N186AN

Part: OIL SYSTEM — LEAKING (NR 2 ENGINE)

DURING CRUISE NO. 2 ENGINE LOST 4 QTS IN 1 HRS

Part: GENERATOR — LEAKING · airframe 64,742 hrs · 16,189 cycles

AIRCRAFT WAS GROUNDED: FLIGHT DIVERTED TO CUN ON ACCOUNT OF LOW OIL PRESSURE INDICATION. AN EMERGENCY WAS DECLARED. MAINTENANCE REPORTS DURING ENGINE LEAK INSPECTION FOUND LEAK FROM DEDICATED GENERATOR. ACCOMPLISHED TASK CARD FOR HIGHER OIL CONSUMPTION, TROUBLESHOTING IAW JOB CARD 79-92-11. REMOVED AND REPLACED RH ENGINE DEDICATED GENERATOR IAW AMM 73-21-08. RAN RH ENGINE, NO LEAKS NOTED. OK FOR SERVICE.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 64,734 hrs · 16,185 cycles

AIRCRAFT IN BASE MAINTENANCE: L4 DOOR EMERGENCY LIGHT MOMENTARY SWITCH WOULD NOT TURN ON EMERGENCY LIGHTS. REPAIRED WIRE BY SPLICE PER SWPM 20-30-12 AND PERFORMED SATISFACTORY OPERATIONAL CHECK OF LIGHTS PER MM 33-51-00.

Part: STRAP — CORRODED (BS 1787) · corrosion level 2 · airframe 64,735 hrs · 16,185 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON APU COMPARTMENT INTAKE DUCT SUPPORT RING STRAP AT BS 1787.64 AND S5R. REPLACED SUPPRT RING STRAP PER AARD 51-00-05-1.

Part: SKIN — CORRODED (RT WING TE FLAP) · airframe 64,735 hrs · 16,185 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING INBOARD TRAILING EDGE FLAP UPPER SKIN AT MFS 91.2. REPLACED FLAP PER TASK CARD 27-94-12.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,863 hrs · 15,649 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE FOUND THE R2 DOOR FWD EXIT SIGN DIM. REPLACED BATTERY PACK AND CHARGER M10952 IAW AMM 33-51-07. R2 DOOR FWD EXIT SIGN CKS GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 62,863 hrs · 15,649 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE FOUND THE L2 DOOR FWD EXIT SIGN VERY DIM. REPLACED BATTERY PACK AND CHARGER M10952 IAW AMM 33-51-07. L2 DOOR FWD EXIT SIGN CHECKS GOOD. SEE SDR # AALA201904109016.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,863 hrs · 15,649 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE FOUND THE L2 DOOR FWD EXIT SIGN VERY DIM. REPLACED BATTERY PACK AND CHARGER M10952 IAW AMM 33-51-07. L2 DOOR FWD EXIT SIGN CHECKS GOOD. SEE SDR # AALA201904109032.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 62,863 hrs · 15,649 cycles

MAINTENANCE FOUND THE R2 DOOR FWD EXIT SIGN DIM. REPLACED BATTERY PACK AND CHARGER M10952 IAW AMM 33-51-07. R2 DOOR FWD EXIT SIGN CHECKS GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,863 hrs · 15,649 cycles

AIRCRAFT WAS NOT GROUNDED: R2 DOOR FORWARD EXIT SIGN WAS DIM. MAINTENANCE REPLACED BATTERY PACK PER AMM 33-51-07 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,863 hrs · 15,649 cycles

AIRCRAFT WAS NOT GROUNDED: L2 DOOR FORWARD EXIT SIGN WAS VERY DIM. MAINTENANCE REPLACED CHARGER PER AMM 33-51-07 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: COMPUTER — MALFUNCTIONED (THRUST MANAGE) · airframe 62,617 hrs · 15,578 cycles

THE PILOT REPORTED, THAT THE LEFT ENGINE DID NOT ACCELERATE TO COMMAND SECTOR LIMITS. EPR WILL SOMETIMES STAY PUT WHILE N1 ACCELERATES TO 2 - 3%. N1 VIBRATION HIGH 1.6, 1.4, 1.8. THE AIRCRAFT WAS GROUNDED. MAINTENANCE PERFORMED AN EPR P1 LEAK CHECK WITH NO FAULTS FOUND. INSPECTED EPR P1 & PF LINES WITH NO FAULTS FOUND. REMOVED AND REPLACED THE THRUST MANAGEMENT COMPUTER AND PERFORMED ALL REQUIRED TESTS, RAN ENGINES. NO FAULTS NOTED.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 60,993 hrs · 15,118 cycles

AFTER LOWERING GEAR HANDLE, THE RIGHT GEAR DID NOT SHOW DOWN WITH GEAR DISAGREE MESSAGE. LIGHTS CHECKED NORMAL, CAME DOWN WITH ALTERNATE GEAR EXTENSION. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. FOUND A HYDRAULIC LEAK ON THE RIGHT GEAR TRUCK POSITIONER PRESSURE LINE. REPLACED THE LINE IAW AMM 20-10-10.

Part: FMC — INTERMITTENT (NR 1) · airframe 60,973 hrs · 15,113 cycles

SHORTLY AFTER TAKEOFF, BOTH LEFT AND RIGHT FLIGHT MANAGEMENT COMPUTERS LOCKED UP AND WERE INOPERATIVE. CREW WAS DIRECTED MY MAINTENANCE CONTROL NOT TO ATTEMPT CIRCUIT BREAKER RESET. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE NR 1 FLIGHT MANAGEMENT COMPUTER IAW AMM 34-61-01.

Part: FMC — INTERMITTENT (NR 2) · airframe 60,973 hrs · 15,113 cycles

SHORTLY AFTER TAKEOFF, BOTH LEFT AND RIGHT FLIGHT MANAGEMENT COMPUTERS LOCKED UP AND WERE INOPERATIVE. CREW WAS DIRECTED MY MAINTENANCE CONTROL TO ATTEMPT CIRCUIT BREAKER RESET. THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED THE NR 2 FLIGHT MANAGEMENT COMPUTER IAW AMM 34-61-01.

Part: LIGHT — DEFECTIVE (ROW 1AB) · airframe 60,079 hrs · 14,902 cycles

OVERHEAD EMERGENCY LIGHT DEFECTIVE ROW 1AB. REPAIRED THE LIGHT WITH A SERVICEABLE TRIM SURROUND AND LENS LATCH. OPS CHECKED GOOD IAW AMM 33-51-05.

Part: LIGHT — DAMAGED (CABIN) · airframe 60,079 hrs · 14,902 cycles

OVERHEAD EMERGENCY LIGHT DAMAGED AT 1AB. REPAIRED THE LIGHT WITH A SERVICEABLE TRIM SURROUND AND LENS LATCH. OPS CHECKED GOOD IAW AMM 33-51-05.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,077 hrs · 14,901 cycles

EMERGENCY EXIT AISLE LIGHTS INOPERATIVE AT SEATS 22DEF, 23ABC, AND 25DEF. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-07. OPS CHECKED NORMAL.

Part: CHANNEL — CORRODED (BS 1714) · corrosion level 2 · airframe 60,076 hrs · 14,900 cycles

CORROSION FOUND ON THE AFT DECK PLATE HAT CHANNEL AT BS 1714 AT CENTERLINE. REPLACED THE HAT CHANNEL IAW 51-00-51-1, AND DRAWING 146N5300-79.

Part: LIGHT — INOPERATIVE (SEAT 2EF) · airframe 60,076 hrs · 14,900 cycles

SEAT MOUNTED SEAT EMERGENCY LIGHT 2 E/F INOPERATIVE. REPAIRED THE SEAT MOUNTED EMERGENCY LIGHT.

Part: LENS — DETACHED (CABIN) · airframe 60,065 hrs · 14,895 cycles

AIRCRAFT WAS NOT GROUNDED. COVER CLOSE TO FLOOR NEXT TO FIRST CLASS GALLEY OFF. INSTALLED EMERGENCY LIGHT LENS TO THE ABOVE LOCATION DESCRIPTION PER AMM 33-51-00.

Part: LENS — MISSING (CABIN) · airframe 59,442 hrs · 14,686 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHT LENS COVER FOUND MISSING BY CABIN CREW AFTER PUSHBACK. INSTALLED LENS COVER. OPERATIONAL CHECK GOOD.

Part: DOOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 59,046 hrs · 14,576 cycles

L2 EMERGENCY DOOR WILL NOT CLOSE. ADJUSTED DOOR GUIDE ARM AND DOOR STOPS IAW AMM 52-11-00. LEAK AND OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: LENS — MISSING (EXIT SIGN) · airframe 59,032 hrs · 14,572 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN FLOOR LEVEL BY THE R1 DOOR AROUND THE CORNER FROM THE GALLEY HAS A MISSING LENS COVER. REPLACED LENS (LIGHT) COVER PER AMM 33-51-00. OPERATIONAL CHECK GOOD.

Part: MECHANISM — INOPERATIVE (L2 DOOR ARMING) · airframe 58,871 hrs · 14,537 cycles

L2 DOOR ESCAPE SLIDE ARMED INDICATOR WILL NOT ARM PROPERLY. ARM INDICATOR WILL NOT POP OUT TO ARMED POSITION. SLIDE LIGHT FUNCTIONS PROPERLY. REMOVED AND REPLACED ARM-DISARM MECHANISM ASSEMBLY IAW AMM 52-11-20. OPS CHECKED GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 58,217 hrs · 14,376 cycles

AIRCRAFT WAS GROUNDED. FIRST CLASS GALLEY DIRECTIONAL EXIT LIGHT IS INOPERATIVE. SECURED CONNECTOR AT THE POWER SUPPLY. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 58,216 hrs · 14,376 cycles

FIRST CLASS GALLEY DIRECTIONAL EMERGENCY EXIT LIGHT INOPERATIVE. SECURED THE CONNECTOR AT POWER SUPPLY. OPS CHECKED IAW MM 33-51-01. ALL CHECKED NORMAL. THE AIRCRAFT WAS GROUNDED.

Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 57,879 hrs · 14,289 cycles

EMERGENCY EXIT SIGN AT R1 DOOR IS MISSING. REPLACED THE SIGN ASSEMBLY IAW AMM 33-51-10. OPERATIONAL CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 57,508 hrs · 14,196 cycles

FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT AFT GALLEY RIGHT OTBD SEAT IS DIM. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-00. OPERATIONAL CHECKED GOOD.

Part: FILTER — CLOGGED (ZONE 200) · airframe 57,168 hrs · 14,097 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. MIA-BSB FLIGHT RETURNED TO MIA ACCOUNT BOTH WEATHER RADAR FAILURE INDICATION. OVERWEIGHT LANDING UNEVENTFUL. REMOVED AND REPLACED EQUIPMENT COOLING FILTER IAW AMM 21-58-00 AND WEATHER RADAR TRANSCEIVER IAW AMM 34-43-01 (AALA20170302014). OPERATIONAL CHECK GOOD.

Part: TRANSCEIVER — FAULTY (WEATHER RADAR) · airframe 57,168 hrs · 14,097 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. MIA-BSB FLIGHT RETURNED TO MIA ACCOUNT BOTH WEATHER RADAR FAILURE INDICATION. OVERWEIGHT LANDING UNEVENTFUL. REMOVED AND REPLACED EQUIPMENT COOLING FILTER IAW AMM 21-58-00 (AALA2017030201) AND WEATHER RADAR TRANSCEIVER IAW AMM 34-43-01. OPERATIONAL CHECK GOOD.

Part: SHELF — BROKEN (R1 DOOR) · airframe 56,864 hrs · 14,004 cycles

AIRCRAFT WAS GROUNDED. R1 DOOR EMERGENCY EVACUATION SLIDE SUPPORT SHELF IS BROKEN. REMOVED AND REPLACED SHELF ASSEMBLY IAW AMM 25-66-01. OPERATIONAL CHECK GOOD.

Part: TRANSCEIVER — INOPERATIVE (WEATHER RADAR) · airframe 54,848 hrs · 13,484 cycles

AIRCRAFT WAS NOT GROUNDED. AIR INTERRUPT, EMERGENCY DECLARED, LANDING UNEVENTFUL. ACFT OVERWEIGHT. DURING CRUISE WEATHER RADAR FAILED WITH NO WEATHER DATA MESSAGE ON BOTH DISPLAYS. R & R WEATHER RADAR TRANSCEIVER ASSEMBLY AND ACCOMPLISHED OPS CHECK IAW AMM 34-43-11. SYS CHECKS NORMAL.

Part: O-RING — FAILED (HYDRAULIC SYS) · airframe 52,510 hrs · 12,944 cycles

LOST ALL LT SYS HYD QTY. THE FLIGHT DECLARED AN EMER INBD, LANDED WITH .18 QTY IN LT SYS. PRESS NEVER WENT TO 0 PSI. ACFT WAS REMOVED FROM SERVICE. R & R O RING FROM LT DPI FROM EDP CASE DRAIN PRESS FILTER MODULE IAW AMM 29-11-14. OPERATIONALLY CHECKED GOOD. NO LEAKS NOTED.

Part: LENS — BROKEN (CABIN) · airframe 52,294 hrs · 12,899 cycles

FORWARD FIRST CLASS LOWER RT EXIT IDENTIFIER DAMAGED IN GALLEY WALL. R & R EXIT IDENTIFIER ASSEMBLY & OPERATIONALLY CHECKED OK IAW MM 33-51-10.

Part: LENS — MISSING (CABIN) · airframe 51,683 hrs · 12,769 cycles

MISSING LENS COVER ON ONE EMER LIGHT AT SEAT 2E. INSTALLED EMER LIGHT LENS ON SEAT 2E EMER LIGHT ASSEMBLY. PERFORMED OPERATIONAL TEST IAW AMM 33-51-11. SYS CHECKED NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 49,798 hrs · 12,321 cycles

AIR INTERRUPT, DIVERTED & EMER DECLARED. LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CRUISE A SMELL OF FUEL IN THE CABIN WAS REPORTED. ACCOMPLISHED ENG RUN UP TEST IAW AMM 71-00-00. PNEUMATIC SYS TEST IAW AMM 36-11-00 & DOOR HEATER OPERATION IAW AMM 21-45-06 WITH NO FUEL SMELL FOUND. SYS CHECKED NORMAL.

Part: MODULE — DEFECTIVE (CABIN) · airframe 49,776 hrs · 12,313 cycles

SEAT MOUNTED EMER ESCAPE PATH LIGHTS AT ROWS 25 - 16 ARE VERY DIM. R & R SEAT MOUNTED EMER ESCAPE PATH LIGHT MODULE & BATTERY FOR ROWS 25 - 16 IAW AMM 33-51-07. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,438 hrs · 12,234 cycles

EMERGENCY EXIT LIGHT ABOVE ROW 23 SEATS ARE INOPERATIVE. R & R LAMPS IN EMER LIGHT ABOVE SEAT 23ABC IAW AMM 33-51-05. SYS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 46,683 hrs · 11,553 cycles

EMERGENCY LIGHTS AT BUSINESS CLASS, LOWER LT & RT NR 1 DOORS SIGNS & FWD GALLEY EMERGENCY LIGHTS WOULD NOT TEST. REPLACED POWER SUPPLY & BATTERY PACK M10798. OPERATIONS CHECKED NORMAL.

Part: GENERATOR — MALFUNCTIONED (LT ENGINE) · airframe 46,224 hrs · 11,430 cycles

SJU INFLIGHT BGI-MIA CREW REPORTED ENG ELC INOPERATIVE WITH LT ENG MILDLY ERRATIC. EMERGENCY DECLARED FLIGHT RETURNED SJU LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT DEDICATED GENERATOR. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: SKIN — DENTED (FUSELAGE) · airframe 46,198 hrs · 11,423 cycles

DENT WITH SHARP GOUGE AT STATION 759 BETWEEN STRINGERS 17 & 18 LT. INSTALLED DOUBLER REPAIR IAW SRM 53-00-01-2R-3.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 43,414 hrs · 10,750 cycles

LEFT NUMBER 4 SLIDE LIGHT FAILED TEST. REPLACED POWER SUPPLY FOR LEFT NUMBER FOUR DOOR SLIDE LIGHT. OPS CHECK NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 41,193 hrs · 10,234 cycles

AISLE EMERGENCY EXIT LIGHT AT THE FORWARD GALLEY POSITION NEAR THE FLOOR INOPERATIVE. RECONNECTED LOOSE CONNECTORS.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,716 hrs · 10,135 cycles

FRAME IS DENTED AT STATION 1500 LEFT SIDE JUST ABOVE TRANSITION PANEL. INSTALLED REPAIR SPLICE PER SRM 51-00-07-2R 5.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,716 hrs · 10,135 cycles

HAT CHANNEL FROM STATIONS 1640 TO 1661 CORRODED. REMOVED AND REPLACED HAT CHANNEL SUPPORT PER AARD 51-00-05.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,716 hrs · 10,135 cycles

HAT CHANNEL FROM STATIONS 1661 TO 1681 CORRODED. REMOVED AND REPLACED HAT CHANNEL PER AARD 51-00-05.

Part: CABLE ASSY — FAULTY (RT IDG) · airframe 39,114 hrs · 9,788 cycles

JFK - CREW REPORTED ELECTRICAL ISSUES FOLLOWED BY RIGHT GENERATOR FAILURE. EMERGENCY DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CABLE ASSEMBLY TO RIGHT INTEGRATED DRIVE GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: IDG — FAILED (RT ENGINE) · airframe 39,110 hrs · 9,786 cycles

YQX - INFLIGHT JFK-CDG. CREW REPORTED RIGHT GENERATOR FAILED. EMERGENCY DECLARED FLIGHT DIVERTED YQX LANDED WITHOUT INCIDENT. PLACARD RIGHT GENERATOR PER MEL. FLIGHT CONTINUED TO DESTINATION. REPLACED INTEGRATED DRIVE GENERATOR AT JFK ON 11/21/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PIN — LOOSE (CONNECTOR) · airframe 37,995 hrs · 9,575 cycles

EMERGENCY PATHWAY LIGHTS AT SEAT 4E INOPERATIVE. FOUND PIN LOOSE IN CONNECTOR AT SEAT 4EF. SECURED PIN IN CONNECTOR. OPS CHECK NORMAL.

Part: TAPE — DEFECTIVE (HEATER SYSTEM) · airframe 35,771 hrs · 9,125 cycles

MCO - INFLIGHT ORD-SJU. PASSENGER REPORTED DOOR FRAME OF RIGHT OVERWING EXIT HOT TO TOUCH AND PLASTIC DISCOLORED. EMERGENCY DECLARED FLIGHT DIVERTED MCO LANDED WITHOUT INCIDENT. REPLACED RIGHT FORWARD CENTER HEATER TAPE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,989 hrs · 8,953 cycles

SEAT 3E EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 3E EMERGENCY LIGHT ASSEMBLY. OPS CHECK NORMAL.

Part: COFFEEMAKER — DEFECTIVE (GALLEY) · airframe 34,021 hrs · 8,764 cycles

LHR - CREW REPORTED COFFEEMAKER MADE POPPING SOUND. HAD SPARKS AND AN ELECTRICAL SMELL. CIRCUIT BREAKER PULLED. FLIGHT LANDED LHR WITHOUT INCIDENT. REPLACED COFFEEMAKER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,362 hrs · 8,641 cycles

SEAT EMERGENCY LIGHTS 9 THRU 15 ARE VERY DIM. REPLACED BATTERY PACK AT RIGHT NUMBER 2 DOOR AREA (CEILING). OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,408 hrs · 8,385 cycles

EMERGENCY LIGHT AT FIRST CLASS SEATS INOPERATIVE. REPLACED BATTERY PACK.

Part: PIN — BROKEN (EMERGENCY LIGHTS)

DFW - EMERGENCY ESCAPE PATH LIGHTING AT SEAT 32D INOPERATIVE. WIRES PULLED OUT AT SIDEWALL. REPLACED PIN AT CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHTING AT SEAT 32D.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS)

DFW - OVERHEAD EMERGENCY LIGHT AT SEAT 34C INOPERATIVE. RECONNECTED WIRING FOR OVERHEAD EMERGENCY LIGHT AT SEAT 34C.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS)

DFW - LEFT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT AFT EXTERIOR.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 28,837 hrs

SFO - EMERGENCY LIGHT AT SEAT ROW 21DEF INOPERATIVE. SECURED LOOSE WIRES AT SEAT ROW 21DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,450 hrs

DFW EMERGENCY LIGHT AT SEAT 18A INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 18A. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LIGHT — INOPERATIVE (CABIN)

SFO - OVERHEAD EMERGENCY LIGHT AT ROW 20ABC INOPERATIVE. RELAMPED EMERGENCY LIGHT AT OVERHEAD SEAT ROW 20ABC. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT AT RIGHT WALL ADJACENT TO FIRST CLASS GALLEY HAS COVER MISSING. REPLACED LENS COVER FOR EMERGENCY LIGHT AT RIGHT WALL ADJACENT TO FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — DEFECTIVE (CABIN)

LAX - EMERGENCY PATH LIGHTING IN AFT SECTION OF COACH ILLUMINATES WHEN SHIP POWER IS REMOVED. REPLACED MODULE IN AFT GALLEY FOR EMERGENCY PATH LIGHTING IN AFT SECTION OF COACH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 33D HAS BROKEN WIRE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)