- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 8258
- Year built
- 2018
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- February 3, 2026
- Certificate issued
- February 14, 2025
- Expires
- February 29, 2032
- Mode S code
- A3DB5E
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56-5B3/3 model are included below.
On this page
Airworthiness directives that may apply · 226
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1996 | 1 |
|---|---|
| 1997 | 1 |
| 2000 | 1 |
| 2001 | 3 |
| 2002 | 2 |
| 2003 | 1 |
| 2004 | 12 |
| 2005 | 8 |
| 2006 | 5 |
| 2007 | 15 |
| 2008 | 8 |
| 2009 | 12 |
| 2010 | 5 |
| 2011 | 11 |
| 2012 | 8 |
| 2013 | 14 |
| 2014 | 16 |
| 2015 | 17 |
| 2016 | 21 |
| 2017 | 24 |
| 2018 | 26 |
| 2019 | 18 |
| 2020 | 21 |
| 2021 | 14 |
| 2022 | 20 |
| 2023 | 18 |
| 2024 | 14 |
| 2025 | 22 |
| 2026 | 17 |
See all 355 ADs
Information bulletins that may apply · 6
Advisory, not mandatory.
Airframe · Airbus A321-213
SAIB NE-19-03Escape Slide Maintenance Tasks and Intervals - JASC 2565SAIB NM-14-21Communications: Honeywell RTA 44D VHF TransceiversSAIB 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 CFM56-5B3/3 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 N348DNMatched 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 A321-213 aircraft
FAA incident reports
No FAA accident or incident reports matched to N348DNMatched 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 A321-213 aircraft
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DALA2026050202781Skin · ground damageAIRCRAFT SUSTAINED GROUND IMPACT DAMAGE DURING REPOSITIONING, RESULTING IN A DENT TO THE LH LOWER LATERAL SKIN PANEL AT FRAME 17LH S33L. TRIMMED OUT THE DENTED FUSELAGE SKIN, MANUFACTURED REPAIR PARTS ER/A 6341-14 PART 3 AND SRM 51-47-20 AND INSTALLED REPAIRSDR DALA2025061304480Actuator · trippedSHIP 3048 - MISC/DE - DUE TO SLATS LOCKED OUT AT ZERO (F/CTL SLATS FAULT ECAM WARNING). CORRECTIVE ACTION: FOUND RIGHT WING #4 SLAT ROTARY ACTUATOR (6087CM) TRIPPED. REPLACED SAME. OK FOR SERVICE. (LP 7481606)SDR DALA2024100109603Skin · dentedAIRCRAFT 3048, DURING SVC CHK FOUND DENT ON RT OUTBOARD FLAP TAB 8" INBOARD OF FAIRING 3C AND 1 5/8" FROM TRANSLATING GDGG. DENT IS 4.5" X 3 3/8" X .1875" DENTED AREA TRANSFERRED TO UPPER SKIN. CORRECTIVE ACTION: REPAIRED DENT REF A321 SRM 57-53-00. COMPLETED SDR DALA2024032503720Shear Plate · crackedAIRCRAFT 3048, CRACK SHEAR PLATE STR 23 R AT AFT GALLEY AREA. MEASURE OF CRACK IS L= 1.065 INCH. CORRECTIVE ACTION: REPLACED SHEAR PLATE LOCATED FR69 TO FR70 AT LEVEL STR23R AFT GALLEY AREA AS PER A321 SRM 51-42-11, SRM 51-72-11 AND DWG D53474180, RELEASE DATESDR DALA2024031203232Shear Plate · crackedCRACK SHEAR PLATE STR 23 L AT AFT GALLEY AREA. MEASURE OF CRACK IS L= 1.109 INCH. REPLACED SHEAR PLATE LOC. STR 23L AT AFT GALLEY AREA AS PER A321 SRM 51-42-11, SRM 51-72-11 AND DWG# D53474180. (LP 0240342)SDR DALA2021110106723None · noneON ARRIVAL DURING LANDING GEAR EXTENSION BRAKES ALTN L REL. ECAM MESSAGE WENT AROUND COMPLIED WITH QRH AND RETURNED FOR LANDING SUBSEQUENT DOWN EXTENSION HAD NO ECAM ALERT NOR STATUS MESSAGES. PERFORMED OPERATIONAL FUNCTION TEST OF THE ALT. BRAKING SYSTEM PER SDR DALA2019121747395Wire Harness · damagedEMERGENCY LIGHT AT 36ABC INOP, FOUND OPEN AT FLOOR HARNESS, RETERMINATED WH5NVR1
STCs that may be installed · 194
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.