N586AA

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 65,538 hrs · 34,044 cycles

LEFT HAND STRUT DOOR AFT HINGE CUT OUT CRACKED. INSTALLED DOUBLER IAW SRM 53-05-00 FIGURE 62.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 65,538 hrs · 34,044 cycles

RIGHT WW GREEN SHELF BRACKET AT THE UPPER END OF THE GEAR DOOR ACTUATOR IS CRACKED AT THE AFT INBD SIDE. INSTALLED DOUBLER IAW AARD 53-10-00-38.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 65,538 hrs · 34,044 cycles

RIGHT HAND STRUT DOOR AFT HINGE CUT OUT CRACKED. INSTALLED DOUBLER IAW SRM 53-05-00 FIGURE 62.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 65,538 hrs · 34,044 cycles

MID CARGO DOOR FWD SIDE STOP FITTING CRACKED. REPLACED STOP FITTING IAW AARD 51-00-05-1.

Part: CONNECTOR — LEAKING (AC BAY) · airframe 65,516 hrs · 34,028 cycles

CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE INDICATION. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND RT PACK LEAKING FROM SLIP CONNECTOR & DUCT OVERHEAT SWITCH INOPERATIVE. REPLACED SEALS IN SLIP CONNECTOR & REPLACED DUCT OVERHEAT SWITCH. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: RIB — CRACKED (RT WING) · airframe 65,486 hrs · 34,009 cycles

RIGHT NR 4 LE SLAT RIB INBD CASTING CRACKED. REPLACED CASTING IAW AARD 51-00-05-1.

Part: FORMER — CRACKED (SLAT TRACK) · airframe 65,486 hrs · 34,009 cycles

LEFT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED LT WING NR 4 INBD FORMER DOUBLER IAW WORK CARD 57-98-03 & EA MD80-57-034944.

Part: CONTROLLER — INOPERATIVE (ANTI-SKID SYS) · airframe 64,539 hrs · 33,484 cycles

IAD INFLIGHT DFW-DCA. CREW REPORTED ANTI SKID FAULT INDICATION DURING APPROACH. FLIGHT DIVERTED IAD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED ANTI SKID CONTROL. SYSTEM GND CHECKED NORMAL OPERATION CLOSED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,556 hrs · 31,823 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED RIGHT AFT LAVATORY BATTERY PACK. OPS CHECK NORMAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 58,127 hrs · 29,892 cycles

DENT ON LEFT SIDE OF FUSELAGE AT THE TOP OF AA OF 586AA. INSTALLED FILLER AND DOUBLER AT STATION 1431 LONGERON 8 LEFT PER SRM 53-04-00 FIGURE 18 SHEET 1 AND 2.

Part: SKIN — DENTED (FUSELAGE) · airframe 58,127 hrs · 29,892 cycles

TWO DENTS APPROXIMATELY 2 INCHES APART IN FUSELAGE 40 AND 58 INCHES FORWARD OF CENTER CARGO DOOR CUTOUT AND 10 INCHES BELOW RIGHT TURNOFF LIGHT STATION 579 AT LONGERON 22 RIGHT. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER PER SRM 53-04-03, DWG SG09530002 AND SRM 51-60-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 3 · airframe 58,127 hrs · 29,892 cycles

NUMBER 6 SEAT TRACK CORRODED BEYOND LIMITS AT STATIONS 215 TO 218. INSTALLED NEW SEAT TRACK NUMBER 6 STATIONS 215 TO 265 AND SPLICE AT STATION 265 PER SRM 53-05-00 FIGURE 4F.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 58,127 hrs · 29,892 cycles

ELONGATED HOLES IN CUSP, UNDER NUMBER 6 SEAT TRACK STATIONS 221 TO 235. INSTALLED CUSP SHEET ON RIGHT SIDE AT STATIONS 218 TO 237 PER AARD 51-10-00-5.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,127 hrs · 29,892 cycles

CORROSION ON SUBFLOOR UNDER G1 GALLEY DRAIN PAN. INSTALLED G1 GALLEY SUB-FLOOR DOUBLER AARD 53-20-00-16.

Part: STRUCTURE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 58,127 hrs · 29,892 cycles

CORROSION AROUND AFT LAV SERVICE PANEL CUTOUT IN CARGO, STATIONS 1316 TO 1322, LONGERONS 21 TO 22. INSTALLED REPAIR DOUBLER PER EA MD80 53-018439.

Part: TIE DOWN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,127 hrs · 29,892 cycles

CORROSION ON TOP OF RIGHT TIE-DOWN TRACK, STATIONS 1007 TO 1155. INSTALLED NEW TIE-DOWN TRACK PER AARD 51-10-00-5 AND SRM 51-30-01.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 58,127 hrs · 29,892 cycles

AFT CARGO CORROSION ON LOWER FORWARD ANGLE IN DOOR CUTOUT FORWARD OF STATION 1155 FRAME. INSTALLED NEW LOWER ANGLE AT STATION 1155 PER SRM 51-30-05.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 58,127 hrs · 29,892 cycles

CABIN FORWARD SUBFLOOR CRACKED AT FASTENER STATIONS 179, 26 INCHES RIGHT OF CENTER LINE. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 58,127 hrs · 29,892 cycles

ELONGATED HOLES IN CUSP UNDER NUMBER 6 SEAT TRACK, STATIONS 221 TO 235. REMOVED DAMAGED CUSP, STATIONS 218 TO 237, AND INSTALLED SERVICEABLE CUSP PER AARD 51-10-00-5.

Part: SKIN — GOUGED (FUSELAGE) · airframe 58,127 hrs · 29,892 cycles

GOUGE IN SKIN AT STATION 1406 ABOVE STRINGER 5 RIGHT. INSTALLED DOUBLER AND FILLER PER SRM 53-01-00 FIGURE 2 SHEET 3.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,127 hrs · 29,892 cycles

CORROSION ON SUBFLOOR UNDER FIBERGLASS HAT CHANNEL INBOARD OF FORWARD SERVICE DOOR. INSTALLED DIAPHRAM REPAIR DOUBLER AT STATIONS 160 TO 200 RIGHT BUTTLINES 36 TO 56 PER AARD 53-20-00-16.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · airframe 58,127 hrs · 29,892 cycles

CORROSION UNDER AFT G-2 MOUNT INBOARD. INSTALLED NEW DOUBLER PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 58,127 hrs · 29,892 cycles

CORROSION ON G1 GALLEY FORWARD MOUNT, 12 INCHES INBOARD OF FORWARD SERVICE DOOR AT STATION 160. INSTALLED NEW GALLEY MOUNT PER AARD 51-10-00-5.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 58,127 hrs · 29,892 cycles

CORROSION ON G2 AFT INBOARD MOUNT. INSTALLED NEW G2 AFT INBOARD MOUNT PER AARD 51-10-00-5.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 58,127 hrs · 29,892 cycles

CORROSION ON G1 GALLEY FORWARD MOUNT, 6 INCHES INBOARD OF FORWARD SERVICE DOOR AT STATION 160. INSTALLED NEW G1 GALLEY MOUNT PER AARD 51-10-00-5.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 58,127 hrs · 29,892 cycles

GOUGED DENT IN SKIN STATION 1380 BETWEEN STRINGERS 8 AND 9 RIGHT. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-01-00 FIGURE 2 SHEET 3.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 58,127 hrs · 29,892 cycles

CORROSION ON BOTTOM OF SUBFLOOR BELOW NUMBER 1 SEAT TRACK STATION 1175. INSTALLED NEW CUSP MEMBRANE PER DRAWING SG09530019.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,127 hrs · 29,892 cycles

CORROSION ON SUBFLOOR WEB STATION 1142 INBOARD OF AFT SERVICE DOOR. INSTALLED .040" 6A1-4V TITANIUM REPAIR DOUBLER LEFT SUBFLOOR WEB STATION 1142 PER AARD 53-20-00-16 AND AARD 51-60-00-01.

Part: SKIN — GOUGED (FUSELAGE) · airframe 58,127 hrs · 29,892 cycles

AFT FUSELAGE IS GOUGED STATION 1320 JUST BELOW LONGERON 24 RIGHT. INSTALLED REPAIR DOUBLERS AND FILLER PER SRM 53-04-02 AND BOEING DOCUMENT SG09530001 ZONE 104 FIGURE H2.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 58,127 hrs · 29,892 cycles

SUBFLOOR CRACKED AT FASTENER STATION 179, 26 INCHES RIGHT OF CENTER LINE. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: DOOR — DENTED (CARGO BAY) · airframe 58,127 hrs · 29,892 cycles

FORWARD CARGO DOOR HAS DENT JUST BELOW NUMBER 3 BEAM AT FORWARD END OF DOOR. INSTALLED DOUBLER ON CARGO DOOR PER SRM 52-02-00 PG 6 FIGURE 1 SHEET 1.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 58,127 hrs · 29,892 cycles

CORROSION ON SUBFLOOR WEB STATION 1165 INBOARD OF AFT SERVICE DOOR. INSTALLED LEFT CUSP DOUBLER REPAIR AT STATION 1165 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 58,127 hrs · 29,892 cycles

HOLE ON LEFT CUSP AT STATION 551. INSTALLED DOUBLER ON LEFT CUSP AT STATION 551 PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 58,127 hrs · 29,892 cycles

RIGHT CUSP DAMAGED AT STATIONS 550 TO 551. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 58,127 hrs · 29,892 cycles

WINDOW PAN CRACKED STATION 1174 RIGHT FORWARD LOWER. INSTALLED REPAIR ANGLE AS PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 58,127 hrs · 29,892 cycles

WINDOW PAN CRACKED STATION 1060 RIGHT AFT UPPER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 58,127 hrs · 29,892 cycles

CRACK ON LEFT CUSP AT STATION 1244. INSTALLED REPAIR DOUBLER ON LEFT CUSP AT STATION 1244 PER AARD 53-20-00-16.

Part: PAN — CRACKED (WINDOW) · airframe 58,127 hrs · 29,892 cycles

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

Part: PAN — CRACKED (WINDOW) · airframe 58,127 hrs · 29,892 cycles

WINDOW PAN CRACKED BETWEEN STATIONS 769 AND 788 LEFT SIDE, TOP FORWARD CORNER. INSTALLED REPAIR ANGLE DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 58,127 hrs · 29,892 cycles

WINDOW PAN CRACKED STATION 1174 RIGHT FORWARD UPPER. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 58,127 hrs · 29,892 cycles

WINDOW PAN CRACKED STATION 1174 RIGHT AFT UPPER. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 58,127 hrs · 29,892 cycles

WINDOW PAN CRACKED BETWEEN STATIONS 769 AND 788 LEFT SIDE, TOP FORWARD CORNER. INSTALLED REPAIR ANGLE DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 58,127 hrs · 29,892 cycles

WINDOW PAN CRACKED BETWEEN STATIONS 946 AND 965 LEFT SIDE, LOWER FORWARD CORNER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 58,127 hrs · 29,892 cycles

WINDOW PAN CRACKED BETWEEN STATIONS 1079 AND 1098 LEFT SIDE, LOWER AFT CORNER. INSTALLED REPAIR ANGLE AS PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 58,127 hrs · 29,892 cycles

WINDOW PAN CRACKED BETWEEN STATIONS 845 AND 864 LEFT SIDE, TOP FORWARD CORNER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 58,127 hrs · 29,892 cycles

WINDOW PAN CRACKED BETWEEN STATIONS 1079 AND 1098 LEFT SIDE, TOP AFT CORNER. INSTALLED REPAIR ANGLE AS PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 58,127 hrs · 29,892 cycles

WINDOW PAN CRACKED BETWEEN STATIONS 1003 AND 1022 LEFT SIDE, TOP AFT CORNER. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 58,127 hrs · 29,892 cycles

WINDOW PAN CRACKED BETWEEN STATIONS 1041 AND 1060 LEFT SIDE, LOWER FORWARD CORNER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 58,127 hrs · 29,892 cycles

WINDOW PAN CRACKED BETWEEN STATIONS 1022 AND 1041 LEFT SIDE, LOWER FORWARD CORNER. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 58,127 hrs · 29,892 cycles

WINDOW PAN CRACKED BETWEEN STATIONS 1041 AND 1060 LEFT SIDE, TOP AFT CORNER, AROUND FASTENER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: BEARING — CRACKED (GEAR HANDLE) · airframe 56,795 hrs · 29,150 cycles

ELP CREW REPORTED ON APPROACH NO DOWN AND LOCKED INDICATION WHEN GEAR SELECTED DOWN. RECYCLED GEAR, STILL NO DOWN AND LOCKED INDICATION. USED ALTERNATE GEAR DOWN AND ALL THREE GEAR INDICATED DOWN AND LOCKED. EMERGENCY DECLARED FLIGHT LANDED ELP WITHOUT INCIDENT. REPLACED GEAR HANDLE BEARING. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SWITCH — FAULTY (COCKPIT) · airframe 55,850 hrs · 28,629 cycles

ON INITIAL APPROACH TO LAX THE CREW DROPPED THE GEAR AND ALL THREE INDICATORS FOR THE LANDING GEAR SHOWED RED. SECOND ATTEMPT AT PUTTING THE GEAR DOWN HAD SAME RESULTS AND GO AROUND WAS MADE. ON THIRD ATTEMPT THE HANDLE WAS PLACED DOWN AND THIS TIME THE NOSE WENT GREEN FOLLOWED A MOMENT LATER BY THE MAINS ALSO GOING GREEN. REPLACED LANDING GEAR LEVER SWITCH AND PROXIMITY SWITCH ELECTRONIC UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY — NOT SEATED (CABIN) · airframe 52,662 hrs · 26,894 cycles

CEILING EMERGENCY LIGHTS INOPERATIVE FROM ROWS 28 TO 32. RESET BATTERIES AT ROW 28. CEILING LIGHTS CHECKED NORMAL AT ROWS 28-32.

Part: WIRE — DAMAGED (CABIN) · airframe 52,662 hrs · 26,894 cycles

EXIT LIGHT BY FLOOR ACROSS FROM FORWARD LAVATORY INOPERATIVE. REPAIRED WIRE AT EXIT LIGHT BY FORWARD LAVATORY. OPS CHECK NORMAL.

Part: SLIDE — INOPERATIVE (GALLEY DOOR) · airframe 51,238 hrs

DFW - CABLE PROTRUDING FROM BEHIND SLIDE PACK AT AFT GALLEY DOOR. REMOVED AND REPLACED SLIDE AT AFT GALLEY DOOR.

Part: CASTING — CRACKED (SPOILER ACTUATOR) · airframe 50,874 hrs · 25,914 cycles

GROUND SPOILER ACTUATOR CASTING CRACKED FORWARD INBD CORNER, LEFT GROUND SPOILER. INSTALLED REPAIR DOUBLER PER AARD 57-20-00-15.

Part: OUTFLOW VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 49,092 hrs

DFW - INFLIGHT T468/10APR - CREW REPORTED UNABLE TO CONTROL CABIN PRESSURE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND OUTFLOW VALVE UNABLE TO CLOSE. REPLACED OUTFLOW VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — DAMAGED (EMERGENCY LIGHTS) · airframe 48,233 hrs

DFW - EMERGENCY LIGHT AT SEAT 10D SHROUD DAMAGED. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — DAMAGED (EMERGENCY LIGHTS) · airframe 48,233 hrs

DFW - EMERGENCY LIGHT AT SEAT 7D SHROUD DAMAGED. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — DAMAGED (EMERGENCY LIGHTS) · airframe 48,233 hrs

DFW - EMERGENCY LIGHT AT SEAT 12D SHROUD DAMAGED. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRAP — BROKEN (FLASHLIGHT MOUNT)

LGA - FORWARD LOWER EMERGENCY FLASHLIGHT HAS BROKEN STRAP. REPLACED STRAP FOR FORWARD LOWER EMERGENCY FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRUT — INOPERATIVE (NLG)

ORD INFLIGHT T1766/03FEB - DURING GEAR RETRACTION GEAR HANDLE WOULD ONLY COME UP HALF WAY. ON THIRD ATTEMPT TO RAISE GEAR THE HANDLE CAME FULL UP AND THE NOSE GEAR RED INDICATION LIGHT ILLUMINATED. GEAR DOOR OPEN LIGHT WAS EXTINGUISHED. HEARD LOUD NOISE COMING FROM NOSE GEAR AREA. AFTER A FEW MINUTES NOISE STOPPED AND ALL INDICATION LIGHTS EXTINGUISHED. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. INSPECTED AND REPACKED NOSE STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: APU — FAILED (APU BAY)

INFLIGHT - DURING CLIMB AND HIGH POWER SETTING SMOKE/HAZE IN BOTH CABIN AND COCKPIT. SMOKE/HAZE WOULD ONLY DISSAPATE DURING LOWER POWER SETTINGS. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED APU. SYSTEM GROUND CHECKED NORMAL OPERATIONS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

OVERHEAD EMERGENCY LIGHTS AT ROWS 4 THROUGH 6 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 4 THROUGH 6. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED.

Part: WIRE — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE OBSERVED EMERGENCY LIGHT INOPERATIVE IN THE TAILCONE WALKWAY. REPAIRED ELECTRICAL WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, LOWER OVERWING EMERGENCY EXIT SIGN AT ROW 21 AB INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT WIRE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, WHILE TROUBLESHOOTING 21AB EMERGENCY EXIT LIGHT BATTERY DISCOVERED BROKEN WIRE ON PLUG. REPLACED EMERGENCY EXIT LIGHT BATTERY AND MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — UNSECURE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT SIGN BY SEAT 21A INOPERATIVE. SECURED EMERGENCY EXIT LIGHT SIGN BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS STATION 140 TO 213 DIM. REPLACED BATTERY PACK FOR EMERGENCY EXIT ESCAPE PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — TORN (CABIN)

JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT BETWEEN 23H AND 24H TORN. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP BETWEEN 23H AND 24H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (TAIL CONE)

DFW DURING OVERNIGHT MAINTENANCE TAIL CONE EMERGENCY EXIT LIGHT BROKEN. REPLACED TAIL CONE EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (COCKPIT)

FLT 447 - EN ROUTE ORD-LAX, AFTER TAKEOFF NOSE GEAR PIN DOWN AND LOCKED INDICATOR GREEN LIGHTS INOPERATIVE. DECLARED EMERGENCY AND LANDED LAX WITHOUT INCIDENT. REPLACED NOSE GEAR DOWN AND LOCKED GREEN LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — LOOSE (CABIN)

PHX - DURING OVERNIGHT MAINTENANCE, RIGHT AFT BOTTOM OVERWING DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPAIRED WIRES ON RIGHT AFT BOTTOM OVERWING DOOR EMERGENCY EXIT SIGN CONNECTOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — MALFUNCTIONED (AIRSTAIRS)

ORD - FLT 1105 - AFTER SHUTDOWN AT MAINTENANCE HANGAR DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHTS ILLUMINATED AND WOULD NOT TURN OFF. RESET AFT AIRSTAIR EMERGENCY EXIT LIGHT CIRCUIT BREAKERS. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: FRAME — CRACKED (BW 1418)

TUL - STA 1418, BELT FRAME CRACKED AT NR 2 LONGERON, RIGHT ATTACHMENT. INSTALLED BELT FRAME REPAIR PER SRM 53-03. TST: 23,816.18 HOURS. CYCLES: 12,127. (X)

Part: LONGERON — GOUGED (BS 1355)

TUL - STA 1355 LONGERON 19L IS GOUGED/WORN. REPAIRED LONGERON 19L AT STA 1355 PER ESO 80559 DATED 7-1-99. TST: 23,816.18 HOURS. CYCLES: 12,127. (X)

Part: LONGERON — CRACKED (BS 1418)

TUL - STA 1418, LONGERON NR 2 RIGHT, CRACKED ON AFT OUTBOARD SIDE, LOCATED AFT SIDE OF BELT FRAME, STA 1418. INSTALLED LONGERON REPAIR PER AARD 53-30-00-2. TST: 23,816.18 HOURS. CYCLES: 12,127. (X)

Part: FITTING — BROKEN (BS 218)

TUL - BOLT BROKEN IN G-2 AFT INBOARD HOLD-DOWN FITTING FOR GALLEY. REPLACED UPPER AND LOWER HOLD-DOWN CASTINGS FOR GALLEY AND ACCOMPLISHED SUB-FLOOR DOUBLER PER SRM 53-01 FIG 4 REV 133 NOTE C AARD 53-00-00-02. TST: 23,816.18 HOURS. CYCLES: 12,127. (X)

Part: LIGHT — DEFECTIVE (ROW 12 DEF)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT ROW 12 DEF WERE INOPERATIVE. REPLACED EMERGENCY FLOOR PATH LIGHT STRIP AT SEAT ROWS 12 DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, FIRST CLASS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT STRIP AT FIRST CLASS EMERGENCY EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, THE SIDEWALL FORWARD POSITION AFT STAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED SPLICE AT SIDEWALL FORWARD POSITION AFT STAIR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: EEL CONNECTOR — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN AFT CABIN FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR IN AFT CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)