N360AA

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 107,607 hrs · 17,399 cycles

LEFT AFT MAIN CABIN DOOR EXTERIOR EMER LIGHT INOPERATIVE. REPLACED LAMP IN LT AFT MAIN CABIN DOOR EXTERIOR EMER LIGHT IAW AMM 33-51-00. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 105,379 hrs · 17,055 cycles

LT & RT NR 1 DOORS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR LT & RT NR 1 DOORS EMERGENCY LIGHTS, OPERATIONS CHECKED NORMAL.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 105,376 hrs · 17,053 cycles

MULTIPLE AREAS OF CORROSION ON FAIL SAFE STRAP. R & R FAIL SAFE STRAP IAW AARD 51-00-05-1.

Part: LATCH — INOPERATIVE (SLIDE DOOR) · airframe 105,376 hrs · 17,053 cycles

SLIDE DOOR IS OUT OF RIG & WILL NOT OPEN. REPLACED FOUR LATCHES IAW AMM 25-65-09-404-007, OPS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 102,952 hrs · 16,686 cycles

LT AFT FLIGHT ATTENDANT DUAL SEAT FLASHLIGHT BATTERY DRAINED/DISCHARGED. R&R AFT FLIGHT ATTENDANT DUAL SEAT FLASHLIGHT BATTERY. OPERATIONS CHECKED NORMAL.

Part: SEAL — DETERIORATED (OIL CAP) · airframe 100,360 hrs · 16,285 cycles

MIA - CREW REPORTED LEFT ENGINE OIL PRESSURE LOW INDICATION DURING CRUISE. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED OIL CAP SEAL THAT HAD DETERIORATED AND WAS LEAKING OIL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SOCKET — CORRODED (EXTERIOR) · airframe 100,018 hrs · 16,232 cycles

RIGHT NUMBER 2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. CLEANED SOCKET THAT WAS CORRODED. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 100,018 hrs · 16,232 cycles

LEFT NUMBER 1 DOOR EXIT SIGN LOWER LIGHT INOPERATIVE. FOUND LOWER SECTION SHORTING BATTERY PACK. FIXED SHORT AND REPLACED BATTERY PACK.

Part: SLAT — DELAMINATED (RT WING) · airframe 99,567 hrs · 16,157 cycles

NUMBER 7 SLAT HAS A DELAMINATION APPROXIMATELY 81.5 INCHES FROM OUTBOARD EDGE, .5 INCHES FROM FORWARD EDGE, AND 7.75 INCHES FROM AFT EDGE. ACCOMPLISHED BONDED REPAIRED PER SRM 51-20-05.

Part: FLAP — DEBONDED (LT WING) · airframe 99,567 hrs · 16,157 cycles

LEFT WING INBOARD AFT FLAP APPROXIMATELY 25 INCHES INBOARD OF CANOE. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-10-2R.

Part: SKIN — DENTED (TE FLAP) · airframe 99,567 hrs · 16,157 cycles

DENT IN UPPER SKIN OF AFT INBOARD FLAP. ACCOMPLISHED HOT BOND REPAIR PER SRM 51-70-10-2R.

Part: SKIN — CRACKED (LE SLAT) · airframe 99,567 hrs · 16,157 cycles

POSITIVE CRACK INDICATION FOUND USING HFEC, A FULL SCREEN DEFLECTION WAS INDICATED. CRACK LOCATED ON LEADING EDGE OF NUMBER 9 SLAT AT APPROXIMATELY 41 INCHES FROM OUTBOARD END ON LOWER SURFACE AT FIRST FASTENER LOCATION FROM FORWARD EDGE. INSTALLED DOUBLER REPAIR PER SRM 57-43-01-2R.

Part: SKIN — CRACKED (LE SLAT) · airframe 99,567 hrs · 16,157 cycles

HIGH FREQUENCY EDDY CURRENT FOUND CRACK INDICATION LOCATED ON LEADING EDGE OF NUMBER 10 SLAT AT APPROXIMATELY 42 INCHES FROM OUTBOARD END ON LOWER SURFACE AT FIRST FASTENER LOCATION FROM FORWARD. INSTALLED DOUBLER REPAIR PER SRM 57-43-01-2R.

Part: ENGINE — FAILED (RIGHT) · airframe 97,101 hrs · 15,742 cycles

JFK - CREW REPORTED A SOUND AS IF GEAR DOOR CLOSED, THEN NUMBER 2 FIRE WARNING. CAPTAIN DISCHARGED BOTH FIRE BOTTLES. RIGHT ENGINE WAS SHUTDOWN (SINGLE ENGINE TIME 12 MINS). EMERGENCY DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. AIRCRAFT CURRENTLY UNDERGOING MAINTANANCE.

Part: SOCKET — DAMAGED (CABIN) · airframe 96,910 hrs · 15,714 cycles

EMERGENCY LIGHT ON SEAT 2HJ INOPERATIVE. REPAIRED CONNECTION IN SOCKET. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 96,910 hrs · 15,714 cycles

LEFT NUMBER 1 DOOR EMERGENCY LIGHT AT UPPER RIGHT SIDE LIGHT PANEL INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 1 DOOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 96,910 hrs · 15,714 cycles

EMERGENCY LIGHT AT SEAT 10AB INOPERATIVE. REPLACED LAMP FOR BOTH LIGHTS AT 10AB. OPS CHECK NORMAL.

Part: WIRE — DAMAGED (CABIN) · airframe 96,910 hrs · 15,714 cycles

EMERGENCY LIGHT ON SEAT 4HJ INOPERATIVE. REPAIRED WIRE THAT WAS DAMAGED. OPS CHECK NORMAL.

Part: PROCESSOR — MALFUNCTIONED (FUEL SYSTEM) · airframe 95,184 hrs · 15,463 cycles

JFK - INFLIGHT ORD-DUB. CREW REPORTED LEFT AND RIGHT MAIN FUEL QUANTITY FAULTS AND RIGHT FUEL FLOW FLUXUATION. FLIGHT DIVERTED LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT PROCESSOR AND RIGHT FUEL FLOW TRANSMITTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PROCESSING UNIT — FAILED (FUEL SYSTEM) · airframe 94,078 hrs · 15,287 cycles

LAX - INFLIGHT DFW-OGG. CREW REPORTED FLUCTUATION OF FUEL QUANTITY SYSTEM WITH ASSOCIATED BLANKING FOR 1 TO 2 MINUTES TOTAL DURATION. FLIGHT DIVERTED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED PROCESSOR UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 94,074 hrs · 15,286 cycles

CORROSION WAS FOUND AT STATION 325 FLOORBEAM UPPER CAP HORIZONTAL FLANGE UPPER SURFACE AT RIGHT BUTTLINE 41. REMOVED CORROSION AND ACCOMPLISHED DOUBLER REPAIR EA B767-53-016297.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 3 · airframe 94,074 hrs · 15,286 cycles

EXCESSIVE CORROSION ON THE FUSELAGE SKIN PANELS BETWEEN STATIONS 414 AND 454 AND STRINGER 35 LEFT TO 26 RIGHT. ACCOMPLISHED REPAIR PER EA B767-53-016757.

Part: SILL — CRACKED (FUSELAGE) · corrosion level 3 · airframe 94,074 hrs · 15,286 cycles

CORROSION ON THE FORWARD CARGO DOOR CUTOUT LOWER SILL SAFE STRAP 143T8204-2. REMOVE CORROSION PER SRM 51-10-02 AND ACCOMPLISH HFEC AND OPEN HOLE HFEC INSPECTION. ACCOMPLISHED REPAIR PER EA 016755.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 3 · airframe 94,074 hrs · 15,286 cycles

CORROSION ON THE FORWARD CARGO DOOR CUTOUT SURROUND STRUCTURE LOWER SILL OUTER CHORD VERTICAL FLANGE TWO LOCATIONS. THE FIRST LOCATION AT STATION 539 AND THE SECOND LOCATION AT STATION 567. REMOVE CORROSION AND ACCOMPLISHED REPAIR PER EA B767-53-016374.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,058 hrs · 15,282 cycles

CORROSION WAS FOUND ON THE CENTER WING BOX RIGHT BUTTLINE 33 LONGITUDAL FLOORBEAM AT STATION 875. REMOVED DAMAGE AND ACCOMPLISHED REPAIR PER EA B767-53-016333.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 3 · airframe 94,058 hrs · 15,282 cycles

CORROSION DAMAGE ON FUSELAGE STRINGER 39 RIGHT AT APPROXIMATE STATION 1298. INSTALLED NEW STRINGER SPLICE PER EA B767-53-016537.

Part: STIFFENER — DAMAGED (FUSELAGE) · airframe 93,790 hrs · 15,240 cycles

DAMAGE TO RIGHT BUTTLINE 5.75 PRESSURE DECK STIFFENER AT STATION 1045 AND 1060. REPAIRED WITH 2024-T42 ALUMINUM ANGLE.

Part: BATTERY PACK — MISSING (CABIN) · airframe 92,350 hrs · 14,995 cycles

IT WAS DISCOVERED THAT THE EXTERNAL EMERGENCY LIGHTS WERE NOT WORKING. FOUND THAT THE LEFT AND RIGHT SIDES OF THE FIRST CLASS CABIN HAD FOUR EMERGENCY BATTERY PACKS MISSING. REPLACED BATTERY PACKS FOR THE RIGHT SIDE OF FIRST CLASS CABIN. OPS CHECKED NORMAL.

Part: BATTERY PACK — MISSING (CABIN) · airframe 92,350 hrs · 14,995 cycles

IT WAS DISCOVERED THAT THE EXTERNAL EMERGENCY LIGHTS WERE NOT WORKING. FOUND THAT THE LEFT AND RIGHT SIDES OF FIRST CLASS CABIN HAD FOUR EMERGENCY BATTERY PACKS MISSING. REPLACED BATTERY PACKS FOR THE LEFT SIDE OF FIRST CLASS CABIN. OPS CHECKED NORMAL.

Part: BULKHEAD — CRACKED (PYLON) · airframe 92,206 hrs · 14,971 cycles

INSPECTION NOTED A CRACK ON INBOARD SIDE OF THE LEFT PYLON STRUT AFT BULKHEAD. ALL REPAIRS WERE ACCOMPLISHED PER EA B767-54-011234.

Part: SKIN — CRACKED (LT WING) · airframe 92,206 hrs · 14,971 cycles

LEFT WING SKIN AT AFT PITCH LOAD FITTING TENSION BOLT INSPECTION AND REPAIR. OUTBOARD TENSION BOLT HOLE, CRACK FOUND. ALL REPAIRS TO THIS DISCREPANCY WERE ACCOMPLISHED IAW EA B767-57-011899 AND INCLUDED ALL REFERENCE ATTACHMENTS.

Part: DOUBLER — CRACKED (NR 1 PYLON) · airframe 92,206 hrs · 14,971 cycles

NUMBER 1 PYLON FORWARD UPPER SPAR WEB REPAIR DOUBLER CRACKED. ACCOMPLISHED REPAIRED PER EA B767-54-011251.

Part: FITTING — CRACKED (NACELLE) · airframe 92,205 hrs · 14,969 cycles

CRACK AT THE AFT ENGINE MOUNT BULKHEAD AT MID SPAR FITTING. REPLACED FITTING IN ACCORDANCE WITH ASB 767-54A0101 INCLUDING INSPECTIONS SPECIFIED BY THE ASB.

Part: O-RING — LEAKING (NR 1 ENGINE) · airframe 90,043 hrs · 14,579 cycles

ON TAKEOFF ROLL AIRCRAFT CABIN SMELL OF AIR CONDITIONING WATER SEPARATOR ODOR. RECIRCULATION FANS WERE TURNED OFF TO ACCOMPLISH ODOR REMOVAL. ODOR DISSIPATED AFTER 5 MINUTES. TURNED RECIRCULATION FANS BACK ON AND HAD A DIFFERENT ODOR. ON DESCENT BOTH ODORS RETURNED AND WERE STRONGER. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. MAINTENANCE REPORTED OIL SMELL IN FIRST CLASS CABIN. FOUND OIL ON HIGH PRESSURE COMPRESSOR. REPLACED NUMBER ONE BEARING CAP O-RING. FERRIED TO JFK FOR NUMBER ONE ENGINE REPLACEMENT.

Part: LENS — MISSING (CABIN)

JFK - EXIT SIGN AT AFT LAVATORY RIGHT HAND SIDE DOOR LEVEL MISSING LENS. REPLACED LENS FOR EXIT SIGN AT AFT LAVATORY RIGHT SIDE DOOR LEVEL.

Part: CONNECTOR — LOOSE (NR 2 ENGINE) · airframe 87,069 hrs · 14,104 cycles

MIA INFLIGHT - CREW REPORTED NR 2 ENGINE GAS TEMPERATURE FLUCTUATION. LOST NR 2 ENGINE GAS TEMPERATURE INDICATION ON BOTH EICAS STANDBY ENGINE INDICATORS. NR 2 ENGINE GAS TEMPERATURE INDICATIONS WENT TO NORMAL IN DESCENT AND THROUGH LANDING. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. FOUND CONNECTOR ON ENGINE GAS TEMPERATURE JUNCTION BO ON NR 2 ENGINE LOOSE. SECURED CONNECTOR ON NR 2 ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COMPRESSOR — CONTAMINATED (NR 2 ENGINE) · airframe 86,680 hrs

JFK INFLIGHT - CREW REPORTED SMOKE IN COCKPIT AND SMOKE ALARMS COULD BE HEARD IN CABIN. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. FOUND OIL IN HIGH PRESSURE COMPRESSOR STAGES 1, 2 AND 3 ON NR 2 ENGINE. REPLACED NR 2 ENGINE ON 12 DEC AT JFK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,856 hrs

JFK - EMERGENCY LIGHT AT SEAT 6H INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 6H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRAP — MISSING (FLASHLIGHT) · airframe 83,586 hrs

ORD - EMERGENCY FLASHLIGHT IN CABIN MISSING STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 83,586 hrs

ORD - EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS)

JFK - EMERGENCY LIGHT AT MID GALLEY MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE HARNESS — DAMAGED

FRA INFLIGHT T84/20AUG - DURING FLIGHT RECEIVED AFT CARGO HEAT OVERHEAD STATUS MESSAGE AND SEVER CIRCUIT BREAKERS RELATED TO AFT AND BULK CARGO HEAT SYSTEM TRIPPED. AFTER NORMAL LANDING SMOKE REPORTED IN CABIN AND EMERGENCY DECLARED. PASSENGERS DEPLANED AND NO INJURIES SUSTAINED. FERRIED AIRCRAFT TO AFW. REPAIRED WIRE BUNDLE W580. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (WARNING BELL)

CDG INFLIGHT T120/02AUG - FIRE BELL AURAL WARNING SOUNDED AND WOULD NOT RESET. ALL OTHER INDICATIONS NORMAL. REPLACED AURAL WARNING BELL MODULE. SYSTEM GROUND CHECKED NORMAL OPERATIONS.

Part: CONTROLLER — SMOKE (WINDOW HEAT)

MAN INFLIGHT T55/14FEB - AT LEVEL OFF RIGHT FORWARD WINDOW HEAT WIRING STARTED SMOKING. REMOVED POWER AND SMOKE DISSAPATED. RETURNED TO MAN AND LANDED WITHOUT INCIDENT. REPLACED RIGHT FORWARD WINDSHIELD AND HEAT CONTROLLER POWER CABLE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SILL — CORRODED (ZONE 800)

FORWARD CARGO DOOR SILL LOWER CHORD HAD CORROSION BLENDED FROM THE HORIZONTAL INSIDE FLANGE AT STATION 616. AREA OF DISCREPANCY IS 2.5 INCHES BY 2.5 INCHES WITH A DEPTH OF .033 INCH. REMOVED FASTENERS AND BLENDED CORROSION AWAY USING A MINIMUM 0.5 INCH BLEND RADIUS WITH AT 20:1 TAPER RATIO. PERFORMED VISUAL 10X MAGNIFICATION INSPECTION TO ENSURE CORROSION WAS REMOVED. PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION OF THE BLENDED AREA AND PERFORMED A BOLT HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION OF FASTENERS WITHIN THE REWORK AREA FOR CRACKS. ENSURED THE REPAIR AREA MEASURED 2.5 INCHES MAXIMUM DIAMETER AND A MINIMUM REMAINING THICKNESS OF 0.170 INCH. APPLIED 2 COATS OF PRIMER TO THE REWORK AREA AND INSTALL

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS)

DFW - ESCAPE PATH EMERGENCY LIGHT AT SEAT 37B INOPERATIVE. REPLACED CONNECTOR AT SEAT TO WALL HARNESS FOR ESCAPE PATH EMERGENCY LIGHTS AT SEAT 37B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — CRACKED (FUSELAGE)

AFW - FUSELAGE SKIN AT STATION 1809 RIGHT HAND UPPER FASTENER HOLE HAD A CRACK INDICATION IN THE FUSELAGE SKIN ONLY AT THE FOUR O`CLOCK POSITION. AREA IS .375 BY .375 AT THE RIGHT HAND FUSELAGE AFT AT STATION 1809. THE HOLE HAD BEEN REAMED TO 0.375 TO REMOVE CRACK INDICATION. OVERSIZED THE HOLE IN THE FUSELAGE OUTER SKIN TO 0.375 INCHES. VERIFIED CRACK WAS COMPLETELY REMOVED. INSTALLED A COUNTERSINK FREEZE PLUG IN SKIN. REINSTALLED EXTERNAL WEAR DOUBLER.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHT INOPERATIVE AT SEAT 33HJ. REPAIRED BROKEN WIRE AT LOWER SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — NOT SEATED (CABIN)

MIA EMERGENCY LIGHT AT 12B INOPERATIVE. RESEATED HARNESS CONNECTOR FOR EMERGENCY LIGHT AT 12B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT)

SFO - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT SEAT HARNESS PLUG AT SEAT 35. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: IDG — FAILED (RT ENGINE)

RIGHT GENERATOR DRIVE INOPERATIVE, EICAS MESSAGE ACCOMPLISHED DISCONNECT PROCEDURE. SERVICED RIGHT IDG TO FULL RECONNECTED IDG RAN ENGINE FOR SEVERAL MIN, OPS CHECKS GOOD. DUE TO PREVIOUS REPORT THAT RT IDG FAILED DUE TO LOW OIL QTY. REPLACED THE IDG. REPLACED IDG PER MM. SERVICED WITH OIL. OPS CHECK AND LEAK CHECK DUE ON ENGINE RUN UP. OPS NORMAL AND LEAK CHECK OK. (M)

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEATS 11B, 12B, AND 13B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 35H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECTOR ON SEAT 35H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 24B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECTOR ON SEAT 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PUMP — FAILED (RT ENGINE)

EN ROUTE LHR-EWR, RT ENGINE HYDRAULIC PUMP FAILED. AIRCRAFT DIVERTED TO BOS LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE HYDRAULIC DRIVEN PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PROJECTOR — MALFUNCTIONED (CABIN)

ZRH - FLT 37 - EN ROUTE ZRH-DFW, PASSENGER VIDEO SYSTEM SMOKED AT POWER SUPPLY AND BLEW MAIN CIRCUIT BREAKER WHEN SWITCHED ON. CREW SMELLED SMOKE IN FLIGHT DECK. REPLACED ZONES ABC PROJECTORS AND ALSO REPLACED CONTROL DISTRIBUTION BOX. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 17B INOPERATIVE. RE-SEATED EMERGENCY EXIT LIGHT PIN AT SIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: OVEN — DIRTY (CABIN)

CDG - FLT 62 - EN ROUTE MIA-CDG - DETECTED BURNING SMELL AT NR 1 FIRST CLASS OVEN. TURNED OFF OVEN. LANDED CDG WITHOUT FURTHER INCIDENT. CLEANED NUMBER ONE FIRST CLASS OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: COMPUTER — FALSE INDICATION (E/E BAY)

ORD - FLT 42 - IN CRUISE FLIGHT AT FL330 FMC 2 CB POPPED AND THE FOLLOWING EICAS MESSAGE APPEARED, R FMC FAIL, EICAS CONTROL PNL, EICAS DISPLAY, R IRS ON DC ALSO AUTO THROTTLES WOULD NOT MATCH N1 POWER SETTINGS. RIGHT ENGINE NR 1 WAS 6 PERCENT HIGHER THAN LEFT ENGINE WITH MATCHED POWER LEVERS ALL OTHER PARAMETERS ALSO UNMATCHED FWD GALLEY CHILLER NAV F/O NAV RMDI INOPERATIVE AS WELL, ALSO NO LAND 3. REINSTATED C/B C307. INSPECTED RIGHT IDG AND RT ENGINE FEEDER HARNESS. NO FAULTS FOUND, CHECKED AND SERVICED RIGHT IDG OIL CHECKED OK. RAN BOTH ENGINES AT CRUISE POWER FOR TWENTY MINUTES. NO FAULTS FOUND. LOADED RIGHT MAIN BUS TO 75 PERCENT LOAD FOR APPROXIMATELY 10 MINUTES. NO FAULTS AND C/B C307 REMAINED I

Part: LIGHT — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT ROW 3B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMLBY AT SEAT ROW 3B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (ROW 27-36)

SFO - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT SEAT PATH LIGHTS AT ROW 27H AND 36H INOPERATIVE. SECURED EMERGENCY EXIT SEAT PATH LIGHT CONNECTOR AT 27H AND 36H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — LOOSE (ROW 21-24)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT 21A-24B INOPERATIVE. SECURED WIRING ON BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (ROW 21 HJ)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT ROWS 21HJ INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT ROW 21HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — FAILED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT 21A AND 21B INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHTS CONNECTOR AT SEAT 21A AND 21B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - FLT 1539 - EN ROUTE MIA-SFO - DURING CRUISE, ALL EMERGENCY EXIT AND FLOOR LIGHTS ILLUMINATED FOR APPROX 30 SECONDS THEN WERE EXTINGUISHED BY RESETTING THE EMERGENCY EXIT LIGHTS AT FLIGHT ATTENDANTS STATION. SITUATION OCCURRED AGAIN DURING FLIGHT. LANDED SFO WITHOUT INCIDENT. SECURED CONNECTOR AT FLT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT ROW 24HJ WOULD NOT ILLUMINATE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT ROW 24HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CORRODED (BS 1113)

AFW - FUSELAGE CROWN SKIN UNDER ADF ANTENNA HAD CORROSION BLENDED BEYOND LIMIT. REPAIRED IAW MRB 767-1547. (M)

Part: CONNECTOR — BROKEN (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AISLE LIGHT AT SEAT 31H INOPERATIVE. REPAIRED CONNECTOR AND SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 29B INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT CONNECTOR ON PAX SEAT 29B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS BETWEEN PASSENGER SEAT ROWS 2B AND 7B INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT ROW 2B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL ASSY — BROKEN (R1 DOOR)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT LOWER EXIT SIGN AT R1 DOOR BROKEN. REPLACED EMERGENCY FLOOR LIGHT LOWER EXIT SIGN AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)

Part: EEL WIRE — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEATS 2B THROUGH 12B, INOPERATIVE. RESECURED EMERGENCY FLOOR LIGHT WIRING FOUND LOOSE BY PASSENGER SEAT 2B. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)