N872GA

Part: WARNING HORN — FALSE ACTIVATION (MLG) · airframe 50,368 hrs · 41,050 cycles

GEAR HORN WOULD NOT STOP GOING OFF. EMERGENCY DECLARED. OPS CHECKED LANDING GEAR AURAL WARNING, NO DEFECTS NOTED.

Part: STIFFENER — CRACKED (VERTICAL ASTB) · airframe 49,427 hrs · 40,548 cycles

RT VERTICAL SKIN STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER IAW SRM 51-10-4, 51-10-2, AND 51-30-2.

Part: PAN — CRACKED (FUSELAGE) · airframe 49,427 hrs · 40,548 cycles

PASSENGER CABIN RT WINDOW PAN CRACKED AT UPPER FWD FLANGE. REPAIRED WINDOW PAN FLANGE IAW SRM 53-05 FIG 122.

Part: PAN — CRACKED (FUSELAGE) · airframe 49,427 hrs · 40,548 cycles

PASSENGER CABIN LT WINDOW PAN CRACKED AT UPPER FWD FLANGE. REPAIRED WINDOW PAN IAW SRM 53-05 FIG 122.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 49,427 hrs · 40,548 cycles

VERTICAL STAB DORSAL LT RIB 3RD DOWN FROM TOP CRACKED. REPAIRED VERTICAL STAB DORSAL RIB IAW MD80 SRM 55-02 FIG 27.

Part: PAN — CRACKED (FUSELAGE) · airframe 49,427 hrs · 40,548 cycles

PASSENGER CABIN RT WINDOW PAN CRACKED AT LOWER FWD FLANGE. REPAIRED WINDOW PAN IAW SRM 53-05 FIG 122.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 49,427 hrs · 40,548 cycles

AFT VENTRAL CEILING SUPPORT CRACKED IN 2 PLACES. REMOVED AND REPLACED CEILING SUPPORT IAW SRM 51-30-2.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 49,427 hrs · 40,584 cycles

AFT SIDE OF FRAME AT BS 1309, LONGERON 30 HAS CORROSION. REPAIRED THE FRAME IAW SRM 53-03 FIG. 2A SH. 3 VIEW Q AND FIG. 2A SH. 5

Part: STEP — CRACKED (STAIR) · airframe 49,427 hrs · 40,548 cycles

AFT VENTRAL STAIR LOWER FOLDING STEP LEFT LOWER DOUBLER IS CRACKED. REMOVED THE DOUBLER, FABRICATED A REPLACEMT AND INSTALLED IAW SRM 52-05, FIG. 62

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,153 hrs · 39,853 cycles

RIGHT STATIC PORT SKIN PLATE DAMAGED ON AIRFRAME SIDE. REPAIR FOR FUSELAGE SKIN DAMAGE FS 598 - 617, LONGERON 24R - 25R AT STATIC PORT, CUT OUT ACCOMPLISHED IAW WO 919-03-2006 FOR ALL WORK DETAILS PERFORMED.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHT AT 3 DEF INOPERATIVE. R & R BATTERY IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 47,606 hrs · 39,573 cycles

FORWARD GALLEY JUMP SEAT FLASHLIGHT INOPERATIVE. R & R FWD EMER FLASHLIGHT IAW AMM 25-60-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

FOUND 14 EMER LIGHTS IN CABIN BURNED OUT. RELAMPED 14 CABIN EMER LIGHTS IAW AMM 33-50-02. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 46,428 hrs · 38,972 cycles

AFT OVERWING EMER LIGHTS ARE OUT. REPLACED BATTERIES FOR POWER SUPPLY. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 46,360 hrs · 38,940 cycles

ONE FLASHLIGHT ON FWD FLIGHT ATTENDANT STATION BROKEN. R & R FLASHLIGHT IAW AMM 25-60-00. OPERATIONS CHECKED GOOD.

Part: PROXIMITY SENSOR — FAULTY (NLG) · airframe 46,294 hrs · 38,906 cycles

RED NOSE GEAR LIGHT ILLUMINATED WITH THE GEAR HANDLE UP. PERFORMED QRH & LIGHT WENT OUT. R & R NOSE GEAR LOCKED PROX SENSOR D1-32 IAW AMM 32-60-05. REF LOG PAGE 499437 FOR OPERATIONS CHECK. ACFT AOG UNTIL 01/15/2015.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 46,262 hrs · 38,890 cycles

RED NOSE GEAR LIGHT ON WITH GEAR HANDLE UP AFTER TAKEOFF. CYCLED GEAR & THE LIGHT WENT OUT IAW QRH 32.9 & IAW AMM 32-60-05. INSPECTED BOTH UP & DOWN PROX SENSORS FOR SECURITY & FOUND NORMAL. CLEANED & INSPECTED GAPS BETWEEN TARGET & SENSORS, ALL FOUND NORMAL. PERFORMED PSEU TEST ON ALL GEAR SENSORS & NO FAULTS FOUND. NO HISTORY IN AIS. ALL GEAR INDICATIONS FOUND NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,173 hrs · 38,849 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,131 hrs · 38,831 cycles

EMERGENCY LIGHTS AT L1 DOOR INOPERATIVE. R & R BULB IAW MM 33-53-00. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: BLEED VALVE — MALFUNCTIONED (RT ENGINE)

AFTER TAKEOFF AT 800 ALT, RT ENG SURGED AGGRESSIVELY A LOUD BAND WAS HEARD & ENG EPR DECREASED FROM 1.92 TO 1.4. EXECUTED QRH 72.8 COMPRESSOR STALL. ENG REMAINED RUNNING & RETURNED TO FIELD AS A PRECAUTION. TAKEOFF PARAMETERS RT ENG -1.92 EPR, 90.6 N1, 622 EGT, 97% N2 & 10980 FF OAT 23.6. R & R PRBC IAW AMM 75-31-01. R & R SBCV IAW AMM 75-31-04. ENG CONTINUES TO COMPRESSOR STALL. REF LOG PAGE 520575 FOR CONTINUED TROUBLESHOOTING. MORE DETAILS TO BE ENTERED WITH PN ABOUT FINAL ROOT CAUSE, CORRECTIVE ACTION & PNS.

Part: LIGHT — INOPERATIVE (CABIN)

ROW 15 OVERHEAD EMER LIGHT INOPERATIVE. RELAMPED ROW 15 OVERHEAD EMER LIGHT IAW AMM 33-53-01. OPERATIONS CHECKED GOOD.

Part: BEAM — CORRODED (CARGO BAY)

AFT CARGO DOOR LOWER BEAM CORRODED STATION 1155 TO 1212. REMOVED DAMAGED AREA & INSTALLED REPAIR DOUBLER IAW SRM 53-05 & STS EA 10-2014-024.

Part: SKIN PANEL — DAMAGED (FUSELAGE)

INTERIM REPAIR DOUBLER INSTALLED AT FS 1205, L28L - L28R ID 36 TO BE R & R WITH A PERMANENT REPAIR AT NEXT C CHECK. COMPLIED WITH PERMANENT REPAIR IAW ERO 5334-006A BELLY SKIN SPLICE, L26L TO L26R FROM STATION 1138.5 TO STATION 1279 ACCOMPLISHED, EMLA 5334406901A L26L & L26R FINGER DOUBLER TRIM ACCOMPLISHED & EMLA 5443406201 EXTERIOR PRODUCTION DOOR DOUBLER ACCOMPLISHED.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY OVERWING LIGHTS INOPERATIVE. R & R OVERWING POWER SUPPLY & OPERATIONS CHECKED GOOD IAW AMM 33-53-00.

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 AT ROW 25. 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: SKIN — CHAFED (TE FLAP)

RIGHT O/B FLAP I/B VANE LEADING EDGE IS CHAFED AT I/B CORNER, 193A029 MARKED. REMOVED RIGHT WING O/B FLAP I/B FLAP VANE AND REPAIRED AREA, RE-INSTALLED AND C/W CLEARENCE CHECKS.

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 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 — 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 POWER SUPPLY BATTERY PACK AND OPS CHECK ACCOMPLISHED PER AMM 33-50-00, OPS CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — DAMAGED (CABIN)

ROW 6 A-C THRU 8 A-C LOWER SIDEWALL LIGHTS INOP. REPAIRED WIRING BEHIND OVERHEAD BIN ROW 7 LEFT IAW SWPM 20-10-01. OPS CHECK 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: 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: COALESCER BAG — DIRTY (AC BAY)

F/A'S REPORTED BURNING RUBBER SMELL ON DESCENT, STRONGER AFT. DISSIPATED PRIOR TO LANDING. INSPECTED AIRCRAFT, REPLACED WATER SEPARATOR BAGS AND OPS CHECK GOOD IAW 21-20-02. AIRCRAFT OK FOR SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE)

MAIN CABIN SEAT TRACK HAS CORROSION AND SCRATCHED AT RBL 22 STA 200 TO 446 MKD. REMOVED CORROSION AND SCRATCHES STA 266 TO 446, RBL 22 IAW MD80 SRM 51-10-3. TREATED, PRIMED AND TOPCOATED. REMOVED AND REPLACED SEAT TRACK SECTION STA 200 TO 266 PER MD80 SRM 51-30-1.

Part: SEAT TRACK — CORRODED (FUSELAGE)

MAIN CABIN SEAT TRACK HAS CORROSION AT RBL STA 200-237 MKD. REMOVED CORROSION AT MAIN CABIN SEAT TRACK STA 200-237 RBL 44 IAW MD80 SRM 51-10-3. ORGINIAL MATERIAL 115 MATERIAL LOSS .053 FOUND OUT OF LIMITS IAW MD80 SRM 53-05 FIG 4-8-1. REMOVED AND REPLACED SEAT TRACK IAW MD80 SRM 51-30-01 AND 53-05 FIG 4 F.

Part: SEAT TRACK — CORRODED (FUSELAGE)

SEAT TRACK AT STA 226 CORRODED. REMOVED AND REPLACED NEW SEAT TRACK SECTION AT MAIN CABIN LBL 22 FROM STA 200 TO STA 304.5 IAW EA 05-2011-136 AND MD80 SRM 51-30-1 AND 53-05.

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: APU — MALFUNCTIONED (TAIL)

FLIGHT CREW PERSONNEL REPORTED DURING TAXI FROM GA RAMP TO THE D GATES IN LAS VEGAS THE LAV SMOKE ALARM WENT OFF AND THE FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE APU IAW TACK CARD R0594902, LEAK AND OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (LEFT)

FLIGHT CREW REPORTED SMOKE IN THE CABIN AND IMMEDIATELY RETURNED TO LAS VEGAS. MAINTENANCE PERSONNEL INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LEFT ENGINE IAW TASK CARD R804101, OPS AND LEAK CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (SMOKE DETECTION)

FLIGHT CREW REPORTED AFTER TAKEOFF FORWARD AND AFT LAV SMOKE DETECTOR ALARMS ANNUNCIATED. FLIGHT ATTENDANT REPORTED NO SMOKE OR FIRE. AIRCRAFT RETURN TO BASE AND MAINTENANCE DEPARTMENT PERSONNEL INSPECTED AND REPALCED SMOKE CONTROL AND REPAIRED CONNECTOR PINS. AIRCRAFT RETURNED TO SERVICE.

Part: LINE — LEAKING (WATER SEPARATOR)

FLIGHT CREW REPORTED BURNING RUBBER ODOR COMING FROM NOSEWHEEL DURING TAKEOFF AND CLIMB-OUT. ODOR WAS THROUGHOUT ENTIRE CABIN. AIRCRAFT RETURNED TO THE AIRPORT OF ORIGIN WITHOUT INCIDENT. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED ALL AIRCRAFT TIRES FOR CONDITION AND PRESSURE. NO DEFECTS NOTED. INSPECTION OF LT AND RT AIR CONDITIONING SYSTEMS FOUND HOLE IN LT PACK WATER SEPARATOR LINE, REPLACED LINE SYSTEM RETURN TO SERVICE CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK, INSPECTION REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINT REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED IAW AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE. (K)

Part: BATTERY — FAILED (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MX DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MX 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 ACFT HAS RETURNED TO SERVICE. (S)

Part: BATTERY — FAILED (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MX DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MX 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 ACFT HAS RETURNED TO SERVICE. (S)

Part: BATTERY PACK — FAILED (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. (A)

Part: UNKNOWN — ODOR (CABIN)

AFTER TAKEOFF HAD A BURNING OIL ODOR, THEN BOTH AFT LAVATORY SMOKE DETECTORS ALARMS WENT OFF. RETURNED TO LAS PER CONVERSATION WITH MAINTENANCE CONTROL PERSONNEL. LAS MAINTENANCE DEPARTMENT PERSONNEL PERFORMED HIGH POWER ENGINE GROUND RUNS, REFERENCE AMM 71-00-00. WITH ENGINES AT HIGH POWER, RAN AIRCRAFT AIR CONDITIONING PACKS LEFT AND RIGHT FOR 20 MINUTES, REFERENCE AMM 21-00-00. NO CABIN OR LAVATORY SMOKE NOTED, AIRCRAFT IS OK FOR SERVICE.

Part: WHEEL — FAILED (MLG)

UPON LANDING AT FAT, RIGHT OUTBOARD TIRE BLOWN OUT ON LANDING. AIRCRAFT PROCEEDED TO THE TERMINAL WITHOUT INCIDENT. INSPECTION BY MAINTENANCE DEPARTMENT PERSONNEL FOUND SEVERAL DISCREPANCIES ASSOCIATED WITH THE DESTRUCTION OF THE TIRE. BROKEN BRAKE LINES, ANTI-SKID VALVE, NR 4 BRAKE, WING FLAP BUTE DOORS AND DENTS IN THE RIGHT WING FLAP. AIRCRAFT WAS REPAIRED AND RELEASED FOR FERRY FLIGHT TO ALLEGIANT AIR CONTRACTED MAINTENANCE FACILITY FOR CONTINUED REPAIRS. THE AIRCRAFT WILL RETURN TO SERVICE UPON COMPLETION OF ALL REPAIRS.