N70504

Part: FRAME — WORN (FUSELAGE) · airframe 73,698 hrs · 39,169 cycles

WORN AREA ON FRAME 1510, ALONG AFT BOTTOM SIDE. INSTALLED DOUBLER ON 1510 FRAME 3" X 12" IAW WITH EA 256856.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 73,698 hrs · 39,169 cycles

CARGO MID CX, CRACKED DOOR STOP PAD SUPPORT BRACKET, FWD SIDE OF DOOR AT LOWER STOP. INSTALLED NEW MID CARGO DOOR, FWD LOWER DOOR STOP PAD FITTING IAW AARD 51-00-05-1 & DWG 4920233.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 73,698 hrs · 39,169 cycles

CARGO MID CX, CRACKED DOOR STOP PAD SUPPORT BRACKET FWD SIDE OF DOOR AT SECOND FROM TOP STOP. INSTALLED NEW MID CARGO DOOR FWD SECOND FROM TOP DOOR STOP PAD FITTING IAW AARD 51-00-05-1 & DWG 4920233.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 73,698 hrs · 39,169 cycles

CARGO MID CX, CRACKED DOOR STOP PAD SUPPORT BRACKET, FWD SIDE OF DOOR AT THIRD FROM TOP STOP. INSTALLED NEW MID CARGO DOOR FWD THIRD FROM TOP DOOR STOP PAD FITTING IAW AARD 51-00-05-1 & DWG 4920233.

Part: PSEU — FAULTY (ZONE 500) · airframe 71,581 hrs · 37,937 cycles

REJECTED TAKEOFF, CREW RECEIVED FLAP 1 SLAT AURAL WARNING AT 130 KNOTS ON TAKEOFF. REPLACED PROX SWITCH ELECTRONIC UNIT IAW AMM 32-60-04. SYS CHECKED NORMAL.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 70,735 hrs · 37,416 cycles

GEAR WOULD NOT RETRACT WHEN THE HANDLE WAS PLACED IN UP POSITION. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. ACCOMPLISHED SEVERAL CYCLES OF LG EXTENSION & RETRACTION WITH NO FAULTS NOTED. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: VALVE — FAULTY (AC BAY) · airframe 70,138 hrs · 37,058 cycles

ACRID ELEC ODOR THROUGHOUT CABIN & COCKPIT DURING CLIMB OUT. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LT & RT PRESS REGULATING & SOV. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: RIB — CRACKED (RT WING) · airframe 70,062 hrs · 37,014 cycles

RIGHT WING NR 4 SLAT INBD SUPPORT RIB CRACKED. INSTALLED REPAIR DOUBLER ON RT WING INBD SUPPORT RIB IAW EA MD80-57-035648 & WORK CARD 57-98-06.

Part: RIB — CRACKED (LT WING) · airframe 70,062 hrs · 37,014 cycles

LEFT WING NR 4 SLAT INBD SUPPORT RIB CRACKED. INSTALLED REPAIR DOUBLER ON LT WING INBD SUPPORT RIB IAW EA MD80-57-035648 & WORK CARD 57-98-05.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 70,062 hrs · 37,014 cycles

LONGERON 2 RT AT STATION 1418 CRACKED AFT OTBD END. INSTALLED LONGERON SPLICE REPAIR IAW SRM 53-02-00 & AARD 53-00-00-05.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,062 hrs · 37,014 cycles

CRACK IN FUSELAGE SKIN AT STATION 1309 & LONGERON 5 RT. INSTALLED DOUBLER IAW SRM 53-04-03 FIGURE 8.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,870 hrs · 36,892 cycles

ONE SECTION OF CABIN EMER LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,710 hrs · 36,222 cycles

CABIN EMERGENCY EGRESS LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR CABIN EMERGENCY EGRESS LIGHTS. OPERATIONS CHECKED NORMAL.

Part: RELAY — INOPERATIVE (CABIN) · airframe 66,582 hrs · 35,004 cycles

BATTERY CHARGER LIGHT ILLUMINATED WITH GROUND SERVICE BREAKERS TRIPPED. REPLACED R2-56 RELAY. OPS CHECK NORMAL.

Part: DIODE — FAILED (BATTERY CHARGER) · airframe 66,582 hrs · 35,004 cycles

DFW - CREW REPORTED BATTERY CHARGER FAIL LIGHT ILLUMINATED AND SEVERAL CABIN LIGHTS FAILED. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED R7-51 DIODE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,582 hrs · 35,004 cycles

BATTERY CHARGER LIGHT ILLUMINATED WITH GROUND SERVICE BREAKERS TRIPPED. REPLACED BATTERY PACK. OPS CHECK NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 66,582 hrs · 35,004 cycles

BATTERY CHARGER LIGHT ILLUMINATED WITH GROUND SERVICE BREAKERS TRIPPED. REPLACED BATTERY CHARGER. OPS CHECK NORMAL.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 66,444 hrs · 34,919 cycles

CORROSION ON RIGHT CUSP ANGLE AT STATIONS 210 TO 220. INSTALLED RIGHT CUSP ANGLE REPAIR SPLICE AT STATION 185 PER SRM 53-05-00 FIGURE 55 AND BOEING DRAWING J060288.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 66,444 hrs · 34,919 cycles

MISDRILLED HOLES IN RIGHT CUSP SHEET INBOARD SIDE OF CUSP BETWEEN STATIONS 237 TO 256. INSTALLED DOUBLER AS PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 66,444 hrs · 34,919 cycles

LONGERON 3 LEFT CRACKED AT FLANGES STATION 160. REPLACED LONGERON FROM STATIONS 148 TO 188 WITH SPLICE AT STATION 188 PER SRM 53-02-00 FIGURE 18.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 66,444 hrs · 34,919 cycles

ELONGATED FASTENER HOLE IN UPPER ANGLE OF FLOORBEAM, STATION 617 RIGHT BUTTLINE 50.5, AT NUT PLATE HOLE. INSTALLED REPAIR ANGLE AND FILLER PER SRM 53-05-00 FIGURE 20A (SHEET 1).

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 66,444 hrs · 34,919 cycles

E AND E COMPARTMENT, RIGHT CUSP HAS CORROSION ON LOWER SIDE FROM STATIONS 180 TO 190 AT LONGERON 18 RIGHT. INSTALLED CUSP REPAIR PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 66,444 hrs · 34,919 cycles

LONGERON 2 LEFT, STATION 160 IS CRACKED ON LEFT FLANGE RADIUS FROM FRAME FASTENER. INSTALLED NEW LONGERON WITH SPLICE AT STATION 168 PER SRM 53-02-00 FIGURE 18.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 66,444 hrs · 34,919 cycles

HOLE TORN IN CUSP SHEET AT STATION 597 AT RIGHT BUTTLINE 56. INSTALLED DOUBLER ON CUSP PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,444 hrs · 34,919 cycles

E AND E COMPARTMENT, RIGHT CUSP HAS CORROSION ON LOWER SIDE FROM STATIONS 180 TO 190 LONGERON 18 RIGHT. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,444 hrs · 34,919 cycles

SUBFLOOR FACTORY DOUBLER FROM STATIONS 160 TO 180, RIGHT BUTTLINES 44 TO 57 CORRODED. INSTALLED NEW SUBFLOOR FACTORY DOUBLER PER AARD51-00-05-1 AND BOEING DRAWING 9936534.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 66,444 hrs · 34,919 cycles

STATION 1338, BUTTLINE 0, DOUBLER CRACKED UPPER END OF STIFFENER ABOVE BULKHEAD DOOR. REMOVED DAMAGED STIFFENER AND CLIP AND INSTALLED SERVICEABLE STIFFENER AND CLIP PER AARD 51-00-05-1 AND EA MD80-53-027537.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,444 hrs · 34,919 cycles

RIGHT CUSP FROM STATIONS 1130 TO 1135 CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 66,444 hrs · 34,919 cycles

AFT CARGO LEFT TIE DOWN TRACK HAS CORROSION AT STATION 1174. INSTALLED NEW LEFT TIE DOWN TRACK FROM STATIONS 1003 TO 1215 PER IPC 25-52-00-03L, SRM 51-30-05 AND SRM 51-30-01.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 66,444 hrs · 34,919 cycles

INTERCOSTAL BETWEEN CABIN FLOORBEAMS FROM STATIONS 1287 TO 1309 BUTTLINE 0 CRACKED AT ATTACH HOLES. REMOVED DAMAGED INTERCOSTAL AND INSTALLED SERVICEABLE INTERCOSTAL PER AARD 51-00-05-1.

Part: PAN — CRACKED (FUSELAGE) · airframe 66,444 hrs · 34,919 cycles

RIGHT WINDOW PAN CRACKED BETWEEN STATIONS 769 TO 788 AT LOWER FORWARD CORNER. INSTALLED DOUBLER REPAIR AND FILLER PER AARD 53-10-00-25.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 66,444 hrs · 34,919 cycles

CORROSION ON CUSP SHEET AT STATION 1166 BELOW AFT SERVICE DOOR GIRT BAR FITTING. INSTALLED CUSP REPAIR DOUBLER PER BOEING DRAWING 9930612 AND AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,444 hrs · 34,919 cycles

AFT CARGO LEFT CUSP CORRODED FROM STATIONS 1136 TO 1155. INSTALLED CUSP REPAIR DOUBLER PER AARD 53-20-00-16.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 66,444 hrs · 34,919 cycles

CORROSION ON T FITTING BELOW CUSP SHEET FOR AFT SERVICE DOOR GIRT BAR FITTING AT STATION 1166. INSTALLED NEW T FITTING PER AARD 53-20-00-16 AND SRM 51-30-05.

Part: BEAM — CORRODED (FUSELAGE) · airframe 66,444 hrs · 34,919 cycles

AFT CARGO DOOR BEAM CORRODED FROM STATIONS 1155 TO 1212. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-10-00-3.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,444 hrs · 34,919 cycles

LEFT CUSP CORRODED FROM STATIONS 725 TO 727. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 66,444 hrs · 34,919 cycles

LIGHTNING STRIKE DAMAGE AT STATION 323 AND LONGERON 28 RIGHT. INSTALLED REPAIR DOUBLER AND FINGERS PER SRM 53-04-03.

Part: FAIRING — CRACKED (ELEVATOR TAB) · airframe 66,444 hrs · 34,919 cycles

TAB FAIRING CRACKED ON LEFT ELEVATOR. INSTALLED REPAIR DOUBLER PER ESO 80080 PG 601(O).

Part: SKIN — DAMAGED (TE FLAP) · airframe 66,444 hrs · 34,919 cycles

RIGHT WING INBOARD FLAP DENT IN BOTTOM SKIN 15 INCHES FROM INBOARD EDGE OF WEDGE. REMOVED AND REPLACED RIGHT INBOARD FLAP AFT WEDGE LOWER SKIN PER ESO 80095 AND SRM 51-01-00.

Part: SKIN — DAMAGED (TE FLAP) · airframe 66,444 hrs · 34,919 cycles

RIGHT WING INBOARD FLAP DENT IN BOTTOM SKIN 18 INCHES FROM INBOARD EDGE OF WEDGE. REMOVED AND REPLACED RIGHT INBOARD FLAP AFT WEDGE LOWER SKIN PER ESO 80095 AND SRM 51-01-00.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 66,247 hrs · 34,810 cycles

SEAT 18D THRU 32D EMERGENCY CEILING LIGHTS INOPERATIVE. RESEATED BATTERY PACK. OPS CHECK NORMAL.

Part: CONTACT — DIRTY (EMERGENCY LIGHTS) · airframe 65,699 hrs · 34,493 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 23 TO 27 INOPERATIVE. FOUND CONTACTS ON BATTERY PACK DIRTY. CLEANED CONTACTS. OPS CHECK NORMAL.

Part: CONTACT — DIRTY (EMERGENCY LIGHTS) · airframe 65,699 hrs · 34,493 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. FOUND CONTACTS ON BATTERY PACK DIRTY. CLEANED CONTACTS. OPS CHECK NORMAL.

Part: CIRCUIT BREAKER — FAILED (AC BUSS) · airframe 64,752 hrs · 33,965 cycles

INFLIGHT, CREW REPORTED MULTIPLE ELECTRICAL FAILURES. LT AC BUSS B BREAKER TRIPPED IN FLT. EMERGENCY DECLARED FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACE LEFT AC BUSS CIRCUIT BREAKER AND AC POWER RELAY. SYSTEM GROUND CHECKED NORMAL.

Part: GYRO — FAILED (COCKPIT) · airframe 62,820 hrs · 32,858 cycles

STL - INFLIGHT DFW-CMH. CREW REPORTED ELECTRICAL ANOMOLY IN WHICH AUTO THROTTLES DISENGAGED, CAPTAINS FD BARS BIASED OUT OF VIEW, CAPTAINS FLIGHT MANAGEMENT ANNUNCIATOR WINDOWS WENT BLANK AND NO AUTOLAND ILLUMINATED. RE-ENGAGED AUTOTHROTTLE WITH NO SUBSEQUENT PROBLEMS. EMERGENCY DECLARED FLIGHT DIVERTED STL LANDED WITHOUT INCIDENT. REPLACED NUMBER 1 AND 2 GYROS AND BOTH FLIGHT GUIDANCE COMPUTERS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: MODULE — DEFECTIVE (CABIN) · airframe 61,979 hrs · 32,381 cycles

OVERWING EXIT DOOR LOWER EXIT LIGHT DIM. REPLACED MODULE FOR OVERWING EXIT DOOR LOWER EXIT LIGHT. OPS CHECK NORMAL.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 61,986 hrs · 32,385 cycles

FORWARD FUSELAGE LONGERON 5 RIGHT DAMAGED. ACCOMPLISHED DOUBLER REPAIR PER EA MD80-53-015522.

Part: GCU — FAULTY (ELECTRICAL SYS) · airframe 60,189 hrs · 31,405 cycles

DFW - CREW REPORTED MULTIPLE ELECTRICAL PROBLEMS. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED GENERATOR CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 58,700 hrs · 30,596 cycles

CREW REPORTED SMOKE IN CABIN OF AIRCRAFT DURING DESCENT. SMOKE LASTED 10 TO 15 MINUTES THEN GOT BETTER. TURNED GALLEY POWER OFF AS A PRECAUTION. SMOKE DISSIPATED PRIOR TO LANDING. LANDED WITHOUT INCIDENT. PERFORMED PACK BURN AND REPLACED SOCKS IN LEFT AND RIGHT WATER SEPARATORS.

Part: ACTUATOR — FAULTED (LE SLAT) · airframe 57,867 hrs · 30,120 cycles

DFW - AUTO SLAT FAIL LIGHT ILLUMINATED ON TAKEOFF OUT OF AUS THEN HAD FLAP DISAGREE LIGHT ON DESCENT. LANDED DFW WITHOUT INCIDENT. FOUND FORWARD AUTO SLAT ACTUATOR FAULTED. REPLACED ACTUATOR AND ADJUSTED CONTROL VALVE. SYSTEM GROUND CHECKED NORMAL OPERATIONS.

Part: SWITCH — DEFECTIVE (AC SYSTEM) · airframe 56,907 hrs · 29,569 cycles

DFW - LEFT AIR CONDITIONING PACK FAILED. RIGHT PACK WAS ON PLACARD. EMERGENCY DECLARED, LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLOW CONTROL VALVE AND LEFT TURBINE INLET AND OUTLET OVERTEMP SWITCHES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CUSP WEB — CORRODED (BS 148-151) · airframe 55,642 hrs · 28,878 cycles

CORROSION FOUND ON RT CUSP DIAPHRAGM AT FORWARD CABIN STATION 148 TO 151. AREA OF DISCREPANCY IS 12 INCHES BY 14 INCHES. INSTALLED DOUBLER IN RT FORWARD CABIN AT STATION 148 TO 151 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (BS 148) · airframe 55,642 hrs · 28,878 cycles

CORROSION FOUND BEYOND LIMITS ON RT CUSP TEE AT CABIN FLOOR STATION 148. SPLICED IN NEW SECTION IN RT CABIN FLOOR IN ACCORDANCE WITH ESO 80559 DATED 19 SEP 2008.

Part: BRACKET — CORRODED (BS 1193 L29R) · airframe 55,642 hrs · 28,878 cycles

CORROSION FOUND ON L BRACKET IN AFT CARGO AT STATION 1193 LONGERON 29 RT. AREA OF DISCREPANCY IS 1/2 INCH BY 1 INCH WITH A DEPTH OF .060 INCH. INSTALLED NEW L BRACKET IN AFT CARGO AT STATION 1193 LONGERON 29 RT PER SRM 51-01-00.

Part: CARGO TRACK — CORRODED (BS 1003-1155) · airframe 55,642 hrs · 28,878 cycles

CORROSION FOUND ON RT CARGO TIE DOWN TRACK IN AFT CARGO. AREA OF DISCREPANCY IS 1 INCH BY 4 INCHES WITH A DEPTH OF .090 INCH. INSTALLED NEW RT CARGO TIE DOWN TRACK IN AFT CARGO PER SRM 51-01-00.

Part: CUSP WEB — CRACKED (BS 226) · airframe 55,642 hrs · 28,878 cycles

LT CUSP IS CRACKED AT STATION 226. CRACK LENGTH IS 3 INCHES. REPLACED LT CUSP PER SRM 51-01-00.

Part: FRAME — CORRODED (BS 1060) · airframe 55,642 hrs · 28,878 cycles

TUL FRAME IN AFT CARGO IS CORRODED. AREA OF DISCREPANCY IS 1 INCH BY 2 INCHES WITH A DEPTH OF .072 INCHES. INSTALLED DOUBLER ON FRAME IN AFT CARGO PER ESO 80559 DATED 17 SEP 2008.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,642 hrs · 28,878 cycles

CRACK IN THE UPPER RADIUS OF OVERWING FRAME TAB AT RT STATION 905. CRACK LENGTH IS .5 INCHES. INSTALLED NEW FRAME SECTION PER SRM 51-01-00.

Part: PAN — CORRODED (BS 370-427) · airframe 55,642 hrs · 28,878 cycles

FORWARD CARGO DOOR PAN IS CORRODED. AREA OF DISCREPANCY IS 57 INCHES BY 8 INCHES. REPLACED FORWARD CARGO DOOR PAN PER SRM 53-05-00.

Part: FLOOR SUPPORT — CORRODED (BS 160-190) · airframe 55,642 hrs · 28,878 cycles

FLOORBOARD SUPPORT IS CORRODED. AREA OF DISCREPANCY IS 1 INCH BY 30 INCHES. REPLACED FLOORBOARD SUPPORT PER SRM 51-01-00.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 55,642 hrs · 28,878 cycles

CUSP IS CRACKED. AREA OF DISCREPANCY IS 18 INCHES BY 8 INCHES. CRACK LENGTH IS 1 INCH. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (BS 1250-1287) · airframe 55,642 hrs · 28,878 cycles

RT CUSP SHEET IS CORRODED. AREA OF DISCREPANCY IS 12 INCHES BY 37 INCHES. INSTALLED NEW CUSP SHEET PER AARD 53-20-00-16.

Part: BEAM — CORRODED (BS 644-684) · airframe 55,642 hrs · 28,878 cycles

DOUBLER ON MID CARGO DOOR BEAM IS CORRODED. AREA OF DISCREPANCY IS 32 INCHES BY 4 INCHES. INSTALLED DOUBLER ON MID CARGO DOOR BEAM PER AARD 53-10-00-03.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS FROM SEAT ROWS 19 TO 22 INOPERATIVE. REPLACED BATTERY PACK OR EMERGENCY LIGHTS FROM SEAT ROWS 19 TO 22. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

LGA EMERGENCY FLASHLIGHT BY LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT BY LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — INOPERATIVE (CENTER FUEL)

AFT CENTER FUEL PUMP CIRCUIT BREAKER POPPED AND WAS UNABLE TO RESET. LANDED DTW WITHOUT INCIDENT. REPLACED AFT CENTER FUEL BOOST PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW LT AND RT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B549 FOR EMERGENCY LIGHTS AT LT AND RT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW CEILING EMERGENCY LIGHTS AT ROWS 3 THROUGH 6 INOPERATIVE. REPLACED BATTERY PACK AT B5100 FOR CEILING EMERGENCY LIGHTS AT ROWS 3 THROUGH 6. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW CEILING EMERGENCY LIGHTS FROM ROWS 21 THROUGH 27 INOPERATIVE. REPLACED BATTERY PACK AT B5106 FOR AFT CABIN CEILING EMERGENCY LIGHTS AT ROWS 21 THROUGH 27. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - EMERGENCY LIGHTS FROM FLIGHT ATTENDANTS FORWARD FLIGHT STATION TO OVERWING INOPERATIVE. REPLACED BATTERY PACK AT OVERWING FOR EMERGENCY LIGHTS FROM FLIGHT ATTENDANTS FORWARD FLIGHT STATION TO OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY OVERHEAD LIGHT AT ROW 29D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY OVERHEAD LIGHT AT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

DFW OVERHEAD EMERGENCY LIGHT AT ROWS 18 THROUGH 21 AND AFT GALLEY ENTRY DOOR AND TAIL CONE EMERGENCY LIGHT INOPERATIVE. CLEANED CONTACTS AND RECHARGED BATTERY FOR ROWS 18 THROUGH 21 OVERHEAD EMERGENCY LIGHTS, REPLACED BATTERY FOR OVERHEAD EMERGENCY LIGHTS AT AFT GALLEY ENTRY DOOR AND REPLACED BATTERY FOR TAIL CONE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE HARNESS — FAULTY (CABIN)

DFW SEAT 22 EMERGENCY SEAT MOUNTED LIGHTS INOPERATIVE. REPLACED LIGHT HARNESS AT SEAT 22. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: WIRE — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE OBSERVED EMERGENCY LIGHTS INOPERATIVE AFT OF ROW 31. REPAIRED ELECTRICAL WIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, SEAT EMERGENCY PATH LIGHTING FRONT HALF OF AIRCRAFT INOPERATIVE. REPLACED NR 2 BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 7D DIM. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: SMOKE — DETECTED (CABIN)

LAX - FLT 1660 - SECONDS AFTER TAKEOFF FLIGHT ATTENDANT REPORTED ELECTRICAL SMOKE SMELL IN FORWARD GALLEY. SMELL DISSIPATED ON DESCENT OT LAX. LANDED WITHOUT INCIDENT. ACCOMPLISHED PACK BURNOUT. UNABLE TO DUPLICATE SMOKE SMELL. REPLACED COALESCER BAGS AS A PRECAUTION. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: UNKNOWN — ODOR (CABIN)

RDU - FLT 0822 - ELECTRICAL BURNING ODOR DETECTED 1.5 HOURS INTO FLIGHT AT FL 330. VERY STRONG AT FIRST AND DISSIPATED AFTER FEW MINUTES. DIVERTED AND LANDED RDU WITHOUT INCIDENT. COMPLETE INSPECTION OF ELECTRICAL, LIGHTS, AND AIR CONDITIONING SYSTEM ACCOMPLISHED. UNABLE TO DUPLICATE ODOR. ACCOMPLISHED PACK BURNOUT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AFT CABIN INOPERATIVE. REPAIRED WIRING ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, AFT LEFT SERVICE DOOR EMERGENCY EXIT SIDEWALL MARKER INOPERATIVE. REPLACED AFT LEFT SERVICE DOOR EMERGENCY EXIT SIDEWALL MARKER LIGHT ASSEMBLY. GRUOND CHECKED NORMAL OPERATION. (M)

Part: WIRE — LOOSE (CABIN)

DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY LIGHTS IN COCKPIT AND BOTH SIDES OF FORWARD ENTRY INOPERATIVE. RE-SECURED LOOSE WIRE TO EMERGENCY LIGHT PACK ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONDUCTOR — DEFECTIVE (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AFT OF PAX SEAT ROW 28 INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIPS AFT OF PAX SEAT ROW 28. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE, FORWARD OF FIRST CLASS TO MID-COACH SECTION. REPLACED TWO JUMPER WIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRIP — INOPERATIVE (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT AFT SECTION OF MAIN CABIN FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT AFT SECTION OF MAIN CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)