N202NV
Registered owner: SUNRISE ASSET MANAGEMENT LLC, NV (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
(AIRCRAFT NOT GROUNDED) AFT FLIGHT ATTENDANTS REPORT DIRTY SOCKS SMELL ABOUT 2 MINUTES BEFORE LANDING. APU BLEED WAS NOT ON AT TIME OF EVENT / PERFORMED LEVEL 1 TASK CARD 21-000-001. NO SMELL REPRODUCED AT THIS TIME. M313 GENERATED ON LP 2121264 FOR LEVEL 2 TC 21-000-002. SEE TC 21-000-001 FOR WORK PERFORMED. "
(AIRCRAFT NOT GROUNDED) SCREW MISSING FROM LH OVERWING ESCAPE SLIDE PANEL. INSTALLED SCREW ON LH OFFWING ESCAPE SLIDE REF AIRBUS AMM 25-62-42-400-001-AITEM: 1INSTALLED SCREW ON LH OFFWING ESCAPE SLIDE REF AIRBUS AMM 25-62-42-400-001-A.
(AIRCRAFT NOT GROUNDED) ON CAP TEST RECIEVED BAT/EPSU(10WL)FWD L. REMOVED AND REPLACED EPSU BATTERY AT LOCATION 10WL IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A, OPS CHECK GOOD. ITEM: 1REMOVED AND REPLACED EPSU BATTERY AT LOCATION 10WL IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A, OPS CHECK GOOD."
(AIRCRAFT NOT GROUNDED) EXIT SIGN COVER R2 DOOR FELL OFF / INSTALLED NEW R2 FLOOR EXIT LIGHT LENSE COVER IAW 33-51-13-400-001-A.(M) PROCEDURES REVERSED.M151
(AIRCRAFT NOT GROUNDED) FAILS EPSU TEST. / REMOVED AND REPLACED EPSU REF WO528339"
(AIRCRAFT NOT GROUNDED) FA NR 4 FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FA NR 4 FLASHLIGHT BATTERY IAW AMM 25-66-00-PB 201. OPS CHECK GOOD.
(AIRCRAFT NOT GROUNDED) EPSU INDICATES BAT FAIL UPON BITE / REMOVED AND REPLACED EPSU BATTERY. PERFORMED SUCSESSFUL OPPERATIONAL TESTS.WORK COMPLETED IAW AIRBUS A320 AMM 33-51-38-000-002-A, 33-51-38-400-002-A, 33-51-00-710-001"
DURING ALLEGIANT ACCOMPLISHMENT A32X-STR-53EO-00055 SB-A320-53-1500 FUSELAGE TAIL CONE SUBSTRUCTURE REMOVAL AND FIXATION OF APU AIR INTAKE DUE TO THE STRUCTURE DEVIATION WAS FOUND.AIRBUS WAS CONTACTED ASKING FOR REPAIR INSTRUCTIONS. PERFORMED DEVIATIONS OF SB A320-53-1500 AT TAIL CONE LH FIREWALL BETWEEN FR81/83 IAW COOPESA EO COO-EO-2025-21504-R00 DOCMENTED AND PAPROVED ON AIRBUS RDAF 81520998/004/2025 ISSUE A, APPROVED BY ALLEGIANT UNDER ERO A32X-STR-53-ERO-00167. THIS REPAIR IS DOCUMENTED UNDER COOPESA JOB A1P259 ITEM 18-19.
DURING ALLEGIANT ACCOMPLISHMENT TASK A32X-71-400-002_P1-OP-UP-ENG/002 RH ENGINE PYLON FWD ENGINE MOUNT LOWER SURFACE FWD AND AFT GUIDE PIN HOLE EDGE STRUCK WAS FOUND.AIRBUS WAS CONTACTED ASKING FOR REPAIR INSTRUCTIONS. PERFORMED REPAIR BUSHING AT RH PYLON TO ENGINE FWD ATTACH SPIGOT FITTING CENTER AND AFT HOLES IAW COOPESA EO COO-EO-2025-21539-R00 AND AIRBUS TECHNICAL DISPOSITION TD/81522549/011/2025 # A.DOCUMENTED APPROVED AND SUBMITTED ON REPAIR AND DESIGN APPROVAL RDAF 81522549/002/2025 ISSUE B APPROVED BY ALLEGIANT ERO A32X-STR-54ERO-00168. AIRBUS CONFIRMS THE RDAF IS CLASSIFIED AS MAJOR WITH NO SPECIFIC CATEGORY. THIS RDAF REPRESENTS A STAGE 1 APPROVAL AND INCLUDES A 6 MONTHS REPAIR LIFE LIMITATIONS.AIRBUS WILL ACCOMPLISH THE FULL FDT ANALYSIS STAGE 2/3 APPROVAL AND AUTOMATICALLY DELIVER ON UP ISSUED RDAF WITH DEFINED CLASSIFICATION AND CATEGORY. THIS REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1P259 ITEM 4-34
FWD MEGAPHONE INOP / REMOVED AND REPLACED FWD MEGAPHONE OPS CK GOOD REF AMM 25-65-51"
IN PASSENGER CABIN, ON FLOOR STRUCTURE, CORROSION FOUND ON R-2 SILL BEAM AROUND HOLES OF NUT PLATE BTW FR67-FR68 (R/H SIDE) / IN PASSENGER CABIN, ON FLOOR STRUCTURE, CORROSION FOUND ON R2 SILL BEAM AROUND HOLES OF NUT PLATES BTW FR67-68 REPAIRED AS PER SRM TASK 53-41-11-300-001 REV 146, REPAIR PRINCIPLE 7. "
(AIRCRAFT NOT GROUNDED) EPSU FAILED CAPACITY TEST / REMOVED AND REPLACED EPSU BATTERIES, REF WO526955"
DURING THE BATTERY CAPACITY TEST IT SHOWED 10WL, 11WL, 13WL FAILED. / REMOVED AND REPLACED 10WL, 11WL, 13WL BATTERIES WITH INSPECTED BATTERIES IAW AMM 33-51-38. OPS CHECK GOOD. NO OTHER DEFECTS NOTED AT THIS TIME."
FAILED EPSU SUS TEST FIN 10WL & 11WL TROUBLE SHOOT TO BATTERY PACK / REPLACED BATTERY PACKS AT 10WL & 11WL, OPS CHECK GOOD REF AMM 33-51-00-710-001-A & AMM 33-51-38"