N909FR

ATA 3397

Part: LIGHT — MISWIRED (CABIN) · airframe 19,162 hrs · 8,091 cycles

BLOCK TURN BACK, FLIGHT CREW REPORTED L2 DOOR EMERGENCY EXIT LIGHT 'ON' DURING TAXI, EMERGENCY EXIT SIGN 'OFF' DURING TAXI. MAINTENANCE FOUND 45WL, EXIT MARKING SIGN, AND 33WL, EMERGENCY CABIN LIGHT, WIRED INCORRECTLY. REWIRED 45WL AND 33WL IAW AMM 33-51-00, SHEET 02, P101, FIG. 3. PERFORMED OPS CHECK IAW AMM 33-51-00, PAGE BLOCK 501, WITH NO DISCREPANCIES NOTED.

ATA 3350

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED "TEST EMERG LIGHT BAT" BATTERY CAPACITY CHECK FAILED. REMOVED AND REPLACED EMERGENCY EXIT BATTERIES IAW AMM 33-51-38-PB401. OPERATIONAL CHECK GOOD IAW 33-51-00-710-001, (S/N'S 26827, 24286, 26936, 042015).

ATA 2565

Part: SLIDE — FAULTED (R1 DOOR) · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED EMERGENCY LIGHT TEST SHOWED LEFT EPSU EXTERNAL FAULT. REPLACED R1 DOOR SLIDE IAW AMM 25-62-44-400-007.

ATA 5280

Part: ATTACH FITTING — CORRODED (RT MLG DOOR) · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED LWR FWD ATTACH FITTING ON RT MLG STRUT DOOR RUSTED. REMOVED AFFECTED PARTS AND INSTALLED LWR FWD ATTACH FITTING IAW MM 32-12-14-400-002.

ATA 5730

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON FUEL PANEL 640JB ATTACHMENT HOLES. REMOVED AND REPLACED FUEL PANEL 640JB ON RT WING IAW AMM 57-27-11-400-002. PERFORMED LEAK CHECK IAW 57-27-11-400-002, NO LEAKS FOUND.

ATA 5321

Part: BOLT — CORRODED (FLOOR MOUNT) · corrosion level 2 · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED THE FLOOR MOUNT BOLT ON THE AFT INBD CORNER OF THE AFT WALL OF LAV A WAS CORRODED AND COULD NOT BE REMOVED WITH STANDARD WRENCHES. THE HEAD WAS CUT OFF FROM BELOW TO REMOVE THE LAV WALL. REMOVED AND REPLACED BOLT IAW AMM 25-41-00.

ATA 5510

Part: PLATE — GOUGED · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED THE TRIMMABLE HORIZONTAL STAB MECHANICAL LINKAGE INBD OF UPPER CHAIN SPROCKET DAMAGED. SWIVEL PLATE AND LINK PLATE GOUGED. REPLACED SWIVEL PLATE AND LINK PLATE IAW AMM 27-41-45-400-001. PERFORMED OPERATIONAL CHECK IAW AMM 27-41-00-720-001, SWIVEL PLATE P/N D2747003600000, LINK PLATE P/N D2747003700000.

ATA 5321

Part: FLOOR PANEL — CORRODED · corrosion level 2 · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL THRESHOLD PANEL 222FF CORRODED TO EDGE. REMOVED AND REPLACED FLOOR THRESHOLD PANEL 222FF IAW AMM 53-12-12 AND WORK CARD CP753-12.

ATA 5321

Part: FLOOR PANEL — CORRODED · corrosion level 2 · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR THRESHOLD PANEL 221FF CORRODED TO EDGE. REMOVED AND REPLACED THRESHOLD PANEL 221FF IAW AMM 53-12-12 AND WORK CARD CP753-12.

ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED LT FLOORBEAM Y1292 CORRODED ON BOTTOM OF NUTPLATE HOLE AT FR66. FLOORBEAM FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14, PAGE 106. REMOVED AND REPLACED DAMAGED FLOORBEAM Y1292 SECTION FROM FR64 TO FR66 IAW 51-42-11.

ATA 5321

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON LOWER SURFACE OF FLOOR PANEL 261FF. REMOVED REPLACED FLOOR PANEL IAW SRM 51-24-00 AND AMM 53-42-12-400-002.

ATA 5321

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON TOP SURFACE OF FLOOR PLANEL 221EF AFT OTBD CONNECTING PLATE. REMOVED AND REPLACED CONNECTING PLATE IAW AMM 53-12-12-400-001.

ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CABIN FLOOR CENTER SUPPORT AT Y254, FR16, CORRODED. REMOVED DAMAGED AREA OF FLOORBEAM Y254 IAW SRM 53-00-14, FIG 204. REMOVED AND REPLACED FLOORBEAM AND ANGLES IAW SRM 51-42-11, EA NR A9-53R-12100 AND EA NR AO-51T-11976.

ATA 5321

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON LOWER SURFACE OF FLOOR PANEL 262FF. REMOVED AND REPLACED FLOOR PANEL 262FF IAW AMM 53-42-12-400-002.

ATA 5411

Part: SUPPORT ANGLE — CRACKED (RT NACELLE) · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED RT ENGINE PYLON SUPPORT ANGLE THAT ATTACHES PYLON PANELS 423DL AND 424CR AT RIB 5 CRACKED (AREA AROUND AFT SCREW HOLE). REMOVED AND FABRICATED REPLACEMENT SUPPORT ANGLE IAW SRM'S 54-52-12, P28, 51-31-00, P44,51-44-11, 51-42-11 AND 51-72-11, AND AIRBUS DRAWING S2 D54630462. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-42-11, P7.

ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT FLOORBEAM FROM STR 38R TO STR 38L CORRODED AROUND FASTENER HOLES. REMOVED AND REPLACED TRANSITION PLATE AT FR28 BETWEEN STR 38R THRU STR 38L IAW SRM 51-42-11.

ATA 5315

Part: FLOORBEAM — CORRODED (CORRODED) · corrosion level 2 · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON UNDERNEATH SIDE OF NUTPLATE HOLE AT FR66. REPLACED COUPLING IAW 51-42-11.

ATA 5320

Part: SHEAR PLATE — CORRODED · corrosion level 2 · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED SURFACE CORROSION AT AFT END OF LT SHEAR PLATE BETWEEN FR69 AND FR70. REMOVED AND REPLACED SHEAR PLATE BETWEEN FR69 AND FR70 IAW SRM 51-72-11 AND 51-42-11.

ATA 5320

Part: SHIM — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FWD FLOOR PROFILER IN FWD CARGO COMPARTMENT HAD CORROSION AROUND FASTENER HOLE. REMOVED CORROSION ON SHIM FROM AROUND FASTENER HOLE IAW SRM 51-73-00. BLENDED AREA WAS APPROX .5" BY .5" WITH MAX DEPTH OF .012". REMOVED, FABRICATED AND INSTALLED NEW SHIM IAW SRM 51-42-11, 53-21-14, FIG 3, 51-21-11, 51-75-12, AND AIRBUS DRAWING C2 D53913797.

ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED RT SUPPORT FRAME BETWEEN FR69 AND FR70 CORRODED. REMOVED AND REPLACED SUPPORT FRAME IAW A319 SRM 51-42-11.

ATA 5210

Part: SEAL — CORRODED (PAX DOOR) · corrosion level 2 · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED LT DOOR SEAL CORRODED AT NUT PLATE HOLE AT FR66. FABRICATED REPAIR ANGLE, FILLERS AND DOUBLER IAW SRM 53-41-14. INSTALLED SPLICE ANGLE, DOUBLERS AND FILLER IAW SRM 53-41-11.

ATA 5340

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FWD CARGO DOOR BOTTOM FRAME ALONG STR 38, JUST FWD OF FR26 FITTING BETWEEN 2ND AND 3RD LOCKING ROLLERS, CORRODED AT OTBD DOME NUT HOLE. REMOVED AND REPLACED FITTING AT FWD CARGO DOOR BOTTOM FRAME 26, STR 38, IAW A319 SRM 51-42-11 AND 51-72-11.

ATA 5730

Part: PANEL — CORRODED (WING) · corrosion level 2 · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON ATTACHMENT HOLES ON PANEL 540JB. REPLACED PANEL IAW A319 WORKCARD CP757-2

ATA 5320

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED RT SHEAR PLATE BETWEEN FR 69 AND FR 70 CORRODED. REMOVED AND REPLACED SHEAR PLATE IAW A319 SRM 51-42-11, PARA 6.B.

ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON UPPER SURFACE OF LT FLOORBEAM Y765 AT FR68. FLOORBEAM FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14, PG 106. REMOVED AND REPLACED FLOORBEAM AT FRAME 68-70 IAW A318 SRM 53-00-14, SRM 51-42-11, DRAWING D53472815 AND DRAWING D53472780.

ATA 5320

Part: PROFILE — CORRODED · corrosion level 2 · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION AROUND FWD CARGO COMPARTMENT AFT FLOOR PROFILE FASTENER HOLES. REMOVED AND REPLACED PROFILE IAW A319 SRM 51-42-11 AND 53-21-14.

ATA 5320

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,106 hrs · 8,074 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CABIN FLOOR LT DUMMY RAIL AT FR12 TO FR16 CORRODED. REMOVED AND REPLACED DUMMY RAIL IAW A319 SRM 51-42-11.

ATA 5610

Part: WINDOW — UNKNOWN (COCKPIT) · airframe 18,785 hrs · 7,956 cycles

DIVERSION AT FL 370, FLIGHT CREW HEARD A LOUD POP AND HISSING SOUND FROM THE CAPTAIN'S AFT SIDE WINDOW. AIRCRAFT DESCENDED TO 14000 RA AND LANDED AT KMCI. REPLACED CAPTAIN'S FIXED WINDOW AS A PRECAUTIONARY MEASURE IAW AMM 56-11-12. PERFORMED OPS TEST OF ANTI-ICE AND DEFOGGING SYSTEM AND CHECKED GOOD IAW AMM 30-42-00-7/0001.

ATA 5610

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 16,915 hrs · 7,205 cycles

UPON ARRIVAL AT GATE, CAPTAIN'S WINDSHIELD CRACKED. REPLACED NR 1 WINDSHIELD IAW AMM 56-11-11, PB 401, P/N STA320-2-7-1A, S/N 5910 (MFG SULLY). ON PUSHBACK, FIRST OFFICER'S WINDSHIELD CRACKED. REPLACED NR 2 WINDSHIELD IAW AMM 56-11-11, PB 401, P/N STA320-2-7-1A, S/N 56109 (PPG).