N182AN

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 53,160 hrs · 18,550 cycles

EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. DURING TEST, FOUND EMERGENCY LIGHT CONNECTOR AT SEAT 26D LOOSE. RECONNECTED THE CONNECTOR AND ACCOMPLISHED AN OPS CHECK IAW AMM 33-51-11.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 53,160 hrs · 18,550 cycles

AFT CARGO DOOR SKIN LOWER FORWARD CORNER FOUND CRACKED. REPAIRED THE SKIN IAW SRM 52-30-01-2R-4.

Part: SPLICE — DEFECTIVE (CABIN) · airframe 52,640 hrs · 18,333 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY EXIT DIRECTIONAL POINTER AT LAVATORY M IS INOPERATIVE. FOUND DEFECTIVE SPLICE AT LAVATORY M EMERGENCY EXIT DIRECTIONAL POINTER LIGHT. REPAIRED SPLICE IAW SWPM 20-30-12. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,640 hrs · 18,333 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY LIGHT FROM ROW 26 THROUGH BACK OF ACFT ARE DIM. R & R THE BATTERY PACK AT LOCATION M10801 IAW AMM 33-51-07. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,640 hrs · 18,333 cycles

AIRCRAFT WAS GROUNDED. RED EMERGENCY LIGHT AT SEAT 18D IS INOPERATIVE. R & R RED EMERGENCY LIGHT ASSY IAW AMM 33-51-11. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,640 hrs · 18,333 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY LIGHTS IN ROWS 1 THROUGH 5 ARE DIM. R & R BATTERY PACK AT M10798 IAW AMM 33-51-07. OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 52,589 hrs · 18,307 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. LANDING UNEVENTFUL. ACFT NOT OVERWEIGHT. DUIRNG DESCENT CREW REPORTED MULTIPLE UNUSUAL AUDIBLE AND VISUAL WARNINGS CULMINATING IN A DUAL FLIGHT MANAGEMENT COMPUTER FAILURE. MAINTENANCE ACCOMPLISHED FIM 34-61-00, BITE CHECKS OF BOTH FLIGHT MANAGEMENT COMPUTERS, MCM 2900. OPS CHECK OF BOTH FLIGHT MANAGEMENT COMPUTERS IAW AMM 34-61-00, VERIFIED SOFTWARE IAW IPC 34-61-01-01B. NOT FAULTS FOUND.

Part: UNKNOWN — SMOKE (LAVATORY) · airframe 51,687 hrs · 17,946 cycles

AIRCRAFT WAS GNDED. EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING DESCENT RECEIVED A FIRE WARNING DETECTION FROM FIRST CLASS LAVATORY. NO SMELL NOTED. SMOKE, HAZE & POWDER OBSERVED WHEN LAVATORY DOOR OPENED. ACCOMPLISHED EXTENSIVE TROUBLESHOOTING & THOROUGH EXAMINATION OF FIRST CLASS LAVATORY. NO FAULTS OR ABNORMALITIES NOTED.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,685 hrs · 17,945 cycles

AIRCRAFT WAS IN BASE MX. FUSELAGE SKIN CORRODED FWD OF AFT LAVATORY SERVICE PAN ASSEMBLY AT APPROX FS 1681 & STRINGER 26R. REPAIRED SKIN IAW EA 256605.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,685 hrs · 17,945 cycles

AIRCRAFT WAS IN BASE MX. L4 DOOR GIRT BAR ATTACH FITTING AT FS 1677 & LBL 61 IS CORRODED. R & R FITTING IAW AARD 51-00-05 REPAIR NR 1 & EA 257262.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,685 hrs · 17,945 cycles

AIRCRAFT WAS IN BASE MX. AFT CABIN DECK HAS MULTIPLE AREAS OF CORROSION, BETWEEN FS 1680 & 1720. R & R AFT CABIN DECK PLATE IAW AARD 51-00-05 & DWG 146N5300.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,685 hrs · 17,945 cycles

AIRCRAFT WAS IN BASE MX. CABIN FLOOR L ANGLE AT FS 1661, BETWEEN LBL 59 & LBL 64. R & R ANGLE IAW SRM 51-40-02 & DWG 146N8722.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,685 hrs · 17,945 cycles

AIRCRAFT WAS IN BASE MX. MAIN CABIN FLOOR THRESHOLD SUPPORT AT FS 1660 & LBL 61 IS CORRODED. R & R SUPPORT IAW SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,685 hrs · 17,945 cycles

AIRCRAFT WAS IN BASE MX. R1 DOOR LOWER SILL CREASE ANGLE IS CORRODED, BETWEEN FS 376 & 384. R & R CREASE ANGLE IAW AARD 51-00-05.

Part: FLOORBEAM — CORRODED (BS 378) · airframe 51,685 hrs · 17,945 cycles

AIRCRAFT WAS IN BASE MX. TOP OF CABIN FLOORBEAM CORRODED AT BS 378 & RBL 60. REPAIRED FLOORBEAM IAW SRM 53-00-51-2R-8.

Part: SKIN — CORRODED (LT WING) · airframe 51,685 hrs · 17,945 cycles

AIRCRAFT WAS IN BASE MX. LT WING TANK OVERWING FILL PORT FAILS BONDING RESISTANCE CHECK DUE TO CORROSION. REPAIRED IAW SRM 57-20-01-2R-6 & EA 256633.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,685 hrs · 17,945 cycles

AIRCRAFT WAS IN BASE MX. CORROSION ON DOOR SILL AROUND FASTENER HOLES & OR NUTPLATES AT FS 1385. R & R SILL PANEL IAW SRM 51-10-02, SRM 51-20-01 & AARD 51-00-05-1.

Part: BULKHEAD — WORN (FUSELAGE) · airframe 51,685 hrs · 17,945 cycles

AIRCRAFT WAS IN BASE MX. APU COMPARTMENT FWD BULKHEAD AT FS 188.2 HAS A WEAR MARK, 6 INCHES FROM THE BOTTOM AT RBL 7.5. ACCOMPLISHED DOUBLER REPAIR IAW SRM 53-80-08-2R.

Part: LIGHT — BROKEN (CABIN) · airframe 50,971 hrs · 17,690 cycles

ESCAPE PATH LIGHT BROKEN AT SEAT 36D. R & R ESCAPE PATH LIGHT AT SEAT 36D IAW AMM 33-51-05.

Part: CONTACT — DIRTY (CABIN) · airframe 50,558 hrs · 17,538 cycles

R3 DOOR EMER LIGHTS WILL NOT ILLUMINATE. SECURED & CLEANED CONTACTS. PERFORMED OPERATIONAL CHECK. SYS CHECKED NORMAL.

Part: CONTACT — DIRTY (CABIN) · airframe 50,558 hrs · 17,538 cycles

L1 DOOR EMER LIGHTS WILL NOT ILLUMINATE. SECURED & CLEANED CONTACTS. PERFORMED OPERATIONAL CHECK. SYS CHECKED NORMAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 49,036 hrs · 16,970 cycles

FUSELAGE SKIN DENTED AT STATION 1397 BETWEEN STRINGERS 27 & 29 RT. REPAIRED IAW EA B757-53-037229 DATED 11/4/2014.

Part: TRANSDUCER — INOPERATIVE (ANTI-SKID SYS) · airframe 48,145 hrs · 16,652 cycles

CREW REPORTED ANTI-SKID LIGHT CAME ILLUMINATED AFTER TAKEOFF. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED NR 7 ANTI-SKID TRANSDUCER. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,701 hrs · 16,490 cycles

FIRST CLASS GALLEY SIDE MOUNTED EMERGENCY EXIT LIGHT AISLE ILLUMINATION INOPERATIVE. REPLACED GALLEY EMERGENCY EXIT LIGHT, OPERATIONS CHECKED NORMAL.

Part: BEAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 44,272 hrs · 15,233 cycles

AFT CARGO DOOR LOWER BEAM (INBOARD CHORD) HAD CORROSION. CLEANED AREA AND ACCOMPLISHED NESTED ANGLE REPAIR PER EA B757-52-029325.

Part: STIFFENER — GOUGED (RT WING) · airframe 44,272 hrs · 15,233 cycles

RIGHT WING INBOARD OF 32 PYLON, LEADING EDGE INTERIOR, UNDER PANEL 611GB, PNEUMATIC DUCT MOUNT GOUGED SPAR VERTICAL STIFFENER (STREAMER ATTACHED). REMOVED AND REPLACED VERTICAL STIFFENER PER BAC DWG 112N2038 AND 112N2002 REVISION D AND SRM 51-40-02.

Part: PUMP — INOPERATIVE (FUEL SYSTEM) · airframe 44,193 hrs · 15,209 cycles

DFW INFLIGHT MIA-SEA. CREW REPORTED LEFT CENTER FUEL BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT. FLIGHT DIVERTED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT FUEL PUMP OVERRIDE MOTOR IMPELLER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: O-RING — CUT (WEATHER RADAR) · airframe 42,866 hrs · 14,720 cycles

MIA - CREW REPORTED WEATHER RADAR FAILED. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. FOUND UPPER WAVE GUIDE O-RINGS CUT. REPLACED BOTH O-RINGS ON UPPER WAVEGUIDE AND WEATHER RADAR ANTENNA. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CHARGER — DEFECTIVE (MAIN BATTERY) · airframe 41,990 hrs · 14,406 cycles

MCO INFLIGHT STL-MIA. CREW REPORTED MAIN BATTERY CHARGER EICAS STATUS MESSAGE. COULD NOT VERIFY REASON OR ISSUES OF BATTERY STATUS. EMERGENCY DECLARED FLIGHT DIVERTED MCO LANDED WITHOUT INCIDENT. REPLACED MAIN BATTERY CHARGER THAT WAS BAD. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 40,884 hrs · 13,979 cycles

CREW REPORTED DURING CLIMBOUT, GOT AMBER LOW OIL PRESSURE WARNING, FOLLOWED BY RED LOW OIL PRESSURE WARNING ON LEFT ENGINE. PULLED THROTTLE BACK TO IDLE AND LEFT ENGINE AUTO SHUTDOWN. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE ON 12/26/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FITTING — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 40,532 hrs · 13,846 cycles

CORROSION ON T-CAP INSIDE AFT CARGO DOOR, LOWER EDGE ABOVE LOWER INTERCOSTALS. INSTALLED REAPIR PER SRM 51-70-12-0G AND EA B757-52-020269.

Part: SKIN — DENTED (L4 DOOR) · airframe 40,532 hrs · 13,846 cycles

DENT IN DOOR SKIN DOOR LEFT NUMBER 4 BOTTOM RIGHT CORNER. INSTALLED DOUBLER REPAIR PER SRM 52-10-01-2R REPAIR 7.

Part: CONNECTOR — BURNED (COFFEMAKER) · airframe 37,986 hrs · 12,893 cycles

DFW - FLIGHT ATTENDANTS REPORTED ELECTRICAL ODOR IN CABIN. ODOR WENT AWAY AFTER UTILITY BUSSES WERE TURNED OFF. EMERGENCY DECLARED, FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND FIRST CLASS NUMBER 1 COFFEEMAKER TRAY CONNECTOR BURNT. REPLACED TRAY. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 37,808 hrs · 12,834 cycles

JFK - FLIGHT ATTENDANT REPORTED SMOKE COMING FROM FIRST CLASS GALLEY COFFEEMAKER. FLIGHT ATTENDANT USED HALON FIRE EXTINGUISHER. FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. AFTER ARRIVAL REMOVED BOTH FIRST CLASS GALLEY COFFEEMAKERS AND INSPECTED THE AREA. NO ABNORMALITIES NOTED. REPLACED BOTH COFFEEMAKERS AS PRECAUTIONARY. REPLACED HALON EXTINGUISHER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PAN — SCRATCHED (L4 DOOR) · airframe 35,559 hrs · 12,069 cycles

HANDLE PAN SCRATCHED ON LEFT NUMBER 4 DOOR 2 PLACES. REMOVED AND REPLACED HANDLE PAN ON LEFT NUMBER 4 DOOR PER ESO 90108.

Part: SKIN — DENTED (LE SLAT) · airframe 35,559 hrs · 12,069 cycles

RIGHT WING NUMBER 10 SLAT DENTED ON NOSE BEAM SKIN. CUT OUT DENTED AREA AND INSTALLED A FLUSH PATCH REPAIR PER AARD 57-43-00.

Part: BLADES — DAMAGED (NR 1 ENGINE) · airframe 34,715 hrs · 11,786 cycles

DURING TAKEOFF CREW REPORTED A BIRD STRIKE ON LEFT ENGINE OUTER FLAP. RETURNED TO MAR AND LANDED WITHOUT INCIDENT. FOUND FAN BLADES 9, 10 AND 11 DAMAGED ON LEFT ENGINE AND SOME DENTS TO ICE IMPACT PANEL AND SOUND SUPPRESSOR PANEL. REPAIRED PANELS AND REPLACED FAN BLADES.

Part: CONNECTOR — INOPERATIVE (CABIN)

DFW - FORWARD EMERGENCY LIGHT ON SEAT 1D INOPERATIVE. REPLACED PLUG ON SEAT 1D FORWARD EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 19D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 19D.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY EXIT SIGN ABOVE LEFT NUMBER 2 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SIGN ABOVE LEFT NUMBER 2 DOOR.

Part: OVEN — DIRTY (ZONE 200) · airframe 32,797 hrs · 11,117 cycles

MIA CREW REPORTED SMOKE IN CABIN. EMERGENCY DECLARED RETURNED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND FIRST CLASS OVENS WITH SPILLED GREASE. CLEANED DEBRIS FROM BOTH OVENS. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)

Part: TRANSMISSION — TRIPPED (TE FLAPS) · airframe 32,653 hrs · 11,062 cycles

BOS DURING APPROACH RECEIVED FLAP DISAGREE INDICATION. EMERGENCY DECLARED LANDED BOS WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND NR 1 FLAP TRANSMISSION LEFT WING OUTBOARD OVERLOAD INDICATOR TRIPPED. REPLACED LEFT OUTBOARD TRAILING EDGE FLAP DRIVE TRANSMISSION AND TEE GEARBOX. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS)

DFW - SEAT MOUNTED EMERGENCY PATH LIGHTING AT SEAT 10D INOPERATIVE. REPAIRED CONNECTOR AT SEAT 10D.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - SEAT MOUNTED EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT AFT COACH CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,632 hrs

DFW - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SENSOR — INOPERATIVE (NLG)

MIA INFLIGHT T973/13DEC - RECEIVED NOSE LANDING GEAR AIR GROUND SWITCH DISAGREE MESSAGE. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION. REPLACING SENSOR.

Part: LIGHT — MISSING (CABIN) · airframe 28,116 hrs

SFO- EMERGENCY LIGHT AT AFT SEAT 18A HAS LENS BROKEN OFF WALL MOUNT. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT AFT SEAT 18A. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

MIA - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 16D TO 26D INOPERATIVE. SECURED CONNECTOR FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 16D TO 26D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - FOUND EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT ON EXTERIOR OF RIGHT NUMBER THREE DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT ON THE EXTERIOR OF RIGHT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

SFO - FOUND EMERGENCY LIGHT AT SEAT 28D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT AT OVERHEAD SEAT 3B INOPERATIVE. RELAMPED EMERGENCY LIGHT AT OVERHEAD SEAT 3B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — LOOSE (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 9D LOOSE. SECURED LOOSE EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (SEAT 16D)

DFW - AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT SEAT 16D INOPERATIVE. REPLACED THE AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING FROM ROW 16D-32D INOPERATIVE. SECURED EMERGENCY EXIT PATH LIGHTING CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (CABIN)

ORD - FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN FIRST CLASS AND HALF OF COACH SECTIONS. REPAIRED WIRING AT FORWARD SEAT AND R2 GALLEY AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT INOPERATIVE AT CLASS DIVIDER. REPLACED LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT 1E THROUGH 6E INOPERATIVE. RE-SEATED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR AT 1E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (GALLEY)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONTROL MODULE — FAILED (ROW 9-17)

JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS FROM ROW 9 TO ROW 17 INOPERATIVE. REPLACED CONTROL MODULE. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT 2L LAVATORY INOPERATIVE. RESECURED CONNECTOR TO EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT 2L LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — LOOSE (R4 DOORWAY)

DFW - DURING OVERNIGHT MAINTENANCE R4 DOOR AFT EXIT SIGN INOPERATIVE. RECONNECTED WIRE ON EMERGENCY EXIT SIGN WIRE QUICK DISCONNECT. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)