N585AA

Part: FUEL CONTROL — DEFECTIVE (RT ENGINE) · airframe 66,185 hrs · 34,654 cycles

RIGHT ENG WOULD NOT MAKE TAKEOFF POWER, ABORTED TAKEOFF. R & R RT ENG FUEL CONTROL IAW MCM 73-91-99, MCM 71-91-17 & MCM 71-91-73. PERFORMED ENG RUN & LEAK CHECK. SYS CHECKED NORMAL.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 66,071 hrs · 34,587 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE CABIN ALTITUDE WARNING ALERTED. RT PACK BECAME UNCONTROLLABLE, OPERATED PRESSURIZATION SYS IAW AMM 21-32-00. SYS CHECKED NORMAL.

Part: SLIDE — DAMAGED (ENTRY DOOR) · airframe 65,490 hrs · 34,225 cycles

FORWARD ENTRY DOOR SLIDE DETACHED FROM DOOR & GIRDLE DAMAGED. REPLACED SLIDE IAW AMM 25-62-00.

Part: SUPPORT RIB — CRACKED (LT WING) · airframe 64,982 hrs · 33,931 cycles

LEFT WING NR 4 SLAT TRACK LE INBD SUPPORT RIB CRACKED AT PULLEY BRACKET SUPPORT BOSS. INSTALLED REPAIR DOUBLER IAW PATTERN CARD 57-98-05 & EA MD80-57-035315.

Part: SUPPORT RIB — CRACKED (RT WING) · airframe 64,982 hrs · 33,931 cycles

RIGHT NR 4 WING SLAT TRACK LE INBD SUPPORT RIB CRACKED AT PULLEY BRACKET ATTACH BOSS. INSTALLED REPAIR DOUBLER IAW PATTERN CARD 57-98-06 & EA MD80-57-035315.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 63,577 hrs · 33,115 cycles

PHX INFLIGHT DFW-SAN CREW REPORTED ODOR IN THE COCKPIT THE CAPTAIN & FIRST OFFICERS PRIMARY FLIGHT DISPLAYS SHOWING SIGNS OF OVERHEATING & BLANKING. EMERGENCY DECLARED FLIGHT DIVERTED PHX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CAPTAIN & FIRST OFFICERS PRIMARY FLIGHT DISPLAYS. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: SENSE LINE — DISCONNECTED (AC BAY) · airframe 63,177 hrs · 32,877 cycles

DFW CREW REPORTED ON TAKEOFF, BOTH AIR CONDITIONING SUPPLY TEMPERATURE HIGH LIGHTS ILLUMINATED & STAYED ON UNTIL POWER REDUCTION. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LT & RT HAND AUGMENTATION VALVE SENSING LINE STILL CAPPED. REMOVED CAPS & CONNECTED LINES, SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: CHARGER — MALFUNCTIONED (MAIN BATTERY) · airframe 63,052 hrs · 32,795 cycles

TUL INFLIGHT MA-DFW CREW REPORTED BATTERY CHARGER LIGHT ILLUMINATED AFTER CLIMB-OUT. FLIGHT ATTENDANTS REPORTED A LARGE AMOUNT OF WATER THAT CAME FROM THE OVERHEAD AREA OF AIRCRAFT. FLIGHT DIVERTED TUL LANDED WITHOUT INCIDENT. FOUND CIRCUIT BREAKER L5, X25, Z24 & ENTIRE GROUND SERVICE BUS INOPERATIVE. REPLACED BATTERY CHARGER & RESET CIRCUIT BREAKERS. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: DUCT — CRACKED (AC BAY) · airframe 62,779 hrs · 32,624 cycles

SAT CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. EMERGENCY DECLARED, FLIGHT LANDED SAT WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RT DUCT INSIDE OF TAIL COMPARTMENT THAT WAS CRACKED. SYSTEM GROUND CHECKED NORMAL. OPERATION (CLOSED).

Part: DUCT — BLOWN (AC BAY) · airframe 62,693 hrs · 32,571 cycles

TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMB OUT. REPLACED BLOWN DUCT. SYSTEM GROUND CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,913 hrs · 30,969 cycles

OVERWING EMERGENCY LIGHTS DID NOT COME ON ON TEST MODE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: DUCT — LEAKING (AC BAY) · airframe 59,840 hrs · 30,931 cycles

LAS - CREW REPORTED TAIL COMPARTMENT HIGH LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED LAS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CONNECTOR ASSEMBLY, PERI SEAL AND DUCT 1858 ON LEFT SIDE OF TAIL COMPARTMENT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: WIRE — BROKEN (CABIN) · airframe 59,522 hrs · 30,750 cycles

AFT AIRSTAIRS SIDEWALL LOWER FORWARD EMERGENCY LIGHT HAS BROKEN WIRE BEHIND PANEL. REPAIRED USING SPLICE TO ENABLE ATTACHMENT OF CONNECTOR, OPS CHECK NORMAL.

Part: REGULATOR VALVE — DEFECTIVE (AC BAY) · airframe 59,289 hrs · 30,630 cycles

DFW - CREW REPORTED STRONG BURNING RUBBER SMELL THROUGHOUT CABIN DURING TAKEOFF AND LIGHT SMOKE IN REAR CABIN. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH AIR CONDITIONING PRESSURE REGULATOR VALVES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — DENTED (ENTRY DOOR) · airframe 57,290 hrs · 29,517 cycles

DENT ON LOWER AFT SIDE OF FORWARD ENTRY DOOR. REMOVED DAMAGED AREA OF LOWER SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 52-05-00 FIGURE 37.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 57,290 hrs · 29,517 cycles

LEFT SIDE, SECOND AND THIRD FRAMES AFT OF RADOME BULKHEAD, DENTS FORWARD OF BOTH FRAMES. INSTALLED DOUBLER PER SRM 53-04-00 FIGURE 14.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,290 hrs · 29,517 cycles

STATION 1437 SHEAR TIE CLIP CRACKED IN 2 PLACES BETWEEN LONGERONS 2 AND 3 LEFT. INSTALLED NEW SHEAR TIE CLIP AT STATION 1437 PER SRM 51-30-05 AND 51-30-02.

Part: SKIN — DENTED (ENTRY DOOR) · airframe 57,290 hrs · 29,517 cycles

DENT ON LOWER AFT SIDE OF FORWARD ENTRY DOOR. REPAIR DOUBLER INSTALLED IN SHOP PER SRM 52-05-00 FIGURE 37.

Part: SKIN — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 57,290 hrs · 29,517 cycles

INTERNAL SKIN CORRODED FROM STATION 1157 TO 1210 OUTBOARD OF AFT CARGO DOOR BEAM. BLENDED AND REMOVED CORROSION PER SRM 51-10-03. INSTALLED REPAIR DOUBLER PER EA MD80-53-018316.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 57,290 hrs · 29,517 cycles

ANGLE UNDER SHEAR TIE CLIP AT STATION 1451 AFT OF LONGERON 2 LEFT IS CRACKED. INSTALLED ANGLE AFT SIDE OF STATION 1451 AT LONGERON 2 LEFT PER AARD 51-10-00-5.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,290 hrs · 29,517 cycles

SHEAR TIE CRACKED AFT SIDE OF 1451 AFT OF LONGERON 2 LEFT. INSTALLED NEW SHEAR TIE AFT SIDE OF STATION 1451 AT LONGERON 2 LEFT PER AARD 51-10-00-5.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 57,290 hrs · 29,517 cycles

SHEAR TIE CRACKED AFT SIDE OF 1451 AFT OF LONGERON 2 RIGHT. REMOVED AND REPLACED SHEAR TIE CLIP PER SRM 51-60-00.

Part: MEMBRANE — DAMAGED (FUSELAGE) · airframe 57,290 hrs · 29,517 cycles

CORROSION AT STATION 200 RIGHT SIDE SUBFLOOR UNDER SEAT TRACK NUMBER 5. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,290 hrs · 29,517 cycles

AFT CARGO STATION 1131 CORRODED STRAP LONGERON 28 RIGHT TO LONGERON 30 GOUGED AND BLENDED OUT OF LIMITS. REMOVED AND REPLACED STRAP STATION 1131 PER AARD 51-10-00-5.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,290 hrs · 29,517 cycles

STATION 1212 FRAME TO BEAM TEE CORRODED OUT OF LIMITS. REMOVED AND REPLACED TEE BRACKET STATION 1212 PER AARD 51-10-00-5 AND SRM 51-30-05.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 57,290 hrs · 29,517 cycles

STATION 1155 FRAME TO BEAM TEE CORRODED OUT OF LIMITS. BLENDED AND REMOVED CORROSION PER SRM 51-30-05. REPLACED T-CLIP PER SRM 51-30-05, AARD 51-10-00-5 AND DRAWING NUMBER DDK4361-1.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,290 hrs · 29,517 cycles

FRAME 1250 AFT SIDE LONGERON 29 TO 30 LEFT CORRODED. INSTALLED "J" ANGLE REPAIR AT STATION 1250 PER AARD 53-10-00-14.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,290 hrs · 29,517 cycles

CORROSION ON CUSP, UNDER AND OUTBOARD OF SEAT TRACK NUMBER 6 STATION 220. INSTALLED NEW CUSP SECTION STATIONS 218 TO 237 RIGHT SIDE PER AARD 53-20-00-16 AND SRM 51-01-00.

Part: SKIN — DAMAGED (ENTRY DOOR) · airframe 57,290 hrs · 29,517 cycles

FORWARD ENTRY DOOR LOWER EDGE OF DOOR SKIN BENT AND DAMAGED. REMOVED DAMAGED AREA OF LOWER SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 52-05-00 FIGURE 37.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,290 hrs · 29,517 cycles

DENT IN FUSELAGE STATIONS 495 TO 503 LONGERON S 23 TO 24 LEFT. INSTALLED DOUBLER REPAIR AT STATION 503 LONGERONS 32 TO 24 LEFT PER BOEING DRAWING SG09530002.

Part: MEMBRANE — DAMAGED (FUSELAGE) · airframe 57,290 hrs · 29,517 cycles

FORWARD CABIN, HOLE IN SUBFLOOR, 15 INCHES RIGHT OF CENTER BUTT LINE, STATION 158. ROUTED OUT DAMAGED AND INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: PAN — CRACKED (WINDOW) · airframe 57,290 hrs · 29,517 cycles

WINDOW PAN CRACK LEFT SIDE FORWARD LOWER CORNER STATIONS 946 TO 965. REPAIR DOUBLER INSTALLED PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,290 hrs · 29,517 cycles

WINDOW PAN CRACKED UPPER AFT CORNER LEFT SIDE STATION 1003 TO 1022. REPAIR DOUBLER INSTALLED PER AARD 53-10-00-25.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 57,290 hrs · 29,517 cycles

WINDOW PANE CRACKED UPPER LEFT SIDE, STATIONS 946 TO 965. REPAIR DOUBLER INSTALLED PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,290 hrs · 29,517 cycles

WINDOW PAN CRACKED UPPER AFT CORNER RIGHT SIDE STATION 1003 TO 1022. REPAIR DOUBLER INSTALLED PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,290 hrs · 29,517 cycles

WINDOW RING CRACKED AT UPPER AFT CORNER, LEFT STATIONS 1041 TO 1060. REPAIRED PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,290 hrs · 29,517 cycles

WINDOW RINGPAN CRACKED AT FORWARD LOWER CORNER AT STATIONS 984 TO 1003. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,290 hrs · 29,517 cycles

WINDOW RING CRACKED AT LOWER AFT UPPER CORNER LEFT STATIONS 1060 TO 1079. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 53,932 hrs · 27,676 cycles

CORROSION ON BOTTOM OF SUB-FLOOR AT FORWARD SERVICE DOOR. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: PAN — CORRODED (FUSELAGE) · airframe 53,932 hrs · 27,676 cycles

CORROSION OUT OF LIMITS UNDER FORWARD SERVICE DOOR PAN BETWEEN STATIONS 191 TO 200. INSTALLED DOUBLER PER EA MD80-53010341.

Part: PAN — DAMAGED (FUSELAGE) · airframe 53,932 hrs · 27,676 cycles

CUT FORWARD SERVICE DOOR PAN RIGHT STATION 184. INSTALLED REPAIR DOUBLER PER SRM 51-30-05.

Part: BRACKET — CORRODED (LT MLG WW) · airframe 53,932 hrs · 27,676 cycles

LEFT WHEEL WELL ANGLE BRACKET CORRODED ABOVE BRAKE ACCUMULATOR. REMOVED AND REPLACED BRACKET PER SRM 51-30-00.

Part: ANTI-ICE VALVE — INOPERATIVE (WING) · airframe 53,465 hrs · 27,423 cycles

DFW - CREW REPORTED AIRFOIL ANTI-ICE HIGH TEMPERATURE LIGHTS FOR BOTH WINGS ILLUMINATED ON CLIMBOUT. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED TAIL ICE PROTECTION VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LENS — MISSING (CABIN) · airframe 52,387 hrs · 26,825 cycles

EMERGENCY PATH LIGHT AT SEAT 20D MISSING LENS. REPLACED LENS AT SEAT 20D.

Part: LAMP — MISSING (CABIN) · airframe 52,387 hrs · 26,825 cycles

EMERGENCY PATH LIGHT AT SEAT 20D LAMP MISSING. REPLACED MISSING LAMP AT 20D.

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 51,304 hrs · 26,225 cycles

IN FLIGHT RIGHT HYDRAULIC FLUID DECREASED TO ZERO. LANDED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RUDDER CONTROL VALVE LEAKING. REMOVED AND REPLACED HYDRAULIC LINE ON RUDDER CONTROL VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,468 hrs

LGA - EMERGENCY LIGHT AT OVERHEAD CATWALK INOPERATIVE. REPLACED LAMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 50,468 hrs

LGA - EMERGENCY LIGHT AT SEAT 7D MISSING LENS. REPLACED LENS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 50,047 hrs · 25,507 cycles

SUB FLOOR HAS 1 INCH AREA OF CORROSION AT G1 GALLEY STATION 154 TO 160. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER ESO 80559 DATED 10-13-2008 AND AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 50,047 hrs · 25,507 cycles

2 EACH CRACKS IN LEFT HAND CUSP BETWEEN STATION 229 AND 237. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: BATTERY PACK — NOT SEATED (CABIN) · 49,767 cycles

LGA EXTERIOR EMERGENCY LIGHTS AT AFT OVERWING DOOR INOPERATIVE. RESEATED BATTERY PACK FOR EXTERIOR EMERGENCY LIGHTS AT AFT OVERWING DOOR. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — NOT SEATED (CABIN) · 49,767 cycles

LGA EMERGENCY LIGHTS AT CAT WALK INOPERATIVE. RESEATED BATTERY PACK FOR EMERGENCY LIGHTS AT CAT WALK. SYSTEM GROUND CHECKED NORMAL OPS.

Part: TUBE — CRACKED (NR 1 ENGINE) · airframe 49,255 hrs

MCI INFLIGHT T358/27JUN PHX TO ORD. CREW REPORTED LOSS OF OIL AND PRESSURE ON NR ONE ENGINE. CREW SHUT DOWN ENGINE. LANDED MCI WITHOUT INCIDENT. SINGLE ENGINE TIME APPROXIMATELY 20 MINUTES. FOUND CRACK IN OIL LOW PRESSURE SWITCH TUBE. REPLACED TUBE FOR OIL PRESSURE SWITCH ON NR ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: A/C PACK — DIRTY

ORD INFLIGHT T730/28MAY - RETURNED TO ORD DUE TO SMOKE AND FUMES FROM AN UNKNOWN SOURCE. SMELLED OF BURNING RUBBER. LANDED ORD WITHOUT INCIDENT. AIRCRAFT OUT OF SERVICE FOR EVALUATION. ACCOMPLISHED PACK BURN OUT PER WORKCARD 21 92 12. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — MISSING (CABIN)

LGA - EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 28 IS MISSING. REPLACED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 28. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS AT FORWARD SEATS INOPERATIVE. REPLACED BATTERY PACK ABOVE FIRST CLASS LAVATORY FOR EMERGENCY LIGHTS AT FORWARD SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CLAMP — BROKEN (APU)

DFW - ON CLIMBOUT NOTICED HOT SMELL. FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. LEFT HAND PACK WAS IN MANUAL PER MEL. TURNED OFF LEFT HAND PACK AND REQUESTED RETURN TO DFW. NEVER GOT OVER 13K FEET. DID AIRCRAFT SMOKE IN CABIN CHECK LIST PULLED CIRCUIT BREAKER FOR RECIRCULATION FAN. FLIGHT ATTENDANT REPORTED SMOKE WAS GETTING BETTER/IMPROVING. TAXIED TO GATE NO SMOKE AT ANYTIME IN COCKPIT. APU WAS NOT RUNNING. REPLACED LEFT TEMPERATURE CONTROL VALVE AND BROKEN CLAMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: SOCKET — DEFECTIVE (EMERGENCY LIGHT)

TPA - EMERGENCY EXIT LIGHT AT SEAT 11D INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT SOCKET AT SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

AFT LEFT SERVICE DOOR INTERIOR EMERGENCY EXIT SIGN LIGHT FORWARD OF THE DOOR IS INOPERATIVE. REPLACED BATTERY PACK AB5 4 IN LEFT GALLEY CEILING NEAR LEFT SERVICE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, DISCOVERED EMERGENCY EXIT CEILING LIGHTS FROM ROW 7 TO 10 INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK AY STA50. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND RIGHT CUSP HAS CRACKS TWO PLACES STATION 1309 BETWEEN LIGHTENING HOLES APPROX 2.5 INCHES AND AT LIGHTENING HOLES STATION 1291-1297 APPROX 3.5 INCHES. REPLACED CUSP PANEL FROM STATION 1250 TO 1310 RIGHT AARD 53-00-00-07 AND SRM 53-05-00 FIG 97. (M)

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT)

DFW - FLT 1806 - DFW-JFK, ON CLIMB-OUT FROM DFW, TAIL COMP TEMP HIGH LIGHT ILLUMINATED. LIGHT EXTINGUISHED AFTER 1.5 MINUTES. AIRCRAFT LANDED ORD WITHOUT INCIDENT. GROUND RAN A/C AT HIGH POWER SEVERAL TIMES FOR SEVERAL MINUTES. NO DEFECTS AND NO LEAKS NOTED. REMOVED AND REPLACED LEFT AND RIGHT TAIL COMPARTMENT OVERHEAT SWITCH AS A PRECAUTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH — DEFECTIVE (A/C BAY)

EWR - FLT 353 - EN ROUTE LGA-ORD, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT AND MASTER WARNING LIGHT ILLUMINATED ON CLIMB-OUT FROM LGA. ACCOMPLISHED RED BOX ITEMS, WAITED TWO MINUTES, LIGHT DID NOT GO OUT. DECLARED EMERGENCY AND LANDED AT EWR. LIGHT WENT OUT AS POWER WAS REDUCED DURING DESCENT. LANDED EWR WITHOUT INCIDENT. REPLACED BOTH TAIL COMPARTMENT TEMPERATURE OVERHEAT SWITCHES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SENSOR — MALFUNCTIONED (TAIL)

DFW - FLT 1682 - EN ROUTE DFW-TPA - WHILE CLIMBING THROUGH 14,000 FEET TAIL COMPARTMENT TEMPERATURE HIGH ILLUMINATED ON DEPARTURE. THE LIGHT EXTINGUISHED SHORTLY AFTER THE EMERGENCY PROCEDURES WERE ACCOMPLISHED, BUT RE-ILLUMINATED AGAIN SEVERAL TIMES. AN EMERGENCY RETURN TO DFW WAS ACCOMPLISHED. LANDED DFW WITHOUT INCIDENT. REPLACED TAIL COMPARTMENT TEMPERATURE SENSORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (R1 DOOR)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R1 DOOR DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HOUSING — LEAKING (APU)

SLC - FLT 1706 - AFTER TAKEOFF, SMOKE REPORTED IN CABIN. APU CHIP DETECTOR AND HOUSING LEAKING OIL. RESEALED CHIP DETECTOR AND HOUSING. CLEANED APU DUCTING AND CHANGED WATER SEPARATOR SOCKS. ACCOMPLISHED BURN OUT, NO SMOKE SMELL DETECTED. SYSTEM GROUND CHECKS NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN IN AFT COACH INOPERATIVE. REPLACED EMERGENCY EXIT SIGN LIGHT ASSEMBLY IN AFT COACH. SYSTEM GROUND CHECKS NORMAL. (M)

Part: SLIDE — DEFECTIVE (AFT FUSELAGE)

DFW - DURING OVERNIGHT CHECK, AIRCRAFT TAIL CONE INADVERTENTLY DEPLOYED BY CABIN SERVICE AND EMERGENCY EVACUATION SLIDE DID NOT DEPLOY. REPLACED AFT EMERGENCY EVACUATION SLIDE AND TAIL CONE ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)