N582AA

Part: LINE — FAILED (FUEL PUMP) · airframe 67,296 hrs · 35,189 cycles

DURING CLIMB OUT CREW NOTED THAT THE CTR FUEL TANK WAS NOT FEEDING. FOLLOWED QRH PROCEDURES & DISCOVERED THAT TURNING OFF EITHER RT OR LT MAIN TANK BOOST PUMPS, & CTR PUMP SWITCHES ON, THAT LOW PRESSURE LIGHT CAME ON TURNED OFF CTR PUMPS IAW PROCEDURE. DIVERTED, NO EMERGENCY DECLARED, AND LANDED UNEVENTFULLY. FOUND THE PUMP OUTLET ASSEMBLY BLOWN. REMOVED, REPLACED AND OPS CHECKED THE CENTER TANK FEED LINE IAW AMM 28-20-19-201.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 67,296 hrs · 35,189 cycles

CENTER TANK LOW PRESS CAME DURING CLIMB OUT. TROUBLESHOOTING THE CTR TANK FUEL SYS.

Part: PERISEAL — LEAKING (ANTI-ICE SYS) · airframe 66,608 hrs · 34,779 cycles

SMOKE & HISSING SOUND IN THE CABIN NEAR ROWS 26 TO 28. EMER DECLARED FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. UNEVENTFUL LANDING DID NOT LAND OVERWEIGHT. REPLACED LEAKING PERI SEALS AT LT SIDE FWD BULKHEAD ANTI-ICE DUCT. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,210 hrs · 33,969 cycles

LT HAND FUSELAGE SKIN CRACKED AT FASTENER HOLE JUST BELOW LONGERON NR 2 & STATION 1418. INSTALLED DOUBLER IAW EA MD80-53-033843 & SRM 53-04-00-001 FIGURE 40.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 65,210 hrs · 33,969 cycles

CRACK FOUND IN DORSAL FIN SKIN AFT OF WRAP AROUND ACCESS PANEL. STOP DRILLED CRACK & INSTALLED DOUBLER IAW SRM 555-01-00 FIGURE 2 SHEET 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,210 hrs · 33,969 cycles

FRAME CRACKED ON FWD SIDE OF STATION 1401 AT LONGERON 1 LT. INSTALLED REPAIR DOUBLER IAW AARD 53-10-00-17.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 65,210 hrs · 33,969 cycles

AFT CARGO DOOR FWD EDGE TOP STOP FITTING CRACKED. REPLACED FITTING IAW SRM 51-30-05.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 65,210 hrs · 33,969 cycles

AFT CARGO DOOR FWD EDGE CTR STOP FITTING CRACKED. REPLACED FITTING IAW SRM 51-30-05.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 65,210 hrs · 33,969 cycles

FWD CARGO DOOR STOP AFT LOWER STOP PAD FITTING CRACKED. INSTALLED NEW STOP PAD FITTING IAW SRM 51-30-05.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,502 hrs · 32,983 cycles

ESCAPE PATH LIGHT AT ROW 17D INOPERATIVE. INSTALLED NEW LIGHT ASSEMBLY FOR ROW 17D ESCAPE PATH LIGHT. OPERATIONS CHECKED NORMAL.

Part: BATTERY — MALFUNCTIONED (CABIN) · airframe 62,340 hrs · 32,354 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. RESET BATTERY TRAY AT OVERHEAD BIN 29D. OPS CHECKS NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 62,340 hrs · 32,354 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. RESEATED BATTERY TRAY AT OVERHEAD 29E. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,365 hrs · 31,854 cycles

MULTIPLE OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED TWO BATTERY PACKS FOR OVERHEAD AISLE EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,374 hrs · 31,859 cycles

MULTIPLE OVERHEAD EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED VARIOUS BATTERY PACKS THROUGHOUT CABIN. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 59,037 hrs · 30,566 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 18 TO 21 INOPERATIVE. RESEATED BATTERY PACK. OPS CHECKS NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 59,037 hrs · 30,566 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 7 TO 11 INOPERATIVE. RESEATED BATTERY PACK. OPS CHECKS NORMAL.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,384 hrs · 29,647 cycles

FORWARD SERVICE DOOR PAN FORWARD LOWER CORNER CRACKED AT FASTENER HOLE. INSTALLED SECTION OF FORWARD SERVICE DOOR PAN, SHIM, SPLICE ANGLE, FILLER AND PLATE PER EA MD80-53-016188, AND SRM 53-05-00 FIG 55, AND BOEING DRAWING J060288.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,384 hrs · 29,647 cycles

CRACK AT STATION 37 UPPER LEFT RADOME ALIGNMENT PIN. PERFORMED REPAIR PER AARD 53-10-00-19.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 57,384 hrs · 29,647 cycles

FUSELAGE - 3 EACH BLEND OUTS MISSING ADL STICKER IN FUSELAGE SKIN STATIONS 600 TO 616 LONGERONS 21 TO 22 RIGHT. INSTALLED NEW REPAIR DOUBLER PER SRM 53-04-02 AND BOEING DWG NUMBER SG0950001.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 57,384 hrs · 29,647 cycles

RIGHT SUBFLOOR CORRODED STATIONS 200 TO 218 BETWEEN SEAT TRACKS NUMBER 5 AND 6. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,384 hrs · 29,647 cycles

CORROSION IN SUBFLOOR DIAPHRAGM AT STATION 194 INBOARD SIDE OF FORWARD ENTRY THRESHOLD ATTACH ANGLE. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,384 hrs · 29,647 cycles

CORROSION ON LOWER DOOR BEAM STATIONS 636 TO 693. INSTALLED DOOR BEAM DOUBLER.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,384 hrs · 29,647 cycles

INTERCOSTAL CRACKED BELOW FORWARD ENTRY SUB-FLOOR STATION 175. INSTALLED NEW INTERCOSTAL PER AARD 51-10-00-5, BOEING DRAWING 5930540 AND BOEING DRAWING 9936534.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,384 hrs · 29,647 cycles

RIGHT TIE DOWN TRACK HAS SEVERAL AREAS OF CORROSION UPPER AND LOWER LEGS STATIONS 1231 TO 1309. INSTALLED SERVICEABLE TIE-DOWN TRACK PER SRM 51-30-01.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,384 hrs · 29,647 cycles

CORROSION ON LOWER DOOR PAN STATIONS 370 TO 427. INSTALLED FORWARD CARGO DOOR LOWER PAN AND DOUBLERS PER SRM 53-05-00.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,384 hrs · 29,647 cycles

LEFT TIE DOWN TRACK HAS CORROSION ON LOWER SIDE OF SPLICE INBOARD AND OUTBOARD SIDES STATIONS 1211 TO 1231. INSTALLED SERVICEABLE SPLICE PARTS PER SRM 51-30-05.

Part: STRAP — GOUGED (FUSELAGE) · airframe 57,384 hrs · 29,647 cycles

STRAP ON TOP OF FRAME HAS OUT OF LIMITS SCREW GOUGE. REPLACED STRAP.

Part: SUPPORT — CORRODED (GIRT BAR) · corrosion level 2 · airframe 57,384 hrs · 29,647 cycles

AFT SERVICE DOOR AFT GIRT BAR T-SUPPORT CORRODED. INSTALLED NEW T-PER AARD 51-10-00-5.

Part: GUSSET — GOUGED (FUSELAGE) · airframe 57,384 hrs · 29,647 cycles

SCREW GOUGE IN STRAP INBOARD SIDE OF RIGHT TIEDOWN TRACK AT STATION 368. INSTALLED NEW GUSSET PER SRM 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,384 hrs · 29,647 cycles

SEAT TRACK NUMBER 2 APPROXIMATELY STATION 219 FOOT HOLD LOCKING TOOTH IS WORN BEYOND LIMITS. REMOVED DAMAGED AREA, TREATED AND PRIME PAINTED AND INSTALLED REPAIR PLUG AND CHANNEL PER AARD 53-20-00-10.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 57,384 hrs · 29,647 cycles

CABIN GALLEY NUMBER 1 ATTACH FITTING FORWARD OUTBOARD IS CORRODED. INSTALLED NEW SERVICEABLE G-1 GALLEY ATTACH FITTING PER AARD 51-10-00-5.

Part: PANEL — DAMAGED (TE FLAP) · airframe 57,384 hrs · 29,647 cycles

THE RIGHT WING INBOARD FLAP HAS A DAMAGED AREA .75 INCH LONG BY .25 INCH WIDE, 41 INCHES FROM THE INBOARD EDGE SEAL AND 4.25 INCHES FORWARD OF TRAILING EDGE. RIGHT INBOARD FLAP REMOVED DAMAGED MATERIAL AS PER SRM 57-01-00, DYE CHECK SHOWS NO FURTHER CRACK MIGRATION. INSTALLED FLUSH DOUBLER REPAIR AS PER SRM 57-01-00.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,384 hrs · 29,647 cycles

DENT IN FUSELAGE STATION 313 BETWEEN LONGERONS 20 AND 21 RIGHT. DYE-CHECKED AREA, COLD WORKED SKIN AND INSTALLED INTERNAL DOUBLER PER BOEING DRAWING SG095300001.

Part: PAN — CRACKED (WINDOW) · airframe 57,384 hrs · 29,647 cycles

STATION 1193 RIGHT LOWER FORWARD WINDOW PAN CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,384 hrs · 29,647 cycles

STATION 1041 RIGHT UPPER AFT WINDOW PAN CRACKED. REMOVED CRACKED AREA AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,384 hrs · 29,647 cycles

STATION 1022 RIGHT LOWER FORWARD WINDOW PAN CRACKED. REMOVED CRACKED AREA AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,804 hrs · 28,185 cycles

FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS EMERGENCY LIGHTS. OPS CHECKED NORMAL.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 53,580 hrs · 27,464 cycles

FOUND .3125 INCH CRACK AT LEFT STRUT DOOR AFT HINGE CUTOUT. INSTALLED DOUBLER REPAIR PER 53-05-00.

Part: SHIELD — MISSING (FLASHLIGHT) · airframe 53,165 hrs · 27,235 cycles

TAMPER SHIELD MISSING FORWARD FLASHLIGHT AT AFT JUMPSEAT. REPLACED TAMPER SHIELD AT FORWARD FLASHLIGHT AFT JUMPSEAT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,998 hrs · 27,140 cycles

FUSELAGE SKIN CRACKED STATION 1474 L23L. INSTALLED DOUBLER UNDER SRM 53-01-00 AND AARD 53-30-00-02.

Part: BATTERY PACK — NOT SEATED (EMERGENCY LIGHTS) · airframe 51,526 hrs

LGA - OVERWING EMERGENCY LIGHTS LEFT TO RIGHT INOPERATIVE. BATTERIES RESEATED IN CHARGER FOR OVERWING EMERGENCY LIGHTS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,232 hrs

LGA - EMERGENCY LIGHT IN TAIL CONE COMPARTMENT BY WATER SEPARATORS INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT IN TAIL CONE COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,232 hrs

LGA - EMERGENCY LIGHT AT OVERHEAD FLIGHT ATTENDANT SEAT BY VENTRAL DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD FLIGHT ATTENDANT SEAT BY VENTRAL DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT AT SEAT ROW 19D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 19D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT ROW 20D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 20D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT AT SEAT ROW 28D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 28D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT ROW 8D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 8D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY EXIT SIGN LIGHT AT FORWARD LEFT OVERWING INOPERATIVE. REPLACED FORWARD LAMP FOR EMERGENCY EXIT SIGN LIGHT AT FORWARD LEFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT ROW 16D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 16D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT AT SEAT ROW 24D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 24D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT EXTERIOR OVERWING INOPERATIVE. REPLACED BATTERY PACK B5 49 FOR EMERGENCY LIGHT AT EXTERIOR OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT ROW 18D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 18D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (EMERGENCY LIGHT)

DEN - SEAT MOUNTED EMERGENCY LIGHTS BY GALLEY CART BROKEN. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHTS BY GALLEY CART. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACM — INOPERATIVE (LT AND RT)

JFK - AIR INTERRUPTED TO JFK DUE TO STRONG ODOR OF OIL AND SMOKE THROUGHOUT CABIN AND COCKPIT. LANDED JFK WITHOUT INCIDENT. PULLED COALESCER BAGS AND FOUND OIL. REPLACED LEFT AND RIGHT HAND PACK AIR CYCLE MACHINE AND COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DTW - FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT ROW 20 FOR FORWARD OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHTS)

DFW EMERGENCY ESCAPE PATH LIGHTING AT 11D INOPERATIVE. REPLACED SOCKET ASSEMBLY AT SEAT 11D FOR EMERGENCY ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE IN THE AFT CABIN SECTION OF THE AIRCRAFT. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS AT ROWS 28-29 AND LEFT SERVICE DOOR IN CEILING PANEL INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY FOR ROWS 22-29. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 10 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT ROW 10. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE)

TUL - FOUND CANT FRAME FS 1474 RIGHT SIDE AFT OF ACCUMULATOR DOOR CUTOUT, ANGLE CRACKED. REMOVED AND REPLACED ANGLE STIFFENER PER SRM 51-01 AT CANT FS 1474 RIGHT SIDE. (M)

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND FS 1474 CRACKED LOWER RIGHT SIDE JUST INBOARD OF DOOR CUTOUT. REPAIRED CRACKED FRAME PER SRM 53-10-00-15 PAGE 1. (M)

Part: FRAME — CRACKED (FUSELAGE)

FOUND FS 1401 FRAME CRACKED AFT SIDE FROM UNDER RADIUS BLOCK STRINGER 2L AREA. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLE PER AARD 53-10-00-15 AND SRM 53-01-00. (M)

Part: WEB — CORRODED (FUSELAGE)

FOUND CORROSION ON BOTTOM SIDE OF CUSP AT STATION 1174 BELOW NR 1 SEAT TRACK. REMOVED CORROSION. INSTALLED DOUBLER REPAIR PER SRM 53-01-00. (M)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

FOUND WHALE BONE TO KEELBEAM ATTACH ANGLE CRACKED INBOARD END RIGHT GEAR WELL. REMOVED AND REPLACED ANGLE PER SRM 51-01. (M)

Part: BEAM — CORRODED (FUSELAGE)

TUL - FOUND SEVERAL AREAS OF CORROSION ON AFT CARGO DOOR BEAM. REMOVED AND REPLACED BEAM PE SRM 53-10-00. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

TUL - FOUND FS 1437 FRAME SHEAR TIE CRACKED AFT SIDE, JUST OUTBOARD OF LARGE TAIL TIE FITTING LEFT OF C/L. REMOVED AND REPLACED SHEAR TIE PER SRM 51-01. (M)

Part: GALLEY TRACK — CORRODED (FUSELAGE)

FOUND CORROSION ON SEAT TRACK NR 1 AT GALLEY TIE DOWN. REMOVED CORROSION CUTOUT AREA BEYOND LIMITS AND INSTALLED PLUG PER AARD 53-20-00-10. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON FLOOR CHANNEL STATION 148-162 RBL 8-12. REMOVED AND REPLACED FLOOR CHANNEL AT STATION 148-162 RBL 8-12 SRM 51-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP, STATION 1287 BETWEEN TRACK NR 1 AND NR 2. INSTALLED NEW CUSP SHEET, STATION 1250-1309 PER SRM 53-05-00 FIG 97. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT SEAT 9D, 12D, 17D, 19D, 20D, 21D, 25D, 26D, 29D, 30D, 31D DIM. REPLACED EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: O-RING — LEAKING (RUDDER)

EWR - FLT 1704 - EN ROUTE ORD-EWR, DURING TAXI AIRCRAFT CABIN FILLED WITH SMOKE. DETECTED HYDRAULIC FLUID EMPTY. REPLACED O-RING AT RUDDER SHUTOFF VALVE PLUG. ACCOMPLISHED LEAK CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — LOOSE (CABIN)

DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 10. RE-SECURED EMERGENCY EXIT LIGHT STRIP AT ROW 10. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)