N311US

Part: DOOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 67,815 hrs · 29,954 cycles

AFT RT EMERGENCY OVERWING EXIT AMBER CAUTION LIGHT CAME ON, ON UPPER ECAM DURING FCF. AFT RT EMERGENCY OVERWING EXIT COVER FLAP ADJUSTED IAW AMM 52-21-11-700-050-B. OPS TEST GOOD.

Part: EPSU — FAILED (EMERGENCY LIGHTS) · airframe 67,788 hrs · 29,938 cycles

DURING NON ROUTINE CHECK, FOUND POWER SUPPLY 13WL FAILED TEST. REMOVED EPSU 13WL IAW AMM 33-51-38-000-001-A. MX INSTALLED SERVICEABLE EPSU AT 13WL AND FUNCTIONAL CHECK WAS NORMAL.

Part: STRUT — WORN (LT WING TE FLAP) · airframe 67,815 hrs · 29,954 cycles

LEFT FLAP INTERCONNECT STRUT HAS EXCESSIVE SIDE PLAY AND ACTUATING ROD WORN. REPLACED WITH NEW INTERCONNECTING STRUT ON LT FLAP IAW AMM 27-51-44, PB 401. ADJUSTMENT GOOD IAW AMM 27-51-44-820-001-A. TEST GOOD IAW AMM 27-51-44-710-056-A AND ACCOMPLISHED OPS TEST ON WC 2750-6020-LT.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, MX REPLACED FWD CENTER TITANIUM & RT FUSELAGE LATERAL SKIN PANEL BETWEEN FR1-FR 12 IAW ER/A 512316-14. REPLACED FWD CENTER TITANIUM SKIN IAW REPAIR DWG R5311269007 & RT FUSELAGE LATERAL SKIN PANEL FR 1-12 IAW REPAIR DWG R53112168000.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131GF HAS MULTIPLE DENTS AND SCRATCHES. FABRICATED FLOOR PANEL IAW SRM 53-02-00 FIG 209 & DWG 3D25-37705.

Part: STRUCTURE — CORRODED (EMERGENCY EXIT) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND RT AFT EMERGENCY EXIT DOOR TEE SECTION HAS CORROSION. REPLACED TEE SECTION IAW SRM 51-42-11 AND SRM 51-44-11. REMOVED CORROSION IAW SRM 51-74-00, NO LIMITS FOUND IN SRM 51-20-00. ORIG MAT IS .078".

Part: STRUCTURE — CORRODED (EMERGENCY EXIT) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND LT AFT EMERGENCY EXIT DOOR LOWER AFT TEE SECTION HAS CORROSION. REPLACED TEE SECTION IAW SRM 51-42-11 AND SRM 51-44-11. REMOVED CORROSION IAW SRM 51-74-00, NO LIMITS FOUND IN SRM 52-20-00.

Part: SKIN — DAMAGED (NR 3 SLAT) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND LT WING NR 3 SLAT TOP SKIN AT RIB OTBD OF TRACK NR 7 DENT IS OUT OF NEARNESS TO RIB & SPAR. NO ALLOWABLE LIMIT ON THIS AREA IAW SRM 57-40-00, FIG 102. CUT OUT DAMAGE IAW SRM 57-40-00, FIG 102. FABRICATED SKIN INSERT, BACKING PLATES. FABRICATED REINFORCING PLATES IAW SRM 57-40-00, FIG 226.

Part: STRUCTURE — CORRODED (EMERGENCY EXIT) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND LEFT FWD EMERGENCY EXIT DOOR LOWER CURVE EDGE AFT TEE SECTION CORRODED. REPLACED TEE SECTION IAW SRM 51-42-11 AND SRM A32 0 51-44-11. REMOVED CORROSION IAW SRM 51-74-00, NO LIMITS FOUND IN SRM A320 52-20-00.

Part: WEB — GOUGED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD CARGO THRESHOLD WEB HAS DEEP GOUGE 7" AFT OF FR26. REPLACED DAMAGED THRESHOLD WEB IAW DWG 53230315 & SRM 51-42-11.

Part: STRUCTURE — CORRODED (EMERGENCY EXIT) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND LT FWD EMERGENCY EXIT DOOR LOWER CURVE EDGE FWD TEE SECTION HAS CORROSION. REPLACED TEE SECTION IAW SRM 51-42-11 AND SRM 51-44-11. REMOVED CORROSION IAW SRM 51-74-00, NO LIMITS FOUND IN SRM 52-20-00.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131HF HAS MULTIPLE DENTS & SCRATCHES. FABRICTATED FLOOR PANEL IAW SRM 53-02-00 FIG 209 & DWG 3D25-37705.

Part: HINGE FITTING — DAMAGED (LT MLG DOOR) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND LT MLG DOOR FWD HINGE AFT LUG, INBD SIDE IS CHAFED. NO ESTABLISHED LIMITS IAW SRM 53-36-11, PAGE 101. REPLACED FITTING IAW DWG R53370500C & SRM 51-42-11.

Part: FITTING — OUT OF ADJUST (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND RT SIDE OF FWD FUSELAGE BETWEEN FR3 - FR4 STATIC PORT FITTING REQUIRES REPLACEMENT. REMOVED STATIC FITTING IAW SRM 51-42-11. LOCATED AND DRILLED REPLACEMENT FITTING IAW DWG R53112169, SH 2, REV A INSTALLED FITTING IAW SRM 51-42-11 AND DWG 53112169 SH 2, REV A.

Part: HINGE FITTING — DAMAGED (LT MLG DOOR) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND LT MLG DOOR FWD HINGE, FWD LUG, FWD FACE HAS CHAFE DAMAGE, FITTING R & R IAW REPAIR DWG R53370500C & SRM 51-42-11.

Part: PLATE — CORRODED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO BAY CENTER SEALING PLATE CRACKED AROUND SCREW HOLE AND FITTING ATTACHMENT CORRODED. REMOVED SEALING PLATE AND TIE DOWN FITTING IAW SRM 51-42-11. FABRICATED NEW SEALING PLATE IAW DWG D53974839. INSTALLED NEW SEALING PLATE AND TIE DOWN FITTING IAW SRM 51-42-11.

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 132DF CORRODED AND GOUGED. REPLACED FLOOR PANEL IAW SRM 51-72-11.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD UTILITY FLOOR PANEL 231AF HAS CORROSION ON HINGE AND PANEL. REPLACED FLOOR PANEL.

Part: FLOOR SUPPORT — BENT (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO BAY FR 58-59 FLOOR SUPPORT BENT AT FWD CORNER & CORRODED AROUND SCREW HOLE. REMOVED CORROSION IAW 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. REPLACED FLOOR SUPPORT IAW SRM 51-44-11 AND SRM 51-42-11, APPLIED TOP COAT TO FASTENERS IAW SRM 51-75-12.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152KF CORROSION ON LOWER SIDE. DAMAGE DIA L=6" X W=18" NO ALLOWABLE LIMIT ON SRM, REPLACED AFT CARGO FLOOR PANEL IAW SRM 51-72-11.

Part: FLOOR PANEL — PUNCTURED (FWD CABIN) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 221AF HAS PUNCTURED 1" X 1". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND LOWER FWD FUSELAGE RT SIDE AT FR 30, S39R EXTERNAL SKIN HAS LIGHTNING STRIKE AS MARKED. DRILLED OUT DAMAGE FASTENER IAW SRM 51-42-11, PERFORMED HFEC ROTARY PROBE INSPECTION OF ONE OPEN FASTENER HOLE IAW NTM 51-10-01 WITH NO INDICATIONS NOTED. COLD WORKED FASTENER HOLE TO 4-4-N & FINAL REAMED HOLE TO 0.189" IAW SRM 51-48-00 SRM 53-21-11.

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 232DF HAS TWO BAD INSERTS. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — CORRODED (FWD CABIN) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 222FF HAS CORROSION. REPLACED FLOOR PANEL IAW SRM 51-72-11.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND LOWER FORWARD FUSELAGE RT SIDE AT FR 30, STGR 39R EXTERNAL SKIN HAS LIGHTNING STRIKE. DRILLED OUT DAMAGE FASTENER IAW SRM 51-42-11, PERFORMED HFEC ROTARY PROBE INSP OF 1EA OPEN FASTENER HOLE IAW NTM 51-10-01 WITH NO INDICATIONS NOTED. COLD WORKED FASTENER HOLE TO 4-4-N & FINAL REAMED HOLE TO 0.189" IAW SRM 51-48-00 & SRM 53-21-11, FIG 213. INSTALLED FASTENER IAW SRM 51-42-11 & SRM 53-21-11, FIG 213.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

LOWER FWD FUSELAGE EXTERNAL SKIN BETWEEN FR26-27 STRGR 40R HAS 2EA LIGHTNING STRIKE. DRILLED OUT DAMAGE FASTENER IAW SRM 51-42-11, PERFORMED HFEC ROTARY PROBE INSPECTION OF ONE OPEN FASTENER HOLE IAW NTM 51-10-01 WITH NO INDICATIONS NOTED. COLD WORKED FASTENER HOLE TO 4-4-N & FINAL REAMED HOLE TO 0.189" IAW SRM 51-48-00 & SRM 53-21-11, FIG 213. INSTALLED FASTENER IAW SRM 51-42-11 & SRM 53-21-11, FIG 213.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND LOWER FWD FUSELAGE EXTERNAL SKIN BETWEEN FR 26-27 S40R HAS TWO LIGHTNING STRIKES. DRILLED OUT DAMAGE FASTENER IAW SRM 51-42-11, PERFORMED HFEC ROTARY PROBE INSPECTION OF ONE OPEN FASTENER HOLE IAW NTM 51-10-01 PT6 WITH NO INDICATIONS NOTED. COLD WORKED FASTENER HOLE TO 4-4-N & FINAL REAMED HOLE TO 0.189" IAW SRM 51-48-00 & SRM 53-21-11, FIG 213. INSTALLED FASTENER IAW SRM 51-42-11 & SRM 53-21-11 FIG 213.

Part: WEB — DAMAGED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD FUSELAGE RT UPPER SPLICE SUPPORT WEB APPROX STR 4R BETWEEN FR 1 & FR 3 HAS SEVERAL TOOL MARKS. REPLACED RT UPPER SPLICE SUPPORT WEB IAW SRM 51-42-11. TOP COATED AREA IAW SRM 51-75-12.

Part: FLOOR PANEL — CORRODED · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FLOOR PANEL 261FF HAS LIGHT CORROSION. REMOVED CORROSION IAW SRM 51-74-00, REPLACED FLOOR PANEL, IAW SRM 51-72-11.

Part: SKIN — GOUGED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND LOWER FUSELAGE 3IN FWD OF FR51 AND ONE INCH BELOW STRG 41L HAS SKIN GOUGE. BLENDED AREA IAW 51-73-00, FOUND TO BE OUT OF LIMITS IAW SRM 53-41-11, FIG 101, MATERIAL LOSS IS MORE THAN 25 PERCENT OF THICKNESS. PERFORMED EXTERNAL DOUBLER REPAIR IAW SRM 53-00-11, FIG 224.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND LWR AFT FUSELAGE LAV VENT, FUSELAGE SKIN BETWEEN STGR 29R AND STG R 30R, BETWEEN FR69 AND FR70 HAS CRACK ON SKIN NEXT TO VENT. CUT OUT DAMAGE SKIN, FABRICATED 1EA REPAIR DOUBLER FROM 2024-73 .071"C & 2 EA FILLERS FROM 2024-73 .063"C, LOCATED & DRILLED PARTS IAW SRM 53-41-11, FIG 205,TREATED & PRIMED AREA IAW SRM 51-21-11. INSTALLED REPAIR PARTS IAW SRM 53-41-11, FIG 205.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND LWR AFT FUSELAGE LAV BENT, FUSELAGE SKIN BETWEEN STGR 29R AND STGR 30R, BETWEEN FR69 AND FR70 HAS CRACK ON SKIN NEXT TO BENT. CUT OUT DAMAGE SKIN, FABRICATED REPAIR DOUBLER & TWO FILLERS, LOCATED & DRILLED PARTS IAW SRM 53-41-11, FIG 205, TREATED & PRIMED AREA IAW SRM 51-21-11. INSTALLED REPAIR PARTS IAW SRM 53-41-11, FIG 205. PAINTED INTERNAL & EXTERNAL AREA OF REPAIR IAW SRM 51-75-1.

Part: SKIN — DENTED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND LT SIDE OF FWD FUSELAGE AT FR15 WHERE DOOR STOP TOUCHES ACFT SKIN DENT IS OUT OF NEARNESS TO FRAME. DENT FOUND FWD OF FRAME 15 BETWEEN STR 19 & 20 NO ALLOWABLE DAMAGE IAW SRM 53-11-11, FIG 201. CUT-OUT DAMAGE AREA IAW SRM 53-11-11, FIG 212.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FLOOR PANEL 261EF CORRODED IN SEVERAL PLACES. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209, DWG 3D25-37498.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FLOOR PANEL 261PF HAS EDGE DAMAGE. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209, & DWG 3D25-37498.

Part: FLOOR PANEL — PUNCTURED (FWD CABIN) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 221AB HAS TWO PUNCTURES. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 DWG 3D25-37498 .

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FLOOR PANEL 262AB HAS NUMEROUS PUNCTURES. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37498.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD UTILITY AREA FLOOR PANEL 232MF IS CRACKED 12 INCHES. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 DWG 3D25-37498.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FLOOR PANEL 261DF IS DELAMINATED. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209, & DWG 3D25-37498.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD UTILITY FLOOR PANEL 232FF HAS PUNCTURE. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209, DWG 3D25-37498.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FLOOR PANEL 262EF HAS CORROSION. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37498.

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 222CF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209, & DWG 3D25-37498.

Part: SEAT TRACK — CORRODED (FWD CABIN) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FORWARD CABIN SEAT TRACK BETWEEN FR 20-24, Y-1292. SEAT TRACK CROWN AND UPPER SURFACE FLANGE HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15, FIG 101. REPLACED SEAT TRACK IAW SRM 51-42-11.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131KF HAS MULTIPLE DENTED & CRACKED. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 152QF DAMAGE. L=3" X W=1". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 162BF DAMAGED. FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151QF DAMAGE. L=3" X W=2" . FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 152FF DAMAGED. FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151GF DAMAGED, L=3" X W=1". FABRICATED FLOOR PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151FF PUNCTURED. FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DELAMINATED (FWD CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 132JF DELAMINATED. L=4" X W=2". FABRICATED FLOOR PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131JF HAS GOUGES AND DELAMINATED. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 152RF DAMAGE, L=2" X W=1". FABRICATED NEW PANEL.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151HF DAMAGE. L=3" X W=1" FABRICATED SLOPE PANEL.

Part: FLOOR PANEL — DELAMINATED (FWD CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 132KF DELAMINATED. L=8" X W=8". FABRICATED FLOOR PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 161BF DAMAGE. L=4" X W= .50". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151JF DAMAGE L=3" X W=1". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DELAMINATED (FWD CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131FF HAS DEEP SCRATCH & DELAMINATED. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151PF DAMAGE, L=3" X W=1". FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131CF PUNCTURED & DELAMINATED. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151NF DAMAGED. FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131AF HAS MULTIPLE DENTS & DELAMINATED. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 152EF DAMAGED. FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151LF DAMAGE, L=3" X W=1.5". FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151RF DAMAGED, L=4" X W=1". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DELAMINATED (FWD CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 132FF DELAMINATED. L=7" XW=4". FABRICATED FLOOR PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FWD CARGO FLOOR PANEL 131EF HAS MULTIPLE DENTS & DELAMINATED. L=2' X W=4'. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151BF DAMAGE. L=3' X W=1'. FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 161AF DAMAGED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 152BF DAMAGE. L=3" X W= .5". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 132GF HAS PUNCTURE & CRACKED. L=7" X W=1". FABRICATED FLOOR PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151CF DAMAGED. FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 152NF DAMAGE, L=3" X W=1". FABRICATED PANEL.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 152MF DAMAGE, CRACKED 1INCH LONG TWO PLACES. FABRICATED NEW PANEL.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151EF DAMAGED. FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151DF DAMAGED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131BF CRACKED AND DELAMINATED. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.

Part: HINGE PIN — GOUGED (LT AILERON) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND LT AILERON HINGE PINS NR1, NR2, NR3, NR4 AND NR5 HAS SCORED AND GOUGED. PINS INSTALLED ON JIC 5760-1010S-LT. NO SPECIFIC LIMITS IAW AMM 27-14-41-420-053-A.

Part: FITTING — CORRODED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND LT AFT PASSENGER ENTRANCE MID SEAL SHAPE FITTING CORRODED. R & R SEAL SHAPE PN D53480048202 BATCH 2433458 IAW SRM 51-42-11 & 51-44-11 & DWG NR 18 D53480020. REMOVED CORROSION IAW SRM 51-74-00 L=1.5" W=.500" D=.040 NO ESTABLISHED LIMITS IAW SRM 53-41-14.

Part: FLOOR SUPPORT — CORRODED (AFT CABIN) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR66 -FR68, Y1292 UPPER SURFACE FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, FOUND TO BE OUT OF LIMITS IAW SRM 53-41-15, FIG. 1. REMOVED FLOOR SUPPORT IAW SRM A320 51-42-11. INSTALLED EIGHT SPLICE ANGLES IAW SRM 51-42-11. LOCATED AND DRILLED NEW FLOOR SUPPORT IAW 51-44-11. TREATED & PRIMED IAW SRM 51-21. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.

Part: FLOOR SUPPORT — CORRODED (AFT CABIN) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR65 -FR66, Y1292 UPPER SURFACE FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO OUT OF LIMITS IAW TRM 53-41-15. REMOVED FLOOR SUPPORT IAW SRM A320 51-42-11. LOCATED AND DRILLED NEW FLOOR SUPPORT IAW SRM 51-44-11. TREATED & PRIMED IAW SRM 51-21-11. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR68 - FR69, Y1292 UPPER SURFACE FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. REMOVED FLOOR SUPPORT IAW SRM 51-42-11 AND INSTALLED IAW SRM 51-44-11.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOORBEAM BETWEEN FR68-69 Y-1292 UPPER & LOWER SURFACE FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 L=2.5" W=2" D=.085" FOUND OUT OF LIMITS IAW TRM 53-41-15, FIG 1. REMOVED FLOORBEAM, PN D5347218920200 IAW SRM 51-42-11 & TRM 53-21-01.

Part: HINGE PIN — GOUGED (AILERONS) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND RT AILERON HINGE PINS NR 1, 2, 3, 4 & 5 SCORED & GOUGEED. HINGE PINS INSTALLED ON JIC 5760-1010S-RT. FOUND RT ORIGINAL AILERON PINS GOUGED L=.020"X W=.015"X D=.003" NO SPECIFIC LIMITS IAW AMM 27-14-41-420-053-A.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOORBEAM BETWEEN FR66 TO FR68, Y-1292 UPPER & LOWER SURFACE FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 L=2." W=2" D=.037" FOUND OUT OF LIMITS IAW TRM 53-41-15, FIG 1. REPLACED FLOORBEAM PN D534721722090 IAW SRM 51-42-11 & TRM 53-21-01.

Part: BEAM — CORRODED (SILL) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND LT AFT PASSENGER DOOR SILL BEAM AT FWD FR68 UPPER SURFACE & HOLES HAS CORROSION. REPLACED DOOR SILL IAW SRM A320 51-42-11,SRM A320 51-44-11 AND DWG D53480020, D53470150, PN D5348004320601 BATCH 1848855. FOUND TO BE OUT OF LIMITS L=5.0" X W=1.5" X D=.080" IAW SRM 53-41-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOORBEAM AT FR 66, Y-1292 UPPER & LANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 L=2.3" W=1.9" D=.045" FOUND OUT OF LIMITS IAW TRM 53-41-15, FIG 1. REPLACED FLOORBEAM PN D5347219020500 IAW SRM 51-42-11 & TRM 53-21-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOORBEAM BETWEEN FR65 -FR67, Y-308 HARD POINT HOLES HAS CORROSION. BLENDED AREA AND CHECKED LIMITS L=2.0" W=1.5" D=0.020" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14 AND SRM 51-74-00. REPLACED FLOORBEAM WITH PN D5347228200200 BATCH NR 0002433497 IAW TRM 53-21-01 AND SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FWD CABIN FLOORBEAM BETWEEN FR20 -FR23Y-189 UPPER SURFACE FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS MEAS. AS FOLLOWS L=4" W=1.5" D=.034 OUT OF LIMITS IAW SRM 53-11-14, FIG 105. R & R FLOORBEAM PN D5311283620200, BATCH 0002433494 IAW SRM 51-42-11 AND TRM 53-21-01.

Part: SILL — CORRODED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND L1 DOOR SILL, CTR SHAPE SILL CORRODED AROUND FASTENER HOLES. REMOVED CORROSION IAW SRM 51-74-00 L=8.0" W=1.0" D=.030", FOUND OUT OF LIMITS IAW SRM 53-11-14, FIG 101. REPLACED SHAPE SILL PN D5311219820000 IAW SRM 51-42-11.

Part: SILL — CORRODED (PAX DOORWAY) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND RT AFT PASSENGER DOOR SILL BEAM AT AFT FR66 UPPER SURFACE & HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, CHECKED LIMITS DIMENSION HOLES .543" FOUND TO BE OUT OF LIMITS IAW TRM 53-41-13, FIG 1. REPLACED DOOR SILL PN D5348004320701 IAW D-53480019 & SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FORWARD CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR16 TO FR24, Y254 UPPER FLANGE HAS CORROSION AND SCRIBE LINE. BLENDED AREA IAW SRM 51-74-00, L=2.2" W=1.850" D=0.036 FOUND OUT OF LIMITS IAW SRM 53-11-14, FIG 106. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND SEAT TRACK & UPPER FLANGE HAS CORROSION. BLENDED AREA IAW SRM 51-74-00, L=3.5" W=0.600" D=0.015 FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 101. REPLACED IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION FOUND AFT CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR66-FR68 Y-765 UPPER SURFACE FLANGE HAS CORROSION. REMOVED CORROSION AND CHECKED LIMITS L=2.0" W=0.8" D=.045" FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15 AND SRM 51-74-00. REPLACED FLOOR SUPPORT IAW TRM 53-21-01 AND SRM 51-42-11.

Part: WEB — CORRODED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FORWARD CABIN RT SIDE FR 20 STRINGER 23R UPPER SURFACE WEB HAS CORROSION. REPLACED FORWARD CABIN RT SIDE FR20 STRG 23R UPPER SURFACE WEB IAW SRM 51-42-11, 51-44-11, 51-21-11. L=2" W=1.5" D=0.020 NO ALLOWABLE LIMIT IAW SRM 53-11-14, FIG 101.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR64-66, Y-765 UPPER SURFACE FLANGE CORROSION. REMOVED CORROSION AND CHECKED LIMITS L=1.8" W=1.5" D=.055" FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15 AND SRM 51-74-00. REPLACED FLOOR SUPPORT IAW TRM 53-21-01 AND SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOOR SUPPORT -Y765 BETWEEN FR68 - FR67 INBD & OTBD UPPER SPLICES HAS CORROSION. REPLACED TWO SPLICES IAW 51-42-11, NO ESTABLISHED LIMITS IAW SRM 51-41-14, FIG 101.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR67 -FR68, Y765 UPPER SURFACE FLANGE HAS CORROSION & SCRIBE LINE MARK. BLENDED AREA AND REMOVED CORROSION IAW SRM 51-74-00,L=3.5" W=1.5" D=.035" FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. REPLACED FLOOR SUPPORT IAW SRM 51-44-11 AND TRM 53-21-01, RESTORED FINISH IAW SRM 51-75-12.

Part: STRUCTURE — CORRODED (CABIN) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND FORWARD CABIN UTILITY AREA AT FR 16, Y765 UPPER FLANGE HAS CORROSION. BLENDED CORROSION IAW SRM 51-74-00. CHECKED LIMITS; LENGTH = 2.5" WIDTH = 2.0" DEPTH = .040", FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 102. REPLACED BEAM IAW SRM 51-42-11 & TRM 53-21-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOOR SUPPPORT BETWEEN FR 68-70, Y254 UPPER SURFACE FLANGE & HARD POINTS HOLES INSIDE HAS CORROSION. REMOVED CORROSION AND BLENDED AREA IAW SRM 51-74-00, L=.750", W=.250, "D=.026" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG 102, R & R FLOOR SUPPORT IAW SRM 51-42-11, 51-44-11

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 67,788 hrs · 29,938 cycles

DURING INSPECTION, FOUND AFT CABIN UTILITY ARE FLOOR SUPPORT BETWEEN FR 64-66, Y765 UPPER SURFACE FLANGE HAS CORROSION. BLENDED AREA L=1.8",W=1.8"D=.034", MAX ALLOWABLE D=.027" AND FOUND TO BE OUT OF LIMIS IAW TRM 53-41-15 AND SRM 51-74-00. REPLACED FLOOR SUPPORT IAW SRM 51-42-11, SRM 51-44-11 AND TRM 53-21-01.

Part: EPSU — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,576 hrs · 29,834 cycles

DURING NON ROUTINE CHECK, FOUND EXIT SIGNS ABOVE DOORS 1L, 1R AND FWD CABIN AISLE ROW 1 ARE INOPERATIVE. MX REPLACE EPSU AT 10WL AND FUNCTIONAL CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,116 hrs · 29,602 cycles

DURING THE TEST OF EMERGENCY LIGHT, TEST FAULT AT FWD L AND R, AND L AFT R. MAINTENANCE REPLACED DOOR 1L EPSU AND BATTERY. FUNCTIONAL TESTED NORMAL.

Part: HYDRAULIC SYSTEM — LOW PRESSURE (GREEN SYSTEM) · airframe 66,844 hrs · 29,482 cycles

AFTER RAISING GEAR AFTER TAKE OFF, LOST GREEN HYD SYSTEM QTY WENT TO ZERO. HYD G RSVR LOW LEVEL ECAM. QRH PROCEDURES FOLLOWED. PINNED AND TOWED TO GATE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 6,223 hrs · 2,717 cycles

DURING SERVICE CHECK, FOUND THE LEFT EMERGENCY POWER SUPPLY UNIT AT 10WL FAILED TEST. MAINTENANCE REPLACED POWER SUPPLY UNIT AND FUNCTIONAL CHECK WAS NORMAL. A/C RETURNED TO SERVICE.

Part: POST — DAMAGED (FUSELAGE) · airframe 4,421 hrs · 1,869 cycles

THE VERTICAL STIFFENER POST P/N D53113-5201 ON THE AFT OF THE FRAME FR1 PRESSURE BULKHEAD WEB SUSTAINED DEFORMATION AT Y=675 Z=169 DUE TO A BIRD STRIKE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 64,114 hrs · 28,199 cycles

BIRD STRIKE JUST BELOW F/O`S WINDSCREEN. POST REPAIR C/W ON ERA 495670-14 REV ORIG. ALL STEPS MATCH. PERMANENT REPAIRS ACCOMPLISHED. SKIN REPAIR C/W ON ERA 495514-1 4 REV ORIG. ALL STEPS MATCH PRIS.

Part: PANEL — CRACKED (NR 1 PYLON) · airframe 64,114 hrs · 28,199 cycles

NR 1 ENG PYLON TO WING PANEL 471AL HAS A CRACK AT L/E. REPAIRED PANEL PERMANENT PER ERA 495620-14 REV ORIG. PAINTED PER 51-35-00 A-320. IDENTIFIED PART PER ERA 495620-14 ORIG. INSTALLED PANEL 471AL PER A320 AMM 54-52. PERM REPAIR ACCOMPLISHED PER ERA 495620-14 REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 67,815 hrs · 29,954 cycles

RT FUSELAGE SKIN DAMAGED, REPLACE WITH NEW SKIN IAW ER/A 512316-14.

Part: LENS — WRONG PART (EMERGENCY LIGHT) · airframe 62,106 hrs · 27,329 cycles

DURING OVER NIGHT LINE CHECK FOUND SEAT 26C PATH LIGHT WITH WRONG COLOR LENS, INSTALLED RED LENS AND CHECKS OK.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 61,645 hrs · 27,137 cycles

DURING L CHECK FOUND FORWARD CARGO PIT FLOOR PANEL 131HF DAMAGED. REMOVED FLOOR PNL 131HF IAW AMM 53-22-14-020-050. FLOOR PNL 131HF FABRICATED IAW SRM 53-02-00 FIG 201. INSTALLED FLOOR PNL 131HF IAW AMM 53-22-14-400-001.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 61,645 hrs · 27,137 cycles

DURING L-CHECK FOUND FORWARD CARGO PIT FLOOR PANEL 131AF DAMAGED. REMOVED FLOOR PNL 131AF IAW AMM 53-42-14-020-050. FABRICATED NEW FLOOR 131AF IAW SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 61,645 hrs · 27,137 cycles

DURING L-CHECK FOUND AFT PIT FLOOR PANEL 151LF IS DELAMINATED, 3 X 3 INCH AREA. REMOVED FLOOR PNL 151LF IAW AMM 53-42-14-020-050. RECEIVED NEW FLOOR PNL 151LF IAW SRM 53-02-00 FIG 201. INSTALLED FLOOR PNL 151LF IAW AMM 53-42-14-14-400-001.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 61,645 hrs · 27,137 cycles

DURING L-CHECK FOUND AFT PIT FLOOR PANEL 151DF IS DELAMINATED, 5" X 3" AREA. REMOVED FLOOR PNL 151DF IAW AMM 53-42-14-020-050. RECEIVED NEW FLOOR PANEL 151DF ON TRAVELER NR T10/860791 MATERIAL NR A402 AB-60X144, BATCH NR 1910500 IAW SRM 53-02-00 FIG 209. INSTALLED FLOOR PANEL 151DF IAW AMM 53-42-14-14-400-001.

Part: LINE — LEAKING (HYD SYSTEM)

ECAM MESSAGE: HYD B RSVR LO LVL, FOLLOWED COM PROC 2.29.5. ACFT LANDED UNEVENTFULLY. SECURED FITTINGS ON BLUE HP MANIFOLD. REPLACED RETURN-LINE UNION (I/P 0014316). BRACKETS/CLAMPS (I/P 0014319). FILTERS (I/P 0013907). BLUE ELECTRIC PUMP (I/P 0014418). (K)

Part: PUMP — MALFUNCTIONED (HYD SYSTEM)

OUT OF AIRPORT, AT APPROX 20,000 FT, RECEIVED "HYD GREEN RSVR LO LVL" CAUTION. FOLLOWED COM, LANDING GEAR GRAVITY EXTENDED AND LANDED UNEVENTFULLY. CORRECTION WAS TO REPLACE HYD LINE IN LT WHEEL WELL AND NR 1 ENG DRIVEN PUMP IAW LOG PAGES 4568789 AND 0011489. (K)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,626 hrs · 21,288 cycles

SEVERAL REPORTS OF EMERGENCY EXIT SIGNS AT 2L AND 2R DOORS INOP. REMOVED AND REPLACED POWER SUPPLY 13WL. NWA STK 32-3350-9-0010, S/N OFF 00447.

Part: TURBINE CASE — PUNCTURED (APU)

DURING MAIN ENGINE START, APU SHUT DOWN.. MAINTENANCE FOUND A HOLE IN APU COMPRESSOR CASE, NO AC DAMAGE NOTED. REPLACED THE APU. CHECKED OK.

Part: VALVE — LEAKED (HYD SYSTEM)

AFTER CLIMB, RECEIVED HYD Y RSVR LO LVL MESSAGE. FOLLOWED COM PROCEDURES AND DIVERTED TO MEM WITH AN UNEVENTFUL LANDING. MAINTENANCE REPLACED LEAKING PARK BRAKE VALVE. OPERATIONAL CHECK OK.

Part: ACTUATOR — FAILED (NR 1 SPOILER ACT)

DURING CRUISE, LOST GREEN HYDRAULIC SYSTEM FLUID. FLIGHT DIVERTED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING SPOILER ACTUATOR, OPERATIONAL CHECK OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING LINE MAINTENANCE TEST, THE AFT LEFT EMERGENCY POWER SUPPLY FAULTED. REPLACED EPSU. OPERATIONAL CHECK OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS TEST FAULTS AFT LT BAT CAP. REPLACED POWER SUPPLY UNIT. OPERATIONAL CHECK OK.

Part: FUEL TANK — CONTAMINATED (NR 1 MAIN)

DURING CLIMBOUT, BOTH LEFT MAIN FUEL PUMPS WENT TO LOW PRESSURE WHEN CLIMB POWER WAS CALLED FOR. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED ICE AND WATER FROM THE NR 1 FUEL TANK. OPERATIONAL CHECK OK.

Part: SILL — CORRODED (DOOR 2R)

DURING IL CHECK, FOUND CORROSION ON THE DOOR 2R LOWER SILL. REPAIRED SILL (P/N D534-80043-205), PER EA 32-104299.

Part: SILL — CORRODED (LT/RT SERV DOOR)

DURING IL CHECK, FOUND CORROSION IN BOTH THE LEFT AND RIGHT AFT SERVICE DOOR LOWER SILLS. REPAIRED SILLS (P/N D534-80043-204, -205), PER EA 32-104298, -104291 RESPECTIVELY.

Part: HYD PUMP — LEAKING (NR 1 ENGINE)

DURING CRUISE AT FL 370 APPROXIMATELY ONE HOUR INTO FLIGHT, THE GREEN HYDRAULIC SYSTEM QUANTITY DROPPED TO ZERO. THE POWER TRANSFER UNIT AND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP WERE DISCONNECTED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND CONTINUED TO DTW WHERE AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL LANDING ACCOMPLISHED. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRALUIC PUMP LEAKING. REPLACED THE NR 1 EDP. LEAK AND OPERATIONAL CHECK OK.

Part: HANDLE — NOT SECURE (AFT CARGO DOOR)

DURING TAKEOFF ROLL, THE AFT CARGO DOOR INDICATED OPEN. THE TAKEOFF WAS ABORTED. MAINTENANCE FOUND THE AFT CARGO DOOR HANDLE POPPED OUT 0.5 INCH. SECURED DOOR HANDLE AND ALL INDICATIONS AND OPERATION NORMAL.

Part: INDICATION — MALFUNCTION (LT MLG DOOR)

DURING CLIMB-OUT FROM MKE AFTER LANDING GEAR RETRACTION, THE LEFT MAIN LANDING GEAR DOOR DID NOT INDICATE FULLY CLOSED. CYCLED THE LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT CONTINUED AND LANDED IN MSP WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES.