N880GA

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,441 hrs · 35,756 cycles

EMERGENCY EXIT SIGN LIGHTS AT ROW 25 REMAIN ILLUMINATED WITH EMER LIGHT SWITCH OFF. R & R BATTERIES FOR ROW 25 EMER LIGHT SIGNS IAW MM 33-53-01. OPERATIONS CHECKED NORMAL.

Part: CUSP WEB — CORRODED (FUSELAGE)

CABIN CUSP WEB AT STATION 368 - 389 RBL 56 HAS CORROSION IN MULTIPLES AREAS. REMOVED DAMAGE FROM CUSP WEB & FABRICATED, DOUBLER, FILLERS, LOCATED, DRILLED & INSTALLED IAW SRM 53-05 FIG 131-21.

Part: DOUBLER — CRACKED (FUSELAGE)

DURING TAIL CONE RELEASE CHECK NOTED CRACK ON REPAIR DOUBLER AT CANTED FRAME 1485, RT LONGERON 3 - 4. REMOVED CRACKED REPAIR AT CANTED FRAME 1485, RT LONGERON 3 - 4 & INSTALLED NEW DOUBLER IAW SRM 53-01 FIG 2 SHEET 3 PG12, 53-14-4 FIG 3 & 51-10-4.

Part: SKIN — DENTED (CARGO DOOR)

FORWARD CARGO DOOR HAS MULTIPLE DENTS ALONG LOWER EDGE. REPAIRED FWD CARGO DOOR LOWER EDGE IAW SRM 52-05 FIG 67.

Part: TEE FITTING — CRACKED (FUSELAGE)

TEE ON CABIN FLOOR FRAME LBL 22 AT FS 905 IS CRACKED. R & R DAMAGED TEE ON CABIN FLOOR FS 905 & LBL 22 IAW SRM 51-01 PARAGRAPH 2 D.

Part: SKIN — DENTED (CARGO DOOR)

FORWARD CARGO DOOR SKIN IS DENTED AT FWD EDGE APPROXIMATELY 14 INCHES FROM THE BOTTOM. CUTOUT DAMAGED AREA, FABRICATED REPAIR DOUBLER, FILLER & INSTALLED REPAIR PARTS IAW SRM 52-05 FIG 67.

Part: FORMER — CRACKED (FUSELAGE)

OUTER SKIN TO FUSELAGE CLIP AT STATION 769 JUST BELOW LONGERON 10 APPEARS TO BE CRACKED IN UPPER CORNER. REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS & INSTALLED REPAIR PARTS IAW SRM 53-03 FIG 44.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. R & R BATTERY PACK AND OPS CHECKED IAW AMM 33-50-00, SYSTEM OPS CHECKED NORMAL. ACFT RETURNED TO SERVICE.

Part: SKIN — DENTED (ELEVATOR TAB)

LEFT ELEVATOR CONTROL TAB UPPER SURFACE HAS HAIL DAMAGE MULTIPLE PLACES. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR PARTS IAW MD80 SRM 51-70-2.

Part: SKIN — DENTED (ELEVATOR TAB)

RIGHT ELEVATOR CONTROL TAB UPPER SURFACE HAS HAIL DAMAGE MULTIPLE PLACES. FABRICATE DOUBLER'S & FILLER. INSTALLED REPAIR IAW MD80 SRM 51-70-2.

Part: SKIN — DENTED (ELEVATOR TAB)

RIGHTT ELEVATOR GEAR TAB UPPER SURFACE HAS HAIL DAMAGE MULTIPLE PLACES. FABRICATED REPAIR DOUBLER & FILLER. INSTALLED REPAIR PARTS IAW MD80 SRM 51-70-2.

Part: SKIN — DENTED (ELEVATOR TAB)

RIGHT ELEVATOR ANTI-FLOAT TAB UPPER SURFACE HAS HAIL DAMAGE MULTIPLE PLACES. FABRICATE REPAIR DOUBLER & FILLER. INSTALLED REPAIR PARTS IAW MD80 SRM 51-70-2.

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 — 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: ENGINE — MALFUNCTIONED (RIGHT)

FLIGHT DECK PERSONNEL REPORTED EN ROUTE, RIGHT AC CROSSTIE LOCK OUT LIGHT ILLUMINATED. RIGHT AC ELECTRICAL FAILURE, PER QRH CONTINUED, APPROXIMATELY 20 MINUTES LATER, RIGHT ENGINE FIRE INDICATION, PER QRH SECURED RIGHT ENGINE AND LANDED AT NEAREST SUITABLE AIRPORT. EMERGENCY EVACUATION. MAINTENANCE DEPARTMENT PERSONNEL REMOVED AND REPLACED THE RIGHT ENGINE IAW ALLEGIANT AIR TASK CARD R0807101. AIRCRAFT RETURNED TO SERVICE.

Part: BEAM — CORRODED (ZONE 100)

WHILE IN WORK AT MAINTENANCE BASE. BOW 1C/2C/S1, FOUND AFT CARGO DOOR BEAM CORRODED STA 1170. ADDRESSED AS REQUIRED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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: 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 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: BATTERY PACK — DISCHARGED (CABIN)

IT HAS BEEN REPORTED BY THE FLIGHT CREW, THE FORWARD RIGHT AND LEFT CABIN DOOR "EXIT" EMERGENCY EVACUATION LIGHT WAS FOUND TO BE INOPERATIVE. 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 (EMERGENCY LIGHTS)

DURING A PREFLIGHT INSPECTION FLIGHT CREW REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WAS INOP THE FIRST THREE METERS. 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: RETAINER — BROKEN (ESCAPE SLIDE)

FLIGHT 9880 FAT/LAS - FLIGHT CREW REPORTED THAT THE MAIN PASSENGER ENTRY DOOR (L1) ESCAPE SLIDE NEEDS TO BE RE-ATTACHED TO THE DOOR. LAS MAINTENANCE REPORT THE REMOVAL AND REPLACEMENT OF A RETAINING CLIP AT L1 DOOR AND THE RE-MOUNTING OF THE ESCAPE SLIDE PER AMM 25-62-00. THE AIRPLANE HAS RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK MAINTENANCE INSPECTION. MAINTENANCE REPORTED THAT THE EMERGENCY EGRESS PATH LIGHTING FROM ROW 25 TO ROW 32 WOULD NOT TEST. MAINTENANCE FURTHER REPORT THE REMOVAL AND REPLACEMENT OF AN EMERGENCY LIGHT POWER SUPPLY BATTERY PACK AT ROW 26 OVERHEAD. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE.