N583AA

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 67,083 hrs · 35,018 cycles

PORTABLE EMER LIGHT FAILED ADJUSTMENT TEST. R & R PORTABLE EMER LIGHT. SYS CHECKED NORMAL.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 65,310 hrs · 33,969 cycles

LT MLG WW LONGERON 20 CRACKED AT STATION 994 FROM FASTENER DOWN TO END OF LONGERON. INSTALLED REPAIR DOUBLER IAW AARD 53-10-00-18.

Part: DOUBLER — WORN (FUSELAGE) · airframe 65,310 hrs · 33,969 cycles

FORWARD ACCESSORY COMPARTMENT DOOR LANDING DOUBLERS LT & RT SIDES WORN OUT OF LIMITS. REMOVED & INSTALLED NEW DOUBLERS IAW EA MD80-53-034088 & AARD 51-00-05-1.

Part: RIB — CRACKED (RT WING) · airframe 65,310 hrs · 33,969 cycles

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

Part: RIB — CRACKED (LT WING) · airframe 65,310 hrs · 33,969 cycles

LEFT HAND WING NR 4 INBD SLAT TRACK SUPPORT RIB CRACKED AT UPPER INBD PULLEY BRACKET BOSS. INSTALLED DOUBLER IAW PATTERN CARD 57-98-05 & EA MD80-57-034030.

Part: FUEL LINE — CRACKED (ZONE 100) · airframe 64,282 hrs · 33,397 cycles

PHX INFLIGHT LAX-STL. CENTER FUEL TANK FAILED TO FEED. EMERGENCY DECLARED FLIGHT DIVERTED PHX LANDED WITHOUT INCIDENT. PLACARDED BOTH CENTER FUEL BOOST PUMPS IAW MEL 28-1B. FLIGHT CONTINUED TO DESTINATION. FOUND TWO CRACKED FUEL LINES. REPLACED FUEL PLUMBING & CONDUIT AT DFW ON 10/25/2013. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: OVERHEAT SENSOR — FAULTY (AC BAY) · airframe 64,019 hrs · 33,237 cycles

DFW CREW REPORTED TAIL OVERHEAT INDICATION DURING CLIMB-OUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT & RT TAIL COMPARTMENT TEMPERATURE SENSORS. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: CLAMP — BROKEN (AC BAY) · airframe 63,896 hrs · 33,157 cycles

DFW CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMB OUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BROKEN AIR CYCLE MACHINE OUTLET CLAMP & HEAT EXCHANGER BOOT THAT WAS LEAKING. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,717 hrs · 29,632 cycles

CORROSION ON LOWER FLANGE OF FRAME STATIONS 1250 AT LONGERON 30. INSTALLED REPAIR STRAP PER EA MD80-53-016796.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,717 hrs · 29,632 cycles

CORROSION ON THE SHEAR TIE AT STATION 1174 BETWEEN LONGERON 30 AND 29 RIGHT. ACCOMPLISHED SPLICE REPAIR OF SHEAR TIE PER SRM 53-03-00 FIGURE 3 SHEET 1.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 57,717 hrs · 29,632 cycles

CORROSION ON THE AFT DOOR FRAME WEB UPPER AND LOWER SIDES AT STATIONS 1212 TO 1218 BETWEEN LONGERONS 28 AND 29 RIGHT. INSTALLED NEW WEB AT STATIONS 1150 TO 1218 FROM LONGERONS 29 TO 26 RIGHT PER AARD 51-10-00-05, PER SRM 51-30-05 AND SRM 51-30-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,717 hrs · 29,632 cycles

CORROSION ON DOOR CUTOUT LOWER FORWARD FITTING AT STATION 1155. INSTALLED NEW DOOR CUTOUT LOWER FORWARD FITTING AT STATION 1155 PER SRM 51-30-05 AND AARD 51-10-00-5.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,717 hrs · 29,632 cycles

CORROSION ON DOOR CUTOUT BEAM WEB STRAP DOUBLER AT STATION 1174. INSTALLED NEW WEB STAP DOUBLER PER SRM 51-30-02 AND AARD 51-10-00-5.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,717 hrs · 29,632 cycles

INTERCOSTAL AT STATION 769 TO 788 BETWEEN LONGERONS 27 AND 28 RIGHT IS CORRODED. INSTALLED SERVICEABLE INTERCOSTAL PER SRM 51-30-05.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,717 hrs · 29,632 cycles

CORROSION ON DOOR BEAM UNDER DOOR BEAM DOUBLER AT STATIONS 1155 TO 1212. INSTALLED DOOR BEAM REPAIR DOUBLER PER AARD 53-10-00-3 AND EA MD80-53-016682.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 57,717 hrs · 29,632 cycles

DEEP GOUGE AND BLENDS ON UPPER DOOR CUTOUT SKIN ALONG LOWER EDGE OF HORIZONTAL LEG OF DOOR BEAM FROM STATIONS 1164 TO 1203. INSTALLED DOUBLER PER EA MD80-53-016682.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,717 hrs · 29,632 cycles

CORROSION ON LOWER FRAME FLANGE AT STATION 1309 BETWEEN LONGERONS 29 RIGHT AND 29 LEFT. REMOVED DAMAGED SECTION AND INSTALLED J-ANGLE REPAIR PER AARD 53-10-00-17 AND EA MD80-53-016655.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,717 hrs · 29,632 cycles

CORROSION ON FRAME LOWER FLANGE STATION 1309 BETWEEN LONGERONS 29 LEFT AND 29 RIGHT. INSTALLED J-ANGLE REPAIR DOUBLER PER AARD 53-10-00-17 AND EA MD80-53-016655 DATED 4-27-2011.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,717 hrs · 29,632 cycles

AFT ACCESSORY 1418 FRAME CRACKED LONGERON 2 LEFT. INSTALLED DOUBLER ON FORWARD SIDE OF STATION 1418 LONGERON 2 LEFT PER SRM 53-03-00. INSTALLED DOUBLER ON AFT SIDE OF 1418 FRAME AT LONGERON 2 LEFT PER AARD 53-10-00-15, SRM 53-01-00 AND SRM 53-03-00.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,717 hrs · 29,632 cycles

MID CARGO HAS CRACK IN CEILING INTERCOSTAL AT ZERO BUTTLINE BETWEEN STATIONS 769 TO 788. INSTALLED NEW INTERCOSTAL BUTTLINE 0 STATIONS 769 TO 788 PER SRM 51-01-00, SRM 51-30-02, AND SRM 51-30-05.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,717 hrs · 29,632 cycles

CORROSION ON FRAME LOWER FLANGE STATION 1271 LONGERON 30 RIGHT. INSTALLED J-ANGLE REPAIR DOUBLER PER AARD 53-10-00-14.

Part: SKIN — DENTED (CARGO BAY) · airframe 57,717 hrs · 29,632 cycles

THREE DENTS IN AFT CARGO DOOR SKIN BETWEEN NUMBERS 4 AND 5 BEAMS 18 INCHES FROM AFT END. REPAIRED AFT CARGO DENTS BY INSTALLING DOUBLER PER SRM 53-04-00 FIGURE 38 SHEET 20.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,717 hrs · 29,632 cycles

STATION 1287 CORROSION ON SHEAR TIE BETWEEN LONGERONS 29 LEFT AND 29 RIGHT. REMOVED DAMAGED SECTION AND SPLICED NEW SECTION PER SRM 53-03-00 FIGURE 3 SHEET 1.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 57,717 hrs · 29,632 cycles

VERTICAL SUPPORT FITTING CRACKED BELOW NUMBER 4 SEAT TRACK AT STATION 826. TRIMMED OUT CRACK AND INSTALLED FILLER AND DOUBLER PER EA MD80-53-016600.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 57,717 hrs · 29,632 cycles

LEFT CUSP STATION 218 TO 237 DAMAGED. REPLACED CUSP SHEET PER AARD 51-10-00-5.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 57,717 hrs · 29,632 cycles

VERTICAL SUPPORT FITTING CRACKED BELOW NUMBER 4 SEAT TRACK AT STATION 864. TRIMMED OUT CRACK AND INSTALLED FILLER AND DOUBLER PER EA MD80- 53-016600.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,717 hrs · 29,632 cycles

LEFT CUSP CRACKED AT LIGHTENING HOLE STATION 225. INSTALLED NEW CUSP SHEET FROM STATIONS 218 TO 237 PER AARD 51-10-00-5 AND INSTALLED ELECTRICAL REPOSITIONING DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,717 hrs · 29,632 cycles

DENT IN FUSELAGE SKIN STATIONS 253 TO 300 ABOVE STRINGER LONGERON 24 LEFT. INSTALLED PERMANENT REPAIR PER SRM 53-04-01 AND BOEING DRAWING SG09530002.

Part: PAN — CRACKED (WINDOW) · airframe 57,717 hrs · 29,632 cycles

RIGHT STATION 1041 FORWARD LOWER EAR CRACKED ON THE WINDOW PAN. INSTALLED REPAIR ANGLE AS PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW FRAME) · airframe 57,717 hrs · 29,632 cycles

RIGHT STATION 1079 FORWARD LOWER EAR CRACKED ON THE WINDOW PAN. INSTALLED REPAIR ANGLE DOUBLER AARD 53-10-00-25.

Part: PAN — CRACKED (ZONE 200) · airframe 57,717 hrs · 29,632 cycles

RIGHT STATION 1041 UPPER AFT EAR CRACKED ON THE WINDOW PAN. INSTALLED REPAIR ANGLE AS PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW FRAME) · airframe 57,717 hrs · 29,632 cycles

RIGHT STATION 1079 UPPER AFT EAR CRACKED ON THE WINDOW PAN. INSTALLED REPAIR ANGLE DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (ZONE 200) · airframe 57,717 hrs · 29,632 cycles

RIGHT STATION 1193 UPPER AFT EAR CRACKED ON THE WINDOW PAN. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,717 hrs · 29,632 cycles

SEAT TRACK NUMBER 6 CORRODED AT STATIONS 630 TO 636. INSTALLED REPAIR PLUG PER AARD 53-20-00-10.

Part: GENERATOR — FAILED (LEFT) · airframe 55,079 hrs · 28,191 cycles

DFW - CREW REPORTED DURING CLIMBOUT LEFT GENERATOR FAILED AND AUXILIARY POWER UNIT ALREADY ON PLACARD. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE GENERATOR AND CONSTANT SPEED DRIVE. REPLACED AUXILIARY POWER UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: RADAR — INOPERATIVE (WX SYSTEM) · airframe 52,472 hrs · 26,752 cycles

DFW INFLIGHT LAX-ORD. WEATHER RADAR FAILED INFLIGHT. LANDED DFW WITHOUT IONCIDENT. REPLACED WEATHER RADAR RIGHT UNIT AND WEATHER RADAR CONTROL PANEL. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — NOT SEATED (EMERGENCY LIGHTS) · airframe 51,808 hrs

LGA - AFT INTERIOR OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERY PACK AT AFT INTERIOR OVERWING EXIT.

Part: BATTERY PACK — NOT SEATED (EMERGENCY LIGHTS) · airframe 51,808 hrs

LGA - EMERGENCY CEILING LIGHTS INOPERATIVE. RESEATED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 51,808 hrs

LGA - AFT EMERGENCY AISLE LIGHT INOPERATIVE. REPLACED BATTERY PACK AT AFT AISLE.

Part: BATTERY PACK — NOT SEATED (EMERGENCY LIGHTS) · airframe 51,808 hrs

LGA - EMERGENCY LIGHT AT AFT LAVATORY INOPERATIVE. RESEATED BATTERY PACK AT AFT LAVATORY.

Part: BATTERY PACK — NOT SEATED (EMERGENCY LIGHTS) · airframe 51,808 hrs

LGA - EMERGENCY CEILING LIGHTS AT AFT STAIRWELL DOOR PANEL INOPERATIVE. RESEATED BATTERY PACK FOR AFT STAIRWELL DOOR PANEL.

Part: APU — CONTAMINATED · airframe 49,589 hrs

ORD INFLIGHT T1861/13APR - CREW REPORTED SMELL OF BURNING DEICING FLUID IN AIR CONDITION SYSTEM. CABIN FILLED WITH SMOKE. CREW SHUT DOWN RIGHT PACK. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. FOUND APU HAD INGESTED FLUID. REPLACED AUXILIARY POWER UNIT AND ACCOMPLISHED BURNOUT OF HIGH PRESSURE PNEUMATIC DUCTING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,440 hrs

LGA - EMERGENCY LIGHT AT MID CABIN RIGHT EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT MID CABIN RIGHT EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — FAILED (R1 DOOR) · airframe 48,947 hrs

SAN - EMERGENCY ESCAPE SLIDE AT R1 DOOR UNSUCCESSFULLY DEPLOYED. SLIDE WAS HANGING FROM GIRT BAR AT DOOR FRAME. REPLACED RIGHT NUMBER ONE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,886 hrs

LGA - EMERGENCY LIGHT AT SEAT ROW 25DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 25DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: VALVE — INOPERATIVE (MLG)

SAT INFLIGHT T304/23AUG - LANDING GEAR WOULD NOT RETRACT. RETURNED TO SAT AND LANDED WITHOUT INCIDENT. FOUND GEAR DOOR BYPASS LEVER OPEN. REPAIRED VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — MISSING (EMERGENCY LIGHT)

MSP - EMERGENCY AISLE LIGHT AT SEAT 15D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY AISLE LIGHT AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SCHRADER VALVE — DEFECTIVE (NLG)

DFW INFLIGHT T1181/07 - UNABLE TO RETRACT NOSE GEAR AFTER TAKEOFF. RAN CHECKLIST. NO DAMAGE TO NOSE GEAR AREA. FOUND NOSE STRUT FLAT. REPLACED SCHRADER VALVE AND SERVICED NOSE GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

SJC - COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY FOR COCKPIT OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHTS ABOVE SEATS 23-28 INOPERATIVE. REPAIRED EMERGENCY EXIT CEILING LIGHTS ABOVE SEATS 23-28 CONNECTION. SYSTEM GROND CHECKED NORMAL OPERATION. (M)

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 DOOR INOPERATIVE. REPAIR EMERGENCY EXIT LIGHT WIRE SPLICE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS FROM ROW 28-29 INOPERATIVE. ADJUSTED EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FRAME — CORRODED (FUSELAGE)

TUL - FOUND CORROSION IN LOWER CHANNEL AND LIP OF FRAME. BLENDED OUT CORROSION. TREATED AND PRIMED AREA AND INSTALLED DOUBLER PER AARD 53-10-00-14 PAGE NR 1. (M)

Part: STRUCTURE — CORRODED (FUSELAGE)

TUL - FOUND CORROSION REMOVAL BEYOND MANUAL LIMITS, CONDITION IV. INSTALLED FULL LENGTH DOUBLER PER AARD 53-10-00-3. (M)

Part: SKIN — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SKIN AND DOUBLER UNDER LOWER AFT CORNER OF AFT LAV PANEL. REPAIRED PER ESO PO559 DATED 1-10-03. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CUSP INBOARD OF SERVICE DOOR FRAME HAS CORROSION. INSTALLED CUSP DOUBLER INBOARD OF SERVICE DOOR AREA APPROX STATION 160-200 PER AARD 53-20. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

TUL - FOUND LOWER WINDOW FRAME TAB CRACKED, BOTTOM FORWARD CORNER. INSTALLED REPAIR ANGLE ON BOTTOM FORWARD CORNER OF WINDOW FRAME AT STATION 1155 LEFT PER AARD 53-10-00-25. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

(BATTERY PACK) DURING OVERNIGHT MAINTENANCE ROW 17-22, EMERGENCY EXIT LIGHTS INOPERATIVE REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHT BY AFT GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT CEILING LIGHT ASSEMBLY BY AFT GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — DEFECTIVE (RT EMERG EXIT)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FORWARD RIGHT OVERWING EMERGENCY EXIT LIGHT MODULE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LONGERON — CRACKED (BS 1003)

TUL - EXTERNAL LONGERON CRACKED AT STATINO 1003, LONGERON 26R. REMOVED AND REPLACED WITH EXTERNAL LONGERON FROM STATION 930 TO STATION 1003 PER STANDARD PRACTICES SRM 51-10 (LONGERON 26). (M)

Part: SKIN — GOUGED (BS 1309)

TUL - DEEP GOUGE IN FUSELAGE SKIN STATION 1309 LONGERON 19R APPROX 1 INCH LONG. INSTALLED DOUBLER PER SRM 53-04 FIG 3A. (M)

Part: SEAT TRACK — CORRODED (BS 1300-1304)

TUL - SEAT TRACK NR 2 HAS CORROSION, STATION 1300-1304. REPLACED SEAT TRACK SECTION FROM STATION 126 TO 1304 PER SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (BS 1300-1304)

TUL - NR 3 SEAT TRACK CORRODED STATION 1300-1304. INSTALLED NEW SEAT TRACK SECTION FROM STATION 1260 TO 1304 PER SRM 53-05. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FORWARD CABIN INOPERATIVE. RESEATED EMERGENCY EXIT FLOOR PATH LIGHT WIRE CONNECTOR IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 7 AND 16 FOUND INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRE BY PASSENGER SEAT, ROW 7. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)