N918FR

Part: SKIN — DEBONDED (RT ELEVATOR) · airframe 38,817 hrs · 19,145 cycles

RT ELEVATOR THERMO GRAPHIC INSPECTION REVEALED INDICATIONS ON UPPER PANEL IRREGULAR IN SHAPE & BLACK IN COLOR. REPAIRED RT ELEVATOR UPPER SURFACE OF LIQUID INGRESS LAW SRM 55-20-00 PB 201, SRM 55-21-11 PB201. ACFT SCHEDULED BACK IN SERVICE ON 07/03/2014.

Part: SKIN — DEBONDED (LT ELEVATOR) · airframe 38,817 hrs · 19,145 cycles

LT ELEVATOR THERMO GRAPHIC INSPECTION REVEALED INDICATIONS ON UPPER PANEL IRREGULAR IN SHAPE & BLACK IN COLOR. REPAIRED LT ELEVATOR UPPER SURFACE OF LIQUID INGRESS IAW SRM 55-20-00 PB201, SRM 55-21-11 PB201 & CMM 55-21-15-210-010-601. ACFT SCHEDULED BACK IN SERVICE ON 07/03/2014.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,038 hrs · 18,184 cycles

EMERGENCY EXIT LIGHT ON SEAT 25C INOPERATIVE. REPLACED LIGHT ASSEMBLY, OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 36,439 hrs · 17,846 cycles

EPSU BATTERY FAULT, 12WL. R & R EPSU BATTERY IAW AMM 33-51-38-000-002 AND AMM 33-51-38-400-002, TESTED OK.

Part: COFFEEMAKER — SHORTED (GALLEY) · airframe 30,803 hrs · 14,925 cycles

ELECTRICAL ODOR, ACRID ODOR REPORTED IN AFT GALLEY AREA ABOVE COFFEE POT - WARM TO THE TOUCH. TOTAL CYCLES 114925. FOUND AFT INBD NR 2 COFFEEMAKER INOPERABLE, CB'S POPPED. PLACED COFFEEMAKER ON NEF 25-99-30AD.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,131 hrs · 14,585 cycles

C-CHECK: NON ROUTINE 38894; MAIN CABIN FLOORBEAM FROM FR66 TO FR68 HAS CORROSION. REPLACED CABIN FLOORBEAM FR66 TO FR68 IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,131 hrs · 14,585 cycles

C-CHECK, MAIN CABIN FLOORBEAM FR68- V765 HAS CORROSION. REPLACED MAIN CABIN FLOORBEAM FR68-V765 IAW SRM 51 -42-11 AND SRM 51 -44-11.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,131 hrs · 14,585 cycles

C-CHECK: MAIN CABIN FLOORBEAM FR68- Y1292 HAS CORROSION. REPLACED MAIN CABIN FLOORBEAM FR68-Y1292 IAW SRM 51-42-11, PARA 5A AND SRM 51 -44-11 TABLE 2.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,131 hrs · 14,585 cycles

C-CHECK: NON ROUTINE 38895; MAIN CABIN FR68 LT AFT DOOR SEAL BEAM HAS CORROSION. REPAIRED LT AFT DOOR SEAL BY REMOVING DAMAGE AND INSTALLING A REPAIR ANGLE IAW SRM 53-41-14, PB 201.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,131 hrs · 14,585 cycles

DURING C CHECK, MAIN CABIN FLOORBEAM FR68 -Y1292 FOUND CORRODED. REPLACED FLOORBEAM IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,131 hrs · 14,585 cycles

C-CHECK: MAIN CABIN FLOORBEAM FR66 Y254 IS CORRODED. REPLACED FLOORBEAM IAW SRM 51-42-11.

Part: ELECTRICAL BOX — FAULTY (NLG STEERING) · airframe 28,905 hrs · 13,966 cycles

PILOT REPORT, ON TAKEOFF AMBER NOSE WHEEL STEERING DISCONNECT ILLUMINATED. NO ASSOCIATED ECAM. PILOT DECLARED EMERGENCY BEFORE LANDING. NO FUTHER ABNORMALITIES. TROUBLESHOT IAW TSM 32-51-00-810-833. R & R NWS ELECTRICAL BOX OPS CHECKED GOOD IAW AMM 32-51-12, PB 401.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 27,669 hrs · 13,411 cycles

PILOT REPORT: LP 594710; AFT CARGO / LAV SMOKE DETECT FAULT. R & R THE AFT CARGO SMOKE DETECT UNIT (3WH) AND AFT LAV (E) DETECT UNIT. IAW AMM 26-46-15, PB 401. OPS TEST OK.

Part: CHANNEL — CORRODED (ZONE 100) · airframe 24,210 hrs · 11,728 cycles

DURING C5 C-CHECK INSP NOTED AFT PIT FRAME 59 FWD U CHANNEL CORRODED AT FASTENER HOLES. MX REMOVED AND REPLACED CHANNEL IAW SRM 51-42-11, SRM 51-44-11 AND SRM 51-75-11.

Part: PROFILE — CORRODED (ZONE 100) · airframe 24,210 hrs · 11,728 cycles

DURING C5 C-CHECK INSP NOTED AFT PIT PROFILE CORRODED. MX REMOVED AND REPLACED AFT PIT PROFILE AT FRAME 61 IAW SRM 51-42-11 PARAGRAPH 5 AND 6.

Part: PROFILE — CORRODED (ZONE 100) · airframe 24,210 hrs · 11,728 cycles

DURING C5 C-CHECK INSP NOTED AFT PIT CENTER FLOOR SUPPORT FRAME 59 TO FRAME 60 CORRODED AT FASTENER HOLE. MX REMOVED AND REPLACED AFT PIT CTR FLOOR SUPPORT FROM FRAME 59 TO FRAME 60 IAW SRM 51-42-11 PARAGRAPH 5, 6 AND 7.

Part: PROFILE — CORRODED (ZONE 100) · airframe 24,210 hrs · 11,728 cycles

DURING C5 C-CHECK INSP NOTED AFT PIT RT FLOOR SUPPORT PROFILE FROM FRAME 52 TO FRAME 55 CORRODED. MX REMOVED AND REPLACED AFT PIT RT FLOOR SUPPORT PROFILE FROM FRAME 52 TO FRAME 55 IAW SRM 51-42-11 PARAGRAPH 6.

Part: PROFILE — CORRODED (ZONE 100) · airframe 24,210 hrs · 11,728 cycles

DURING C5 C-CHECK INSP NOTED UPON REMOVAL OF PROFILE AT FRAME 58 IN AFT PIT FOUND CORROSION AT 2 FASTENER HOLES. MX REMOVED AND REPLACED SUPPORT FITTING REFERENCE SRM 51-42-11.

Part: PROFILE — CORRODED (ZONE 100) · airframe 24,210 hrs · 11,728 cycles

DURING C5 C-CHECK INSP NOTED AFT PIT LT FLOOR SUPPORT PROFILE FRAME 56 TO FRAME 58 CORRODED. MX REMOVED AND REPLACED AFT PIT LT FLOOR SUPPORT PROFILE FROM FRAME 56 TO FRAME 58 IAW SRM 51-42-11 PARAGRAPH 6.

Part: PROFILE — CORRODED (ZONE 100) · airframe 24,210 hrs · 11,728 cycles

DURING C5 C-CHECK INSP NOTED AFT PIT LT FLOOR SUPPORT PROFILE FRAME 52 TO FRAME 56 CORRODED. MX REMOVED AND REPLACED AFT PIT LT FLOOR SUPPORT PROFILE FRAME 52 TO FRAME 56 IAW SRM 51-42-11.

Part: FRAME — CORRODED (ZONE 100) · airframe 24,210 hrs · 11,728 cycles

DURING C5 C-CHECK INSP NOTED AFT PIT FRAME 56 ANGLE ON FWD SIDE OF FRAME IS CORRODED AT 2 FASTENER HOLES. MX REMOVED AND REPLACED ANGLE AT FRAME 56 IAW SRM 51-44-11.

Part: PROFILE — CORRODED (ZONE 100) · airframe 24,210 hrs · 11,728 cycles

DURING C5 C-CHECK INSP NOTED AFT PIT FRAME 56 PROFILE CORRODED AT FASTENER HOLES. MX REMOVED AND REPLACED PROFILE AT FRAME 56 IAW SRM 51-42-11 AND SRM 51-44-11.

Part: PROFILE — CORRODED (ZONE 100) · airframe 24,210 hrs · 11,728 cycles

DURING C5 C-CHECK INSP NOTED AFT PIT CTR FLOOR SUPPORT BETWEEN FRAME 57 AND FRAME 58 CORRODED AT FASTENER HOLE. MX REMOVED AND REPLACED FLOOR SUPPORT BETWEEN FRAME 57 AND FRAME 58 IAW SRM 51-42-11.

Part: PROFILE — CORRODED (ZONE 100) · airframe 24,210 hrs · 11,728 cycles

DURING C5 C-CHECK INSP NOTED AFT PIT CTR FLOOR SUPPORT BETWEEN FRAME 56 AND FRAME 57 CORRODED AT FASTENER HOLE. MX REMOVED AND REPLACED FLOOR SUPPORT BETWEEN FRAME 56 AND FRAME 57 IAW SRM 51-42-11, SRM 51-75-12 AND DWG D53470340.

Part: PROFILE — CORRODED (ZONE 100) · airframe 24,210 hrs · 11,728 cycles

DURING C5 C-CHECK INSP NOTED AFT PIT CTR FLOOR SUPPORT BETWEEN FRAME 58 AND FRAME 59 CORRODED AT FASTENER HOLE. MX REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-11.

Part: FRAME — CORRODED (ZONE 100) · airframe 24,210 hrs · 11,728 cycles

DURING C5 C-CHECK INSP NOTED AFT PIT FRAME 59 HAS EVIDENCE OF CORROSION IN FASTENER HOLES. MX REMOVED AND REPLACED FITTING IAW EA A9-53R-31612 AND EA A9-53R-31625.

Part: PROFILE — CORRODED (ZONE 100) · airframe 24,210 hrs · 11,728 cycles

DURING C5 C-CHECK INSP NOTED AFT PIT FRAME 59 PROFILE HAS CORROSION. MX REMOVED AND REPLACED PROFILE IAW SRM 51-42-11.

Part: PROFILE — CORRODED (ZONE 100) · airframe 24,210 hrs · 11,728 cycles

DURING C5 C-CHECK INSP NOTED AFT PIT FRAME 58 PROFILE CORRODED AT SEVERAL FASTENER HOLES. MX REMOVED AND REPLACED PROFILE IAW SRM 51-42-11.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK, INSP NOTED R1 DOOR FWD LOWER EXIT LIGHT IS BROKEN. MAINT REMOVED AND REPLACED R1 DOOR FWD LOWER EXIT LIGHT IAW AMM 33-51-13-400-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK, INSP NOTED THE RT LATERAL SHEAR PLATE AT Y-1162, FROM FRAME 69 TO FRAME 70, HAD CORROSION AND FOUR SHEARED FASTENERS AT THE FWD EDGE. MAINT REMOVED AND REPLACED THE LATERAL SHEAR PLATE AT Y-1162 AT FRAME 69 TO FRAME 70 IAW SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: SILL — DAMAGED (R2 DOOR) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK, INSP NOTED THE R2 DOOR SILL PLATE REQUIRED REPLACEMENT DUE TO MISDRILLED HOLE. MAINT REMOVED AND REPLACED R2 DOOR SILL PLATE IAW A319 SRM 51-42-11 AND 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — BROKEN (CARGO BAY) · airframe 18,974 hrs · 9,028 cycles

DURING C4 S1 C CHECK, INSPECTION NOTED THE AFT CARGO FLOORBOARD, 151CE, HAD TWO BROKEN CORNERS. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 151CE. INSTALLATION WAS COMPLETED ON EMPIRE AERO CENTER NON ROUTINE NR 9642. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: SKIN — DENTED (NR 1 NACELLE) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED THAT THE DAMAGE ON NR 1 ENGINE INLET COWL REQUIRES PERMANENT REPAIR OF DENT AT THE 2 O`CLOCK POSITION. MAINT REPAIRED DAMAGED AREA IAW CMM 54-10-00, REPAIR PROCEDURE NR 23. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FITTING — CORRODED (R1 GIRT BAR) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED THE R1 DOOR GIRT BAR FITTING IB MOUNT HOLES ON SILL PLATE HAD CORROSION. MAINT BLENDED CORROSION IAW SRM 51-74-00. MAINT REPAIRED AREAS THAT WERE DEEPER THAT .016" WITH A FILLER AND FILLED AREAS THAT WERE LESS THAN .016" WITH ADHESIVE IAW EA NR A9-53R-30461. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED THE AFT CARGO COMPARTMENT RT SIDE PROFILE HAD CORROSION AT FRAME 59 ON RT SIDE IAW A319 SRM 51-72-11 AND 51-44-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED THE AFT CARGO COMPARTMENT SMALL PROFILE RT SIDE JUST INSIDE DOOR FWD OF FRAME C56 HAS CORROSION. MAINT REMOVED SMALL PROFILE, FABRICATED NEW PROFILE, TREATED, PRIMED AND TOP COATED NEW PROFILE AND INSTALLED IAW SRM 51-21-11, 51-53-11, 51-42-11 AND DRAWING NR D53477068. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FITTING — CRACKED (NR 1 NACELLE) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED THE NR 1 ENGINE PYLON PANEL NR 413CL MOUNTS STRUCTURE WAS CRACKED AT AFT UPPER SCREW HOLE. MAINT REPAIRED NR 1 ENGINE PYLON PANEL NR 413CL MOUNT STRUCTURE AT AFT UPPER HOLE IAW SRM 54-52-12 AND 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: PROFILE — GOUGED (FUSELAGE) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED THE AFT CARGO COMPARTMENT PROFILE AT FRAME C63 IS GOUGED AND HAS A RIVET PULLING THROUGH. MAINT REMOVED AND REPLACED PROFILE AT FRAME C63 IAW SRM 51-72-11, 51-21-11 AND 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED CORROSION ON TOP LEG OF FRAME C55A AT FWD EDGE OF C2 DOOR. MAINT REPAIRED DAMAGE ON TOP LEG OF FRAME C55A IAW EA NR A9-53R-30442. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: BATTERY BOX — WORN (FUSELAGE) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP, NOTED AFT BATTERY TRAY OB FWD AND AFT MOUNTS HAVE WEAR. MAINT REMOVED AND REPLACED AFT BATTERY TRAY, OB FWD AND AFT MOUNTS IAW SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED THE AFT CARGO COMPARTMENT PROFILE AT FRAME C59 HAD CORROSION AT BOTH ENDS OF THE PROFILE. MAINT REMOVED AND REPLACED THE PROFILE IAW SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FRAME — CORRODED · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED AFT CARGO COMPARTMENT INSIDE OF C2 DOOR SHORT ANGLE PIECE AT FRAME C59 HAS CORROSION. MAINT REMOVED SHORT ANGLE PIECE APPLIED PROTECTION TREATMENT FABRICATED NEW SHORT ANGLE TREATED, PRIMED AND PAINTED AND INSTALLED IAW SRM 51-72-11, SRM 51-21-11, SRM 51-23-11 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED AFT CARGO COMPARTMENT CENTER FLOORBEAM HAS CORROSION BETWEEN FRAME C57 AND FRAME C58. MAINT REMOVED AND REPLACED CORRODED FLOORBEAM AT FRAME C57 AND FRAME C58 IAW SRM 51-41-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,974 hrs · 9,028 cycles

DURING C-4/S-1 C-CHECK, INSPECTION NOTED AFT CARGO COMPARTMENT CENTER FLOORBEAM BETWEEN FRAME C58 AND C59 HAS CORROSION. MAINTENANCE REMOVED AND REPLACED CORRODED FLOORBEAM IN ACCORDANCE WITH A319 SRM 51-42-11.

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,974 hrs · 9,028 cycles

DURING C-4/S-1 C-CHECK, INSPECTION NOTED AFT CARGO COMPARTMENT PROFILE AT FRAME C58 HAS CORROSION. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 AND 51-21-11.

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,974 hrs · 9,028 cycles

DURING C-4/ S-1 C-CHECK, INSPECTION NOTED THE AFT CARGO COMPARTMENT, LEFT SIDE PROFILE AFT OF FRAME C62, HAS CORROSION. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11, 51-21-11 AND 51-44-11.

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED CORROSION SEVERAL PLACES ON AFT MOST PROFILE AT FWD CARGO COMPARTMENT AFT OF FRAME C30. MAINT REMOVED AND REPLACED PROFILE IAW SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED RT LONGERON BEAM AT Y-1162 FROM FRAME 68 TO FRAME 69 HAD AREAS OF CORROSION. MAINT REMOVED AND REPLACED FLOORBEAM LONGERON Y-1162 FROM FRAME 68 TO FRAME 69 IAW SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP, NOTED CORROSION ON AFT CARGO COMPARTMENT LT PROFILE, FWD AREA OF AFT CARGO, AT FRAME C47 TO FRAME C51. MAINT REMOVED AND REPLACED PROFILE AT FRAME C47 TO FRAME C51 IAW SRM 51-72-11, 51-21-11 AND 51-42-11. UPON COMPLETION FO THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED RT LONGERON BEAM AT Y-1292 FROM FRAME 66 TO FRAME 68 HAD AREAS OF CORROSION. MAINT REMOVED AND REPLACED FLOOR SUPPORT LONGERON Y-1292 FROM FRAME 66 TO FRAME 69 IAW SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED CORROSION ON THE AFT CARGO COMPARTMENT PROFILE AT FRAME C56. MAINT REMOVED AND REPLACED PROFILE IN AFT CARGO COMPARTMENT AT FRAME C56 IAW A319 SRM 51-72-11 AND 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED CORROSION ON PROFILE PARALLEL WITH FRAME C28 FWD CARGO COMPARTMENT. MAINT REMOVED AND REPLACED CORRODED PROFILE ON FRAME C28 IN FWD CARGO COMPARTMENT IAW FO A319 SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: GIRT BAR — STICKING (R1 DOORWAY) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED R1 GIRT BAR FITTING FOR DOOR SLIDE STOP LEVER STICKS, DOES NOT SNAP BACK WHEN PRESSED DOWN AND RELEASED. MAINT REMOVED AND REPLACED WITH NEW GIRT BAR FITTING IAW AMM 52-11-31-000-003 AND 52-11-31-400-003. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED THE RT LONGERON BEAM Y-765 AT FRAME 66 HAD CORROSION AROUND THE HOLE. MAINT REMOVED AND REPLACED CORRODED LONGERON BEAM AT Y-765 FRAME 64 TO FRAME 66 IAW SRM 51-42-11 AND 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: SKIN — CHAFED (RT WING AILERON) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED THE RT AILERON APPEARS TO BE CHAFING AT IB LOWER EDGE. MAINT CLEANED AREA OF DAMAGE AND REPAIRED IAW SRM 51-75-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED CORROSION ON PLATE BELOW TIE-DOWN PLATE AT FRAME C29 FWD CARGO COMPARTMENT. MAINT REMOVED AND REPLACED FITTING, REINSTALLED PLATE AND TIE-DOWN AT FWD CARGO COMPARTMENT FRAME C29 IAW SRM 51-42-11 AND 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP, NOTED FLOOR PANEL 261PF HAD COMPOSITE DAMAGE. MAINT REMOVED AND REPLACED FLOOR PANEL 261PF WITH NEW PANEL, REFERENCED ON EAC NON ROUTINE ITEM 9651. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED CORROSION SEVERAL PLACES ON PROFILE LT SIDE AFT OF FRAME C28 FWD CARGO COMPARTMENT. MAINT REMOVED OLD PROFILE AT FRAME C28 ON LT SIDE, LOCATED AND DRILLED HOLES ON NEW PROFILE AND INSTALLED NEW PROFILE IAW SRM 51-72-11 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED CORROSION ON PLATE BELOW TIE-DOWN PLATE UNDER FRAME C25 FWD CARGO PIT. MAINT REMOVED PLATE AND BLENDED CORROSION, MORE THAN 50 PERCENT MATERIAL LOSS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-14 OUT TO LIMITS OR ACTIONS NOT STATED. MAINT FABRICATED AND INSTALLED PLATE IAW EA NR 918-5299 AND SRM 51-42-11. UPON COMPLETION OF REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED THE LT LONGERON BEAM AT Y765 AND FRAME 68 HAS AREAS OF CORROSION. MAINT REMOVED AND REPLACED THE LT LONGERON BEAM AT Y765 AND FRAME 68 IAW SRM 51-42-11 PAGE 1 AND 2.UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FITTING — WORN (FUSELAGE) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED BEAM NR TWO AT AFT WALL OF FWD CARGO COMPARTMENT MOUNT AND WALL BEAM HAS EXCESSIVE PLAY. MAINT REMOVED AND REPLACED BEAM NR 11 AFT WALL MOUNT FITTING IN THE FWD CARGO BAY IAW SRM 51-72-11 PAGE 1 AND 2. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FLOOR SUPPORT — WORN (FUSELAGE) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED BEAM NR FOUR AT AFT WALL MOUNT HAS EXCESSIVE PLAY AT MOUNT AT FLOOR TRACK IN THE FWD CARGO COMPARTMENT. MAINT REMOVED AND REPLACED BEAM NR FOUR AFT WALL MOUNT FITTING IN THE FWD CARGO COMPARTMENT IAW SRM 51-72-11 PAGE 1 AND 2. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP, NOTED THE LT LONGERON BEAM AT Y1162 AND FRAME 68 HAS AREAS OF CORROSION. MAINT REMOVED AND REPLACED THE LT LONGERON BEAM AT Y1162 AND FRAME 68 IAW SRM 51-72-11 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED LIGHTNING STRIKE ON FASTNER AT FRAME 29 STATION 1270 STRINGER 41. MAINT REPAIRED BY REMOVING BLIND FASTNER AND COLD WORKING HOLE AND INSTALLING LOCK FASTENER IAW SRM 51-42-11, SRM 51-48-00 AND SRM 53-21-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FITTING — WORN (FUSELAGE) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED THE FWD CARGO COMPARTMENT AFT WALL BRACE MOUNT AT UPPER FLOOR TRACKS HAS EXCESSIVE PLAY ON BEAM NR 1. MAINT REMOVED AND REPLACED BEAM NR 1 AFT WALL MOUNT FITTING IN THE FWD CARGO BAY IAW SRM 51-72-11 PAGE 1 AND 2. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: CARGO TRACK — WORN (CARGO BAY) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP, NOTED BEAM NR 11 HAS EXCESSIVE PLAY AFT WALL OF FWD CARGO PIT AT FLOOR TRACK. MAINT REMOVED AND REPLACED BEAM NR 11 AFT WALL MOUNT FITTING IN FWD CARGO BAY IAW SRM 51-72-11 PAGE 1 AND 2. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FLOORBOARD — PUNCTURED (FUSELAGE) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED AFT CARGO COMPARTMENT FLOORBOARD 151DE HAS A PUNCTURE IN IT. MAINT CLEANED, PREPPED AND REPAIRED FLOORBOARD 151DE IAW SRM 53-02-00 PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FLOORBOARD — PUNCTURED (FUSELAGE) · airframe 18,974 hrs · 9,028 cycles

REFERENCE NON ROUTINE 36564. DURING C-CHECK INSP NOTED AFT CARGO COMPARTMENT FLOORBOARD 151AE IS PUNCTURED. MAINT CLEANED PREPPED AND REPAIRED FLOORBOARD 151AE IAW OF SRM 53-02-00 PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED LIGHTNING STRIKE ON FASTNER AT FRAME 26 STATION 1057 STRINGER 40. MAINT REPAIRED BY MOVING BLING FASTNER AND COLD WORKING HOLE AND INSTALLING HI-LOCK IAW SRM 51-42-11, SRM 51-48-00 AND SRM 53-21-11 FIGURE 201. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FLOORBOARD — PUNCTURED (FUSELAGE) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED AFT CARGO COMPARTMENT FLOORBOARD 151TG HAS A PUNCTURE IN IT. MAINT CLEANED, PREPPED AND REPAIRED FLOORBOARD 151TG IAW SRM 53-02-00 PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FLOORBOARD — CRACKED (FUSELAGE) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED FLOORBOARD 251HF HAS A CRACK IN THE TOP OF THE BOARD. MAINT PREPPED AREA OF DAMAGE ON FLOORBOARD 251HF FOR REPAIR AND REPAIRED IAW ARM 53-12-00 PARAGRAPH 5B FIGURE 202. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED LT LATERAL SHEAR PLATE AT Y1162 FROM FRAME 69 TO FRAME 70 HAS CORROSION AND FOUR SHEARED FASTNERS AT FWD END. MAINT REMOVED AND REPLACED LT LATERAL SHEAR PLATE AT Y1162 FRAME 69 TO FRAME 70 IAW SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 18,974 hrs · 9,028 cycles

REFERENCE NON ROUTINE 29004. DURING C-CHECK INSP NOTED LIGHTNING STRIKE FOUND AT FRAME 25 STATION 1003 STRINGER 41R. MAINT REPAIRED BY REMOVING BLIND FASTNER AND INSTALLED HI-LOCK IAW SRM 51-42-11, SRM 51-48-00, AND SRM 53-21-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FLOORBOARD — PUNCTURED (FUSELAGE) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED CABIN FLOORBOARD 242FF IS PUNCTURED IN THE CENTER OF THE PANEL. MAINT PREPPED FLOORBOARD 242FF FOR REPAIR AND REPAIRED IAW SRM 53-12-00 PARAGRAPH 5B FIGURE 202. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: SKIN — DAMAGED (BS 927 S38L) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP, NOTED LIGHTNING STRIKE BURN MARK BELOW FWD CARGO DOOR STATION 927 AT STRINGER 38. MAINT REPAIRED BY REMOVING BLIND FASTENER COLD WORKING HOLE AND INSTALLING LOCK FASTENER IAW SRM 51-42-11, SRM 51-48-00 AND SRM 53-21-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FLOORBOARD — PUNCTURED (FUSELAGE) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED AFT CARGO COMPARTMENT FLOORBOARD 151BE HAS A PUNCTURE IN IT. MAINT CLEANED, PREPPED AND REPAIRED FLOORBOARD 151BE IAW SRM 53-02-00 PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED AFT CARGO COMPARTMENT FLOORBOARD 152TG HAS A PUNCTURE IN PANEL. MAINT CLEANED, PREPPED AND REPAIRED FLOORBOARD 152TG IAW SRM 53-02-00 PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED LIGHTNING STRIKE BURN MARK BELOW FWD CARGO DOOR STATION 979 AT STRINGER 38. MAINT REMOVED AND REPLACED BLIND FASTNER WITH HI-LOCK AFTER COLD WORKING HOLE AT STATION 979 STRINGER 38 IAW SRM 53-21-11 FIGURE 210. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FLOORBOARD — DELAMINATED (FUSELAGE) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED FLOORBOARD 241FF HAS DELAMINATION ALONG THE EDGE OF THE FLOORBOARD. MAINT PREPPED AREA OF DAMAGE ON FLOORBOARD 241FF FOR REPAIR AND REPAIRED IAW SRM 53-02-00 PARAGRAPH 8J FIGURE 212. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FLOOR SUPPORT — CORRODED (EMERGENCY LIGHT) · corrosion level 2 · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED AFT CARGO COMPARTMENT CENTER FLOORBEAM BETWEEN FRAME C60 AND FRAME C61 HAS CORROSION. MAINT REMOVED AND REPLACED FLOORBEAM BETWEEN FRAME C60 AND FRAME C61 IAW REQUIREMENTS OF SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: BOTTLE — LOW (L2 DOOR ASSIST) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP, NOTED L2 DOOR ASSIST BOTTLE PRESSURE IS LOW. MAINT SERVICED L2 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED RT INTERCOSTAL WEB UNDER LATERAL SHEAR PANEL AT STRINGER 23 RT FROM FRAME 69 TO FRAME 70 HAS CORROSION ON BOTTOM SIDE. MAINT REMOVED CORRODED INTERCOSTAL, LOCATED AND DRILLED NEW INTERCOSTAL, TREATED AND PRIMED HOLES AND INSTALLED NEW INTERCOSTAL WEB IAW SRM 51-72-11, SRM 51-42-11 AND SRM 51-21-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FITTING — WORN (BATTERY TRAY) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP NOTED FWD BATTERY TRAY OB AFT MOUNT HAS WEAR. MAINT REMOVED AND REPLACED FWD BATTERY TRAY OB AFT MOUNT IAW SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 18,974 hrs · 9,028 cycles

DURING C-CHECK INSP, NOTED LT INTERCOSTGAL WEB UNDER LATERAL SHEAR PLATE AT STRINGER 23 LT FROM FRAME 69 TO FRAME 70 HAS CORROSION ON TOP AND BOTTOM SIDES. MAINT REMOVED CORRODED WEB, DRILLED, TREATED AND PRIMED HOLES AND INSTALLED NEW WEB IAW SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: SKIN — DAMAGED (LT WING) · airframe 16,102 hrs · 7,626 cycles

INSPECTION REPORTED LIGHTNING DAMAGE TO LEFT WING UPPER SURFACE RIB 17, APPROX 12 INCHES AFT OF MIDSPAR AT FASTENER LOCATION. REMOVED FASTENER, BLENDED DAMAGE TO COUNTERSINK IAW SRM 51-11-13. REPLACED FASTENER IAW EA A9-574-12145.

Part: FASTENER — DAMAGED (LT WING) · airframe 16,102 hrs · 7,626 cycles

INSPECTION REPORTED LIGHTNING DAMAGE TO LEFT WING UPPER SURFACE AT FASTENER INBOARD OF RIB 17 AT MID SPAR. REMOVED DAMAGED FASTENER, BLENDED DAMAGED AREA, PERFORMED REQUIRED NDT PROCESS, AND INSTALLED NEW FASTENER IAW EA A9-57R-12145.

Part: FASTENER — DAMAGED (LT WING) · airframe 16,102 hrs · 7,626 cycles

INSPECTION REPORTED LIGHTNING DAMAGE TO LEFT WING UPPER SURFACE AT FASTENER RIB 17, JUST FWD OF NR 4 SPOILER. REMOVED DAMAGED FASTENER, PERFORMED REQUIRED NDT PROCESS, AND INSTALLED NEW FASTENER IAW EA A9-57R-12145.

Part: FASTENER — DAMAGED (LT WING) · airframe 16,102 hrs · 7,626 cycles

INSPECTION REPORTED LIGHTNING DAMAGE TO LEFT WING UPPER SURFACE AT FASTENER RIB 17, 12 INCHES FWD OF AFT SPAR. REMOVED DAMAGED FASTENER, BLENDED DAMAGED AREA, PERFORMED REQUIRED NDT PROCESS AND INSTALLED NEW FASTENER IAW EA A9-57R-12145.

Part: MONITOR — INOPERATIVE (BRAKE TEMP) · airframe 15,345 hrs · 7,253 cycles

AFTER TAKEOFF FROM KDCA, RECEIVED ECAM FOR HOT BRAKES. LOWERED GEAR AND NR 2 BRAKE INDICATED 980 DEG C. SHORTLY AFTER, NR 2 BRAKE INDICATOR WENT TO 2 AMBER XX FOR TEMP INDICATOR. FLIGHT CREW DECLARED AN EMERGENCY AND DIVERTED TO KIAD. AIRCRAFT LANDED WITHOUT INCIDENT AND TAXI WAS NORMAL. ITEM WAS TRANSFERRED TO MEL REF 32-47-01A, CONTROL NR 1028764. PULLED AND COLLARED C/B 37 PER MEL. UPON ARRIVAL IN DEN, REPLACED THE BRAKE TEMP MONITORING UNIT IAW AMM 32-47-18-400-001 AND OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,792 hrs · 6,512 cycles

DURING C-3 CHECK, INSPECTION REPORTED FWD EMERGENCY LIGHTING BATTERY FAILED DURING OPS CHECK. REPLACED FWD EPSU BATTERY(10WL) IAW AMM 33-51-38-400-002.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 13,792 hrs · 6,512 cycles

DURING C-3 CHECK, INSPECTION REPORTED AFT EMERGENCY LIGHTING BATTERY FAILED DURING OPS CHECK. REPLACED AFT EPSU BATTERY (13WL) IAW AMM 33-51-38-400-002.

Part: CONTROL CABLE — STUCK (ESCAPE SLIDE) · airframe 13,792 hrs · 6,512 cycles

DURING C-3 CHECK, INSPECTION REPORTED RT FLEXIBLE CONTROL CABLE FOR OVERWING SLIDE INFLATION BOTTLES WOULD NOT RETRACT. REPLACED RT FLEXIBLE CONTROL CABLE FOR OVERWING SLIDE INFLATION BOTTLE IAW AMM 25-62-43-000-001, AMM 25-62-43-400-001, MM 25-23-43, PB 401, AND MM 25-23-48, PB 401.

Part: RESERVOIR — DAMAGED (EMERGENCY SLIDE) · airframe 13,792 hrs · 6,512 cycles

DURING C-3 CHECK, INSPECTION REPORTED CABLE END ON LT OVERWING EMERGENCY SLIDE INFLATION BOTTLE BROKEN OFF. REPLACED LT INFLATION RESERVOIR OVER-WING ESCAPE SLIDE IAW AMM 25-62-46-000-001 AND 25-62-46-400-001. CONNECTED LT OVERWING ESCAPE SLIDE CABLE IAW 25-62-43-400-001.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 13,792 hrs · 6,512 cycles

DURING C-3 CHECK, INSPECTION REPORTED RT OVERWING EMERGENCY LIGHTING BATTERY FAILED DURING OPS CHECK. REPLACED RT OVERWING EPSU BATTERY IAW AMM 33-51-38-400-002.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 13,792 hrs · 6,512 cycles

DURING C-3 CHECK, INSPECTION REPORTED LT OVERWING EMERGENCY LIGHTING BATTERY FAILED DURING OPS CHECK. REPLACED LT OVERWING EPSU BATTERY (11WL) IAW AMM 33-51-38-400-002.

Part: GIRT BAR — CORRODED (R2 DOOR) · corrosion level 2 · airframe 13,792 hrs · 6,512 cycles

DURING C-3 CHECK, INSPECTION REPORTED R2 FWD GIRT BAR PLATE CORRODED. REPLACED R2 DOOR FWD GIRT BAR PLATE IAW MM 52-13-31. REPLACED R2 DOOR FWD GIRT FITTING BLANKING PLATE IAW MM 52-13-31.

Part: GIRT BAR — CORRODED (L2 DOOR) · corrosion level 2 · airframe 13,792 hrs · 6,512 cycles

DURING C-3 CHECK, INSPECTION REPORTED L2 FWD GIRT BAR PLATE CORRODED. REPLACED L2 DOOR GIRT BAR PLATE IAW AMM 52-13-31. REPLACED L2 DOOR GIRT BAR BLANKING PLATE IAW AMM 52-13-31-400-007.

Part: PLATE — CORRODED (GIRT BAR) · corrosion level 2 · airframe 13,792 hrs · 6,512 cycles

DURING C-3 CHECK, INSPECTION REPORTED L2 AFT GIRT BAR PLATE CORRODED. REPLACED L2 DOOR GIRT BAR PLATE PER MM 52-13-31. REPLACED L2 DOOR GIRT BAR FITTING BLANKING PLATE PER AMM 52-13-31-400-007.

Part: GIRT BAR — CORRODED (R2 DOOR) · corrosion level 2 · airframe 13,792 hrs · 6,512 cycles

DURING C-3 CHECK, INSPECTION REPORTED R2 AFT GIRT BAR PLATE CORRODED. REPLACED R2 DOOR AFT GIRT BAR PLATE IAW MM 52-13-31. REPLACED R2 DOOR AFT GIRT BAR FITTING BLANKING PLATE IAW AMM 52-13-31400-007.

Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,792 hrs · 6,512 cycles

DURING C-3 CHECK, INSPECTION REPORTED FLOORBOARDS 261FF AND 262FF CORRODED. REPLACED FLOORBOARDS 261FF AND 262FF PER AMM 53-42-12-400-002.

Part: TIRE — FAILED (MLG) · airframe 9,115 hrs · 4,187 cycles

UPON LANDING IN DEN, BOTH NOSE WHEEL TIRES CAME APART. REPLACED BOTH NOSE TIRES PER MM 32-41-12, PG 401. COMPLIED WITH INSPECTION AFTER TIRE BURST PER MP 05510-7.

Part: FLOW VALVE — FAULTY (LT A/C PACK) · airframe 5,143 hrs · 2,279 cycles

FLIGHT CREW REPORTED PASSENGERS IN AND AROUND ROWS 9, 10 AND 11 REPORTED ODOR WHICH SMELLED LIKE RUBBER. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. PRESSURIZED AIRCRAFT TO 4.5 DIFFERENTIAL PRESSURE, NO UNUSUAL ODORS NOTED. FOUND NR 1 (LT) PACK FLOW CONTROL VALVE FAULTY. REPLACED FCV AND CHECKED OKAY. PERFORMED VISUAL INSPECTION OF LIVE TV COMPONENTS BETWEEN ROWS 9 AND 13, FOUND ALL CONNECTORS SECURE AND NO SIGNS OF OVERHEATING/BURNING. SYSTEM OPS CHECKED GOOD PER MM 44-25-00.

Part: SKIN — GOUGED (FUSELAGE) · airframe 3,901 hrs · 1,741 cycles

INSPECTION REPORTED A GOUGE IN LT AFT FUSELAGE JUST FWD OF PRESSURE BULKHEAD, ZONE 261, STR 19L. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-41-11 FIG 105. REPAIRED DAMAGE PER SRM 53-00-11, 51-42-11, 51-47-00, 51-21-11, 51-23-00 AND 51-76-16.