N905FR

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,004 hrs · 21,979 cycles

AIRCRAFT C 9 CHECK. LT SHEAR PLATE IS CRACKED AT FRAME 69. R & R LT SHEAR PLATE SRM 57-42-11 EA A0-53T-30654.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,004 hrs · 21,979 cycles

AIRCRAFT DUE C 9 CHECK. MAIN CABIN FLOORBEAM HAS CORROSION AT FRAME 68, -Y1292. BLENDED DAMAGED AREA & REMOVED CORROSION. ORIGINAL THICKNESS .150 INCHES & .116 INCHES REMAINS. MAX ALLOWABLE DAMAGE DEPTH IS .016 INCHES SO BLEND OUT WAS OUT OF LIMITS. R & R FLOORBEAM IAW SRM 51-42-11 PAR 5 A-C. ACFT DUE OUT OF C CHECK 11-15-2014.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,004 hrs · 21,979 cycles

AIRCRAFT DUE C 9 CHECK. MAIN CABIN RT SHEAR PLATE IS CRACKED 3 INCHES AFT OF FRAME 69. R & R CRACKED SHEAR PLATE IAW SRM 51-42-11 PAR 6 & 13 & EO A0-53EO-31434. ACFT DUE OUT OF C CHECK 11-15-2014.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 44,320 hrs · 21,616 cycles

EPSU FWD LT INT LOAD FAULT FOUND ON HEAVY SERVICE CHECK. R & R 6 LAMPS ON R1 DOOR OVERHEAD EXIT SIGN & 6 LAMPS ON THE R2 DOOR OVERHEAD SIGN IAW AMM 33-51-11-PB 401.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 44,320 hrs · 21,616 cycles

EPSU FWD LT INT LOAD FAULT FOUND ON HEAVY SERVICE CHECK. R & R 6 LAMPS ON R1 DOOR OVERHEAD EXIT SIGN & 6 LAMPS ON THE R2 DOOR OVERHEAD SIGN IAW AMM 33-51-11-PB 401.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 40,500 hrs · 19,556 cycles

DURING HEAVY SERVICE CHECK, PERFORMED OPS CHECK OF EMERGENCY LIGHT SYSTEM. RECEIVED FAULT MESSAGE, EPSU INT. LOAD EMERGENCY RT. R & R L2 AND R2 EMERGENCY LOCATION SIGNS IN REF TO AMM 33-51-17 PB 40. OPS CHECKED GOOD. REPLACED BOTH THE L2 (45WL) AND RT (44WL) EXIT SIGN ASSEMBLIES BECAUSE THERE WERE LAMPS BURNED OUT. REPLACED BOTH ASSEMBLIES CLEARED THE EPSU FAULT. REPLACED THE OLD STYLE INCANDESCENT SIGN WITH THE NEW STYLE LED SIGN.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 40,134 hrs · 19,362 cycles

THERMOGRAPHIC INSPECTION REVEALED INDICATIONS ON UPPER PANEL IRREGULAR IN SHAPE AND BLACK IN COLOR. LT ELEVATOR, PN D55280001004, SN CC2451. REPAIRED IAW SRM 55-20-00, PB201, PARAGRAPH 2.A(1-2), 2.B(1), 2.B(2)1-10, SRM 55-21-11, PB201, C1 PARAGRAPH 5.E (2) (C) 2, 5.E (2) (C) 3. 5.E(2) (F)1-6, 5.E(2) (G) AND CMM 55-21-15-2010-G01, SECTION A(1-8) (9) (B). ACFT TO BE PLACED BACK INTO SERVICE 5/24/2013.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 40,134 hrs · 19,362 cycles

THERMOGRAPHIC INSPECTION REVEALED INDICATIONS ON BOTH UPPER AND LOWER PANELS IRREGULAR IN SHAPE AND BLACK IN COLOR, RT ELEVATOR, PN D55280001005, SN CC2452. REPAIRED IAW SRM 55-20-00, PB201, PARAGRAPH 2.A(1-2), 2.B(1), 2.B(2)1-10, SRM 55-21-11, PB201, C1 PARAGRAPH 5.E(2)(C)2, 5.E(2)(C)3. 5.E(2)(F)1-6, 5.E(2)(G) AND CMM 55-21-15-2010-G01, SECTION A(1-8)(9)(B). AIRCRAFT TO BE PLACED BACK INTO SERVICE 5/24/2013.

Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 38,429 hrs · 18,450 cycles

LEFT SHEAR PLATE CRACKED,& CORRODED, FRAME 70. R & R SHEAR PLATE IAW EO AO-53EO-31434.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 38,429 hrs · 18,450 cycles

DURING C-CHECK, MAIN CABIN FLOORBEAM BETWEEN FRAME 16 AND FRAME 18 AT Y254 HAS CORROSION. R & R BEAM REF SRM 51-42-11, PARA 5, 6 AND 7.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,429 hrs · 18,450 cycles

DURING C-CHECK, SILL PLATE AT AFT CARGO DOOR HAS NUMEROUS PLACES OF CORROSION. REMOVED CORROSION IAW SRM 51-74 -00, FOUND AREAS TO BE WITHIN LIMITS IAW SRM 51-73-00, FIGURE 001. TREATED, PRIMED AND PAINTED IAW SAM 51-21-11 AND SRM 5L-75-12.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,163 hrs · 18,313 cycles

DURING C-CHECK, WHILE PERFORMING HEAVY SERVICE CHECK, FOUND LT WINDSCREEN FWD EMERGENCY LIGHT WAS INOPERATIVE. R & R LT FORWARD EMERGENCY LIGHT BULB IAW AMM 33-51-19-020-002-A, STEP 4A2, 482A AND OPERATIONAL CHECKED GOOD IAW AMM 33-51-00-710-009.

Part: TRAY — CORRODED (ZONE 200) · corrosion level 2 · airframe 38,429 hrs · 18,450 cycles

DURING C-CHECK, FRAME 68, RT SIDE TRAY IS CRACKED. R & R TRAY IAW SRM 51-42-11 PARA 6, 7 AND 13.

Part: WARNING LIGHT — FALSE ACTIVATION (NR 1 GENERATOR) · airframe 38,352 hrs · 18,412 cycles

VENT VANES SVS FAULT IN FLIGHT. GENERATOR 1 LINE SMOKE INDICATION UPON LANDING NO VISIBLE SMOKE SEEN OR SMELLED IN FLIGHT DECK OR IN CABIN. NO EVIDENCE FOUND OF SMOKE PERFORMED SYS RESET NO FAULT NOTED REF AMM AMM 21-26-00 PB 501.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 37,760 hrs · 18,100 cycles

ON HEAVY CHECK, FOUND SEAT ROW 15 EMERGENCY EXIT LIGHT LAMP INOPERATIVE AND LIGHT LENS CRACKED. THE LAMP AND LENS WERE REPLACED IAW THE AMM AND THE LIGHT CHECKED GOOD.

Part: PROXIMITY SENSOR — FAILED (MLG) · airframe 37,115 hrs · 17,765 cycles

NR 2 ENGINE THRUST REVERSER DURING FLIGHT. DIVERTED, IAW FOM VOL 2 LAND ASAP LANDING WHEIGHT 126.5 ALL INDICATION NORMAL. REPLACED LT MLG PROXIMITY SENSOR.

Part: SUPPORT FITTING — CORRODED (MLG) · corrosion level 2 · airframe 34,352 hrs · 16,394 cycles

C-CHECK: NON ROUTINE NR 36085; RT WING MLG SUPPORT RIB 5 FORWARD LUG INNER BORE HAS CORROSION. REFERENCES EO AO-57EO-20243. REMOVED CORROSION BY OVER SIZING BORE TO 3.7995" AND INSTALL NEW BUSHINGS IAW SRM 57-26-13, PARA 5C, FIG 203 AND 204.

Part: WARNING LIGHT — ILLUMINATED (R2 DOOR) · airframe 31,147 hrs · 15,347 cycles

F/A REPORT DOOR 2R, "CABIN PRESS" LIGHT CYCLING/FLASHING, NOTE : LEVELED OFF AT 10K, CHECKED "DOOR" SLIDE AT 2R SHOWED DISARMED: P"PRESS" PG SHOWED NORMAL. PRESS & DIFF UPON LANDING "CABIN PRESSURE" IT WENT OUT AND 2R SHOWED ARMED. MEL REF 52-70-02A F/A REPORTS "SLIDES DISARMED" LIGHT FLASHING ON THE F/A PANEL. NOTE SLIDES ALL ARMED PRIOR TO TAKE OFF. SLIDE AT 2R SHOWED DISARMED AND AFTER TAKE OFF SLIDE SHOWED ARMED AFTER LANDING. CORRECTED ACTION MEL REF 25-60-03A.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 31,661 hrs · 15,109 cycles

ATB PILOT DECLARE AN EMERGENCY, PILOT LOG REPORT PAGE 546390 ITEM 1. ATB DUE TO HYDRAULIC BLUE SYSTEM LOSS. REMOVED AND REPLACED BLUE HYDRAULIC PUMP IAW AMM 29-12-51 PB 401. OPERATIONAL AND LEAK CHECK NORMAL.

Part: ENGINE — OVERSERVICED (NR 2) · airframe 31,106 hrs · 14,841 cycles

AIR TURN BACK DUE TO OIL TEMP TRENDING TOWARD EXCEEDANCE. REACHED 135 DEGREES CELCIUS MAXIMUM. PRECAUTIONARY RETURN BASED. ALSO ON ENGINE START, OIL PRESSURE REMAINED IN RED ARC UNTIL ABOUT 52.5 PERCENT N1. OIL QUANTITY INDICATED 20.5 QUARTS. FOUND NR 2 ENGINE OIL TO BE OVERSERVICED. REMOVED 32 QUARTS TOTAL OIL FROM NR 2 ENGINE OIL TANK, ANGLE GEARBOX, AND TRANSFER GEARBOX. RESERVICED OIL. R & R MAIN OIL SUPPLY FILTER. PERFORMED VISUAL INDICATOR POP OUT FUNCTIONAL CHECK. PERFORMED CHECK OF THE ELECTRICAL MASTER CHIP DETECTOR FOR PARTICLES. NO ABNORMALATIES NOTED. PERFORMED CHECK OF FWD AND AFT SUMP, ANGLE GEARBOX AND TRANSFER GEARBOX SUMP SCAVENGE SCREENS. NO ABNORMAILITIES NOTED. DRAINED, REPLACED IDG FILTERS AND REPLENISHED IDG OIL. PERFORMED MINIMUM IDLE LEAK CHECK OF NR 2 ENG. NO LEAKS NOTED. FLIGHT CREW PERFORMED ENG RUNS, OBSERVED NR 2 ENG RAN AT NORMAL PARAMETERS ABOVE THE MIN 70 PERCENT N1 AND MORE THAN TEN MINUTES. CHECKED SCAVENGE OIL SCREENS (FWD, AFT, ANGLE GB AND TRANSFER GB. CHECKED MASTER CHIP DETECTOR. NO ABNORMAILITIES FOUND.

Part: VALVE — FAILED (FUEL RETURN) · airframe 31,105 hrs · 14,840 cycles

ON CLIMBOUT NR 2 ENGINE OIL OVERTEMP. SHUTDOWN ENGINE NR 2 IAW ECAM. MAXIMUM NOTED OIL TEMP 160 DEGREES CELCIUS. MAXIMUM NOTED OIL PRESSURE WAS ABOUT 36 PSI, 10 PSI LOWER THAN ENGINE NR 1. R & R FUEL RETURN VALVE ASSY FOR NR 2 ENGINE. REF AMM 73-11-50 PAGE BLOCK 401. NOTE: POST FLIGHT REPORT FROM THE CFDS MCDU SHOWED A FAILURE MESSAGE FOR THE "FRV". TSM 79-00-00-810-805 DRIVES TOWARD REPLACEMENT OF THE FUEL RETURN VALVE WHEN THIS FAULT MESSAGE IS RECORDED BY THE CFDS.

Part: ANTI-ICE VALVE — FAULTY (LEFT) · airframe 28,423 hrs · 13,590 cycles

PILOT MADE AN AIR TURN BACK TO DEN DUE TO A WARNING ON THE ELECTRONIC CENTRALIZED ACFT MONITORING SYS FOR 'WING ANTI-ICE LT AND RT VALVE OPEN'. MX REMOVED AND REPLACED THE LT WING ANTI-ICE VALVE AND PERFORMED AN OPS TEST IAW AMM 30-11-51-000-001, 30-11-51-400-001 AND 30-11-00-710-001. (NOTE: RT VALVE WAS PLACED ON MEL.) OPS CHECK WAS NORMAL AND ACFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 28,422 hrs · 13,589 cycles

DURING C6 C-CHECK, INSPECTION NOTED CORROSION ON THE FLOOR PANEL ATTACH HOLES, LOCATED AT STATION -Y1292 BETWEEN FRAMES 66 AND 68. MAINTENANCE REMOVED AND REPLACED THE FLOOR BEAM IAW SRM 51-74-00, SRM 53-00-14, SRM 51-42-11, SRM 51-44-11 AND SRM 51-75-12.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 28,422 hrs · 13,589 cycles

DURING C6 C-CHECK, INSPECTION NOTED CORROSION ON THE FLOOR PANEL ATTACH HOLES, LOCATED A STATION Y1292, BETWEEN FRAMES 66 AND 68. MAINTENANCE REMOVED AND REPLACED THE FLOOR BEAM IAW SRM 53-00-14, SRM 51-42-11 AND SRM 51-44-11.

Part: SHEAR PLATE — CORRODED (ZONE 100) · airframe 28,422 hrs · 13,589 cycles

REFERENCE NON ROUTINE C072599. DURING DEN C6 C-CHECK, INSPECTION NOTED CORROSION ON A RIGHT HAND AFT SHEAR PLATE. MAINTENANCE REMOVED AND REPLACED THE SHEAR PLATE IAW SRM 51-42-11, 51-44-00, 51-46-00, 51-21-11, AMM 38-31-36-000-001 AND AMM 38-31-00-710-062.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 28,422 hrs · 13,589 cycles

REFERENCE NON ROUTINE C072422. DURING DEN C6 C-CHECK, INSPECTION NOTED CORROSION ON THE FLOOR SUPPORT AT STATION Y765 AND FRAME 68. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, 53-00-14, 53-41-14 ABD 51-23-11.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 28,422 hrs · 13,589 cycles

REFERENCE NON ROUTINE C072454. DURING DEN C6 C-CHECK, INSPECTION NOTED CORROSION AT THE FLOOR BOARD ATTACH HOLES AT STATION -Y762 AND FRAMES 66 TO 68. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, 51-44-11, 51-75-12 AND 53-00-14.

Part: SILL — CORRODED (ZONE 200) · airframe 28,422 hrs · 13,589 cycles

REFERENCE NON ROUTINE C072351. DURING DEN C6 C-CHECK, INSPECTION NOTED CORROSION ON THE L2 DOOR SILL BEAM NUT PLATE HOLE AT FRAME 66. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE AND COMPLETED REAPIR IAW SRM 51-42-11, SRM 53-41-14, SRM 51-75-12 AND EA A9-53R-31454.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 26,257 hrs · 12,477 cycles

DURING CLIMB THROUGH FL25000, PILOT REPORTED THAT THE NR 1 ENGINE WENT TO IDLE AND STARTED TO RUN ROUGH. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE AND PERFORMED OPERATIONAL TEST IAW MP71042-01 AND MP71042-02 AND PERFORMED ENGINE IDLE LEAK CHECK IAW AMM 71-00-00-710-006.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,808 hrs · 12,247 cycles

EMERGENCY LIGHT AT ROW 1, LT SEAT, REFERENCE AMM 33-51-18 PB401 AND PERFORMED OPERATIONAL TEST.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 22,804 hrs · 10,925 cycles

DURING C5 C CHECK INSPECTION NOTED SEAT ROWS 9 ABC AND 10 ABC EMERGENCY PATH LIGHTS ARE INOPERATIVE. MAINTENANCE TROUBLESHOT EMERGENCY LIGHTS AND FOUND CONNECTOR DISCONNECTED ON SIDEWALL. MAINTENANCE RE-CONNECTED CONNECTOR AND OPERATIONAL CHECKED GOOD. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,073 hrs · 10,832 cycles

DURING PRE FLIGHT INSPECTION, THE FLIGHT CREW REPORTED SEAT ROWS 9 AND 22 HAD ONE SEGMENT OF LIGHTS FOUND BURNED OUT DURING PRE FLIGHT TEST. MAINTENANCE REMOVED AND REPLACED ONE BULB FROM ROW 22 IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 31-51-00 AND DEFERRED EMERGENCY LIGHT IN ACCORDANCE WITH THE REQUIREMNTS OF MEL 33-50-03A.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,073 hrs · 10,832 cycles

DURING PRE FLIGHT INSPECTION, THE FLIGHT CREW REPORTED SEAT ROWS 9 AND 22 HAD ONE SEGMENT OF LIGHTS FOUND BURNED OUT DURING PRE FLIGHT TEST. MAINTENANCE REMOVED AND REPLACED ONE BULB FROM ROW 22 IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 31-51-00 AND DEFERRED EMERGENCY LIGHT IN ACCORDANCE WITH THE REQUIREMNTS OF MEL 33-50-03A.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,073 hrs · 10,832 cycles

DURING PRE FLIGHT INSPECTION THE FLIGHT CREW REPORTED SEAT ROWS 9 AND 22 HAD ONE SEGMENT OF LIGHTS FOUND BURNED OUT DURING PRE FLIGHT TEST. MAINTENANCE REMOVED AND REPLACED ONE BULB FROM ROW 22 IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 31-51-00 AND DEFERRED EMERGENCY LIGHT IN ACCORDANCE WITH THE REQUIREMENTS OF MEL 33-50-03A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,090 hrs · 10,386 cycles

DURING AN EARLIER FLIGHT, ROW 11, SEATS ABC EMERGENCY LIGHT ASSEMBLY WAS TESTED AND FOUND INOPERATIVE. IT WAS PLACED ON MEL 1031603 ON 01/15/2008. DURING RON MAINTENANCE, THE MEL WAS CLEARED BY THE REPLACEMENT OF THE EMERGENCY LIGHT ASSEMBLY AT ROW 11, SEATS ABC. THE REPLACEMENT WAS ACCOMPLISHED IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-51-19 PB 401. AFTER THE REPLACEMENT, THE ASSEMBLY WAS TESTED AND FOUND OKAY. MEL 1031603 WAS CLOSED ON 01/16/2008. REFERENCE LOG BOOK PAGE 32572, ITEM 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,453 hrs · 8,155 cycles

DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON BOTTOM OF AFT FUSELAGE LT FLOOR SUPPORT AT Y1292 BETWEEN FRAMES FR69 AND FR70. FOUND FRAME SUPPORT TO BE OUT OF LIMITS IAW SRM 53-41-11. INSTALLED NEW FLOOR SUPPORT IAW SRM'S 51-44-11, 53-41-11 AND 51-42-12.

Part: PLATE — CORRODED (L1 DOOR GIRT BAR) · corrosion level 2 · airframe 17,453 hrs · 8,155 cycles

DURING C-4 CHECK, INSPECTION REPORTED PLATE UNDER AFT L1 GIRT BAR FITTING CORRODED. REPLACED AFT L1 GIRT BAR BLANKING PLATE IAW AMM 52-11-31-000-005. INSTALLED AFT L1 GIRT BAR FITTING IAW AMM 52-11-31-400-003.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 17,453 hrs · 8,155 cycles

DURING C-4 CHECK, INSPECTION REPORTED FLOOR PANEL 261FF CORRODED IN LOWER AREA. REMOVED AND REPLACED PANEL 261FF PER WORK CARD CP753-36.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,543 hrs · 8,155 cycles

DURING C-4 CHECK, INSPECTION REPORTED FWD LAV AREA DUMMY RAIL Y503.2, BETWEEN FRAMES C12 AND C16, CORRODED ALONG ENTIRE LENGTH OF BEAM. CORRODED AREAS FOUND TO BE OUT OF LIMITS PER SRM 53-11-14. REPLACED DUMMY RAIL PER SRM'S 51-44-11 AND 51-42-11.

Part: PLATE — CORRODED (CABIN) · corrosion level 2 · airframe 17,453 hrs · 8,155 cycles

DURING C-4 CHECK, INSPECTION REPORTED PLATE UNDER FWD L2 GIRT BAR FITTING CORRODED. REPLACED PLATE PER MM 53-12-12-400-001.

Part: SPAR — DAMAGED (LT WING) · airframe 17,453 hrs · 8,155 cycles

DURING C-4 CHECK, INSPECTION REPORTED LT WING, OTBD FLAP L/E BETWEEN TRACKS 3 AND 4, INSIDE FRONT SPAR (BACKSIDE), ATTACHMENT HOLES HAD SPLINTERING, COMPOSITE MATERIAL SPLITTING FROM AROUND RIVETS. REMOVED DAMAGED SECTION FOR FURTHER EVALUATION AS REQUESTED BY ENGINEERING IAW SRM 51-42-11. RE-INSTALLED LT OTBD FLAP L/E SECTION IAW SRM 51-42-11 AND EA A9-57R-11610 AND ISSUED RW NR 000899 FOR 1000 FLT CYCLES.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,543 hrs · 8,155 cycles

DURING C-4 CHECK, INSPECTION REPORTED CORROSION THROUGH FLOORBEAM Y254L AT FRAME C16 IN FWD CABIN. CORRODED AREAS FOUND TO BE OUT OF LIMITS PER SRM 53-11-14. CUT OUT CORRODED AREA PER SRM 53-11-14, FIG 201. FABRICATED AND INSTALLED REPAIR ANGLES PER SRM'S 53-11-14 AND 51-23-11.

Part: FASTENER — CORRODED (FWD CARGO BAY) · corrosion level 2 · airframe 17,543 hrs · 8,155 cycles

DURING C-4 CHECK, INSPECTION REPORTED CORRODED HARDWARE ON ALL 3 CARGO NET TIE DOWNS INBOARD OF DOOR THRESHOLD IN FWD CARGO COMPARTMENT. REPLACED CORRODED HARDWARE AS REQUIRED ON TIE DOWNS.

Part: ATTACH FITTING — CORRODED (GIRT BAR) · corrosion level 2 · airframe 17,453 hrs · 8,155 cycles

DURING C-4 CHECK, INSPECTION REPORTED (2) CORRODED NUT PLATE HOLES AT INBD AFT CORNER OF L2 THRESHOLD FWD GIRT BAR FITTING ATTACH POINT. FOUND L2 DOOR THRESHOLD FITTING TO BE OUT OF LIMITS PER SRM 53-41-14. REMOVED AND REPLACED THRESHOLD PER SRM'S 51-42-11 AND 51-42-12.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,453 hrs · 8,155 cycles

DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR PANEL 262FF BY R2 DOOR. REPLACED FLOOR PANEL 262FF PER WORK CARD CP753-36.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 17,453 hrs · 8,155 cycles

DURING C-4 CHECK, INSPECTION REPORTED FLOOR PANEL 222FF CORRODED ON BOTTOM CORNER. REMOVED AND REPLACED FLOOR PANEL 222FF PER WORK CARD CP753-12.

Part: STAND OFF — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,543 hrs · 8,155 cycles

DURING C-4 CHECK, INSPECTION REPORTED DAMAGED STANDOFF ON AFT BULKHEAD RT FLOORBEAM, Y1732 AT CROSSBEAM FR66. FOUND DAMAGE TO BE OUT OF LIMITS PER SRM 53-00-14, FIG 102. REMOVED CORROSION FROM SILL BEAM AT FR66 PER SRM 53-41-14 FIG 201. FABRICATED AND INSTALLED REPAIR ANGLES PER SRM'S 53-41-14, FIG 201; 51-42-11; 53-41-14, PAGES 207/208; 53-41-14, PAGES 215/216/217; 53-41-14, PAGES 103/104, FIG 101; 53-41-14, FIG 201, SHEET 4.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,543 hrs · 8,155 cycles

DURING C-4 CHECK, INSPECTION REPORTED HEAVY CORROSION ON AFT FUSELAGE RT FLOORBEAM SHEAR PLATE WEB AT Y1292 (BETWEEN CROSSBEAMS FR69 AND FR70). FOUND CORROSION ON SHEAR PLATE AND ANGLED WEB TO BE OUT OF LIMITS PER SRM 51-11-15. REMOVED DAMAGED SHEAR PLATE AND ANGLED WEB PER SRM 51-42-11. INSTALLED NEW SHEAR PLATE AND ANGLED WEB PER SRM 51-42-11 AND 51-44-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,453 hrs · 8,155 cycles

DURING C-4 CHECK, INSPECTION REPORTED AFT FUSELAGE LT FLOORBEAM FASTENER HOLES CORRODED AT Y1292, BETWEEN FS 69 AND FS 70. REMOVED CORROSION ON FLOORBEAM AND FOUND FLOORBEAM TO BE OUT OF LIMITS PER SRM 53-00-14, FIG 102. REMOVED AND REPLACED FLOORBEAM BETWEEN FS 69 AND FS 70 AT Y1292 PER SRM'S 51-42-12 AND 51-41-44.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,543 hrs · 8,155 cycles

DURING C-4 CHECK, INSPECTION REPORTED HEAVY CORROSION ON AFT FUSELAGE LT FLOORBEAM SHEAR PLATE WEB AT Y1292 (BETWEEN FRAMES FR69 AND FR70). FOUND CORROSION ON SHEAR PLATE WEB TO BE BEYOND REPAIR LIMITS PER SRM 53-41-14. REMOVED DAMAGED SHEAR PLATE AND SUPPORT FRAME PER SRM 51-42-12. INSTALLED NEW SHEAR PLATE AND SUPPORT ANGLE PER SRM 51-42-11, 51-44-11 AND DWG 18D53474180.

Part: FLOORBEAM — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 17,453 hrs · 8,155 cycles

DURING C-4 CHECK, INSPECTION REPORTED CORRODED FLOORBEAM FASTENER HOLE AT Y1292, CROSSBEAM FS 68, RT SIDE AFT FUSELAGE. FOUND FLOORBEAM TO BE OUT OF LIMITS PER SRM 53-00-14. REMOVED AND REPLACED FLOORBEAM AT Y1292 FROM FS 66 TO FS 68 PER SRM'S 51-42-11, 51-44-11, 51-42-12 AND DRAWING D53472780.

Part: BOLT — CORRODED (CABIN) · corrosion level 2 · airframe 17,453 hrs · 8,155 cycles

DURING C-4 CHECK, INSPECTION REPORTED FLOOR MOUNTING BOLTS ON AFT LT FLIGHT ATTENDANT SEAT CORRODED. REPLACED FLOOR MOUNTING BOLTS PER SICMA CMM 25-11-97 AND CMM 25-11.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 13,203 hrs · 6,032 cycles

ABORTED TAKEOFF. FLIGHT CREW REPORTED ECAM FAULTS ON TAKEOFF ROLL. AIR PACK 1 AND 2 FAULT, VENT AVIONICS SYS FAULT, VENT BLOWER FAULT, AND VENT EXTRACT FAULT. HOT BRAKES - HIGHEST TEMP WAS 470 DEG. PERFORMED BITE TEST ON VENT SYSTEM (AEVC) AFTER RESET AEVC C/B. SYSTEM BITE CHECK OKAY. NO FAULTS PRESENT. REF AMM 21-26-00-710-001. COMPLIED WITH F9 JOB CARD MP05510, INSPECTION AFTER BRAKE OVERHEAT, AND NO DEFECTS FOUND.