N599AA

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,459 hrs · 30,729 cycles

AFT FLIGHT ATTENDANT CEILING EMER LIGHTS WON`T TEST. R & R EMER LIGHT BATTERY PACK B5-27 IAW AMM 33-53-00. SYSTEM CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 70,459 hrs · 30,729 cycles

TAIL CONE EMER LIGHTS WON`T TEST. R & R TAIL CONE EMER LIGHT BATTERY PACK IAW MM 33-53-00. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,459 hrs · 30,729 cycles

FIRST CLASS OVERHEAD EMER LIGHTS WON`T TEST. R & R FIRST CLASS EMER LIGHT BATTERY PACK IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,459 hrs · 30,729 cycles

OVERHEAD EMER LIGHTS AT ROWS 29 - 31 WON`T TEST. R & R EMER BATTERY PACK FOR ROWS 29 - 31 IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,106 hrs · 29,477 cycles

INTERCOSTAL FROM STATIONS 1287 TO 1309 CRACKED. INSTALLED NEW INTERCOSTAL IAW AARD 51-00-05.

Part: CASTING — CRACKED (LE SLAT) · airframe 68,106 hrs · 29,477 cycles

LT HAND WING INBD NR 4 SLAT TRACK CASTING CRACKED. INSTALLED DOUBLER IAW EA MD80-57-033438.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,106 hrs · 29,477 cycles

CORROSION ON BOTTOM SIDE OF CUSP AT LT STATION 712. INSTALL REPAIR DOUBLER IAW AARD 53-20-00-16.

Part: DUCT — DAMAGED (AC BAY) · airframe 68,104 hrs · 29,476 cycles

MSP CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMB OUT. EMERGENCY DECLARED FLIGHT RETURNED MSP LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED 13 STAGE DUCT ON RT HAND AUGMENTATION VLV. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,402 hrs · 27,507 cycles

LEFT NUMBER 1 DOOR PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT ASSEMBLY FOR LEFT NUMBER 1 DOOR. OPS CHECK NORMAL.

Part: ELECTRICAL SYS — FAILED · airframe 62,632 hrs · 26,565 cycles

INFLIGHT, CREW REPORTED AUTO-PILOT AND AUTO-THROTTLES DISCONNECTED WITH NUMERIOUS CAWS WARNINGS AND HORNS GOING OFF. AIRCRAFT WENT DARK AND EMERGENCY POWER WAS SELECTED. AUXILIARY POWER UNIT CAME ONLINE BUT HAD TO DISCONNECT LEFT GENERATOR FOR APU TO PICK UP BUSSES. EMERGENCY DECLARED, FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT GENERATOR, LEFT AND RIGHT A/C POWER RELAYS, AND LEFT AND RIGHT GENERATOR CONTROL UNITS. SYSTEM GROUND CHECKED NORMAL.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 61,740 hrs · 26,129 cycles

DFW - CREW REPORTED IMMEDIATELY AFTER TAKEOFF A STRONG RUBBER ODOR WAS NOTICED IN THE CABIN AND COCKPIT WITH NO SMOKE PRESENT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED PACK BURN AND REPLACED PNEUMATIC COALESCER SEPARATORS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: STRUT — DISCHARGED (ZONE 700) · airframe 60,198 hrs · 25,339 cycles

CREW REPORTED NOSE LANDING GEAR UNSAFE INDICATION. INDICATOR IN PEDESTAL WENT DOWN ON RETRACTION BUT DOORS DID NOT APPEAR TO CLOSE AS REPORTED BY CREW. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT ICIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NOSE GEAR STRUT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: STRUT — DISCHARGED (ZONE 700) · airframe 60,196 hrs · 25,336 cycles

CREW REPORTED NOSE GEAR WOULD NOT RETRACT AND NOSE GEAR UNSAFE INDICATION. EMERGENCY DECLARED FLIGHT RETURNED TUS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED REPACK OF NOSE LANDING GEAR STRUT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 60,000 hrs · 25,238 cycles

REPAIR DOUBLER ON AFT SIDE OF LEFT AFT OVERWING EMERGENCY EXIT DOOR JAMB IS CRACKED. REMOVED AND REPLACED REPAIR DOUBLER PER EA MD80-53-016005.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 60,000 hrs · 25,238 cycles

CARGO AFT STATIONS 1212 TO 1271 - RIGHT SIDE TIE-DOWN TRACK HAS CORROSION AT ATTACH FASTENERS. INSTALLED AFT RIGHT TRACK IN AFT CARGO PER AARD 51-10-00-5.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 60,000 hrs · 25,238 cycles

DOUBLE DRILLED CLIPNUT HOLES IN FLOORBOARD SUPPORT STATIONS 1193 TO 1212 ABOVE LONGERON 29 RIGHT. INSTALLED NEW FLOORBOARD SUPPORT PER SRM 51-30-01.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,000 hrs · 25,238 cycles

FUSELAGE LEFT SIDE, AFT LAVATORY SERVICE PAN HAS CORROSION ALONG BOTTOM SIDE OF PAN. REPLACED LAV PAN PER SRM 51-30-02, 51-30-05, 53-01-00, 53-14-03, AARD 53-00-00-05, AND EA MD80-53-015843.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,000 hrs · 25,238 cycles

AFT ACCS 1510 CANT FRAME CRACKED BELOW MAINTENANCE LIGHT SWITCH. REPAIRED 1510 CANT FRAME PER EA MD80-53-015821.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 60,000 hrs · 25,238 cycles

CARGO/MID - AFT DOOR FRAME WEB CRACKED UNDER RIGHT TIE-DOWN AT STATION 695. REPAIRED CRACKED DOOR FRAME WEB PER EA MD80-53-015844.

Part: SKIN — DENTED (FUSELAGE) · airframe 60,000 hrs · 25,238 cycles

FUSELAGE DENT WITH A SCRATCH IN SKIN AT STATION 1287 BETWEEN LONGERONS 27 AND 28 RIGHT. INSTALLED DOUBLER PER SRM 53-04-00 FIGURE 30 VIEW P.

Part: SHEAR TIE — DAMAGED (HORIZ STAB) · airframe 60,000 hrs · 25,238 cycles

LEFT HORIZONTAL STAB OUTBOARD SHEAR TIE CRACKED STATION XHS 50 INTERNAL AFT TOP SHEAR TIE BY AFT SPAR. INSTALLED CLIP PER AARD 51-10-00-5.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 60,000 hrs · 25,238 cycles

CUSP CRACKED AT STATION 218 RIGHT. INSTALLED CUSP SECTION FROM STATIONS 218 237 RIGHT PER AARD 51-10-00-5.

Part: SHEAR TIE — DAMAGED (HORIZ STAB) · airframe 60,000 hrs · 25,238 cycles

LEFT HORIZONTAL STAB SHEAR TIE CRACKED STATION XHS 50 INTERNAL AFT TOP SHEAR TIE BY AFT SPAR. ACCOMPLISHED REPAIR PER AARD 51-10-00-5.

Part: SKIN — DENTED (FUSELAGE) · airframe 60,000 hrs · 25,238 cycles

FUSELAGE FORWARD-DENT WITH GOUGE TOP OF FORWARD FUSELAGE STATION 198 JUST ABOVE LONGERON 5 LEFT. INSTALLED DOUBLER PER SRM 53-04-00 FIGURE 38 SHEET 30 VIEW P.

Part: TEE FITTING — DAMAGED (FUSELAGE) · airframe 60,000 hrs · 25,238 cycles

HEAVY CARGO/AFT - CORROSION ON DOOR JAMB LOWER FORWARD FITTING STATION 1155. REMOVED DAMAGED T-CLIP AND INSTALLED NEW T-CLIP PER AARD 51-10-00-5, SRM 51-30-05, BOEING DRAWING 9936073, 5930483.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 60,000 hrs · 25,238 cycles

LEFT FUSELAGE STATION 313 HAS 3 INCH BY .03 INCH SMOOTH DENT BETWEEN LONGERON 22 LEFT AND 23 LEFT. INSTALLED INTERNAL DOUBLER PER SRM 53-04-01 AND SG 09530001 REPAIR E-1 SECTION 12 CARD 51-92-02.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 60,000 hrs · 25,238 cycles

G-1 GALLEY FORWARD CENTER MOUNT HAS CORROSION. INSTALLED NEW GALLEY MOUNT PER AARD 51-10-00-5.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · airframe 60,000 hrs · 25,238 cycles

G-1 GALLEY FORWARD OUTBOARD MOUNT HAS CORROSION. REMOVED AND REPLACED GALLEY MOUNT FITTING PER AARD 51-00-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,000 hrs · 25,238 cycles

LEFT CUSP CORROSION IS BEYOND LIMITS STATIONS 491 TO 493. CUT OUT DAMAGED AREA, VERIFIED MATERIAL, FABRICATED DOUBLER AND INSTALLED PER AARD 53-20-00-16.

Part: PAN — CRACKED (WINDOW) · airframe 60,000 hrs · 25,238 cycles

WINDOW PAN UPPER FORWARD TAB CRACKED AT LEFT STATION 886. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 60,000 hrs · 25,238 cycles

WINDOW PAN LOWER AFT TAB CRACKED AT LEFT STATION 905. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 60,000 hrs · 25,238 cycles

WINDOW PAN UPPER AFT TAB CRACKED AT LEFT STATION 1022. INSTALLED REPAIR DOUBLER REF AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 60,000 hrs · 25,238 cycles

WINDOW PAN UPPER AFT TAB CRACKED AT LEFT STATION 1060. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 60,000 hrs · 25,238 cycles

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

Part: PAN — CRACKED (FUSELAGE) · airframe 60,000 hrs · 25,238 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,711 hrs · 25,096 cycles

DURING FUNCTIONAL TEST OF EMERGENCY ESCAPE PATH LIGHTING FOUND BATTERY PACK AB5-2 HAVING A LOW RESIDUAL CHARGE. REMOVED AND REPLACED BATTERY PACK AB5-2. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,711 hrs · 25,096 cycles

LEFT AND RIGHT FORWARD OVERWING DOOR EMERGENCY EXIT SIGNS NOT ILLUMINATING. REMOVED AND REPLACED BATTERY PACK AT B5-27. OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,711 hrs · 25,096 cycles

LEFT AND RIGHT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT B5-29. OPS CHECKS NORMAL.

Part: SOCKET — DAMAGED (CATWALK) · airframe 58,256 hrs · 24,398 cycles

LIGHT OVER CATWALK IN TAIL HAS WHITE WIRED PULLED. REPLACED SOCKET ON WIRE TO EMERGENCY LIGHT IN CATWALK OVERHEAD. OPS CHECKED NORMAL.

Part: LENS — BROKEN (CABIN) · airframe 57,636 hrs · 24,085 cycles

EMERGENCY LIGHT AT SEAT 10A HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 10A. OPS CHECKED NORMAL.

Part: PRESSURE SWITCH — FAILED (LT ENGINE) · airframe 57,570 hrs · 24,059 cycles

DFW - CREW REPORTED LEFT ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED DURING CLIMB AND OIL TEMPERATURE STARTED TO RISE. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED DIFFERENTIAL PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACM — LEAKING (AC BAY) · airframe 55,913 hrs · 23,349 cycles

INFLIGHT SAN TO STL. DURING CLIMB TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. LANDED LAX WITHOUT INCIDENT. FOUND RIGHT PACK AIR CYCLE MACHINE HAS A ONE INCH DIAMETER HOLE AT THE FORWARD SIDE. TEMPERATURE TABS DID NOT INDICATE AN OVER TEMPERATURE HAD OCCURRED. REPLACED RIGHT AIR CYCLE MACHINE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,809 hrs

LGA CEILING EMERGENCY LIGHTS FROM ROW 13 TO ROW 17 INOPERATIVE. REPLACED BATTERY PACK AT SEAT 14D.

Part: WIRE — BROKEN (CABIN) · airframe 54,809 hrs

LGA TAIL COMPARTMENT EMERGENCY LIGHT INOPERATIVE. REPAIRED BROKEN WIRE ON EMERGENCY LIGHT IN CATWALK.

Part: SLIDE — INOPERATIVE (TAILCONE)

JFK - TAIL CONE DROPPED BUT SLIDE DID NOT UNRAVEL OR INFLATE. RE-INSTALLED TAIL CONE AND REPLACED AFT SLIDE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: DOOR LATCH — DIRTY (NLG) · airframe 53,928 hrs · 22,467 cycles

PSP INFLIGHT - AT GEAR RETRACTION CREW REPORTED LOUD BUFFETING NOISE FROM NOSE GEAR AREA. RETURNED TO PSP AND LANDED WITHOUT INCIDENT. FOUND RIGHT NOSE LANDING GEAR DOOR OPEN. CHECKED AND CLEANED NOSE GEAR DOOR LATCH AND LINKAGE. VERIFIED NOSE LANDING GEAR DOOR LOCKED. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACCELEROMETER — FAILED (AUTOPILOT) · airframe 53,764 hrs

ORD INFLIGHT - AFTER TAKEOFF CREW REPORTED AUTO THROTTLE AND AUTO PILOT WERE INOPERATIVE. CAPTAIN ELECTED TO RETURN TO ORD. LANDED ORD WITHOUT INCIDENT. REPLACED BOTH ACCELEROMETERS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TRANSDUCER — INOPERATIVE (ANTI SKID SYS)

COS INFLIGHT T1009/20OCT - EXTENDED LANDING GEAR ON FINAL. ATTEMPTED TO ARM AUTO BRAKES NUMBER TWO. ANTI-SKID LIGHT ILLUMINATED ON LEFT OUTBOARD AND RIGHT INBOARD. ALSO, LANDING WHEEL NOT TURNING INDICATION. LANDED COS WITHOUT INCIDENT. BOTH LEFT OUTBOARD AND RIGHT INBOARD TRANSDUCERS BAD. REPLACED ANTI-SKID CONTROL BOX. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT)

SFO EMERGENCY LIGHTS AT SEAT ROWS 27 TO 30 INOPERATIVE. CLEANED CONTACTS FOR EMERGENCY LIGHTS AT SEAT ROWS 27 TO 30. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: PIN — INOPERATIVE (TAIL CONE)

STL - TAIL CONE JETTISON SYSTEM INSPECTION AND OPERATIONAL CHECK FAILED FIRST DROP FROM AFT PASSENGER DOOR. ADJUSTED AND LUBRICATED PUSH PIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - CEILING EMERGENCY LIGHTS AT FORWARD LAVATORY L1, AFT RIGHT HAND LAVATORY AND AFT OF ROW 28 INOPERATIVE. REPLACED BATTERY PACKS FOR CEILING EMERGENCY LIGHTS AT FORWARD LAVATORY L1, AFT RIGHT HAND LAVATORY AND AFT OF ROW 28. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SWITCH — INOPERATIVE (RIGHT & LEFT)

DFW - PRESSURIZATION LOSS AT CRUISE (34,000). BOTH PACKS WENT TO ZERO FLOW. STARTED DESCENT PERFORMED PROCEDURES BUT NO HELP. DROPPED 02 MASKS IN BACK. PACKS BEGAN TO WORK AGAIN BETWEEN 8000 AND 6000 FEET. FLOW ON METERS BEFORE CABIN PRESSURIZED DOWN TO AROUND 4000 THEN THE LEFT FLOW BEGAN TO BACK OFF TO MATCH ON THE RIGHT SIDE. REPLACED BOTH RIGHT AND LEFT ENGINE SINGLE ENGINE CLIMB SWITCH. PERFORMED SPECIAL ITEM CARD 4354. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MECHANISM — LACK OF LUBE (TAILCONE RELEASE)

LAX TAIL CONE FAILED TO DEPLOY WHILE ACCOMPLISHING SPECIAL ITEMS CARD 5918, TAIL CONE JETTISON SYSTEM INSPECTION AND OPERATIONS CHECK. LUBED RELEASE MECHANISM. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

ORD FIRST CLASS CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5 FOR FIRST CLASS CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PLATE — CORRODED (FUSELAGE)

FOUND CORROSION AND PITTING ON 8 HINGE LUG PLATES FOR HORIZONTAL STABILIZER PIVOT, STATION YV170. INSTALLED NEW HINGE PLATES FOR HORIZONTAL STABILIZER PIVOT PER KF0488. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FOUND CORROSION ON SEAT TRACK BETWEEN STATION 1207 AND 1299. INSTALLED NEW SEAT TRACK PER SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK NR 2 FROM STATION 1203 TO 1300. INSTALLED NEW SEAT TRACK NR 2, STATION 1184-1307 AND INSTALLED NEW SPLICE PER SRM 53-05 PART 1. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP AT STATION 1174. INSTALLED CUSP DOUBLER STATION 1174 PER AARD 53-00-00-02. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON RIGHT CUSP AT STATION 468. INSTALLED DOUBLER PER SRM 53-01-00. (M)

Part: SMOKE — DETECTED (CABIN)

SAN - FLT 460 - EN ROUTE SAN-ORD, SMOKE AND SMELL OF SMOKE IN CABIN BY SEAT 15B. SMOKE AND SMELL DISSIPATED, BUT SMELL CAME BACK. RETURNED SAN AND LANDED WITHOUT INCIDENT. PERFORMED CABIN ODOR TROUBLESHOOTING CARD AND PACK BURN OUT. SYSTEM GROUND CHECKED NORMAL OPERATION. AIRCRAFT SCHEDULED FOR FUNCTIONAL CHECK FLIGHT. FUNCTIONAL CHECK FLIGHT ACCOMPLISHED WITH NO SMOKE OBSERVED. (M)

Part: DUCT — DEFECTIVE (A/C BAY)

SAN - FLT 512 - EN ROUTE SAN-ORD, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMB-OUT. AFTER EMERGENCY PROCEDURES WERE COMPLETE LIGHT CAME BACK ON WITH INCREASE IN POWER. POWER WAS REDUCED AND THE LIGHT STAYED OUT FOR REMAINDER OF FLIGHT. RETURNED SAN AND LANDED WITHOUT INCIDENT. REPLACED GASKET ON THERMOSTAT LEFT SIDE IN TAIL COMPARTMENT. REPLACED TUBE ON AIR CONDITIONING DUCT ON RIGHT SIDE IN TAIL COMPARTMENT. REPLACED SEALS ON RIGHT SIDE SLIP JOINT NEAR COOLING TURBINE IN TAIL COMPARTMENT. LEAK CHECKS GOOD. NO TAIL COMPARTMENT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT SIDE OF FORWARD GALLEY INOPERATIVE. RECONNECTED CONNECTOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE LIGHT AT SEAT 6E INOPERATIVE. REPLACED EMEGENCY EXIT ESCAPE PATH LIGHT AT SEAT 6E. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — SHORTED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE FLOOR PATH LIGHTS FROM FORWARD OF FIRST CLASS TO ROW 20 INOPERATIVE. REPAIRED SHORTED WIRES AT SEAT DEF. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS CABIN WERE INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT ASSY — BROKEN (VENTRAL STAIRS)

RDU - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT VENTRAL STAIR FLOOD LIGHT WAS FOUND BROKEN. REPLACED EMERGENCY EXIT VENTRAL STAIR FLOOD LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: EEL CONNECTOR — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 30D AND 31D AND PASSENGER SEAT ROWS 22D AND 23D FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTORS BY PASSENGER SEATS 30D AND 22D. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: EEL STRIP — DEFECTIVE (CABIN)

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