- Registered owner
- Umb Bank Na Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 7845
- Year built
- 2017
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- February 18, 2025
- Certificate issued
- May 8, 2026
- Expires
- May 31, 2033
- Mode S code
- A384F2
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 N326DNMatched 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 N326DNMatched 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 DALA2025121109056Handle · stuckATB, DUE TO THE FLAP/SLAT CONTROL UNIT HANDLE STUCK AT POSITION 2. FOUND HANDLE TRIGGER SECURING PIN BROKEN. CORRECTIVE ACTION: REPLACED FLAP/SLAT COMMAND SENSE UNIT. (LP 7796736)SDR DALA2024112511214Hydraulic Line · damagedSHIP 3026 - HYD - DUE TO HYD G RSVR LO LVL AND HYD G SYS LO PR ECAM MESSAGES. CORRECTIVE ACTION: FOUND HYDRAULIC SUPPLY LINE AND CLAMP AT ENGINE #1 EDP DAMAGED. REPLACED GREEN EDP HYDRAULIC PUMP, PRESSURE LINE AND CLAMP. OPS AND LEAK CHECK GOOD. (LP 6670196)SDR DALA2024010800236Unknown · unknownSHIP 3026 EMER LIGHT HOLDER AT SEAT 25C BROKEN. CORRECTIVE ACTION: REPLACED EMER LIGHT HOLDER AT SEAT 25C LIGHT OPS CHECKED NORMAL. (4852995)SDR DALA2023081506650Unknown · unknownCORROSION LOWER SILL LOC. FR 67 TO FR 68 R/H AT AFT GALLEY AREA. PERFORMED PERMANENT REPAIR LOC. ON LOWER SILL FRAME 67 TO FRAME 68 RH SIDE AS PER A321 SRM 53-41-14-300-001 FIGURE 001 SHEET 3PRINCIPLE 5, TOOK MEASURE OF CORROSION ARE: P1 L=1.118 INCH, W= 0.668SDR DALA2022051703406None · noneDURING HAIL STRIKE INSP FOUND PREVIOUS REPAIR ON SLAT 4 WITH PART OF FILLER MISSING REF LOG 7753214. REMOVED REMAINING FILLER WIP 890970. HFEC INSPECTION OF DENTED AREA PER A321 NTM 51-10-08. NO CRACKS INDICATIONS. QC5114. REPAIRED LEADING EDGE# SLAT PER A321 SDR DALA2022032502005Handle · failedSHIP 3026 - DIV - TO JFK DUE TO FLAP CONTROL HANDLE FAILURE. FOUND LEVER RELEASE TRIGGER SECURING PIN SHEARED. CORRECTIVE ACTION: REPLACED PIN. (LP# 6178808)SDR DALA2020010800135Brake · failedBRAKES NORM BRK FAULT ECAM MESSAGE ON LANDING RIGHT BRAKES FAILED; FOUND #4 BRAKE SHEARED & ROTATED 180 DEGREES FROM NORMAL POSITION. BOTH HYDRAULIC LINES SEVERED, BRAKE TEMP MONITORING LINE KINKED & CONNECTOR DAMAGED. FWD HYDRAULIC LINE BRACKET UNDER SHIMMY D
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.