N915FR

ATA 5321

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 21,062 hrs · 9,025 cycles

LINE MECHANIC NOTED THE AFT CARGO PIT TRANSITION PANEL 151AE WAS DAMAGED. MAINT REPAIRED DAMAGED PANEL 151AE IAW SRM 53-02-00, STEP 2, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

ATA 5270

Part: PROXIMITY SWITCH — FAILED (L1 DOOR) · airframe 20,422 hrs · 8,755 cycles

REFERENCE NON ROUTINE C045163. DURING C4 S1 C-CHECK INSPECTION NOTED CHECK DOOR SWITCH POWER SUPPLIED BY EMERGENCY LIGHT SYSTEM FAILS AT PAGE 4 STEP 3, WORK CARD C335004-2 FOR THE FORWARD DOORS AND WORK CARD C335004-2 AT PAGE 6 STEP 8 FOR THE L1 DOOR. MAINTENANCE REMOVED AND REPLACED PROXIMITY SWITCH 13WVI IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 52-71-11-400-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE AND OPERATIONAL CHECKED GOOD. (A)

ATA 5320

Part: PLATE — CORRODED (L1 GIRT BAR) · airframe 20,422 hrs · 8,755 cycles

DURING C-CHECK INSP, NOTED L1 DOOR GIRT BAR PLATE ON SILL IS CORRODED. MAINT REMOVED OLD GIRT BAR PLATE, FABRICATED NEW PLATE AND INSTALLED NEW GIRT BAR PLATE IAW DRAWING 351-1234 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5320

Part: SILL — CORRODED (FUSELAGE) · airframe 20,422 hrs · 8,755 cycles

DURING C-CHECK INSP, NOTED UPON CLOSURE OF AFT PIT CORROSION WAS FOUND ON THE SILL WEDGE PANEL 152YG. MAINT INSTALLED A NEW PANEL IAW WORK CARD CP753-25. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · airframe 20,422 hrs · 8,755 cycles

DURING C-CHECK INSP NOTED AFT CARGO FLOOR FRAME 59 HAS CORROSION AT NUTPLATE HOLES. MAINT REPAIRED HOLES WITH REPAIR DOUBLERS IAW EA A9-53R-30346. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) THE PERMANENT REPAIR FOR CORROSION DAMAGE WAS DEFERRED FOR 500 FLIGHT CYCLES. CUT AND REMOVED DAMAGED FRAME SECTION AND SLICED IN NEW SECTION, PN D53477711000000. MX WAS COMPILED WITH IAW EO A9-53R-30346. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. PERMANENT REPAIR ACCOMPLISHED AT AIRCRAFT TT: 21534 AND TOTAL CYCLES: 9251

ATA 5321

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,422 hrs · 8,755 cycles

REFERENCE NON ROUTINE C044797. DURING C4 S1 C-CHECK INSPECTION NOTED PANEL 222FF HAS SEVERE CORROSION ON BOTTOM SIDE. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF WORK CARD CP753-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5321

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,422 hrs · 8,755 cycles

REFERENCE NON ROUTINE C044808. DURING C4 S1 C-CHECK INSPECTION NOTED PANEL 222EF SPLICE PLATE CORRODED. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL SPLICE PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF WORK CARD CP753-12. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5320

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,422 hrs · 8,755 cycles

REFERENCE NON ROUTINE C044450. DURING C4 S1 C-CHECK INSPECTION NOTED FORWARD CARGO PIT PROFILE FOR LOWER AFT BULKHEAD HAS CORROSION IN NUT PLATE HOLES FROM STRINGER 28 LT TO STRINGER 28 RT. MAINTENANCE REMOVED AND REPLACED PROFILE AT STRINGER 28 LT TO STRINGER 28 RT IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-44-11 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 20,422 hrs · 8,755 cycles

REFERENCE NON ROUTINE C044879. DURING C4 S1 C-CHECK INSPECTION NOTED AFT CARGO COMPARTMENT STANCHION RECEPTABLE AND AREA CORRODED AT FLOOR FRAME 56 AND STRINGER 37 RT. MAINTENANCE REPAIRED IN ACCORDANCE WITH EA A9-53R-30365 AND SRM 51-42-11, SRM 51-75-12, SRM 51-21-11 AND NTM 51-10-01 AND AIRBUS DRAWING 53477067. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5321

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,422 hrs · 8,755 cycles

REFERENCE NON ROUTINE C044794. DURING C4 S1 C-CHECK INSPECTION NOTED PANEL 221FF HAS LITE CORROSION ON BOTTOM SIDE. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 221FF IN ACCORDANCE WITH THE REQUIREMENTS OF WORK CARD SP753-12. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5315

Part: FLOORBEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 20,422 hrs · 8,755 cycles

REFERENCE NON ROUTINE C044885. DURING C4 S1 C-CHECK INSPECTION NOTED AFT CARGO COMPARTMENT FLOOR FRAME 59 U-CHANNEL IS CORRODED FROM STRINGER 41 RT TO STRINGER 38 LT. MAINTENANCE REMOVED AND REPLACED U-CHANNEL IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-44-11 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 20,422 hrs · 8,755 cycles

REFERENCE NON ROUTIN C044731. DURING C4 S1 C-CHECK INSPECTION NOTED CORROSION ON OUTBOARD NUT CLIP HOLE 2 INCHES FORWARD OF FRAME 66 ON FLOORBEAM Y1732 LT. MAINTENANCE REPAIRED FLOORBEAM Y1732 LT IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30354, SRM 51-44-12, SRM 51-42-11 AND SRM 53-41-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5320

Part: PROFILE — CORRODED (FUSELAGE) · airframe 20,422 hrs · 8,755 cycles

REFERENCE NON ROUTINE C044887. DURING C4 S1 C CHECK INSPECTION NOTED AFT CARGO COMPARTMENT FLOOR FRAME CAP AT FRAME 59 FROM STRINGER 38 LT TO STRINGER 38 RT IS CORRODED. MAINTENANCE REMOVED FRAME 59 PROFILE, UPSIZED AND COUNTERSUNK HOLES AS REQUIRED, INSTALLED NEW PROFILE ON FRAME 59 FROM STRINGER 38 LT AND STRINGER 38 RT IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11, SRM 51-44-00, SRM 51-44-11 AND SRM 51-46-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5321

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 20,422 hrs · 8,755 cycles

REFERENCE NON ROUTINE C44993. DURING C4 S1 C-CHECK INSPECTION NOTED AFT PIT FLOOR PANEL 151VG HAS A 2 INCH SECTION MISSING ON TOP PIECE SHOWING COMPOSITE ALONG EDGE. MAINTENANCE CUT OUT DAMAGE, TRIMMED CORE, INSTALLED NEW CORE AND REPAIRED LOWER SKIN FLOOR PANEL 151VG IN ACCORDANCE WITH THE REQUIREMENTS OF EA A0-53T-10131 AND AMM 25-00-00-370-003. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5320

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,422 hrs · 8,755 cycles

DURING C4 S1 C-CHECK INSP, NOTED AFT CARGO COMPARTMENT LT FLOOR PROFILE IS CORRODED FROM FRAME 51 TO FRAME 56 AT STRINGER 38 LT. MAINT REMOVED AND REPLACED LT HAND FLOOR PROFILE IAW SRM 51-42-11 PARAGRAPH 5. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,422 hrs · 8,755 cycles

DURING C-CHECK INSP, NOTED CORROSION ON FLOOR TRACK AT Y189 FRAME 20. MAINT REMOVED DAMAGED FLOORBEAM Y189 AND INSTALLED NEW FLOORBEAM FROM FRAME 20 TO FRAME 24 IAW SRM 51-42-11 PARAGRAPH 7. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,422 hrs · 8,755 cycles

REFERENCE NON ROUTINE C044835. DURING C4 S1 C-CHECK INSPECTION NOTED CORROSION ON SEAT TRACK AT Y1292 BETWEEN FRAME 19 AND FRAME 20. MAINTENANCE REMOVED AND REPLACED BEAM IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. UPON COMPLETION OF THE REPAIR IN WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 20,422 hrs · 8,755 cycles

DURING C-CHECK INSP NOTED THE CENTER LONGITUDINAL FLOORBEAM FROM FRAME 58 TO FRAME 59 HAS CORROSION AROUND THE FWD NUTPLATE HOLE. MAINT REPAIRED THE FLOORBEAM IAW EA A9-53R-30355 AND SRM 51-75-00, SRM 53-00-14 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5320

Part: PANEL — PUNCTURED (CARGO BAY) · airframe 20,422 hrs · 8,755 cycles

REFERENCE NON ROUTINE C044396. DURING C4 S1 C CHECK INSPECTION NOTED AFT PIT TRANSITION PANEL 151AE HAS PUNCTURE DAMAGE. MAINTENANCE REMOVED DAMAGE, CLEANED PANEL AND REPAIRED PUNCTURE DAMAGE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5321

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 20,422 hrs · 8,755 cycles

DURING C-CHECK INSP, NOTED AFT PIT FLOOR PANEL 151PE HAS SURFACE CORROSION AROUND ATTACHMENT HOLES AND EDGES. MAINT CLEANED CORROSION, FILLED COUNTER SINK AREA, PREPPED AND PRIMED PANEL 151PE IAW DRAWING 319-53-0001-11 AND AMM 25-00-00-870-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5321

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 20,422 hrs · 8,755 cycles

DURING C-CHECK INSP NOTED FLOOR PANEL 231XG HAS TWO SMALL PUNCTURE HOLES ON SURFACE. MAINT REPAIRED PUNCTURE DAMAGE TO FLOOR PANEL 231XG IAW SRM 53-02-00 STEP 8A. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5321

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 20,422 hrs · 8,755 cycles

REFERENCE NON ROUTINE C045066. DURING C4 S1 C CHECK INSPECTION NOTED FLOOR PANEL 221BF HAS DELAMINATION AROUND SCREW HOLES. MAINTENANCE REMOVED DELAMINATED AREA AND APPLIED MOISTURE BARRIER FOIL IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 PAGE 245 FIGURE 212. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5321

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 20,422 hrs · 8,755 cycles

DURING C-CHECK INSP NOTED FLOOR PANEL 251JG HAS DAMAGE IN TWO PLACES ON UPPER SURFACE. MAINT REMOVED DAMAGE AND APPLIED MOISTURE BARRIER IAW SRM 53-02-00 AND SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5340

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,422 hrs · 8,755 cycles

DURING C-CHECK INSP, NOTED L2 DOOR AFT TOP SLIDE ATTACH POINT BRACKET CORRODED. MAINT REMOVED CORRODED FITTING AND INSTALLED SERVICEABLE FITTING IAW SRM 51-42-11 PARAGRAPH 5, AMM 20-21-11-911-01 AND AMM 20-21-11-991-003 SHEET 203. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,422 hrs · 8,755 cycles

DURING C-CHECK INSP NOTED CORROSION ON BEAM Y1292 LT UPPER OB SIDE NUTCLIP HOLE AT FRAME 68. MAINT REMOVED CORRODED FLOORBEAM Y1292 AND INSTALLED NEW FLOORBEAM FROM FRAME 68 TO FRAME 69 IAW SRM 51-42-00 AND DRAWINGS D53472780, D53472816 AND E53473250. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5320

Part: PANEL — DENTED (CARGO BAY) · airframe 20,422 hrs · 8,755 cycles

DURING C-CHECK INSP, NOTED AFT PIT TRANSITION PANEL 161BF HAS A DENTS. MAINT REMOVED DAMAGE AND CLEANED PANEL, FILLED DENTS ON PANEL 161BF IAW SRM 51-73-00 STEP 3C. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5320

Part: PANEL — DELAMINATED (CARGO BAY) · corrosion level 2 · airframe 20,422 hrs · 8,755 cycles

DURING C4 S1 C-CHECK INSP NOTED FWD PIT TRANSITION PANEL 32DG HAD A CORNER DELAMINATED. MAINT CLEANED DAMAGED AREA AND REPAIRED DAMAGE IAW SRM 53-02-00 PAGE 209. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5320

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,422 hrs · 8,755 cycles

REFERENCE NON ROUTINE C044730. DURING C4 S1 C-CHECK INSPECTION NOTED CORROSION ON UPPER SURFACE OF Y1292 RT BEAM 7 INCHES FORWARD OF FRAME 68. MAINTENANCE REMOVED OLD BEAM Y1292 AND INSTALLED NEW BEAM IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5320

Part: PANEL — DENTED (CARGO BAY) · airframe 20,422 hrs · 8,755 cycles

DURING C-CHECK INSP NOTED AFT PIT TRANSITION PANEL 151HE HAS DENTS. MAINT REMOVED DAMAGE AND CLEANED PANEL FILLED DENTS ON PANEL 151HE IAW SRM 53-73-00 STEP 3C. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5320

Part: PANEL — DAMAGED (FUSELAGE) · airframe 20,422 hrs · 8,755 cycles

DURING C-CHECK INSP, NOTED FWD PIT TRANSITION PANEL 131BF HAS GOUGE IN CORE. MAINT REMOVED DAMAGE AND CLEANED PANEL REPAIRED PUNCTURED DAMAGE PANEL 131BF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,422 hrs · 8,755 cycles

DURING C-CHECK INSP, NOTED FLOORBEAM 1292 RT AT FRAME 68 CORROSION IN OB NUTCLIP HOLE. MAINT INSTALLED NEW FLOORBEAM Y1292 FROM FRAME 68 TO FRAME 69 IAW THE REQUIREMENTS OF SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5320

Part: PANEL — DAMAGED (FUSELAGE) · airframe 20,422 hrs · 8,755 cycles

DURING C-CHECK INSP NOTED AFT PIT TRANSITION PANEL 162CF HAS DENTS AND GOUGES. REMOVED DAMAGE AND CLEANED PANEL FILLED DENTS AND REPAIRED PUNCTURE DAMAGE IAW SRM 51-73-00 STEP 3C AND SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,422 hrs · 8,755 cycles

DURING C-CHECK INSP, NOTED FLOORBEAM Y765 RT HAS PITTING CORROSION AT FRAME 68 ON TOP SURFACE. MAINT REMOVED BEAM AND INSTALLED NEW BEAM IAW DRAWING D53472815 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5320

Part: PANEL — DENTED (FUSELAGE) · airframe 20,422 hrs · 8,755 cycles

DURING C-CHECK INSP, NOTED AFT PIT TRANSITION PANEL 151FE HAS DENTS. MAINT REMOVED DAMAGE AND CLEANED PANEL, FILLED DENTS, PANEL 151FE IAW SRM 51-73-00 STEP 3C. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5320

Part: PANEL — DAMAGED (FUSELAGE) · airframe 20,422 hrs · 7,855 cycles

DURING C4 S1 C-CHECK INSPECTION NOTED AFT PIT TRANSITION PANEL 162BF HAS DENTS. MAINT REMOVED DAMAGE AND CLEANED PANEL FILLED DENTS ON PANEL 162BF IAW SRM 53-02-00. STEP 3C. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5320

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,422 hrs · 8,755 cycles

DURING C-CHECK INSP, NOTED THE SUPPORT FRAME FOR SHEAR PLATE CORRODED ON BOTTOM SURFACE AT NUTCLIP HOLES LOCATED AT THE LT OB SIDE AT FRAME 70. MAINT REMOVED CORRODED SUPPORT FRAME AND INSTALLED NEW SUPPORT FRAME IAW SRM 51-42-11 AND SRM 51-44-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · airframe 20,422 hrs · 8,755 cycles

DURING C4 S1 C-CHECK INSPECTION NOTED SUPPORT FRAME FOR SHEAR PLATE CORRODED ON BOTTOM SURFACE AT NUT CLIP HOLE. MAINTENANCE REMOVED OLD SUPPORT FRAME AND INSTALLED A NEW SUPPORT FRAME IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11 PARAGRAPH 6 AND 7. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.