- Registered owner
- Umb Bank Na Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 2133
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Certificate issued
- October 2, 2026
- Expires
- October 31, 2033
- Mode S code
- A22778
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 370
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1990 | 5 |
|---|---|
| 1991 | 1 |
| 1992 | 6 |
| 1993 | 10 |
| 1994 | 10 |
| 1995 | 4 |
| 1996 | 5 |
| 1997 | 9 |
| 1998 | 20 |
| 1999 | 14 |
| 2000 | 13 |
| 2001 | 8 |
| 2002 | 12 |
| 2003 | 3 |
| 2004 | 23 |
| 2005 | 19 |
| 2006 | 13 |
| 2007 | 14 |
| 2008 | 9 |
| 2009 | 11 |
| 2010 | 6 |
| 2011 | 12 |
| 2012 | 11 |
| 2013 | 16 |
| 2014 | 18 |
| 2015 | 23 |
| 2016 | 24 |
| 2017 | 23 |
| 2018 | 31 |
| 2019 | 23 |
| 2020 | 29 |
| 2021 | 15 |
| 2022 | 22 |
| 2023 | 18 |
| 2024 | 15 |
| 2025 | 21 |
| 2026 | 17 |
See all 533 ADs
Information bulletins that may apply · 6
Advisory, not mandatory.
Airframe · Airbus A320-214
SAIB NE-19-03Escape Slide Maintenance Tasks and Intervals - JASC 2565SAIB NM-15-02Cabin Equipment/FurnishingsSAIB NM-14-21Communications: Honeywell RTA 44D VHF TransceiversSAIB NM-13-24Air Conditioning System: Air Distribution FanSAIB NM-13-03Hydraulic Power System: Power Transfer UnitSAIB NM-06-57Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.NTSB investigations
No NTSB investigations matched to N238NVMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Airbus A320-214 aircraft
FAA incident reports
No FAA accident or incident reports matched to N238NVMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Airbus A320-214 aircraft
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR EE4Y2025032722083Window Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-212-020 COCKPIT LATERAL WINDOW FRAME 4RHS STIFFENER WITH CRACK WAS FOUND. THE COCKPIT LATERAL WINDOW FR4 RHS STIFFENER WAS REPAIRED FOLLOW REPAIR INSTRUCTIONS AS PER A320 SB 53-1043 REV 02 AND RI R53113452 ISSDR WX0A2024101432199Warning Light · false activation(AIRCRAFT NOT GROUNDED) R1 DOOR INDICATION OPEN ON CLIMB OUT AND APPROACH NO PRESSURE CHAMGES / PREFORMED TSM 52-11-00-810-803-A. REPLACED WARNING LIGHT PANEL (1WN2) RELAY PWR SPLY SWITCHOVER (12WN) PROXIMITY SWITCH (13WV2) CANNOT REPRODUCE FAULT ON GROUND. OPSDR WX0A2024100432194Warning Message · false activation(AIRCRAFT NOT GROUNDED) R1 DOOR SHOWED OPEN ON FLIGHT DESCENT. / PERFORMED OPS CHK OF DOOR WARNING SYSTEM OF R1 DOOR, AND PERFORMED PRESSURIZATION TEST. REF AMM 52-71-00-710-001-A AND 05-53-00-780-002-A01. NO DEFECTS NOTED AT THIS TIME OK FOR SERVICE."SDR WX0A2024092532188Receptacle · corroded(AIRCRAFT NOT GROUNDED) PASSING 10,000 R1 DOOR OPEN INDICATION ON ECAM. PRESSURIZATION NORMAL FOR FLIGHT / PER TSM 52-11-00-810-803-A FOUND CORROSION ON RECEPTACLE OF PROX SENSOR 13WV2. REMOVED AND REPLACED PROX SENSOR 13WV2 IAW AMM 52-71-11-000-001 AND AMM 5SDR EE4Y2023121018948Door Frame · crackedDURING ACCOMPLISHMENT ALLEGIANT TASK CARD 53-260-003 AND AD 2022-22-04, IT WAS FOUND ATFR68 LHS DOOR STOP FITTING # 6 FASTENER HOLES AREA WITH CRACK INDICATION. THE PERMANENT REPAIRWAS ACCOMPLISHED IAW A320 SRM 53-41-12-300-008 AND SRM 53-41-12-300-009.THE REPSDR EE4Y2023121018947Door Frame · crackedDURING ACCOMPLISHMENT ALLEGIANT TASK CARD 53-260-003 AND AD 2022-22-04, IT WAS FOUND AT FR68 DOOR STOP FITTING # 1 FASTENER HOLES AREA WITH CRACK INDICATION. THE PERMANENT REPAIR WAS ACCOMPLISHED IAW A320 SRM 53-41-12-300-008 AND SRM 53-41-12-300-010.THE REPAISDR WX0A1900010031766Harness · unknown(EMERGENCY DECLARED) ON APPROACH LEFT MAIN LANDING GEAR UNLOCK LIGHT//FOUND CONNECTOR AT PROC SWITCH (15GA) DAMAGED. REMOVED &INSTALLED NEW 1M HARNESS REF AMM 32-11-43-000-001A & 32-11-43-400-002A. OPS CK & LK CK GOOD. NO DEFECTS NOTED AT THIS TIME"SDR WX0A2021051273711Battery Pack · no testALL FOUR EPSU BATTERIES FOUND BAD DURING TEST. / REMOVED AND REPLACED ALL FOUR EPSU BATTERIES IAW AMM 33-51-38"SDR WX0A2020081073551Cids · malfunctionedAFTER LANDING RECEIVED UNCOMMANDED PA AND INTERPHONE ACTIVATION WITH ASSOCIATED CHIMES. EMER EVAC HORN ALSO CAME ON INTERMITTENTLY. / REMOVED & REPLACED CIDS DIRECTOR IAW AMM 23-73-34. OPS CHECK GOOD NO DEFECTS NOTED."SDR WX0A2020080373544Warning Light · false activationAFTER LANDING EMERGENCY CALL WAS CONTINUOUS UNTIL PLANE SHUTDOWN. PERFORMED TSM 23-73-00-810-955-A 4B(3). R & R PUSH BUTTON SWITCH (3WP) FOR EVAC COMMAND IAW ASM 25-63-01. PERFORMED BITE TEST OF SIDS IAW 23-73-00-740-005-A. NO FAULTS NOTED AT THIS TIME. MONSDR WX0A2020073173536Cids · malfunctionedEMERGENCY EVAC HORN KEEPS SOUNDING IN TH COCKPIT UNCOMMANDED. REMOVED & REPLACED (CIDIS) DIRECTOR(S) 101RH&102RH BITE TEST GOOD NO FAULTS NOTED AT THIS TIME REF AMM 23-73-34"SDR WX0A2020062973520Epsu · no testEPSU BATTERY FIN# 10WL FAILED EPSU BAT CAP TEST / REPLACED EPSU BATTERY"
STCs that may be installed · 301
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 301 STCs