N7538A

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,135 hrs · 30,901 cycles

LEFT AND RIGHT AFT OVERWING DOOR UPPER EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK AT ROW 20DEF. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,135 hrs · 30,901 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS, ABOVE CATWALK INOPERATIVE. REPLACED BATTERY PACK AT AFT LAVATORY B5 - 28. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,135 hrs · 30,901 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. REPLACED BATTERY PACK AT ROW 28 DEF. OPS CHECK NORMAL.

Part: SYMBOL GENERATOR — FAULTY (COCKPIT) · airframe 57,741 hrs · 29,582 cycles

JFK - INFLIGHT LGA-DFW. CREW REPORTED PRIMARY FLIGHT DATA AND PRIMARY NAVIGATION DATA FAILED. EMERGENCY DECLARED, DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER ONE AND TWO SYMBOL GENERATORS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: GUARD — DAMAGED (CABIN) · airframe 56,847 hrs · 29,109 cycles

EMERGENCY LIGHT AT SEAT 19 HAS DAMAGED GUARDS. REPLACED GUARDS FOR EMERGENCY LIGHT AT SEAT 19.

Part: BATTERY PACK — DISCHARGED (COCKPIT) · airframe 56,719 hrs · 29,044 cycles

EMERGENCY LIGHTS STAY ON IN COCKPIT, FORWARD ENTRANCE AND SERVICE ENTRANCE WHEN AIRCRAFT IS POWERED DOWN. REMOVED AND REPLACED EMERGENCY BATTERY PACK B5-23 AT STATION 211, OPS CHECKS NORMAL.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,535 hrs · 28,950 cycles

RIGHT CUSP TEE CORRODED STATIONS 154 TO 229. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 53-05-00 AND EA MD80-53-009094.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 56,535 hrs · 28,950 cycles

RIGHT CUSP T ANGLE OUT OF LIMITS APPROXIMATE STATION 150 TO 250. INSTALLED SECTION OF CUSP T ON RIGHT SIDE STATION 154 TO 229 PER SRM 53-05-00 AND EA MD80-53-009094.

Part: FITTING — CORRODED (FUSELAGE) · airframe 56,535 hrs · 28,950 cycles

GALLEY TIE DOWN CORRODED 17 INCHES INBOARD OF FORWARD SERVICE DOOR STATION 160. REMOVED AND REPLACED GALLEY TIE DOWN PER SRM 51-30-05.

Part: MOUNT — DAMAGED (FUSELAGE) · airframe 56,535 hrs · 28,950 cycles

CORROSION ON GALLEY TIE DOWN 10 INCHES OF FORWARD SERVICE DOOR. INSTALLED GALLEY MOUNT PER AARD 53-20-00-19 AND REPAIR PLUG PER AARD 53-20-00-19.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,535 hrs · 28,950 cycles

CORROSION ON WEB INBOARD OF FORWARD SERVICE DOOR STATION 168 TO 200. REMOVED CORRODED AREA INSTALLED NEW CUSP PER AARD 53-20-00-16.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,535 hrs · 28,950 cycles

AFT LEFT NOSE GEAR DOOR AFT HINGE CUTOUT ON SKIN IS CORRODED & CRACKED. INSTALLED REPAIR DOUBLER PER EA MD80-53-009048.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 56,535 hrs · 28,950 cycles

EMERGENCY EQUIPMENT COMPARTMENT HAS CORROSION ON LOWER SURFACE OF CABIN SUBFLOOR WEBBING AT STATION 190 LEFT SIDE. CORRODED SECTION OF WEBBING WAS REMOVED AND NEW SECTION DOUBLED IN ACCOMPLISHED PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,535 hrs · 28,950 cycles

CORROSION ON RIGHT CUSP OUT OF LIMITS. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,535 hrs · 28,950 cycles

CORROSION ON RIGHT CUSP OUT OF LIMITS. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 56,535 hrs · 28,950 cycles

CRACK IN STATION 160 AT OUTBOARD HAT CHANNEL. INSTALLED NEW NUMBER 4 LEFT LONGERON STATION 148 TO 190 PER SRM 53-02-00 AND SRM 51-30-00.

Part: SUPPORT FITTING — CRACKED (CARGO BAY) · airframe 56,535 hrs · 28,950 cycles

AFT CARGO CRACK ON VERTICAL FLOORBOARD TIE DOWN SUPPORT FITTING STATION 1150 BETWEEN LONGERON 29 RIGHT AND LONGERON 30. REMOVED AND REPLACED SUPPORT FITTING PER SRM 51-30-05.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,535 hrs · 28,950 cycles

STATION 190 AT FORWARD ENTRY DOOR SUBFLOOR HAS CORROSION ON BOTTOM SIDE. REMOVED CORRODED AREA AND INSTALLED DOUBLER PER SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,535 hrs · 28,950 cycles

FOUND CORROSION UNDER SEAT TRACK NUMBER 6 AT STATION 237 IN RIGHT CUSP. REPLACED CUSP PER AARD 53-20-00-16.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,535 hrs · 28,950 cycles

CORROSION ON SHEAR TIE FORWARD OF FRAME STATION 1155 LONGERON 29 RIGHT TO LONGERON 30. REPLACED SHEAR TIE AT STATION 1155 PER SRM 51-30-01.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 56,535 hrs · 28,950 cycles

CRACK IN LONGERON 3 LEFT STATION 160 AT OUTBOARD HAT CHANNEL. INSTALLED NEW LONGERON 3 LEFT STATION 148 TO 178 PER SRM 5302-00 FIG 18.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,535 hrs · 28,950 cycles

CORROSION SHEAR TIE FORWARD SIDE OF FRAME STATION 1155 BETWEEN LONGERON 29 RIGHT AND LONGERON 30. REMOVED AND REPLACED SHEAR TIE PER SRM 53-30-1.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,535 hrs · 28,950 cycles

FOUND CRACK IN CUSP RIGHT SIDE STATION 242 TO MIDDLE LIGHTNING HOLE OUTBOARD OF SEAT TRACK NUMBER 6. REPAIRED PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,535 hrs · 28,950 cycles

CUSP CORRODED STATION 1309 BETWEEN NUMBER 1 AND 2 SEAT TRACKS. CORRODED SECTION OF CUSP REMOVED AND NEW SECTION OF CUSP INSTALLED PER AARD 53-00-00-013 AND SRM 51-30-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 3 · airframe 56,535 hrs · 28,950 cycles

CORROSION REMOVAL BEYOND LIMITS ON NUMBER 2 SEAT TRACK AT STATION 1200 TO 1309. REPAIRED PER SRM 53-05-00.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 56,535 hrs · 28,950 cycles

CORROSION ON INTERCOSTAL STATION 1309 TO 1322 UNDER LEFT TIE DOWN TRACK. INSTALLED A NEW SERVICEABLE SHEAR TIE SRM 51-30-05 AND SRM 51-30-2.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,535 hrs · 28,950 cycles

CORROSION ON INTERCOSTAL BETWEEN STATION 1309 AND 1322 AFT CARGO UNDER LEFT TIE DOWN TRACK. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-05.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 56,535 hrs · 28,950 cycles

CORROSION ON FRAME AND SHEAR TIE STATION 1287 LONGERON 30. INSTALLED SHEAR TIE PER SRM 53-03-00.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,535 hrs · 28,950 cycles

CORROSION AT LEFT TIE DOWN TRACK IN AFT CARGO STATION 1231 TO 1250. INSTALLED NEW TIE DOWN TRACK PER AARD 51-00-00-012.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 56,535 hrs · 28,950 cycles

CORROSION ON FRAME AND SHEAR TIES EACH SIDE OF LONGERON 30 AT STATION 1287. REPAIRED PER SRM 53-03-00 FIGURE 3 SHEET 1.

Part: SKIN — BENT (E&E DOOR) · airframe 56,535 hrs · 28,950 cycles

FORWARD ELECTRICAL EQUIPMENT COMPARTMENT DOOR RIGHT AFT CORNER OF LOWER SKIN IS BENT. INSTALLED NEW SKIN PER ESO 80179.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,535 hrs · 28,950 cycles

CORROSION ON SEAT TRACK NUMBER 3 AT STATION 217 TO 219. REMOVED CORROSION AND INSTALLED TRACK PLUG PER 53-05.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,535 hrs · 28,950 cycles

INTERCOSTAL CRACKED FROM FASTENER AT AFT END STATION 1309. INSTALLED NEW INTERCOSTAL AT STATION 1287 TO 1309 PER SRM 51-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,535 hrs · 28,950 cycles

CORROSION ON SEAT TRACK NUMBER 3. REMOVED CORROSION AND INSTALLED TRACK PLUG PER 53-05.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,535 hrs · 28,950 cycles

CRACK FOUND IN CUSP SHEET AT STATION 1245 OUTBOARD OF SEAT TRACK NUMBER 1. INSTALLED DOUBLER AT STATION 1245 OUTBOARD OF SEAT TRACK NUMBER 1 PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,535 hrs · 28,950 cycles

CORROSION ON SEAT TRACK NUMBER 3 AT STATION 317 TO 320. REMOVED CORROSION AND INSTALLED TRACK PLUG PER 53-05.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,535 hrs · 28,950 cycles

RIGHT CUSP CRACKED AT STATION 1265. INSTALLED DOUBLER PER SRM 53-20-00-16.

Part: BUSHING — WORN (LE SLAT) · airframe 56,535 hrs · 28,950 cycles

LEFT WING KNUCKLE BUSHINGS WORN OUTBOARD END OF NUMBER 4 SLAT. REPLACED KNUCKLE RIB ON NUMBER 4 OUTBOARD SLAT WITH NEW ONE IAW AARD 27-80-00-2.

Part: PAN — CRACKED (WINDOW) · airframe 56,535 hrs · 28,950 cycles

WINDOW PAN 32 RIGHT HAS CRACK IN UPPER FORWARD CORNER. TRIMMED OUT CRACK ON WINDOW PAN AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,535 hrs · 28,950 cycles

STATION 946 TO 965 LEFT SIDE WINDOW PAN CRACKED AT FORWARD UPPER CORNER. TRIMMED OUT CRACK ON WINDOW PAN AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: BEARING — WORN (LE SLAT) · airframe 56,535 hrs · 28,950 cycles

RIGHT WING SLAT EXCESSIVE PLAY IN KNUCKLE AT INBOARD END OF NUMBER 5 SLAT. REMOVED OLD BEARINGS AND INSTALLED NEW BEARINGS PER ESO 80117.

Part: PAN — CRACKED (WINDOW) · airframe 56,535 hrs · 28,950 cycles

STATION 1003 TO 1022 LEFT SIDE WINDOW PAN CRACKED AT UPPER AFT CORNER. TRIMMED OUT CRACK ON WINDOW PAN AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,535 hrs · 28,950 cycles

STATION 946 TO 965 LEFT SIDE WINDOW PAN CRACKED AT FORWARD UPPER CORNER. TRIMMED OUT CRACK IN PAN AND INSTALLED DOUBLER IAW AARD53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,535 hrs · 28,950 cycles

WINDOW PAN 38 RIGHT FORWARD UPPER CORNER HAS CRACK. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,535 hrs · 28,950 cycles

WINDOW PAN 44 RIGHT AFT UPPER CORNER HAS CRACK. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,110 hrs · 28,727 cycles

EMERGENCY LIGHT AT SEAT 12D INOPERATIVE. REPLACED LAMP.

Part: LENS — MISSING (CABIN) · airframe 55,364 hrs · 28,314 cycles

SEAT 27D LENS AND GUARD MISSING. REPLACED SEAT 27D LENS AND GUARD LIGHT. OPS CHECK GOOD.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 52,841 hrs · 26,928 cycles

CRACK ON CUSP MEMBRANE BELOW G1 GALLEY DRAIN PAN AT STATION 160. CRACK LENGTH IS 2 INCHES. INSTALLED DOUBLER IN ACCORDANCE WITH AARD 53-20-00-16.

Part: FRAME — CRACKED (BS 1485) · airframe 52,841 hrs · 26,928 cycles

CRACK IN CANTED FRAME WEB AT AFT ACCESSORY AT STATION 1485. CRACK LENGTH IS .5 INCH. INSTALLED DOUBLER IN ACCORDANCE WITH AARD 53-10-00-32.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 52,841 hrs · 26,928 cycles

CORROSION ON CUSP MEMBRANE BELOW G1 GALLEY DRAIN PAN BETWEEN STATIONS 160 TO 168. AREA OF DISCREPANCY IS 6 INCHES BY 8 INCHES. INSTALLED DOUBLER UNDER G1 GALLEY DRAIN PAN IN ACCORDANCE WITH AARD 53-20-00-16.

Part: FRAME — CRACKED (BS 1510) · airframe 52,841 hrs · 26,928 cycles

CRACK IN CANTED FRAME AT LONGERON 23 RT AT STATION 1510. CRACK LENGTH IS 1 INCH. INSTALLED DOUBLER IN ACCORDANCE WITH ESO 80559 DATED 25 SEP 2008.

Part: BATTERY PACK — DISCHARGED (CABIN) · 52,543 cycles

LGA EMERGENCY LIGHTS AT AFT LAVATORY AREA INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT LAVATORY AREA. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LIGHT — INOPERATIVE (CABIN) · 52,543 cycles

LGA PORTABLE EMERGENCY LIGHT ASSEMBLY AT FIRST CLASS CABIN INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR PORTABLE EMERGENCY LIGHT AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,387 hrs

LGA - EMERGENCY LIGHTS AT SEAT ROWS 8 TO 13 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 8 TO 13. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,777 hrs

LGA - EMERGENCY LIGHT AT FIRST CLASS ENTRY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FIRST CLASS ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT RIGHT EXTERIOR OVERWING INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT EXTERIOR OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE HARNESS — BROKEN (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 8D IS INOPERATIVE. REPAIRED WIRE FROM SIDEWALL AREA TO SEAT FOR EMERGENCY LIGHT AT SEAT 8D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EMERGENCY LIGHTS)

DFW - PORTABLE EMERGENCY LIGHT AT FORWARD CABIN IS INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT FORWARD CABIN CEILING FLIGHT DECK, FORWARD ENTRY AND GALLEY INOPERATIVE. REPLACED BATTERY PACK B5 23 FOR EMERGENCY LIGHTS AT FORWARD CABIN CEILING FLIGHT DECK, FORWARD ENTRY AND GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HOOK AND LOOP — FAILED (SERVICE DOOR)

DFW - EMERGENCY SLIDE AT AFT SERVICE DOOR HANDLE HOOK AND LOOP INOPERATIVE. REPLACED EMERGENCY SLIDE AT AFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 12AB IS INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROW 12AB. 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: BULB — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 13AB IS INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROW 13AB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — FAILED (R1 DOOR)

FLL - RIGHT NUMBER ONE DOOR SLIDE FELL TO RAMP WHEN DOOR OPENED BY CATERING. SLIDE WAS NOT ARMED. FOUND DEFECTIVE CLIPS THAT HOLD CHUTE INSIDE DOOR. SLIDE FELL OFF DOOR AND LANDED INTACT. DID NOT DEPLOY. PRESSURE INDICATOR IS DAMAGED AND UNREADABLE. REPLACED RIGHT NUMBER ONE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — LOW PRESSURE (GALLEY DOOR)

DFW - EMERGENCY SLIDE AT AFT GALLEY DOOR HAS LOW PRESSURE. REPLACED AFT GALLEY DOOR EMERGENCY SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - CEILING EMERGENCY EXIT LIGHTS BETWEEN ROWS 13 AND 16 AND ROWS 23 AND 26 INOPERATIVE. ADDITIONALLY, FORWARD ENTRY DOOR PORTABLE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACKS FOR ROWS 13 AND 16 AND ROWS 23 AND 26. ALSO REPLACED FORWARD ENTRY DOOR PORTABLE EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHTS AT FIRST EMERGENCY EXIT ROW LT AND RT INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS AT FIRST EMERGENCY EXIT ROW LEFT AND RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

MIA - EMERGENCY ESCAPE PATH LIGHT AT 7D INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ATL - OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO OVERHEAD EMERGENCY LIGHT AT 1L DOOR IS INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT AT 1L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, OVERWING EMERGENCY LIGHTS WERE INOPERATIVE ON LEFT AND RIGHT SIDES. REPLACED BATTERY PACK B5-105. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — BROKEN (TAIL CONE)

DFW - DURING OVERNIGHT MAINTENANCE, AFT TAIL CONE EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. REPLACED AFT TAIL CONE EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DOOR FRAME — DAMAGED (FUSELAGE)

TUL - FOUND FORWARD SERVICE DOOR FRAME DAMAGED AT LOWER FORWARD CORNER, HOLE GOUGED IN LOWER DOOR PAN. REPLACED ENTIRE DOOR PAN ON E58'S NR 4208140, 9142105, 9109005 SRM REF 53-05-00/53-10-3/51-20, 51-30 AND 51-60. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND FUSELAGE SKIN DENTED STATION 408 L30R/L29R. COLD WORKED DENT OUT THEN DYE CHECKED AREA. NO CRACKS FOUND. INSTALLED PERMANENT REPAIR DOUBLER PER SRM 53-04 PAGE 218H. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION REMOVAL OUT OF LIMITS. SEAT TRACK REPLACED MM 53-40-01-2. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION REMOVAL OUT OF LIMITS. SEAT TRACK REPLACED STATION 795-1032, 53-40-01-02 MM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL 0 FOUND CORROSION REMOVAL BEYOND LIMITS. REPLACED NR 1 SEAT TRACK PER MM 53-40-01-02 STATION 1174-1308. (M)

Part: WINDOW — CRACKED (CABIN)

TUL - FLT 1318 - EN ROUTE DFW-IND, AIR INTERRUPTED TO TUL DUE TO CRACKED WINDOW AT 12A. LANDED TUL WITHOUT INCIDENT. REPLACED CRACKED WINDOW AT 12A. PRESSURIZATION AND LEAK CHECK OK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, CEILING MOUNTED EMERGENCY EXIT LIGHTS IN AFT CABIN INOPERATIVE. REPLACED CEILING MOUNTED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: CONNECTOR — DIRTY (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT SEAT 24, 25, AND 26 INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT CONNECTOR AT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — FAILED (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT INOPERATIVE IN FORWARD CABIN. REPAIRED EMERGENCY EXIT FLOOR PATH CONNECTOR IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — DISCONNECTED (CABIN)

DFW - DURING OVERNIGHT CHECK, AFT OVERHEAD COMPARTMENT EMERGENCY EXIT LIGHT ABOVE CATWALK INOPERATIVE. REATTACHED WIRE TO AFT OVERHEAD COMPARTMENT EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DISCONNECTED (AFT STAIR WELL)

DFW - DURING OVERNIGHT CHECK AFT STAIR SIDE WALL EMERGENCY EXIT LIGHT INOPERATIVE. REATTACHED WIRE TO AFT STAIR SIDE WALL EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — FAILED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS IN AFT STAIR AREA INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT WIRE AND SPLICE IN TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SLIDE — DEFECTIVE (L1 DOOR)

LAS - AT GATE, FLIGHT ATTENDANT FAILED TO DISARM L1 DOOR AND SLIDE FELL OUT OF PACK, BUT DID NOT SUCCESSFULLY DEPLOY. REPLACED L1 SLIDE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: AC ELECT SYSTEM — ODOR (COCKPIT)

HSV - FLT 2077 - AFTER TAKEOFF HSV, ELECTRICAL ODOR NOTED IN COCKPIT. AIRCRAFT RETURNED TO HSV AND LANDED OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED VISUAL CHECK OF COCKPIT, ALL ELECTRICAL BAYS AND CARGO COMPARTMENTS WITH NO DEFECTS FOUND. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. SYSTEMS GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS FOUND. SYSTEMS OPERATIONAL CHECKED NORMAL. UNABLE TO DUPLICATE PROBLEM AND AIRCRAFT RETURNED TO SERVICE. (M)

Part: ENGINE — FOD (LEFT)

DFW - FLT 700 - AFTER TAKEOFF DFW, DURING INITIAL CLIMB-OUT, LT ENGINE EXPERIENCED MULTIPLE COMPRESSOR STALLS FOLLOWED BY BURNING ODOR NOTED IN CABIN AND COCKPIT. REDUCED LT ENGINE POWER TO IDLE AND ENGINE INDICATED NORMAL OPERATION. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. ACCOMPLISHED BIRD STRIKE INSPECTION WITH NO DAMAGE FOUND OTHER THAN LT ENGINE. REPLACED LT ENGINE DUE TO FAN FOD. ACCOMPLISHED LEAK CHECK AND GROUND ENGINE RUN WITH NO DEFECTS OR ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SLIDE — LOW PRESSURE (GALLEY DOOR)

SEA - DURING OVERNIGHT CHECK, FORWARD GALLEY EMERGENCY EVACUATION SLIDE BOTTLE PRESSURE LOW. REPLACED FORWARD GALLEY EMERGENCY EVACUATION SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: COALESCER — DIRTY (CABIN)

AUS - FLT 1083 - AFTER TAKEOFF AUS DURING CLIMB-OUT, ACRID ODOR NOTED IN CABIN BUT NO VISIBLE SMOKE OR HAZE. AIRCRAFT RETURNED TO AUS AND LANDED WITHOUT INCIDENT. ACCOMPLISHED INTERGRATED ELECTRICAL SYSTEM CHECK WITH NO DEFECTS FOUND. ACCOMPLISHED PACK BURNOUT PROCEDURE AND REPLACED WATER SEPARATOR COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO ODORS NOTED. (M)

Part: EEL STRIP — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 12D INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)