N703TW

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 97,136 hrs · 25,094 cycles

SHIP 6802 RH EMERGENCY LIGHT UNDER BAG BIN ROW# 43 MISSING COVER. CORRECTIVE ACTION: INSTALLED EMERGENCY LIGHT LENS ON ROW 43 RH PER B757 AMM 33-51. OPS CHECKS GOOD. (4368533)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,611 hrs · 24,966 cycles

SHIP 6802 L-3 DOOR HANDLE HAS BEEN OPENED AND DOOR SLIGHTLY BEEN RAISED WHILE IN THE ARM POSITION. CORRECTIVE ACTION REMOVED AND REINSTALLED SLIDE IAW B757 AMDS 2566-9002-32. (4424614)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,311 hrs · 24,455 cycles

SHIP 6802 -FIRE- NBR 3 BRAKE LEAKED HYDRAULIC FLUID AFTER LANDING. FLUID BRIEFLY IGNITED AND SELF-EXTINGUISHED. CORRECTIVE ACTION: FOUND (4) HYDRAULIC LINES BURNED NEAR #3 BRAKE, REMOVED AND REPLACED HYD LINES, #3 TIRE BRAKE ASSY COUPLING AND BRAKE ASSY.

Part: NONE — NONE · airframe 94,107 hrs · 24,407 cycles

SHIP 6802 DURING SVC CHECK FOUND R4 DOOR ASSIST BOTTLE LOW IN PRESSURE. CORRECTIVE ACTION: RPLCD BOTTLE PER B757 AMM52-11-30. (9870597)

Part: LIGHT — MISSING (SEAT 31D) · airframe 93,727 hrs · 24,311 cycles

SEAT 31D SEAT MOUNTED EPL ASSY MISSING DURING SVC CHECK. INSTALLED 31D SEAT MOUNTED EPL ASSY PER B757 AMM 33-51. OPS CHECK NML.

Part: SKIN — DENTED (BS 500-520) · airframe 93,151 hrs · 24,175 cycles

INITIAL INSPECTION: SEVERAL DENTS ON EXTERNAL FUSELAGE SKIN BTW STA 500-520 AND STGR 14-16LT. SKIN REPAIRED PER ER/A 603500- 14 REV. ORIGINAL SECTION I AND PRI 603500 REV. 4.

Part: NONE — NONE (NONE) · airframe 93,151 hrs · 24,175 cycles

SHIP 6802 EXISTING REPAIR WAS FOUND IN THE INSPECTION AREA ON STA 1360 LH AT AFT COMPARTMENT CARGO COMPARTMENT. FRAME ON STA 1360 LH AT AFT COMPARTMENT CARGO WAS REPAIRED PER ER/A 603580-14AD REV. ORIGINAL. (2497902)

Part: SNUBBER — OUT OF LIMITS (L2 DOOR) · airframe 93,151 hrs · 24,175 cycles

OUT OF LIMITS ROTARY SNUBBER PIN EXTENSION AT 2L DOOR OF CABIN PAX IN EF AMDS. CORRECTIVE ACTION: SUMMARY OF NRC 00061: ROTARY SNUBBER AT 2L DOOR OF CABIN PAX WAS REPLACED SERVICEABLE SNUBBER PER B757-200 AMM 52-11-10.

Part: NONE — NONE (NONE) · airframe 93,343 hrs · 24,220 cycles

FUSELAGE FRAME BS 1360, S25L TO S27L. EXISTING REPAIR. CORRECTIVE ACTION: REF ERA 603580-14AD. (2497638)

Part: SNUBBER — OUT OF LIMITS (R1 DOOR) · airframe 93,148 hrs · 24,174 cycles

OUT OF LIMITS ROTARY SNUBBER PIN EXTENSION AT R1 DOOR OF CABIN PAX (CPAX). ROTARY SNUBBER AT 1R DOOR OF PASSENGER CABIN WAS REPLACED BY SERVICEABLE ROTARY SNUBBER.

Part: SNUBBER — OUT OF LIMITS (R2 DOOR) · airframe 93,148 hrs · 24,174 cycles

OUT OF LIMITS ROTARY SNUBBER PIN EXTENSION AT 2R DOOR OF CABIN PAX IN EF AMDS. ROTARY SNUBBER AT 2R DOOR WAS REPLACED BY SERVICEABLE SNUBBER PER B757-200 AMM 52-11-10. (2488092)

Part: NONE — NONE · airframe 92,996 hrs · 24,138 cycles

SHIP 6802 4R DOOR FAILED TO ARM LIGHT COME ON. CORRECTIVE ACTION: REMOVED DEBRIS FROM GRIT BAR AS REQUIRED. AT 4R DOOR. OPS CHECK GOOD PER B757 AMM 25-66. (9239650)

Part: NONE — NONE · airframe 92,870 hrs · 24,108 cycles

SHIP 6802 L CENT ENT DOOR MSG ILLUMINATED DURING CLIMB OUT AROUND FL260. FA WENT TO CHECK DOOR, SEATED HANDLE BETTER AND COINCIDENTALLY LIGHT WENT OUT. PRESSURIZATION WAS NORMAL. CORRECTIVE ACTION: ADJUSTED SENSOR S10095 PER B757 AMM 52-71. (9239608

Part: NONE — NONE · airframe 92,855 hrs · 24,105 cycles

SHIP 6802 L CEN ENT DOOR MSG ILLUMINATED AT 12,000 FT. ON AND OFF INTERMITTENTLY THROUGH TAXI IN. CORRECTIVE ACTION: FOUND DEBRIS ON 2L DOOR GIRT BAR SENSORS. CLEANED AS REQ. CYCLED DOOR CLSD THEN OPEN AGAIN. IND OK IAW B757 AMM 52-71. (9239606)

Part: SIGN — DETACHED · airframe 91,921 hrs · 23,882 cycles

SHIP 6802 L2 EXIT SIGN FELL OFF. CORRECTIVE ACTION: R/R L2 EMERGENCY EXIT SIGN. (8835962)

Part: NONE — NONE · airframe 91,515 hrs · 23,789 cycles

SHIP 6802 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:602. CORRECTIVE ACTION: SECURED LOOSE HARDWARE. (2205625)

Part: NONE — NONE · airframe 91,141 hrs · 23,701 cycles

SHIP 6802 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 588925-14 REV A. CORRECTIVE ACTION: REF ERA 588925-14 REV A. (2141636)

Part: NONE — NONE · airframe 90,901 hrs · 23,650 cycles

SHIP 6802 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 588829-14 REV A. CORRECTIVE ACTION: REF ERA 588829-14 REV A. (2114985)

Part: NONE — NONE · airframe 90,123 hrs · 23,468 cycles

SHIP 6802 FA STATED THE R1 DOOR ARM/DISARM LEVEL (RED TO GREEN) WAS VERY DIFFICULT TO MOVE. CORRECTIVE ACTION: READJUSTED R1 DOOR RAFT MOUNTING TENSION SCREW. OPS CHK NML. REF B757 AMM 25-66. (7001412)

Part: OVEN — ODOR (AFT GALLEY) · airframe 89,449 hrs · 23,322 cycles

SHIP 6802 AFT GALLEY(LOC405) OVEN #5 BURNING/PLASTIC/ELECTRICAL SMELL FROM SURROUNDING VENTS ONLY WHEN OVEN IS IN USE. CORRECTIVE ACTION: REMOVED AND REPLACED AFT GALLEY OVEN #5 IAW B757 AMM 25-31, OPS CKS NML. (7987770)

Part: DOOR — MALFUNCTIONED (DOOR ARMING) · airframe 88,153 hrs · 23,047 cycles

SHIP 6802 F/A REPORTS UNABLE TO DISARM 2R DOOR. CORRECTIVE ACTION: DISARMED DOOR NO TROUBLE FOUND CONT IN SERVICE. (7480147)

Part: FITTING — DAMAGED (RT ENGINE) · corrosion level 2 · airframe 86,954 hrs · 22,779 cycles

DURING INITIAL INSPECTION, MAINTENANCE FOUND DAMAGES ON OPEN HOLES AT RT ENGINE DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW: HOLE NR 1 CORROSION ON FITTING AT 12; HOLE NR 2 CORROSION ON SKIN AND FITTING BETWEEN 12 AND 2 O`CLOCK POSITION; HOLE NR 4 TOOL MARKS AND CORROSION ON FITTING AT 4 O`CLOCK POSITION; HOLE NR 5 CORROSION ON SKIN AT 3 O`CLOCK POSITION AND ON FITTING AT 12 O`CLOCK POSITION; HOLE NR 6 CORROSION ON SKIN AND FITTING BETWEEN 12 AND 2 O`CLOCK POSITION; HOLE NR 7 CORROSION ON SKIN AND FITTING BETWEEN 2 AND 3 O`CLOCK POSITION; HOLE NR 8 CORRIOSION ON SKIN AND FITTING AT 3 O`CLOCK POSITION; HOLE NR 9 CORROSION ON FITTING AT 12 O`CLOCK POSITION; HOLE NR 10 CORROSION ON SKIN AND FITTING AT 10 O`CLOCK POSITION. REPAIRED PER ERA 588925-00.

Part: BUSHING — CORRODED (LT NACELLE) · corrosion level 2 · airframe 86,954 hrs · 22,779 cycles

DURING INSPECTION MAINTENENANCE FOUND CORROSION LEVEL 2 BUSHINGS ON LT PYLON ATTACH FITTING.

Part: BUSHING — CORRODED (RT NACELLE) · corrosion level 2 · airframe 86,954 hrs · 22,779 cycles

DURING UPPER LINK REMOTION MAINTENANCE FOUND DISPLACED AND CORRODED BUSHING ON RT PYLON FITTING. FITTING REPLACED PER SRM.

Part: DOOR FRAME — CRACKED (R2) · airframe 86,954 hrs · 22,779 cycles

DURING INSPECTION MAINTENANCE FOUND A CRACK ON INNER CHORD FRAME AT UPPER HINGE CUTOUT OF PASSENGER ENTRY DOOR R2. CRACK REPAIRED, PER ERA 588830-14.

Part: DRAG FITTING — CORRODED (LT NACELLE) · corrosion level 2 · airframe 86,954 hrs · 22,779 cycles

DURING INSPECTION MAINTENANCE FOUND LEVEL 2 CORROSION ON OPEN HOLES AT LT ENGINE DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW: HOLE NR 1 CORROSION ON SKIN AND FITTING BETWEEN 8 AND 9 O'CLOCK POSITION; HOLE NR 2 CORROSION ON SKIN AND FITTING AT 12 O'CLOCK POSITION; HOLE NR 3 CORROSION AND TOOL MARKS ON SKIN AND FITTING AT 6 AND 8 O'CLOCK POSITION; HOLE NR 4 CORROSION ON SKIN AND FITTING AT 6 O`CLOCK POSITION; HOLE NR 5 CORROSION AND TOOL MARKS ON SKIN AND FITTING BETWEEN 6 AND 7 O'CLOCK POSITION; HOLE NR 6 CORROSION ON SKIN AND FITTING AT 6 O'CLOCK POSITION; HOLE NR 7 CORROSION ON SKIN AND FITTING AT 10 O'CLOCK POSITION; HOLE NR 8 CORROSION AND TOOL MARKS BETWEEN 10 AND 12 O'CLOCK POSITION; HOLE NR 9 CORROSION ON SKIN AND FITTING AT 9 O'CLOCK POSITION; HOLE NR 10 CORROSION AND TOOL MARKS ON SKIN AT 6 O'CLOCK POSITION AND FITTING AT 4 O'CLOCK POSITION. REPAIRED PER ERA 588829-14.

Part: SHIM — DEGRADED (DOOR ROLLER) · airframe 86,954 hrs · 22,779 cycles

DURING INITIAL INSPECTION MAINTENANCE FOUND DEGRADED COMPOSITED MATERIAL SHIM OF ROLLER ON L3 EMERGENCY EXIT. CORRECTIVE ACTION: SHIMS ON ROLLER WERE REPLACED.

Part: SKIN — DENTED (FUSELAGE) · airframe 86,954 hrs · 22,779 cycles

DURING INITIAL INSPECTION FOUND DENT ON EXTERNAL FUSELAGE BETWEEN STA 377 TO STA 395 AND STG 13R TO STR 14R . REPAIRED PER SRM.

Part: CONTROL PANEL — MALFUNCTIONED (AUTOPILOT SYS) · airframe 86,808 hrs · 22,748 cycles

'SHIP 6802 -ETOPS, DIV- MODE CONTROL PANEL WOULD NOT INCREASE BEYOND ALT 19,000. AUTOPILOT AND FLIGHT DIRECTOR WOULD NOT RESPOND CORRECTLY. DIVERTED TO ATL. CORRECTIVE ACTION: R/R MCP PER B757 AMM 22-11. ALL TESTS PASSED.

Part: OIL SYSTEM — LOW PRESSURE (RT ENGINE) · airframe 85,818 hrs · 22,537 cycles

SHIP 6802 - IFSD/DIV - FLIGHT CREW DIVERTED TO SYR DUE TO LOST OIL PRESSURE ON RIGHT ENGINE. QRH WAS FOLLOWED AND ENGINE WAS SHUT DOWN. CORRECTIVE ACTION: VISUALLY INSPECTED INLET AND EXHAUST - NTF (N1 WILL TURN BY HAND). INSPECTED RIGHT ENGINE CHIP DETECTORS - NTF. MAINTENANCE UNABLE TO TURN N2 THROUGH GEARBOX TURN PAD, ENGINE CHANGE REQUIRED. RIGHT ENGINE WAS REPLACED AND AIRCRAFT RTS. ENGINE CHANGED ON LOGPAGE 1373023.

Part: GIRT BAR — OUT OF ADJUST (L2 DOOR) · airframe 85,368 hrs · 22,448 cycles

DOOR 2L HARD TO ARM. ADJUSTED 2L DOOR GIRT BAR MECHANISM IAW AMM 52-11-25. COMPLIED WITH RII REQUIREMENTS IAW AMM 52-11-25 FOR THE PROPER ADJUSTMENT AND RIG OF THE 2L DOOR GIRT BAR MECHANISM. VERIFIED SAFETY PIN REMOVED AND STOWED.

Part: DOOR — OBSTRUCTED (L2) · airframe 85,224 hrs · 22,421 cycles

(AIRCRAFT 6802, L/P 6606738) DOOR 2L UNABLE TO ARM DOOR. CORRECTIVE ACTION: CLEARED DEBRIS OPS NML AT DOOR 2L.

Part: GIRT BAR — OBSTRUCTED (L2 DOOR) · airframe 85,195 hrs · 22,416 cycles

L2 DOOR WILL NOT ARM. FOUND DEBRIS BY GRIT BAR STRIKER, REMOVED DEBRIS, OPS CHECKED NORMAL IAW 52-12.

Part: HEATER — ODOR · airframe 84,737 hrs · 22,330 cycles

SMELL OF BURNING PLASTIC COMING OUT OF VENT BY 1L RIGHT SIDE. INSPECTED FWD GALLEY FOR ANY SIGNS OF DAMAGE OF COFFEE MAAKERS, OVENS, AND LIGHTS. NONE FOUND INSPECTED E/E COMPT. FOR ANY SIGNS OF DAMAGE OR ELECTRICAL SMELL. NONE FOUND. FOUND C/B FOR DOOR 1 HEAT POPPED. REMOVED AND REPLACED 1L DOOR HEATER PER B757 AMM 21-45. OPS CHECK GOOD, BURNING PLASTIC ODOR NO LONGER PRESENT. NO GO ODI CHECKLIST C/W. C/B FOR DOOR 1 HEAT NO LONGER OPENS.

Part: WIRE HARNESS — FAULTY (CABIN) · airframe 84,141 hrs · 22,217 cycles

(AIRCRAFT 6802, L/P 6050770) PED OUTLET AT SEAT 1B FAILED WITH A STRONG ELECTRICAL FUME ODOR. GREEN LED POWER LIGHT WAS BLINKING RAPIDLY BEFORE IT FAILED. TURNED OFF PED POWER + FUMES DISSPATED. FAULT CONFIRMED, HARNESSES REQUIRED TO BE R/R ARE RD-FM6004-B0909 AND RD-FM7583-L1922 IAW AIPC 23-36-07. UNABLE TO R/R AT / JFK DUE TO PART NIS AT JFK. ITEM REMAINS ON DEFERRAL.

Part: UNKNOWN — MALFUNCTIONED (R3 DOOR) · airframe 82,727 hrs · 21,958 cycles

SHIP 6802 AT DEPARTURE TIME 3R DOOR WOULD NOT ARM. CORRECTIVE ACTION: VERIFIED DOOR WAS DISARMED. OPENED AND CLOSE 3R DOOR PROPERLY AND ABLE TO ARM/DISARM DOOR NORMAL NOW. (5640944)

Part: OXYGEN MASK — UNWANTED DEPLOY (LAVATORY) · airframe 82,413 hrs · 21,897 cycles

SHIP 6802 FWD LAV O2 MASK DROPPEDON TAKEOFF. REPACKED AND SECURED O2 MASK. (0942425)

Part: WINDSCREEN — CRACKED (COCKPIT) · airframe 82,246 hrs · 21,863 cycles

CAPTAINS FWD WINDSCREEN GLASS CRACKED WITH ARCING DURING TAXI OUT, OCCURRED APPROXIMATELY 30 MINUTES AFTER DEICING. R&R CAPT FIXED WINDOW (L1), INITIAL TORQUE AND SEALANT COMPLETE REF AMM 56-11, COMPLETED SECOND TORQUE PER AMM 56-11.

Part: GIRT BAR — ICED (R4 DOOR) · airframe 82,153 hrs · 21,844 cycles

SHIP 6802 4R DOOR WILL NOT ARM. CORRECTIVE ACTION: FOUND ICE ON LOWER RT GIRT BAR REMOVED ICE BUILD UP. 4R DOOR OPS CHK NML. ARM SYS CHKS NML PER AMM 52-11. (3742410)

Part: SKIN — WORN (LT WING TE FLAP) · airframe 81,494 hrs · 21,716 cycles

(AIRCRAFT 6802, L/P 0837742) INITIAL INSPECTION. WORN UPPER SKIN ON INBD MAIN FLAP MF STA 295 AT LH WING. SUMMARY OF NRC 00258: PERMANET REPAIR ON UPPER SKIN ON INBD MAIN FLAP WAS ACCOMPLISHED PER ERA 573186-14 REV. ORG SECTION I.

Part: SKIN — CORRODED (BS 1020-1040) · airframe 81,491 hrs · 21,715 cycles

SHIP 6802 INITIAL INSPECTION. CORROSION ON WING CENTER SECTION UPPER SKIN BTW STA 1020 TO 1040, RBL 65 ALSO LBL 33 AT PAX CABIN. CORRECTIVE ACTION: SUMMARY OF NRC 00224. ATTENDED WITH ETI-57-18-035 REV. ORIGINAL AND ER/A:572819-14 REV. ORIGINAL. (0835624)

Part: DOOR — NOT REPORTED (AFT CARGO) · airframe 81,488 hrs · 21,714 cycles

SHIP 6802 TRANSFER FROM LOG 2875462;730D;ERA554307;SEC II; 00965;AFT CARGO DOOR / PRESSURE BOX ASSY /HANDLE INTERIOR HOUSING. CORRECTIVE ACTION: AFT CARGO DOOR WAS REMOVED PER B757-200 AMM 52-34 AND AFT CARGO DOOR WAS INSTALLED PER B-757-200 AMM 52-34, CARGO DOOR HINGE LINKAGE WAS REMOVED AND INSTALLED PER B-757-200 AMM 52-34 AND AFT CARGO DOOR WAS LUBRICATED AND VERIFIED PER B-757-200 AMM 12-21. (0831920)

Part: SKIN — CRACKED (PAX DOOR) · airframe 81,488 hrs · 21,714 cycles

(AIRCRAFT 6802, L/P 0829085) INITIAL INSPECTION. CRACKED INNER SKIN ON AFT PASSENGER ENTRY DOOR (L4) PROTECTION STA 1661 AT PAX CABIN. (CPAX). SUMMARY OF NRC 00263. CRACK ON INNER SKIN ON AFT PASSENGER ENTRY DOOR (L4) WAS REPAIRED PER ETI-57-18-034 REV. 3 AND ER/A 572880-14 REV. ORIGINAL.

Part: SKIN — CRACKED (PAX DOOR) · airframe 81,488 hrs · 21,714 cycles

(AIRCRAFT 6802, L/P 0829075) INITIAL INSPECTION. CRACKED INNER SKIN ON AFT PASSENGER ENTRY DOOR (L4) PROTECTION STA 1661 AT PAX CABIN. (CPAX). SUMMARY OF NRC 00263. CRACK ON INNER SKIN ON AFT PASSENGER ENTRY DOOR (L4) WAS REPAIRED PER ETI-57-18-034 REV. 3 AND ER/A 572880-14 REV. ORIGINAL.

Part: STRUCTURE — CORRODED (BS 1510) · airframe 81,488 hrs · 21,714 cycles

(AIRCRAFT 6802, L/P 0818227) INITIAL INSPECTION: CORROSION ON PREVIOUS REPAIRS ON STRINGERS RBL/LBL 2.90, 7.55 AND 10.45, STA 1510 AT AFT CARGO COMPARTMENT FLOOR STRUCTURE. (CCT). SUMMARY : OF NRC 00126 PREVIOUS REPAIRS DOUBLERS ON STRINGERS RBL 7.55 AND 10.45, STA 1510 AT AFT CARGO COMPARTMENT FLOOR STRUCTURE, ALSO LBL 2.90 , 7.55 WERE REPLACED PER B757-200 SRM 53-00-53 REPAIR 1. FIGURE 201 BUT PREVIOUS DOUBLER REPAIR STA 1510 RBL 2.90 WAS REPLACED PER ER/A 332525-14MA REV. C. REPAIR DOUBLER ON LBL 10.45, STA 1510 WAS CLEANED PER PS 900-1-2-1 N.01 AND RE-INSPECTED PER B757-200 SRM 51-10-02 PAR. 15 A 5A AND NOT CORROSION WAS FOUND.

Part: SKIN — DENTED (BS 1400-1460) · airframe 81,488 hrs · 21,714 cycles

(AIRCRAFT 6802, L/P 0814923) AWR HIDDEN PREVIOUS BLEND OUT: SEVERAL PREVIOUS BLEND OUT WERE FOUND DURING EVALUATION OF DENTS FROM STA 1400 TO 1460 BTW S-26L AND S-29L AT EXTERNAL FUSELAGE SKIN. IN REFERENCE NRC 00424.(FUS). SUMMARY: OF NRC 00427 AWR HIDDEN PREVIOUS BLEND OUT: SEVERAL PREVIOUS BLEND OUT WERE FOUND DURING EVALUATION OF DENTS FROM STA 1400 TO 1460 BTW S-26L AND S-29L AT EXTERNAL FUSELAGE SKIN. IN REFERENCE NRC 00424.(FUS) (UT) WAS ACCOMPPLISHED PER B-757 NDT MANUAL PART. 4. 51-00-02. WITHIN LIMITS PER B-757-200 SRM 53-00-01. FIG.101 SHT. 3 NOTE "D" EQUIPMENT: PANAMETRICS OLIMPUS 38 DL.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 80,394 hrs · 21,517 cycles

1R DOOR WILL NOT ARM. CLEANED DEBRIS FROM GIRT BAR. DOOR ARMED AND DISARMED NORMAL.

Part: COVER — MISSING (R4 DOOR HANDLE) · airframe 79,209 hrs · 21,298 cycles

R4 DOOR HANDLE TRIM COVER PLATE MISSING. INSTALLED HANDLE COVER PLATE IAW AMM 52-11.

Part: COVER — DAMAGED (R4 DOOR) · airframe 78,825 hrs · 21,222 cycles

R4 DOOR HANDLE TRIM COVER PLATE DAMAGED. REPLACED THE DOOR HANDLE INSERT.

Part: UNKNOWN — ODOR (CABIN) · airframe 78,043 hrs · 21,074 cycles

FLIGHT ATTENDANTS & PAX REPORTED AN ELECTRICAL ODOR AT ROWS 25 - 26, BOTH SIDES OF AIRCRAFT. TURNED OFF MASTER IFE POWER, WALKED TO THE BACK OF THE ACFT. ODOR DISSIPATED. LEFT IFES OFF REMAINDER OF THE FLIGHT. BOARDED ACFT AND IFE SYSTEM WAS OFF. INSPECTION OF ALL RELATED CONNECTORS SHOW NO PHYSICAL DAMAGE OR DISCONNECTION. ENERGIZED IFE SYSTEM AND NO BURNING ODOR WAS NOTED. NO FAULTS ON QUICK TEST OR CONFIGURATION. AS PRECAUTION, R & R THE SPM AT 25 BE - 26 BE IAW AMM 00380 23-81-08. OPS CHECKED NORMAL.

Part: DOOR — OBSTRUCTED (CABIN) · airframe 77,484 hrs · 20,964 cycles

1L DOOR WILL NOT DISARM. REMOVED DEBRIS. LUBRICATED GIRT BAR AND ARM/DISARM TEST PERFORMED IAW AMM 52-11. TEST OK.

Part: COVER — UNKNOWN (EXIT SIGN) · airframe 75,121 hrs · 20,521 cycles

DOOR 3R EXIT SIGN LOOSE/MISSING COVER. REATTACHED OPS NML AMM REF 33-51.

Part: UNKNOWN — SMOKE (COCKPIT & CABIN) · airframe 74,447 hrs · 20,392 cycles

ATB, DUE TO AFTER TAKEOFF SMOKE REPORTED IN FLIGHT DECK AND CABIN - RETURNING TO LAX. PERFORMED FIM 71-05-00-815-811-P00 STEPS 1 & 2 NO ODOR FROM EITHER ENGINE. COMPLETED FIM TASK STEP 5 NO EVIDENCE OF FUEL OR HYDRAULIC FLUID SMELL ALSO RAN BOTH PACKS TO FULL HOT CKS OK.

Part: HOUSING — DAMAGED (CABIN) · airframe 73,974 hrs · 20,284 cycles

EEPLS HOUSING DAMAGED AT 22 DEF. R&R HOUSING AT SEAT 22DEF.

Part: HOUSING — CRACKED (CARGO DR HANDLE) · airframe 81,488 hrs · 21,714 cycles

SHIP 6802 DURING MAINTENANCE CHECK, INSPECTION FOUND THE AFT CARGO DOOR PRESSURE BOX ASSY HANDLE INTERIOR HOUSING CRACKED. CORRECTIVE ACTION: REF ERA 554307-14 REV ORIG AND NRC 00429. (2875462)

Part: HOUSING — CRACKED (CARGO DOOR) · airframe 73,803 hrs · 20,249 cycles

AFT CARGO DOOR HANDLE INTERIOR HOUSING WEB CRACKED COMMON TOFASTENER. ACCOMPLISHED TIME-LIMITED REPAIR ON AFT CARGO DOOR HANDLE INTERIOR HOUSING (PRESSURE BOX ASSY.) IAW ER/A 554307-14 REV ORIG.

Part: SKIN — CORRODED (BS 1460-1480) · airframe 73,801 hrs · 20,248 cycles

DURING REMOVAL OF VHF3 ANTENNA, FOUND CORROSION ON FUSELAGE SKIN BS 1460 & 1480 AND STRINGERS 29 & 30R, UNDERNEATH OF VHF3 ANTENNA. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01 ALLOWABLE DAMAGE 1 DETAIL II FIG 101 AND DWG 146N3531. REPAIRED IAW SRM 51-40-02 PAG 2,3, AND 51-20-01 PAGE 6. NO CRACKS NOTED ON BLENDED AREA.

Part: SCREW — LOOSE (CYLINDER SPRING) · airframe 73,801 hrs · 20,248 cycles

R4 DOOR EMERGENCY POWER SPRING CYLINDER LOOSE. REMOVED CYLINDER CAP AND TIGHTENED TWO SCREWS. INSTALLED THE CYLINDER CAP IAW AMM 52-11-33.

Part: SKIN — CORRODED (BS 1720) · corrosion level 2 · airframe 72,710 hrs · 20,016 cycles

DURING WALK AROUND, FOUND CORROSION ON AFT BELLY BS 1720 BETWEEN STRINGERS 28 - 30. SURFACE CORROSION ONLY. REMOVED CORROSION. CUT AREA WITHIN LIMITS IAW SRM, REPLACED SEALANT AND PAINTED.

Part: BALLSCREW — CORRODED (NR 4) · corrosion level 2 · airframe 70,149 hrs · 19,526 cycles

NR 4 BALLSCREW IS CORRODED. REPLACED ON AMDS CARD.

Part: BALLSCREW — CORRODED (NR 6) · corrosion level 2 · airframe 70,149 hrs · 19,526 cycles

NR 6 BALLSCREW CORRODED. INSTALLED ON AMDS CARD.

Part: SKIN — DAMAGED (RT NACELLE) · airframe 69,769 hrs · 19,438 cycles

DURING WALKAROUND, FOUND RT ENGINE LOWER BOTTOM, BEHIND L/E OF COWLING EXPOSED FIBERGLASS. DAMAGE IS OUT OF LIMITS IAW SRM 54-11-01, P102. REMOVED RT INLET COWL, INSTALLED NOSE INLET COWL RT ENGINE IAW MM 71-11.

Part: FRAME — DAMAGED (BS 1480) · airframe 65,655 hrs · 18,607 cycles

FRAME ON AFT CARGO COMPARTMENT AT STA 1480 BETWEEN STR 25R-24R HAS A .2500" HOLE ON THE RADIUS. REMOVED FACTORY SPLICE FROM STA 1480 RT, CUTOUT 2 EA DAMAGE, INSP AND NO CRACKS. FABRICATED NEW REPAIR AND INSTALLED IAW SRM.

Part: SEAT TRACK — CORRODED (BS 1540-1640) · corrosion level 2 · airframe 65,655 hrs · 18,607 cycles

MAIN CABIN SEAT TRACK BS 1540 - 1640, LBL 45.5 CORRODED. FOUND TO BE OUT OF LIMITS, R & R SEAT TRACK IAW SRM.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 62,971 hrs · 18,029 cycles

FOUND EMERGENCY LIGHT AT GALLEY 404 DAMAGED AND WIRE BROKEN. SECURED WIRE IAW WDM 20.

Part: SKIN — DAMAGED (BS 360) · airframe 62,270 hrs · 17,908 cycles

DURING CHEM-MILL INSPECTION. FOUND FASTENER AT S4R, BS 360 DAMAGED WITH EVIDENCE OF LIGHTNING STRIKE. REMOVED DAMAGE AND INSPECTED, NO CRACKS FOUND , AND INSTALLED REPAIR IAW SRM 53-00-01.

Part: SKIN — DAMAGED (BS 1520-1540) · airframe 74,012 hrs · 20,300 cycles

FUSELAGE SKIN BS 1520 - 1540, BETWEEN STRINGERS 15 - 16R, AT G4 SIDE MOUNT ANTENNA DAMAGED.

Part: LIGHT — DAMAGED (CABIN) · airframe 61,433 hrs · 17,736 cycles

FOUND WALL MOUNTED EMERGENCY LIGHT FWD OF R1 DOOR DAMAGED. R & R WALL MOUNTED EMERGENCY LIGHT.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 61,154 hrs · 17,680 cycles

DURING SERVICE, FOUND R2 DOOR SLIDE PRESSURE IN RED. R & R R2 DOOR SLIDE.

Part: SKIN — DAMAGED (BS 557) · airframe 60,811 hrs · 17,612 cycles

FOUND LIGHTNING STRIKE DAMAGE AT A FASTENER LOCATION AT BS 557 BETWEEN S24-25R. REMOVED DAMAGED FASTENER IAW SRM 53-00-01, FIG 201, SEC II. PERFORMED EDDY CURRENT INSPECTION IAW NDT MANUAL, 51-00-16 AND INSTALLED PERMANENT REPAIR FASTENERS IAW SRM 53-00-01, FIG 201.

Part: SKIN — DAMAGED (BS 572-603) · airframe 60,811 hrs · 17,612 cycles

FOUND LIGHTNING STRIKE DAMAGE AT A FASTENER LOCATION AT BS 572 AND 603 AT S25R. REMOVED DAMAGED FASTENERS IAW SRM 53-00-01, FIG 201, SEC II AND SRM 52-30-01. PEFORMED EDDY CURRENT INSPECTION IAW NDT MANUAL, 51-00-16. INSTALLED PERMANENT REPAIR FASTENERS IAW SRM 53-00-01, FIG 201 AND SRM 52-30-01.

Part: FUEL CELL — CORRODED (BS 1038 LBL 67) · airframe 57,555 hrs · 17,020 cycles

MAIN CABIN CTR TANK UPPER SURFACE HAS CORROSION BS 1038, LBL 67. REPAIRED IAW ERA 511589-14, REV ORIGINAL.

Part: DECK PLATE — CORRODED (BS 1712-1718) · airframe 57,555 hrs · 17,020 cycles

AFT CABIN DECKPLATE BS 1712-1718 LBL 10-48, PREVIOUS REPAIR HAS CORROSION. REPAIRED IAW ERA 512662-14 REV ORIGINAL.

Part: ANGLE — CORRODED (BS 1715, LBL12) · airframe 57,555 hrs · 17,020 cycles

LWR SURFACE OF DECK PLATE ANGLE AND NUTPLATE STRAP HAVE CORROSION BS 1715, LBL12. REPLACED ANGLE AND NUTPLATE IAW SRM 51-40-02.

Part: PAN — CORRODED (FUSELAGE) · airframe 57,555 hrs · 17,020 cycles

LAVAVATORY SERVICE PAN HAS EXFOILATING CORROSION IN SEVERAL AREAS AROUND DUMP CHUTE. REPLACED NUTPLATE CHANNEL AND INTERNAL SUPPORT STRUCTURE (PN 141N8631-3 AND 141N6831-4 IAW SRM 51-40-02, PARA 4 AND 7D.

Part: STRINGER — CORRODED (BS 1500-1520) · airframe 57,555 hrs · 17,020 cycles

AFT CARGO BS 1500 TO 1520 S29L HAS CORROSION. REPAIRED IAW SRM 53-00-03, FIG 201 REPAIR 1.

Part: STRAP — CORRODED (BS 1715 RBL 37) · airframe 57,555 hrs · 17,020 cycles

AFT DECK PLATE LOWER SURFACE NUTPLATE STRAPS HAS CORROSION AT BS 1715, RBL 37. REPLACED ANGLE AND NUTPLATE STRAP IAW SRM 51-40-02.

Part: ANGLE — CORRODED (BS 1715 LBL5) · airframe 57,555 hrs · 17,020 cycles

LOWER SURFACE OF DECK PLATE ANGLE HAS CORROSION AT BS 1715 LBL 5. REPLACED ANGLE AND NUTPLATE IAW SRM 51-40-02, PGS 1-3.

Part: SKIN — DENTED (BS 635 S16L) · airframe 57,555 hrs · 17,020 cycles

DENT IN FUSELAGE SKIN, BS 635, STR 16L. REPAIRED IAW ERA 508943-14, REV ORIG.

Part: SEAT TRACK — CHAFED (BS 440-620) · airframe 57,555 hrs · 17,020 cycles

200-125 CHAFE/WEAR ON MAIN CABIN SEAT TRACK CROWN & BOTTOM BS 440 TO 620, RBL 45.5. REPAIRED IAW SRM 53-00-52, REPAIR 3.

Part: SKIN — DENTED (VERTICAL STAB) · airframe 57,555 hrs · 17,020 cycles

LT SIDE VERTICAL STAB DENTED 18 INCHES. REMOVED DAMAGE AND PREPARED AREA FOR REPAIR IAW SRM 51-70-10. INSTALLED REPAIR IAW SRM 51-70-10 942294 RESTORED FINISH IAW MM 51-21.

Part: SKIN — DENTED (BS 620-S15L) · airframe 57,555 hrs · 17,020 cycles

DENT ON FUSELAGE SKIN AT FRAME BS 620 BETWEEN STRINGER 15L AND 16L. REPAIRED IAW ERA 508943-14, REV ORIGINAL.

Part: GATE — CORRODED (R2 DOOR) · airframe 57,555 hrs · 17,020 cycles

R2 DOOR LOWER GATE HAS PITTING CORROSION. REPLACED GATE IAW CMM 52-11-15.

Part: SEAT TRACK — CORRODED (BS 700-780) · airframe 57,555 hrs · 17,020 cycles

CORROSION ON MAIN CABIN SEAT TRACK CROWN BOTTOM FLANGES AREA STA 700 TO 780, LBL 45.5. REPLACED SEAT TRACK SECTION IAW SRM 53-00-52, PG101. (TO 200-131/200)

Part: SEAT TRACK — CORRODED (BS 632-642) · airframe 57,555 hrs · 17,020 cycles

CORROSION ON MAIN CABIN SEAT TRACK BETWEEN STA 632 AND 642 RBL 45.5. REPAIRED SEAT TRACK IAW SRM 53-00-52, FIG 201, REPAIR 3.

Part: SILL — CORRODED (BS 1383) · airframe 57,555 hrs · 17,020 cycles

AFT CARGO DOOR LOWER SILL FITTING HAS CORROSION ON FWD SIDE AT STA 1383. REPLACED FITTING IAW SRM 51-40-02, PG 10 AND 51-40-04, PG 3.

Part: GATE — CORRODED (L2 DOOR) · airframe 57,555 hrs · 17,020 cycles

L-2 LOWER GATE HAS PITTING CORROSION. REPLACED GATE IAW B757 52-11-38-004-001.

Part: MOUNT — CORRODED (GALLEY) · airframe 57,555 hrs · 17,020 cycles

CORROSION ON GALLEY MOUNT FITTING . REMOVED AND REPLACED GALLEY MOUNTS PER SRM 51-40-02 PG 10 PAR 9.

Part: SEAT TRACK — GOUGED (BS 900-1074) · airframe 57,555 hrs · 17,020 cycles

MID CABIN SEAT TRACK RBL 25 BS 900-1074 HAS GOUGES IN MULTIPLE AREAS. REPAIRED SEAT TRACK IAW SRM 53-00-52, REPAIR 4.

Part: DOUBLER — CORRODED (BS 1500-1520) · airframe 57,555 hrs · 17,020 cycles

AFT CARGO BAY LT AIRPHONE ANTENNA INTERNAL DOUBLER HAS CORROSION BETWEEN BS 1500-1520 AND STRINGERS 28L-29L. R & R IAW SRM 51-40-02 AND DWG 42-0040-00 (TO 100-59).

Part: FRAME — DENTED (BS 1360 S25-26L) · airframe 57,555 hrs · 17,020 cycles

AFT CARGO FRAME HAS DENT AT BS 1360 BETWEEN STR25-26L. REPAIRED IAW SRM 53-00-07, REPAIR 5.

Part: FRAME — DENTED (BS 1500 S26-27L) · airframe 57,555 hrs · 17,020 cycles

AFT CARGO FRAME IS DENTED AND GOUGED AT BS 1500 BETWEEN S26 AND 27L. REPAIRED IAW SRM 53-00-07 REPAIR 5.

Part: SEAT TRACK — CORRODED (BS 634-642) · airframe 57,555 hrs · 17,020 cycles

CORROSION ON MAIN CABIN SEAT TRACK BETWEEN STA 634 - 642. REPAIRED PER SRM 53-00-52 FIG 201 REPAIR 3.

Part: SEAL DEPRESSOR — BENT (AFT CARGO DOOR) · airframe 57,555 hrs · 17,020 cycles

AFT CARGO DOOR INNER SEAL DEPRESSOR FLANGE AT FWD LWR CORNER PREVIOUS REPAIR BENT. REPLACED SEAL DEPRESSOR IAW SRM 51-40-02 P. 31 AND 2. (TO 100-270)

Part: FRAME — DENTED (BS 1420) · airframe 57,555 hrs · 17,020 cycles

AFT CARGO FRAME HAS A DENT AT BS 1420 S26L. REPAIRED IAW SRM 53-00-07, REPAIR 5.

Part: ANGLE — CORRODED (BS 685-740) · airframe 57,555 hrs · 17,020 cycles

CORROSION EXFOLIATED ON MAIN CABIN FLOOR SUPPORT SKATE ANGLE BS 685 TO 740, LBL 63. R & R ANGLE IAW SRM 51-40-02, PG2.

Part: DOUBLER — CORRODED (BS 1510 RBL 101) · airframe 57,555 hrs · 17,020 cycles

AFT CARGO LOWER BILGE SKIN ANTENNA DOUBLER HAS CORROSION AT BS 1510, RBL 101. FABRICATED INTERNAL ANTENNA DOUBLER IAW AFP42-0040-00, REV D. INSTALLED ANTENNA DOUBLER IAW SRM 51-40-02, PG 2.

Part: DOUBLER — CORRODED (BS 1510 RBL 10) · airframe 57,555 hrs · 17,020 cycles

AFT CARGO LOWER BILGE SKIN ANTENNA DOUBLER HAS CORROSION AT STA 1510, RBL 10. REPLACED ANTENNA DOUBLER FABRICATED INTERNAL ANTENNA DOUBLER IAW AFP42-0040-00 REV 0, INSTALLED ANTENNA DOUBLER IAW SRM 51-40-02.

Part: ANGLE — CORRODED (BS 1715) · airframe 57,555 hrs · 17,020 cycles

AFT BULK CARGO CEILING AREA LWR SURFACE OF DECK PLATE ANGLE AND NUTPLATE STRAP HAVE CORROSION AT BS 1715, LBL24. REPLACED ANGLE AND NUT PLATE STRAP IAW SRM 51-40-02, PG 3.

Part: FITTING — CORRODED (BS 1437) · airframe 57,555 hrs · 17,020 cycles

AFT CARGO DOOR LOWER SILL AFT FITTING HAS CORROSION ON AFT SIDE AND ON AFT SIDE ATTACHMENT BOLT AREA STA 1437. R & R FITTING IAW SRM 51-40-02.

Part: FITTING — CORRODED (BS 1400) · airframe 57,555 hrs · 17,020 cycles

AFT CARGO DOOR LOWER SILL FITTING HAS CORROSION AT BS 1400. R & R FITTING IAW SRM 51-40-02.

Part: FRAME — DENTED (BS 1440 S25-26L) · airframe 57,555 hrs · 17,020 cycles

AFT CARGO FRAME HAS A DENT AT BS 1446 BETWEEN S25 AND 26L. REPAIRED IAW SRM 53-00-07 FIG 201, REPAIR 5.

Part: SILL — CORRODED (BS 1340-1360) · airframe 57,555 hrs · 17,020 cycles

AFT CARGO NR 3 EMERGENCY EXIT DOOR LOWER SILL SURFACE HAS CORROSION BETWEEN BS 1340-1360. R & R SILL IAW SRM 51-40-02.

Part: PUSHROD — CHAFED (L2 DOOR) · airframe 57,555 hrs · 17,020 cycles

L2 DOOR LOWER GIRT BAR MECHANISM PUSHROD HAS TWO AREAS OF BARE METAL. BARE METAL HAS CHAFE DAMAGE. REPLACED GIRT BAR MECHANISM PUSHROD IAW AMM 52-11-38.

Part: SEAL DEPRESSOR — DENTED (AFT CARGO DOOR) · airframe 57,555 hrs · 17,020 cycles

AFT CARGO DOOR LOWER AFT CORNER SEAL DEPRESSOR DENTED. REPLACED SEAL DEPRESSOR IAW SRM 51-40-02, PG 2 P4-7 AND P 31.

Part: OVEN — DIRTY (GALLEY) · airframe 50,931 hrs · 15,724 cycles

CREW REPORTED SMOKE FROM THE GALLEY OVENS AND PULLED THE OVEN CIRCUIT BREAKERS. MAINTENANCE FOUND GREASE AND CONDENSATION BEHIND OVENS NR 4 AND NR 5. CLEANED BEHIND ALL FOUR OVENS, CHECKED THE WIRING AND LIGHTING. OPERATED OVENS FOR 20 MINUTES WITH NO SMOKE AND NORMAL OVEN OPERATION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,025 hrs · 15,573 cycles

DURING PSV IN ATL, MAINT NOTED CORROSION TO THE UPPER CAP OF THE FLOORBEAM AT STA 1640. SUBJECT CAP WILL BE CUT FROM LBL 13 TO THE RT END. A REPLACEMENT CAP WILL BE SPLICED INTO THE WEB AND THE REMAINING UNDAMAGED SECTION. SUBJECT CAP IS 7075-T6511, EXTRUSION SHAPED PER BAC1518-338. MAINT WILL COMPLY WITH REPAIR PER ERA 493128-14, REV ORIGINAL.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 60,797 hrs · 28,264 cycles

STA 324 BULKHEAD UPPER CHORD CORRODED. REPAIR C/W PER ERA 492992-14 - RBL 33 TO RT END OF PART.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,797 hrs · 28,264 cycles

TRANSVERSE FLOORBEAM STA 365 LBL 9.5 RBL 70.5 - UPPER CAP CORRODED. REPAIR COMPLETED PER ERA492888-14 REV ORIG.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 45,114 hrs · 14,626 cycles

DURING INTIAL TAKEOFF ROLL RIGHT ENGINE DID NOT RESPOND TO THROTTLE ABORTED T/O ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: BLADE — BENT (NR 2 ENGINE) · airframe 42,433 hrs · 14,124 cycles

CREW REPORTED, SAW A BIRD DURING T/O ROLL AND THEN HEARD A BANG. F/O THEN TOLD CAPT THAT THE RT ENG WAS ROLLING BACK DUE TO EPR DROP FROM 1.4 TO 1.25. THE CAPT THEN ABORTED T/O. THE F/O SAID THE EPR RECOVERED JUST AFTER THAT, BUT THE CAPT WAS ALREADY DOING THE RTO. THE F/O REPORTED THAT THE EPR WAS THE ONLY ENGINE IND THAT WAS ABNORMAL. THE EPR FLUX WAS DUE TO COMPRESSOR STALL. ONE (1EA) FAN BLADE BENT. INSPECTED BLADE AND FOU________________________ MM 72-31-02-601 FIG 611. PERFORMED ________________________ AND 16TH STAGE IAW MM 72-00-00. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: TRANSCEIVER — FAILED (WX RADAR) · airframe 42,027 hrs · 14,050 cycles

EN ROUTE FROM ATL TO REC, WX RADAR FAIL MESSAGE APPEARED ON HSI'S AND WX RADAR INDICATOR. REPLACED WX RADAR RECEIVER. ALL CHECKS NORMAL.

Part: EEC — INOPERATIVE (NR 1 ENGINE) · airframe 41,867 hrs · 14,012 cycles

AFTER ENGINE START, LT ENG REV CONT STATUS MSG APPEARED CA-LT T/REV INOP DUE TO LT EEC PRI CONT MCO. FWD LT ENG T/REV TO MCO/PLAC IAW MEL 78-31-01 REMOVED EEC L IAW AMM NOW HARD FAULTS P TLR/EEC MFG PN 815770-2-008 811241. RAN ENG - AFTER SHUTDOWN MSG CLEARED EPCS.

Part: PCA — MALFUNCTIONED (NR 3) · airframe 40,326 hrs · 13,682 cycles

SPOILER MSG AND LIGHT FOUND FUSE LIGHT ON SCM 2R FAULT POWER CONTROL ACTUATOR (PCA) NR 3. INSTALLED KNOWN GOOD SAM AT 2R. NO HELP. REPLACED FUSE. REMOVED C/P FROM NR 3 PCA. NO FUSE LIGHT ON SCM 2R NOW. INSTALLED C/P AT PCA NR 3.506080. REMOVED PCA NR 3 PER AMM. OK TO INSTALLED PER A NARINE611731 250/JFK RII. INSTALLED NR 3 PCA PER AMM. DID NOT ADJUST ROD END NUT OR LVDT DUE TO NO FUSE IN BOX. REPLACED FUSE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 39,679 hrs · 13,557 cycles

AFTER STARTING RT ENGINE GOT STEADY RT GEN DRIVE LIGHT. IDG GEN OIL SERVICED AND INSPECTED RUN UP REFORMED AND PROBLEM CONTINUE. FWD TO MEL 24-00-01. APU OIL CHECKED SERVICED TO FULL. CONFIRMED NO FAULT HISTORY LAST 20 DAYS. REP PLA INSTALLED.

Part: FMC — MALFUNCTIONED (LEFT) · airframe 39,423 hrs · 13,505 cycles

ON TAXI OUT LEFT FMC FAILED. REPLACED LT FMC AS PER AMM CROSSLOAD NAV DATA, ALL CHECKS NORMAL. NO FAULTS NOTED.

Part: WARNING LIGHT — ILLUMINATED · airframe 35,647 hrs · 12,432 cycles

RUDDER RATIO LIGHT ON DURING TAXI OUT A/C RTB RESET FAIL LIGHT ON LEFT AND RIGHT RUDDER RATIO BOX-ALL IS NORMAL.

Part: PROBE — INOPERATIVE (PITOT STATIC) · airframe 35,639 hrs · 12,428 cycles

AFTER ENGINE START F/O PITOT EICAS MESSAGE WILL NOT EXTINGUISH. F/O PITOT PROBE REPLACED PER M/M.

Part: STRUCTURE — DAMAGED (RT WING) · airframe 35,621 hrs · 12,419 cycles

DURING THE INSTALLATION OF THE APB BLENDED WINGLET, THERE WAS AN INSTALLATION ERROR WHILE TRIMMING THE SHEAR TIE AT THE RT WING BETWEEN S-11 AND S-12 ON RIB 18 AT WING STATION 565.50. THE HORIZONTAL LEG OF THE 112N5176-6 CHORD UPPER SHEAR TIE SURFACE WAS BLENDED RESULTING IN AN AREA OF REDUCED MATERIAL THICKNESS NEAR THE RADIUS OF THE CHORD. APB WAS CONTACTED AND PROVIDED AN APPROVED REPAIR CONSISTING OF TRIMMING OUT A PORTION OF THE CHORD, AND LETTING SOME OF THE BLENDS REMAIN. PLEASE REFER TO 462999-14.

Part: STATOR — INOPERATIVE (ALTERNATOR)

GEG INFLIGHT T1092/01MAY - LEFT ENGINE AUTO FLAMEOUT DURING CLIMB. RESTART UNSUCCESSFUL. LANDED GEG WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE ELECTRIC ENGINE CONTROL ALTERNATOR STATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY ESCAPE PATH LIGHT AT ROWS 11 TO 14 INOPERATIVE. EMERGENCY TRACK LIGHT AT 24D MISSING END CAP AND BROKEN CABLE. REPLACED EMERGENCY ESCAPE PATH LIGHT SEGMENTS AT ROWS 11 TO 14. REPLACED EMERGENCY TRACK LIGHT END CAP AT 24D AND REPLACED EMERGENCY LIGHT STRIP AT SEAT 24 TO LAVATORY D FOR BROKEN CABLE ON EMERGENCY TRACK LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHTS ON RIGHT HAND FIRST CLASS BAGGAGE BINS INOPERATVE. REPLACED BATTERY CHARGER ASSEMBLY FOR EMERGENCY LIGHTS ON RIGHT HAND FIRST CLASS BAGGAGE BINS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — DISLODGED (CABIN) · airframe 23,105 hrs · 7,271 cycles

ON ARRIVAL EMERGENCY STRIP BY MID LAV PULLED UP. REINSTALLED EGRESS LIGHT SYS PN 5774-1 TWA 91-8032. OPS CHECKED NORMAL PER MM33-51-11. CHECK-C MCI 10-12-02.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,391 hrs · 6,995 cycles

SECTION OF EGRESS LIGHTING INOPERATIVE, REPLACED BATTERY AND POWER SUPPLY UNIT. LAST CHECK C PERFORMED MCI 10/12/2002

Part: CONNECTOR — DIRTY (CABIN) · airframe 17,679 hrs · 5,374 cycles

THE EGRESS LIGHT AT SEAT ROW 1 WAS INOPERATIVE. CLEANED AND RE-INSTALLED THE LAMP CONNECTOR. CHECK-C 4-12-01 LAX.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,577 hrs · 5,343 cycles

THE EGRESS LIGHT WAS INOPERATIVE AT SEAT 1A. REPLACED THE FLEX LAMP ASSY. CHECK-C 4-12-01 LAX.

Part: DOOR — DENTED (L4 DOOR) · airframe 17,023 hrs · 5,190 cycles

ENGINEERING REQUESTED A PERMANENT REPAIR TO A DENT JUST FWD AND BELOW THE LEFT SIDE NUMBER 4 CABIN DOOR, STA 1610 AND STRINGER 18L. INSTALLED AN EXTERNAL DOUBLER 8 IN BY 10 INCHES USING BLIND FASTENERS PER SRM 53-00-01. CHECK-C 9-27-99 LAX.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE) · airframe 16,579 hrs · 5,065 cycles

THE LEFT SIDE NUMBER 4 CABIN DOOR EVACUATION SLIDE HAD LOW BOTTLE PRESSURE. REPLACED THE SLIDE ASSEMBLY. CHECK-C 9-27-99 LAX.

Part: LIGHT — BROKEN (ROW 29) · airframe 15,371 hrs · 4,715 cycles

THE EGRESS LIGHT STRIP AT SEAT ROW 29 WAS INOPERATIVE. REPLACED THE FLEX-LAMP. CHECK-C 9-27-99 LAX.

Part: LIGHT — DAMAGED (CABIN) · airframe 15,108 hrs · 4,633 cycles

EGRESS LAMP WAS INOPERATIVE IN THE MIDDLE OF FIRST CLASS AND THE BEGINNING OF COACH. REPLACED FLEX LAMP STRIP. CHECK-C 9-27-99 LAX.

Part: VIDEO UNIT — OVERHEATED (ROW 27) · airframe 15,044 hrs · 4,611 cycles

THE VIDEO MONITOR AT ROW 27 ABC OVERHEATED. A SMALL AMOUNT OF SMOKE WAS OBSERVED AND IT WAS WARM TO TOUCH. VIDEO SYSTEM WAS DISABLED BY PULLING THE CIRCUIT BREAKER. THE VIDEO SCREEN WAS REPLACED. CHECK-C 9-27-00 LAX.

Part: CONNECTOR — WORN (CABIN) · airframe 13,054 hrs · 3,931 cycles

CABIN EGRESS LIGHTS LOOSE CONNECTION IN FIRST CLASS FWD OF THE LAV. REMOVED AND REPLACED JUMPER CABLE TWA (P/N 91-8055). CHECKS MADE TO ASSURE NORMAL PERFORMANCE, OPS CK EGRESS LTS. AC 02 12-23-00 LAX.

Part: BATTERY PACK — DISCHARGED (CABIN)

THE EMERGENCY LIGHT OVER SEAT ROW 12, RT SIDE OF CABIN, WAS INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 9-12-99 LAX.

Part: LIGHT — DISCONNECTED (ROWS 1 & 2)

THE CABIN EGRESS LIGHTS WERE INOPERATIVE AT ROWS 1 AND 2. FOUND LOOSE CONNECTION. RECONNECTED LAMPS. CHECK-C 9-12-99 LAX.

Part: SKIN — CORRODED (WS 341.5-425.5)

DURING CHECK-C MAINT, FOUND APPROX 200 RIVETS WITH STAGE 2 CORROSION ON TOP OF THE LEFT WING UNDER THE ICE DETECTION STRIPE, STA 341.5 THRU 425.5. *S/D* CORROSION WAS REMOVED BY BLENDING PER SRM 57-30-1 FIG 6, AT A 10:1 REMOVAL RATIO. ALL BLEND OUT AREAS WERE MEASURED AND INFORMATION GIVEN TO BOEING ENGINEERING. A BOEING TEAM ACCOMPLISHED FASTENER REMOVAL AND INSTALLATION OF 120 FASTENERS WITH MATERIAL REMOVED GREATER THAN 0.020 INCHES. THE DAMAGED BACR15FH8* RIVETS WERE REPLACED WITH BACB30NY8K*Y HI-LOKS. TWA MAINTENANCE RESTORED THE AREA TO THE ORIGINAL PROTECTIVE FINISH PER SRM 57-30-1, FIGURE 6.

Part: CONNECTOR — CONTAMINATED (ROW 26-34)

FOUND THE EGRESS LIGHTS DIM AT ROWS 26 TO 34. DRIED OUT THE POWER SUPPLY CABLE AND THE LAMP CONNECTIONS. CHECK-C 5-9-98 LAX.

Part: BULB — FAILED (CABIN)

FOUND THE LEFT SIDE NUMBER 4 CABIN DOOR SLIDE LIGHT INOPERATIVE ON TEST. REPLACED THE LAMP AND SECURED THE LAMP IN THE SOCKET. CHECK-C 5-9-98 LAX.

Part: SKIN — TORN (BS 1860)

THE FUSELAGE SKIN WAS TORN 6 INCHES BY 3 INCHES, BETWEEN S28 AND S29 ON LEFT SIDE AT STA 1806. EXTERNAL DOUBLER REPAIR INSTALLED PER MCIER RELEASE AND 757 SRM 53-00-01, FIG 204. CHECK-C 5-9-98 LAX.