N926FR

Part: FLOORBEAM — CORRODED (FRAME 66) · airframe 47,185 hrs · 23,374 cycles

DURING C-CHECK, N1718N154 INSPECTION FLOORBEAM BETWEEN Y1292 AND Y765 CORRODED AT FRAME 66. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, AND SRM 51-72-11-911-001.

Part: SPLICE PLATE — CORRODED (FRAME 26) · corrosion level 2 · airframe 47,185 hrs · 23,374 cycles

THE FORWARD CARGO SKIN SPLICE PLATE CORRODED AT FRAME 26, STRINGER 40 - 41R. REMOVED AND REPLACED THE PLATE IAW SRM 53-21-42-11, AND 53-21-11.

Part: DOOR SILL — CORRODED (FRAMES 24-28) · corrosion level 2 · airframe 47,185 hrs · 23,374 cycles

FORWARD CARGO DOOR SILL WEB HAS MULTIPLE VISUAL INDICATIONS OF CORROSION FROM FRAMES 24 TO 28. REMOVED AND REPLACED THE WEB IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,185 hrs · 23,374 cycles

FLOORBEAM -Y1292, BETWEEN FR66 AND FR70 CORRODED. REMOVED AND REPLACED FLOORBEAM -Y1292, BETWEEN FR66-FR68 AND FR68-FR70, IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · airframe 47,185 hrs · 23,374 cycles

DURING C-CHECK, FOUND THE FLOOR SUPPORT Y765 BETWEEN FRAMES 66 - 70 CORRODED AT FASTNER HOLE. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,185 hrs · 23,374 cycles

RT SHEAR WEB BETWEEN FR 69 THRU FR 70 CORRODED. EVALUATED RT SHEAR WEB FOUND TO BE OUT OF LIMITS IAW SRM 51-73-11, REMOVED AND REPLACED RT SHEAR WEB IAW SRM 51.4211.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-70) · corrosion level 2 · airframe 47,185 hrs · 23,374 cycles

FLOOR SUPPORT Y160 BETWEEN FRAMES 68 - 70, CORRODED AT FASTNER HOLE. REMOVED AND REPLACE THE FLOOR SUPPORT IAW SRM 53-41-14, 51-42-11, AND 51-44-00.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · corrosion level 2 · airframe 47,185 hrs · 23,374 cycles

FLOOR SUPPORT Y765 BETWEEN FRAMES 66 THRU 70 CORRODED AT FASTENER HOLES. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 319 51-72-11.

Part: DOOR SILL — CORRODED (R2 DOORWAY) · corrosion level 2 · airframe 47,185 hrs · 23,374 cycles

R2 DOOR SILL CORRODED AT SEVERAL FASTNER HOLES. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-72-11-911-001.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-70) · corrosion level 2 · airframe 47,185 hrs · 23,374 cycles

FLOOR SUPPORT Y1292 BETWEEN FRAMES 68 AND 70 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · airframe 47,185 hrs · 23,374 cycles

DURING C-CHECK, NR 1718N150 INSPECTION NOTED FLOOR SUPPORT, Y-768 BETWEEN FRAMES 66 AND 68 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, AND SRM 51-72-11-911-001.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,185 hrs · 23,374 cycles

FLOORBEAM -Y1292, BETWEEN FR66 AND FR70 CORRODED. REMOVED AND REPLACED FLOORBEAM -Y1292, BETWEEN FR66-FR68 AND FR68-FR70, IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FRAME 66) · corrosion level 2 · airframe 47,185 hrs · 23,374 cycles

FLOORBEAM BETWEEN Y254 AND Y765 CORRODED AT FASTENER HOLE FRAME 66. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, SRM 53-41-14-283-004, 51-44-00, AND 51-21-00.

Part: DOOR SILL — CORRODED (L2 DOORWAY) · corrosion level 2 · airframe 47,185 hrs · 23,374 cycles

L2 DOOR SILL CORRODED AT SEVERAL FASTNER HOLES. REMOVED AND REPLACED THE DOOR SILL, IAW IAW SRM 51-72-11-911-001.

Part: SLIDE RAFT — OUT OF TOLERANCE (L1 DOOR) · airframe 41,329 hrs · 20,608 cycles

LOG PAGE 953280 ITEM 2, EPSU INTERNAL LOAD, FWD LEFT FAULT ATA 33-51-38. R & R L1 DOOR SLIDE RAFT IAW EO A9-25EO-33139 REC C STEPS 3 -12, TEST STILL FAILED. LOG PAGE 953283 ITEM 2, EPSU INTERNAL LOAD FWD LEFT FAULT. R & R R1 DOOR SLIDE IAW EO A9-25EO-33139 REV C STEPS 13 - 22. PERFORMED EPSU OPERATIONS TEST IAW AMM 33-51-00-710-001, TESTED OKAY.

Part: PIPE — BROKEN (HYDRAULIC SYS) · airframe 36,762 hrs · 18,398 cycles

REFERENCE LOG PAGE 868242 ITEM 1. HYD GREEN RESERVOIR LOW LEVEL. FOUND GREEN HCU PIPE BROKEN. REMOVED HCU PIPE AMM 29-11-49-000-049. INSTALLED HCU PIPE AMM 29-11-49-400-049.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,126 hrs · 18,051 cycles

EPSU EMER LIGHT BATTERY FIN 12WL FAILED CAPACITY TEST RT SIDE. R & R BATTERY ASSEMBLY IAW AMM 33-51-39-000-005A & 33-51-39-400-005A.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 31,515 hrs · 15,537 cycles

EMERGENCY LIGHT ROW 2 AND 3 INOPERATIVE. REPLACED LIGHT ASSY OPS CHECKED NORMAL. IAW AMM 33-51-19 PB 401.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 30,987 hrs · 15,258 cycles

AFT GALLEY FLOOR SUPPORT AT FR67 TO FR68, Y1292 HAS OUT OF LIMITS CORROSION. REMOVED OLD BEAM, LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-11, PAR 5.A-C

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 30,987 hrs · 15,258 cycles

AFT GALLEY FLOOR SUPPORT AT FR68 TO FR69. Y1292 HAS OUT OF LIMITS CORROSION. REMOVED OLD BEAM. LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-11, PAR 5. A-C

Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 30,987 hrs · 15,258 cycles

RIGHT SHEAR PLATE FR 69 TO FR 70, Y1292 HAS OUT OF LIMITS CORROSION. REMOVED OLD SHEAR PLATE. LOCATED, DRILLED AND INSTALLED NEW PLATE IAW SRM 51 -42-11, PAR 6.B, 1-8.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 30,987 hrs · 15,258 cycles

AFT GALLEY FLOOR BEAM AT FR67 - FR68, -Y1292 HAS OUT OF LIMITS CORROSION. REMOVED OLD BEAM. LOCATED, DRILLED AND INSTALLED NEW BEAM IAW A319 SRM 51-42-11, PAR5(A-C).

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 30,987 hrs · 15,258 cycles

AFT GALLEY FLOOR BEAM AT FR68 - FR69, -Y1292 HAS OUT OF LIMITS CORROSION. REMOVED OLD BEAM. LOCATED, DRILLED AND INSTALLED NEW BEAM IAW A319 SRM 51-42- 11, PAR5(A-C).

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,741 hrs · 14,068 cycles

SEAT ROW 9 ABC SEATS EMERGENCY LIGHT INOPERATIVE. R & R BULBS IAW AMM 33-51-18-400-002A, OPS CHECKED OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,799 hrs · 13,327 cycles

EMERGENCY EXIT LIGHTS LIGHTS AT R2 AND L2 INOPERATIVE. R & R CONNECTOR 2244VC, REF ESPM 20-44-29. R & R EPSU 13WL, OPS CHECKED GOOD IAW AMM 33-51-38-000-001.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS)

AFT EMERGENCY LIGHTS INOPERATIVE. EPSU WOULD NOT RESET. R & R 13WL EMERGENCY POWER SUPPLY UNIT & BATTERY IAW AMM 33-51-38, PB401. OPS CHECKED GOOD.

Part: LINE — RUPTURED (HYD SYSTEM) · airframe 27,036 hrs · 13,225 cycles

AIRCRAFT LOST PARTIAL GREEN SYS HYD FLUID IN FLIGHT. UPON ARRIVAL, ON-CALL MX IDENTIFIED A HYD LINE IN THE PYLON RUPTURED. TUBE WAS CHANGED. LEAK CHECK GOOD.

Part: BATTERY — DEFECTIVE (EMERGENCY LIGHT) · airframe 26,766 hrs · 13,082 cycles

DURING HEAVY CHECK, PERFORMED EMERGENCY LIGHT OPS CHECK ON PTP PANEL. TEST FAILED WITH MESSAGE "EPSU BATTERY EMER L". LOCATED OVERWING EPSU ON LT SIDE AND PERFORMED TEST ON INDIVIDUAL UNIT. TEST FAILED WITH "BATT FAULT" LIGHT ILLUMINATED. R & R EPSU BATTERY PACK. PERFORMED OPS CHECK. EMERGENCY LIGHTS TEST "OK". ALL INDICATIONS NORMAL.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 24,798 hrs · 12,126 cycles

LT OVERWING EXIT SIGN LENS CRACKED. R & R LT OVER WING EXIT SIGN LENS.

Part: CYLINDER — SHEARED (DOOR DAMPER) · airframe 21,484 hrs · 10,585 cycles

REF LOG PAGE NR 503901. DURING A CHECK MX NOTED CYL - DOOR DAMPER PERCUSSION LEVER PIN SHEARED. MX R & R THE CYLINDER - DOOR DAMPER, OPS CHECK NORMAL, IAW AMM 52-11-14 PB 401.

Part: ENTERTAIN SYS — SMOKE (LIVE TV) · airframe 21,460 hrs · 10,575 cycles

PILOT WRITE UP FOR LIVE TV SMOKE WARNING AT GATE. MX ACCOMPLISHED VISUAL INSP IAW LIVE TV AMM 44-25-00. NO DAMAGE OR DEFECTS NOTED AT THIS TIME. PERFORMED OPS TEST OF THE SMOKE DETECTOR CONTROL PANEL IAW LIVE TV AMM 44-25-00 PAGES 5040 AND 5041. SYS OPS TEST GOOD. LIVE TV SYS DEACTIVATED IAW MEL 44-20-01AA CNTRL NR 1074053. MEL PLACARDS INSTALLED AND TRANSFERED TO LOG BOOK SUP SHEET. ADDITIONAL INFORMATION TO BE SUBMITED UPON CLEARANCE OF MEL 44-20-01AA CONTROL NR 1074053.

Part: CLAMP — LOOSE (FAN DUCT) · airframe 21,460 hrs · 10,575 cycles

PILOT WRITE UP FOR LIVE TV SMOKE WARNING AT GATE. MX ACCOMPLISHED VISUAL INSP IAW LIVE TV AMM 44-25-00. NO DAMAGE OR DEFECTS NOTED AT THIS TIME. PERFORMED OPS TEST OF THE SMOKE DETECTOR CONTROL PANEL IAW LIVE TV AMM 44-25-00 PAGES 5040 AND 5041. SYS OPS TEST GOOD. LIVE TV SYS DEACTIVATED IAW MEL 44-20-01AA CNTL NR 1074053. MEL PLACARDS INSTALLED AND TRANSFERED TO LOG BOOK SUP SHEET. ADDITIONAL INFO TO BE SUBMITED UPON CLEARANCE OF MEL 44-20-01AA CONTROL NR 1074053. REF PAGE NR 512394, 03/15/2010. MX NOTED AFT RACK FAN DUCT CLAMPS LOOSE. MX SECURED CLAMPS AND ACCOMPLISHED NR ONE ENG RUN UP AND POWER SWITCH OVER. NO SMOKE DETECTOR FAULTS ON ENGINE SHUTDOWN. LIVE TV SYS OPS CHECK GOOD. IAW LIVE TV AMM 44-25-00. MEL 44-20-01AA CONTROL NR 1074053 REMAINS. REF PAGE NR 503907, 03/17/2010. MX R & R LIVE TV SMOKE DETECTOR AS PRECAUTIONARY. LIVE TV SYS OPS CHECK GOOD. IAW LIVE TV AMM 44-25-00. MEL 44-20-01AA CONTROL NR 1074053 REMOVED.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 20,342 hrs · 10,048 cycles

REFERENCE NON ROUTINE C074947. DURING DEN C4 C-CHECK, INSPECTION NOTED CORROSION ON THE NUT PLATE HOLES LOCATED ON THE FWD SIDE OF FRAME 58. MX REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-74-00, SRM 51-42-11 AND SRM 51-44-11.

Part: PROFILE — CORRODED (ZONE 100) · airframe 20,342 hrs · 10,048 cycles

DURING DEN C4 C-CHECK, INSP NOTED CORROSION ON THE PROFILE ON THE LT BRACE BETWEEN FRAME 56 AND FRAME 58. MX REMOVED AND REPLACED THE PROFILE IAW SRM51-42-11, SRM 51-44-11, SRM 51-74-00.

Part: PROFILE — CORRODED (ZONE 100) · airframe 20,342 hrs · 10,048 cycles

DURING DEN C4 C-CHECK, INSPECTION NOTED CORROSION ON THE AFT CARGO PIT PROFILE LOCATED AT FRAME 58. MX REMOVED AND REPLACED THE PROFILE IAW SRM 51-74-00, SRM 51-42-11 AND SRM 51-44-11.

Part: PROFILE — CORRODED (ZONE 100) · airframe 20,342 hrs · 10,048 cycles

DURING DEN C4 C-CHECK, INSPECTION NOTED CORROSION ON THE PROFILE LOCATED IN THE AFT CARGO PIT AT FRAME 56. MX REMOVED AND REPLACED THE PROFILE IAW SRM 51-42-11 AND 51-42-12.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 17,710 hrs · 8,690 cycles

DURING THE HEAVY SERVICE CHECK, IT WAS NOTED THAT THE EMERGENCY EXIT LIGHT FOR ROW 10ABC WAS INOPERATIVE. MAINTENANCE RESECURED WIRE 3351-9005 AT TERMINAL STRIP 7225VT AND PERFORMED OPERATIONAL CHECK. REFERENCE ENGINEERING ORDER A9-25EO-30667 AND AMM 33-51-00 PB 501.

Part: CONTROL UNIT — MALFUNCTIONED (MLG) · airframe 15,279 hrs · 7,434 cycles

AFTER TAKEOFF THE FLIGHT CREW NOTICED THE NLG FAILED TO RETRACT. THE FLIGHT CREW FOLLOWED THE ECAM AND CYCLED GEAR AND NOSE GEAR RETRACTED NORMALLY AND THE AC RETURNED TO DEPARTURE. MAINT PERFORMED GEAR SWING SUCCESSFULLY 8 TIMES AND REMOVED AND REPLACED NR 2 LGCIU IAW TSM 32-31-00-810-812 AND ARM 32-31-31-71 PAGE BREAK 401. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED, BITE CHECK WAS NORMAL AND OPERATIONAL CHECKED GOOD. (A)

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP NOTED RT CABIN FLOOR LATERAL SHEAR PLATE AT Y1162 BETWEEN FRAMES 69 AND FRAMES 70 HAS AREAS OF CORROSION. MAINT REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP NOTED RT CABIN FLOOR LATERAL SHEAR PLATE AT Y1162 BETWEEN FRAMES 69 AND FRAMES 70 HAS AREAS OF CORROSION. MAINT REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP NOTED AFT CARGO FLOOR PANEL 151AE HAS CORNER DAMAGE. MAINT REMOVED DAMAGED AREA AND REPAIRED AFT CARGO FLOOR PANEL 151AE IAW OF SRM 53-02-00. UPON COMPLETIONS OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP NOTED AFT CARGO FLOOR PANEL 152UG HAS A DENT AND A HOLE. MAINT REPAIRED AFT CARGO FLOOR PANEL 152UG IAW SRM 53-02-00 PARAGRAPH 8E. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP NOTED RT CABIN FLOOR LOGERON BEAM Y1732 AT FRAME 66 HAS CORROSION AROUND FASTENER HOLE. MAINT FABRICATED ANGLES AND FILLER AND ACCOMPLISHED DETAILED REPAIR IAW EA A0-53F-12234, EA A0-53R-30370 AND SRM 53-41-14. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: SPAR CAP — DAMAGED (HORIZONTAL STAB) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP NOTED LT HORIZONTAL STABILIZER OB REAR SPAR LOWER CAP HAS COMPOSITE DAMAGE LOCATED OB OF RIB 11 18 INCHES OF REAR SPAR TEE SEPARATED. MAINT REMOVED DAMAGED AREA ON LT HORIZONTAL STABILIZER OB REAR SPAR AND APPLIED REPAIR DAMAGE IAW SRM 51-77-11 AND EA A9-55R-30340. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP NOTED AFT CARGO FLOOR PANEL 152XG HAS FOUR HOLES IN IT. MAINT REPAIRED FLOOR PANEL 152XG IAW SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,261 hrs · 7,424 cycles

DURING C-CHECK INSP, NOTED RT HAND CABIN FLOOR PANEL 262FF HAS CORROSION. MAINT REMOVED AND REPLACED CABIN FLOOR PANEL 262FF IAW ROUTINE CARD 9625. UPON COMPLETION OR THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 15,261 hrs · 7,424 cycles

DURING C-CHECK INSP, NOTED LT CABIN FLOOR LONGERON BEAM Y1732 AT FRAME 66 HAS CORROSION AROUND FASTENER HOLE. MAINT FABRICATED REPAIR ANGLES AND FILLER AND ACCOMPLISHED REPAIR IAW EA A0-53F-12234, EA A0-53T-12235, SRM 53-41-14 FIGURE 201 AND SRM 53-51-14 FIGURE 201. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOORBOARD — DAMAGED (FUSELAGE) · airframe 15,261 hrs · 7,424 cycles

DURING C-CHECK INSP, NOTED AFT CARGO FLOORBOARD 151GE HAS A DAMAGED EDGE. MAINT REPAIRED FLOORBOARD 151GE IAW SRM 53-02-00 FIGURE 207. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,261 hrs · 7,424 cycles

DURING C-CHECK INSP, NOTED AFT CARGO FLOOR PANEL 151UG HAS SEVERAL HOLES AND DENTS. MAINT REPAIRED FLOOR PANEL 151UG IAW EA A0-53F-12307. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP, NOTED AFT CARGO FLOOR PANEL 151HE HAS A DENT AND A HOLE. MAINT REPAIRED PANEL 151HE IAW SRM 53-02-00 REPAIR 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP, NOTED AFT CABIN FLOOR PANEL 261HG DAMAGED BEYOND LIMITS. MAINT REMOVED AND REPLACED PANEL 261HG IAW SRM 53-22-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP, NOTED DENT IN UPPER SURFACE OF BULK CARGO FLOOR PANEL 162BF. MAINT REPAIRED PANEL 162BF IAW SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP, NOTED CARGO FLOOR PANEL 161CF HAS THREE HOLES IN IT. MAINT REPAIRED PANEL 161CF IAW SRM 53-02-00 REPAIR 204 AND REPAIR 207. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: SKIN — DENTED (FUSELAGE) · airframe 15,261 hrs · 7,425 cycles

DURING C3 S1 C-CHECK INSP NOTED RT FUSELAGE SKIN DENT BETWEEN FRAME 12 AND FRAME 13 ABOVE LWR EDGE OF STRINGER 29. MAINT PERFORMED PERMANENT REPAIR IAW EA A9-53R-11684 REVISION C AND SRM 53-11-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP, NOTED CARGO FLOORBOARD PANEL 161BF HAS TWO HOLES. MAINT REPAIRED PANEL 161BF IAW SRM 53-02-00 REPAIR PROCEDURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP, NOTED AFT CARGO FLOOR PANEL 151FE HAS A HOLE. MAINT REPAIRED PANEL 151FE IAW SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,261 hrs · 7,425 cycles

REFERENCE NON ROUTINE 34384. DURING C3 S1 C-CHECK INSP NOTED AFT CARGO FLOOR PANEL 152WG HAS A DENT AND A HOLE. MAINT REPAIRED FLOOR PANEL 152WG IAW SRM 53-02-00 REPAIR 204 AND REPAIR 207. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP, NOTED CRACKED DENT ON UPPER SURFACE OF BULK CARGO FLOOR PANEL 161BF. MAINT REPAIRED PANEL 161BF IAW SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 15,261 hrs · 7,425 cycles

REFERENCE NON ROUTINE 34659. DURING C3 S1 C CHECK INSPECTION NOTED SEVERAL LARGE DENTS ON IPPER SURFACE OF BULK CARGO FLOOR PANEL 161CF. MAINTENANCE REPAIRED PANEL 161CF IN ACCORDANCE WITH SRM 53-02-00 REPAIR 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCETABLE. (A)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP, NOTED CARGO FLOOR PANEL 162BF HAS TWO HOLES. MAINT REPAIRED AFT CARGO FLOOR PANEL 162BF IAW SRM 53-02-00 REPAIR 207. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP, NOTED CARGO FLOOR PANEL 151TG HAS A HOLE. MAINT REPAIRED PANEL 151TG IAW SRM 53-02-00 REPAIR 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: ARM — CHAFED (FLAP TRACK) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP NOTED RT NR TWO FLAP TRACK DRIVE LEVER EXTENSION ARM THAT ATTACHES TO FLAP AT AFT ATTACH POINT IS CHAFING INTO FITTING ON OB EAR BOTTOM END AND IB EAR TOP END. MAINT REPAIRED AREA IAW EA A9-57R-30378, SRM 51-73-00 AND SRM 51-21-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: MOUNT — CORRODED (GIRT BAR) · airframe 15,261 hrs · 7,424 cycles

DURING C-CHECK INSP, NOTED R1 DOOR FWD GIRT BAR MOUNT AFT TWO HOLES IN FUSELAGE WEB HAVE CORROSION AROUND THEM. MAINT REMOVED CORROSION AND MADE UP REPAIR SHIMS IAW EA A9-53R-30358. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP NOTED CABIN FLOOR PANEL 242FF HAS AREA OF ELIMINATION. MAINT REPAIRED FLOOR PANEL 2422FF IAW SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP, NOTED FLOOR PANEL 242LF HAS DAMAGED ON TOP SURFACE PEELED BACK 4" X 6" ON AFT CORNER. MAINT REPAIRED PANEL 242LF IAW SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP NOTED AFT CARGO FLOOR PANEL 152TG HAS A CRACK AND A HOLE. MAINT REPAIRED PANEL 152TG IAW SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP, NOTED CABIN FLOOR PANEL 252HF AREA OF ELIMINATION. MAINT REPAIRED PANEL 252HF IAW SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,621 hrs · 7,425 cycles

REFERENCE NON ROUTINE 34332. DURING C3 S1 C-CHECK INSPECTION NOTED CABIN FLOOR LATERAL SHEAR PLATE AT Y1162 BETWEEN FRAMES 69 AND FRAMES 70 HAS AREAS OF CORROSION ON TOP AND BOTTOM SIDES. MAINTENANCE REMOVED AND REPLACED LATERAL SHEAR PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,621 hrs · 7,425 cycles

DURING C-CHECK INSP NOTED CABIN FLOOR PANEL 251SF HAS LARGE PUNCTURE HOLE. MAINT REPAIRED PANEL 251SF IAW SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,621 hrs · 7,425 cycles

DURING C-CHECK INSP, NOTED RT CABIN FLOOR SUPPORT Y1162 BETWEEN FRAMES 66 AND FRAMES 68 HAS SEVERAL AREAS OF CORROSION AND SIX SHEARED RIVET HEADS. MAINT REMOVED AND REPLACED FLOOR SUPPORT Y1162 BETWEEN FRAMES 68 AND FRAME 69 IAW SRM 51-72-11 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 15,261 hrs · 7,425 cycles

REFERENCE NON ROUTIN 34301. DURING C3 S1 C-CHECK INSPECTION NOTED CABIN FLOOR PANEL 251FF HAS AREA OF DELAMINATION FROM FRAME 47 TO FRAME 64. MAINTENANCE REPAIRED PANEL IN ACCORDANCE WITH SRM 53-42-13-400-001. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP NOTED FLOOR PANEL 262EF HAS SEVERAL PUNCTURES. MAINT REMOVED AND REPLACED FLOOR PANEL IAW REQUIREMENTS OF WORK CARD CP753-36. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: PROFILE — CORRODED (FUSELAGE) · airframe 15,621 hrs · 7,425 cycles

REFERENCE NON ROUTINE 33985. DURING C3 S1 C-CHECK INSPECTION NOTED AFT CARGO COMPARTMENT LT SIDE PROFILE HAS CORROSION BETWEEN FRAMES C57 AND C58. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH SRM 51-72-11. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 15,621 hrs · 7,425 cycles

REFERENCE NON ROUTINE 34615. DURING C3 S1 C-CHECK INSPECTION NOTED FORWARD CARGO FLOOR PANEL 131AF HAS A HOLE. MAINTENANCE REPAIRED HOLE ON PANEL 131AF IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP NOTED CARGO PIT FLOOR PANEL 161DF HAS A DAMAGED AREA. MAINT REPAIRED PANEL 161DF IAW SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,261 hrs · 7,425 cycles

REFERENCE NON ROUTINE 34045. DURING C3 S1 C-CHECK INSPECTION NOTED FORWARD CARGO PIT PROFILE AT FRAME C28 HAS CORROSION IN NUT PLATE AND RIVETS. MAINTENANCE REMOVED CORROSION FROM NUT PLATE PROFILE AND FOUND PROFILE TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11, SRM 51-46-11 AND SRM 51-44-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,261 hrs · 7,425 cycles

REFERENCE NON ROUTINE 34649. DURING C3 S1 C-CHECK INSPECTION NOTED RT HAND CABIN SUPPORT BRACKET AT LETRAL SHEAR PLATE STATION Y1162 BETWEEN FRAMES 69 AND FRAMES 70 REQUIRE REPLACEMENT DUE TO CORROSION. MAINTENANCE REMOVED AND REPLACED SUPPORT BRACKET IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: PROFILE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 15,261 hrs · 7,425 cycles

DURING C-3/S-1 C-CHECK, INSPECTION NOTED AFT CARGO COMPARTMENT LEFT SIDE PROFILE AT FRAME C58 HAS CORROSION. MAINTENANCE REMOVED CORRODED PROFILE AND INSTALLED NEW IN ACCORDANCE WITH A319 SRM 51-42-11 PAGE 7 AND 8.

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP NOTED AFT CARGO PIT RT SIDE PROFILE HAS CORROSION SEVERAL PLACES BETWEEN FRAMES C59 TO FRAME C61. MAINT REMOVED AND REPLACED PROFILE IAW SRM 51-72-11, SRM 51-44-11 AND SRM 51-46-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOORBOARD — DAMAGED (FUSELAGE) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP NOTED LAVATORY A FLOORBOARD 221PF HAS A HOLE AND IS DELAMINATED. MAINT REMOVED AND REPLACED FLOORPANEL 221PF IAW AMM 53-22-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP NOTED CABIN FLOOR PANEL 251TF HAS A LARGE PUNCTURE HOLE. MAINT REPAIRED FLOOR PANEL 251TF IAW SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,261 hrs · 7,425 cycles

REFERENCE NON ROUTINE 34326. DURING C3 S1 C-CHECK INSPECTION NOTED LT HAND CABIN FLOOR LONGERON BEAM Y1162 BETWEEN FRAMES 66 AND FRAME 68 HAS CORROSION AROUND TWO FASTENER HOLES. MAINTENANCE REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED BEAM IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-00-14 BLOCK 201. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP, NOTED CABIN FLOORBEAM Y1292 AT FRAME 66 HAS CORROSION AROUND FASTENER. MAINT REMOVED CORROSION ON LONGERON BEAM Y1291 AT FRAME 66 AND FOUND TO BE OUT OF LIMITS. MAINT REMOVED AND REPLACED FLOORBEAM Y1292 AT FRAME 66 IAW SRM 53-00-14. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: PROFILE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 15,261 hrs · 7,425 cycles

REFERENCE NON ROUTINE 34044. DURING C3 S1 C CHECK INSPECTION NOTED FORWARD CARGO PIT HAS CORROSION BETWEEN FRAMES C28 AND FRAMES C34. MAINTENANCE REMOVED PROFILE AND INSTALLED NEW PROFILE AND ATTACH ANCHORS AND SPLICE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11 AND SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,261 hrs · 7,425 cycles

REFERENCE NON ROUTINE 34043. DURING C3 S1 C-CHECK INSPECTION NOTED CORROSION ON THE RT SIDE FORWARD CARGO COMPARTMENT RT PROFILE BETWEEN FRAMES C28 AND C34. MAINTENANCE REMOVED PROFILE ON THE RT SIDE FORWARD CARGO COMPARTMENT AT FRAME C28 TO FRAME C34 AND REPLACED WITH NEW PROFILE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11 AND SRM 51-42-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP, NOTED THE FWD FLOOR PANEL 132DG HAS A PUNCTURE. MAINT CLEANED AND PREPPED DAMAGED, APPLIED FILLER, FABRICATED REPAIR PATCH AND INSTALLED REPAIR PATCH IAW SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,261 hrs · 7,425 cycles

REFERENCE NON ROUTINE 34329. DURING C3 S1 C-CHECK INSPECTION NOTED THE CABIN FLOOR LONGERON BEAM Y765 HAD CORROSION AROUND FASTNER HOLE AT FRAME 68 AND BARE METAL FROM FRAME 66 TO FRAME 68. MAINTENANCE REMOVED AND REPLACED RT HAND CABIN FLOOR LONGERON BEAM Y765 FROM FRAME 66 TO FRAME 70 IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP, NOTED THE AFT CARGO COMPARTMENT HAS CORROSION ON RT PROFILE BETWEEN FRAMES C54 AND FRAMES C55. MAINT REMOVED AND REPLACED PROFILE AT AFT CARGO RT HAND SIDE BETWEEN FRAMES C54 AND C55 IAW SRM 51-72-11 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IN WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,261 hrs · 7,425 cycles

DURING C-CHECK INSP, NOTED THE FWD CARGO COMPARTMENT AFT MOST PROFILE HAS CORROSION ON SEVERAL SPOTS BETWEEN FRAMES C30 AND FRAME C34. MAINT REMOVED AND REPLACED PROFILE IAW SRM 51-72-11 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)