- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 8233
- Year built
- 2018
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- February 4, 2026
- Certificate issued
- June 11, 2025
- Expires
- June 30, 2032
- Mode S code
- A3DF1E
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56-5B2 model are included below.
On this page
Airworthiness directives that may apply · 236
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 | 2 |
| 1998 | 2 |
| 2000 | 3 |
| 2001 | 4 |
| 2002 | 5 |
| 2003 | 1 |
| 2004 | 12 |
| 2005 | 8 |
| 2006 | 5 |
| 2007 | 15 |
| 2008 | 9 |
| 2009 | 12 |
| 2010 | 6 |
| 2011 | 11 |
| 2012 | 8 |
| 2013 | 14 |
| 2014 | 16 |
| 2015 | 17 |
| 2016 | 21 |
| 2017 | 24 |
| 2018 | 26 |
| 2019 | 19 |
| 2020 | 21 |
| 2021 | 15 |
| 2022 | 20 |
| 2023 | 18 |
| 2024 | 14 |
| 2025 | 22 |
| 2026 | 17 |
See all 368 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 CFM56-5B2 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 N349DXMatched 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 N349DXMatched 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 · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DALA2026011400338Engine · failedIFSD- DIVERSION TO MCI DUE TO RIGHT ENGINE FAILURE AND IFSD. ENGINE CHANGE REQUIRED DUE TO METAL IN THE TAILPIPE. REPLACED NBR 2 ENGINE. (LP 8168908, 1384104)SDR DALA2025042203126Light · inoperativeSHIP 3049 1B EMERGENCY IGHT INOP. CORRECTIVE ACTION: REPLACED LIGHT ASSY CKS OK (7156208)SDR DALA2025042203125Light · inoperativeSHIP 3049 04B EMERGENCY LIGHT INOP. CORRECTIVE ACTION: REPLACED MISSING EMERGENCY LIGHT AT SEAT 04B PER A320 AMM 33-50 OPS NML. OK FOR SERVICE. MEL AND PLAC REMOVED (7156209)SDR DALA2024120311426Brake · overheatedSHIP 3049 - ATO - AT 50KTS DUE TO#4 BRAKE OVERHEATING TO ALERT LEVEL. CORRECTIVE ACTION: NO TROUBLE FOUND. (LP 6738692)SDR DALA2024041604501Skin · damagedAIRCRAFT 3049, PERFORATION ON UPPER SKIN SLAT 1 AT 6 INCH NEAR INBOARD EDGE ON LH WING. CORRECTIVE ACTION: PERFORMED SECTION I REPAIR INSTRUCTIONS ON UPPER SKIN SLAT 1 INBOARD EDGE ON LH WING AS PER ER/A 616878-14 REVISION ORIGINAL APPROVED DATE: 15-APR-24 HASSDR DALA2024032903922Floor Support · corrodedARCRAFT 3049, CORROSION FLOOR BEAM +Y765 BTW FR66 TO FR70 AT AFT GALLEY AREA. MEASURES OF CORROSION ARE: L= 1.165 INCHES, W= 1.146 INCHES, D=0.064 INCHES. CORRECTIVE ACTION: REPLACED FLOOR BEAM Y765 AND FASTENERS ON AREA LOCATED BTW FR66 TO FR70 AT AFT GALLEY SDR DALA2024032903921Shear Plate · crackedAIRCRAFT 3049, CRACK SHEAR PLATE STR 23 L BTW FR69 TO FR70 AT AFT GALLEY AREA. MEASURE OF CRACK L=1.067 INCH. CORRECTIVE ACTION: REPLACED SHEAR PLATE AND FASTENERS LOCATED AT LEVEL STR 23 L BTW FR69 TO FR70 AT AFT GALLEY AREA AS PER A321 SRM 51-72-11. A321 SRMSDR DALA2024032703850Shear Plate · crackedAIRCRAFT 3049, CRACK SHEAR PLATE STR 23 R BTW FR69 TO FR70 AT AFT GALLEY AREA. MEASURE OF CRACK L= 0.912 INCH. CORRECTIVE ACTION: REPLACED SHEAR PLATE AND FASTENERS LOCATED AT LEVEL STR 23R BTW FR69 TO FR7O AT AFT GALLEY AREA AS PER A321 SRM 51-72-11. A321 SRMSDR DALA2023120609987Unknown · unknownSHIP 3049 EMERGENCY LIGHT AT SEAT 32 ABC INOP. CORRECTIVE ACTION: FOUND ELECTRICAL CONNECTOR UNDER SEAT DISCONNECTED. RECONNECTED (REF. A321 AMM 33-51). (5497454)SDR DALA2023090807382Unknown · unknownODOR PASSING 11,000 FEET LEAVING LAS. 'SWEET' SMELL SIMILAR TO WHAT DEICING FLUID SMELLS LIKE. UPON DECENT INTO SLC, MORE ODOR, THIS TIME A SLIGHT BURNING SMELL. BOTH TIMES ODOR GONE LESS THAN 1 MINUTE. ODOR AGAIN AFTER LANDING. FOUND EVIDENCE OF OIL WETTING #SDR DALA2022080205321None · noneON S/C FOUND R1 DOOR EMER. LIGHT LENS MISSING. INSTALLED NEW R1 LWE EMER LIGHT LENS. REF A321 AMM 33-51. CK'S GOOD. (LP# 9302188)SDR DALA2022061004105None · noneBRAKE NO. 3 TEMP INDICATOR WENT UP EXTREMELY FAST. UP TO 700-800 DEGREES. WHEN PUT LANDING GEAR DOWN ON FINAL. DID GO AROUND TO TROUBLESHOOT AND EVENTUALLY GOT AMBER XXS WHEN COMING BACK TO AIRFIELD. CORRECTIVE ACTION : MEL 32-47-01. (LP# 8662988)SDR DALA2021012500472Smoke Warning · false activationLAV A SMOKE WARNING WENT OFF FOR 5 SECONDS IN FLIGHT. PERFORMED SELF TEST OF SMOKE WARNING SYSTEM OF LAV A, PER A321 AMM 26-17. NO FAULT DETECTED. INSPECTED F/C LAV NO SMELL DETECTED. FIRE EXTINGUISHER BOTTLE STILL IN GREEN BAN. NO 30 DAY HISTORY. A/C OKSDR DALA2019111746734Power Supply · no testWHILE PERFORMING SERVICE CHECK DOING EMERGENCY ESCAPE PATH LIGHTINING TEST THROUGH MCDU SYSTEM TEST PAGE FOUND 3 PAGES OF CLASS 1 FAULTS RELATING TO EPSU (13WL). AFT L, REPLACED EPSU (13WL) AND BATTERYSDR DALA2019072504393Cover · missingEMERG EXIT LIGHT COVER @ 2C MISSING, REPLACED EMERG LIGHT EXIT COVER AS 2R DOOR.
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.