N77421

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,216 hrs · 36,273 cycles

CORROSION ON PAN ALONG THE FORWARD CARGO DOOR THRESHOLD. INSTALLED NEW DOOR PAN PER SRM 53-05 FIG 44.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,216 hrs · 36,273 cycles

FORWARD CABIN HAS CORROSION AT G-1 GALLEY, FORWARD INBOARD SUBFLOOR BRACKET AT STATION 160. INSTALLED FLOORBEAM I ANGLE REPAIR PER SRM 53-05-00 FIG 20A AND AARD 53-00-00-06.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 68,216 hrs · 36,273 cycles

FORWARD CABIN HAS A CRACK AT LONGERON 4 LEFT STATION 200. INSTALLED LONGERON SPLICE PER SRM 53-02-00 FIGURE 18.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 68,216 hrs · 36,273 cycles

FORWARD CABIN HAS A CRACK AT LONGERON 3 LEFT STATION 160. INSTALLED LONGERON SPLICE AND END FITTING PER SRM 53-02-00 FIGURE 18.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,216 hrs · 36,273 cycles

CORROSION ON SUB FLOOR STATION 148 AT RIGHT BUTTLINE 8. INSTALLED 7075 T-6 DOUBLER AS PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 68,216 hrs · 36,273 cycles

FORWARD CABIN HAS A CRACK AT LONGERON 3 LEFT, STATION 200. INSTALLED LONGERON SPLICE AND END FITTING PER SRM 53-02-00 FIG 18.

Part: PAN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 68,216 hrs · 36,273 cycles

FORWARD CARGO DOOR CUTOUT THRESHOLD PAN CORRODED. REMOVED AND REPLACED DOOR JAMB PAN AND SPLICE PLATES PER SRM 53-05-00 FIGURE 44.

Part: FLAP — DAMAGED (LT WING) · airframe 68,216 hrs · 36,273 cycles

AIRCRAFT FLAP DAMAGED DUE TO IMPACT. REMOVED DAMAGED SECTION OF FIBERGLASS TRAILING EDGE AND SPLICED IN NEW SECTION BOTH INBOARD AND OUTBOARD ENDS UNDER SRM 57-03-00.

Part: BEAM — CRACKED (ENTRY DOOR) · airframe 68,216 hrs · 36,273 cycles

FORWARD ENTRY DOOR NUMBER FIVE BEAM CRACKED IN RADIUS FORWARD SIDE. STOPPED DRILLED AND INSTALLED DOUBLER PER SRM 52-05-00 FIG 31.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,216 hrs · 36,273 cycles

CRACK IN FRAME STATION 1497 AT 4 O`CLOCK POSITION. INSTALLED DOUBLER PER ENGINEERING AUTHORIZATION 53-008466, DATED 12/18/09.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 68,216 hrs · 36,273 cycles

CRACK IN LONGERON 2 LEFT SIDE AT STATION 160. REPLACED LONGERON PER SRM 53-02-00 FIG 18.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 68,216 hrs · 36,273 cycles

LONGERON 3 LEFT CRACKED AT STATION 160. ACCOMPLISHED SPLICE REPAIR UNDER SRM 53-02-00 FIG 18.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 68,216 hrs · 36,273 cycles

THREE EACH CRACKS AT LEFT CUSP STATION 218 TO 225. REPLACED CUSP UNDER AARD 53-20-00-16.

Part: CASTING — CRACKED (LT WING) · airframe 68,216 hrs · 36,273 cycles

LEFT WING LEADING EDGE FRONT SPAR FRONT SIDE CASTING CRACKED AT STATION XRS 240. NEW CASTING INSTALLED PER SRM 51-30-05.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 68,216 hrs · 36,273 cycles

RIGHT CUSP CRACKED AT STATION 1244. REPAIRED PER AARD 53-20-00-16.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 68,216 hrs · 36,273 cycles

CRACK ON FORWARD CARGO DOOR AT FORWARD EDGE MIDDLE BRACKET. REMOVED OLD FITTING, DRILLED UP AND INSTALLED NEW FITTING PER ESO 80174.

Part: SKIN — DENTED (FUSELAGE) · airframe 68,216 hrs · 36,273 cycles

FOUND 2 DENTS IN SKIN AT STATION 235 BETWEEN LONGERON 18 LEFT AND 17 LEFT. REPAIRED PER SRM 53-04 FIG 12B.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 68,216 hrs · 36,273 cycles

SKIN DAMAGED AT WATER DRAIN AT STATION 275. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-04-03 AND DRAWING SG09530002.

Part: PAN — CRACKED (FUSELAGE) · airframe 68,216 hrs · 36,273 cycles

RIGHT FORWARD UPPER WINDOW PAN TAB IS CRACKED AT STATION 927. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 68,216 hrs · 36,273 cycles

RIGHT FORWARD UPPER WINDOW PAN TAB IS CRACKED AT STATION 946. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: RIB — CRACKED (LE SLAT) · airframe 68,216 hrs · 36,273 cycles

NUMBER 15 LEADING EDGE SLAT RIB SHOWS CRACK INDICATION AT INBOARD SIDE LEFT WING OUTBOARD SLAT. REPLACED CRACKED RIB AT OUTBOARD NUMBER 15 POSITION, LEFT NUMBER 5 SLAT PER ESO 80117.

Part: PIN — PULLED (EVAC SLIDE) · 64,583 cycles

ATL FORWARD ENTRY DOOR SLIDE PINS WERE PULLED. REPLACED SLIDE AT FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHT AT OVERHEAD SEATS 20DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD SEATS 20DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHT AT OVERWING FORWARD POSITION INOPERATIVE. REPLACED BATTERY PACK IN OVERHEAD BIN FOR EMERGENCY LIGHT AT OVERWING FORWARD POSITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

BOS - EMERGENCY EXIT SIGN LIGHT AT UPPER FORWARD OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN LIGHT AT UPPER FORWARD OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MANIFOLD — DEFECTIVE (A/C PACK)

JAX - AFTER TAKEOFF SMOKE IN CABIN. TURNED OFF PACK DURING APPROACH AND SMOKE DISSIPATED. LANDED JAX NO INCIDENT. REPLACED ELEVATOR POWER MANIFOLD AND COALESCER BAGS. CONDUCTED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT)

EMERGENCY LIGHT AT TAIL COMPARTMENT SLIDE HANDLE INOPERATIVE. RESPLICED WIRES FOR EMERGENCY LIGHT AT TAIL COMPARTMENT SLIDE HANDLE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - TAIL COMPARTMENT WALKWAY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR TAIL WALKWAY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, LEFT AFT OVERWING EMERGENCY EXIT LIGHTS INTERMITTENT. REPAIR LEFT AFT OVERWING EMERGENCY EXIT LIGHTS CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — LOOSE (CABIN)

DURING OVERNIGHT MAINTENANCE, FORWARD LEFT HAD OVERWING EMERGENCY EXIT LIGHT DIM. SECURED GROUND ON FORWARD LEFT HAND OVERWING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — LOOSE (CABIN)

DFW - DURNG OVERNIGHT MAINTENANCE, FORWARD OVERHEAD EMERGENCY EXIT LIGHT INTERMITTENT. TIGHTENED EMERGENCY EXIT LIGHT WIRES ON BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CAT WALK SIDEWALL MARKERS INOPERATIVE. REPLACED EMERGENCY EXIT CAT WALK SIDEWALL MARKERS WIRE SPLICES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

BDL - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING FROM ROW 20 THROUGH 31 INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, AFT LEFT SIDE EMERGENCY EXIT ESCAPE PATH LIGHTS DIM. REPLACED BATTERY PACK FOR AFT LEFT SIDE EMERGENCY EXIT ESCAPE PATH LIGHTS. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — BROKEN (OVERWING)

RDU - DURING OVERNIGHT MAINTENANCE, LEFT SIDE OVERWING EMERGENCY EXIT LIGHT DIM. REPAIRED EMERGENCY EXIT LIGHT GROUND WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 26DEF INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 26DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CORRODED (FUSELAGE)

TUL - MINOR CORROSION AROUND ANTENNA FASTENER ATTACH HOLE IN FUSELAGE SKIN AND ALSO DENT SHOWING EDGE OF ANTENNA DOUBLER. BLENDED MINOR GOUGES AND REMOVED MINOR CORROSION, TREATED WITH ALODINE. DENT IS COND II PER SRM 53-04 FMR MADE FOR REPAIR AT NEXT HEAVY C-CHECK. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FORWARD SECTION OF COACH INOPERATIVE. REPAIRED WIRING ON EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN FIRST CLASS AND COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — CHAFED (FUSELAGE)

STL - FLT 2257 - NEAR TOP OF CLIMB, CREW HEARD A LOUD POP AND SAW A FLASH OF LIGHT FROM THE EPC CIRCUIT BREAKER PANEL. NO BREAKERS WERE TRIPPED. MINUTES LATER ANOTHER POP AND FLASH CAME FROM THE EPC CIRCUIT BREAKER PANEL. AN ACRID SMELL OF BURNING INSULATION WAS NOTED AT FL 30. FLIGHT LANDED STL AND CREW PERFORMED EMERGENCY FIRE/ELECTRICAL CHECKLIST WITH NO SMOKE OR FIRE DETECTED. MAINTENANCE TROUBLESHOT AND FOUND PASSENGER POWER PORT FEEDER CABLE CHAFFED AT COCKPIT DOOR SOLENOID. SYSTEM WAS DEACTIVATED PER ECO. GROUND RAN BOTH ENGINES AND OPERATED PACKS WITH BUSSES LOADED AND NO ABNORMAL SMELL NOTED. AIRCRAFT OPERATED TO DFW AND OVERNIGHTED. MAINTENANCE REPAIRED DAMAGED POWER PORT FEEDER CABLE. REROU

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS BY AFT ENTRY DOOR INOPERATIVE. REPAIRED WIRE ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL. (M)

Part: LIGHT — DEFECTIVE (CABIN)

PHX - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY FLOOR LIGHTING NEAR PASSENGER SEAT 20DEF INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT PASSENGER SEAT 20DEF. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — DEFECTIVE (STAIRWAY)

DFW - DURING OVERNIGHT CHECK, AFT SIDEWALL EMERGENCY LIGHT IN AFT STAIRWAY INOPERATIVE. REPLACED AFT SIDEWALL EMERGENCY LIGHT IN AFT STAIRWAY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)