N593AA

Part: SWITCH — INOPERATIVE (CABIN PRESSURE) · airframe 61,365 hrs · 26,448 cycles

LIT - INFLIGHT CLT-DFW. CREW REPORTED CABIN PRESSURIZATION ISSUES AND BOTH PACKS FAILED INFLIGHT. EMERGENCY DECLARED FLIGHT DIVERTED LIT LANDED WITHOUT INCIDENT. REPLACED 450 SWITCH. SYSETM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,354 hrs · 26,440 cycles

FUSELAGE SKIN CRACKED AT RIGHT AFT NOSE LANDING GEAR DOOR-AFT HINGE CUTOUT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-05-00.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,354 hrs · 26,440 cycles

FUSELAGE SKIN STATION 101 DAMAGED. INSTALLED DOUBLER PER SRM 53-05-00.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,354 hrs · 26,440 cycles

FUSELAGE SKIN CRACKED AT LEFT AFT NOSE LANDING GEAR DOOR - AFT HINGE CUTOUT. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-05-00 FIGURE 62 SHEET 1 AND 2.

Part: TURBINE BLADES — DAMAGED (RT ENGINE) · airframe 60,268 hrs · 25,883 cycles

DFW - CREW REPORTED ON TAKEOFF THERE WAS A LOUD BANG AND THE RIGHT ENGINE BEGAN TO SPOOL DOWN. ENGINE AND AIRFRAME VIBES WERE FELT. RIGHT ENGINE SHUTDOWN ON ITS OWN. EXAMINATION OF THE RIGHT ENGINE ON THE GROUND SHOWED AFT SECTION OF TURBINE BLADES MISSING. ALL PARTS WERE CONTAINED INSIDE ENGINE. REPLACED RIGHT HAND ENGINE AT DFW ON 07/16/2010. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: DUCT — FAULTY (ZONE 100) · airframe 59,789 hrs · 25,649 cycles

DFW - CREW REPORTED A BURNING ODOR IN CABIN AFTER TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND FORWARD CARGO HEATER DUCT ASSEMBLY FAULTY. REPLACED DUCT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,186 hrs · 24,459 cycles

FRAME CRACKED FORWARD SIDE AT LONGERON 2 RIGHT HAND. REPAIRED FRAME PER EA MD80-53-006722.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,186 hrs · 24,459 cycles

FRAME CRACKED FORWARD AND AFT SIDES AT LONGERON 2 LEFT. REPAIRED FRAME PER EA MD80-53-006722.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,188 hrs · 24,460 cycles

RIGHT HAND TIE DOWN TRACK HAS CORROSION STATION 1279-1231. INSTALLED NEW RIGHT HAND TIE DOWN TRACK 1231-1279 PER SRM 51-30-01.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,186 hrs · 24,459 cycles

SHEAR TIE CRACKED AFT SIDE STATION 1451 LONGERON 2L. INSTALLED NEW SHEAR TIE PER SRM 51-01.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 57,186 hrs · 24,459 cycles

LEFT TIE DOWN TRACK CORRODED IN AFT CARGO. INSTALLED NEW TIE DOWN TRACK PER SRM 51-00.

Part: SHELF — CRACKED (RT MLG WW) · airframe 57,186 hrs · 24,459 cycles

SHELF CRACKED AT FASTENER ABOVE RIGHT GEAR DOOR STRUT IN WHEEL WELL. REMOVED AND REPLACED SHELF AS PER DRAWING 9930582 AND 51-30-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,186 hrs · 24,459 cycles

CORROSION ON NR 2 SEAT TRACK STATION 1200. REMOVED CORROSION AND INSTALLED SEAT TRACK PLUG AS PER 53-05-00 PAGE 19 AND AARD 53-20-00-10 REPAIR 10.

Part: CASTING — CRACKED (SPOILER) · airframe 57,186 hrs · 24,459 cycles

SPOILER CASTING CRACKED. REPLACED SPOILER CASTING PER SRM 57-20-00-50.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 57,186 hrs · 24,459 cycles

AFT CARGO HAS CORROSION ON LOWER SIDE OF CUSP BETWEEN STATION 1174-1193. INSTALLED NEW CUSP SHEET FROM STATION 1174-1250 LEFT PER AARD 53-20-00-16.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 57,186 hrs · 24,459 cycles

DOUBLE DRILLED HOLE IN 1212 FRAME, RIGHT SIDE ABOVE STRINGER 18, BOTTOM HOLE OF UPPER HALF OF STRAP. INSTALLED FREEZE PLUG PER EA MD80-53-006681.

Part: SKIN — CRACKED (ZONE 100) · airframe 57,186 hrs · 24,459 cycles

CRACK IN FUSELAGE SKIN AT RIGHT HAND CANT STATION 1474 BELOW RAIN GUTTER. INSTALLED DOUBLER PER SRM 53-01-52.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 57,186 hrs · 24,459 cycles

J-ANGLE DOUBLER CRACKED, STATION 47. REMOVED AND REPLACED DOUBLER PER AARD 53-10-00-4.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,186 hrs · 24,459 cycles

CORROSION ON CUSP BETWEEN TRACKS 1 AND 2 STATION 1305 TO 1308. INSTALLED NEW CUSP SHEET FROM STATION 1250 TO 1309 LEFT PER SRM 51-01-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,186 hrs · 24,459 cycles

RIGHT CUSP CORRODED. REMOVED AND REPLACED CUSP PER SRM 51-01-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,186 hrs · 24,459 cycles

CORROSION ON CUSP, STATION 700 LEFT. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: STOP FITTING — CRACKED (DOOR) · airframe 57,186 hrs · 24,459 cycles

CRACKED ANGLE ON LOWER STOP FITTING AREA. INSTALLED NEW ANGLE PER ESO 80174.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,186 hrs · 24,459 cycles

CRACKED WEB AT STATION 210, LONGERON 11L. INSTALLED DOUBLER PER AARD 53-10-00-11.

Part: STRUCTURE — FOD (CARGO DOOR) · airframe 57,186 hrs · 24,459 cycles

FOREIGN OBJECT DAMAGE TO FORWARD CARGO DOOR, DOO2492. REPAIRED WITH DOUBLER AT 2ND BEAM FROM TOP PER ESO 80174 AND SRM 53-04-00 FIG 38 ON DWMS 1183144.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 57,186 hrs · 24,459 cycles

LEFT NUMBER 4 DOOR ON LEFT SIDE CRACKED ON OUTBOARD SIDE AT STATION 160. REPAIRED WITH LONGERON SPLICE PER SRM 53-02-00 FIGURE 18.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 57,186 hrs · 24,459 cycles

NR 1 BEAM STOP-PAD FITTING CRACKED. REMOVED AND REPLACED STOP-PAD FITTING PER ESO-80174.

Part: STOP FITTING — CRACKED (DOOR) · airframe 57,186 hrs · 24,459 cycles

STOP PAD FITTING CRACKED AT NUMBER 5 BEAM AFT SIDE. REMOVED AND REPLACED STOP-PAD FITTING PER ESO-80174.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,186 hrs · 24,459 cycles

DENT IN LEFT FUSELAGE AT STATION 243, 7 INCHES ABOVE FLOOR LINE AT L18 LEFT. CUT OUT DAMAGE, INSTALLED DOUBLER AND FINGER DOUBLER PER SRM 53-04 FIGURE 12B.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,186 hrs · 24,459 cycles

CRACK IN LEFT WINDOW PAN STATION 788. INSTALLED REPAIR DOUBLER ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,186 hrs · 24,459 cycles

WINDOW FRAME PAN CRACKED, RIGHT STATION 1060. INSTALLED DOUBLER REPAIR ANGLE PER AARD 53-10-00-25.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 57,186 hrs · 24,459 cycles

STOP FITTING IS CRACKED AT AFT CARGO COMPARTMENT LOCATION. REMOVED AND REPLACED FITTING PER ESO 80174.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,186 hrs · 24,459 cycles

FORWARD UPPER LEG OF WINDOW PAN IS CRACKED AFT OF STATION 788. REMOVED DAMAGED SECTION, INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,186 hrs · 24,459 cycles

WINDOW PAN CRACKED STATION 1022R. INSTALLED DOUBLER REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 57,186 hrs · 24,459 cycles

WINDOW PAN CRACKED STATION 946L. INSTALLED REPAIR ANGLE DOUBLER PER AARD 53-10-00-25.

Part: STOP FITTING — CRACKED (DOOR) · airframe 57,186 hrs · 24,459 cycles

DOOR STOP FITTING CRACKED. REMOVED AND REPLACED DOOR STOP FITTING PER ESO 80174.

Part: DUCT — LEAKING (ANTI ICE) · airframe 56,797 hrs · 24,262 cycles

LEFT ENGINE FIRE WARNING. EMERGENCY DECLARED RETURNED LAS WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NR 1 ENGINE UPPER RT ANTI-ICE DUCT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 55,414 hrs

SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROWS 3EF TO 20EF EXTINGUISHED AFTER 10 TO 25 SECONDS. CHARGED EMERGENCY LIGHTS FROM SEAT ROWS 3EF TO 20EF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN) · airframe 55,029 hrs

LGA - EXTERIOR EMERGENCY LIGHTS AT LEFT AND RIGHT OVERWING INOPERATIVE. RESEATED CONNECTOR ON CHARGER FOR LEFT AND RIGHT EXTERIOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRAP — MISSING (FLASHLIGHT) · airframe 55,029 hrs

LGA - EMERGENCY FLASHLIGHT AT STRAP MISSING AT AFT GALLEY. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRAP — MISSING (FLASHLIGHT) · airframe 55,029 hrs

LGA - EMERGENCY FLASHLIGHT AT AFT JUMPSEAT HAS TWO STRAPS MISSING. REPLACED TWO STRAPS FOR EMERGENCY FLASHLIGHT AT AFT JUMPSEAT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PRESSURE SWITCH — INOPERATIVE (A/C BAY) · 54,697 cycles

LAX INFLIGHT T1960/28AUG. BOTH AIR CON PACKS WENT TO ZERO FLOW ON CLIMB. ACFT WOULD NOT PRESSURIZE. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED BOTH LT AND RT HAND SINGLE ENGINE SECON SEGMENT CLIMB PRESSURE SWITCHES. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY EXIT LIGHTS ON LEFT AND RIGHT SIDE UPPER SIDEWALL AT ROW 20 FORWARD OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD OVERWING EMERGENCY EXIT LIGHTS AT ROW 20 LEFT AND RIGHT UPPER SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — UNSECURE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHTS IN CEILING AT SEAT ROWS 23 TO 27 INOPERATIVE. RESEATED BATTERIES IN POWER SUPPLY FOR EMERGENCY LIGHTS IN CEILING AT SEAT ROWS 23 TO 27. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TERMINAL — INOPERATIVE (BATTERY)

SFO - EMERGENCY EXIT LIGHTS AT AFT OVERWING INOPERATIVE. CLEANED AFT OVERWING BATTERY PACK TERMINALS FOR EMERGENCY EXIT LIGHTS AT AFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHTS AT EMERGENCY OVERWING DOOR LEFT AND RIGHT INOPERATIVE. SPUN BATTERIES IN PACK FOR EMERGENCY LIGHTS AT EMERGENCY OVERWING DOOR LEFT AND RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

JFK AFT OVERWING EMERGENCY EXIT SIGN LIGHT AT ROW 21 LEFT AND RIGHT INOPERATIVE. RESECURED LOOSE CONNECTION ON BATTERY PACK FOR AFT OVERWING EMERGENCY EXIT SIGN LIGHT AT ROW 21 LEFT AND RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BOLT — MISSING (MLG DOOR)

PHX INFLIGHT T1007/19JULY GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR EXTENSION. VERIFIED LEFT HAND GEAR DOOR OPEN. LANDED WITH DOORS OPEN. INSTALLED MISSING BOLT FROM LEFT HAND GEAR DOOR FOLLOW UP MECHANISM. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — OUT OF POSITION (CABIN)

TUL - VARIOUS CEILING EMERGENCY LIGHTS AND TAIL COMPARTMENT LIGHTS INOPERATIVE. REPOSITIONED BATTERY FOR INOPERATIVE CEILING EMERGENCY LIGHTS AND TAIL COMPARTMENT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SCISSOR LINK — CRACKED (LT MLG)

SJC - LEFT GEAR SCISSORS UPPER LINK CRACKED AT FORWARD PIVOT POINT. REPLACED LEFT SCISSORS SUPPORT LINK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND FUSELAGE SKIN IS CRACKED THROUGH RIVET STATION 1380 RIGHT SIDE JUST ABOVE PYLON. DOUBLER INSTALLED PER SRM 53-01, FIG 2 SHEET 3 AND AARD 53-30-00-00 REV DATED 8-30-02. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND LONGERON 2L IS CRACKED AFT OF STATION 1418 FRAME, CRACK APPROX .125 INCH LONG. REMOVED DAMAGED SECTION OF LONGERON, OBTAINED AND INSTALLED EXTRUSION PER AARD 53-30-00-2. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND LONGERON 2R IS CRACKED AFT OF STATION 1418 FRAME, CRACK IS APPROX .125 INCH LONG. REMOVED DAMAGED SECTION OF LONGERON, OBTAINED AND INSTALLED EXTRUSION PER AARD 53-30-00-2. (M)

Part: BATTERY — DISCHARGED (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS SYSTEM INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

AUS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS B5-27 INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING FORWARD EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SENSOR — DEFECTIVE (TAIL COMPARTMENT)

ENROUTE, AFTER TAKEOFF ON CLIMBOUT TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. STAYED ON FOR SEVERAL MINUTES. RETURNED RDU, WITH POWER REDUCED LIGHT EXTINGUISHED. LANDED RDU WITHOUT INCIDENT. REPLACED RT TAIL COMPARTMENT OVERHEAT SENSOR. RAN ENGINES TO ALL POWER SETTINGS WITH NO LEAKS NOTED, ALL INDICATIONS NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND CANTED FRAME AT STATION 1485 AT AFT AIRSTAIR ACTUATOR IS CRACKED. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER AARD 53-10-00-33 PAGE 1. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND DEEP GOUGE IN FUSELAGE SKIN STATION 402 AT LONGERON 30 AT ANTENNA MOUNT. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-04 FIG 12B. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT IN FUSELAGE SKIN AT STATION 237 BETWEEN LONGERON 18L AND LONGERON 19L. COLD WORK DENT AND INSTALLED DOUBLER PER SRM 53-30-00-9. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND TEMPORARY DOUBLER INSTALLED ON LEFT SIDE OF FUSELAGE, JUST FORWARD OF STATION 579, L20L - L21L. REMOVED TEMPORARY REPAIR AND INSTALLED NEW CLASS 1 PERMANENT REPAIR PER SRM 53-04 FIG 128. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT APPROXIMATELY 2.5 INCHES AFT OF FORWARD ENTRY DOOR IN RED STRIPE. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 1 SEAT TRACK HAS HEAVY CORROSION IN CHANNEL FROM BS 1205 TO 1208. REMOVED CORROSION AND INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: SLIDE — DEPLOYED (AFT FUSELAGE)

BNA - AT GATE, TAILCONE SLIDE WAS INADVERTENTLY DEPLOYED. INITIALLY INFLATED THEN DEFLATED AFTER TOUCHING GROUND. REPLACED SLIDE. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: SKIN — DENTED (RT WING TIP)

TUL - FOUND RIGHT WING TIP L/E DAMAGED, DENTED. REMOVED AND REPLACED DAMAGED WING TIP PARTS. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR TRACT LIGHTING IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR TRACK LIGHT STRIP IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR TRACK LIGHTING IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR TRACK LIGHT CONNECTOR IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: OIL CAP — DEFECTIVE (APU)

BOS - FLT 1055 - AFTER TAKEOFF, A BURNING SMELL OF OIL AND SMOKE WERE NOTED IN THE CABIN. AIRCRAFT AIR INTERRUPTED AND RETURNED TO BOS WITHOUT FURTHER INCIDENT. REPLACED APU OIL FILLER CAP AND AS A PRECAUTIONARY, REPLACED BOTH COALESCER BAGS. SYSTEM GROUND AND LEAK CHECKED, NORMAL OPERATION. (X)

Part: EEL WIRE — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, FOUND THE FIRST CLASS FORWARD EMERGENCY EXIT FLOOR PATH LIGHT STRIP INOPERATIVE. REPAIRED WIRE ON FIRST CLASS FORWARD EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)