N916FR

ATA 3350

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 214,978 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION NOTED LIGHT OUT IN AFT LEFT OVERWING EXIT. MAINTENANCE REMOVED AND REPLACED LAMP IN AFT LEFT EMERGENCY OVERWING LIGHT 63WL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-51-15-000-001 AND AMM 33-51-15-400-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5340

Part: BRACKET — CORRODED (L2 DOOR SLIDE) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION NOTED L2 DOOR SLIDE UPPER AFT MOUNT BRACKET HAD CORROSION. MAINTENANCE REMOVED AND REPLACED L2 DOOR SLIDE UPPER AFT MOUNT BRACKET IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5240

Part: BRACKET — CORRODED (R2 DOOR) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION NOTED R2 DOOR SLIDE UPPER AFT MOUNT BRACKET HAD CORROSION. MAINTENANCE REMOVED AND REPLACED R2 DOOR SLIDE UPPER AFT MOUNT BRACKET IN ACCORDANCE WITH SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 2520

Part: SEAT — CORRODED · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION NOTED CORROSION AT MOUNTING HOLES AFT LEFT FLIGHT ATTENDANT SEAT. MAINTENANCE REMOVED AND REPLACED AFT LEFT FLIGHT ATTENDANT SEAT IN ACCORDANCE WITH THE REQUIRMENTS OF AMM 25-22-41-400-011. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5321

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION NOTED FORWARD GALLEY FLOORBOARD 222EF HAS TWO PUNCTURES IN TOP RIGHT EDGE OF FLOORBOARD. MAINTENANCE REPAIRED PUNCTURES IN GALLEY FLOORBOARD 222EF IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-12-00 PAGE 205 AND PAGE 206. MAINTENANCE SANDED RESIN SMOOTH IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-12-00 PAGE 205 AND PAGE 206. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5321

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION NOTED FLOOR PANEL 232MF HAS HOLE IN FACE 1/4 INCH DIAMETER, 3 INCHES FROM INBOARD EDGE AND 3 FEET FROM FORWARD EDGE. MAINTENANCE REPAIRED DAMAGE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 PAGE 205 FIGURE 201. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5340

Part: FITTING — CORRODED (FUSLEAGE) · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION NOTED GIRT BAR FITTING WAS REMOVED ON R1 DOOR DUE TO CORROSION UNDER SPACERS. MAINTENANCE FABRICATED NEW NUT CLIP PLATES IN ACCORDANCE WITH THE REQUIREMENTS OF AIRBUS DRAWING D53112534. MAINTENANCE INSTALLED NEW DRAIN PANS AND NEW NUT PLATES AND GIRTH BAR FITTINGS IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5320

Part: SUPPORT FITTING — CORRODED · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION, NOTED CENTER FLOORBEAM SUPPORT FITTING BETWEEN C59 AND C60 CORRODED. MAINTENANCE REMOVED CORROSION ON SUPPORT FITTING AND REINSTALLED SUPPORT FITTING AND CENTER FLOORBEAM IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11 AND EA A9-53R-30227. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION REPORTED CORROSION WAS FOUND ON NUT CLIP HOLE FLOORBEAM Y1292 AT FRAME 67 AND WAS FOUND UNSERVICEABLE. MAINTENANCE REMOVED AND REPLACED FLOORBEAM Y1292 AT FRAME 67 IN ACCORDANCE WITH SRM 51-42-11 PARAGRAPHS 5 AND 7 AND AIRBUS DRAWINGS D53472815 AND E53474250. UPON COMPLETION OF THE INSTALLATION THE FLOORBEAM WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5320

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON DUMMY RAIL Y503.2 AT FRAME 16. MAINTENANCE REMOVED AND REPLACED THE DUMMY RAIL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11. UPON COMPLETION OF THE INSTALLATION, THE NEW DUMMY RAIL WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5320

Part: FLOOR SUPPORT — CORRODED (BULKHEAD) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE AFT BULKHEAD FLOOR SUPPORT PLATE, IN THE FORWARD CARGO PIT, AT FRAME 31, BETWEEN STRINGERS 38 LEFT AND 38 RIGHT. MAINTENANCE REMOVED AND REPLACED THE PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11, PARAGRAPH 6. UPON COMPLETION OF THE INSTALLATION, THE NEW PLATE WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON FLOOR SUPPORT-Y1292, BETWEEN FRAMES 16 AND 20. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOORBEAM IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11 AND A319 SRM 51-72-11. UPON COMPLETION OF THE INSTALLATION, THE NEW SUPPORTWAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND AROUND THE NUT PLATE HOLES OF THE FLOOR SUPPORT PLATE ON THE LEFT SIDE OF THE FORWARD CARGO COMPARTMENT BETWEEN FRAMES 28 TO 30. MAINTENANCE REMOVED AND REPLACED THE FLOOR PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11. UPON COMPLETION OF THE REPLACEMENT OF THE PLATE, IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION AT NUT PLATES FWD CARGO PIT RIGHT SIDE FLOOR SUPPORT PLATE FRAME 28 TO FRAME 31. MAINTENANCE REMOVED AND REPLACED SUPPORT PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11. UPON COMPLETION OF THE INSTALLATION THE SUPPORT PLATE WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5321

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION REPORTED FLOOR PANEL 261CG HAD DELAMINATION FROM ONE SCREW HOLE. MAINTENANCE REPAIRED FLOOR PANEL 261CG IN ACCORDANCE WITH SRM 53-08-00 STEP 8J, SRM 51-77-11 PARAGRAPH A11 AND SRM 51-44-21 PARAGRAPH 3A. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5340

Part: MOUNT — CORRODED (WINDSCREEN) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION NOTED RIGHT WIND SCREEN LOWER ATTACH MOUNTS WERE CORRODED. MAINTENANCE REMOVED AND REPLACED RIGHT WINDSCREEN LOWER ATTACH MOUNTS IN ACCORDANCE WITH THE REQUIRMENTS OF WORK CARD CP725-18. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5340

Part: FITTING — CORRODED (GIRT BAR) · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION NOTED R2 FORWARD GIRT BAR FITTING PLATE CORODDED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED FITTING PLATE. OKAY TO INSTALL AND INSTALL WILL BE ACCOMPLISHED ON WORK CARD CP753-36.

ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION NOTED CORROSION AT NUT PLATES AFT PIT LEFT FLOORBEAM UNDER COVER PROFILE AT FRAME 56 LOCATED FROM STRINGER 38 LEFT TO 38 RIGHT. MAINTENANCE FABRICATED REPLACEMENT PART IN ACCORDANCE WITH THE REQUIREMENTS OF AIRBUS DRAWING D53476476200 AND MATERIAL SPECIFICATION DAN26H35. INSTALLED NEW SUPPORT ANGLE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11 PARAGRAPH 6. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5340

Part: FITTING — CORRODED (GIRT BAR) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION NOTED R1 FORWARD GIRT BAR FITTING PLATE WAS CORRODED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED FITTING PLATE. OKAY TO INSTALL AND INSTALL WILL BE ACCOMPLISHED ON WORK CARD CP7553-12.

ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION NOTED CORROSION AT NUT PLATES AFT PIT LEFT HAND FLOORBEAM UNDER COVER PROFILE AT FRAME 58 LOCATED FROM STRINGER 38 LEFT TO 38 RIGHT. MAINTENANCE FABRICATED AND REPLACED FLOORBEAM SUPPORT FITTING IN ACCORDANCE WITH THE REQUIREMENTS OF AIRBUS DRAWING D53470394 SHEET 3 REVISION H AND SRM 51-44-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5320

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION NOTED FRAME 59 COVER PROFILE NUT PLATE HOLES WERE CORRODED FROM STRINGER 38 RIGHT TO 38 LEFT. MAINTENANCE BLENDED OUT CORROSION AND INSTALLED NEW SUPPORT AT FRAME 59 STRINGER 41 LEFT IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. INSTALLED REPAIR DOUBLER AND FILLER IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30247. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5320

Part: PLATE — CRACKED (FUSELAGE) · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK, INSPECTION REPORTED A CRACK WAS FOUND IN THE MOULLION PLATE LOCATED AFT OF THE L2 DOOR FRAME AT THE JOINT SHEET ATTACH POINT. MAINTENANCE REMOVED AND REPLACED THE MOULLION PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11, PARAGRAPH 6. UPON COMPLETION OF THE INSTALLATION OF THE NEW MOULLION PLATE, IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5321

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION NOTED FLOOR PANEL 222EF DELAMINATED AT EDGE. MAINTENANCE REPAIRED FLOOR PANEL 222EF IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30217 AND SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5320

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION NOTED CORROSION AROUND NUT PLATES AFT CARGO PIT LEFT FLOOR PROFILE AT C 58. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11 PARAGRAPH 5 AND 6 AND AIRBUS DRAWING D53476318. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION NOTED CORROSION AROUND NUT PLATES AFT CARGO PIT FLOOR PROFILE BETWEEN C55 AND C56. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-35-00 AND SRM 51-42-11 PAGE 7. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION REPORTED FLOORBEAM Y1292 SHOWS SIGNS OF CORROSION AT FRAME 16. MAINTENANCE REPLACED ONE SECTION OF THE BEAM IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11 AND BLENDED OTHER AREA LOCATED AT 62.875" AFT OF FWD END OF BEAM IN ACCORDANCE WITH SRM 51-74-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION NOTED AFT CARGO PIT CENTER FLOORBEAM BETWEEN C58 AND C59 NUT PLATES HAVE SIGNS OF CORROSION. MAINTENANCE REMOVED OLD FLOORBEAM AND REPAIR ANGLES, FABRICATED NEW FLOORBEAM AND REPAIR ANGLES IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30229 AND INSTALLED NEW PARTS IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5347

Part: DUMMY RAIL — CORRODED · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C-CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON DUMMY RAIL Y503.2 AT FRAME 16. MAINTENANCE REMOVED AND REPLACED DUMMY RAIL IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. UPON COMPLETION OF THE INSTALLATION THE NEW RAIL WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5321

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION NOTED FLOOR PANEL 221PF LAV A HAS CORROSION ON BOLT HOLES. MAINTENANCE RECEIVED NEW FLOOR PANEL 221PK, OKAY TO INSTALL AND INSTALL WILL BE ACCOMPLISHED ON ROUTINE CARD CP753-12.

ATA 5320

Part: STRIP — CORRODED · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION NOTED BOTH LEFT 1 AND RIGHT 1 GAP STRIPS CORRODED ON LOWER SURFACE. MAINTENANCE REMOVED AND REPLACED LEFT 1 AND RIGHT 1 GAP STRIPS IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-12-12 PAGE BREAK 401. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION REPORTED NUT PLATE CORRODED OUTBOARD OF CENTER FLOORBEAM AFT CARGO PIT C 56 1. MAINTENANCE REMOVED AND REPLACED NEW C 56 PROFILE PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11 PARAGRAPH 6 AND AIRBUS DRAWING 17D53974965. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5321

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE UNDERSIDE OF FLOOR PANEL 221FF. MAINTENANCE REMOVED CORRODED PANEL. THE NEW PANEL WAS INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF TASK CARD CP 753-12. FOLLOWING INSTALLATION OF THE NEW PANEL, IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5321

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE UNDERSIDE OF FLOOR PANEL 222FF. MAINTENANCE REMOVED THE CORRODED PANEL. THE NEW PANEL WAS INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF TASK CARD CP 753-12. UPON COMPLETION OF THE INSTALLATION OF THE NEW PANEL, IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5321

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION NOTED FLOOR PANEL 261HG HAS DELAMINATION AROUND EDGES. MAINTENANCE REPAIRED FLOOR PANEL 261HG IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30226. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5320

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION NOTED R2 DOOR SILL HAS CORROSION AROUND NUT CLIP HOLE AT FRAME 66. MAINTENANCE FABRICATED REPAIR ANGLE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-41-14, FABRICATED LEFT AND RIGHT REPAIR ANGLES IN ACCORDANCE WITH THE REQUIREMENTS OF EA A0-53F-12234. REMOVED CORROSION IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-41-14 FIGURE 201, MATERIAL FOR ANGLE REPAIR 7075T7351. INSTALLED REPAIR SPLICE IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30218 AND SRM 53-41-14 FIGURE 201. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5320

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C-CHECK, INSPECTION REPORTED CORROSION WAS FOUND AT FRAME SUPPORT OF FLOORBEAM Y1732 AFT OF FRAME 69. MAINTENANCE REMOVED AND REPLACED FRAME SUPPORT IN ACCORDANCE WITH SRM 51-42-11 AND SRM 51-72-11 AND SRM 51-44-11. UPON COMPLETION OF THE INSTALLATION THE FRAME SUPPORT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5321

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THREE INSERTS ON FLOOR PANEL 261PF. MAINTENANCE REMOVED THE CORRODED PANEL. THE NEW PANEL WAS INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF TASK CARD CP 753-36. FOLLOWING THE INSTALLATION OF THE NEW PANEL, IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND AROUND THE NUT CLIP HOLES ON FLOOR BEAM Y1292 BETWEEN FRAMES 68 AND 69. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11, PARAGRAPH 6. UPON COMPLETION OF THE INSTALLATION OF THE NEW BEAM, IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE FORWARD LAVATORY FLOOR ANGLE BRACKET, ON ITS UNDERSIDE. MAINTENANCE REMOVED AND REPLACED THE ANGLE BRACKET IN ACCORDANCE WITH THE REQUIREMENTS OF A0-25EO-20299. UPON COMPETION OF THE REPLACEMENT, THE BRACKET WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5320

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C-CHECK INSPECTION REPORTED CORROSION WAS FOUND ON SHEAR PLATE AT FLOORBEAM Y1732 AFT OF FRAME 69. MAINTENANCE REMOVED AND REPLACE SHEAR PLATE IN ACCORDANCE WITH SRM 51-42-11 PARAGRAPH 6, 7, 13 AND EA A9-53R-30196. UPON COMPLETION OF THE INSTALLATION OF THE SHEAR PLATE IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5320

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C-CHECK, INSPECTION REPORTED CORROSION WAS FOUND AT FRAME SUPPORT OF FLOORBEAM Y1732 AFT OF FRAME 69. MAINTENANCE REMOVED AND REPLACED FRAME SUPPORT IN ACCORDANCE WITH SRM 51-42-11 PARAGRAPH 6, 7 AND 14 AND EA A9-53R-30196. UPON COMPLETION OF THE INSTALLATION THE FRAME SUPPORT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5320

Part: SHEAR PLATE — CORRODED · corrosion level 2 · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 CHECK INSPECTION REPORTED CORROSION WAS FOUND ON SHEAR PLATE AT FLOORBEAM Y1732 AFT OF FRAME 69. MAINTENANCE REMOVED AND REPLACED SHEAR PLATE IN ACCORDANCE WITH SRM 51-42-1 PARAGRAPH 6, 7 AND EA A9-53R-30196. UPON COMPLETION OF THE INSTALLATION OF THE SHEAR PLATE IT WAS INSPECTED AND FOUND ACCEPTABLE.

ATA 5280

Part: SUPPORT BRACKET — CORRODED (NLG DOOR) · airframe 21,497 hrs · 8,472 cycles

DURING C4 S1 C CHECK INSPECTION NOTED THE NOSE LANDING GEAR DECORATIVE DOOR LOWER ATTACH POINTS ON STRUT WERE CORRODED AND WORN. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR SUPPORT BRACKET IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 32-22-15-400-001 AND EA A0-32T-11699. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.