N976TW

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 37,530 hrs · 18,067 cycles

NUMEROUS OVERHEAD CEILING EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED FIRST CLASS EMERGENCY LIGHT BATTERY PACK. OPS CHECK NORMAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 34,544 hrs · 16,533 cycles

DENT AFT RADOME STATION 37 STRINGER 30. INSTALLED NEW SKIN PER SRM 51-01-00.

Part: SKIN — DAMAGED (ENTRY DOOR) · airframe 34,544 hrs · 16,533 cycles

FORWARD ENTRY DOOR, SKIN DAMAGED AT HOLD OPEN HOOK CUTOUT. ACCOMPLISHED REPAIR PER SRM 52-05-00 FIGURE 20A.

Part: SKIN — BENT (ENTRY DOOR) · airframe 34,544 hrs · 16,533 cycles

FORWARD ENTRY DOOR, LOWER EXTERNAL SKIN BENT. ACCOMPLISHED REPAIR PER SRM 52-10-00-0 FIGURE 1.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 34,544 hrs · 16,533 cycles

LONGERON 2 RIGHT IS CRACKED AFT OF FRAME STATION 1418. PERFORMED LONGERON SPLICE REPAIR PER SRM 53-02-00 FIGURE 18.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 34,544 hrs · 16,533 cycles

SUPPORT CRACKED AT FORWARD END OF NUMBER 1 SEAT TRACK STATION 213. INSTALLED NEW SUPPORT PER AARD 51-10-00-5.

Part: SKIN — DENTED (FUSELAGE) · airframe 34,544 hrs · 16,533 cycles

DENT IN FUSELAGE SKIN AT STATION 218 BETWEEN LONGERON 18 AND 19 LEFT SIDE. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-04-05 FIGURE 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,544 hrs · 16,533 cycles

FRAME CRACKED AFT SIDE OF 1418 AT LONGERON 2. INSTALLED FRAME DOUBLER PER SRM 53-03-00 FIGURE 31A.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 34,544 hrs · 16,533 cycles

LONGERON 2 LEFT IS CRACKED AFT OF FRAME STATION 1418. PERFORMED LONGERON SPLICE REPAIR PER SRM 53-02-00 FIGURE 18.

Part: DRAIN PAN — DAMAGED (FUSELAGE) · airframe 34,544 hrs · 16,533 cycles

HOLE AT OUTBOARD SIDE OF G1 GALLEY DRAIN PAN IN SUBFLOOR. REPLACED MOUNT PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,544 hrs · 16,533 cycles

G1 GALLEY, AFT INBOARD MOUNT CORRODED. REPLACED MOUNT PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,544 hrs · 16,533 cycles

RIGHT CUSP SHEET STATIONS 598 TO 712 CORRODED. INSTALLED NEW CUSP SHEET RIGHT STATIONS 598 TO 712 PER AARD 51-10-00-5.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,544 hrs · 16,533 cycles

CORROSION ON OUTBOARD G1 GALLEY MOUNT. REPLACED MOUNT.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,544 hrs · 16,533 cycles

G2 GALLEY, FORWARD INBOARD MOUNT CORRODED. REPLACED MOUNT.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,544 hrs · 16,533 cycles

CORROSION ON NUMBER 4 SEAT TRACK STATION 208. ACCOMPLISHED SPLICE REPAIR AT STATIONS 280 TO 280 PER SRM 53-05-00 FIGURE 4F.

Part: WEB — DAMAGED (FUSELAGE) · airframe 34,544 hrs · 16,533 cycles

SUBFLOOR DAMAGED UNDER AFT INBOARD G2 GALLEY MOUNT. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,544 hrs · 16,533 cycles

FRAME CRACKED AFT SIDE OF 1418. INSTALLED DOUBLER REPAIR PER SRM 53-03-00.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,544 hrs · 16,533 cycles

RIGHT CUSP CRACKED AT STATION 1214. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: BEAM — CORRODED (CARGO DOOR) · corrosion level 3 · airframe 34,544 hrs · 16,533 cycles

AFT CARGO HORIZONTAL DOOR BEAM STATIONS 1163 TO 1174 CORRODED. BLENDED OUT CORROSION FROM VERTICAL AND HORIZONTAL SURFACES OF AFT CARGO DOOR BEAM BETWEEN STATIONS 1155 AND 1212 PER AARD 53-10-00-3. INSTALLED AFT CRAGO BEAM DOUBLER AS PER AARD 53-10-00-3.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 34,544 hrs · 16,533 cycles

MID CARGO DOOR PLUG ON OUTER SKIN AROUND CENTER OF DOOR ABOUT 3 INCHES FROM EDGE DAMAGED. INSTALLED DOUBLER PER SRM 52-05-00 FIGURE 2 SHEET 1.

Part: SKIN — WORN (CARGO DOOR) · airframe 34,544 hrs · 16,533 cycles

AFT CARGO DOOR SKIN 14 INCHES FROM FORWARD SIDE 9.5 INCHES WORN. FABRICATED AND INSTALLED DOUBLER PER BSD #SG09530001.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,544 hrs · 16,533 cycles

RIGHT CUSP STATIONS 1162 TO 1166 CORROSION IS OUT OF LIMITS. INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,544 hrs · 16,533 cycles

SEAT TRACK NUMBER 3 AT STATION 793 HAS CORROSION THAT IS OUT OF LIMITS. INSTALLED REPLACEMENT SEAT TRACK AND SPLICE PER SRM 53-05-00 FIGURE 4F.

Part: BEAM — CORRODED (FUSELAGE) · airframe 34,544 hrs · 16,533 cycles

CORROSION ON DOOR BEAM VERTICAL LEG STATIONS 642 TO 676. REPAIRED DOOR BEAM PER AARD 53-10-00-3.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,544 hrs · 16,533 cycles

CORROSION ON SUBFLOOR, STATION 199, INBOARD OF FORWARD SERVICE THRESHOLD ATTACH CHANNEL OUT OF LIMITS. INSTALLED DOUBLER AND OVERLAY DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DAMAGED (PAX DOOR) · airframe 34,544 hrs · 16,533 cycles

FORWARD PASSENGER DOOR OUTER SKIN DAMAGED AT HOLD OPEN HOOK AREA AFT END OF CUT OUT. BLENDED TO REMOVE DAMAGE. FABRICATED AND INSTALLED DOUBLER PER SRM 52-05-00 FIGURE 20A.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,544 hrs · 16,533 cycles

STATION 376 TO 378 RIGHT CUSP CORROSION OUT OF LIMITS. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DAMAGED (TE FLAP) · airframe 34,544 hrs · 16,533 cycles

LEFT WING OUTBOARD FLAP, MOST OUTBOARD REMOVABLE TRAILING EDGE PANEL HAS A LARGE DENT ON LOWER OUTBOARD SIDE. REPLACED DENTED SKIN, 3-DAMAGED RIBS AND DISBONDED TRAILING EDGE WEDGE WITH NEW SKIN, RIBS AND TRAILING EDGE WEDGE AS PER ESO 80096.

Part: REGULATOR VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 33,658 hrs · 16,080 cycles

DFW - FLIGHT ATTENDNANTS REPORTED VISIBLE SMOKE AND ODOR IN AFT CABIN AREA. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT AND RIGHT PRESSURE REGULATOR VALVES AND ACCOMPLISHED HIGH PRESSURE PACK BURN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: UPLOCK SENSOR — FAULTY (NLG) · airframe 33,431 hrs · 15,978 cycles

DFW - INFLIGHT ORD-PVR. CREW REPORTED NOSE GEAR UNSAFE INDICATION DURING FLIGHT. EMERGENCY DECLARED FLIGHT DIVERTED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE D1-31 NOSE GEAR UP LOCK POSITION SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: GENERATOR — FAILED (LT ENGINE) · airframe 33,145 hrs · 15,826 cycles

DEN - INFLIGHT SEA-DFW CREW REPORTED LEFT GENERATOR FAILED AND AIXILIARY POWER UNIT WOULD NOT START. EMERGENCY DECLARED FLIGHT DIVERTED DEN LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT HAND ENGINE DRIVEN GENERATOR AND SERVICE APU OIL TO FULL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY — NOT SEATED (CABIN) · airframe 31,673 hrs · 15,118 cycles

ROW 20 RIGHT SIDE EMERGENCY EXIT SIGN INOPERATIVE. RE-SEATED BATTERIES FOR ROW 20 RIGHT SIDE EMERGENCY EXIT SIGN. OPS CHECK NORMAL.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 31,673 hrs · 15,118 cycles

SEAT 8D EMERGENCY AISLE LIGHT INOPERATIVE. FOUND LOOSE CONNECTORS AT SEATS 8D, RE-SEATED CONNECTOR. OPS CHECK NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 31,673 hrs · 15,118 cycles

SEAT 21D EMERGENCY AISLE LIGHT INOPERATIVE. FOUND LOOSE CONNECTORS AT SEATS 21D. RESEATED CONNECTOR. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 31,673 hrs · 15,118 cycles

ROW 20 LEFT SIDE EMERGENCY EXIT SIGN INOPERATIVE. RESEATED BATTERIES FOR ROW 20 LEFT SIDE EMERGENCY EXIT SIGN. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,651 hrs · 14,656 cycles

EMERGENCY PATH LIGHT BATTERIES WEAK AT CONTROLLERS AB5-1 AND AB5-2. REPLACED BATTERY PACK FOR EMERGENCY PATH LIGHTS AT CONTROLLERS AB5-1 AND AB5-2 PER MM 33-60-98-4, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,651 hrs · 14,656 cycles

EMERGENCY LIGHTS ABOVE SEAT ROWS 23 THRU 26 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ABOVE SEAT ROWS 23 THRU 26. OPS CHECKED NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,651 hrs · 14,656 cycles

FUSELAGE SKIN CRACKED AT STATION 1474 LEFT SIDE OUTBOARD OF AIR STAIR CUTOUT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01-00.

Part: SENSOR — FAILED (LE SLAT) · airframe 29,592 hrs · 14,149 cycles

WHEN RETRACTING THE SLATS ON DEPARTURE THE SLAT DISAGREE LIGHT STAYED ILLUMINATED. THERE WAS NO ADVERSE YAW OR ROLL. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED RIGHT SLOT C SENSOR.

Part: DUCT — DAMAGED (AC BAY) · airframe 27,707 hrs

DFW - TAIL COMPARTMENT OVERHEAT INDICATION ILLUMINATED. RETURNED DFW WITHOUT INCIDENT. REPLACED WATER SEPARATOR DUCT ASSEMBLY AND ICE TO WATER SEPARATOR DUCT MPN 5953624U513 IN TAIL COMPARTMENT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 26,685 hrs

ORD INFLIGHT - CREW REPORTED SUSPECTED NUMBER ONE ENGINE COMPRESSOR STALL DURING CLIMB THROUGH 25000 FEET. FELT AND HEARD BANG N1 ENGINE PRESSURE RATIO RAPID FLUCTUATION. CREW BROUGHT ENGINE TO IDLE. FLIGHT ATTENDANTS REPORTED EXTREME VIBRATION ON LEFT SIDE OF AIRCRAFT. CREW SHUT ENGINE DOWN AND VIBRATION STOPPED. LANDED ORD WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE ON 27 OCT AT ORD DUE TO BOROSCOPE FINDINGS.

Part: TERMINAL — DIRTY (EMERGENCY LIGHTS) · airframe 23,747 hrs

SFO - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 8 TO 16 INOPERATIVE. CLEANED BATTERY PACK TERMINALS FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 8 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHTS AT OVERWING LEFT AND RIGHT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERWING LEFT AND RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (MASTER BATTERY)

LBB INFLIGHT T1873/06OCT DFW TO ABQ - DURING CRUISE BATTERY CHARGER LIGHT ILLUMINATED. LANDED LBB WITHOUT INCIDENT. REPLACED BATTERY CHARGER, SHIP BATTERIES AND BATTERY CHARGER TRANSFER RELAY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

SEA EMERGENCY LIGHT AT SEAT 4E MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 4E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — MISSING (EMERGENCY LIGHT)

SEA - EMERGENCY LIGHT AT SEAT 4E MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 4E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY CEILING LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK IN CEILING AT FIRST CLASS GALLEY FOR EMERGENCY CEILING LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LGA - EMERGENCY EGRESS LIGHTS AT AFT OVERWING INOPERATIVE. REPLACED BATTERY PACK AT B5105 FOR EMERGENCY EGRESS LIGHTS AT AFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LGA - EMERGENCY CEILING LIGHTS FROM SEAT ROWS 16 TO 18 INOPERATIVE. REPLACED BATTERY PACK AT B5102 FOR EMERGENCY CEILING LIGHTS FROM SEAT ROWS 16 TO 18. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DIRTY (CABIN)

SFO - EMERGENCY EXIT SIGN LIGHT ABOVE ROW 21A TO 21E INOPERATIVE. CLEANED EMERGENCY BATTERY FOR INOPERATIVE EMERGENCY EXIT SIGN LIGHT ABOVE ROW 21A TO 21E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

SFO - EMERGENCY ESCAPE PATH SEAT MOUNTED LIGHT AT ROW 22 AND AFT OF CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT 22E AND 29E FOR EMERGENCY ESCAPE PATH SEAT MOUNTED LIGHT AT ROWS 22 AND AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: APU — ODOR

DFW - DURING TAXI WHEN APU WAS TURNED ON, CAUSED SMOKE IN CABIN AND COCKPIT. AN EMERGENCY EVACUATION OCCURRED. TAIL CONE SLIDE DEPLOYED. REPLACED SLIDE AND TAIL CONE. REPLACED APU DUE TO SKYDROL INGESTION CAUSING SMOKE AND ODOR IN CABIN AND COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - OVERHEAD EMERGENCY LIGHTS AT FORWARD LIFE RAFT BIN INOPERATIVE. REPLACED BATTERY PACK AT B5101 FOR OVERHEAD EMERGENCY LIGHTS AT FORWARD LIFE RAFT BIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — LOOSE (CABIN)

RDU AFT VENTRAL STAIR AREA OVERHEAD EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERIES FOR AFT VENTRAL STAIR AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: COVER · airframe 9,162 hrs · 5,025 cycles

THE EGRESS LIGHTING AT SEAT 25D WAS INOPERATIVE. REPLACED THE TRACK COVER. CHECK-C 9-17-02 STL. --CLOSED--

Part: POWER SUPPLY (B5-103) · airframe 5,507 hrs · 2,969 cycles

THE FORWARD OVERWING EMERGENCY EXIT LIGHTS STAYED ON WITH POWER OFF. REPLACED THE POWER SUPPLY. CHECK-C 11-8-00 STL. --CLOSED--