N296NV

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 54,375 hrs · 18,964 cycles

(AIRCRAFT NOT GROUNDED) FAIL THE BATTERY CAPACITY CHECK. REMOVED AND REPLACED EPSU REF WO533018"

Part: PACKING — LEAKING (APU OIL SYS) · airframe 53,167 hrs · 18,413 cycles

(AIRCRAFT NOT GROUNDED) FA'S REPORT MUSTY ODOR AT ROWS 18-23 IN CRUISE AND ON DESCENT. ACCOMPLISHED TASK CARD 21-000-002. DURING 21-000-002 TASK CARD FOUND OIL SEEPING FROM APU OIL COOLER TRANSFER TUBES FWD CONNECTIONS. REMOVED AND REPLACED PACKINGS FOR APU OIL COOLER TRANSFER TUBES FWD CONNECTION IAW AMM 49-91-44-000-802-A AND 49-91-44-400-802-A. OPS CHECK AND LEAK CHECK GOOD. COMPLETED TASK CARD 21-000-003.

Part: WIRE — CHAFED (ZONE 100) · airframe 51,959 hrs · 17,782 cycles

(AIRCRAFT NOT GROUNDED) (DISCREPANCY NOTED DURING AIRCRAFT HEAVY MX VISIT) NRC 2000-0053: PASSENGER COMPARTMENT, AFT PRESSURE BULKHEAD, ELECTRICAL WIRES CAHFING. / APU FEEDER CABLE FROM CABIN TERMINAL BLOCK 2996VT TO APU GENERATOR AND STARTER. MOTOR AND TERMINAL BLOCK 7508VT REPLACED IAW ESPM 20-33-42-0I, 20-44-52-01 AND AMM 24-23-51-400-00J-A, 49-42-51-400-006-A. SEE AWS FOR DETAILS."

Part: EPSU — FAILED (EMERGENCY LIGHTS) · airframe 51,391 hrs · 17,445 cycles

(AIRCRAFT NOT GROUNDED) FOUND ESPU BATT 10WL BAD / REMOVED AND REPLACED ESPU BATT 10WL IAW AMM 33-51-38-000-002 AND 33-51-38-400-002. OPS CK GOOD. NO DEFECTS NOTED."

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 50,449 hrs · 16,936 cycles

(EMERGENCY DECLARED) ON TAKEOFF AND LANDING GEAR WAS VERY SLOW TO CYCLE TRIGGERING ECAM ALERTS. GEAR AND DOORS EVENTUALLY WENT TO CORRECT POSITIONS / PERFORMED T/S PER TSM 32-31-00-810-898-A, FOUND R/H MAIN GEAR DOOR CABLE BROKEN, SEE NR 1270294 FOR REMOVAL AND REPLACEMENT OF CABLE. WITH OPS CHECK OF DOOR, PER AMM 32-12-00-710-002-A, PERFORMED FUNCTIONAL TEST OF THE NORMAL EXTENSION AND RETRACTION SYSTEM, TEST GOOD, TIME WITHIN LIMITS, NO FAULTS NOTED PER AMM 32-31-00-720-002-A. A/C OK FOR SERVICE"

Part: EPSU — UNKNOWN (UNKNOWN) · airframe 50,159 hrs · 16,809 cycles

FAILED EMERGENCY LIGHT TEST / REPLACED EPSU BATTERY IAW AMM 33-51-38-400-002-A. OPERATION CHECK GOOD AT THIS TIME."

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,837 hrs · 16,663 cycles

FA REPORTS FWD MEGAPHONE INOP / R & R BATTERIES WITH NEW IN FWD MEGAPHONE W/REF TO AMM:25-65-51-920-001-A. OPS CHECK GOOD, NO OTHERDISCREPANCIES FOUND AT THIS TIME."

Part: SWITCH — OUT OF TOLERANCE (ZONE 100) · airframe 49,788 hrs · 16,641 cycles

DURING PASSENGER OXYGEN SYSTEM FUNCTIONAL CHECK IAW ALLEGIANT TASK 352000-02-1-001 OF AUTOMATIC MASK RELEASE FOUND ALTITUDE SWITCH OUT OF LIMITS. DUE THIS CONDITION THE ALTITUDE SWITCH WAS REPALCED IAW A320 AMMTASK 35-23-15-000-001-A AND 35-23-15-400-001-A REV 40 DATED 05-01-2023. AFTER THE SYSTEM TEST WAS FOUND OK. THIS WORK IS COVERED BY COOPESA JOB A1N150 ITEM 1-23 P/N OFF 4441085-000 S/N OFF 02102 P/N ON 4441085-000 S/N ON 42085-000-05465,

Part: BEAM — CORRODED (ZONE 200) · airframe 49,788 hrs · 16,641 cycles

DURING ALLEGIANT TASK 534143-01-1 INSPECTION UPPER FUSELAGE AFT ENTRY CABIN WET AREA AT FR66 +Y1580 GIRT BAR FITTING AREA WITH CORROSION WAS FOUND.THE LH DOOR SILL BEAM AT FR66 DAMAGE WAS REPAIRED IAW A320 SRM 53-41-14-300-001 PARAG 2A FIG 001 REPAIR PRINCIPLE II. THE REPAIR IS COVERED WITH COOPESA JOB A1N150 ITEM 2-41.

Part: STRINGER — CORRODED (ZONE 100) · airframe 49,788 hrs · 16,641 cycles

DURING ALLEGIANT TASK 532180-01-2 INSPECTION LOWER FUSELAGE FWD CARGO COMPARTMENT BETWEEN FR33 AND FR34 STGR 44 WITH CORROSION WAS FOUND.THE DAMAGE WAS REPAIRED IAW A320 SRM 53-21-13-300-018 PARAG 2 FIG 001. THE REPAIR IS COVERED WITH COOPESA JOB A1N150 ITEM 1-21.

Part: BEAM — CORRODED (ZONE 200) · airframe 49,788 hrs · 16,641 cycles

DURING ALLEGIANT TASK 534143-01-1 INSPECTION UPPER FUSELAGE AFT RH ENTRY CABIN WET AREA AT FR66 AND FR68 Y-1580 GIRT BAR FITTING AREA AND LOWER SILL WITH CORROSION WAS FOUND.THE RH DOOR SILL BEAM AT FR66 DAMAGE WAS REPAIRED IAW A320 SRM 53-41-14-300-001 PARAG 2A FIG 001 REPAIR PRINCIPLE II AND 8.THE REPAIR IS COVERED WITH COOPESA JOB A1N150 ITEM 2-42.

Part: EPSU — UNKNOWN (UNKNOWN) · airframe 49,498 hrs · 16,487 cycles

CABIN EMERGENCY LIGHT CAPACITANCE TEST FAILED / REMOVED AND REPLACED ALL 4 CABIN EMERGENCY LIGHT BATTERIES. OPS CHECK GOOD. REF. AMM 33-51-38-400-002-A"

Part: SKIN — DAMAGED (FRMS 49-50 S1-2L) · airframe 45,228 hrs · 14,383 cycles

WHILE REMOVING THE DOUBLER AND TRIPLER FROM INTERNAL SKIN BETWEEN FRAMES 49 AND 50, AT STRINGER L1 AND L2, 5EA. FASTENER HOLES WERE FOUND TO BE ELONGATED.

Part: PANEL — MISSING · airframe 46,940 hrs · 15,182 cycles

LOWER EXIT PANEL AT L1 DOOR COMING OFF AND IS MISSING A SCREW / REINST LOWER EMERG EXIT PANEL AT L1 DOOR AND REPLACED MISSING SCREW IAW AMM 25-23-45"

Part: EPSU — FAILED (13WL) · airframe 46,324 hrs · 14,921 cycles

DURING CABIN EMERGENCY LIGHTING TEST AFT LEFT BATTERY (13WL) FAILED / REMOVED AND REPLACED AFT LEFT BATTERY 13WL IAW AMM 33-51-38"

Part: LINE — LEAKING (HYD SYSTEM) · airframe 45,329 hrs · 14,427 cycles

AT CRUISE HYD G RSVR LO LVL. / FOUND HYDRAULIC LINE 642-5658-503 CHAFFED ON THE #1 ENGINE. LINE IS CURRENTLY BEING REPLACED."

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 45,233 hrs · 14,383 cycles

L-1 CABIN EMERGENCY EXIT LIGHTING BATTERY FAILED OPS CHECK REQUIRES REPLACEMENT / REMOVED AND REPLACED L-1 CABIN EMERG EXIT LIGHTING BATTERY IAW AMM 33-51-38, OPS CHECKED IAW AMM 33-51-00"