N372AA

Part: UNKNOWN — MALFUNCTIONED (LAVATORY) · airframe 96,214 hrs · 15,048 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CRUISE, LAVATORIES FS3, M2, A5 WOULD NOT FLUSH. ACCOMPLISHED FIM PROCEDURE 38-30-00-815-804. SERVICED LAVATORY TANKS. SYS CHECKED NORMAL.

Part: TRANSCEIVER — FAULTY (WEATHER RADAR) · airframe 95,961 hrs · 15,009 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB CREW REPORTED WEATHER RADAR INOPERATIVE. R & R WEATHER RADAR TRANSCEIVER IAW AMM 34-43-01. PERFORMED OPERATIONAL CHECK. SYS CHECKED NORMAL.

Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY) · airframe 95,391 hrs · 14,904 cycles

F1 LAVATORY SMOKE DETECTOR SOUNDING INTERMITTENTLY. MX ACTION ACCOMPLISHED IAW FIM TASK 26-13-815-806. R & R SMOKE DETECTOR IAW AMMA 26-13-01. PERFORMED OPERATIONAL CHECK IAW AMM 26-13-00. SYS CHECKED NORMAL.

Part: FRAME — CRACKED (RT PYLON) · airframe 94,987 hrs · 14,835 cycles

RIGHT PYLON OTBD VERTICAL FRAME FOUND WITH A CRACK DURING THE ACCOMPLISHMENT OF WORK CARD 6986. R & R VERTICAL STIFFENER IAW FEA 18082.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 94,534 hrs · 14,744 cycles

AIR INTERRUPT, NO EMER DECLARED. LANDING UNEVENTFUL & ACFT WAS NOT OVERWEIGHT. LT ENG ANTI-ICE DISPLAYED ON EICAS. LT VLV LIGHT ON ENG ANTI-ICE WHEN SELECTED, UPON LANDING & VLV LIGHT WENT OUT & OPERATED NORMALLY. NO ACTION REQUIRED SYS OPERATES NORMALLY IAW 30-21-00.

Part: SIGN — BROKEN (CABIN) · airframe 93,352 hrs · 14,561 cycles

LEFT NR 2 DOOR EXIT LIGHT ASSEMBLY BROKEN. REPLACED LT NR 2 DOOR EXIT SIGN ASSEMBLY. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 93,352 hrs · 14,561 cycles

RIGHT NR 1 DOOR EXTERIOR FUSELAGE EMER LIGHT INOPERATIVE. REPLACED LAMP FOR RT NR 1 DOOR EXTERIOR FUSELAGE EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — MISSING (CABIN) · airframe 93,243 hrs · 14,547 cycles

SEAT MOUNTED EMER LIGHT AT ROW 29AB MISSING LAMP. REPLACED LAMP FOR SEAT MOUNTED EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 93,219 hrs · 14,544 cycles

SEAT MOUNTED EMER LIGHT AT ROW 29AB MISSING CLEAR LENS. REPLACED LENS FOR SEAT MOUNTED EMER LIGHT AT ROW 29AB. OPERATIONS CHECKED NORMAL.

Part: BOTTLE — DEFECTIVE (CREW O2) · airframe 93,138 hrs · 14,533 cycles

CREW O2 PRESS DROPPING. EMER DECLARED FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. REPLACED CREW O2 BOTTLE & LEAK CHECKED. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 92,368 hrs · 14,412 cycles

RIGHT NR 1 DOOR, LOWER EMER LIGHT SIGN INOPERATIVE. REPLACED LAMP FOR RT NR 1 DOOR LOWER EMER LIGHT SIGN. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 92,368 hrs · 14,412 cycles

LEFT NR 4 DOOR, UPPER AFT EMER LIGHT SIGN INOPERATIVE. REPLACED LAMP FOR LT NR 4 DOOR, UPPER AFT EMER LIGHT SIGN. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 92,368 hrs · 14,412 cycles

EMERGENCY LIGHT AT SEAT 13H INOPERATIVE. REPLACED LAMP FOR EMER LIGHT AT SEAT 13H. OPERATIONS CHECKED NORMAL. RELAMPED LIGHT ASSEMBLY IAW MM 33-51-10. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 92,368 hrs · 14,412 cycles

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

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 92,368 hrs · 14,412 cycles

FS3 LAVATORY LOWER EMER LIGHT SIGN INOPERATIVE. REPLACED LAMP FOR FS3 LAVATORY LOWER EMER LIGHT SIGN. OPERATIONS CHECKED NORMAL.

Part: DUCT — RUPTURED (ZONE 400) · airframe 91,417 hrs · 14,258 cycles

HNL CREW REPORTED LT ENG OVERHEAT CAUTION CAME ON UPPER EICAS & PEDESTAL ANNUNCIATOR LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED HNL LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RUPTURED SUPPLY DUCT & FAULTY CLAMP. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 91,046 hrs · 14,193 cycles

AFT CARGO FWD ROLLOUT STOP SUPPORT BEAM AT STATION 1300 CRACKED. REPLACED BEAM IAW SRM 51-10 -02-0G.

Part: LIGHT — NOT SEATED (EXTERIOR) · airframe 91,046 hrs · 14,193 cycles

EXTERNAL EMERGENCY EXIT LIGHT AT AFT LT DOOR INOPERATIVE. FOUND LAMP NOT FULLY SECURED IN FIXTURE. PROPERLY RESEATED LAMP IN FIXTURE, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 91,046 hrs · 14,193 cycles

EXTERNAL EMERGENCY EXIT LIGHT AT AFT LT DOOR IS INOPERATIVE. REPLACED LIGHT FOR EXTERNAL EMERGENCY EXIT LIGHT AT AFT LT DOOR. OPERATIONS CHECKED NORMAL.

Part: BYPASS SWITCH — INOPERATIVE (RT ENGINE) · airframe 88,943 hrs · 13,863 cycles

OPO INFLIGHT MAD-MIA CREW REPORTED RT ENGINE FILTER BYPASS EICAS MESSAGE. CREW SHUT ENGINE DOWN, SINGLE ENGINE TIME 60 MINUTES. EMERGENCY DECLARED FLIGHT DIVERTED OPO LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RT ENGINE OIL FILTER BYPASS SWITCH. SYSTEM GROUND CHECK NORMAL OPERATION CLOSED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 85,359 hrs · 13,302 cycles

INTERCOSTAL ANGLE AT CEILING AREA IN FORWARD CARGO BETWEEN STATIONS 742 TO 764 AT LEFT BUTTLINE 40 HAS 2 CRACKS AT NUT PLATES. REPLACED INTERCOSTAL PER SRM 51-20-00-2.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,359 hrs · 13,302 cycles

STRINGER 34 RIGHT FROM STATIONS 742 TO 764 CORRODED. ACCOMPLISHED STRINGER SPLICE REPAIR SRM 53-00-03-2R2.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 85,099 hrs · 13,266 cycles

LEFT AND RIGHT NUMBER 2 DOORS THRESHOLD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK NORMAL.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 83,164 hrs · 12,940 cycles

CORROSION TO STRINGER 22 LEFT AT STATION 960. REMOVED CORROSION AND ACCOMPLISHED REPAIR PER EA B767-53-021621.

Part: FITTING — CRACKED (RT WING) · airframe 83,164 hrs · 12,940 cycles

RIGHT WING AFT PITCH LOAD FITTING OUTBOARD TENSION BOLT HOLE CRACKED. INSTALLED AFT PITCH LOAD FITTING PER EA B767-57-021245.

Part: FITTING — CRACKED (LT WING) · airframe 83,164 hrs · 12,940 cycles

LEFT WING AFT PITCH LOAD FITTING OUTBOARD TENSION BOLT HOLE CRACKED. INSTALLED AFT PITCH LOAD FITTING PER EA B767-57-021103.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 83,164 hrs · 12,940 cycles

LEFT SKIN PANEL STATION 960 CORRODED. ACCOMPLISHED HIGH FREQUENCY EDDY CURRENT AND REMOVED CORROSION PER EA B767-53-021212.

Part: SKIN — CORRODED (CENTER WING) · corrosion level 2 · airframe 83,164 hrs · 12,940 cycles

CENTER WING UPPER SKIN FORWARD OF STATION 955, RIGHT AND LEFT BUTTLINE 82 CORRODED. REMOVED CORROSION AND ROTO PEENED AREA PER EA B767-57-021172.

Part: STRAP — CRACKED (FUSELAGE) · airframe 83,164 hrs · 12,940 cycles

LEFT BODY STATION 955 FAILSAFE STRAP CRACKED. ACCOMPLISHED REPAIR PER ECO C3039AE.

Part: MODULE — FAULTY (AUTOPILOT SYS) · airframe 81,754 hrs · 12,735 cycles

MIA - INFLIGHT STI-JFK. CREW REPORTED AILERON AND AUTO-PILOT FAULTS. EMERGENCY DECLARED FLIGHT DIVERTED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED STABILIZER TRIM/ELEVATOR ASYMMETRY MODULE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: MODULE — DEFECTIVE (CABIN) · airframe 81,035 hrs · 12,633 cycles

EMERGENCY EVACUATION SYSTEM ALARM CAME ON UNCOMMANDED ON GROUND. FOUND M885 COMMAND SWITCH DEFECTIVE. REPLACED MODULE AT RIGHT NUMBER 4 DOOR CONTROL PANEL. OPS CHECK NORMAL.

Part: PYLON — CRACKED (LEFT) · airframe 80,516 hrs · 12,552 cycles

CRACK WAS FOUND FROM THE FORWARD INBOARD RADII OF THE POWER FEEDER CABLE PASS THROUGH HOLE JUST AFT OF LEFT PYLON STATION 221.25. ACCOMPLISHED DOUBLER REPAIR PER EA 015771.

Part: PYLON — CRACKED (RIGHT) · airframe 80,516 hrs · 12,552 cycles

CRACK WAS FOUND FROM THE FORWARD INBOARD RADII OF THE POWER FEEDER CABLE PASS THROUGH HOLE JUST AFT OF RIGHT PYLON STATION 221.25. ACCOMPLISHED DOUBLER REPAIR PER EA 015770.

Part: SPAR — CRACKED (RT PYLON) · airframe 80,516 hrs · 12,552 cycles

CRACK WAS FOUND ON THE RIGHT PYLON FORWARD UPPER SPAR WEB COMMON TO THE IDG POWER FEEDER CABLE PASS THROUGH. INSTALLED DOUBLER REPAIR PER EA B767-54-015643.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 80,516 hrs · 12,552 cycles

BLEND WAS FOUND ON STRINGER 8 RIGHT LAP SKIN JOINT AT STATION 724. ACCOMPLISHED AN OPEN HOLE AND SURFACE HIGH FREQUENCY EDDY CURRENT INSPECTION. REPLACED FASTENERS PER EA B767-53-015606.

Part: WEB — CRACKED (LT PYLON) · airframe 80,516 hrs · 12,552 cycles

CRACKS AROUND THE LEFT PYLON STRUT TORQUE BOX FORWARD UPPER WEB POWER FEEDER CABLE CUTOUT. ACCOMPLISHED DOUBLER REPAIR PER EA B767-54-015644.

Part: START VALVE — INOPERATIVE (NR 2 ENGINE) · airframe 78,813 hrs · 12,256 cycles

JFK - INFLIGHT MIA-CDG. CREW REPORTED NUMBER TWO ENGINE START VALVE MESSAGE ILLUMINATED. FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED START VALVE, CONTROL PANEL, SPEED CARD, AND RELAY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 78,080 hrs · 12,116 cycles

JFK - CREW REPORTED WEATHER RADAR FAILED SHORTLY AFTER TAKEOFF. EMERGENCY DECLARED RETURNED JFK LANDED WITHOUT INCIDENT. REPLACED WEATHER RADAR TRANSCEIVER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 77,828 hrs · 12,070 cycles

MIA - TRAILING EDGE FLAP DISAGREE LIGHT ON FINAL WHEN SELECTING 25 DEGREE FLAPS. FLAP INDICATOR STUCK AT 20 DEGREE FLAPS. ACCOMPLISHED QUICK REFERENCE HANDBOOK CHECKLIST. EMERGENCY DECLARED ACCOMPLISHED GO AROUND LANDED MIA WITH 20 DEGREE FLAPS WITHOUT INCIDENT. ACCOMPLISHED BITE OF FLAP SLAT ELECTRONIC UNIT NO FAULTS FOUND. REPLACED FLAP SLAT ELECTRONIC UNIT AS PRECAUTIONARY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TRANSMITTER — FAULTY (TE FLAP) · airframe 76,741 hrs · 11,888 cycles

ORD - DURING APPROACH HAD A TRAILING EDGE FLAP ASSYMETRY. RAN THE QRH AND LANDED WITH FLAPS 20. ALSO HAD TRAILING EDGE FLAPS SHUTDOWN STATUS MESSAGE. FLIGHT LANDED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLAP TRANSMITTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PIN — BURNED (CABIN) · airframe 76,495 hrs · 11,851 cycles

POWERPORTS 5AB CAUSED AC ADAPTOR TO SMOKE. REPLACED BURNT PIN ON POWER PORT HARNESS. OPS CHECKS NORMAL.

Part: WARNING SYSTEM — MALFUNCTIONED (TE FLAP) · airframe 74,673 hrs · 11,533 cycles

PAP - AIRCRAFT HAD TRAILING EDGE FLAP DISAGREE INDICATION DURING ARRIVAL TO PAP. EMERGENCY DECLARED, LANDED AT PAP WITHOUT INCIDENT. ACCOMPLISHED FAULT ISOLATION MANUAL 27-51-00 FIGURE 104 OF FLAP SLAT ELECTRICAL UNIT. CYCLED FLAPS CHECKS OK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: VALVE — INOPERATIVE (RT ENGINE) · airframe 73,814 hrs · 11,396 cycles

RIGHT ENGINE BLEED OVERHEAT INDICATION. EMERGENCY DECLARED RETURNED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RT ENGINE HP VALVE AND CONTROLLER. REPLACED FAN AIR VALVE. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)

Part: INDICATOR — INOPERATIVE (COCKPIT) · airframe 73,287 hrs · 11,311 cycles

BOS - INFLIGHT JFK-CDG. CAPTAIN REPORTED STANDBY ATTITUDE INDICATOR GYRO FLAG WAS IN VIEW. LANDED BOS WITHOUT INCIDENT. REMOVED AND REPLACED STANDBY ATTITUDE INDICATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · 70,781 cycles

MIA EMERGENCY EXIT LIGHTS AT SEAT ROWS 20H AND 21H INOPERATIVE. REPLACED BATTERY PACK AT RT HAND OVERWING DOOR FOR EMERGENCY EXIT LIGHTS AT SEAT ROWS 20H AND 21H. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 70,781 hrs

MIA - EMERGENCY EXIT LIGHTS AT RIGHT LEFT OVERWING AND EMERGENCY LIGHTS AT SEATS 20H AND 21H INOPERATIVE. REPLACED BATTERY PACK FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · 70,781 cycles

MIA EMERGENCY LIGHT AT LT HAND OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LT HAND OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — DISCHARGED (CABIN) · 70,781 cycles

MIA EMERGENCY LIGHT AT RT HAND OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RT HAND OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · 70,781 cycles

MIA EMERGENCY LIGHTS AT SEAT ROWS 20H TO 21H INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 20H TO 21H. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 69,156 hrs

DFW - EXTERNAL EMERGENCY LIGHT AT LEFT AFT OVERWING INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT LEFT AFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EXTERIOR) · airframe 69,156 hrs

DFW - EXTERNAL EMERGENCY LIGHT AT LEFT AFT OVERWING MISSING LENS. REPLACED LENS FOR EXTERNAL EMERGENCY LIGHT AT LEFT AFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHT AT SEAT 17H INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 17H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 26H INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 26H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHTS AT SEAT ROWS 22H TO 24H INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY LIGHTS AT SEAT ROWS 22H TO 24H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 28H INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 28H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHT AT SEAT 12H INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 12H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,057 hrs

LAX - SEAT MOUNTED AND OVERHEAD EMERGENCY LIGHTS AT LEFT SEAT ROWS 21 TO 24 INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED AND OVERHEAD EMERGENCY LIGHTS AT LEFT SET ROWS 21 TO 24. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WINDSHIELD — ARCED (COCKPIT)

CDG T062/11OCT - CAPTAINS NUMBER ONE WINDOW HAD ARCING. ARCING STOPPED WHEN LEFT FORWARD SWITCH TURNED OFF. REPLACED CAPTAINS NUMBER ONE WINDSHIELD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS)

JFK - EMERGENCY LIGHT AT SEAT ROW 2HJ INOPERATIVE. REPLACED CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 2HJ. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

SFO - EMERGENCY EXIT LIGHT AT LEFT OVERHEAD FORWARD GALLEY INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT LIGHT AT LEFT OVERHEAD FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

LAX - EXTERIOR EMERGENCY EXIT LIGHT AT RIGHT NUMBER ONE INOPERATIVE. RELAMPED EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE HARNESS — DISCONNECTED (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHT AT SEAT 29B INOPERATIVE. SECURED WIRE HARNESS TO LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 29B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — CORRODED (BS 1085 S37R)

AFW - FOUND INNER SURFACE OF FUSELAGE SKIN AT STATION 1085 BETWEEN RIGHT KEEL BEAM AND STRINGER 37 RIGHT HAD CORROSION BLENDED AT DRAIN LOCATION. AREA OF DISCREPANCY IS 2.8 INCHES BY 2.3 INCHES WITH A DEPTH OF 0.266. REMOVED ALL CORROSION. PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION FOR CRACKS. ALODINED AND PRIMED BLENDED AREAS. REINSTALLED FASTENERS ON BLENDED AREAS PER MRB 2879 DATED 06 SEP 2006. RETURNED TO SERVICE WITH THE NOTED CONDITION.

Part: LIGHT — INOPERATIVE (CABIN)

SFO - EMERGENCY LIGHT AT SEAT 32B INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 32B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

SFO - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 32B INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 32AB FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 32B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — MISSING (EMERGENCY LIGHT)

MIA - ESCAPE PATH LIGHTING AT 24R MISSING SHROUD ASSEMBLY LIGHT. REPLACED ESCAPE PATH LIGHTING 24R SHROUD ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACTUATOR — INOPERATIVE (OVERWING SLIDE)

SFO - OVERWING SLIDE DOOR ACTUATED UNSUCCESSFUL WHILE STILL PINNED. REPLACED BLOW DOWN ACTUATORS. SYSTEM GROUND CHECKED NORMAL OPERATIONS.

Part: CONNECTOR — OVERSIZED (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT AT SEAT 5B INOPERATIVE. FOUND CONNECTION ON AFT LIGHT OVERSIZED. RESIZED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 5B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DISCONNECTED (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE AT STATION 870. RECONNECTED WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BURNED (CABIN)

AFW - DURING ROUTINE MX CHECK, FOUND WIRE HARNESS TO CONNECTOR EPL POWER SUPPLY WIRES CHAFED AND BURNED. INSPECTED HARNESS FOUND PLUG MISWIRED JUMPER BETWEEN PIN 24-20 WAS ACTUALLY IN POSITION 24-21. THIS A/C FLEW IN LIKE THIS EPL SYSTEM OPS CHECKED GOOD UNDER THESE CONDITIONS. HOWEVER, 4 WIRES WERE BURNED DOWN TO CONDUCTOR. INSPECTED, REPAIRED AND SECURED WIRES PER WDM CHP 20 STANDARD PRACTICES. OPS CHECK EMERGENCY LIGHTING SYSTEM, CHECKED GOOD. INSTALLED JUMPER IN CORRECT LOCATION PER SDM 33-51-14. (M)

Part: DISPLAY — MALFUNCTIONED (COCKPIT)

AFW - TCAS DISPLAY UNIT STARTED FLASHING OFF AND ON FOLLOWED BY SMOKE COMING OUT OF IT. REMOVED AND INSPECTED UNIT FOUND INTERNAL CIRCUITRY BURNED. REMOVED AND REPLACED TCAS DISPLAY UNIT. OPS CHECK GOOD. (M)

Part: WIRE — CHAFED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE CHECK OF THE FORWARD CARGO LOADING SYSTEM A CIRCUIT BREAKER WAS POPPING. WHEN RESET IT WAS OBSERVED THAT THE SMOKE WAS COMING FROM THE RIGHT LOWER SIDEWALL AREA. REMOVED PANEL AND NOTED A DAMAGED WIRE BUNDLE. POSSIBLE FUSELAGE REPAIR MAY HAVE CAUSED THE WIRES TO CHAF. INSTALLED TWO NEW CONNECTOR PLUGS AND FABRICATED BRACKET FOR CONNECTOR PLUGS. (M)

Part: SOCKET — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS DIM AT SEAT 31H THROUGH 33H. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 31H THROUGH 33H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY PATH LIGHTING AT 34H INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY PATH LIGHTING AT SEAT 34H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 10AB INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 10AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — CHAFED (CABIN)

LHR - FLT 121 - ELEC ARC REPORTED ABOVE SEAT 28HJ ALL READING LIGHTS IN AREA INOPERATIVE. APPROXIMATELY 30 MIN INTO FLIGHT, CABIN ATTENDANT AND PASSENGER REPORTED AN ELECTRICAL ARC/SPARK ORIGINATING FROM PSU/OVERHEAD BIN AT SEAT 28HJ. ALL READING LIGHTS ON RT CABIN INOPERATIVE. TEN MINUTES LATER THE REMAINING COACH CABIN READING LIGHTS BECAME INOPERATIVE. CARRIED OUT T/S AND FOUND PSS WIRING CHAFED AT OVERHEAD DECODER AT SEATS 28HJ DUE INCORRECT ROUTING OF WIRES ACCOMPLISHED AIRWORTHY REPAIR TO PSS WIRING AND CARRIED OUT ALL CHECKS OK. (M)

Part: WIRE — PINCHED (CABIN)

LHR - FLT 121 - CDG-JFK - APPROXIMATELY 30 MINUTES INTO FLIGHT PASSENGERS AND FLIGHT ATTENDANT REPORTED ELECTRICAL ARCING AND SPARKING ORIGINATING FROM PSU OVERHEAD BIN AT SEAT 28H-J. ALL READING LIGHTS ON RIGHT CABIN SIDE BECAME INOPERATIVE. ALL REMAINING CABIN READING LIGHTS ALSO BECAME INOPERATIVE. AIRCRAFT DIVERTED TO LHR AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PINCHED. CHAFFED WIRE AND ACCOMPLISHED INTERIM REPAIR PRIOR TO AIRCRAFT DEPARTURE. PERMANENT REPAIR ACCOMPLISHED AT ORD. TWO SUBSEQUENT FLIGHTS REVEALED NO REPEAT WRITE-UPS. (M)

Part: GENERATOR — FAILED (LT ENGINE)

BHX - CLIMBING AT FL250, LEFT GENERATOR DRIVE LIGHT ILLUMINATED STEADY. ACCOMPLISHED ABNORMAL PROCEDURE AND DISCONNECTED GEN DRIVE. REMOVED AND REPLACED LEFT IDG AS PER MM. OPS CHECK AND LEAK CHECK GOOD CLEARED MEL/MIC SHEET. (M)

Part: WIRE — DISCONNECTED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT LAVATORY WALL INOPERATIVE. RE-CONNECTED EMERGENCY EXIT WIRE AT LAVATORY WALL. SYSTM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — CHAFED (AFT LAVATORY)

LAX - DURING OVERNIGHT MAINTENANCE, RIGHT AFT LAVATORY EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED AFT LAVATORY EMERGENCY EXIT WIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — CHAFED (F/A SEATS)

LAX - DURING OVERNIGHT MAINTENANCE, FLIGHT ATTENDANTS EMERGENCY EXIT LIGHT AT SEAT INOPERATIVE. REPAIRED FLIGHT ATTENDANTS EMERGENCY EXIT CONNECTOR AT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — SHORTED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT SEAT LIGHTS FROM 32 TO 41 AB INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT ASSY DUE TO SHORTED WIRE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — SHORTED (ROW 2-3)

ORD - FLT 955 - SEAT 2 A WIRING HARNESS AT FLOOR PANEL SHORTED OUT CAUSING A FLASHING ARC AS HIGH AS THE WINDOW. BOTH SEATS AT 2 A/B AND 3 A/B HAVE LOST ALL AUDIO VISUAL AND SEAT CONTROLS. AT TIME OF SHORTING, SMOKE WAS SMELLED IN FIRST CLASS. INSPECTED AND FOUND SEVERAL WIRES SHORTED TO GROUND ADJACENT TO 3A FOOT REST AT FLOOR/SIDEWALL WIRE RUN. INSTALLED GROMMET AND REPAIRED POWER FOOT REST WIRING TO SEATS 2 A/B, 3 A/B, 4 A/B. ALL SEAT CONTROLS OPS CHECK NORMAL. AIRCRAFT OK FOR SERVICE. (M)

Part: WIRE — SHORTED (ROW 2-4)

MIA - FLT 995 - AFTER TAKEOFF, SEAT WIRING HARNESS AT ROW 2AB SHORTED OUT CAUSING AN ARC AND SMOKE IN FIRST CLASS CABIN. FLIGHT AIR INTERRUPTED AND RETURNED TO MIA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND SEVERAL WIRES SHORTED TO GROUND ADJACENT TO PASSENGER SEAT 3A FOOT REST. MAINTENANCE INSTALLED A GROUND GROMMET AND REPAIRED SHORTED WIRING TO POWER FOOT RESTS AT SEAT ROWS 2AB THROUGH 4AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (ROW 4 AB)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH MARKER LIGHT INOPERATIVE AT SEAT 4AB. RESEATED CONNECTOR AT SEAT 4AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 31H INOPERATIVE. RESET EMERGENCY EXIT SEAT LIGHT CONNECTOR AT SEAT 31H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: FLOORBEAM — CORRODED (BS 790-809)

AFW - FOUND AND BLENDED FIVE SMALL AREAS OF CORROSION ON THE UPPERS SURFACE OF THE LONGITUDINAL FLOORBEAM. THE BLENDOUTS EXCEED SRM MAX ALLOWABLE LIMITS. ROTOPEENED, TREATED, PRIMED AND FILLED BLEND AREAS. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1634. (M)

Part: FLOORBEAM — CORRODED (BS 1480)

AFW - FLOORBEAM HAS CORROSION BEYOND SRM LIMITS. BLENDED AREA FLAT SO THE FASTENER WILL SEAT PROPERLY WHEN REINSTALLED AND REFINISHED AREA PER THE REF/D1 SRM SECTION. (M)

Part: SEAT TRACK — CORRODED (BS 343)

AFW - CORROSION REMOVED FROM UPPER SURFACE OF SEAT TRACK. BLENDED OUT EXCEEDED SRM MAX ALLOWABLE LIMITS. BLENDED OUT CORROSION AND REMOVED TABS ADJACENT TO THE DAMAGED AREA ALODINED AND PRIMED. APPROCHED BY ENGINEER WITH NOTED CONDITION PER MRB 767-1632. (M)

Part: WIRE — DISCONNECTED (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PAX SEAT 32H INOPERATIVE. RECONNECTED LOOSE EMERGENCY EXIT LIGHT WIRE AT PAX SEAT 32H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EGT PROBE — FAILED (LT ENGINE)

LAX - FLT 38 - EGT LEFT ENGINE WENT TO 30 MOMENTARILY ON APPROACH. ITEM PREV ACCOMP AT ORD NR 133275. REF L/P 4254905. REMOVED AND REPLACED 3 EGT PROBES ON LOWER HARNESS. SYTEM GROUND CHECK NORMAL ON GROUND. (M)

Part: CONNECTOR — BROKEN (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 24H INOPERATIVE. REPLACED BROKEN PINS IN EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 24H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HOUSING — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 4B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT HOUSING AT PAX SEAT 4B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — DAMAGED (NR 4 SLAT)

AFW - FOUND NR 4 SLAT HAS A GOUGE WORN INTO LOWER SKIN SURFACE. DYE PENETRANT CHECKED, TAP TESTED AND RESTORED SURFACE FINISH PER ENGINEERING MRB 767-976. (M)

Part: EEL CONTROL PNL — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS COME ON WITH SWITCH IN DISARM POSITION. REPLACED CONTROL PANEL. SYSTEM GROUND CHECKS NORMAL OPERATION. (M)

Part: FIRE LOOP — DEFECTIVE (NR 1 ENG)

JFK - FLT 59 - DURING CLIMB-OUT, BOTH A AND B ENGINE FIRE WARNING LOOPS ON NR 1 ENGINE ILLUMINATED. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED BOTH FIRE WARNING LOOP DETECTORS. SYSTEM GROUND CHECKS NORMAL OPERATION. (W)