N598AA

Part: BATTERY — DISCHARGED (CABIN) · airframe 70,117 hrs · 30,531 cycles

NUMBER 2 EMER LIGHT BATTERY INOPERATIVE. R & R BATTERY. SYS CHECKED NORMAL.

Part: ENGINE — OVERTEMP (LEFT) · airframe 69,949 hrs · 30,432 cycles

DIVERTED, EMER DECLARED & LANDING UNEVENTFUL. ACFT NOT OVERWEIGHT. DURING CRUISE NOTED LT ENG OIL TEMPERATURE INDICATED HIGH & OIL QTY INDICATED ZERO. OIL PRESS INDICATED IN THE NORMAL RANGE. ALL OIL TEMPERATURE TABS FOUND BLACK. R & R LT ENG IAW MCM 71-91-99. SYS CHECKED NORMAL.

Part: ENGINE — FAILED (LEFT) · airframe 69,204 hrs · 30,040 cycles

LEFT ENG OIL QTY LIGHT ILLUMINATED & INDICATOR WENT TO ZERO. CAPTAIN SHUT DOWN LT ENG, SINGLE ENG TIME 10 MINUTES. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LT ENG ON 08/09/2014. SYS GND CHECKED NORMAL OPERATION OPEN.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,940 hrs · 29,901 cycles

OVERHEAD EMER LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMER LIGHTS IN FIRST CLASS. OPERATIONS CHECKED NORMAL.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 68,342 hrs · 29,574 cycles

FORWARD CARGO DOOR UPPER STOP CASTING CRACKED, REPLACED CASTING.

Part: FORMER — CRACKED (LE SLAT) · airframe 68,332 hrs · 29,566 cycles

RIGHT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED RT WING NR 4 INBD FORMER DOUBLER IAW WORK CARD 57-98-06 & EA MD80-57-034516.

Part: REGULATOR — LEAKING (CREW O2) · airframe 68,092 hrs · 29,442 cycles

PHX CREW REPORTED LOSS OF CREW OXYGEN PRESS. EMERGENCY DECLARED FLIGHT LANDED PHX WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED CAPTAIN`S & FIRST OFFICER`S DEMAND REGULATORS THAT WERE LEAKING. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: GENERATOR — MALFUNCTIONED (RT ENGINE) · airframe 67,190 hrs · 28,952 cycles

DFW CREW REPORTED RT GENERATOR FAULT & AC CROSSTIE FAULT. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RT GENERATOR & CONSTANT SPEED DRIVE TRANSMISSION UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 64,710 hrs · 27,620 cycles

OVERHEAD EMERGENCY LIGHTS FROM ROWS 18 TO 21 INOPERATIVE. RESEATED BATTERY PACK AT ROW 20. OPS CHECK NORMAL.

Part: CHARGER — DISCHARGED (CABIN) · airframe 63,863 hrs · 27,204 cycles

NUMEROUS CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED B1-106 CHARGER ASSEMBLY. OPS CHECK NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 63,863 hrs · 27,204 cycles

NUMEROUS CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED B1-102 CHARGER ASSEMBLY.

Part: VALVE — FAILED (CABIN PRESSURE) · airframe 63,458 hrs · 26,998 cycles

PHL - CREW REPORTED SMOKE IN THE CABIN. EMERGENCY DECLARED FLIGHT LANDED PHL WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT AND RIGHT PRESSURE REGULATING AND SHUT-OFF VALVES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 62,664 hrs · 26,580 cycles

CEILING EMERGENGY LIGHTS FROM ROWS 20 TO 30 INOPERATIVE. RESEATED BATTERY PACK FOR CEILING EMERGENCY LIGHTS FROM ROWS 20 TO 30. OPS CHECK NORMAL.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 62,664 hrs · 26,580 cycles

SEAT 28D FORWARD AND AFT EGRESS LIGHTS INOPERATIVE. RESEATED CONNECTOR UNDER SEAT 28D. OPS CHECK NORMAL.

Part: PRESSURE SWITCH — LEAKING (OIL SYSTEM) · airframe 61,824 hrs · 26,161 cycles

ELP - INFLIGHT SJD-DFW. CREW REPORTED RIGHT ENGINE OIL QUANTITY LOSS. PRECAUTIONARY RIGHT ENGINE SHUTDOWN (SINGLE ENGINE TIME 25 MINS). EMERGENCY DECLARED FLIGHT DIVERTED ELP LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED DIFFERENTIAL PRESSURE SWITCH AND LOW PRESSURE SWITCH THAT WERE LEAKING. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: REGULATOR VALVE — INOPERATIVE (AC BAY) · airframe 61,194 hrs · 25,853 cycles

DFW - CREW REPORTED ELECTRICAL/PLASTIC ODOR IN CABIN. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT AND RIGHT PRESSURE REGULATING AND SHUT-OFF VALVES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,417 hrs · 25,435 cycles

CORROSION ON BOTTOM SIDE OF CUSP T-ANGLE FROM STATIONS 200 TO 217. REMOVED DAMAGED CUSP ANGLE AND INSTALLED NEW ANGLE FROM STATIONS 186 TO 229. ACCOMPLISHED SPLICE REPAIR PER SRM 53-05-00 FIGURE 55 AND BOEING DWG J060288.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,417 hrs · 25,435 cycles

CORROSION ON SUBFLOOR STATIONS 200 TO 210, FORWARD OF SEAT TRACK NUMBER 6. INSTALLED NEW SUBFLOOR PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,417 hrs · 25,435 cycles

CORROSION ON SUBFLOOR, STATION 170, APPROXIMATELY 1 INCH INBOARD OF FORWARD SERVICE DOOR SILL, BETWEEN FLOORBOARD SUPPORTS. INSTALLED NEW SUBFLOOR PER AARD 53-20-00-16.

Part: DOOR FRAME — BENT (FUSELAGE) · airframe 60,417 hrs · 25,435 cycles

WEB AFT OF FORWARD SERVICE DOOR FROM STATIONS 200 TO 207 BENT AT STRINGER 17 RIGHT. INSTALLED FORWARD SERVICE DOOR JAMB INNER WEBBING STATIONS 200 TO 208 PER SRM 51-70-04.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,417 hrs · 25,435 cycles

REINFORCING DOUBLER ON TOP OF SUBFLOOR INBOARD OF FORWARD SEVRICE DOOR FROM STATIONS 160 TO 180 IS CORRODED BEYOND MANUAL LIMITS. INSTALLED NEW DOUBLER ON TOP OF SUBFLOOR STATION 160-180 PER AARD 53-20-00-16.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 60,417 hrs · 25,435 cycles

SEAT TRACK NUMBER 6 CORRODED BEYOND LIMITS STATION 218. REPLACED SEAT TRACK PER SRM 53-05-00.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,417 hrs · 25,435 cycles

SKIN IS CRACKED AT THE UPPER FASTENER IN THE SHEAR TIE AT STATION 1417 BETWEEN LONGERONS 2 AND 3 RIGHT JUST OUTBOARD OF THE VERTICAL STAB RIGHT SKATE ANGLE. INSTALLED REPAIR DOUBLER PER SRM 53-04-00 AND SRM 51-30-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,417 hrs · 25,435 cycles

FRAME CRACKED AFT SIDE OF STATION 1418 AT LONGERON 2 RIGHT. INSTALLED FRAME DOUBLER REPAIR ON AFT SIDE OF STATION 1418 FRAME AT LONGERON 2 RIGHT PER AARD 53-10-00-15.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,417 hrs · 25,435 cycles

FUSELAGE - SKIN IS CRACKED AT THE UPPER FASTENER IN THE SHEAR TIE AT STATION 1417 BETWEEN LONGERONS 2 AND 3 RIGHT JUST OUTBOARD OF THE VERTICAL STABILIZER RIGHT SKATE ANGLE. INSTALLED INTERNAL AND EXTERNAL DOUBLER WITH FILLER PER AARD 51-10-00-5.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 60,417 hrs · 25,435 cycles

VERTICAL STRAP DAMAGED STATION 200 RIGHT SIDE. INSTALLED NEW BELLFRAME STRAP STATION 200 PER AARD 51-10-00-5.

Part: SKIN — DENTED (FUSELAGE) · airframe 60,417 hrs · 25,435 cycles

SHARP DENT IN SKIN ABOVE LONGERON 18 RIGHT STATION 1118. INSTALLED DOUBLER PER SRM 53-04-00 FIGURE 12B.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,417 hrs · 25,435 cycles

CORROSION ON RIGHT TIE DOWN TRACK AT STATION 1155. SPLICED IN NEW TRACK STATIONS 1090 TO 1155 PER SRM 53-05-00.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,417 hrs · 25,435 cycles

SUBFLOOR CORRODED STATION 218 RIGHT BUTTLINES 6 TO 16. INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 60,417 hrs · 25,435 cycles

AFT ACCS LONGERON 2 LEFT CRACKED AFT OF 1418. INSTALLED SPLICE AND LONGERON PER SRM 53-02-00.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 60,417 hrs · 25,435 cycles

G2 GALLEY MOUNT CORROSION OUT OF LIMITS. INSTALLED G2 GALLEY MOUNT PER AARD 51-10-00-5.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,417 hrs · 25,435 cycles

CORROSION ON AFT INBOARD G2 GALLEY MOUNT. REPLACED GALLEY MOUNT PER AARD 51-10-00-5.

Part: STRAP — GOUGED (FUSELAGE) · airframe 60,417 hrs · 25,435 cycles

SCREW GOUGE ON WEBBING STRAP STATION 1150 LONGERON 28 RIGHT. REPLACED STRAP PER AARD 51-10-00-5.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,417 hrs · 25,435 cycles

WEBBING STRAP HAS CORROSION STATION 1193 LONGERON 28 RIGHT. REPLACED STRAP PER AARD 51-10-00-5.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,417 hrs · 25,435 cycles

FUSELAGE SKIN ON FORWARD LOWER CORNER OF AFT LAVATORY SERVICE PAN IS SEPARATED FROM TITANIUM HOURGLASS. INSTALLED INTERNAL TITANIUM REPAIR DOUBLER AT THE AFT LAVATORY PAN CUT OUT AREA PER SRM 53-04-00 FIGURE 38 AND EA MD80-53-017519.

Part: DOOR FRAME — CRACKED (ENTRY DOOR) · airframe 60,417 hrs · 25,435 cycles

FORWARD ENTRY DOOR CRACK IN DOOR AT BAYONET CUTOUT. REMOVED CRACKED FRAME PART AND INSTALLED NEW FRAME PER ESO 80172.

Part: PAN — CRACKED (WINDOW) · airframe 60,417 hrs · 25,435 cycles

LEFT WINDOW PAN CRACKED AT UPPER CORNER STATION 1230. REMOVED DAMAGE AND INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 60,417 hrs · 25,435 cycles

LEFT WINDOW PAN CRACKED AT UPPER CORNER STATION 1078. REMOVED DAMAGE AND INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 60,417 hrs · 25,435 cycles

RIGHT WINDOW PAN CRACKED AT UPPER CORNER STATION 1192. REMOVED DAMAGE AND INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 60,417 hrs · 25,435 cycles

UPPER AFT CORNER OF WINDOW RINGPAN IS CRACKED LEFT STATION 1041. CUT OUT CRACKED AREA OF WINDOW RINGPAN. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 60,417 hrs · 25,435 cycles

UPPER AFT CORNER OF WINDOW RINGPAN IS CRACKED LEFT STATION 1022. CUT OUT CRACKED AREA OF WINDOW RINGPAN. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: DUCT — BLOWN (ACM) · airframe 56,894 hrs · 23,716 cycles

DFW - CREW REPORTED TAIL HIGH TEMP LIGHT COME ON TWICE. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RIGHT PACK ON OUTLET SIDE OF AIR CYCLE MACHINE FLEX DUCT BLOWN OFF. REPOSITIONED DUCT AND SECURED CLAMPS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — GOUGED (FUSELAGE) · airframe 56,229 hrs · 23,426 cycles

DEEP GOUGE IN SKIN. INSTALLED DOUBLER PER AARD 53-30-00-6.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,229 hrs · 23,426 cycles

CUSP DAMAGED RIGHT SIDE. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: PRESSURE SWITCH — DEFECTIVE (OIL SYSTEM) · airframe 54,567 hrs · 22,712 cycles

DFW - CREW REPORTED OIL STRAIN LIGHT INDICATION IN THE RIGHT ENGINE. EMERGENCY DECLARED, RETURNED TO DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED OIL STRAINER DIFFERENTIAL PRESS SWITCH. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY — LOOSE (CABIN) · airframe 54,256 hrs

LGA - AFT TAIL COMPARTMENT EMERGENCY LIGHT ABOVE SLIDE INOPERATIVE. RESECURED LOOSE BATTERIES IN EMERGENCY BATTERY PACK AT AFT RIGHT LAVATORY.

Part: BATTERY — LOOSE (AC BAY) · airframe 54,256 hrs

LGA - AFT TAIL COMPARTMENT EMERGENCY LIGHT ABOVE CATWALK INOPERATIVE. RESECURED LOOSE BATTERIES IN EMERGENCY BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,159 hrs

LGA- FORWARD HOSTESS JUMPSEAT FLASHLIGHT INOPERATIVE. REPLACED BATTERY PACK FOR FLASHLIGHT AT FORWARD HOSTESS JUMPSEAT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LAX - EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5103 FOR EMERGENCY LIGHTS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BLADE — DAMAGED (LT ENGINE)

EWR INFLIGHT T1179/21APR DURING CLIMB LEFT ENGINE COMPRESSOR STALLED AT 600 FEET ABOVE GROUND LEVEL. POSSIBLE BIRD STRIKE. RETURNED TO EWR AND LANDED WITHOUT INCIDENT. ENGINE SHUT DOWN FOR TAXI. REPLACED NUMBER ONE ENGINE ON 20 APR 2007 AT EWR DUE TO BLADE DAMAGE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHTS FROM FLIGHT ATTENDANT STATION NR 1 INOPERATIVE. RECONNECTED BATTERY PACK B549 FOR EMERGENCY LIGHTS FROM FLIGHT ATTENDANT STATION NR 1. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

SFO - AFT GALLEY DOOR SIDEWALL EMERGENCY LIGHT INOPERATIVE. REPINNED CANNON PLUGS FOR AFT GALLEY DOOR SIDEWALL EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY ESCAPE PATH LIGHT IN TAIL CONE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY ESCAPE PATH LIGHT IN TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

SAT EMERGENCY LIGHTS FROM ROWS 21 THROUGH 31 INOPERATIVE. REPLACED CENTER AFT BATTERY MODULE AND BATTERY FOR EMERGENCY LIGHTS FROM ROWS 21 THROUGH 31. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED--

Part: BATTERY — DISCHARGED (CABIN)

STL INSEAT EMERGENCY LIGHTS AT SEAT 13 INOPERATIVE. REPLACED ROW 13 OVERHEAD EMERGENCY LIGHT BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

STL ROW 16 INSEAT EMERGENCY LIGHTS INOPERATIVE. REPLACED ROW 16 INSEAT EMERGENCY LIGHTS BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

STL SEAT 15 LEFT INSEAT EMERGENCY LIGHT INOPERATIVE. REPLACED ROW 15 OVERHEAD EMERGENCY LIGHT BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS WERE INOPERATIVE AT ROWS 23 AND 24. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS WERE INOPERATIVE AT SEAT ROW 25 AND 26. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CORRODED (FUSELAGE)

TUL - FOUND CORROSION AROUND ANTENNA CUTOUT 1 INCH HOLE STATION 380. REMOVED LIGHT CORROSION BY BLENDING PER SRM 51-10-03. (M)

Part: STRUCTURE — CRACKED (FUSELAGE)

TUL - FOUND FS 1418 CRACKED AT 2R. INSTALLED DOUBLER PER 53-01-00 AND AARD 53-10-00-15. (M)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

TUL - FOUND LEFT AFT END OF VERTICAL STAB JOINT IS CRACKED BETWEEN FASTENERS .5 INCH. INSTALLED SKATE ANGLE REPAIR DOUBLER PER AARD 53-10-00-2. (M)

Part: DUCT — BLOWN (A/C BAY)

EWR - FLT 1927 - ON CLIMB-OUT, EN ROUTE EWR-ORD, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER AIRFOIL ANTI-ICE SWITCHES PLACED ON. LIGHT WENT OUT AFTER COMPLETED PROCEDURE. PRESSURIZATION FLOW LIGHT ALSO CAME ON SEVERAL TIMES. RETURNED AND LANDED EWR WITHOUT INCIDENT. REPLACED RAM AIR EXHAUST DUCT. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, HELD EMERGENCY LIGHT INOPERATIVE. REPLACED HAND HELD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 7D, 11D, 13D, 14D, 17D, 19D, 20D, 21D, 22D, 25D, 26D, 27D, 29D, 30D, 31D DIM. REPLACED EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: COALESCER BAG — DIRTY (ACM BAY)

SFO - FLT 1992 - DURING FLIGHT, THE FLIGHT ATTENDANT REPORTED SMOKE VISIBLE FROM AIR CONDITIONER VENTS. RETURNED AND LANDED SFO WITHOUT INCIDENT. REPLACED COALESCER BAGS AND ACCOMPLISHED PACK BURN-OUT. UNABLE TO DUPLICATE SMOKE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WHEEL — BROKEN (MLG)

BROKEN HUB. UNDER INVESTIGATION.

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT PATH FLOOR LIGHTS OVERWING EXIT TO AFT DOOR INOPERATIVE. REPAIRED WIRING TO EMERGENCY EXIT PATH FLOOR LIGHTS OVERWING EXIT TO AFT DOOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — BROKEN (TAIL CONE)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOD LIGHTS IN TAIL CONE INOPERATIVE. REPAIRED HOT WIRE TO EMERGENCY EXIT FLOOD LIGHT SYSTEM. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SWITCH — FAILED (COCKPIT)

ORD - FLT T1881 - EN ROUTE DTW/ORD, EMERGENCY POWER SWITCH WAS INTERMITTENT. LANDED ORD WITHOUT INCIDENT. REPLACED EMERGENCY POWER SWITCH. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)