N39364

Part: LIGHT — INOPERATIVE (CABIN) · airframe 106,372 hrs · 17,097 cycles

FLOOR EMER LIGHT AT A5 LAVATORY INOPERATIVE. REPLACED LAMP FOR FLOOR EMER LIGHT AT A5 LAVATORY. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 106,372 hrs · 17,097 cycles

RIGHT NR 1 DOORWAY EMER LIGHT L288 INOPERATIVE. REPLACED LAMP FOR RT NR 1 DOORWAY EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 105,888 hrs · 17,016 cycles

EMERGENCY LIGHT AT SEAT 13H INOPERATIVE. SECURED CONNECTOR & WIRING UNDER SEAT FOR EMERGENCY LIGHT AT 13H.

Part: CONNECTOR — LOOSE (CABIN) · airframe 105,888 hrs · 17,016 cycles

EMERGENCY LIGHT AT SEAT 11B INOPERATIVE. SECURED CONNECTOR UNDER SEAT AREA FOR EMERGENCY LIGHT AT SEAT 11B, OPERATIONS CHECKED NORMAL.

Part: LIGHT — NOT SEATED (CABIN) · airframe 105,888 hrs · 17,016 cycles

EMERGENCY LIGHT AT LT NR 1 DOORWAY INOPERATIVE. RESEATED LAMP FOR EMERGENCY LIGHT AT LT NR 1 DOORWAY, OPERATIONS CHECKED NORMAL.

Part: FLASHLIGHT — NO TEST (CABIN) · airframe 105,435 hrs · 16,941 cycles

LT MID GALLEY FWD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT DOES NOT TEST. REPLACE LT MID GALLEY FWD EMERGENCY FLASHLIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 105,042 hrs · 16,877 cycles

A5 LAVATORY SMOKE ALARM WENT OFF INFLIGHT. NO SMOKE WAS FOUND IN LAVATORY AT TIME OF ALARM. SMOKE DETECTOR IN LAVATORY A5 CHECKED & APPROVED FOR DEFERRAL IAW MEL 26-10B AUTH 2-488DC-C. REPLACED A5 LAVATORY SMOKE DETECTOR AT ORD ON 02/15/2014. OPERATIONS CHECKED NORMAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 105,014 hrs · 16,872 cycles

DENT IN FUSELAGE SKIN AT STATION 1605 OVER STRINGER 15 RT. INSTALLED DOUBLER IAW SRM 53-00-01-2R-1.

Part: HOUSING — DEFECTIVE (EXTERIOR) · airframe 105,014 hrs · 16,872 cycles

FUSELAGE EXTERIOR, LT HAND SLIDE WING GND ILLUMINATION LIGHT DOES NOT ILLUMINATE. INSTALLED NEW LIGHT HOUSING, OPERATIONS CHECKED NORMAL.

Part: SKIN — DENTED (CARGO DOOR) · airframe 105,014 hrs · 16,872 cycles

DENT IN BULK CARGO DOOR SKIN IN LINE WITH STRINGER 26 LT ON LE. ACCOMPLISHED REPAIR IAW SRM 52-30-01-2R-6.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 105,014 hrs · 16,872 cycles

LT NR 1 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 1 DOOR EXTERNAL EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 104,355 hrs · 16,769 cycles

LT NR 2 DOOR EXIT SIGN INOPERATIVE. REPLACED LAMP FOR LT NR 2 DOOR EXIT SIGN. OPERATIONS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 102,342 hrs · 16,458 cycles

LEFT SIDE MIDDLE EMERGENCY EXIT SIGN MISSING LENS. REPLACED LENS FOR EMERGENCY EXIT SIGN. OPS CHECK NORMAL.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 101,161 hrs · 16,259 cycles

JFK - CREW REPORTED AFTER ENGINE START EICAS MESSAGE, EMERGENCY LIGHTS ILLUMINATED WITH ASSOCIATED EMERGENCY LIGHTS UNARMED LIGHT WITH SWITCH IN ARMED POSITION. REPLACED C/P EMERGENCY LIGHT OXY SWITCH PANEL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ENGINE — FAILED (RIGHT) · airframe 101,161 hrs · 16,259 cycles

JFK - CREW REPORTED FUEL ODOR THROUGH OUT CABIN ON DESCENT. EMERGENCY DECLARED FLIGHT LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE AT JFK ON 03/11/2013. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 101,161 hrs · 16,259 cycles

EXTERIOR EMERGENCY LIGHT ON RIGHT SIDE NEAR AFT CARGO DOOR LIGHT INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT ON RIGHT SIDE NEAR AFT CARGO DOOR. OPS CHECK NORMAL.

Part: IDG — LACK OF LUBE (RT ENGINE) · airframe 100,675 hrs · 16,186 cycles

BSB - INFLIGHT JFK-GIG. CREW REPORTED RIGHT INTEGRATED DRIVE GENERATOR FAILED WITH AUXILIARY POWER UNIT ON MEL. EMERGENCY DECLARED FLIGHT DIVERTED BSB LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. SERVICED RIGHT ENGINE IDG WITH OIL AND ACCOMPLISHED ENGINE RUN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,413 hrs · 15,983 cycles

FORWARD GALLEY LEFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR FORWARD GALLEY LEFT OVERHEAD EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,413 hrs · 15,983 cycles

AFT GALLEY RIGHT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR AFT GALLEY RIGHT OVERHEAD EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: WEDGE — DEBONDED (LE SLAT) · airframe 99,257 hrs · 15,960 cycles

NUMBER 5 SLAT TRAILING EDGE WEDGE DISBONDED. ACCOMPLISHED BONDED REPAIR PER SRM 57-43-02.

Part: SKIN — DEBONDED (TE FLAP) · airframe 99,257 hrs · 15,960 cycles

DISBOND ON LEFT OUTBOARD FLAP LOWER INBOARD SURFACE. ACCOMPLISHED BONDED REPAIR PER SRM 57-53-01.

Part: SKIN — DEBONDED (TE FLAP) · airframe 99,257 hrs · 15,960 cycles

DISBOND ON LEFT OUTBOARD FLAP UPPER INBOARD SURFACE. ACCOMPLISHED BONDED REPAIR PER SRM 57-53-01.

Part: SKIN — DEBONDED (TE FLAP) · airframe 99,257 hrs · 15,960 cycles

DISBOND ON LEFT OUTBOARD FLAP UPPER SURFACE. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-07.

Part: SKIN — DEBONDED (TE FLAP) · airframe 99,257 hrs · 15,960 cycles

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

Part: WEDGE — DEBONDED (LE SLAT) · airframe 99,257 hrs · 15,960 cycles

DISBOND ON NUMBER 6 SLAT TRAILING EDGE WEDGE. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-10.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 97,322 hrs · 15,629 cycles

ESCAPE PATH EMERGENCY LIGHTING INOPERATIVE LEFT SIDE IN FIRST CLASS. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 95,220 hrs · 15,314 cycles

LEFT NUMBER 4 EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK FOR LEFT NUMBER 4 EMERGENCY EXIT SIGN. OP CHECK NORMAL.

Part: SIGN — INOPERATIVE (CABIN) · airframe 95,108 hrs · 15,298 cycles

RIGHT FORWARD OVERWING INTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT SIGN. OPS CHECK NORMAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 93,816 hrs · 15,112 cycles

CORROSION WAS FOUND AT STATION 325 FLOORBEAM UPPER CAP HORIZONTAL FLANGE UPPER SURFACE. REMOVED ALL CORROSION PER 767-300 SRM 51-10. ACCOMPLISHED REPAIR PER EA B767-53-015766.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 93,816 hrs · 15,112 cycles

CORROSION TO THE UPPER CAP OF THE STATION 347 PASSENGER FLOORBEAM AT RIGHT BUTTLINE 49.5. BLENDED CORROSION PER SRM CH 51, PERFORMED DVI, FABRICATED REPAIR PARTS, TREATED AND SEALED. ACCOMPLISHED REPAIR PER EA B767-53-015781.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 3 · airframe 93,816 hrs · 15,112 cycles

CORROSION WAS FOUND UNDERNEATH STRINGER 39 LEFT BETWEEN STATIONS 1175 AND 1185. REMOVED ALL CORROSION PER 767-300 SRM 51-10. ACCOMPLISHED SURFACE HFEC INSPECTION AND OPEN HOLE HFEC INSPECTION. ACCOMPLISHED REPAIR PER EA B767-53-015662.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 3 · airframe 93,816 hrs · 15,112 cycles

CORROSION TO FORWARD CARGO CUTOUT LOWER SILL STRUCTURE AT 4 LOCATIONS BETWEEN STATIONS 540 AND 624. ACCOMPLISHED BOLT HOLE HFEC FOR REWORKED SURFACES, ALODINED AND PRIMED & SEALED. ACCOMPLISHED REPAIR PER EA 767-53-015753.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 89,212 hrs · 14,316 cycles

INFLIGHT ORD TO LHR. SHORTLY AFTER TAKEOFF THE EMERGENCY LIGHTS AT LEFT AND RIGHT NUMBER ONE DOORS ILLUMINATED. LIGHTS REMAINED ON FOR 1 HOUR BEFORE THEY EXTINGUISHED. LANDED BOS WITHOUT INCIDENT. REPLACED BATTERY PACK.

Part: SENSOR — FAULTY (LE SLAT) · airframe 88,842 hrs · 14,246 cycles

JFK - CREW REPORTED LEADING EDGE SLAT ASYMMETRY LIGHT ILLUMINATED. RETURNED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER FOUR OUTBOARD SLAT SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COVER — BROKEN (CABIN) · airframe 87,777 hrs

LHR RIGHT WING AISLE EMERGENCY EXIT SIGN BROKEN. REPLACED COVER FOR RIGHT WING AISLE EMERGENCY EXIT SIGN.

Part: PRESSURE SWITCH — FAULTED (HYD SYSTEM) · airframe 85,656 hrs

INFLIGHT - LEFT HYDRAULIC SYSTEM LOW PRESSURE INDICATION. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED LEFT HYDRAULIC PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BEZEL — MISSING (CABIN)

MIA - EMERGENCY AISLE LIGHT AT SEAT 40C MISSING LENS BEZEL. REPLACED LENS BEZEL FOR EMERGENCY AISLE LIGHT AT SEAT 40C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACTUATOR — STUCK (DEFUELING VALVE) · airframe 82,395 hrs

LIM INFLIGHT T0957/13JAN - AIRCRAFT EXPERIENCED FUEL IMBALANCE DURING FLIGHT. LANDED LIM WITHOUT INCIDENT. FOUND RIGHT DEFUELING VALVE ACTUATOR STUCK IN OPEN POSITION DUE TO ICE FORMATION. CLEANED RIGHT DEFUELING VALVE ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

ORD - EMERGENCY LIGHT DOOR HANDLE SPOT LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT DOOR HANDLE SPOT LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FASTENER — LOOSE (RT PYLON)

AFW - RIGHT HAND PYLON MID SPAR FITTINGS FASTENERS ARE TURNING IN THE ENGINE UNLOADED CONDITION. REPAIRED PER MRB 767 2870. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COFFEEMAKER — INOPERATIVE (CABIN)

NUMBER TWO COFFEE MAKER SPARKS. ITEM DEFERRED AS PDL 2599J AUGH 119168CC. PULLED CIRCUIT BREAKER AND COLLARED.

Part: SKIN — WORN (LT WING)

AFW - LEFTHAND LOWER WING OF SKIN HAS TWO AREAS OF WEAR CAUSED BY WING TO BODY PANELS AT WING BUTTLINE 103 AND 105. WEAR IS BEYOND SRM LIMITS. AREA IS 36 BY 2.0 INCHES WITH A DEPTH OF 0.023 INCHES. BLEND THE WORN AREA PER SRM 51 20 01 AND DYE PENETRANT INSPECT TO ENSURE THE REWORKED AREA IS FREE OF DEFECTS. ROTOPEEN PER SOPM 20 10 03 AND REFINISH. APPLY THE TEFLON PAINT PER DRAWING 110T3102.

Part: SILL — CORRODED (FUSELAGE)

AFW - LEFTHAND LOWER SILL EMERGENCY EXIT OUTER CHORD AT STATION 861 HAD CORROSION BLENDED FROM UPPER FLANGE. AREA OF CORROSION IS 0.9 BY 3.7 WITH A DEPTH OF 0.062. REMOVED CORROSION AND DYE CHECKED AREA FOR CRACKS. HFEC THE HOLES WHERE FASTENERS WERE REMOVED. REFINISH THE BLENDED AREA WITH ALODINE AND TWO COATS BMS 10 11 PRIMER. REINSTALL FASTENERS WET WITH SEALANT, ENSURED PROPERLY SEALED.

Part: FLOORBEAM — CORRODED (FUSELAGE)

AFW - TOP CAP OF FLOORBEAM AT STATION 325 RIGHT BUTTLINE 40 CORRODED. BLENDED BEYOND SRM LIMITS. AREA IS ONE INCH BY ONE INCH WITH DEPTH OF 0.10 BY 0.044 INCH FROM PARENT 0.090 INCH. REMOVED CORROSION. FABRICATED REPAIR STRAP OUT OF 301 1/2 H STAINLESS STEEL 0.050 INCH THICK. ALODINE ALL BARE ALUMINUM SURFACES. FINISHED BLENDS AND REPAIR PARTS WITH TWO COATS OF BMS10 11 PRIMER. FILLED BLEND WITH BMS 5 95 SEALANT. INSTALLED REPAIR STRAP WET WITH BMS 5 95 SEALANT. FASTENERS INSTALLED WITH 4 60 SPACING.

Part: FLOORBEAM — CORRODED (FUSELAGE)

AFW - FLOORBEAM AT STATION 347 AT RIGHT BUTTLINE 30 CORRODED. REMOVED CORROSION AT RIGHT BUTTLINE 30. THE BLEND IS 0.090 INCH BY 0.047 DEPTH FROM 0.090 INCH PARENT. VERIFIED ALL CORROSION WAS REMOVED. FABRICATED REPAIR STRAP OUT OF 301 1/2 H STAINLESS STEEL 0.050 INCH THICK. ALODINE ALL BARE ALUMINUM SURFACES. FINISHED BLENDS AND REPAIRED PARTS WITH 2 COATS OF BMS 10 11 PRIMER. FILLED BLENDS WITH BMS 5 95 SEALANT. INSTALLED REPAIR STRAP WET WITH BMS 5 95 SEALANT. FASTENERS INSTALLED WITH 4 60 SPACING.

Part: SOCKET — LOOSE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 39B INOPERATIVE. RESEATED SOCKET FOR EMERGENCY LIGHT AT SEAT 39B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS BY 1L AND 1R DOOR INOPERATIVE. SECURED EMERGENCY EXIT LIGHT BATTERY CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS BY 1L AND 1R DOOR INOPERATIVE. SECURED EMERGENCY EXIT LIGHTS CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: IDG — FAILED (RT ENG GEARBOX)

OGG - FLT 7 - DURING CRUISE, THE RIGHT GEN DRIVE LIGHT ILLUMINATED PERFORMED CHECKLIST PROCEDURE RAN APU AND CONTINUED TO DESTINATION, NO FURTHER PROBLEMS. REMOVED AND REPLACED RIGHT ENGINE IDG PER MM, OPS AND LEAK CHECK GOOD, OK FOR SERVICE. (M)

Part: IDG — MALFUNCTIONED (RT ENGINE)

RIGHT GEN DRIVE LIGHT ILLUMINATED STEADY DURING CRUISE PERFORMED ABNORMAL PROCEDURE AND DISCONNECTED DRIVE RT IDG VALVE EICAS ALSO DISPLAYED. RECONNECTED RIGHT IDG AND SERVICED IDG. C/OUT BPCU BITE TEST AND RAN ENGINE ALL INDICATIONS NORMAL. IDG OPS NORMAL. (M)

Part: LIGHT — INOPERATIVE (COCKPIT)

DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED OVERHEAD COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT FIRST CLASS GALLEY INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — BROKEN (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT STRIP BROKEN. REPLACED EMERGENCY EXIT LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: VIDEO UNIT — DEFECTIVE (ROW 2HJ)

LAX - FLT 137 - EN ROUTE LHR-LAX - LAX SMOKE WAS NOTED FROM CENTER ARM REST OF SEATS 2HJ. SMOKE STOPPED WHEN POWER TO VIDEO UNIT AT SEAT 2HJ WAS DISCONNECTED. AIRCRAFT CONTINUED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED VIDEO POWER UNIT AT CENTER ARM REST OF SEAT 2HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ELECT UNIT — DEFECTIVE (NLG)

DFW - FLT 0901 - AFTER RAISING LANDING GEAR, THE RIGHT HALF OF NOSE LANDING GEAR GREEN LIGHT REMAINED ILLUMINATED. CYCLED GEAR WITH NO SUCCESS. AIRCRAFT RETURNED DFW AND LANDED WITHOUT INCIDENT. REPLACED PROXIMITY SWITCH ELECTRONIC UNIT, ACCOMPLISHED GEAR SWING, AND SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PASSENGER SEATS 28/29B, AND 36H INOPERATIVE. RECONNECTED CONNECTOR AT SEAT 29B, RESEATED RECESSED PIN AT EMERGENCY EXIT LIGHT CONNECTOR PASSENGER SEAT 36H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LAMP — DEFECTIVE (CABIN)

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

Part: CONNECTOR — LOOSE (ROWS 36H-41H)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS BETWEEN PAX SEAT ROWS 36H THROUGH 41H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT SIDEWALL CONNECTOR AT PAX SEAT ROW 41H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PASSENGER SEATS 8 THROUGH 12 AND 35 THROUGH 41 FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTORS AT PASSENGER SEATS 8 THROUGH 12 AND 35 THROUGH 41. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: EEL INVERTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS IN MID-GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT INVERTOR AND LEFT GALLEY CROSS AISLE LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL PIN — LOOSE (CABIN)

JFK - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS ON RIGHT AISLE BETWEEN SEATS 24H THROUGH 37H INOPERATIVE. SECURED EMERGENCY EXIT FLOOR PATH LIGHT PIN AT 5702 VT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS ON THE LEFT SIDE OF BUSINESS CLASS INOPERATIVE. RESECURED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR AT 12B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS FROM 8B TO 12B INOPERATIVE. RECONNECTED CONNECTOR AT 12B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTORS — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT RT AISLE IN FIRST CLASS CABIN AND BUSINESS CLASS CABIN AND LEFT AISLE IN BUSINESS CLASS CABIN INOPERATIVE. RESECURES EMERGENCY EXIT LIGHT CONNECTORS FOUND DISCONNECTED AT PAX SEAT LOCATIONS 11B AND 11H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

JFK - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHTING AT 26AB THROUGH 39AB INOPERATIVE. REPLACED LOOSE CONNECTOR AT 39AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)