- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 2778
- Year built
- 2006
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- May 31, 2006
- Certificate issued
- August 4, 2021
- Expires
- August 31, 2028
- Mode S code
- A310BB
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56-5B4/P model are included below.
On this page
Airworthiness directives that may apply · 389
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 | 10 |
| 1998 | 21 |
| 1999 | 14 |
| 2000 | 15 |
| 2001 | 9 |
| 2002 | 15 |
| 2003 | 3 |
| 2004 | 23 |
| 2005 | 20 |
| 2006 | 13 |
| 2007 | 16 |
| 2008 | 10 |
| 2009 | 13 |
| 2010 | 8 |
| 2011 | 12 |
| 2012 | 11 |
| 2013 | 17 |
| 2014 | 18 |
| 2015 | 23 |
| 2016 | 25 |
| 2017 | 24 |
| 2018 | 31 |
| 2019 | 24 |
| 2020 | 29 |
| 2021 | 17 |
| 2022 | 22 |
| 2023 | 19 |
| 2024 | 15 |
| 2025 | 21 |
| 2026 | 17 |
See all 556 ADs
Information bulletins that may apply · 8
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.Engine · CFM International CFM56-5B4/P series
SAIB NE-08-17R3Turbine Section - Propulsion Technology LLC Unapproved RepairSAIB NE-12-29Engine Fuel Distribution CFM56-5B LPTACC Fuel ManifoldHistorical bulletins · 1
NTSB investigations
No NTSB investigations matched to N297NVMatched 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 N297NVMatched 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 · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR WX0A2026080332908Wire Harness · damaged(AIRCRAFT GROUNDED) (EMERGENCY DECLARED) THROUGHOT FLIGHT INTERMITENT ECAM EBG 1 THR LEVER DISAGREE / R/R ENGINE CONTROL UNIT (CHANNEL A) HARNESS IAW AMM 71-51-43-00-046-A, REMOVE AND AMM 71-51-43-400-046-A, INSTALL. R/R ENGINE CONTROL HARNESS UNIT (CHANNEL B)SDR WX0A2025012732282Power Supply · inoperative(AIRCRAFT NOT GROUNDED) L/H OVERWING EMERGENCY EXIT LIGHTS INOP / REMOVED AND REPLACED L/H MID CABIN EPSU BATTERY REF AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A OPS CHECK GOOD."SDR EE4Y2024041119894Skin · corrodedDURING THE INSPECTION ACCORDING TO ALLEGIANT WORK CARD: 532180-01-2-001, THE FASTENER HEADS OF THE EXISTING EXTERNAL DOUBLERS WERE FOUND WITH CORROSION AND AFTER REMOVAL WERE FOUND ELONGATED HOLES. AIRBUS PROVIDED REPAIR INSTRUCTIONS AND THE CORRODED AREA WAS SDR EE4Y2024041119893Frame · crackedDURING THE ACCOMPLISHMENT OF ALLEGIANT TASK 53-260-003 RELATED TO AD2022-22-04 AT FR68RH STOP FITTING # 1 IT WAS FOUND A FASTENER HOLE WITH CRACK INDICATION IN THE FRAME ONLY.
AIRBUS PROVIDED REPAIR INSTRUCTIONS AND FR68RH HOLE WAS REPAIRED FOLLOWING AIRBUS SDR EE4Y2024031519619Frame · damagedDURING THE ACCOMPLISHMENT OF ALLEGIANT TASK 53-260-002 AT FR66LH STOP FITTING # 7 WITH OUTBOARD HOLES ELONGATED WERE FOUND.AIRBUS WAS CONTACTED ASKING REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS AND FR66LH HOLES WERE REPAIRED FOLLOW THE REPAIR INSSDR WX0A2024022631966Epsu · no testEXTERIOR LTS FAULT ON EPSU DURING EPSU SYS TEST- FOUND ON WEEKLY T/C / REMOVED AND REPLACED 13WL EPSU IAW AMM 33-51-38 PB 401. OPS CHECK GOOD. NO DEFECTS NOTED."SDR 1E1R2022102600418Frame · damagedDURING DE-MOD OF THE GOGO 2KU SYSTEM, AN ELONGATED HOLE MEASURING 0.305" L X 0.300" W WAS LOCATED AT FRAME 47 BETWEEN STRINGERS 1R AND 2R. PER DRAWING DG211-9932-01, THE FRAME WAS INTENDED TO HAVE A #5 FASTENER AT THE LOCATION NOTED. THE FINAL HOLE SIZE PRIOR SDR WX0A2022062074117Epsu · inoperativeEPSU BATT FAULT INDICATED / REMOVED AND REPLACED FWD L EPSU UNIT IAW AMM 33-51-38Â PBÂ 401. COMPLETED OPS CHECK. NO FAULTS FOUND AT THIS TIME."SDR WX0A2022053174098Epsu · failed inspOPERATINAL TEST OF THE EMERGENCY LIGHTS FAIL. / EPSU BATTERIES REMOVED AND REPLACED IAW AMM 33-51-38-860-060-F AND AMM 33-51-38-400-002-A, PERFORMED EMERGENCY LIGHT OPERATINAL CHECK, OPS CHECKED GOOD."SDR WX0A2021122973911Epsu · failedPERFORM EPSU BIT CH 10WL BATT FAIL. / REMOVED AND REPLACED BATTERY 10WL. OPS CHECKS GOOD REF. AMM 33-51-38 P/B 401."SDR WX0A2021072873799Battery Pack · no testN0019 DURING PREDEPARTURE CHECK FOUND THE EMERGENCY POWER SUPPLY UNIT IS INOP / REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY AT LOCATION 11WL IAW A320 AMM 33-51-38"
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