N259NV
Registered owner: BANK OF UTAH TRUSTEE, UT (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 FA'S REPORTED CHEMICAL CHLORINE LIKE ODOR BELOW 10,000FT FOR APPROXIMATELY 5 MINS. FWD FA REPORTED SCENT ON GROUND DURING TAXI IN.
(AIRCRAFT NOT GROUNDED) FA'S REPORT DIRTY SOCK ODOR AROUND 12,000 ON DECENT. SMELL CLEARED JUST BEFORE LANDING. C/W T/C A32X-21-000-002.ITEM: 1C/W T/C A32X-21-000-002 (RESOLVED ON W/O: 552831 TASKCARD: NR-00002 ).
(AIRCRAFT NOT GROUNDED) AFT L/H FLIGHT ATTENDANT SEAT FLASHLIGHT INOP. / REMOVED AND REPLACED AFT L/H FLIGHT ATTENDANT SEAT FLASHLIGHT PER AMM STANDARD INDUSTRY PRACTICES. OPS CHECK GOOD."
DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-240-001, UPPER FUSELAGE PAX CABIN FR43 S-15 RH AT SIDE BOX BEAM AREA,MID AND REAR OPEN FASTENER HOLE LOCATION WITH CRACK INDICATION WAS FOUND.AIRBUS WAS CONTACTED REQUESTING REPAIR INSTRUCTIONS. AIRBUS PROVIDED THE REPAIR INSTRUCTIONS.PERFORMED MID HOLE SECOND OVERSIZE AND AFT HOLE FREEZE PLUG REPAIR ON RH SIDE BOX FLANGE FR43 IAW COOPESA EO COO-EO-2025-23263-R00. THIS REPAIR IS APPROVED AND DOCUMENTED ON AIRBUS RDAF REF 81666791/009/2025 # A AND ALLEGIANT ERO A32X-STR-53ERO-00416.THE REPAIR WAS CLASSIFIED AS CAT C. THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1Q218 ITEM 2-18.
DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-240-001, UPPER FUSELAGE PAX CABIN FR43 S-15LH AT SIDE BOX BEAM AREA, REAR OPEN FASTENER HOLE LOCATION WITH CRACK INDICATION WAS FOUND.AIRBUS WAS CONTACTED REQUESTING REPAIR INSTRUCTIONS. AIRBUS PROVIDED THE REPAIR INSTRUCTIONS.PERFORMED AFT HOLE FREEZE PLUG REPAIR ON LH SIDE BOX FLANGE FR43 IAW COOPESA EO COO-EO-2025-23263-R00. THIS REPAIR IS APPROVED AND DOCUMENTED ON AIRBUS RDAF REF 81666791/009/2025 # A AND ALLEGIANT ERO A32X-STR-53ERO-00416.THE REPAIR WAS CLASSIFIED AS CAT C. THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1Q218 ITEM 2-17.
DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-240-001, UPPER FUSELAGE PAX CABIN FR43 S-15LH AT SIDE BOX BEAM AREA, REAR OPEN FASTENER HOLE LOCATION WITH CRACK INDICATION WAS FOUND.AIRBUS WAS CONTACTED REQUESTING REPAIR INSTRUCTIONS. AIRBUS PROVIDED THE REPAIR INSTRUCTIONS.PERFORMED AFT HOLE FREEZE PLUG REPAIR ON LH SIDE BOX FLANGE FR43 IAW COOPESA EO COO-EO-2025-23263-R00. THIS REPAIR IS APPROVED AND DOCUMENTED ON AIRBUS RDAF REF 81666791/009/2025 # A AND ALLEGIANT ERO A32X-STR-53ERO-00416.THE REPAIR WAS CLASSIFIED AS CAT C. THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1Q218 ITEM 2-17.
(AIRCRAFT NOT GROUNDED) WALL MOUNTED EMERGENCY EXIT LIGHT COVER AT L1 PASSENGER DOOR BROKEN. REMOVED AND REPLACED BROKEN DOOR EMERGENCY EXIT LENS IAW AIRBUS AMM 33-35-13-000-001-A AND 33-51-13-400-001-A.
SCREW POPPED OUT OF PANEL DIRECTLY ABOVE RT WING EMERGENCY EXIT SLIDE PANEL / TIGHTENED SCREW IAW A320 AMM 20-21-11-911-001-A AIRCRAFT OK FOR SERVICE."
EPSU BATTERY 13WL FAILED BATTERY CAPACITY CHECK PER TC 335100-03-1-001 / REMOVED AND REPLACED EPSU BATTERY 13WL PER A320 AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. OPS CHECK GOOD."
DURING DETAILED INSPECTION OF PASSENGER/CREW DOOR FOR INTEGRITY AND GOOD ADJUSTMENT OF MECHANISMS (INCLUDING GIRT BAR), FWD LEFT IAW ALLEGIANT TASK 521000-04-1-001 UPPER FUSELAGE FWD ENTRY DOOR SCAPE SLIDE OPERATIONAL CHECK OF EMERGENCY POWER SUPPLY BY BITE CHECK WAS FOUND FAILED. DUE THIS CONDITION WAS REPLACED FWD LH DOOR SCAPE SLIDE PACK ASSY WAS REPLACED IAW A320 AMMTASK 25-62-44-000-012-A AND 25-62-44-400-007-A . AFTER THE SYSTEM TEST WAS FOUND OK. THIS WORK IS COVERED BY COOPESA JOB A1N152 ITEM 2-5 P/N OFF D30664-515 S/N OFF A7663 P/N ON D30664-515 S/N ON M16922.
DURING ALLEGIANT TASK INSPECTION 53-260-003 REAR FUSELAGE AFT PASS DOOR LH SIDE FR68 DOORSTOP FITTING # 1 LOWER I/B HOLE HAS BEEN FOUND WITH CRACK INDICATION. COOPESA PERFORMED REPAIR IN ACCORDANCE A320 SRM TASK 53-41-12-300-010. THIS REPAIR IS COVERED WITH COOPESA JOB A1N152 ITEM 2-17.
DURING ALLEGIANT TASK INSPECTION 53-260-003 REAR FUSELAGE AFT PASS DOOR RH SIDE FR66 DOORSTOP FITTING # 1 LOWER I/B HOLE HAS BEEN FOUND WITH CRACK INDICATION. COOPESA PERFORMED REPAIR IN ACCORDANCE A320 SRM TASK 53-41-12-300-010. THIS REPAIR IS COVERED WITH COOPESA JOB A1N152 ITEM 2-16.
EPSU (12WL) REQUIRES REPLACEMENT DUE TO EMERGENCY LIGHT OPS CHECK FAILURE. REF NR01000428 / REMOVE AND REPLACED EPSU OPS CK GOOD. REF AMM33-51-38-000-001A"
FWD MEGAPHONE VOLUME KNOB BROKEN. / REMOVED AND REPLACED FORWARD MEGAPHONE IAW AMM 25-65-51 PB 201 CONF 00, OPS CHECK GOOD."
EPSU TEST SHOWS BATTERY (10WL) FAULT. REMOVED AND REPLACED BATTERY (10WL), IAW AMM 33-51-38 PB 401. OPERATIONS CHECK GOOD.
12WL EPSU BATTERY FAILED OPERATIONS CHECK. REPLACED EPSU BATTERY 12WL, IAW AMM 33-51-38. OPERATIONS CHECK GOOD.
PERFORMED EPSU SYSTEM TEST, RECEIVED MESSAGE "BAT/ EPSU (10WL) FWD L AND BAT/EPSU (11WL) EMER L. REMOVED AND REPLACED BOTH EPSU BATTERY (10WL FWD) AND (11WL EMER L), IAW AMM 33-51-38. OPERATIONS CHECK GOOD.
FWD MEGAPHONE INOP. R&R MEGAPHONE.