N576AA

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 66,220 hrs · 34,417 cycles

LEFT ENG LOW OIL PRESS LIGHT ILLUMINATED & LOW OIL PRESS GAUGE AT ZERO. LT ENG WAS SHUTDOWN, SINGLE ENG TIME 15 MINUTES. EMER DECLARED FLIGHT RETURNED, LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LT ENG. SYS GND CHECKED NORMAL OPERATION OPEN.

Part: ENGINE — FAILED (RIGHT) · airframe 65,887 hrs · 34,232 cycles

AIRCRAFT SHOOK & RT ENG LOST OIL PRESS. RT ENG WAS SHUTDOWN, SINGLE ENG TIME 15 MINUTES. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT ENG ON 07/21/2014. SYS GND CHECKED NORMAL OPERATION OPEN.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,117 hrs · 33,767 cycles

FUSELAGE FWD SKIN CRACKED AT AFT HINGE CUT OUT FOR LT AFT NLG DOOR. INSTALLED DOUBLER IAW SRM 53-05-00-001 FIGURE 62.

Part: VALVE — OPEN (FUEL SYSTEM) · airframe 65,117 hrs · 33,767 cycles

DFW CREW REPORTED ON CLIMB OUT FUEL TANK IMBALANCE APPROACHING LIMITS. ALL PUMPS & CROSS FEED VLVS OPERATED NORMALLY. SUSPECTED FUEL TRANSFER PROBLEM. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. UPON ARRIVAL FOUND LT & RT FUELING VLVS IN OPEN POSITION. REFUELED ACFT & VERIFIED FUEL LEVEL USING MEASURING STICKS. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: RIB — CRACKED (NR 4 SLAT) · airframe 65,076 hrs · 33,737 cycles

LEFT NR 4 SLAT RIB CRACKED. INSTALLED RIB DOUBLER REPAIR IAW EA MD80-57-034150.

Part: RIB — CRACKED (NR 4 SLAT) · airframe 65,076 hrs · 33,737 cycles

RIGHT NR 4 SLAT RIB CRACKED. INSTALLED RIB REPAIR DOUBLE IAW EA MD80-57-034150.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,714 hrs · 33,546 cycles

AFT OVERWING EMERGENCY EXIT LIGHTS FAILED TO TEST. REPLACED BATTERY PACK FOR AFT OVERWING EMERGENCY EXIT LIGHTS, OPERATIONS CHECKED NORMAL.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 64,714 hrs · 33,546 cycles

LT NR 1 DOOR PORTABLE EMERGENCY LIGHT FAILED TO TEST. REPLACED LIGHT ASSEMBLY, OPERATIONS CHECKED NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 64,579 hrs · 33,462 cycles

LIGHTNING STRIKE DAMAGE AT STATION 447.75 & LONGERON 22 RT. INSTALLED DOUBLER IAW SRM 53-04-02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 64,579 hrs · 33,462 cycles

LIGHTNING STRIKE DAMAGE AT STATION 331 APPROXIMATELY 2 INCHES ABOVE STRINGER 22 RT. INSTALLED DOUBLER IAW SRM 53-04-02 FIGURE 2.

Part: OVEN — MALFUNCTIONED (GALLEY) · airframe 62,117 hrs · 32,085 cycles

STL - INFLIGHT DFW-CMH. CREW REPORTED SMOKE IN CABIN COMING FROM FORWARD GALLEY OVEN. EMERGENCY DECLARED FLIGHT DIVERTED STL LANDED WITHOUT INCIDENT. DEFERRED FORWARD GALLEY OVEN PER NEF. FLIGHT CONTINUED TO DESTINATION. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY — NOT SEATED (CABIN) · airframe 61,889 hrs · 31,951 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30. RESEATED BATTERIES. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 61,889 hrs · 31,951 cycles

RIGHT CENTER CEILING EMERGENCY LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. RESEATED BATTERIES. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 61,889 hrs · 31,951 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERIES. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 61,889 hrs · 31,951 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,889 hrs · 31,951 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. RESEATED BATTERY PACK IN ROW 29.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 61,889 hrs · 31,951 cycles

RIGHT AND CENTER CEILING EMERGENCY LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. RESEATED BATTERY PACK I RIGHT AFT LAVATORY. OPS CHECK NORMAL.

Part: SHUTOFF VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 60,848 hrs · 31,329 cycles

PIT - CREW REPORTED LOSS OF PRESSURIZATION CONTROL. EMERGENCY DECLARED FLIGHT LANDED PIT WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED PRESSURE REGULATING AND SHUT-OFF VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 59,959 hrs · 30,815 cycles

LIGHTNING/STATIC DISCHARGE AT FRAME STATION 144 AND LONGERON 14 RIGHT. TRIMMED OUT DAMAGE AND INSTALLED EXTERNAL DOUBLER PER EA MD80-53-023130.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,644 hrs · 29,494 cycles

DENTS IN SKIN FROM DOUBLER INSTALL, STATION 1250, STRINGER 1. INSTALLED DOUBLER, TRIPLER, FILLER AND FINGER DOUBLERS PER EA MD80-53-017444 DATED 6-10-11.

Part: BEAM — CORRODED (FUSELAGE) · airframe 57,644 hrs · 29,494 cycles

AFT CARGO DOOR BEAM HAS CORROSION ON WEB STATIONS 1155 TO 1212. REPLACED WEB PER AARD 51-10-00-5.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,644 hrs · 29,494 cycles

STATION 1322 INTERCOSTAL CRACKED UNDER RIGHT TIE DOWN TRACK. INSTALLED NEW INTERCOSTAL PER AARD 51-10-00-5.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,644 hrs · 29,494 cycles

AFT ACCESSORY 1485 CANT FRAME CRACKED AT STAIR ACTUATOR. ACCOMPLISHED INSTALLATION OF DOUBLER PER AARD 53-10-00-33.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,644 hrs · 29,494 cycles

STATION 1474 CANT FRAME CRACKED AFT OF LONGERON 17 LEFT. TRIMMED OUT CRACK AND INSTALLED DOUBLER REPAIR PER EA MD80-53-017388.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,644 hrs · 29,494 cycles

SEAT TRACK NUMBER 4 LUG AT G-2 GALLEY TIE DOWN AREA STATION 235 CORRODED. INSTALLED NUMBER 4 SEAT TRACK SPLICE AND NEW SECTION OF TRACK FROM STATIONS 200 TO 265 PER SRM 53-05-00 FIGURE 4F.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,644 hrs · 29,494 cycles

STATION 1418 FRAME CRACKED LONGERON 2 RIGHT. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-03-00 FIGURE 31A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,644 hrs · 29,494 cycles

STATION 1418 FRAME CRACKED LONGERON 2 LEFT. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-02-00 FIGURE 31A.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,644 hrs · 29,494 cycles

CORROSION ON LEFT TIEDOWN TRACK SPLICE STATION 1220. INSTALLED SPLICE ASSEMBLY PER AARD 51-10-00-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,644 hrs · 29,494 cycles

CORROSION BLENDED OUT OF LIMITS ON SEAT TRACK NUMBER 5 STATIONS 200 TO 218. INSTALLED NUMBER 5 SEAT TRACK AT STATIONS 200 TO 245 RIGHT PER SRM 51-10-01 FIGURE 26 SHEET 2.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,644 hrs · 29,494 cycles

SHEAR TIE CLIP CRACKED AT STATION 1437 BETWEEN LONGERONS 2 AND 3 RIGHT. REMOVED AND REPLACED SHEAR TIE CLIP AT STATION 1437 BETWEEN LONGERONS 2 AND 3 RIGHT PER AARD 51-10-00-5.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,644 hrs · 29,494 cycles

CRACK ON CUSP INBOARD CORNER AT STATION 218 UNDER SEAT TRACK NUMBER 5. INSTALLED DOUBLER ON CUSP CORNER AT STATION 218 RIGHT INBOARD SIDE OF NUMBER 5 SEAT TRACK PER AARD 53-20-00-16.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 57,644 hrs · 29,494 cycles

CABIN RIGHT SIDE, STATION 927, BELOW NUMBER 5 SEAT TRACK, LOWER LEG OF VERTICAL STIFFENER FROM FLOORBEAM TO TOP OF TANK IS CRACKED. INSTALLED DOUBLER AND FILLER ALL PER EA MD80-53-017224.

Part: FITTING — WORN (LE SLAT) · airframe 57,644 hrs · 29,494 cycles

RIGHT NUMBER 5 SLAT INBOARD KNUCKLE FITTING WORN. REPLACED WORN KNUCKLE FITTING BUSHING AND PIVOT PIN AT RIGHT SLAT PER ESO 80117.

Part: BRACKET — GOUGED (FUSELAGE) · airframe 57,644 hrs · 29,494 cycles

T-BRACKET GOUGED STATION 1155 LONGERON 29 RIGHT. REMOVED AND REPLACED T-BRACKET STATION 1155 LONGERON 29 RIGHT PER AARD 51-10-00-5, BOEING DRAWING NUMBER 9936073, SRM 51-30-05.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,644 hrs · 29,494 cycles

CORROSION ON SHEAR TIE STATION 1155 BETWEEN LONGERONS 30 AND 29 RIGHT. REMOVED AND REPLACED SHEAR TIE STATION 1155 LONGERONS 30 TO 29 RIGHT PER AARD 51-10-00-5, BOEING DRAWING NUMBER 9936073 AND SRM 51-30-05.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 57,644 hrs · 29,494 cycles

FUSELAGE FORWARD SCRATCHES IN SKIN STATION 200, BETWEEN LONGERONS 4 AND 5 LEFT. INSTALLED INTERNAL DOUBLER PER BOEING DRAWING SG09530001.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 57,644 hrs · 29,494 cycles

FUSELAGE FORWARD SCRATCHES IN SKIN STATION 207 BETWEEN LONGERONS 4 AND 5 LEFT. INSTALLED INTERNAL DOUBLER PER BOEING DRAWING SG09530001.

Part: RIB — CRACKED (LE SLAT) · airframe 57,644 hrs · 29,494 cycles

LEFT NUMBER 5 SLAT NUMBER 14 RIB CRACK INDICATION. REPLACED NUMBER 14 RIB WITH NEW ONE IAW ES0 27-80-1.

Part: RIB — CRACKED (LE SLAT) · airframe 57,644 hrs · 29,494 cycles

RIGHT NUMBER 5 SLAT NUMBER 14 RIB CRACKED INDICATION. REPLACED RIB RIGHT NUMBER 14 POSITION PER ESO 80117 27-80-1.

Part: PAN — CRACKED (WINDOW) · airframe 57,644 hrs · 29,494 cycles

WINDOW RING PAN CRACKED RIGHT SIDE, LOWER FORWARD CORNER AT STATION 984. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,644 hrs · 29,494 cycles

WINDOW RING PAN CRACKED RIGHT SIDE, UPPER FORWARD CORNER AT STATION 927. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,644 hrs · 29,494 cycles

WINDOW RING PAN CRACKED RIGHT SIDE, LOWER AFT SIDE OF STATION 845. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,644 hrs · 29,494 cycles

WINDOW RING PAN CRACKED LEFT SIDE, LOWER FORWARD CORNER AT STATION 984. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,644 hrs · 29,494 cycles

WINDOW RING PAN CRACKED RIGHT SIDE, UPPER FORWARD CORNER AT STATION 886. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,644 hrs · 29,494 cycles

WINDOW RING PAN CRACKED RIGHT SIDE FORWARD LOWER CORNER AT STATION 1155. TRIMMED OUT CRACKED TAB AND INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,644 hrs · 29,494 cycles

WINDOW RING PAN CRACKED RIGHT SIDE FORWARD LOWER CORNER AT STATION 1211. TRIMMED OUT CRACKED TAB AND INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,644 hrs · 29,494 cycles

WINDOW RING PAN CRACKED LEFT SIDE LOWER AFT CORNER AT STATION 826. CUT OUT CRACKED AREA OF WINDOW RINGPAN. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,644 hrs · 29,494 cycles

WINDOW RING PAN CRACKED LEFT SIDE UPPER AFT CORNER AT STATION 1041. INSTALLED REPAIR ANGLE AS PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,644 hrs · 29,494 cycles

WINDOW RING PAN CRACKED RIGHT SIDE LOWER FORWARD CORNER AT STATION 984. INSTALLED REPAIR ANGLE DOUBLER AT STATION 984 RIGHT LOWER FORWARD CORNER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,644 hrs · 29,494 cycles

WINDOW RING PAN CRACKED LEFT SIDE UPPER FORWARD CORNER AT STATION 788. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,644 hrs · 29,494 cycles

WINDOW RING PAN CRACKED LEFT SIDE LOWER FORWARD CORNER AT STATION 984. INSTALLED REPAIR ANGLE DOUBLER AT STATION 984 LOWER FORWARD CORNER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,644 hrs · 29,494 cycles

WINDOW RING PAN CRACKED LEFT SIDE LOWER FORWARD CORNER AT STATION 1041. INSTALLED REPAIR ANGLE AS PER AARD 53-10-00-25.

Part: SENSOR — INOPERATIVE (NLG) · airframe 57,415 hrs · 29,360 cycles

CREW REPORTED ON APPROACH DURING INITIAL GEAR EXTENSION, NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED. CREW ACCOMPLISHED GO AROUND AND SUBSEQUENT GEAR EXTENSION WAS NORMAL. FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NOSE GEAR LOCKED SENSOR D1-3L. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SENSOR — OUT OF ADJUST (RT MLG) · airframe 55,448 hrs · 28,255 cycles

ELP - CREW REPORTED LANDING GEAR UNSAFE INDICATION ON GEAR EXTENSION. LANDING GEAR LOWERED BY ALTERNATE GEAR EXTENSION. GEAR DOORS DID NOT RETRACT. FLIGHT LANDED ELP WITHOUT INCIDENT. SECURED MAIN LANDING GEAR DOORS FOR FERRY FLIGHT TO TUL FOR FURTHER MAINTENANCE. REPLACED RIGHT MAIN LANDING GEAR DOOR AND ADJUSTED GEAR DOOR LIGHT SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: REGULATOR — FAULTY (CABIN PRESSURE) · airframe 54,947 hrs · 27,986 cycles

DFW - CREW REPORTED ON CLIMB THE CABIN RATE OF PRESSURE CONTINUED TO RISE BEYOND NORMAL. THE FLOW LIGHT CAME ON AND THE OUTFLOW VALVE FULLY CLOSED AND THEN THE CABIN RATE OF CLIMB RETURNED TO NORMAL. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED AIR PRESSURE REGULATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRUT — DAMAGED (CARGO BAY) · airframe 54,780 hrs · 27,895 cycles

RIGHT STATION 1287 AFT CARGO SIDEWALL STRUT HAS DAMAGE. INSTALLED L ANGLE, STRAP, AND FILLER PER EA MD80-53-010051.

Part: SLAT — GOUGED (LT WING) · airframe 54,780 hrs · 27,895 cycles

LEFT NUMBER 1 SLAT HAS A GOUGE ON LOWER SIDE OF SLAT AND HOLE AT TRAILING EDGE. INSTALLED FLUSH REPAIR AT GOUGED AREA 60 INCHES FROM INBOARD END TRAILING EDGE PER AARD 57-50-00-4.

Part: VANE — WORN (TE FLAP) · airframe 54,780 hrs · 27,895 cycles

LEFT WING HAS NUMBER 3 VANE WORN ON LEADING EDGE ABOVE OUTBOARD FLAP INBOARD HINGE. HOT BONDED METAL DOUBLER ON NUMBER 3 VANE TRAILING EDGE OUTBOARD FLAP PER SRM 51-70-02.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,252 hrs · 27,034 cycles

EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED FUNCTIONAL TEST. REPLACED BATTERY PACK IN CABIN.

Part: BATTERY PACK — FAILED (CABIN) · airframe 53,310 hrs · 27,065 cycles

EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED FUNCTIONAL TEST. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - OVERHEAD EMERGENCY LIGHT ON ROW 7 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT ON ROW 7.

Part: PIN — DAMAGED (CABIN) · airframe 51,295 hrs

LGA- FORWARD EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. HARNESS AT SEAT 3E SIDEWALL REPLACED PIN.

Part: PAN — CORRODED (ZONE 100) · airframe 50,661 hrs · 25,647 cycles

AFT LAV SERVICE PANEL PAN HAS CORROSION AT OUTBOARD RADIUS OF PAN STATION 1322. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-30-00-7.

Part: BULB — MISSING (EMERGENCY LIGHTS)

LGA - FOUND EMERGENCY LIGHT AT SEAT 5E HAS BULBS MISSING. REPLACED BULBS FOR EMERGENCY LIGHT AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — BROKEN (EMERGENCY LIGHT)

LGA - FOUND EMERGENCY LIGHT AT SEAT 5E HAS LENS BROKEN. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COMPRESSOR — DAMAGED (LEFT ENGINE)

TUL - ON CLIMB, LEFT ENGINE LOW PRESSURE ROTOR SPEED STARTED TO FLUCTUATE DRAMATICALLY ACCOMPANIED BY LOUD BANGING NOISES. BROUGHT THRUST LEVER BACK TO 1.3 TO 1.2 AND ENGINE STABILIZED. RETURNED TO TUL AND LANDED WITHOUT INCIDENT. NO REMARKABLE EXHAUST GAS TEMPERATURE OR HIGH PRESSURE ROTOR SPEED. FLIGHT DATA RECORDER DOWNLOADED. FOREIGN OBJECT DAMAGE SUSPECTED. REPLACED NUMBER ONE ENGINE ON 03 DEC 2006 AT TUL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS)

LGA - EMERGENCY EXIT LIGHT AT SEAT 19D RED LENS MISSING. REPLACED BEZEL AND RED LENS FOR EMERGENCY EXIT LIGHT AT SEAT 19D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BROKEN (EMERGENCY LIGHTS)

LGA - EMERGENCY EXIT LIGHT AT SEAT 12D HAS BROKEN LENS AND BEZEL. REPLACED LENS AND BULB FOR EMERGENCY EXIT LIGHT AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHT AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (CABIN)

DEN - EMERGENCY CEILING LIGHTS AT ROWS 28 THROUGH 29 INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD BIN 29 FOR ROWS 28 THROUGH 29. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN)

DFW EMERGENCY LIGHTS AT SEATS 20D AND 2D INOPERATIVE. RESECURED CONNECTOR FOR SEATS 20D AND 2D EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN)

DFW EMERGENCY LIGHTS AT SEAT 20D INOPERATIVE. RESECURED LOOSE CONNECTOR FOR EMERGENCY LIGHTS AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT OVERWING EXIT. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT SEAT ROW 2B. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — NOT SEATED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING INOPERATIVE AT THE AFT OVERWING CABIN SECTION. RESEATED BATTERIES IN PACK B5-105. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONTACTOR — DIRTY (CABIN)

DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT ABOVE RIGHT HAND SERVICE DOOR INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT GROUND CONTACT ABOVE RIGHT HAND SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

(LIGHT ASSEMBLY) DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT 7D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (FWD LAVATORY)

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

Part: LIGHT — DEFECTIVE (FWD LAVATORY)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AISLE MARKER AT FORWARD LAVATORY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. (M)

Part: APU — LEAKING (APU BAY)

ABQ - FLT 498 - AFTER TAKEOFF AT 5000 AGL, FLIGHT ATTENDANT IN AFT CABIN REPORTED BLUE SMOKE AND OILY SMELL IN AFT CABIN UP TO MID CABIN AREA. RETURNED AND LANDED ABQ WITHOUT INCIDENT. SOME SMOKE WAS SEEN COMING FROM NR 4 WHEEL AREA AT GATE. REPLACED AUXILLARY POWER UNIT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: MODULE — FAILED (CABIN)

TPA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT LOCATED IN AFT SECTION INOPERATIVE. REPLACED TWO EACH EMERGENCY EXIT FLOOR PATH LIGHT MODULES. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — BROKEN (ROW 14D)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT MOUNTED PATHWAY LIGHTS AT SEAT ROW 14D/E/F INOPERATIVE. REPAIRED WIRING TO EMERGENCY EXIT SEAT MOUNTED PATHWAY LIGHTS AT SEAT ROW 14D/E/F. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)