N491AA

Part: SEAL — CUT (NLG) · airframe 73,361 hrs · 38,649 cycles

RETURNED, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. NLG WOULD NOT RETRACT AFTER TAKEOFF. FOUND NLG STRUT FLAT. INSPECTION OF NLG FOUND THE SHRADER VLV SEAL CUT. PERFORMED NLG STRUT REPACK IAW AMM 32-21-02. PERFORMED GEAR SWING. SYS CHECKED NORMAL.

Part: TIRE — SEPARATED (RT MLG) · airframe 72,968 hrs · 38,409 cycles

DAMAGE TO RT INBD FLAP MIDDLE DUE TO TIRE SEPARATION. DRILLED & INSTALLED DOUBLER ON RT INBD FLAP MIDDLE IAW SRM 57-01-00-001.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,779 hrs · 38,298 cycles

CORROSION FOUND ON SKIN BETWEEN LONGERON 29 & 30 RT & STATIONS 636 TO 655. CUT OUT CORROSION & INSTALLED FILLER, DOUBLER, TRIPLER & FINGER DOUBLER IAW EA MD80-53-036412 & DWG SG09530002.

Part: SKIN — CORRODED (FUSELAGE) · airframe 72,779 hrs · 38,298 cycles

DENT & CORROSION FOUND ON SKIN AT STATION 674 BETWEEN LONGERONS 29 & 30 LT. CORROSION & DENT CUT OUT. INSTALLED FILLER, DOUBLER, TRIPLER & FINGER DOUBLER IAW EA MD80-53-036412 & DWG SG09530002.

Part: RADOME — CRACKED (FUSELAGE) · airframe 72,779 hrs · 38,298 cycles

RADOME & FAIRING AT STATION YV280 TRAILING TIP OF AFT END OF VERTICAL HAS DAMAGE TO RADOME MOUNTING RING. ACCOMPLISHED REPAIR IAW EA MD80-55-036387.

Part: FORMER — CRACKED (RT WING) · airframe 71,603 hrs · 37,638 cycles

RIGHT HAND WING LE NR 4 SLAT TRACK INBD FORMER CRACKED. INSTALLED DOUBLER IAW EA MD80-57-033945.

Part: FLAP — CRACKED (RT WING) · airframe 71,034 hrs · 37,320 cycles

FOUND 4 INCH CRACK ON RT HAND TE FLAP APPROXIMATELY 18 INCHES OTBD OF FLAP CANTILEVER. ACCOMPLISHED INTERIM REPAIR TO RT HAND TE IAW FEA AUTH 16095.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 67,751 hrs · 35,443 cycles

PREVIOUSLY BLENDED AREA ON FUSELAGE AT STATION 229 AND LONGERON 18 LEFT. INSTALLED DOUBLER REPAIR PER SRM 53-04-05 FIGURE 5 AND EA MD80-53-026234.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,751 hrs · 35,443 cycles

MID CARGO THRESHOLD DOOR BEAM CORRODED. INSTALLED DOUBLER PER AARD 53-10-00-3.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 67,751 hrs · 35,443 cycles

RIGHT CUSP SHEET IS CRACKED AT STATIONS 810 TO 812 RIGHT BUTTLINES 58 TO 60. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,751 hrs · 35,443 cycles

FORWARD SERVICE DOOR LOWER AFT JAM SUB FLOOR CORRODED AT STATIONS 200 TO 204. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,751 hrs · 35,443 cycles

CARGO AFT CX CORROSION ALONG DOOR CUTOUT BEAM UNDER DOUBLER STATION 1155 TO 1212. ACCOMPLISHED NESTED ANGLE REPAIR PER AARD 53-10-00-3 AND EA MD80-53-026045.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,751 hrs · 35,443 cycles

LEFT CUSP CORRODED AT STATION 583 OUTBOARD NUMBER 1 SEAT TRACK. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 67,751 hrs · 35,443 cycles

FLOORBOARD MOUNT HOLE IN THE CENTER OF SUB FLOOR 10 INCHES INBOARD OF AFT SERVICE DOOR LOWER JAM AT APPROXIMATE STATION 1155 DAMAGED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 67,751 hrs · 35,443 cycles

TWO EACH CRACKS AT LONGERON 3 LEFT, INBOARD AND OUTBOARD SIDE, STATION 160. INSTALLED LONGERON SPLICE REPAIR PER SRM 53-02-00 FIGURE 18.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 67,751 hrs · 35,443 cycles

CORROSION BELOW FORWARD ENTRY DOOR THRESHOLD SUPPORT ON SUBFLOOR AT STATION 164. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 67,751 hrs · 35,443 cycles

DENT AND SCRATCH LN FUSELAGE SKIN BELOW AND AFT OF FORWARD LAVATORY SERVICE AREA, STATION 294, LONGERON 24 LEFT. INSTALLED REPAIR DOUBLER PER SRM 53-04-0 FIGURE 8.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 67,751 hrs · 35,443 cycles

CABIN HAS A GOUGE IN NUMBER 3 SEAT TRACK AT STATION 568. INSTALLED PLUG IN SEAT TRACK 3 AT STATION 568 PER AARD 53-20-00-10.

Part: PAN — CRACKED (FUSELAGE) · airframe 67,751 hrs · 35,443 cycles

WINDOW AT STATION 1070 RIGHT SIDE: WINDOW RING PAN HAS CRACK BOTTOM FORWARD AT FORWARD MOST FASTENER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 67,751 hrs · 35,443 cycles

WINDOW AT STATION 1070 LEFT SIDE: WINDOW RING PAN HAS CRACK AFT UPPER AT AFT MOST FASTENER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,751 hrs · 35,443 cycles

STATION 927 AND BELOW SEAT TRACK NUMBER 5 HAS VERTICAL ANGLE CRACKED AT LOWER END. REPLACED DAMAGED VERTICAL FITTING UNDER SEAT TRACK NUMBER 5, STATION 927 PER AARD 51-00-05-1.

Part: PAN — CRACKED (FUSELAGE) · airframe 67,751 hrs · 35,443 cycles

WINDOW AT STATION 1070 LEFT SIDE: WINDOW RING PAN HAS CRACK AT FORWARD LOWER FASTENER AND AT RADIUS. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 67,751 hrs · 35,443 cycles

WINDOW AT STATION 1070 RIGHT SIDE: WINDOW RING PAN HAS CRACK AFT UPPER AT AFT MOST FASTENER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: ENGINE — FAILED (LEFT) · airframe 67,681 hrs · 35,395 cycles

BHM - INFLIGHT DFW-CLT CREW REPORTED LEFT ENGINE OIL PRESSURE LOW AND OIL QUANTITY WENT TO ZERO. CAPTAIN FOLLOWED QRH PROCEDURES AND SHUT DOWN LEFT ENGINE (SINGLE ENGINE TIME 15 MINUTES). EMERGENCY DECLARED FLIGHT DIVERTED BHM LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE AT BHM ON 08/25/2012. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 66,713 hrs · 34,859 cycles

FORWARD EMERGENCY LIGHT AT L1 DOOR IS VERY DIM. REPLACED LIGHT ASSEMBLY AT L1 DOOR. OPS CHECKED NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,713 hrs · 34,859 cycles

TAIL COMPARTMENT LIGHTS INOPERATIVE. REPLACED AND SECURED BATTERY CHARGER. OPS CHECKED NORMAL.

Part: CHARGER — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 66,713 hrs · 34,859 cycles

L1 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED AND SECURED BATTERY CHARGER. OPS CHECKED NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,713 hrs · 34,859 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER IN AFT RIGHT LAVATORY. OPS CHECKED NORMAL.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,245 hrs · 31,881 cycles

CORROSION ON FORWARD CARGO DOOR PAN STATION 370 TO 408 HORIZONTAL LEG OUTBOARD EDGE AND FORWARD VERTICAL LEG. INSTALLED NEW CARGO DOOR PAN SPLICE STATION 370 TO 427 PER SRM 53-05-00.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,245 hrs · 31,881 cycles

INTERCOSTAL IN CEILING BETWEEN STATIONS 1287 AND 1309 AT BUTTLINE 0 CRACKED AT AFT RADIUS. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-01-00.

Part: CASTING — CRACKED (SPOILER) · airframe 61,245 hrs · 31,881 cycles

LEFT WING FORWARD INBOARD CORNER OF GROUND SPOILER ACTUATOR CASTING CRACKED. REMOVED AND REPLACED CASTING PER SRM 57-01-00.

Part: SHROUD — BROKEN (CABIN) · airframe 60,507 hrs · 31,473 cycles

EMERGENCY LIGHT AT SEAT ROW 9 HAS DAMAGED SHROUD. REPLACED TWO LAMPS, LENS AND SHROUD AT ROW 9.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 58,433 hrs

LGA - SEAT MOUNTED ESCAPE PATH LIGHTING FROM ROW 20D TO 32D INOPERATIVE. REPLACED BATTERY PACK.

Part: BATTERY PACK — NOT SEATED (EMERGENCY LIGHTS) · airframe 58,433 hrs

LGA- TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. CLEANED AND RECONNECTED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 58,433 hrs

LGA - AFT STAIRS LEFT SIDEWALL EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY PATH LIGHTING BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · 57,289 cycles

LGA EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,536 hrs

LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 24 TO 26 INOPERATIVE. REPLACED BATTERY PACK AT B5 1 FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 24 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY CEILING LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. REPLACED BATTERY PACK IN OVERHEAD BIN ABOVE ROW 29 FOR INOPERATIVE EMERGENCY CEILING LIGHTS FROM ROWS 28 TO 30. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: LENS — MISSING (CABIN)

DFW - FORWARD EMERGENCY LIGHT LENS MISSING FROM SEAT 7D. REPLACED MISSING EMERGENCY LIGHT LENS AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DAMAGED (CABIN)

DFW - SIDEWALL EMERGENCY EXIT LIGHTS IN AFT STAIRWAY INOPERATIVE. REPAIRED WIRE AT STATION 1462 FOR INOPERATIVE SIDEWALL EMERGENCY EXIT LIGHTS IN AFT STAIRWAY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - EXIT EMERGENCY LIGHT AT AFT SERVICE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS AT AFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHT IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK IN OVERHEAD BIN ABOVE SEAT 20D FOR FORWARD OVERWING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY EXIT)

DFW - AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK IN OVERHEAD BIN ABOVE SEAT 20D FOR AFT OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (TAIL CONE)

EMERGENCY LIGHTS ABOVE AFT TAIL CONE ENTRANCE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ABOVE AFT TAIL CONE ENTRANCE. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED--

Part: BATTERY PACK — DEFECTIVE (EMERGENCY LIGHT)

SAT - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT THE SEAT ROW 22B CEILING LIGHT. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY EXIT LIGHT AT SEAT 7D INOPERATIVE. REPLACED AFT EMERGENCY EXIT LIGHT SOCKET AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND .25 INCH CRACK IN FUSELAGE SKIN AT RIVET HEAD. INSTALLED EXTERNAL DOUBLER PER SRM 53-01. (M)

Part: CONTACTOR — DIRTY (EMERGENCY LIGHT)

DFW NO TRIP/26 - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTS IL2-674 AND L2-637 INOPERATIVE. CLEANED EMERGENCY EXIT LIGHTS CONTACTS FOR B5-28 CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — CORRODED (TAILCONE)

DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE HANDLE LOWER EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED TAIL CONE HANDLE LOWER EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH — DIRTY (SMOKE DETECTOR)

ORD - DURING OVERNIGHT MAINTENANCE, AFT LAVATORY SMOKE ALARM RINGS CONTINUOUSLY. CLEANED TEST SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: MODULE — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS FROM SEAT 20 AFT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT MODULE AND BATTERY PACK. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHT SEAT 8D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY FLOOR PATH LIGHT INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WEB — CORRODED (CABIN)

TUL - FOUND CUSP SHEET CORRODED STATION 1085-1095. INSTALLED DOUBLER ON CUSP PER SRM 53-01 FIG 4-3. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

TUL - FOUND CRACK AT AFT UPPER END. INSTALLED NEW INTERCOSTAL WITH ORIGINAL TYPE FASTENERS SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND CORROSION ON SEAT TRACK AND MOUNTING FLANGES, TRACK NR 2. INSTALLED NEW SEAT TRACK NR 2 FROM STATION 1170 TO 1309 SRM 51-60-0. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND LEFT CUSP HAS CORROSION. REMOVED AND REPLACED LEFT CUSP STATION 1174-1250 SRM 53-01 FIG 4. (M)

Part: ANGLE — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON L-ANGLE ATTACHED TO INBOARD UPPER SIDE OF TRAPEZOID. ANGLE REMOVED FROM AIRCRAFT, RE-INSTALLED NEW ANGLE SRM 51-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND LEFT CUSP STATION 1022-1041 SURFACE CORROSION. INSTALLED NEW CUSP SHEET STA 1022-1098, LEFT SIDE SRM 53-01 FIG 4. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND SEAT TRACK NR 6 CORRODED AND WORN STATION 763-796. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK PER SRM 53-05 PART 1 FIG 4E. REMOVED SEAT TRACK FROM STATION 7600-797. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND LEFT CUSP CORRODED AROUND LIGHTENING HOLE. INSTALLED DOUBLER PER AARD 53-00-00-02 AND SRM 53-01 FIG 4. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

TUL - FOUND SHEAR TIE CORRODED, STATION 1148-1149, LONGERON 29-30R. REMOVED SHEAR TIE. REMOVED CORROSION. REINSTALLED SHEAR TIE PER MM 20-10-15-2. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND CORROSION ON SEAT TRACK NR 1 STATION 670. INSTALLED SEAT TRACK PLUG PER SRM 53-05 FIG 4A. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON DOOR JAMB BEAM FROM STATION 1159 TO 1208, BOTTOM SIDES. INSTALLED DOUBLER PER AARD 53-10-00-3 OF STATION 1194. (M)

Part: FITTING — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON FITTING AT AFT CARGO DOOR OPENING LOWER FORWARD CORNER AT LONGERON 28R, STATION 1155. INSTALLED NEW FITTING ON LOWER FORWARD CORNER OF AFT CARGO DOOR OPENING AT STATION1155 L28R PER MM 20-10-15-2. (M)

Part: FITTING — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON FITTING AT AFT CARGO DOOR OPENING LOWER AFT CORNER AT L28R STATION 1212. INSTALLED NEW FITTING AT AFT CARGO DOOR OPENING LOWER AFT CORNER AT L28R STATION 1212. AS PER MM 20-10-15-2 AND SRM 51-10-4. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND CORROSON UNDER DOUBLER AT FORWARD END NR 6 SEAT TRACK STATION 218. COMPLETED SEAT TRACK, SPLICE 218-313 STATION SRM 53-05 FIG 4. (M)

Part: CUSP — CORRODED (BS 484-503)

TUL - CUSP MEMBRANE CORRODED BETWEEN CUSP AND NR 1 SEAT TRACK, STATION 484 TO 503 LEFT SIDE OF A/C. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-01 FIG 4-3. (M)

Part: LIGHT — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS FROM PAX SEAT ROW 27 AND AFT INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP FROM PAX SEAT ROW 27 AND AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS FROM FORWARD PART OF MAIN CABIN TO PAX SEAT ROW 21 INOPERATIVE. RESECURRED EMERGENCY FLOOR LIGHT STRIP CONNECTOR AT PAX SEAT ROW 21. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS FROM FORWARD PART OF MAIN CABIN TO OVERWING EXIT INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR AT FORWARD PART OF MAIN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONDUCTOR — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT FLAT CONDUCTOR WIRE BY FORWARD GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)