N292NV

Part: BUTTON — NO TEST · airframe 34,681 hrs · 20,284 cycles

(AIRCRAFT NOT GROUNDED) EMERG BUTTON ON FAP NOT WORKING . NO AUDIBLE CHIMES WHEN PRESSED. / PERFORMED AMM 33-51-00-710-804-A OPERATIONAL CHECK OF MANUAL EMERGENCY LIGHTING ACTIVATION. NO DEFECTS . NO CHIMES ARE NORMAL OPERATION.

Part: EPSU — NO TEST (ZONE 200) · airframe 33,888 hrs · 19,930 cycles

(AIRCRAFT NOT GROUNDED) BATTERY FAIL EPSU CHECK / R/R EPSU REF WO510177"

Part: MODULE — INOPERATIVE (ZONE 200) · airframe 33,149 hrs · 19,587 cycles

(AIRCRAFT NOT GROUNDED) AFT GALLEY OXYGEN STORAGE MODULE INOP. / SWAPPED DAMAGED J-HOOK SUPPORTS WITH NEW PER CMM 35-22-25. REINSTALLED OXYGEN STORAGE MODULE (33WR) IAW AMM 35-21-41-400-001-A. OPS CHECK GOOD. THIS CLEARS MEL 35-21-01E, MDDR 200363. INOP PLACARDS REMOVED."

Part: MEGAPHONE — NO TEST (AFT CABIN) · airframe 32,698 hrs · 19,377 cycles

(AIRCRAFT NOT GROUNDED) REAR MEGAPHONE NO SIGNAL FEEDBACK / REMOVED & REPLACED AFT CABIN MEGAPHONE PER ALLEGIANT AIRLINES LOPA A2250013L03."

Part: EPSU — UNKNOWN (UNKNOWN) · airframe 30,998 hrs · 18,528 cycles

10WL,11WL,13WL EPSU FAILED EMERGENCY LIGHT TEST. BOTH BATTERIES FAULT / REMOVED AND REPLACED EPSU BATTERIES (10WL,11WL, 13WL) IAW AMM 33-51-38-000-001A AND 33-51-38-400-001A OPS CHECK GOOD"

Part: SLIDE — UNKNOWN (UNKNOWN) · airframe 30,873 hrs · 18,456 cycles

R1 DOOR EMERGENCY SLIDE RAFT DEPLOYED / REMOVED AND REPLACED RIGHT HAND ESCAPE SLIDE RAFT PACK ASSEMBLY IAW AMM 25-62-44-000-804-A AND AMM 25-62-44-400-803-A AND LOPA A2250013L03"

Part: STRINGER — CORRODED (ZONE 100) · airframe 30,560 hrs · 18,278 cycles

DURING ACCOMPLISHMENT ALLEGIANT TASK 532180-01-2-001 WAS FOUND A CORROSION ON LOWERFUSELAGE FWD CARGO COMPARTMENT AT FR33+230MM. PERMANENT REPAIR ON FWD CARGO COMPARTMENTSTGR 44LH OUTER FLANGE BETWEEN FR31-32 WAS PERFORMED IAW A320 SRM TASK 53-21-13-300-019 PARAG 2 FIG 001 SHEET 2. THIS REPAIR IS CLASSIED AS CATEGORY B.THE REPAIR WAS DOCUMENTEDUNDER COOPESA JOB A1N075 ITEM 1-82.

Part: STRINGER — CORRODED (ZONE 100) · airframe 30,560 hrs · 18,278 cycles

DURING ACCOMPLISHMENT ALLEGIANT TASK 532180-01-2-001 WAS FOUND A CORROSION ON LOWER FUSELAGE FWD CARGO COMPARTMENT AT FR31+280MM. PERMANENT REPAIR ON FWD CARGO COMPARTMENT STGR 44LH OUTER FLANGE BETWEEN FR31-32 WAS PERFORMED IAW A320 SRM TASK 53-21-13-300-019 PARAG 2 FIG 001 SHEET 2. THIS REPAIR IS CLASSIED AS CATEGORY B.THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1N075 ITEM 1-81.

Part: REINFORCEMENT — CORRODED (ZONE 100) · airframe 30,560 hrs · 18,278 cycles

DURING THE AIRCRAFT INSPECTION, IT WAS FOUND CORROSION ON REINFORCEMENT CASE TRAIN DOUBLER NLG BETWEEN FR20 - FR21 AND Y175 AND Y-175. DUE TO THE DAMAGE IS BEYOND SRM ADL LIMITS, AIRBUS WAS CONTACTED REQUESTING REPAIR INSTRUCTIONS AND FINAL APPROVAL .AIRBUS PROVIDED REPAIR INSTRUCTIONS UNDER TD TD/81206500/013/2023#B AND RDAF 81206500/004/2023#B.THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1N075 ( ITEM 1-70).

Part: SKIN — CORRODED (ZONE 500) · airframe 29,009 hrs · 17,557 cycles

DURING THE STRUCTURE INSPETION WAS FOUND IN THE LH WING TOP SKIN LOWER SURFACE OVERHANG AREA BETWEEN RIB 14 AND RIB 16 SKIN WITH CORROSION. DUE TO THIS FACT DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTUCTIONS AND FINAL APPROVAL. AFTER AIRBUS EVALUATION REPAIR INSTRUCTIONS WERE PROVEDED UNDER DOSSIER 81068684 THE REPAIR WAS HANDLED UNDER COOPESA JOB: A1M114 ITEM 5-29

Part: SKIN — CORRODED (ZONE 600) · airframe 29,009 hrs · 17,557 cycles

DURING TH ESTRUCTURE INSPECTION WAS FOUND IN THE RH WING FIXED T/E AREA BETWEEN RIBS 14-16 OVERHANG WITH CORROSION. DUE TO THIS FACT DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL. AFTER AIRBUS EVALUATION REPAIR INSTRUCTIOINS WERE PROVIDED UNDE DOSSIER 81068690 THE REPAIR WAS HANDLED UNDER COOPESA JOB: A1M114 ITEM 6-4

Part: BRACKET — CORRODED (ZONE 600) · airframe 29,009 hrs · 17,557 cycles

DURING TH ESTRUCTURE INSPECTION WAS FOUND IN THE RH WING FIXED T/E RIBS (3EA) WITH CORROSION BETWEEN WING RIBS 13-17. DUE TO THIS FACT THE BRACKETS P/N: D5754042720100 WERE REPLACED IAW A320 SRM 51-72-11-911-001 THE REPLACED WAS HANDLED UNDER COOPESA JOB: A1M114 ITEM 6-6

Part: BRACKET — CORRODED (ZONE 500) · corrosion level 2 · airframe 29,009 hrs · 17,557 cycles

DURING INSPECTION LEFT WING TRAILING EDGE CAVITY RIBS (3EA) BETWEEN WING RIB 15 AND 19 WITH CORROSION WAS FOUND. THE BRACKET P/N D5754042720000 WAS REPLACED IAW A320 SRM 51-72-11-911-001 REV 141 DATED 05/01/2022. THIS REPLACEMENT IS CAPTURED IN COOPESA NON ROUTINE JOB A1M114 ITEM 5-20.

Part: EPSU — NONE · airframe 29,446 hrs · 17,756 cycles

EPSU BATTERY TEST FAILURE AT 12WL. / REMOVED AND REPLACED EPSU BATTERY AT 12WL IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A. PERFORMED EPSU BITE CHECK, OPS CHECK GOOD IAW AMM 33-51-00-710-001."

Part: LIGHT — INOPERATIVE · airframe 29,288 hrs · 17,685 cycles

L1 DOOR EMERGANCY LIGHT COVER IS BROKEN / R&R L1 DOOR EMERGENCY LEN COVER IAW AMM 33-51-06 OPS CHKS GOOD"

Part: EPSU — FAILED · airframe 29,105 hrs · 17,599 cycles

EPSU AT 12WL BAD / INSTALLED EPSU AT 12WL IAW AMM 33-51-38-400-001-A OPPS CK GOOD TEST GOOD"

Part: NONE — NONE · airframe 29,105 hrs · 17,599 cycles

(EMERGENCY DECLARED) AFTER TO NOSE LANDING GEAR DID NOT RETRACT. FOLLOWED ECAM ACTION. DID NOT FIXED THE PROBLEM. DID NOT EXCEED 220 KTS. FELT THE DRAG FROM A GEAR AND DOORS. FOLLOWED FCOM FOR OVERWEIGHT LANDING. TOUCHDOWN @100FT/MIN. LANDING WEIGHT 154.8 / REF W/O 459021-1 FOR REMOVAL AND REPLACEMENT OF NOSE LANDING GEAR ACTUATING CYLINDER PER AMM 32-31-22-000-001 AND AMM 32-31-22-400-001. PERFORMED 10 SUCCESSFUL GEAR UP CYCLES PER AMM 32-31-00-720-002A. REF NON-ROUTINE FOR OVERWEIGHT LANDING INSPECTION COMPLIED WITH. AIRCRAFT OK FOR RETURN TO SERVICE."

Part: SKIN — CORRODED · airframe 29,009 hrs · 17,557 cycles

DURING THE INSPECTION ACCOMPLISHMENT PER ALLEGIANT WORK CARD Nº: ZL-575-01-1-001 IT WAS FOUND THE RIBLET E CORRODED. DUE TO THIS FACT IT WILL BE REPLACED BY NEW ONE, DUE TO FLY BY WIRE CABLES PASS THROUGH THE MENTIONED RIBLET E AND A HOLE COMMON TO THE REBLET E WAS FOUND ELONGATED, DETAILS, WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL, UNDER AIRBUS DOSSIER 81065802

Part: SKIN PANEL — CORRODED (ZONE 600) · airframe 29,009 hrs · 17,557 cycles

DURING THE STRUCTURAL INSPECTION PER TASK CARD Nº: 572062-01-1-002 MPD, IT WAS FOUND AT RH WING, T/E FALSE REAR SPAR OVERHANG AREA BETWEEN RIB 6 AND RIB 7, RIB 15, RIB 21 AND RIB 22 OVERHANG TOP SKIN LOWER SURFACE WITH CORROSION. THE RESULTING BLEND OUTS AFTER CORROSION REMOVAL WERE FOUND OUT OF THE SRM LIMITS. DUE TO THIS FACT, DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL, UNDER AIRBUS DOSSIER 81068690.

Part: HINGE FITTING — CRACKED (ZONE 100) · airframe 29,009 hrs · 17,557 cycles

DURING THE STRUCTURAL INSPECTION PER TASK CARD Nº: 323300-05-2-001_P1-OP-CK/0, IT WAS FOUND AT LOWER FUSELAGE NLG LH DOOR HINGE FITTING UPPER SECTION CRACKED. . DUE TO THIS FACT THE HINGE P/N D5392538120000 WAS REPLACED I/A/W A320 SRM 51-72-11-911-001, AND AIRBUS DRAWING D53926173

Part: SKIN PANEL — CORRODED (ZONE 500) · airframe 29,009 hrs · 17,557 cycles

DURING THE STRUCTURAL INSPECTION PER TASK CARD Nº: 572062-01-1-001 MPD, IT WAS FOUND AT LH WING, T/E FALSE REAR SPAR OVERHANG AREA BETWEEN RIB 6 AND RIB 7 OVERHANG TOP SKIN LOWER SURFACE WITH CORROSION. THE RESULTING BLEND OUT AFTER CORROSION REMOVAL WAS FOUND OUT OF THE SRM LIMITS. DUE TO THIS FACT, DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL

Part: EPSU — FAILED INSP (13WL) · airframe 28,267 hrs · 17,206 cycles

CABIN EMERGENCY LIGHT TEST FAULTED BAT/EPSU (13WL) AFT L. / T/S REPLACED BATTERY ON EPSU (13WL) ,NO HELP. REMOVED & REPLACED EPSU (13WL), OPS CHECK GOOD I/A/W AMM 33-51-38 PB 401."

Part: EPSU — FAILED INSP (11WL) · airframe 28,267 hrs · 17,206 cycles

EMERGENCY BATTERY AT POSITION 11WL FAILED THE BATTERY CAPACITY CHECK / REMOVED AND REPLACED EMERGANCY LIGHT BATTERY AT LH OVER WING EXIT FIN 11WL RE AMM 33-51-38"

Part: EPSU — FAILED INSP (10WL) · airframe 28,267 hrs · 17,206 cycles

CABIN EMERGENCY LIGHT TEST FAULTED EPSU(10WL) FWD L. / T/S EPSU (10WL) SELF TEST NO LIGHT SHOWN, REMOVED & REPLACED EPSU(10WL), OPS CHECK GOOD I/A/W AMM 33-51-38 PB 401."

Part: EPSU — NO TEST (EMERGENCY LIGHTS) · airframe 27,288 hrs · 16,728 cycles

EMERGENCY POWER SUPPLY (12WL) REQUIRES REPLACEMENT DUE TO BITE TEST FAULT / REMOVED AND REPLACED EMERGENCY POWER SUPPLY (12WL) BITE TEST GOOD REF AMM 33-51-38"

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 25,423 hrs · 15,776 cycles

DURING EPSU BATTERY TEST, FIN POSITION 10WL AND 13WL FAILED EPSU BATTERY CAPACITANCE TEST AND REQUIRES REPLACEMENT. / REMOVED/REPLACED (2EA) EPSU BATTERIES IAW A320 AMM 33-51-38-01A. BITE TEST PERFORMED SATISFACTORILY."