N203NV
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) ON WEEKLY FOUND EPSU (12WL) FAUTING EXTERNAL EMERG LIGHT (62WL). REMOVED AND REPLACED EXTERNAL EMERGENCY LIGHT BULB (62WL) PER TSM 33-51-00-810-809-A IAW AMM 33-51-15-000-001-A AND 33-51-15-400-001-A. THIS CLEARS MEL 33-50-04A MDDR 232025 OPS CHECK GOOD AND PLACARDS REMOVED.
(AIRCRAFT NOT GROUNDED) EPSU FAILS TO SELF TEST VIA MCDU SYS TEST. REPLACED THE EPSU IAW AMM 33-51-38-400-001-A. "
(AIRCRAFT NOT GROUNDED) DIRTY SOCK SMELL ON DESCENT, CORUSON REPORT SUBMITTED / PERFORMED TC 21-000-001, VERIFIED APU INLET PLENUM IS CLEAN, NO FLUID NOTED. FOUND SMELL IS REPRODUCED WITH ONLY PACK 2 RUNNING. PACK 2 DEFERRED REF. LP # 2088142, M313 CREATED MDDR # 229607 FOR TC 21-000-002 TO BE PERFORMED WITHIN 5 CALENDAR DAYS"
DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-ZL-471-01-4-001, LH WING BOTTOM SKIN LOWER SURFACE AFT SECTION AREA SKIN AT RIB 8 WITH CORROSION WAS FOUND. AIRBUS WAS CONTACTED FOR REPAIR INSTRUCTIONS. THE REPAIR INSTRUCTIONS WERE RECEIVED AND PERFORMED PERMANENT BLEND OUT REPAIR ON LH WING LOWER PYLON REINFORCEMENT PLATE, RIB 8 IAW COOPESA EO # COO-EO-2025-23161-R00, R01 AND R02 LAST REV DATE 09,23,2025 APPROVED AND DOCUMENTED ON AIRBUS FORM RDAF REF: 81658837/004/2025 # A DATED 09/23/2025 AND ALLEGIANT ERO # A32X-STR-57ERO-00403-R00 DATED 09/25/2025. THIS REPAIR IS MAJOR. THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1Q202 ITEM 5-3.
(AIRCRAFT NOT GROUNDED) EMER R BATTERY AND AFT L BATTERY FAILED EPSU TEST / REMOVED AND REPLACED BATTERY 13WL AND 12WL IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. OPS CHECK GOOD. "
DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK ZL-500-03-1-001_P1-OP-UP-W , LH WING BETWEEN STA4067/RIB7 & STA4862/RIB 8, UPPER SURFACE, TRAILING EDGE SKIN WITH SPOT CORROSION (2EA) WERE FOUND.THE OEM WAS CONTACTED FOR REPAIR INSTRUCTIONS. ´PERFORMED PERMANENT REPAIR AT LH WING TOP SKIN PANEL 2 TEOH UPPER SURFACE BETWEEN WX 4010.2 AND WX 4490.52 IAW COOPESA EO # COO-EO-2024-20955-R02 AND AIRBUS RDAF 80604749/017/2021 # B APPROVED BY ALLEGIANT UNDER ERO A32X-STR57ERO-00070 REV 00. THIS IS MAJOR REPAIR CAT B. THIS REPAIR IS COVERED COOPESA JOB A1P208 ITEM 5-11.
DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 572111-01-1-001_P1-OP-UP-W , LH WING (BETWEEN STA4862/RIB 9 & STA5512/RIB10) FIXED TRAILING EDGE PANEL OVERHANG WITH LOOSE FASTENER AND CORROSION FOUND AT TOP SKIN LOWER SURFACE..THE OEM WAS CONTACTED FOR REPAIR INSTRUCTIONS. ´PERFORMED PERMANENT REPAIR AT LH WING TOP SKIN PANEL 2 TEOH LOWER SURFACE BETWEEN RIB 9 AND RIB 11 IAW COOPESA EO # COO-EO-2024-20955-R02 AND AIRBUS RDAF 80604749/017/2021 # B APPROVED BY ALLEGIANT UNDER ERO A32X-STR57ERO-00070 REV 00. THIS IS MAJOR REPAIR CAT B. THIS REPAIR IS COVERED COOPESA JOB A1P208 ITEM 5-7.
DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 572112-01-1-002_P1-OP-UP-W , RH WING REAR SPAR TRAILING EDGE OVERHANG TOP SKIN LOWER SURFACE AT WING RIB 10 CORROSION WAS FOUND.THE OEM WAS CONTACTED FOR REPAIR INSTRUCTIONS. ´PERFORMED PERMANENT REPAIR AT RH WING TOP SKIN PANEL 2 TRAILING EDGE OVERHANG BETWEEN RIBS 9-11 IAW COOPESA EO # COO-EO-2024-20953-R01 AND AIRBUS RDAF 80947349/111/2024 # A APPROVED BY ALLEGIANT UNDER ERO A32X-STR57ERO-00072 REV 00. THIS IS MAJOR REPAIR CAT B. THIS REPAIR IS COVERED COOPESA JOB A1P208 ITEM 6-1.
DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 572112-01-1-002_P1-OP-UP-W , RH WING BOX TOP SKIN TRAILING EDGE OVERHANG WITH CORROSION AT RIB 14 AND RIB 14+415MM LOWER SURFACE AND RIB 14+185MM UPPER SURFACE.THE OEM WAS CONTACTED FOR REPAIR INSTRUCTIONS.´PERFORMED PERMANENT REPAIR AT RH WING TOP SKIN PANEL 2 TRAILING EDGE OVERHANG BETWEEN RIBS 13-15 IAW COOPESA EO # COO-EO-2024-20953-R01 AND AIRBUS RDAF 80947349/111/2024 # A APPROVED BY ALLEGIANT UNDER ERO A32X-STR57ERO-00072 REV 00. THIS IS MAJOR REPAIR CAT B. EVALUATED REWORKED AREA AT RIB 14+415 LOWER SURFACE AND WAS FOUND WITIHN LIMITS IAW A320 SRM TASK 57-21-11-283-007 PARAG 2.A (1) FIG 001(SHEET 1,6 AND 7) FIG 005 (SHEET 1) AND AREA AT RIB 14+185MM UPPER SURFACETHIS REPAIR IS COVERED COOPESA JOB A1P208 ITEM 6-1.
R1 SLIDE DEPLOYED. GROUND CREW ACTIVATED SLIDE AND OPENED DOOR / REMOVED AND REPLACED R1 DOOR SLIDE IAW AMM 25-62-44-000-803-A AND 25-62-44-400-802-A. OPS CHECK GOOD."