- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 8200
- Year built
- 2018
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- February 24, 2026
- Certificate issued
- April 15, 2020
- Expires
- April 30, 2030
- Mode S code
- A3C8CB
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 N343DNMatched 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 N343DNMatched 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 · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DALA2026041602410Door · openSHIP 3043 - ATB - DUE TO A THUMPING NOISE HEARD AT THE NOSE OF THE AIRCRAFT AFTER LIFTOFF. CORRECTIVE ACTION: EXTERNAL POWER CONNECTION ACCESS DOOR WAS FOUND OPEN. COMPLIED WITH SECTION I OF ER/A 633751-14, EXTERNAL POWER TAPED CLOSED AND LABELED AND PLACED ONSDR DALA2026040302151Shear Tie · damagedSHEAR TIE AT FR74 P33 RIGHT DAMAGED. REPLACED SHEAR CLIP PER SRM 53-51-29-300-002 AND A321 DWG D53571523008. (LP 1525339)SDR DALA2026040302150Skin · dentedTHE FWD RH DENT IS OUTSIDE OF LIMITS DUE TO BEING PARTIALLY WITHIN AN EXCLUDED ZONE AND THE AFT RH DENT IS OUTSIDE OF LIMITS DUE TO THE MAX DEPTH BEING GREAT THAN 0.020. MAINTENANCE CONFIRMS THE DAMAGE TO THE TWO (2) SHEAR TIES. FIRST SHEAR TIE IS AT FRAME 73SDR DALA2024042004611Shear Plate · crackedAIRCRAFT 3043, CRACK SHEAR PLATE STR 23 L BTW FR69 TO FR70 AT AFT GALLEY AREA. MEASURE OF CRACK IS L:0.993 INCH. REPLACED SHEAR PLATE STR 23L LOC. BTW FR69 TO FR70 AT AFT GALLEY AREA AS PER A321 SRM 51-42-11-801 AND A321 SRM 51-72-11-911-001AND DWG: D5347418SDR DALA2024041904610Fitting · corrodedAIRCRAFT 3043, CORROSION CENTER FITTING LOC STR 23L AND BTW FR66 TO FR68 AFT GALLEY AREA. MEASURE OF CORRODED AREA IS L= 1.105 INCHES W= 0.331 INCHES. CORRECTIVE ACTION: REPLACED CENTER FITTING AND FASTENERS.LOC STR23L AND BTW FR66 TO FR68 AFT GALLEY AREA AS PSDR DALA2024040404056Shear Plate · crackedAIRCRAFT 3043, CRACK SHEAR PLATE STR 23 R LOC BTW FR69 TO FR70 AT AFT GALLEY AREA. MEASURE OF CRACK IS L 0.202 INCHES TOOL USED CALIPER P/N 500-196-30 S/N A23325692 DUE DATE 24-DEC-24. CORRECTIVE ACTION: REPLACED SHEAR PLATE LOCATED FR 69 TO FR 70 STRG 23 R ATSDR DALA2024011000468Unknown · unknownSHIP 3043 1R CABIN DOOR DOES NOT INDICATE "ARMED" ON FLT DECK PANEL OR F/A PANEL. CORRECTIVE ACTION: FOUND PROX SWITCH 4WN2 IN TOO FAR CONDITION. ADJUSTED SAME REF A321 AMM 52-71. INDICATION NOW OPS NML. (5076546)SDR DALA2023112309660Unknown · unknownSHIP 3043 SLIDE DISARMING PIN ATTACHING LANYARD MISSING OR DAMAGED / LOCATIONS:605. CORRECTIVE ACTION: R/R LANYARD AT 3L PER A321 AMM 52-73. (0067988)SDR DALA2023021001080None · noneEXHAUST/OIL SMELL WHEN APU BLEED TURNED ON. COMPETED CARD 0550-2002 FOUND TO BE TYPE 1. RAN APU AND INSPECTED WTIH BLACK LIGHT. FOUND SMALL LEAK AT APU OIL COOLER. REPLACED ORING ON COOLER BYPASS VALVE. RAN APU FOR 1 HOUR WITH NO LEAK OR SMELL. COMPLETED CARD SDR DALA2022031801824None · noneCATERING LIFT TRUCK INTO R1 DOOR RESULTING SKIN DAMAGE. NDS DOOR RIG CK. TRIMMED DAMAGED SECTION OF SKIN PER A321 SRM 52-10-00-300-003 FIG 1 AND BEGAN DRILLINGDOUBLER (367524) FABRICATED REPAIR PARTS PER AIRBUS 321 SRM 53-10-00-300-003 FIG 1 ANODIZED AND PRIMESDR DALA2018091205569Light · inoperative29 ABC AND 2L LAV EMERGENCY LIGHTS INOP. REPLACED 29ABC SEAT AND 2L LAV EMERGENCY PATH LIGHTS.
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.