N289NV

Part: FRAME — CRACKED (ZONE 200) · airframe 41,412 hrs · 27,891 cycles

DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-E5316-0003, UPPER FUSELAGE PASSENGER CABIN FR16 LH AT DOOR STOP FITTING LOCATION # 7 UPPER AND LOWER INBOARD OPEN HOLES WITH CRACK INDICATION WAS FOUND. PERFORMED FREEZE PLUG FASTENER HOLE REPAIR AT FR16 STOP FITTING # 7 FRAME UPPER INBOARD HOLE AND FITTING REPLACMENT IAW A320 SRM TASK 53-11-12-300-011 PARAG 2A FIG 001 FIG 005 FIG 006 AND 51-72-11-911-001 REPAIR CATGEROY B.THIS REPAIR IS CLASSIFIED AS MAJOR. THIS REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1Q154 ITEM 2-21.

Part: FRAME — CRACKED (ZONE 200) · airframe 41,412 hrs · 27,891 cycles

DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-E5311-0018, UPPER FUSELAGE FR16 RHS DOUBLE JOGGLE UPPER AREA HOLES POSITIONS # 7, #A, #B AND #C WITH CRACK INDICATION WERE FOUND. PERFORMED TEMPORARY FASTENER HOLES # 7, #A, #B AND #C BUSHES REPAIR AT FR 16 RHS DOUBLE JOGGLE AREA IAW COOPESA EO # COO-EO-2025-22565-R00 , APPROVED AND DOCUMENTED ON AIRBUS FORM RDAF 81610048/003/2025 # A AND ALLEGIANT ERO A32X-STR-53ERO-00306 THIS REPAIR IS CLASIFIED AS MAJOR. THIS REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1Q154 ITEM 2-18.

Part: FRAME — CRACKED (ZONE 200) · airframe 41,412 hrs · 27,891 cycles

DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-260-003, UPPER FUSELAGE FR68 RHS AT DOOR STOP FITTING # 1 LOWER OUTBOARD FASTENER HOLE WITH CRACK INDICATION. PERFORMED FREEZE PLUG FASTENER HOLE REPAIR AND OVERSIZE BOLT INSTALLATION AT FR68 STOP FITTING # 1 IAW A320 SRM TASK 53-41-12-300-008 AND 53-41-12-300-010 PARAG 2 A REPAIR CAT B.THIS REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1Q154 ITEM 2-19.

Part: FRAME — CRACKED (ZONE 200) · airframe 41,412 hrs · 27,891 cycles

DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-E5316-0003, UPPER FUSELAGE PASSENGER CABIN FR 16 LHS AT DOOR STOP FITTING # 1 LOWER INBOARD OPEN HOLE WITH CRACK INDICATION. PÉRFORMED FREEZE PLUG FASTENER HOLE REPAIR FR16 LHS STOP FITTING # 1 LOWER INBD HOLE AND STOP FITTING OVERSIZE HOLES IAW COOPESA EO # COO-EO-2025-22576-R01 APPROVED AND DOCUKMENTED ON AIRBUS FORM RDAF 81609950/002/2025 # A AND ALLEGIANT ERO A32X-STR-53ERO-00308-R00. THIS REPAIR IS CLASSIFIED AS MAJOR.THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1Q154 ITEM 2-20.

Part: FRAME — CRACKED (ZONE 200) · airframe 41,412 hrs · 27,891 cycles

DURING ALLEGIANT ACCOMPLISHMENT OF THE TASK A32X-E5311-0019, UPPER FUSELAGE FR16 LH SIDE DOUBLE JOGGLE AREA HOLE POSITION # 7 WITH CRACK INDICATION WAS FOUND. PERFORMED NEXT NOMINAL FASTENER HOLE # 7 REPAIR AND ASSOCIATED HOLE # 8 SECOND OVERSIZE REPAIR IAW A320 SRM TASK 53-11-12-300-0134 PARAG 2A FIG 001 FIG 008 MAJOR REPAIR CAT B. THIS REPAIR IS DOCUMENTED UNDER COOPESA JOB A1Q154 ITEM 2-17.

Part: LATCH — OUT OF POSITION (ZONE 800) · airframe 40,601 hrs · 27,534 cycles

(AIRCRAFT NOT GROUNDED) ROW 12 L OVERWING EXIT SLIDE NOT ARMED / DURING INSPECTION L OVERWING EMERGENCY HATCH FOUND LATCH PIN OF THE SLIDE RELEASE MECHANISM RETRACTED. PUT THE LATCH MECHANISM BACK IN THE ARMED POSTION PER AMM 52-21-11-400-001-A. A/C OK FOR SERVICE "

Part: MEGAPHONE — INTERMITTENT (ZONE 200) · airframe 40,551 hrs · 27,511 cycles

(AIRCRAFT NOT GROUNDED) FWD MEGAPHONE WORKS INTERMITENTLY / REMOVED AND REPLACED MEGAPHONE IAW AMM 25-65-51-710-002-A. OPS CHECK GOOD.

Part: BATTERY — NO TEST (ZONE 200) · airframe 40,492 hrs · 27,487 cycles

(AIRCRAFT NOT GROUNDED) EPSU BATTERY 10WL FAILED BITE / (RESOLVED ON W/O: 512591 TASKCARD: NR-00005 ) REMOVED AND REPLACED EPSU BATTERY 10WL IAW AMM 33-51-38-400-002-A AND 33-51-38-000-002-A. OPS CHECKS GOOD. ITEM: 1REMOVED AND REPLACED EPSU BATTERY 10WL IAW AMM 33-51-38-400-002-A AND 33-51-38-000-002-A. OPS CHECKS GOOD. "

Part: COMPRESSOR — LEAKING (APU) · airframe 40,072 hrs · 27,309 cycles

(AIRCRAFT NOT GROUNDED) DIRTY SOCK SMELL FILLED FLIGHT DECK WHEN OUTFLOW VALVE OPENED AROUND 3,000' / C/W ALLEGIANT AIR A320 TC 21-000-002. FOUND EVIDENCE OF WETTNESS IN LOAD COMPRESSOR WITH BORESCOPE. APU LOAD COMPRESSOR LEAK. REMOVED APU IAW AMM TASK 49-11-11-000-004-A. C/W STEPS #2 & #3. CLEANING OF THE APU COMPARTMENT AND APU AIR INTAKE WITHOUT THE APU INSTALLED IAW 49-00-00-100-805-A AND 49-16-00-100-005-A. COMPLETED INSTALLATION OF THE APU IAW A320 AMM 49-11-11-400-A STEPS 4 (D) THRU COMPLETION. NO DEFECTS NOTED AT THIS TIME. "

Part: EMER LIGHT SYS — BROKEN (UNKNOWN) · airframe 40,006 hrs · 2,728 cycles

(AIRCRAFT NOT GROUNDED) R1 LOWER EMERGENCY EXIT SIGN LENS BROKEN OFF WALL / R1 EMERGENCY EXIT SIGN RECONNECT AND REINSTALLED ,OPS CHECK GOOD IAW A320 AMM 33-51-17"

Part: SLIDE RAFT — FAULTY (R1 DOOR) · airframe 39,170 hrs · 26,877 cycles

(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 2000-0066: R1 DOOR ESCAPE SLIDE FOUND FAULTY / R1 DOOR ESCAPE SLIDE REPLACED AS PER AMM 25-62-44-400-803-A. FOR THE OPERATIONAL TEST SEE AWS FOR DETAILS."

Part: SKIN — CORRODED (LT WING TE) · airframe 39,170 hrs · 26,877 cycles

(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 5000-0035: LH WING TRAILING EDGE OVERHANG, CORROSION FOUND AT UPPER SKIN LOWER SURFACE BETWEEN INBD OF RIB 14 AND RIB 16. / LH WING TOP SKIN PANEL #2 LOWER SURFACE TEOH AREA BTW INBD OF RIB 14 AND RIB 16 PERMANENTLY REPAIRED PER AIRBUS DOSSIER #81414982, TD 81414982/007/2024 #A, REPAIR INSTRUCTIONS R572-58979 ISSUE E, R572-58616 ISSUE M AND ALLEGIANT ERO #R5721-**** REV.**. REPAIR MAJOR CATEGORY B PER AIRBUS RDAF #81414982/004/2024 #A, INSPECTION REQUIREMENTS:THRESHOLD FROM REPAIR EMBODIMENT: 11000FC/19000FH, INTERVAL: 11000FC/19000FH, METHOD: DET. REFER TO AIRBUS DOSSIER #81414982 FOR MORE DETAILS (ADMINISTRATIVE DOSSIER. SEE AWS FOR DETAILS. AFTER COMPLETION OF THIS WORK M205, M36 AND M313 FORMS HAVE BEEN SEND TO CUSTOMER ON 06/24/2024. SEE NRC 4002604-6000-0026/5000-0024/7000-0004 FOR ZERO STRESS JACKING AND ACCESS. R5721-0168, REV. 00, N289NV - AAR - LH WING RIB 14 TO RIB 17 TOP SKIN PANEL #2 LWR SURFACE TEOH - CORROSION, ACCOMPLISHED."

Part: SKIN — CORRODED (RT WING TE) · airframe 39,170 hrs · 26,877 cycles

(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 6000-0022: (1042-001A) RH WING TOP SKIN LOWER SURFACE AT OVERHANG TRAILING EDGE, CORROSION FOUND BETWEEN RIB 15 AND RIB16. / RH WING TOP SKIN PANEL #2 LOWER SURFACE TEOH AREA BTW RIB 14 AND 16 PERMANENTLY REPAIRED PER AIRBUS DOSSIER #81413579, TD 81413579/010/2024 #A, REPAIR INSTRUCTIONS R572-58979 ISSUE E, R572-58616 ISSUE M AND ALLEGIANT ERO #R5721-0167 REV.00. REPAIR MAJOR CATEGORY B PER AIRBUS RDAF #81413579/004/2024 #A, INSPECTION REQUIREMENTS:THRESHOLD FROM REPAIR EMBODIMENT: 11000FC/19000FH, INTERVAL: 11000FC/19000FH, METHOD: DET. REFER TO AIBUS DOSSIER #51413579 FOR MORE DETAILS (ADMINISTRATIVE DOSSIER). SEE AWS FOR DETAILS. AFTER COMPLETION OF WORK M205, M360 AMD M313 FORMS HAVE BEEN SEND TO CUSTOMER ON 06/16/2024. SEE NRC 4002604-6000-0026/6000-0021 FOR ZERO STRESS JACKING AND ACCESS. R5721-0167 REV. 00, N289NV-AAR-RH WING UPPER SKIN PANEL #2-LWR SURFACE TEOH-CORROSION ACCOMPLISHED."

Part: SKIN — CORRODED (RT WING TE) · airframe 39,170 hrs · 26,877 cycles

(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 6000-0005: 33284-001 RH WING TOP SKIN LOWER SURFACE AT OVERHANG TRAILING EDGE, CORROSION FOUND BETWEEN RIB16 AND RIB17 (WMRX 5855.60). / RH WING TOP SKIN PANEL #2 LOWER SURFACE TEOH AREA BTW RIB 16 AND OUTBD OF RIB 17 PERMANENTLY REPAIRED PER AIRBUS DOSSIER #81413579, TD 81413579/010/2024 #A, REPAIR INSTRUCTIONS R572-58616 ISSUE M AND ALLEGIANT ERO #R5721-0167 REV.00. REPAIR MAJOR CATEGORY B PER AIRBUS RDAF #81413579/004/2024 #A, INSPECTION REQUIREMENTS:THRESHOLD FROM REPAIR EMBODIMENT: THRESHOLD FROM REPAIR EMBODIMENT: 11000FC/21000FH, INTERVAL: 11000FC/21000FH, METHOD: DET. REFER TO AIBUS DOSSIER #51413579 FOR MORE DETAILS (ADMINISTRATIVE DOSSIER). SEE AWS FOR DETAILS. AFTER COMPLETION OF WORK M205, M360 AMD M313 FORMS HAVE BEEN SEND TO CUSTOMER ON 06/16/2024. SEE NRC 4002604-6000-0026/6000-018/7000-0002 FOR ZERO STRESS JACKING AND ACCESS. R5721-0167 REV.00, N289NV-AAR-RH WING UPPER SKIN PANEL #2 - LWR SURFACE TEOH-CORROSION ACCOMPLISHED."

Part: SKIN — CORRODED (LT WING TE) · airframe 39,170 hrs · 26,877 cycles

(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 5000-0023: 1711-15 LH WING TRAILING EDGE OVERHANG, CORROSION FOUND ON UPPER SKIN LOWER SURFACE BTW RIB 16 TO OUTBD OF RIB 17. / LH WING TOP SKIN PANEL #2 LOWER SURFACE TEOH AREA BTW RIB 16 AND OUTBD OF RIB 17 PERMANENTLY REPAIRED PER AIRBUS DOSSIER #81414982, TD 81414982/007/2024 #A, REPAIR INSTRUCTIONS R572-58979 ISSUE E, R572-58616 ISSUE M AND ALLEGIANT ERO #R5721-**** REV.**. REPAIR MAJOR CATEGORY B PER AIRBUS RDAF #81414982/004/2024 #A, INSPECTION REQUIREMENTS:THRESHOLD FROM REPAIR EMBODIMENT: 11000FC/21000FH, INTERVAL: 11000FC/21000FH, METHOD: DET. REFER TO AIRBUS DOSSIER #81414982 FOR MORE DETAILS (ADMINISTRATIVE DOSSIER. SEE AWS FOR DETAILS. AFTER COMPLETION OF THIS WORK M205, M36 AND M313 FORMS HAVE BEEN SEND TO CUSTOMER ON 06/24/2024. SEE NRC 4002604-6000-0026/5000-0028/5000-0034/7000-0003 FOR ZERO STRESS JACKING AND ACCESS. R5721-0168, REV. 00, N289NV - AAR - LH WING RIB 14 TO RIB 17 TOP SKIN PANEL #2 LWR SURFACE TEOH - CORROSION, ACCOMPLISHED."

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,170 hrs · 26,877 cycles

(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 2000-0005: (S/M)34240-01 REAR FUSELAGE SKIN, AT L2 DOOR CUTOUT, UPPER FWD CORNER FOUND DAMAGED. / REAR FUSELAGE SKIN L2 DOOR CUTOUT UPPER FWD CORNER PERMANENTLY REPAIRED PER AIRBUS DOSSIER #81411219 AND ALLEGIANT AIR ERO #R5341-0130 REV.00. MAJOR REPAIR CATEGORY B PER AIRBUS RDAF #81411219/004/2024#A, INSPECTION REQUIREMENTS: THRESHOLD FROM REPAIR EMBODIMENT: 12700FC (FH NOT RELEVANT), INTERVAL: 12700FC (FH NOT RELEVANT), METHOD: DET AS PER NTM 51-90-00. REFER TO AIRBUS DOSSIER #81411219 FOR MORE DETAILS (ADMINISTRATIVE DOSSIER). SEE AWS FOR DETAILS. AFTER COMPLETION OF THIS WORK M360 AND M313 FORMS HAVE BEEN SEND TO CUSTOMER ON 06/11/2024. R5341-0130, REV. 00, N289NV - AAR - LH AFT PASSENGER DOOR CUTOUT FWD UPPER CORNER - CHAFING, ACCOMPLISHED."

Part: DEU — FAULTED (EMERGENCY LIGHTS) · airframe 39,132 hrs · 26,854 cycles

EPSU BITE TEST EPSU FWD L 10WL/DEU FAULT / REPLACED REF TC 23-73-47-400-001-A"

Part: EPSU — NO TEST (EMERGENCY LIGHTS) · airframe 39,132 hrs · 26,854 cycles

EPSU BITE TEST EPSU FWD L 10WL/DEU.B FAULT / R&R EPSU IAW AMM REF 33-51-38-000-001-A & 33-51-38-400-001-A. OPS CHECK GOOD."

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 38,391 hrs · 26,455 cycles

PERFORMED EPSU SYS TEST AND FOUND CLASS 1 FAULT FOR SPSU (10WL) FWD BATTERY / ALEX CAMPBELL INSTALLED EPSU IAW AMM 33-51-38-400-001-A UP TO STEP 4(E). KOLTON WHITMORE INSTALLED CEILING PANELS IAW AMM 25-23-42-400-001."

Part: SLIDE RAFT — UNKNOWN (L1 DOOR) · airframe 38,383 hrs · 26,449 cycles

L1 DOOR WILL NOT ARM SLIDE. / INSTALLED NEW L1 DOOR ESCAPE-SLIDE RAFT PACK ASSY IAW AMM 25-62-44-400-007-A. OPS CHECK GOOD AT THIS TIME. NO DEFECTS NOTED AT THIS TIME. AIRCRAFT OKAY FOR SERVICE."

Part: RIB — CORRODED (ZONE 500) · airframe 37,249 hrs · 25,826 cycles

DURING THE INSPECTION ACCOMPLISHMENT PER ALLEGIANT WORK CARD Nº: ZL-575-01-1-001 IT WAS FOUND THE RIBLET J CORRODED. DUE TO THIS FACT IT WILL BE REPLACED BY NEW ONE, DUE TO FLY BY WIRE CABLES PASS THROUGH THE MENTIONED RIBLET J, DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL.AIRBUS PROVIDED THE REPAIR INSTRUCTIONS UNDER DOSSIER 81237682 AND REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1N115 ITEM5-1).

Part: STRINGER — CORRODED (ZONE 100) · airframe 37,249 hrs · 25,826 cycles

DURING INSPECTION TASK ZL-171-01-2-001 STRINGER 43 LEFT FLANGE UPPER CORROSION WAS FOUND.PERFORMED PERMANENT REPAIR AT STGR43L, BETWEEN FR64 AND FR66 I.A.W A320 SRM TASK 53-41-13-300-004 FIGURE 001 (SHEET 1), REV 144 DATED 02- 01-2023. THIS IS A MAJOR PERMANENT REPAIR CATEGORY A WITH NO ADDITIONAL REQUIREMENTS.THE REPAIR INSTRUCTIONS WAS DOCUMENTED UNDER COOPESA JOB A1N115 ITEM 1-12).

Part: NONE — NONE · airframe 35,872 hrs · 25,154 cycles

L1 LOWER EMERGENCY EXIT SIGN FELL OFF. / REPLACED L1 LOWER EMERGENCY EXIT SIGN IAW AMM 33-51-13-400-001-A."

Part: NONE — NONE · airframe 35,741 hrs · 25,084 cycles

REF. W/O 463019-2 PERMANENT REPAIR OF RUDDER DAMAGE REQUIRES REPAIR/PERFORMED RUDDER SKIN REPAIR AROUND TRAILING EDGE SCREW LINE IN THE GFRP AREA UP TO STEP 2.A.2 H.13 SRM 55-41-13-300-025.COMPLETED RUDDER SKIN REPAIR AROUND TRIALING EDGE SCREW IN GFRP AREA FROM STEP 2.A.2.H.14 THRU 2.A.6.A OF SRM 55-41-13-300-025.COMPLETED RUDDER SKIN REPAIR AROUND TRAILING EDGE SCREW LINE IN GFRP AREA FROM STEP 2.A.6.B OF SRM 55-41-13-300-025 THROUGH COMPLETION. NO FURTHER DEFECTS NOTED AT THIS TIME."

Part: SLIDE & SLEEVE — INOPERATIVE · airframe 35,571 hrs · 24,989 cycles

L2 SLIDE BLOWN / REINSTALLED SERVICEABLE SLIDE PER AMM 25-62-44 REPLACED DOOR ASSIST BOTTLE DIAPHRAGM AND SERVICED BOTTLE PER AMM 52-10-00.L2 DOOR SLIDE CHECKS NORMAL."

Part: SIGN — MISSING · airframe 35,508 hrs · 24,948 cycles

EXIT SIGN MISSING ROW 14 AIRCRAFT RIGHT / DETAILED VISUAL INSPECTION C/W AND PLACED CLEAR TAPE OVER EXPOSED AREA IAW EA 72-2022-138. 1 FC PERMANENT REPAIR TRACKED BY M313# 05330004/1."

Part: LIGHT — INOPERATIVE · airframe 35,478 hrs · 24,927 cycles

EMERGENCY LIGHTS AT LEFT AND RIGHT OVERWING EXITS ARE INOP / PERFORMED OPS CHECK OF EMERGENGY LIGHTS IAW AMM 33-51-00. REMOVED AND REPLACED OVERWING EXITS BATTERIES 12WL AND 11WL IAW AMM 33-51-38. OPS CHECK GOOD."

Part: EPSU — FAILED INSP (13WL) · airframe 34,138 hrs · 24,309 cycles

13WL EPSU BATTERY FAIL ON TEST / REMOVED AND REPLACED (13WL) EPSU BATTERIE IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A; OP'S CHECK GOOD"

Part: EPSU — NO TEST (EMERGENCY LIGHTS) · airframe 33,933 hrs · 24,212 cycles

EPSU SYSTEM TEST REVEALED EPSU (10WL) FAILED. / REMOVED AND REPLACED EPSU (10WL) IAW AMM 33-51-38 PB 401. OPS CHECK GOOD."