N297NV

ATA 5497

Part: WIRE HARNESS — DAMAGED (ZONE 400) · airframe 56,917 hrs · 19,606 cycles

(AIRCRAFT GROUNDED) (EMERGENCY DECLARED) THROUGHOT FLIGHT INTERMITENT ECAM EBG 1 THR LEVER DISAGREE / R/R ENGINE CONTROL UNIT (CHANNEL A) HARNESS IAW AMM 71-51-43-00-046-A, REMOVE AND AMM 71-51-43-400-046-A, INSTALL. R/R ENGINE CONTROL HARNESS UNIT (CHANNEL B) HARNESS IAW AMM 71-51-43-000-047A, REMOVE. AND AMM 71-51-43-400-047-A, INSTALL. REQUESTED BY TECH SUPPORT. REF 73-21-60-720-040-B FOR RII QC INSPEC TASKCARD. RII FOR ECU CONNECTORS VERFIED."

ATA 3350

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 53,590 hrs · 18,047 cycles

(AIRCRAFT NOT GROUNDED) L/H OVERWING EMERGENCY EXIT LIGHTS INOP / REMOVED AND REPLACED L/H MID CABIN EPSU BATTERY REF AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A OPS CHECK GOOD."

ATA 5330

Part: SKIN — CORRODED (NOT REPORTED) · airframe 52,138 hrs · 17,253 cycles

DURING THE INSPECTION ACCORDING TO ALLEGIANT WORK CARD: 532180-01-2-001, THE FASTENER HEADS OF THE EXISTING EXTERNAL DOUBLERS WERE FOUND WITH CORROSION AND AFTER REMOVAL WERE FOUND ELONGATED HOLES. AIRBUS PROVIDED REPAIR INSTRUCTIONS AND THE CORRODED AREA WAS REPAIRED FOLLOWING AIRBUS REPAIR INSTRUCTIONS UNDER DOSSIER 81375337 AS PER COOPESA ENGINEERING ORDER COO-EO-2024-19775 REV. 01 AND ALLEGIANT ERO R5321-0042 REV. 00. THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1P107 NRI 1-46.

ATA 5311

Part: FRAME — CRACKED (FRM 68) · airframe 52,138 hrs · 17,253 cycles

DURING THE ACCOMPLISHMENT OF ALLEGIANT TASK 53-260-003 RELATED TO AD2022-22-04 AT FR68RH STOP FITTING # 1 IT WAS FOUND A FASTENER HOLE WITH CRACK INDICATION IN THE FRAME ONLY. AIRBUS PROVIDED REPAIR INSTRUCTIONS AND FR68RH HOLE WAS REPAIRED FOLLOWING AIRBUS REPAIR INSTRUCTIONS UNDER DOSSIER 81371492 AS PER COOPESA ENGINEERING ORDER COO-EO-2024-19685-R01 AND ALLEGIANT ERO R5341-0125-R00.THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1P107 NRI 2-53.

ATA 5311

Part: FRAME — DAMAGED (FRM 66) · airframe 52,618 hrs · 33,351 cycles

DURING THE ACCOMPLISHMENT OF ALLEGIANT TASK 53-260-002 AT FR66LH STOP FITTING # 7 WITH OUTBOARD HOLES ELONGATED WERE FOUND.AIRBUS WAS CONTACTED ASKING REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS AND FR66LH HOLES WERE REPAIRED FOLLOW THE REPAIR INSTRUCTIONS AS PER COOPESA ENGINEERING ORDER COO-EO-2024-19619-R00 .AND ALLEGIANT ERO R5341-0123-R00.THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1P009 NRI 2-8.

ATA 3350

Part: EPSU — NO TEST (EMERGENCY LIGHTS) · airframe 52,072 hrs · 17,227 cycles

EXTERIOR LTS FAULT ON EPSU DURING EPSU SYS TEST- FOUND ON WEEKLY T/C / REMOVED AND REPLACED 13WL EPSU IAW AMM 33-51-38 PB 401. OPS CHECK GOOD. NO DEFECTS NOTED."

ATA 5311

Part: FRAME — DAMAGED (FRM 47 S1-2R) · airframe 46,693 hrs · 14,765 cycles

DURING DE-MOD OF THE GOGO 2KU SYSTEM, AN ELONGATED HOLE MEASURING 0.305" L X 0.300" W WAS LOCATED AT FRAME 47 BETWEEN STRINGERS 1R AND 2R. PER DRAWING DG211-9932-01, THE FRAME WAS INTENDED TO HAVE A #5 FASTENER AT THE LOCATION NOTED. THE FINAL HOLE SIZE PRIOR TO INSTALLATION IT 0.309".

ATA 3350

Part: EPSU — INOPERATIVE · airframe 48,533 hrs · 15,609 cycles

EPSU BATT FAULT INDICATED / REMOVED AND REPLACED FWD L EPSU UNIT IAW AMM 33-51-38 PB 401. COMPLETED OPS CHECK. NO FAULTS FOUND AT THIS TIME."

ATA 3350

Part: EPSU — FAILED INSP · airframe 48,395 hrs · 15,545 cycles

OPERATINAL TEST OF THE EMERGENCY LIGHTS FAIL. / EPSU BATTERIES REMOVED AND REPLACED IAW AMM 33-51-38-860-060-F AND AMM 33-51-38-400-002-A, PERFORMED EMERGENCY LIGHT OPERATINAL CHECK, OPS CHECKED GOOD."

ATA 3350

Part: EPSU — FAILED (10WL) · airframe 47,368 hrs · 15,106 cycles

PERFORM EPSU BIT CH 10WL BATT FAIL. / REMOVED AND REPLACED BATTERY 10WL. OPS CHECKS GOOD REF. AMM 33-51-38 P/B 401."

ATA 3350

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 46,694 hrs · 14,765 cycles

N0019 DURING PREDEPARTURE CHECK FOUND THE EMERGENCY POWER SUPPLY UNIT IS INOP / REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY AT LOCATION 11WL IAW A320 AMM 33-51-38"