND INSTALLED SIDEWALL RETAINER IAW A320 SRM 51-42-11. EVALUATED DAMAGE AND FOUND OUT OF LIMITS IAW A320 SRM 53-41-14. 100% MATERIAL LOSS.

Part: SKIN — DENTED (UNKNOWN) · airframe 47,562 hrs · 15,607 cycles

LESSOR ITEM-LH INBOARD FLAP UPPER SURFACE HAS SMALL DENT APPROXIMATELY 4 INCHES FROM TRAILING EDGE AND 20 INCHES FROM INBOARD END GROUNDED - YES. COMPLETED EXTERNAL BONDED METAL DOUBLER REPAIR CATEGORY A PERMANENT REPAIR ON LH INBOARD FLAP UPPER SURFACE LOCATED 4" FORM T/E, 20" FROM I/B END AND 5" IN DIA. REPAIR DOUBLER IAW A320 SRM 57-52-00-300-095 AND EA# CMPT-57EA-01860-REV. 00 FH: 47561:57, FC: 15607, WTV: 010

Part: FLOOR SUPPORT — CORRODED (UNKNOWN) · corrosion level 2 · airframe 47,497 hrs · 15,574 cycles

MAIN CABIN FR20 Y-254 FLOORBOARD SUPPORT (LONGERON) ACCOMPLISHED THE REPAIR WITH WRONG SRM REPAIR. REF. G1758761 GROUNDED - YES. REMOVED AND REPLACED DUMMY RAIL P/N D5311141420200 P.O. 1061654.1 IAW A320 SRM 51-42-11 AND AIRBUS DWG# D5311406. REMOVED AND REPLACED BEAM P/N 5311146020201. P.O. 1065047.1 IAW A320 SRM 51-42-11 AND AIRBUS DWG# D53111460. REMOVED AND INSTALLED FLOOR BOARDS 232CF AND 231 KF IAW A320 AMM 53-22-12.

Part: SKIN — GOUGED (UNKNOWN) · airframe 47,562 hrs · 15,607 cycles

LESSOR ITEM - BETWEEN FRAME 50 AND 51 STRG 7 AND STRG 8 THERE IS GOUGE MARK ON FUSELAGE THAT IS NOT LISTED ON DENT AND DAMAGE MAP AND LISTING GROUNDED - YES. MEASURED GOUGE FOUND BEYOND LIMITS IAW A320 SRM 53-41-11. LENGTH OF .5' WIDTH OF .5" AND DEPTH OF .028 T8492H. REMOVED GOUGE IAW A320 SRM 53-41-11-300-019 CAT B INSPECTION THRESHOLD OF 60000 FC INSPECTION INTERVALS TBD, INSPECTION METHOD TBD

Part: SHEAR PLATE — CORRODED (UNKNOWN) · corrosion level 2 · airframe 47,562 hrs · 15,607 cycles

RH MAIN CABIN AFT AT FR69 TO FR70, SHEAR PLATE HAS CORROSION AT FASTENER HOLES AT 3EA SPOTS, MARKED IN RED GROUNDED - YES. REMOVED AND REPLACED SHEAR PLATE R/H MAIN CABIN AT FR69 TO FR70 IAW A320 SRM 51-42-11 AND A320 DWG 18 D53474180 REV. U P/N:D5347112420300 PO:1055897.8

Part: SHEAR PLATE — GOUGED (UNKNOWN) · airframe 47,562 hrs · 15,607 cycles

MAIN CABIN FLOOR AFT L/H AT FR69 TO FR70, SHEAR PLATE HAS GOUGE, MARKED IN RED GROUNDED - YES. REMOVED AND REPLACED LH AFT SHEAR PLATE FROM FR69-FR70 PN D5347112420200 PO: 975781.1 IAW AIRBUS DWG D53474180, A320-SRM 51-72-11

Part: FLOORBEAM — CORRODED (UNKNOWN) · corrosion level 2 · airframe 47,497 hrs · 15,574 cycles

MAIN CABIN AFT R/H AT FR 66, FLOOR BEAM 2ND FROM CENTER, HAS CORROSION ON TOP OF BEAM. MARKED IN RED GROUNDED - YES. REMOVED AND REPLACED FLOOR BEAM IAW ASA A320 SRM 51-42-11/001 AND DWG D53472284 ISSUE A AT RH SIDE FR 66 -Y464.8, IAW A320 SRM 51-72-11

Part: FLOOR SUPPORT — CORRODED (UNKNOWN) · corrosion level 2 · airframe 47,562 hrs · 15,607 cycles

MAIN CABIN AFT R/H FROM FR 67 TO FR 68, FLOOR BEAM 3RD FROM CENTER, HAS CORROSION ON TOP OF BEAM. MARKED IN RED. GROUNDED - YES. REMOVED AND REPLACED FLOOR BEAM RH SIDE AT FR 67 3RD FROM CENTER -Y969.0 IAW ASA SRM 51-42-11 AND AIRBUS DWG D53472193 ISSUE A

Part: FLOORBEAM — CORRODED (UNKNOWN) · airframe 47,562 hrs · 15,607 cycles

MAIN CABIN LH AT FR 67 FLOOR ON BEAM 3RD FROM CENTER, HAS 2 EA SPOT OF CORROSION ON TOP OF BEAM, MARKED IN RED GROUNDED - YES. REMOVED CORROSION ON LH FLOOR BEAM AT FR 67 21 INCHES AFT OF FWD SPLICE ORIGINAL THICKNESS .170 REMOVED .016 REMAINING OF .154. FOUND TO BE IN LIMITS IAW ASA A320 SRM 53-00-14-283-009.RESTORED SURFACE PROTECTION IAW ASA A320 SRM 51-21-11 AND 51-75-12 CAT A.

Part: DOOR SILL — CORRODED (UNKNOWN) · corrosion level 2 · airframe 47,497 hrs · 15,574 cycles

MAIN CABIN AFT R/H AFT FR66 FLOOR AT R2 DOOR FWD OF GIRT BAR FITTING, HAS CORROSION ON TOP OF BEAM. GROUNDED - YES. MAJOR REPAIR ACCOMPLISHED - R2 DOOR SILL MULTIPLE CORROSION AREAS - REPAIR PERFORMED PER AIRBUS DOSSIER 81233224 AND APPROVED PER AIRBUS RDAF 81233224/003/2023#A DATED 26JUL2023. EA A320-53EA-01834.

Part: DOOR SILL — CORRODED (UNKNOWN) · corrosion level 2 · airframe 47,562 hrs · 15,607 cycles

MAIN CABIN L/H AT FR68 FLOOR AT L2 DOOR, HAS CORROSION AT 4EA FASTENER HOLES, MARKED IN RED GROUNDED - YES. REMOVED CORROSION AND REPAIRED DAMAGE AREA AT FR68 L/H SIDE ON L2 DOOR SILL IAW ASA A320 SRM 53-41-14-300--001 ORIGINAL MATERIAL THICKNESS IS .063 AT NUTPLATE HOLES REMOVED .031 REMAINING THICKNESS OF .032 ONLY ALLOWED 25% LOSS CATEGORY A

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 47,562 hrs · 15,607 cycles

MAIN CABIN AFT R/H AT FR68, FLOOR BEAM 2ND FROM CENTER, HAS CORROSION ON TOP OF BEAM. MARKED IN RED GROUNDED - YES. REMOVED AND REPLACED RH FLOOR BEAM AT FR68 2ND FROM CENTER- Y464.8 IAW ASA A320 SRM 51-42-11 AND AIRBUS DWG D53472095 ISSUE E

Part: FLOORBEAM — CORRODED (UNKNOWN) · corrosion level 2 · airframe 47,561 hrs · 15,607 cycles

MAIN CABIN AFT WET AREA FLOORS STRUCTURE UNDER FLOORBOARD 261JG BETWEEN FRAMES 69 AND 70 APPROX 3 INCHES RIGHT FROM CENTER BUTTLINE HAS CORROSION. DOT ATTACHED. CIRCLED IN RED GREASAE PEN. GROUNDED - YES. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM A320 53-00-14. CORROSION LOCATED AT HARD POINT WHERE NO CORROSION ALLOWED. REMOVED STRUCTURE IAW A320 SRM 51-42-11. LOCATED, DRILLED, AND DEBURRED NEW BEAM PN D5347219720200 PO 1064973.1 IAW A320 SRM 51-44-11. INSTALLED ATTACH FITTINGS IAW A320 SRM 51-42-11. INSTALLED BEAM IAW A320 SRM 51-42-11 AND AIRBUS DWG D58472097

Part: FLOORBEAM — CORRODED (UNKNOWN) · corrosion level 2 · airframe 47,562 hrs · 15,607 cycles

MAIN CABIN AFT R/H AFT FR 68, FLOOR BEAM 4TH FROM CENTER HAS CORROSION ON TOP OF BEAM. MARKED IN RED. GROUNDED - YES. REMOVED AND REPLACED RH FLOOR BEAM AT FR 68 4TH FROM CENTER -Y 1162.5 IAW ASA A320 SRM 51-72-11

Part: FLOORBEAM — CORRODED (UNKNOWN) · corrosion level 2 · airframe 47,562 hrs · 15,607 cycles

MAIN CABIN AFT R/H AFT FR 66, FLOOR BEAM 3RD FROM CENTER, HAS CORROSION ON TOP OF BEAM, MARKED IN RED. GROUNDED - YES. REMOVED AND REPLACED FLOOR BEAM R/H SIDE FR 64-66 -Y765 IAW ASA A320 SRM 51-72-11-911-001 AND DWG D53472209 ISSUE F

Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 47,562 hrs · 15,607 cycles

AFT WET AREA FLOOR PNL 261AC DELAMINATED GROUNDED - YES. FABRICATED NEW FLOOR PANEL 261AG IAW A320 SRM 53-02-00-300-011 AND GILL CORPORATION MANUAL TGC IRM 9701-REV L FH: 47561:57, FC:15607,WTV:010

Part: SKIN PANEL — CORRODED · corrosion level 2 · airframe 44,782 hrs · 14,060 cycles

SUBSURFACE CORROSION INDICATIONS FOUND: L/H WING LOWER SURFACE T/E OVERHANG, MARKED 1.5" X 3" STA5512 / RIB10. DOT:A374 GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS. ORIGINAL THICKNESS IS .197, REMAINING IS .146, .051 WAS REMOVED. OUT OF LIMITS REF A320 SRM 57-21-11. REPAIRED DAMAGE REF ASA EA A320-57EA-01132 REV"00" DOT REMOVED

Part: SUPPORT — CORRODED (FRAME 69-70) · corrosion level 2 · airframe 41,303 hrs · 12,542 cycles

AFT WET AREA, AFT OF L2 DOOR, FLOOR STRUCTURE FRAME SUPPORT HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED FRAME SUPPORT IAW A320 SRM 51-42-11 REF AIRBUS DWG #D53474180. NO ALLOWABLE LIMITS GIVEN IN A320 SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,303 hrs · 12,542 cycles

AFT CABIN UNDERFLOOR COMPARTMENT FLOORBEAM HAS CORROSION ON TOP SURFACE AT FRAME C66 RBL1300MM ADJACENT TO R2 DOOR. GROUNDED - YES. REMOVED AND REPLACED FLOORBEAM SUPPORT PER SRM 51-42-11 AND DWG D53472840

Part: FLOOR SUPPORT — CORRODED (FRAMES 65-66) · corrosion level 2 · airframe 41,303 hrs · 12,542 cycles

AFT CABIN UNDERFLOOR COMPARTMENT FLOOR BEAM HAS CORROSION ON TOP SURFACE AT FRAME C66 RBL735MM ADJACENT TO R2 DOOR. STREAMER ATTACHED. GROUNDED - YES. REMOVED AND REPLACED FLOOR BEAM IAW A320 SRM 51-42-11 REF AIRBUS DWG #D53472836.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · corrosion level 2 · airframe 41,303 hrs · 12,542 cycles

AFT CABIN UNDER FLOOR COMPARTMENT FLOOR BEAM HAS CORROSION ON TOP SURFACE AT FRAME C66 RBL1473 MM ADJACENT TO R2 DOOR. ATTACHED. GROUNDED. REMOVED CORROSION IAW SRM 53-41-14-283-002. ORIG. MAT S .150, REMAINING MAT IS .00. 100% MAT LOSS. REMOVED DAMAGED AREA AND REPAIRED IAW A320 SRM 53-41-14-300-001 REPAIR PRINCIPLE 6. THIS IS A CATEGORY A REPAIR.

Part: SHEAR PLATE — CORRODED (FRAMES 69-70) · corrosion level 2 · airframe 41,303 hrs · 12,542 cycles

AFT MAIN CABIN RH LATERAL SHEAR PLATE HAS CORROSION UPPER SURFACE STA.69 TO 70 GROUNDED - YES. REMOVED AND REPLACED SHEAR PLATE IAW A320 SRM 51-42-11 REF AIRBUS DWG D53474180. OPS CHECK PERFORMED IAW A320 AMM 38-31-36-710-050-A

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,303 hrs · 12,542 cycles

MAIN CABIN FLOOR SUPPORT STRUCTURE APPROX 7" FWD OF FRAME 70 AT LBL 7 FLOOR BOARD SUPPORT BEAM UPPER SURFACE IS CORRODED GROUNDED - YES. REMOVED AND REPLACED FLOOR BEAM SUPPORT PER SRM 51-42-11 AND DWG D53472780.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,303 hrs · 12,542 cycles

MAIN CABIN R2 DOOR SILL HAS CORROSION 2" AFT STA.69 @ I/B FASTENER HOLE UPPER SURFACE GROUNDED - YES. ACCOMPLISHED DOUBLER REPAIR IAW SRM 53-41-14-300-01. EVALUATED CORROSION - ORIGINAL THICKNESS .063, REMAINING .00, MAT'L LOSS .063 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,303 hrs · 12,542 cycles

AFT MAIN CABIN LT LATERAL SHEAR PLATE HAS CORROSION UPPER SURFACE STA 69 TO 70 GROUNDED - YES. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11 REF DWG D53474180.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,303 hrs · 12,542 cycles

MAIN CABIN DUMMY RAIL AT STA. Y-81 HAS CORROSION AT FR16 GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN DUMMY RAIL IAW SRM 51-42-11 AND SRM 51-72-11. REMOVED CORROSION, ORIGINAL THICKNESS .149, REMOVED .038, REMAINING .111 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14-283-004.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,303 hrs · 12,542 cycles

MAIN CABIN DUMMY RAIL AT STA.Y-254 HAS CORROSION AT FR16 GROUNDED - YES. ACCOMPLISHED DOUBLER REPAIR TO FLOOR SUPPORT IAW SRM 53-00-14-300-007 REMOVED CORROSION - ORIGINAL THICKNESS .079, REMOVED .045, REMAINING .034 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-11-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,303 hrs · 12,542 cycles

MAIN CABIN SEAT TRACK AT STA.Y-765 HAS CORROSION AT FR16 GROUNDED - YES. REMOVED CORROSION FROM EDGE OF FLANGE, ORIGINAL WIDTH .787, REMOVED .075 AND REMAINING .712 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-11-15 (NO ALLOWABLE DAMAGE CRITERIA GIVEN FOR EDGE REMOVAL). ACCOMPLISHED DOUBLER REPAIR IAW SRM 53-11-15-300-004. APPLIED TOPCOAT IAW SRM 51-75-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,303 hrs · 12,542 cycles

MAIN CABIN SEAT TRACK AT STA. Y-1292 HAS CORROSION AT FR16 AND 10" AFT GROUNDED - YES. REMOVED CORROSION - ORIGINAL .087, REMOVED .040, REMAINING .047 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-11-15. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-42-11 AND SRM 51-72-11.

Part: CONTROL UNIT — FAILED

THE FLIGHT CREW REPORTED AN ELECTRICAL BURNING ODOR IN THE FLIGHT DECK, ASSOCIATED WITH POWER TRANSFER BETWEEN GROUND AND APU ELECTRICAL POWER. DURING TROUBLESHOOTING THE GAPCU UNIT WAS DISCOVERED FAILED, THE UNIT WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. INSPECTION FOR ELECTRICAL ODORS WAS ACCOMPLISHED WITH NO FINDINGS IAW AMM-24-0 0-00-810. NO REPORTS OF ODOR ON SUBSEQUENT FLIGHTS.

Part: UNKNOWN — ODOR (CABIN)

A FUEL ODOR IN THE CABIN DURING TAXI TO TAKEOFF. RETURNED TO THE GATE, ACCOMPLISHED TSM 055000810831A WITH NO FINDINGS. THE ACFT CONTINUED TO ITS DESTINATION WITHOUT FURTHER ISSUE. NO REPORTS OF ODOR ON SUBSEQUENT FLIGHTS.

Part: RESERVOIR — LOW PRESSURE (RT OVRWING SLIDE) · airframe 28,866 hrs · 8,588 cycles

ACFT WAS BEING TOWED FROM REMOTE SPOT TO THE GATE BY MAINTENANCE, WHEN THE FOLLOWING DEFECT WAS DISCOVERED: RT OVERWING SLIDE PRESSURE LOW. R & R RT OVERWING SLIDE RESERVOIR IAW AMM 25-62-46. OPS CHECKED GOOD.

Part: SUPPORT — CORRODED (FUSELAGE)

LEFT SHEAR PLATE SUPPORT BETWEEN FR69-70, ST 23-24 LT CORRODED BEYOND LIMITS. EXTENT OF DAMAGE 2"L X 2" W, X .020"D.

Part: SUPPORT — CORRODED (FUSELAGE)

RIGHT SHEAR PLATE SUPPORT BETWEEN FR69-70, ST 23-24 RT CORRODED BEYOND LIMITS. EXTENT OF DAMAGE 2"L X 2"W X .040" D.

Part: SHEAR PLATE — CORRODED (FUSELAGE)

RT AFT SHEAR PLATE BETWEEN FR 69-70, ST23-24, RT CORRODED BEYOND LIMITS. EXTENT OF DAMAGE, 2" L X 2" W X .030" D.

Part: SHEAR PLATE — CORRODED (FUSELAGE)

LEFT AFT SHEAR PLATE BETWEEN FR 69-70, ST 23-24 LEFT CORRODED BEYOND LIMITS. EXTENT OF DAMAGE 1"L X 1"W X .025" D.

Part: STRINGER — DAMAGED (FUSELAGE)

ON APPROACH, AC SUSTAINED LIGHTING STRIKE, DAMAGING THE FUSELAGE SKIN FASTENER. LOCATION OF DAMAGE STRINGER 41, RT 4.40 INCHED AFTER FRAME 25. FASTENER REQUIRED REPLACEMENT AND STRINGER REPAIR. ADDITIONALLY, THE LT FWD NLG DOOR AND LT AFT NLG DOOR, RT WING TIP FENCE, TAT SENSOR, FWD DME ANTENNA, MARKER BEACON ANTENNA WERE REPLACED AS A RESULT OF LIGHTENING DAMAGE. (K)