N871GA

Part: CONNECTOR — DEFECTIVE (STALL WARNING) · airframe 47,076 hrs · 40,046 cycles

STALL INDICATOR FAILURE ON OAP. DURING CRUISE RAN QRH 85.4, STALL SYS 2 DID NOT TEST, PULLED FIRST OFFICERS STALL SYS NR 2 CB. FOUND HARD FAULT ON STALL COMP NR 2 RT AOA VANE ON MX TEST. R & R RT AOA VANE TRANSDUCER CONNECTOR, BITE TEST STALL WARNING SYS OK & RT AOA HEATER TESTED OK IAW AMM 34-19-01 & SWPM 20-31-00.

Part: COMPUTER — FAULTY (STALL WARNING) · airframe 47,071 hrs · 40,044 cycles

STALL IND FAILURE ON OAP SEVERAL TIMES IN FLIGHT. STALL SYS 2 WOULDN’T TEST, WENT OUT IN APPROX 1 MINUTE EACH TIME. R & R STALL WARNING COMPUTERS 1 & 2. OPERATIONS HECK GOOD IAW AMM 34-19-02.

Part: PROXIMITY SENSOR — FAULTY (LE SLAT) · airframe 47,009 hrs · 40,012 cycles

DURING THE T/O ROLL RECEIVED THE SLAT DISAGREE & THE SLAT AURAL WARNING AROUND 70 KTS. ABORTED T/O. TAXIED BACK TO THE GATE. CAPTAIN WILL PUT THE DISCREPANCY IN THE LOG BOOK. PSEU SN 668 HAD PRIOR FAULT ISSUES WITH SLAT DISAGREE. R & R PSEU IAW AMM 32-60-04-2-0. PERFORMED FAULT ISOLATION TEST AUGMENTING SLATS TROUBLESHOOTING IAW AMM 27-80-00-1-0. OPERATIONS CHECKED GOOD. AMBER SLAT DISAGREE LIGHT ILLUMINATED DURING PREFLIGHT. R & R PROX BOX, S/U CONTROL UNIT. OPERATIONS CHECKED NORMAL IAW MM 32-60-04-20. PERFORMED SLAT TROUBLESHOOTING 27-80-00-1-0. OPERATIONS CHECKED NORMAL PREVIOUS UNIT FAULTED LT OTBD SENSOR CODE 32. CONFIRMED SENSOR & WIRING A GAPS, CHECKED NORMAL ALSO.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,582 hrs · 39,731 cycles

EMERGENCY LIGHTS OVER AFT F/A SEATS OUT. REPLACED BULBS & BATTERY TASKS IN AFT RT LAV REF AMM 33-53-00-4.

Part: BATTERY — DISCHARGED (CABIN) · airframe 46,361 hrs · 39,607 cycles

ROW 10 - 11 FED OVERHEAD EMER LIGHTS WON’T TURN OFF. R & R ROW 10 - 11 FED OVERHEAD EMER LIGHT BATTERIES IAW AMM 33-50-00. OPERATIONS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (TCAS) · airframe 46,274 hrs · 39,559 cycles

T CAS SYS NOT REPORTING TRAFFIC PROPERLY WITH VISUAL CONTACT OF TRAFFIC CLEARLY ON LEFT SIDE OF ACFT FLIGHT PATH, T CAS INDICATED TRAFFIC TO BE THE RIGHT SIDE OF ACFT. FLIGHT PATH PASSED DIRECTLY OVER ACFT AT 1000 FEET ABOVE WITH T CAS SELECTED BELOW POSITION & T CAS SLOPE DID NOT REPORT TRAFFIC AT ALL. PERFORMED TRAFFIC COLLISION AVOIDANCE SYS TEST. TEST PASSED IAW AMM 34-46-00.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 46,000 hrs · 39,414 cycles

L2, AFT ENTRY & TAIL CONE EMER EXIT SIGN LIGHT INOPERATIVE. R & R L2, AFT ENTRY & TAIL CONE EMER EXIT SIGN POWER SUPPLY IAW MM 33-53-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR)

LEFT EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED LT EXTERIOR EMER LIGHT IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 45,918 hrs · 39,366 cycles

APU RUNNING AT GATE, STRONG SMELL OF FUEL IN CABIN. PERFORMED LEAK CHECK OF APU, NO LEAKS NOTED IAW MM 49-00-00. SEE LOG PAGE 533394 FOR COALESCER SOCK LT & RT REPLACEMENT. NO FUEL SMELL IN CABIN NOTED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 45,916 hrs · 39,365 cycles

TAIL COMPARTMENT EMER EXIT LIGHTS INOPERATIVE. REPLACED POWER SUPPLY BATTERIES FOR TAIL COMPARTMENT LIGHTS. OPERATIONS CHECKED NORMAL IAW AMM 33-50-00.

Part: SLAT — DENTED (NR 2)

NUMBER 2 SLAT DENT, DMI 15786. RE-INSPECT REQUIRED AT NEXT C-CHECK IS NOW BEING TRACKED BY CONTROL 51000014. THIS CLEARS MEL 05-05-10 DMI 15786.

Part: OIL SYSTEM — LEAKING (APU) · airframe 44,782 hrs · 38,780 cycles

ON CLIMB OUT STRONG SMELL OF FUMES THROUGHOUT CABIN & COCKPIT. RAN QRH 26.2 FUMES DISSIPATED ONLY BRIEFLY & RETURNED DURING DESCENT. PERFORMED QRH 26.5 FUMES REMOVAL PRESSURIZED. LANDED WITHOUT INCIDENT. COMPLIED WITH WORK ORDER 00234942 FOR TROUBLESHOOTING. REF LP 545051 FOR APU OIL LEAK & CORRECTIVE ACTION. REF LP'S 545050 FOR SOCK R & R, 545055 FOR RECIRC FILTER R & R. NO FURTHER DEFECTS NOTED AT THIS TIME. OPERATED PACKS WITH NO ABNORMAL SMELLS NOTED. SSE CONCURRENCE RECEIVED, OK FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

L1 ENTRANCE UPPER EMER FLASHLIGHT INOPERATIVE. R & R BATTERY FOR UPPER FWD EMER FLASHLIGHT IAW AMM 25-60-00. OPERATIONS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN)

FWD FLIGHT ATTENDANT PORTABLE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERIES & OPERATIONS CHECKED NORMAL IAW AMM 33-53-00.

Part: SIGN — DEFECTIVE (CABIN)

SELF-ILLUMINATED EXIT SIGNS AT AFT OVERWING EXIT FAILED COMPARATOR CHECK DURING C-CHECK

Part: SKIN — CHAFED (VERTICAL STAB)

VERTICAL STABILIZER SKIN, PN 5912166-185, CHAFED. REMOVED DAMAGED SECTION OF SKIN & INSTALLED REPAIR DOUBLER & FAIRING PLATE IAW SRM 55-01 FIG 4.

Part: SKIN — CHAFED (VERTICAL STAB)

VERTICAL STABILIZER SKIN, PN 5912166-11, BONDED DOUBLER, PN 5912166-89, CHAFED. FABRICATED NEW SKIN PANEL IAW EA NR 15570 & INSTALLED IAW SRM 51-30-2.

Part: SIGN — DEFECTIVE (CABIN)

SELF-ILLUMINATING EXIT SIGNS AT FWD OVERWING EXIT FAILED COMPARATOR CHECK DURING C-CHECK.

Part: FLOOR PANEL — CORRODED (CARGO BAY)

AFT CARGO FLOOR PANEL HAS CORROSION ON UPPER & LOWER SURFACES, OUT OF SRM LIMITS. LOCATED & DRILLED REPLACEMENT PANEL PN 5936603-1 IAW SRM 51-10-4.

Part: SKIN — DENTED (CARGO DOOR)

AFT CARGO DOOR SKIN DENTED OUT OF SRM LIMITS. REMOVED DAMAGED SECTION OF DOOR SKIN & INSTALLED REPAIR DOUBLER & FILLER IAW SRM 52-05 FIG 66.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE)

CLIMBING THROUGH FL 220 PRESSURIZATION FAILED CABIN ALT CLIMBING RAPIDLY, NO FLOW HIGH. FOLLOWED QRH LED TO DEPLOYING PAX O2 MASKS. R & R NR 1 & NR 2 PRESS CONTROLLERS IAW MM 21-32-03. R & R ONE EACH PRESS CONTROLLER LINE ON NR 1 PRESS CONTROLLER IAW MM 21-32-00. PERFORMED SYS LEAK CHECK IAW MM 34-11-00 & IAW LOG PG 485750 FOR RE-STOWING OF PAX O2 MASK'S & PANELS IAW TASK CARD I0583501.

Part: BULKHEAD — CRACKED (BS 1463)

CRACK FOUND ON FWD AND AFT SIDES OF CANTED BULKHEAD WEB AT BS 1463 BETWEEN LONGERON 8 & 9R.

Part: PACKING — DAMAGED (APU)

WHILE AT THE GATE IT WAS NOTICED THERE WAS FUEL DRIPPING FROM THE APU AND A SMELL OF FUEL WAS NOTICED IN THE CABIN AREA. REMOVED AND REPLACED THE FUEL CONTROL UNIT'S PACKINGS AND PERFORMED PACK BURN AND APU HEALTH CHECK. OPS AND LEAK CHECKED NORMAL. C/W TASK CARD 505920101 AND AMM 49-30-01.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BALLAST — MALFUNCTIONED (CABIN)

FLIGHT CREW PERSONNEL REPORTED SMOKE FROM ROW 36 DEF FROM PASSENGER SERVICE UNIT. MAINTENANCE DEPARTMENT REMOVED AND REPLACED LIGHT BALLAST IAW MD80 AMM 33-50. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE EMERGENCY FLASHLIGHT ASSY AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERIES IN POWER SUPPLY BATTERY PACK. AN OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, OPS CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: COALESCER BAG — DIRTY (AC BAY)

WHILE DEPLANING, CABIN FILLED WITH SMOKE, ALL PASSENGERS AND CREW TAKEN OFF PLANE. SHUT OFF ELECTRICAL ON PLANE. DURING WALK AROUND FOUND PUDDLE OF HYDRAULIC FLUID FROM REVERSER ACCESS PANEL. FOUND RETURN LINE LEAKING AT THRUST REVERSER LEFT CONTROL VALVE. TIGHTENED SAME. LEAK CHECK OK PER AMM 29-10-00. DEPLOYED LEFT THRUST REVERSER CHECKS OK PER AMM 78-30-01. REPLACED WATER SEPARATOR BAGS IAW AMM 21-20-02 AND CHECKED AIR CONDITIONING SYSTEM. CHECKS GOOD IAW 21-50-00. ALL WORK DONE IAW MAINTENANCE PROCEDURES AND OPS CHECKS GOOD IAW 21-00-00, AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: CUSP WEB — CORRODED (FUSELAGE)

FLOOR CUSP WEB CORRODED IN MAIN CABIN FS 215 LBL 15. INSTALLED REPAIR DOUBLER TO FLOOR WEB AS FS 215 LBL 15 IAW MD80 SRM 53-01 FIG 4.

Part: CUSP WEB — CORRODED (FUSELAGE)

FLOORBOARD CUSP WEB CORRODED AT FS 200 IN MAIN CABIN LBL 44. REPAIRED CUSP WEB IAW MD80 SRM 53-01 FIG 4.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BALLAST — FAILED (CABIN)

FLIGHT CREW PERSONNEL REPORTED ON THE GROUND AT STATION TOL, SMOKE AND FUMES COMING OUT OF OVERHEAD SEAT ROW 31 AND 30 A AND C. CONTRACT MAINTENANCE PERSONNEL ACCESSED CEILING LIGHT BALLAST IAW 33-21-03 AND DISCONNECTED CONNECTOR. CONFIRMED BAD BALLAST. DEFERRED CEILING LIGHT BALLAST IAW MWL 33-02 SIT 1. DMI 258080, M PROCEDURE COMPLIED WITH, INOP, PLACARD INSTALLED. ALLEGIANT MAINTENANCE PERSONNEL REMOVED AND REPLACED CEILING LIGHT BALLAST IAW AMM 33-21-03, OPS CHECK GOOD. CLEARED DMI AND RETURNED AIRCRAFT TO SERVICE.

Part: WINDOW FRAME — CRACKED (FUSELAGE)

THE WINDOW PAN WAS FOUND CRACKED AT STA 886-905 RT LOWER AFT TAB. REF AA N/R 6200761.

Part: PAN — CRACKED (BS 946-965)

LEFT SIDE STA 946-965 FWD TOP EAR CRACKED ON WINDOW PAN.

Part: PAN — CRACKED (BS 1155)

WO 94582 AT STA 1155 RT WINDOW BELT CRACKED AT LOWER FWD CORNER. REPAIRED PER ESO 80559 DATE 28 AUG 2009.

Part: CUSP WEB — CRACKED (FUSELAGE)

LEFT CUSP CRACKED AT STA 837.

Part: LONGERON — CRACKED (FUSELAGE)

FOUND LT LONGERON 2 AT STA 1418 CRACKED.

Part: PAN — CRACKED (BS 1136)

CABIN RT SIDE STA 1136 TOP AFT WINDOW PAN EAR CRACKED.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY)

FLIGHT CREW REPORTED SMOKE IN CABIN AND AFT LAV SMOKE DETECTORS WERE SET OFF. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED ALL RELATED SYSTEM AND FOUND NO DEFECTS. AIRCRAFT WAS RETURNED TO SERVICE

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK MAINTENANCE INSPECTION. MAINTENANCE REPORTED THAT THE EMERGENCY EGRESS PATH LIGHTING FROM ROW 20 TO 24, BOTH FORWARD LEFT AND RIGHT OVERWING ESCAPE HATCH EMERGENCY EXIT SIGNS AND BOTH AFT LEFT AND RIGHT OVERWING ESCAPE HATCH EMERGENCY EXIT SIGNS WOULD NOT TEST. MAINTENANCE FURTHER REPORT THAT A BATTERY PACK AT POSITION BS-600S WAS REMOVED AND REPLACED FOR THE EGRESS PATH ISSUE AND THAT A POWER SUPPLY AND BATTERY PACK AT POSITION BS-49 WERE REMOVED AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-51-13. THE AIRPLANE HAS RETURNED TO SERVICE.

Part: PORTABLE LIGHT — MALFUNCTIONED (L1 DOOR)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION LAS VEGAS MAINTENANCE REPORTED THAT THE MAIN PASSENGER DOOR (L1) PORTABLE EMERGENCY LIGHT WOULD NOT EXTINGUISH. LAS VEGAS MAINTENANCE REMOVED AND REPLACED THE PORTABLE LIGHT ASSY AT THE L1 DOOR. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT MAINTENANCE SERVICE CHECK LAS VEGAS MAINTENANCE REPORTED THAT THE ELECTROLUMINESCENT EGRESS PATH LIGHTING WOULD NOT TEST BETWEEN ROWS 21 AND 24. FURTHER REPORT THAT TIGHTENED THE ELECTROLUMINESCENT STRIP ELECTRICAL CONNECTION. A SATISFACTORY OPERATIONAL TEST WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE.

Part: BATTERY — SEPARATED (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT MAINTENANCE SERVICE CHECK LAS VEGAS MAINTENANCE REPORTED THAT THE FORWARD OVERWING HATCH EXIT SIGNS WOULD NOT TEST. FURTHER REPORT THAT THE BATTERY HAD BECOME PARTIALLY DISMOUNTED FROM THE POWER SUPPLY. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE.

Part: SKIN — GOUGED (L1 DOOR)

FLIGHT 5184 IFP/SJC - DURING THE PRE-FLIGHT WALKAROUND A PILOT NOTICED WHAT APPEARED TO BE A GOUGE IN THE FUSELAGE ABOVE L1 MAIN PASSENGER DOOR. INVESTIGATION REVEALED SKIN DAMAGE BEGINNING APPROXIMATELY 24 INCHES ABOVE THE L1 DOOR AND CONTINUING LATERALLY ACROSS THE FUSELAGE APPROXIMATELY 10 INCHES WHERE THE GOUGE TERMINATED IN A PUNCTURE. THE DEPTH ATTAINED WAS APPROXIMATELY 1 INCH NEAR THE PUNCTURE. NO PRESSURIZATION, NOISE OR DRIPPING FLUID ISSUES HAVE BEEN REPORTED AGAINST THIS AIRPLANE SO DETERMINATION OF ORIGIN OF THE DAMAGE IS NOT POSSIBLE. THE AIRPLANE WAS FERRIED TO TULSA WHERE AMERICAN AIRLINES PERFORMED A TEMPORARY REPAIR APPROXIMATELY AT STATION 220, LONGERON 3L IN-ACCORDANCE-WITH AA ESO NR 805

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

LAS - MAINTENANCE FOUND THE OVERHEAD EMERGENCY LIGHT INOPERATIVE AT ROW 6. REMOVED AND REPLACED BULB AND OPERATIONALLY CHECKED GOOD IAW MM 33-50-00. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

LAS - MAINTENANCE FOUND THE EMERGENCY LIGHT INOPERATIVE AT ROW 8. REPLACED BULB FOR EMERGENCY LIGHT AT ROW 8 IAW MM 33-53-00. OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAS - MAINTENANCE FOUND THE EMERGENCY LIGHTS IN THE TAIL CONE AREA INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN THE TAIL CONE IAW MM 33-53-00. OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.