N204NV

Part: FAN — ODOR (ZONE 100) · airframe 30,132 hrs · 18,270 cycles

(AIRCRAFT NOT GROUNDED) APPROX @ TOP OF DESCENT BRIEF ACRID SMELL CB X18 POPPED, RECIRC FAN SUPPLY. PERFORMED TSM 21-21-00-810-802-A CONFIRMED RECIRC FAN FAULT. REMOVED AND REPLACED IAW AMM 21-21-51-000-001-A AND AMM 21-21-51-400-001-A OPS CHECK GOOD.

Part: UPLOCK SWITCH — FAULTED (ZONE 700) · airframe 29,895 hrs · 18,146 cycles

(AIRCRAFT NOT GROUNDED) (EMERGENCY DECLARED) ECAM L/G GEAR NOT UPLOCKED ON DEPARTURE. UPLOCK INDICATIONS AMBER ON NOSEWHEEL IN THE GEAR UP POSITION. / RAR NLG UPLOCK SWITCH ASSEMBLY IAW AMM 32-31-21-000/400-001-A. OPS CHECK GOOD. NO OTHER DEFECTS NOTED. "

Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 29,155 hrs · 17,705 cycles

(AIRCRAFT NOT GROUNDED) FWD FA MEGAPHONE INOP / REPLACED FWD FA MEGAPHONE IAW AC 204NVLOPA A2256500I02"

Part: BATTERY — NO TEST (ZONE 200) · airframe 28,180 hrs · 17,297 cycles

(AIRCRAFT NOT GROUNDED) LEAD FA'S FLASHLIGHT DOES NOT FLASH (BLANK) DURING PREFLIGHT INSPECTION / REPLACED FA FLASHLIGHT BATTERY, OPS CHECK GOOD AT THIS TIME. IAW AMM 25-65-00-00"

Part: INDICATION SYS — FALSE INDICATION (ZONE 800) · airframe 28,138 hrs · 17,282 cycles

(AIRCRAFT NOT GROUNDED) R1 SLIDE INTERMITTENT INDICATION ON THE GROUND / PERFORMED OPERATIONAL TEST OF R1 SLIDE INDICATION IAW AMM 25-62-44-400-802-A. OPS CHECK GOOD, A/C OK FOR CNT SVC "

Part: BATTERY — NO TEST (ZONE 200) · airframe 28,109 hrs · 17,270 cycles

(AIRCRAFT NOT GROUNDED) DURING WEEKLY, EPSU 13WL FAILS EMERGENCY LIGHT CHECK / REMOVED AND REPLACED EPSU BATTERY 13WL, OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD AT THIS TIME IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A."

Part: EPSU — NO TEST (EMERGENCY LIGHTS) · airframe 26,773 hrs · 16,603 cycles

NRC 7000-0008: IN PASSENGER CABIN, EPSU 12WL FAILED CHECK OF THE MANUAL OPERATION FROM THE TWO CONTROL PANELS AND OF ALL THE CABIN LIGHTS AND SIGNS ILLUMINATED BY BATTERIES IAW AMM 33-51-00-710-004-A / IN PASSENGER CABIN, BATERRY PACK OF EPSU 12WL REPLACED AND TESTED SERVICEABLE IAW AMM 33-51-38-400-002-A."

Part: SKIN — DAMAGED (RT WING) · airframe 26,773 hrs · 16,603 cycles

DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 6000-0033: 1205-15 RH WING BOTTOM SKIN LOWER SURFACE, PREVIOUS BLEND FOUND AT RIB 25 APPROX 6 INCHES FROM T/E. / RH WING BOTTOM SKIN PANEL #2 LOWER SURFACE BTW RIB 25-26 AND STGR11 REPAIRED PER AIRBUS DOSSIER #81396830 AND ALLEGIANT AIR ERO #R5721-**** REV.**. REPAIR MAJOR WITH NO SPECIFIC REPAIR CATEGORY PER RDAF #81396830/003/2024#A, THIS RDAF REPRESENT A STAGE 1 APPROVAL AND INCLUDES A 6 MONTHS REPAIR LIFE LIMITATION. PRIOR TO THE EXPIRATION OF THIS LIFE LIMITATION AIRBUS AUTOMATICALLY DELIVER AN UP-ISSUED RDAF WITH THE DEFINED CLASSIFICATION AND REPAIR CATEGORY. REFER TO AIRBUS DOSSIER #81396830 FOR DETAILS (ADMINISTRATIVE DOSSIER). SEE AWS FOR DETAILS. AFTER COMPLETION OF THIS WORK , M360 AND M313 SEND TO CUSTOMER ON 05/22/2024.R5721-0163, REV 00, N204NV-AAR-RH WING-LWR SKIN PANEL #2 BTWN RIB 25-26 AT STGR 11-EXISTING REPAIR, ACCOMPLISHED."

Part: STRINGER — CORRODED (FRMS 21-22 S38L) · airframe 26,773 hrs · 16,603 cycles

NRC 1000-0008: 130-06 (S/M) ON LOWER FUSELAGE STRUCTURE, CORROSION FOUND ON STR 38L BTW FR 21-FR 22. / LOWER FUSELAGE STRUCTURE, STRINGER 38L BTW FR 21-22 FOUND WITHIN LIMITS PER SRM 51-73-11 PARA.4 , TABLE 1 AND FIG.012 REV.148. REPAIR CATEGORY A, NO FURTHER ACTION REQUIRED, SEE AWS FOR DETAILS. BLEND DIMENSIONS: L: 2.500IN, W: 1.00IN, D: 0.003IN, NOMINAL THICKNESS: 0.078IN"

Part: SKIN — DENTED (FRMS 17-18 S25R) · airframe 26,773 hrs · 16,603 cycles

NRC 1000-0004: 130-02 (S/M) ON EXTERNAL FUSELAGE SKIN, DENT FOUND BTW FR 17-FR 18 AT STR 25R.(UNDER R-1 DOOR CUTOUT) / DISCREPANCIE SHOULD BE READ ON EXTERNAL FUSELAGE SKIN, PREVIOUS BLEND FOUND BTW FR 17-18 BTW STR 25R-26R (UNDER R-1 DOOR CUTOUT). EXTERNAL FUSELAGE SKIN BTW FR 17-18 BTW STGR 25R-26R FOUND WITIHN LIMITS PER SRM 53-11-11-283-011 FIG.001, 002, 007 SHT.7 AND 11 AND DIAGRAM 001 REV.148. REPAIR CATEGORY B SEE SRI 53-11-11-205-027 TABLE 1 UNRIVETED AREA, ZONE 1 REV.148 FOR INSPECTION REQUIREMENTS. INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT: 60000FC/120000FH (WICHEVER OCCURS FIRST), SUBSEQUENT INSPECTION INTERVALS: TBD, INSPECTION METHOD: TBD. SEE AWS FOR DETAILS. BLEND DIMENSIONS: L: 2.00IN, W: 1.500IN, D: 0.013IN, NOMINAL THICKNESS 0.079IN."

Part: SKIN PANEL — CORRODED (ZONE 500) · airframe 24,577 hrs · 15,456 cycles

DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: ZL-500-03-1-001 EWIS AT LH WING TOP SKIN PANEL 2, LOWER SURFACE TRAILING EDGE OVERHANG AT RIBS 14-15 CORROSION WAS FOUND. DUE THE CORROSION IS OUT SRM ADL DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL. AIRBUS PROVIDED REPAIR INSTRUCTION UNDER DOSSIER81191642. COOPESA PERFORMED REPAIR UNDER EO COO-EO-2023-17438-R00.

Part: MEGAPHONE — MALFUNCTIONED (FWD CABIN) · airframe 23,997 hrs · 15,163 cycles

FWD MEGAPHONE SIREN INOP / FWD MEGAPHONE REMOVED AND REPLACED IAW SIP, OPS CHECK GOOD IAW AMM 25-65-51-710-002-A"

Part: BATTERY — FAILED · airframe 23,107 hrs · 14,747 cycles

EPSU BATTERIES AT 10WL AND 11WL FAILED BITE TEST / R+R EPSU BATTERY AT 10WL & 11WL IAW AMM 33-51-38, OPS CHECK GOOD."

Part: BATTERY — FAILED · airframe 23,107 hrs · 14,747 cycles

EPSU BATTERY AT 12WL FAILED BITE TEST / R+R EPSU BATTERY AT 12WL IAW AMM 33-51-38"