N966TW

Part: WIRE — CHAFED (EMERGENCY LIGHT) · airframe 53,325 hrs · 27,261 cycles

WIRES WERECHAFED TO THE RAMP LIGHT ON THE CEILING PANEL IN THE TAIL COMPARTMENT. REPLACED THE EMERGENCY LIGHT. OPS CHECKED OK IAW AMM 33-53-00.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 53,102 hrs · 27,115 cycles

LEFT AFT FLASHLIGHT WAS INOPERATIVE. RESTRAINING STRAP WAS MISSING. REPLACED THE FLASHLIGHT BATTERY PACK AND STRAP IAW AMM 25-60-00. OK FOR SERVICE.

Part: LANYARD — DETACHED (L1 DOOR SLIDE) · airframe 53,056 hrs · 27,082 cycles

L1 DOOR SLIDE CABLE THAT CONNECTS TO THE GIRT BAR IS NOT CONNECTED. ATTACHED THE GIRT BAR LANYARD IAW AMM 25-62-00. OK FOR SERVICE.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 52,998 hrs · 27,047 cycles

ONE OF THE EMERGENCY FLASHLIGHTS NEAR THE FORWARD GALLEY WAS INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-60-00.

Part: PIN — MIGRATED (JETTISON PULLEY) · airframe 52,950 hrs · 27,021 cycles

WHILE TROUBLESHOOTING MIC 32218889, MAINTENANCE DISCOVERED THE TAILCONE JETTISON CABLE HAD JUMPED OUT OF THE PULLEY TRACK AND THAT SAME PULLEY HAS A PIN OR PAWL THAT HAS RETRACTED OUT OF THE PULLEY MECHANISM. AND THE CABLE WAS FRAYED. INSPECTED CABLE AND FOUND TO BE OK FOR SERVICE. REINSTALLED CABLE OVER PULLEY AND REINSTALLED FULLEY PIN IAW AMM 53-53-00.

Part: VALVE — FAULTED (TAIL) · airframe 52,757 hrs · 26,904 cycles

AFTER TAKEOFF, TAIL COMPARTMENT TEMPERATURE LIGHT AND MASTER WARNING LIGHT ILLUMINATED. LIGHTS REMAINED ON APPROXIMATELY 10 SECONDS AFTER COMPLETING MEMORY ITEMS ON CHECKLIST. EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. AIRCRAFT WAS GROUNDED. ACCOMPLISHED CARD 0930 SUMMER PREP, 26-96-11 TAIL COMPARTMENT TEMP HIGH LIGHT, 36-95-14 TAIL COMPARTMENT LEAKS AND 5770-20. REPLACED RIGHT AUGMENTATION VALVE.

Part: DUCT — FAULTY · airframe 52,757 hrs · 26,904 cycles

AFTER TAKEOFF, TAIL COMPARTMENT TEMPERATURE LIGHT AND MASTER WARNING LIGHT ILLUMINATED. LIGHTS REMAINED ON APPROXIMATELY 10 SECONDS AFTER COMPLETING MEMORY ITEMS ON CHECKLIST. EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO DFW. AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED MCM CARDS 0930 SUMMER PREP, 26-96-11 TAIL COMPARTMENT TEMP HIGH LIGHT, 36-95-14 TAIL COMPARTMENT LEAKS AND 5770-20. REPLACED PYLON DUCT TO AUGMENTATION VALVE.

Part: DUCT — LEAKING (AC BAY) · airframe 52,661 hrs · 26,839 cycles

AIRCRAFT WAS GROUNDED. DFW-MSY RETURNED DFW ACCOUNT FIRE INDICATION LIGHT. EMERGENCY WAS DECLARED, FLIGHT LANDED WITHOUT INCIDENT AND UNDERWEIGHT. AFTER TAKE OFF, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT CAME ON. IT WAS INTERMITTENT AT FIRST GOING THROUGH 2000 FT. CAME ON STEADY UNTIL THRUST LEVERS WERE BROUGHT BACK TO CRUISE THRUST AT LEVEL OFF AT 4000 FT. LIGHT THEN WENT OUT. MAINTENANCE FOUND RT CROSSFEED DUCT LEAKING AT RT CROSSFEED VALVE AND DUCT MATING SURFACE. REMOVED AND REPLACED R/H CROSSFEED DUCT PER AMM 36-00-00, LEAK CHECK GOOD.

Part: SENSOR — FAULTY (TAIL COMPARTMENT) · airframe 52,633 hrs · 26,819 cycles

AIRCRAFT WAS GROUNDED. DFW-IAD RETURNED DFW ACCOUNT TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. EMERGENCY DECLARED. LANDED OVERWEIGHT WITHOUT INCIDENT. AT 2500 FEET TAIL COMPARTMENT HIGH LIGHT FLASHED ON 2-3 TIMES. MAINTENANCE ACCOMPLISHED MCM CARDS 0930 SUMMER PREP, 26-96-11 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT AND 36-95-15 TAIL COMPARTMENT LEAKS. REPAIRED ALL LEAKS FOUND AND REPLACED ALL WORN PARTS. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT, FAILED CHECK FLIGHT. MAINTENANCE REPLACED LT AND RT TAIL COMPARTMENT OVERHEAT SENSORS IAW AMM 36-20-02. OPS CHECKED GOOD. ACCOMPLISHED ANOTHER FUNCTIONAL CHECK FLIGHT, PASSED CHECK FLIGHT.

Part: DUCT — LEAKING (TAIL BAY) · airframe 52,491 hrs · 26,731 cycles

TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ANNUNCIATED ON ROLL OUT AND TAKEOFF. EMERGENCY DECLARED, LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED MCM 36-95-14 AND 0930, FOUND FLEX DUCT LEAKING. REPLACED FLEX DUCT IAW AMM 36-00-00, OPS CHECKED GOOD.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 52,443 hrs · 26,699 cycles

AIRCRAFT WAS GROUNDED. CAPTAINS LEFT HAND FORWARD WINDOW IS DELAMINATED AND IS OUT OF LIMITS AS PER CARD 0495 AND 56-00-00 AND AMM 56-10-00. REPLACED CAPTAINS FORWARD WINDOW PER AMM 56-10-02.

Part: LENS — CRACKED (EXIT SIGN) · airframe 50,936 hrs · 25,673 cycles

AIRCRAFT WAS NOT GROUNDED. OVERWING EMERGENCY EXIT SIGN BY SEAT 21A HAS A CRACKED LENS COVER. INSTALLED NEW LENS COVER. OPERATIONAL CHECK GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,792 hrs · 25,581 cycles

CEILING EMERGENCY EXIT LIGHTS ABOVE SEATS 23B, 23D, 24, 26B, AND 26D ARE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK B5-106 ABOVE SEAT ROW 25DEF IAW AMM 33-53-00. OPS CHECKED GOOD.

Part: CRANK ASSY — BROKEN (L1 DOOR GUST LOK) · airframe 50,791 hrs · 25,580 cycles

L1 DOOR HINGE HOOK ACTUATOR CRANK IS BROKEN. REMOVED AND REPLACED GUST LOCK CRANK IAW ESO 80172. AIRCRAFT WAS GROUNDED.

Part: LENS — MISSING (EXIT SIGN) · airframe 50,552 hrs · 25,411 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN ACROSS FROM THE FORWARD LAVATORY HAS A MISSING LENS COVER. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY PER AMM 33-42-00. OPERATIONAL CHECK GOOD.

Part: BAYONET — OUT OF ADJUST (L1 DOOR) · airframe 50,473 hrs · 25,364 cycles

THE L1 DOOR WILL NOT OPEN OR CLOSE FROM INSIDE OR OUTSIDE. INSPECTED AND FOUND THE DOOR BAYONET OUT OF SEQUENCE. RESET BAYONET, DOOR OPS NORMAL IAW AMM 52-11-00.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 49,871 hrs · 24,983 cycles

L1 FA AISLE FLASHLIGHT LED DOES NOT FLASH. REPLACED BATTERY. CHECKS OK AMM 25-60-00. THE AIRCRAFT WAS NOT GROUNDED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,465 hrs · 24,738 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. FORWARD WHALEBONE FRAME IS CRACKED AT THE KEEL BEAM, FORWARD INBOARD CORNER OF LEFT WHEEL WELL, BETWEEN FUSELAGE STATIONS 930 AND 937. REPAIRED IAW AARD 53-10-00-6.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 49,465 hrs · 24,738 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. FORWARD CARGO DOOR LOWER FORWARD STOP PAD FITTING 5 IS CRACKED. REMOVED AND REPLACED FITTING IAW AARD 51-00-05-1, AND DRAWINGS CDK2345 AND 5910141.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 49,465 hrs · 24,738 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. FORWARD CARGO DOOR MIDDLE FORWARD STOP PAD FITTING NR 3 IS CRACKED. REMOVED AND REPLACED FITTING IAW AARD 51-00-05-1, AND DRAWINGS CDK2345 AND 5910141.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,023 hrs · 24,431 cycles

AIRCRAFT WAS GROUNDED. FUSELAGE SKIN IS CRACKED AT UPPER AFT CORNER OF FORWARD CARGO DOOR OPENING AT APPROXIMATELY STATION 427. REPAIRED SKIN IAW SRM 53-50-00-001 FIGURE 68.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,022 hrs · 24,430 cycles

AIRCRAFT NOT GROUNDED. EMERGENCY ESCAPE PATH MARKING POWER SUPPLY AB5-3 FAILED TEST. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-60-98. OPERATIONAL CHECK GOOD.

Part: APU — LEAKING · airframe 48,823 hrs · 24,300 cycles

DURING TAXI IN A HAZE GRADUALLY FILLED THE CABIN. MAINTENANCE FOUND OIL IN APU AIR INLET. REMOVED AND REPLACED APU. AIRCRAFT WAS GROUNDED. (OPEN)

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 48,715 hrs · 24,236 cycles

AIRCRAFT NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BY THE FORWARD ENTRY DOOR INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-60-00. OPERATIONAL CHECK GOOD.

Part: COMPRESSOR BLADE — DAMAGED (RT ENGINE) · airframe 47,577 hrs · 23,512 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING ROTATION RT ENG EXPERIENCED COMPRESSOR STALL LIGHT ENG COMPRESSOR STALL AFTER TAKEOFF, ROUTED TO HANGAR TO COMPLETE 71-91-16. BORESCOPE INSPECTION FOUND DAMAGED COMPRESSOR BLADES IN STAGES 11 - 13. R & R ENG IAW MCM 71-91-99. ACCOMPLISHED OPERATIONAL & LEAK CHECKS. SYS CHECKED NORMAL.

Part: ENGINE — FAILED (LEFT) · airframe 47,112 hrs · 23,222 cycles

THE INBD CREW REPORTED ODOR & HAZE IN THE CABIN, CAUSING EYES TO WATER & WAS DIFFICULT TO BREATHE. ACCOMPLISHED SIC 21-96-01 & FOUND LT ENG TO BE THE SOURCE OF THE ODOR. R & R THE LT ENG IAW SIC 71-91-99 & BOW. LEAK CHECK & OPERATIONS CHECKED GOOD. ACCOMPLISHED SIC 21-92-12 PACK BURN OUT CARD, NO FURTHER ODORS NOTED. THE ACFT WAS GNDED.

Part: TRIM MOTOR — MALFUNCTIONED (ZONE 300) · airframe 47,075 hrs · 23,202 cycles

EMERGENCY LANDING WAS DECLARED, INBD ACCOUNT STAB TRIM JAMMED AT 6 DEG UP, AFTER SELECTING FLAPS 40 DEG. PERFORMED GO AROUND, ON SECOND ATTEMPT WAS ABLE TO LAND SAFELY BUT STAB TRIM DID JAM AGAIN AT 6 DEG NOSE UP WITH FLAPS AT 40. NO FURTHER INCIDENTS WAS REPORTED. R & R ALTERNATE TRIM MOTOR IAW MCM 27-94-18. STABILIZER SYS OPERATIONS CHECKED NORMAL. THE ACFT WAS GNDED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,042 hrs · 23,181 cycles

EMERGENCY EXIT LIGHTS IN CEILING AISLE, FC WILL NOT TURN OFF, NO POWER ON A/C. REPLACED EMER LIGHT BATTERY PACK B5-100 IAW MM 33-53-00. OPERATIONS CHECKED GOOD. THE ACFT WAS NOT GNDED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 46,840 hrs · 23,043 cycles

ON APPROACH WITH GEAR DOWN, ALL FOUR ANTI-SKID FAIL LIGHTS ILLUMINATED. AN EMER WAS DECLARED. FLIGHT ACCOMPLISHED GO AROUND & LANDED NORMALLY ON SECOND ATTEMPT. ACCOMPLISHED ANTI-SKID OPERATIONAL SYS CHECK IAW AMM 32-43-00. SYS CHECKED GOOD. OK FOR SERVICE. THE ACFT WAS NOT GNDED.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 46,092 hrs · 22,583 cycles

AFT CARGO LT AFT TIE DOWN TRACK, STATION 1231 - 1250, IS CORRODED. INSTALLED NEW AFT LT TIE DOWN TRACK AT STATION 1220 - 1322 IAW SRM 51-30-01 & SRM 51-30-05.

Part: BEAM — CORRODED (FUSELAGE) · airframe 46,092 hrs · 22,583 cycles

CORROSION FOUND ON AFT CARGO LOWER DOOR BEAM, STATION 1155 - 1212. CORROSION BLENDED OUT OF LIMITS. INSTALLED DOOR BEAM REPAIR DOUBLER IAW AARD 53-10-00-3.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 46,092 hrs · 22,583 cycles

LEFT TIE DOWN TRACK CORRODED STATION 1193. INSTALLED NEW LT TIE DOWN TRACK, STATION 1220 - 1108 IAW AARD 51-00-05-1 & PRINT 5936663.

Part: SKIN — DENTED (FUSELAGE) · airframe 46,092 hrs · 22,583 cycles

DENT & SCRATCHES AT STATION 194, BETWEEN L20R - L22R. BLENDED OUT SCRATCHES, WITHIN LIMITS IAW SRM 53-04-01 CONDITION 1 PARAGRAPH 5 C. INSTALLED INTERNAL DOUBLER TO REPAIR DENT IAW SRM 53-04-02 FIGURE 2 SHEET 4 VIEW E.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,092 hrs · 22,583 cycles

RIGHT CUSP AT STATION 863 TO 866 HAS CORROSION OUT OF LIMITS. BLENDED AREA WAS OUT OF LIMITS. REPLACED RT CUSP SECTION FROM STATION 845 TO 905 IAW AARD 53-20-00-16, SRM 51-10-03-001, SRM 51-30-05 & DWG FDK 3203.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,092 hrs · 22,583 cycles

CORROSION LT CUSP STATION 1050 - 1057. INSTALLED CUSP DOUBLER REPAIR IAW AARD 53-20-00-16 & SRM 51-30-02.

Part: WEB — CRACKED (FUSELAGE) · airframe 46,092 hrs · 22,583 cycles

WEB IS CRACKED AT STATION 208 ABOVE L15L. INSTALLED REPAIR DOUBLER & FILLER IAW SRM 53-05-00-001 & SRM 51-60-00-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,092 hrs · 22,583 cycles

SEAT TRACK NR 6, CORROSION OUT OF LIMITS FROM STATION 384 - 385. INSTALLED SEAT TRACK PLUG IAW AARD 53-20-00-10.

Part: ENGINE — FOD (NR 1) · airframe 45,273 hrs · 22,107 cycles

DURING CLIMB, FLIGHT CREW REPORTED HOT PLASTIC, VARNISH ODOR & SMOKE IN COCKPIT. TURNED OFF RECIRCULATION FAN & SMOKE DISSIPATED. ATTEMPTED PACK BURNOUT PROCEDURE IAW AMM 21-20-02-201 DURING WHICH BLACK SMOKE & SPARKS WERE OBSERVED EXITING NR 1 ENGINE TAIL CONE. AIR INTERRUPT, EMERGENCY DECLARED, AND LANDING UNEVENTFUL. R & R NR 1 ENG IAW MCCS 71-91-99 & 7948. LEAK & PERFORMANCE RUN ACCOMPLISHED IAW MCC 71-91-03. SYS CHECKED NORMAL. DAMAGE FOUND TO LPC STAGE 6 & ALL HPC STAGE BLADES & STATORS, ATTRIBUTED TO FOD OF UNKNOWN ORIGIN.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 43,038 hrs · 20,896 cycles

AFT CARGO DOOR STOP CRACKED. R & R STOP IAW AARD 51-00-05-1.

Part: DOOR — CRACKED (NLG) · airframe 43,038 hrs · 20,896 cycles

LEFT AFT HOSE GEAR DOOR AFT HINGE CUT OUT CRACKED. INSTALLED DOUBLER IAW SRM 53-05-00-001 FIGURE 62.

Part: RIB — CRACKED (LT WING) · airframe 42,972 hrs · 20,853 cycles

CRACK IN THE LT WING NR 4 SLAT TRACK INBD SUPPORT RIB. INSTALLED REPAIR FITTING & HAT BUSHING.

Part: RIB — CRACKED (RT WING) · airframe 42,972 hrs · 20,853 cycles

CRACK IN THE RT WING NR 4 SLAT TRACK INBD SUPPORT RIB. INSTALLED REPAIR FITTING & HAT BUSHING.

Part: BATTERY PACK — OUT OF POSITION (AC BAY) · airframe 37,274 hrs · 17,936 cycles

TAIL COMPTMENT EMERGENCY LIGHTS ABOVE CATWALK INOPERATIVE. REPOSITIONED BATTERY PACK FOR TAIL COMPARTMENT EMERGENCY LIGHTS ABOVE CATWALK. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,162 hrs · 17,365 cycles

BOTH AFT OVERWING EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK FOR BOTH AFT OVERWING EXIT LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 35,602 hrs · 17,116 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS ABOVE CATWALK INOPERATIVE. RESEATED AFT BATTERY PACK. OPS CHECK NORMAL.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 35,073 hrs · 16,848 cycles

MID CARGO DOOR CENTER OF EXTERIOR SKIN BETWEEN NUMBER 4 AND 5 BEAM HAS SKIN DAMAGED AT 4 PLACES. REMOVED AND REPLACED OUTER DOOR SKIN PER ESO 80174.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,073 hrs · 16,848 cycles

CORROSION AT STATIONS 1212 TO 1220 TOP AND BOTTOM OF WEB AT AFT LOWER CORNER OF CARGO DOOR. INSTALLED NEW WEB SECTION PER AARD 53-10-00-24.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 35,073 hrs · 16,848 cycles

FORWARD FUSELAGE HAS A CRACK BEYOND STOP DRILL IN SKIN AT NOSE WHEEEL WEEL RIGHT AFT DOOR AFT HINGE CUTOUT. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-05 FIGURE 62.

Part: SKIN — DENTED (FUSELAGE) · airframe 35,073 hrs · 16,848 cycles

DENT LEFT FUSELAGE SKIN STATION 237 BETWEEN LONGERONS 17 AND 18 LEFT. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-04-00 FIGURE 12B.

Part: SKIN — DENTED (FUSELAGE) · airframe 35,073 hrs · 16,848 cycles

DENT IN FUSELAGE STATION 244, BETWEEN LONGERONS 17 AND 18 LEFT. INSTALLED REPAIR DOUBLER, FILLER MATERIAL AND FINGER DOUBLER PER SRM 53-04-00 FIGURE 12B SHEET 36.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,073 hrs · 16,848 cycles

G2 GALLEY FORWARD OUTBOARD MOUNT, STATION 215 RIGHT BUTTLINE 55 CORRODED. REPLACED MOUNT PER AARD 51-10-00-5.

Part: SKIN — CANNING (ENTRY DOOR) · airframe 35,073 hrs · 16,848 cycles

MAIN ENTRY DOOR OUTER SKIN HAS WAVINESS AND OIL CANNING AT BOTTOM. STRAIGHTENED LOWER EDGE OF DOOR SKIN IN AREAS OF WAVINESS. BLENDED TO REMOVE ROUGH EDGES OF SKIN. TREATED AND PRIMED AFFECTED AREA`S. FABRICATED AND INSTALLED REPAIR DOUBLER PER AARD 52-10-00-2 FIG 1.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,073 hrs · 16,848 cycles

DOUBLER ON SUBFLOOR, STATIONS 160 TO 180 RIGHT BUTTLINES 42 TO 57 CORRODED. INSTALLED NEW DOUBLER PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,073 hrs · 16,848 cycles

LEFT CUSP SHEET STATIONS 1174 TO 1250 CORRODED. REPLACED CUSP SHEET PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,073 hrs · 16,848 cycles

RIGHT CUSP STATIONS 878 TO 880 CORRODED. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 35,073 hrs · 16,848 cycles

INTERCOSTAL STATIONS 1287 TO 1307 BUTTLINE 0 AT FLOORLINE, CRACKED. REPLACED INTERCOSTAL PER AARD 51-10-00-5.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,073 hrs · 16,848 cycles

CORROSION ON SUBFLOOR, STATIONS 165 TO 195, LEFT BUTTLINES 48 TO 56. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — PUNCTURED (FUSELAGE) · airframe 35,073 hrs · 16,848 cycles

PUNCTURE IN SUBFLOOR STATION 158 RIGHT BUTTLINE 12. ROUTED OUT DAMAGED AREA AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,073 hrs · 16,848 cycles

CORRODED CUSP STATION 900. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,073 hrs · 16,848 cycles

CORRODED SUBFLOOR BELOW G1 GALLEY DRAIN PAN. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,073 hrs · 16,848 cycles

SUBFLOOR STATIONS 160 TO 200 RIGHT BUTTLINES 42 TO 57 CORRODED. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,073 hrs · 16,848 cycles

NUMBER 4 SEAT TRACK STATION 203 CORRODED. CUT OUT DAMAGED TRACK STATIONS 200 TO 266 AND ACCOMPLISHED SPLICE REPAIR PER SRM 53-05-00 FIGURE 4F.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,073 hrs · 16,848 cycles

RIGHT CUSP STATIONS 857 TO 858 CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 35,073 hrs · 16,848 cycles

DENT IN FUSELAGE STATION 1287, BETWEEN LONGERONS 27 AND 28 LEFT. INSTALLED DOUBLER PER SGO9530002 DRAWING ZONE76 AND SRM 53-04-03.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,073 hrs · 16,848 cycles

RIGHT CUSP SHEET, STATIONS 1060 TO 1079 CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 35,073 hrs · 16,848 cycles

INTERCOSTAL STATIONS 1271 TO 1287 BUTTLINE 0 AT FLOORLINE CRACKED. INSTALLED NEW INTERCOSTAL PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,073 hrs · 16,848 cycles

CORROSION ON CUSP SHEET AT STATION 1141 BELOW FORWARD GIRT BAR FITTING INBOARD MOUNT BOLT. INSTALLED 6AL-4V TITANIUM CUSP REPAIR DOUBLER AT STATION 1141 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,073 hrs · 16,848 cycles

CORROSION BEYOND MANUAL LIMITS AT RIGHT CUSP STATIONS 878 TO 880. INSTALLED RIGHT CUSP DOUBLER REPAIR AT STATIONS 878 TO 880 PER AARD 53-20-00-16.

Part: PAN — CRACKED (WINDOW) · airframe 35,073 hrs · 16,848 cycles

CRACK IN FORWARD UPPER WINDOW PAN BRACKET AT STATION 1098 RIGHT SIDE. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 35,073 hrs · 16,848 cycles

LEFT WINDOW PAN CRACKED AT STATION 1059, UPPER AFT CORNER. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 35,073 hrs · 16,848 cycles

LEFT WINDOW PAN CRACKED AT STATION 1040, UPPER AFT CORNER. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 35,073 hrs · 16,848 cycles

LEFT WINDOW PAN CRACKED AT STATION 1078, UPPER AFT CORNER. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 35,073 hrs · 16,848 cycles

LEFT WINDOW PAN CRACKED AT STATION 1021, UPPER AFT CORNER. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-10-00-25.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 34,944 hrs · 16,783 cycles

SEAT ROW 5 OVERHEAD EMERGENCY LIGHT INOPERATIVE. RESEATED BATTERY PACK FOR ROW 5 OVERHEAD EMERGENCY LIGHT. OPS CHECKS NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 34,944 hrs · 16,783 cycles

ROW 4 OVERHEAD CEILING LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER FOR ROW 4 OVERHEAD CEILING EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 34,944 hrs · 16,783 cycles

ROW 15 OVERHEAD EMERGENCY LIGHT INOPERATIVE. RESEATED BATTERY PACK FOR ROW 15 OVERHEAD EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 34,944 hrs · 16,783 cycles

ROW 16 EMERGENCY LIGHT INOPERATIVE. RESEATED BATTERY PACK FOR ROW 16 EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 34,944 hrs · 16,783 cycles

OVERHEAD EMERGENCY LIGHT BY RIGHT SIDE OF AFT LAVATORY INOPERATIVE. RESEATED BATTERY PACK FOR AFT CABIN OVERHEAD EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 34,944 hrs · 16,783 cycles

ROW 7 EMERGENCY OVERHEAD LIGHT INOPERATIVE. RESEATED BATTERY PACK FOR ROW 7 EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: A/C PACK — DIRTY (AC BAY) · airframe 34,316 hrs · 16,457 cycles

ORD - FLIGHT ATTENDANTS REPORTED DURING CLIMBOUT ELECTRICAL ODOR. EMERGENCY DECLARED, FLIGHT RETURNED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED PACK BURN AND FUNCTIONAL CHECK FLIGHT WITH NO SMOKE OR ODOR NOTED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: UPLOCK SENSOR — FAULTY (NLG) · airframe 31,311 hrs · 15,001 cycles

DFW - CREW REPORTED NOSE GEAR UNSAFE INDICATION ILLUMINATED WITH GEAR HANDLE IN UP POSITION. FLIGHT RETURNED DFW GEAR EXTENDED AND HAD THREE GREEN DOWN/LOCKED INDICATIONS AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SEVICE. REPLACED UPLOCK SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 31,310 hrs · 15,000 cycles

LONGERON 20 LEFT CRACKED AT LOWER FORWARD FASTENER HOLE TO EDGE. INSTALLED DOUBLER AT LONGERON 20 LEFT PER AARD 53-10-00-18.

Part: CONTROL VALVE — FAILED (AC SYSTEM) · airframe 30,447 hrs · 14,626 cycles

CREW REPORTED UNABLE TO PRESSURIZE AIRCRAFT. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED LEFT AIR CONDITIONING FLOW CONTROL VALVE AND RIGHT AIR CONDITIONING PRESSURE REGULATOR SHUT OFF VALVE.

Part: LENS — BROKEN (CABIN)

DFW - EMERGENCY LIGHT AT AFT LEFT OVERWING EXIT SIGN HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT AFT LEFT OVERWING EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 16D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 9D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 9D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACTUATOR — INOPERATIVE (RT MLG)

MCI - INFLIGHT T1926 - TUS TO ORD - RED GEAR DOOR LIGHT REMAINED ON WITH GEAR HANDLE UP. CYCLED GEAR AND RED GEAR DOOR LIGHT REMAINED ON. LANDED MCI WITHOUT INCIDENT. REPLACED RIGHT GEAR ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SEAL — INOPERATIVE (NLG STRUT)

DTW INFLIGHT T2265/02FEB - NOSE LANDING GEAR FAILED TO RETRACT. RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING HEAR SHOCK STRUT SEAL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS AT FORWARD AND AFT CABIN INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS AT FORWARD AND AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SFO - OVERHEAD EMERGENCY LIGHTS AT SEAT 3E INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT SEAT 3E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SFO - CEILING EMERGENCY LIGHTS AT SEAT ROW 23 INOPERATIVE. REPLACED BATTERY PACK AT 23D FOR CEILING EMERGENCY LIGHTS AT SEAT ROW 23. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: OVEN — FIRE (GALLEY)

IAH INFLIGHT T1383/26AUG - RESIDUE IN LEFT OVEN IN FORWARD GALLEY CAUGHT FIRE. FLIGHT ATTENDANT CLOSED OVEN DOOR AND FIRE EXTENGUISHED. CLEANED LEFT HEAD OVEN IN FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

AUS - CEILING EMERGENCY LIGHTS AT ROWS 28 THROUGH 31 INOPERATIVE. REPLACED BATTERIES FOR CEILING EMERGENCY LIGHTS AT ROWS 28 THROUGH 31. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

MIA - CEILING EMERGENCY LIGHTS AT COCKPIT TO ROW 7D INOPERATIVE. REPLACED BATTERY FOR CEILING EMERGENCY LIGHTS AT COCKPIT TO ROW 7D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,110 hrs · 6,050 cycles

THREE EGRESS LAMPS WERE INOPERATIVE AT THE FLOOR BETWEEN FIRST CLASS AND COACH. REPLACED ONE LAMP, REPLACED ONE COVER, AND RE-INSERTED LAMP AT ROW 5. CHECK-C 6-7-02 STL.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 10,956 hrs · 5,965 cycles

DURING OVERNIGHT INEPECT EMERGENCY LITE COVER AT 3E MISSING. REPLACED EMERGENCY LITE COVER AT 3E. PERF OPS CHECK PER MM 33-53-00. CHECK-C 6-07-02 STL. --CLOSED--

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 10,956 hrs · 5,965 cycles

DURING OVERNITE INSPECT EMERGENCY LITE AT 27D INOP. RE-INSTALLED LITE BULB AT 27D. OPS CHECK NORMAL PER MM 33-53-00. CHECK-C 6-7-02 STL. --CLOSED--

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 10,811 hrs · 5,879 cycles

THE FIRST FOUR EGRESS LIGHTS IN THE FIRST CLASS CABIN WERE INOPERATIVE. RESEATED THE ELECTRICAL CONNECTOR AT ROW 3 AND 4. CHECK-C 6-7-02 STL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 10,424 hrs · 5,674 cycles

THE EGRESS LIGHTS WERE INOPERATIVE FROM ROW 26 TO 29. FOUND ELECTRICAL CONNECTOR AT ROW 29 WAS LOOSE. TIGHTENED CONNECTOR.

Part: LAMP — BURNED OUT · airframe 9,079 hrs · 4,844 cycles

LOWER TAILCONE EMERGENCY LIGHTING INOP. RELAMPED LIGHT ASSEMBLY. LAST CHECK C PERFORMED IN STL 03/23/2001 --CLOSED--

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 9,079 hrs · 4,844 cycles

THE EMERGENCY OVERHEAD LIGHTS WERE INOPERATIVE AT ROW 19 AND 22. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 3-23-01 STL. --CLOSED--

Part: BULB — BURNED OUT (TAIL CONE) · airframe 9,079 hrs · 4,844 cycles

THE OVERHEAD CENTER EMERGENCY LIGHT IN THE TAIL CONE AREA, AND THE EGRESS LIGHT AT ROWS 7 AND 31, WERE INOPERATIVE. REPLACED THE BULB PN 1315 IN TAIL CONE AREA, AND REPLACED THE BULB PN 7732 AT BOTH ROWS 7 AND 31. CHECK-C 3-23-01 STL. --CLOSED--

Part: LAMP — UNSECURE · airframe 9,079 hrs · 4,844 cycles

EGRESS LIGHTING AT ROW 28 INOP. RESEATED LAMP IN SOCKET. LAST CHECK C PERFORMED IN STL 03/23/2001. --CLOSED--

Part: BATTERY PACK — DISCHARGED · airframe 9,079 hrs · 4,844 cycles

EMERGENCY OVERHEAD LIGHTS AT ROW 19 INOP. REPLACED BATTERIES IN BATTERY PACK. LAST CHECK C PERFORMED IN STL 03/23/2001 --CLOSED--

Part: BATTERY — DISCHARGED (CABIN) · airframe 9,079 hrs · 4,844 cycles

THE RT AND LT SIDE EMERGENCY OVERWING EXIT LIGHTS WERE INOPERATIVE. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 3-23-01 STL. --CLOSED--

Part: CONNECTOR — LOOSE (CABIN) · airframe 7,805 hrs · 4,097 cycles

THE EGRESS LIGHTS WERE INOPERATIVE FROM ROW 26 THROUGH 29. SECURED A LOOSE CONNECTION AT ROW 29.

Part: LAMP · airframe 7,746 hrs · 4,059 cycles

THE RED EGRESS LIGHT AT ROW 28 WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 3-23-01 STL. --CLOSED--

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 7,677 hrs · 4,021 cycles

THE CABIN EMERGENCY LIGHTS WERE INOPERATIVE FROM ROW 1 TO 20. REPLACED THE POWER SUPPLY, AND THE EMERGENCY SWITCH.

Part: BATTERY PACK (TAIL COMPT) · airframe 6,610 hrs · 3,426 cycles

THREE EMERGENCY LIGHTS IN THE TAIL COMPT WERE INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 3-23-01 STL. --CLOSED--