N357AA

Part: FRAME — CRACKED (RT PYLON) · airframe 106,816 hrs · 17,422 cycles

FOUND SMALL CRACK ON THE RT ENG PYLON NAC STATION 285 INBD FRAME. R & R RT ENG PYLON INBD FRAME AT NAC STATION 285 IAW AARD 51-00-005-1.

Part: INDICATION SYS — MALFUNCTIONED (FUEL SYSTEM) · airframe 106,556 hrs · 17,378 cycles

INFLIGHT CREW REPORTED TWO HOURS 30 MINS INTO FLIGHT LT WING IS LIGHT 1000 LBS, FUEL SCORE IS DOWN 2000 LBS. LT ENG IS BURNING 200 LBS PER HR LESS THAN RT ENG & RUNNING COOLER. EMER DECLARED FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND FUEL QTY WITHIN ALLOWABLE LIMITS. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 105,826 hrs · 17,269 cycles

LEFT AFT INTERIOR, OVERWING LOWER EXIT SIGN INOPERATIVE. REPLACED LAMP FOR LT AFT INTERIOR, OVERWING LOWER EXIT SIGN. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 105,826 hrs · 17,269 cycles

RED EMERGENCY LIGHT AT SEAT 20H INOPERATIVE. REPLACED LAMP FOR RED EMERGENCY LIGHT AT SEAT 20H. OPERATIONS CHECKED NORMAL.

Part: PUMP — INOPERATIVE (RT ENGINE) · airframe 104,975 hrs · 17,134 cycles

TUL DURING FCF RT ENG WAS SHUT DOWN & WOULD NOT RESTART DURING FLIGHT. RT ENG FUEL VLV IS ILLUMINATED STEADY WITH FUEL SWITCH IN THE RUN POSITION. ALSO FUEL FLOW INDICATED "0000" FUEL FLOW. FLIGHT LANDED TUL WITHOUT INCIDENT. REPLACED RT ENG FUEL PUMP. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 104,973 hrs · 17,132 cycles

SKIN PANEL FROM STATIONS 420 TO 445 & STRINGERS 33 TO 35 LT DAMAGED. INSTALLED DOUBLER IAW EA B767-53-033867.

Part: SKIN — DENTED (FUSELAGE) · airframe 104,973 hrs · 17,132 cycles

SKIN AT STATION 1522 & STRINGERS 27 TO 29 RT DENTED. REMOVED DAMAGE AREA & INSTALLED DOUBLER IAW SRM 53-00-01 & EA B767-53-033833.

Part: SKIN — DENTED (FUSELAGE) · airframe 104,973 hrs · 17,132 cycles

DENT IN FUSELAGE FROM STATIONS 1509 TO 1603 AT STRINGER 29 RT. INSTALLED EXTERNAL DOUBLER IAW SRM 53-00-01-2R-1.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 104,973 hrs · 17,132 cycles

RT NR 4 DOOR EXTERNAL LIGHT DID NOT ILLUMINATE, REPLACED LAMP FOR RT NR 4 DOOR EXTERNAL EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 104,067 hrs · 16,994 cycles

SEAT 28H EMERGENCY LIGHT INOPERATIVE. RECONNECTED LOOSE CONNECTOR, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 103,923 hrs · 16,971 cycles

ESCAPE PATH MARKER MOUNTED TO FS3 LAVATORY LOWER WALL INOPERATIVE. REPLACED LAMP FOR ESCAPE PATH MARKER MOUNTED TO FS3 LAVATORY LOWER WALL. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 103,923 hrs · 16,971 cycles

CEILING MOUNTED ESCAPE PATH ILLUMINATION LIGHT BETWEEN SEATS 37BC INOPERATIVE. REPLACED LAMP FOR CEILING MOUNTED ESCAPE PATH ILLUMINATION LIGHT BETWEEN SEAT 37BC. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 103,923 hrs · 16,971 cycles

RT NR 2 EMERGENCY EXIT SIGN HANDLE ILLUMINATION LIGHT INOPERATIVE. REPLACED LAMP FOR RT NR 2 EMERGENCY EXIT SIGN HANDLE ILLUMINATION LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 103,923 hrs · 16,971 cycles

INTERIOR LT OVERWING AFT DOOR LOWER EXIT MARKER INOPERATIVE. REPLACED LAMP FOR INTERIOR LT OVERWING AFT DOOR LOWER EXIT MARKER. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 103,923 hrs · 16,971 cycles

INTERIOR RT OVERWING AFT DOOR LOWER EXIT MARKER INOPERATIVE. REPLACED LAMP FOR INTERIOR RT OVERWING AFT DOOR LOWER EXIT MARKER. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 103,923 hrs · 16,971 cycles

LT NR 1 EMERGENCY EXIT SIGN HANDLE ILLUMINATION LIGHT INOPERATIVE. REPLACED LAMP. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 103,923 hrs · 16,971 cycles

LT NR 2 EMERGENCY EXIT SIGN HANDLE ILLUMINATION LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 2 EMERGENCY EXIT SIGN HANDLE ILLUMINATION LIGHT. OPERATIONS CHECKED NORMAL.

Part: SPLICE — DAMAGED (FUSELAGE) · airframe 103,500 hrs · 16,894 cycles

BUTT SPLICE AT STATION 654 DAMAGED. REPLACED BUTT SPLICE.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 103,500 hrs · 16,894 cycles

STRINGER 36 LT FROM STATIONS 626 TO 654 DAMAGED. REPLACED STRINGER.

Part: FRAME SPLICE — DAMAGED (FUSELAGE) · airframe 103,500 hrs · 16,894 cycles

DAMAGED FRAME SPLICE AT STATION 632. REPLACED FRAME SPLICE.

Part: STRINGER SPLICE — DAMAGED (FUSELAGE) · airframe 103,500 hrs · 16,894 cycles

STRINGER SPLICE DAMAGED AT STATION 654 & STRINGER 39 LT. REPLACED STRINGER SPLICE.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 103,500 hrs · 16,894 cycles

STRINGER 37 RT FROM STATIONS 626 TO 654 DAMAGED. REPLACED STRINGER.

Part: STRINGER SPLICE — DAMAGED (FUSELAGE) · airframe 103,500 hrs · 16,894 cycles

STRINGER SPLICE AT STATION 654 & STRINGER 38 LT DAMAGED. REPLACED STRINGER SPLICE.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 103,500 hrs · 16,894 cycles

STRINGER 38 RT FROM STATIONS 626 TO 654 DAMAGED. REPLACED STRINGER.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 103,500 hrs · 16,894 cycles

FRAME & ASSOCIATED STRUCTURE AT STATION 632 SUSTAINING HEAT DAMAGE FROM CARGO FIRE. REPLACED FRAME & ASSOCIATED STRUCTURE IAW SRM 51-40-02-0G, AARD 51-00-05-1 & DRAWING 143T1209.

Part: TEAR STRAP — DAMAGED (FUSELAGE) · airframe 103,500 hrs · 16,894 cycles

TEAR STRAP AT STATION 632 & STRINGERS 36 LT & RT DAMAGED. REPLACED TEAR STRAP.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 103,500 hrs · 16,894 cycles

DAMAGED STRINGER 37 LT FROM STATIONS 626 TO 654. REPLACED STRINGER.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 103,500 hrs · 16,894 cycles

FIRE DAMAGE TO AIRCRAFT SKIN FROM STATIONS 632 TO 654 & STRINGERS 35 LT & 36 RT. CUT OUT AREA & INSTALLED DOUBLER & TRIPLER.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 103,500 hrs · 16,894 cycles

CORRODED FLOOR PANEL AT STATION 481. REPLACED PANEL.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 103,500 hrs · 16,894 cycles

STRINGER DAMAGED AT STATION 654 & STRINGER 39 RT. REPLACED STRINGER.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 103,500 hrs · 16,894 cycles

STRINGER DAMAGED AT STATION 626 TO 654 & STRINGER 35 LT. STRINGER REPLACED.

Part: WEB — DAMAGED (FUSELAGE) · airframe 103,500 hrs · 16,894 cycles

WEB ASSEMBLY AT STATION DAMAGED. REPLACED WEB ASSEMBLY.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 103,500 hrs · 16,894 cycles

PDU MOUNT FRAME IN FWD CARGO DAMAGED FROM CARGO FIRE. REPLACED PDU MOUNT FRAME IAW AARD 51-00-05 REPAIR 1 & EA B767-53-031331.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 103,500 hrs · 16,894 cycles

PDU MOUNT FRAME IN FWD CARGO DAMAGED FROM CARGO FIRE. REPLACED PDU MOUNT FRAME IAW AARD 51-00-05 REPAIR 1 & EA B767-53-031331.

Part: PAN — DAMAGED (FUSELAGE) · airframe 103,500 hrs · 16,894 cycles

PDU PAN ASSEMBLY DAMAGED DUE TO CARGO FIRE. REPLACED PDU PAN ASSEMBLY SUPPORT STRUCTURE IAW AARD 51-00-05-1 & EA B767-53-031278 & DRAWING 451T2451.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 103,500 hrs · 16,894 cycles

FLOOR SUPPORT WEB & EXTRUSION DAMAGED FROM CARGO FIRE. REPLACED FLOOR SUPPORT WEB & EXTRUSION IAW SRM 51-70-12 & SRM 51-70-13.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 103,500 hrs · 16,894 cycles

INTERCOSTAL FROM STATIONS 610 TO 632 CORRODED. REPLACED INTERCOSTAL.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 103,500 hrs · 16,894 cycles

FIRE RELATED DAMAGE TO STRINGER 36 RT BETWEEN STATIONS 600 & 654. ACCOMPLISHED DOUBLER REPAIR IAW SRM 53-00-03 & EA B767-53-030963.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 103,500 hrs · 16,894 cycles

CARGO FLOOR PANEL AT STATION 481.6 CORRODED. REPLACED FLOOR PANEL.

Part: SKIN — GOUGED (FUSELAGE) · airframe 99,960 hrs · 16,329 cycles

TWO GOUGES IN FUSELAGE UPPER CROWN SKIN, STATIONS 855 TO 861, JUST BELOW STRINGER 5 RIGHT. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-00-01-2R REPAIR 1 AND EA B767-53-025449.

Part: SKIN — GOUGED (FUSELAGE) · airframe 99,960 hrs · 16,329 cycles

GOUGES IN FUSELAGE UPPER CROWN SKIN, STATION 835, BETWEEN STRINGERS 3 AND 4 RIGHT. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-00-01-2R REPAIR 1 AND EA B767-53-025449.

Part: SKIN — GOUGED (FUSELAGE) · airframe 99,960 hrs · 16,329 cycles

GOUGE IN FUSELAGE UPPER CROWN SKIN, STATION 886, BETWEEN STRINGERS 4 AND 5 RIGHT. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-00-01-2R REPAIR 1 AND EA B767-53-025449.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,960 hrs · 16,329 cycles

SKIN CORROSION AT STATION 434 BETWEEN STRINGERS 33 TO 35 LEFT. INSTALLED EXTERNAL DOUBLER PER EA B767-53-015392.

Part: TEAR STRAP — DAMAGED (FUSELAGE) · airframe 99,960 hrs · 16,329 cycles

TEAR STRAP AT STATION 1241 BELOW STRINGER 36 LEFT DAMAGED. SPLICE REPAIR OF TEAR STRAP.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,960 hrs · 16,329 cycles

CORROSION ON LAP SEAM, STATION 1241 AT STRINGER 36 LEFT. CUT OUT DAMAGE AND INSTALLED EXTERNAL DOUBLER PER SRM 53-00-01-2R.

Part: WEB — CRACKED (LT PYLON) · airframe 99,960 hrs · 16,329 cycles

LEFT PYLON UPPER TORQUE BOX FEEDER CABLE THRU HOLE CRACKED. INSTALLED DOUBLER REPAIR PER AARD 54-52-01-1.

Part: SKIN — DEBONDED (TE FLAP) · airframe 99,960 hrs · 16,329 cycles

LEFT OUTBOARD FLAP LOWER SURFACE DISBONDED. ACCOMPLISHED BONDED REPAIR PER SRM 57-53-01.

Part: SKIN — DAMAGED (TE FLAP) · airframe 99,960 hrs · 16,329 cycles

HAIL DAMAGE ON RIGHT OUTBOARD FLAP UPPER SURFACE. ACCOMPLISHED BONDED REPAIR PER SRM 57-53-01.

Part: SKIN — DAMAGED (TE FLAP) · airframe 99,960 hrs · 16,329 cycles

HAIL DENT TO LEFT OUTBOARD UPPER SURFACE. ACCOMPLISHED BONDED REPAIR PER SRM 57-53-01.

Part: FIRE LOOP — FAULTY (LT ENGINE) · airframe 99,836 hrs · 16,309 cycles

LAX - INFLIGHT DFW-OGG. CREW REPORTED A FIRE LOOP WARNING DURING CRUISE. EMERGENCY DECLARED FLIGHT DIVERTED LAX LANDED WITHOUT INCIDENT. AIRCRACFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE LOWER AFT LOOP ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 98,043 hrs · 15,992 cycles

SEAT MOUNTED EMERGENCY LIGHTS FROM ROWS 20AB TO 24AB INOPERATIVE. REPLACED BATTERY PACK.

Part: WIRE — LOOSE (CABIN) · airframe 96,733 hrs · 15,796 cycles

EMERGENCY EXIT LIGHT AT 28DEF FAILED TO ILLUMINATE. RECONNECTED LOOSE WIRE AT LIGHT ASSY, OPS CHECK NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 96,448 hrs · 15,754 cycles

SEAT MOUNTED EMERGENCY LIGHT AT 17 H/J INOPERATIVE. REPAIRED BROKEN WIRE AT 17 H/J. OPS CHECK NORMAL.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 95,893 hrs · 15,657 cycles

DFW - CREW REPORTED CENTER SYSTEM HYDRAULIC AIR DRIVEN PUMP FAILED INFLIGHT. NO FLUID LOSS REPORTED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. PLACARD AIR DRIVEN PUMP INOPERATIVE PER MEL. REPLACED ADP AT JFK ON 07/26/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: APU — FAILED (APU BAY) · airframe 95,212 hrs · 15,555 cycles

DURING BOARDING THE AUXILIARY POWER UNIT FAILED CAUSING THE CABIN AND COCKPIT TO FILL WITH SMOKE. PASSENGERS WERE EVACUATED WITH NO INJURIES REPORTED. AIRCRAFT REMOVED FROM SERVICE. REPLACED AUXILIARY POWER UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SENSOR — INOPERATIVE (BLEED AIR SYS) · airframe 94,815 hrs · 15,497 cycles

HNL - CREW REPORTED RIGHT ENGINE BLEED AIR OVERHEAT MESSAGE ON EICAS. EMERGENCY DECLARED FLIGHT RETURNED HNL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE FAN AIR TEMP SENSOR, FAN AIR VALVE AND OVERHEAT SWITCH S359. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SILL — CORRODED (FUSELAGE) · airframe 94,684 hrs · 15,465 cycles

BULK CARGO DOOR CUTOUT LOWER SILL INNER CHORD HAD CORROSION. ACCOMPLISHED REPAIR PER EA B767-53-015443.

Part: SKATE ANGLE — CRACKED (LT NACELLE) · airframe 94,687 hrs · 15,467 cycles

IN LINE CRACK IN THE LEFT OUTBOARD NACELLE SKATE ANGLE FOR THE AFT FAIRING. ACCOMPLISHED REPAIR PER EA B767-64-005449.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,687 hrs · 15,467 cycles

CORROSION OF THE FUSELAGE SKIN INNER SURFACE AT STATION 439 AND UNDER STRINGER 34 LEFT. ACCOMPLISHED DOUBLER REPAIR PER EA B767-53-015392.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 94,687 hrs · 15,467 cycles

STATION 1809 BULKHEAD FORWARD OUTER CHORD HAD 4 HOLE CRACKS. ACCOMPLISHED REPAIR PER EA 767-53-01-5391,

Part: SKIN — DELAMINATED (LE SLAT) · airframe 94,687 hrs · 15,467 cycles

DELAMINATION OF NUMBER 6 SLAT LOWER SKIN 3 INCHES INBOARD OF THE OUTBOARD EDGE. ACCOMPLISHED REPAIR PER EA COMP-57-01-5569.

Part: FRAME — DENTED (FUSELAGE) · airframe 94,687 hrs · 15,467 cycles

DENT DAMAGE TO THE STATIONS 500 AND 522 FUSELAGE FRAME INNER CHORD BETWEEN STRINGERS 29 TO 31 LEFT. ACCOMPLISHED REPAIR PER EA B767-53-015336.

Part: WEDGE — DENTED (LE SLAT) · airframe 94,687 hrs · 15,467 cycles

NUMEROUS DENTS ON ALL 12 WING LEADING EDGE SLAT WEDGES. ACCOMPLISHED REPAIR PER EA B767-57-015326.

Part: PUMP — INOPERATIVE (FUEL SYSTEM) · airframe 93,909 hrs · 15,338 cycles

SFO - INFLIGHT DFW-HNL. CREW REPORTED IN CRUISE THE LEFT AFT FUEL BOOST PUMP PRESSURE LIGHT ILLUMINATED AND EICAS MESSAGE ALSO ILLUMINATED. EMERGENCY DECLARED FLIGHT DIVERTED SFO LANDED WITHOUT INCIDENT. DURING TROUBLESHOOTING FOUND A PUSHED BACK ELECTRICAL PIN ON THE BOOST PUMP. REPLACED THE PUMP AND THE LOW PRESSURE SWITCH. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: GENERATOR — FAILED (RT ENGINE) · airframe 93,837 hrs · 15,323 cycles

DFW - CREW REPORTED RIGHT GENERATOR FAILED ON CLIMBOUT. EMERGENCY DECLARED, RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SWITCH — FAULTY (BLEED AIR SYS) · airframe 91,794 hrs · 14,975 cycles

LAX INFLIGHT DFW-HNL. CREW REPORTED DURING CLIMB EICAS MESSAGE "LEFT ENGINE BLEED OVERHEAT" INDICATION CAME ON. EMERGENCY DECLARED FLIGHT DIVERTED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BLEED SWITCH AND LEFT FAN AIR VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: UNKNOWN — FIRE (LAVATORY)

FIRE REPORTED IN WATER HEATER COMPARTMENT IN M1 LAVATORY WHILE IN FLIGHT. FLIGHT CREW USED ALL WATER FIRE EXTINGUISHERS AND HALON BOTTLE TO EXTINGUISH FIRE. AIRCRAFT MADE AN UNSCHEDULED LANDING AT HALIFAX NS, CANADA. AIRCRAFT IS SCHEDULED FOR FERRY FLIGHT TO AFW AFTER ACCOMPLISHMENT OF PRE-FERRY BOW FOR FURTHER INSPECTION AND REPAIRS OF DAMAGED AREA'S.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 87,478 hrs

SFO - EMERGENCY LIGHT BATTERY PACK FOR SEAT ROWS RIGHT 10 TO 17 HAS FUSE BLOWN. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SEAL — LEAKING (NR 2 ENG GEARBOX) · airframe 87,160 hrs

INFLIGHT FCF - APPROXIMATELY FIVE MINUTES AFTER LEVEL OFF AT 40000 FEET OIL QUANTITY INDICATION ILLUMINATED OR NUMBER TWO ENGINE THEN WENT RAPIDLY TO ZERO. OIL PRESSURE BEGAN TO DROP AND OIL TEMPERATURE BEGAN TO RISE. REDUCED ENGINE TO IDLE. ON DESCENT OIL QUANTITY BEGAN TO RISE AND OIL PRESSURE AND TEMPERATURE NORMALIZED. OIL TEMPERATURE OR PRESSURE NEVER WENT TO AMBER BAND. NO EICAS MESSAGE ON OIL QUANTITY. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE ON 25 NOV AT JFK DUE TO INLET GEARBOX SEAL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — MALFUNCTIONED (FUEL SYSTEM) · airframe 84,872 hrs

JFK INFLIGHT T92/28APR ORD TO DUB - CREW REPORTED LEFT AFT FUEL BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED AND CIRCUIT BREAKER POPPED. LANDED JFK WITHOUT INCIDENT. REPLACED LEFT AFT FUEL BOOST PUMP.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 84,821 hrs · 13,813 cycles

AFW - FUSELAGE STRINGER 35L AT STATION 1307 HAD CORROSION. REPAIRED FUSELAGE STRINGER 35L AT STATION 1307 PER MRB 767 3181 DATED 08 APR 2008.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHT AT OVERHEAD A6 LAVATORY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD A6 LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HANDLE — INOPERATIVE (EMERGENCY EXIT)

CDG - FOUND EMERGENCY EXIT HANDLE AT SEAT 20J PANEL INOPERATIVE. REINSTALLED EMERGENCY EXIT HANDLE AT SEAT 20J PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - OUTSIDE EMERGENCY LIGHTS ON RIGHT SIDE OF CABIN INOPERATIVE. REPLACED BATTERY PACK AND CHARGER M733 FOR OUTSIDE EMERGENCY LIGHTS ON RIGHT HAND SIDE OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN)

DFW - EMERGENCY PATH LIGHT AT SEAT 25H INOPERATIVE. RESEATED EMERGENCY LIGHT CONNECTOR AT SEAT 25H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — DAMAGED (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 41B HAS DAMAGED LENS. REPLACED EMERGENCY LIGHT LENS AT SEAT 41B. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - EMERGENCY LIGHTS FROM 20AB TO 24AB SEATS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FORM 20AB TO 24AB SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (CABIN)

ORD - LEFT OVERWING SLIDE SQUIB DOES NOT TEST IN COCKPIT. REPLACED M961 AND M962 BATTERY PACKS FOR LEFT OVERWING SLIDE SQUIB IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FASTENER — CRACKED (WING FUEL TANK)

AFW - SEVEN LOCK FASTENER COLLARS CRACKED INSIDE FUEL TANKS AT WING STATION 261.2 LEFT HAND 394.2 LEFT HAND, 308.1 RT, 798.2 RIGHT HAND. REPLACED SEVEN EACH LOCK FASTENER COLLARS. NO LOOSE OR LEAKING LOCK FASTENERS AFTER REPLACEMENT OF COLLARS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FLOORBEAM — CORRODED (FUSELAGE)

AFW - FLOORBEAM AT STATION 325 (GENERAL LOCATION SECTION 41) HAS CORROSION REMOVAL ON UPPER SURFACE. MATERIAL REMAINING IS BEYOND SRM LIMITS. AREA IS 1.0 INCH BY 1.0 INCH WITH A DEPTH OF .026 INCHES. COMPLETELY REMOVED CORROSION AND ENSURED BLEND AREA WAS CRACK FREE. REFINISHED BLEND AREA WITH ALODINE AND TWO COATS BMS1011 PRIMER. FILLED BLEND WITH BMS595. AIRCRAFT RETURNED TO SERVICE WITH NOTED CONDITION.

Part: LONGERON — CRACKED (FUSELAGE)

AFW - RIGHT HAND UPPER LONGERON WEB AT STRINGER 12 RIGHT JUST FORWARD OF STATION 1809 CRACKED. CUT OUT DAMAGED WEB AT APPROXIMATELY STATION 1798 AND FABRICATED A REPAIR WEB FROM .032 7075T6 CLAD. DOUBLER FROM .040 7075T6 CLAD AND FILLER FROM 0.080 7075T6 AND MACHINE SPLICE. ALODINE AND PRIME ALL ALUMINUM SURFACES PER 767 SRM. INSTALLED WEB SPLICES WITH BMS595 SEALANT AND INSTALLED BACR15FTC7K6 AT ALL RIVET LOCATIONS AND BACB30VT OR BACB30NX AT ALL HIL OK LOCATIONS IN TRANSITION FIT.

Part: LIGHT — DAMAGED (SEAT 36H)

DFW - EMERGENCY EXIT LIGHT AT SEAT 36H DAMAGED. REPAIRED EMERGENCY LIGHT AT SEAT 36H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TERMINAL — SMOKE (WINDSHIELD)

EZE - TEN MINUTES AFTER TAKEOFF STRONG ELECTRICAL SMOKE SMELL IN COCKPIT. PERFORMED ELECTRICAL FIRE AND SMOKE EMERGENCY CHECKLIST BUT SMOKE NEVER ABATED. RETURNED TO EZE AND LANDED WITHOUT INCIDENT. FOUND SOURCE OF SMOKE IN J5 TERMINAL AT RIGHT HAND WINDSHIELD. REPLACED RIGHT HAND WINDSHIELD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN)

EMERGENCY LIGHT AT SEAT 35H INOPERATIVE. FOUND LOOSE CONNECTOR. TIGHTENED AND SECURED EMERGENCY LIGHT CONNECTOR AT SEAT 35H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN)

DFW - EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 17H. BATTERY PACK FAILED DUAL FEED CHECK. CONNECTED SEAT WIRING CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FOUND EXTERNAL EMERGENCY EXIT LIGHTS LEFT OVERWING, ALL THREE ARE INOPERATIVE. ALSO, 1L EXT EMERGENCY EXIT LIGHT IS INOPERATIVE. REPLACED M736 AND OPS CHECKED OK. (M)

Part: TRANSCEIVER — INOPERATIVE (WEATHER RADAR)

FLT 1539 - MIA-SFO - WEATHER RADAR INOPERATIVE. AIRCRAFT RETURNED MIA AND LANDED WITHOUT INCIDENT. REPLACED WEATHER RADAR TRANSCEIVER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TRANSCEIVER — FAILED (WX RADAR SYSTEM)

WEATHER RADAR DISPLAYED RT WEAK AND THEN WX FAIL BOTH SIDES, RADAR WAS COMPLETELY INOPERATIVE. REMOVED ND REPLACED WX RADAR TRANSCEIVER AS PER MM ACCOMPLISHED REQ'D TESTS, ALL CHECKS NORMAL. (M)

Part: CONNECTOR (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS BEHIND SEAT 3AB INOPERATIVE. RESECURED CONNECTOR AT SEAT 3AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: INDICATOR — MALFUNCTIONED (HYDRAULIC SYS)

DFW - FLT 78 - AFTER TAKEOFF, HYDRAULIC QUANTITY EICAS MESSAGE ILLUMINATED AND QUANTITY INDICATION SHOWED OO RF. RETURNED AND LANDED DFW WITHOUT INCIDENT. REPLACED HYDRAULIC MONITOR UNIT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, RIGHT AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED RIGHT AFT SERVICE DOOR EXERIOR EMERGENCY LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — FAILED (ROW 26)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEAT/ROW 26AB INOPERATIVE. REPLACED WIRING FOR EMERGENCY EXIT PATH LIGHT AT SEAT/ROW 26AB SYSTEM GROUND CHECK, NORMAL OPERATION. (X)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT SEAT LIGHT AT 24H INOPERATIVE. REPAIRED CONNECTOR WIRE AT SEAT 24H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DAMAGED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTS AT SEATS 26H AND 31H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECTORS AT SEATS 26H AND 31H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: AIR DISTRIBUTION — ODOR (CABIN)

MIA - FLT 596 - AFTER TAKEOFF MIA DURING CLIMB-OUT, SLIGHT SMOKE AND OIL ODOR NOTED IN AREA OF PAX SEAT ROWS 25 AND 26 WITH NO OTHER ABNORMAL INDICATIONS. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. ACCOMPLISHED GROUND ENGINE RUN AT TAKEOFF POWER SETTINGS AND OPERATED BOTH PACKS FULL RANGE WITH ENGINES AND APU WITH NO SMOKE OR ODOR NOTED. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO SMOKE OR ODOR NOTED. SYSTEMS OPERATIONAL CHECKED NORMAL. UNABLE TO DUPLICATE PROBLEM AND AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT ON PAX SEAT 29H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR ON PAX SEAT 29H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH — DEFECTIVE (CABIN)

DFW - FLT 79 - AFTER TAKEOFF LGW DURING CLIMB TO CRUISE ALTITUDE, EMERGENCY EXIT AND PATH LIGHTING BEGAN OPERATING INTERMITTENTLY. AFTER 20 MINUTES OF INTERMITTENT OPERATION, LIGHTS EXITNGUISHED AND COULD NOT BE ILLUMINATED WITH EITHER COCKPIT SWITCH OR AT F/A STATION. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED EMERGENCY LIGHT TEST SWITCH AT AFT RIGHT SIDE FLIGHT ATTENDANTS PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 27H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 27H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — FAILED (CABIN)

SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT LIGHT AT 24H INOPERATIVE. REPAIRED CONNECTOR, SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL ASSY — DEFECTIVE (MID-GALLEY)

SFO - DURING OVERNIGHT CHECK, MID-GALLEY EMERGENCY LIGHT LEFT SIDE OF LAMP INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT MID-GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS UNDER AFT FLIGHT ATTTENDANT SEATS INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR UNDER AFT FLIGHT ATTENDANT SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)

Part: OVEN — DIRTY (GALLEY)

LHR - FLT 108 - EN ROUTE BOS-LHR - DURING CRUISE, FIRST CLASS GALLEY OVEN EMITTED SMOKE FROM INSIDE OVEN COMPARTMENT DURING USE. NO OTHER ABNORMAL INDICATIONS. AIRCRAFT PROCEEDED LHR AND LANDED WITHOUT INCIDENT. CLEANED INTERIOR OF FIRST CLASS GALLEY OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)

Part: EEL STRIP — DEFECTIVE (CABIN)

ORD - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT AT FIRST CLASS GALLEY RT AISLE FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT AT FIRST CLASS GALLEY RT AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)