- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 8207
- Year built
- 2018
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- February 11, 2026
- Certificate issued
- April 16, 2020
- Expires
- April 30, 2030
- Mode S code
- A3E525
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 N350DNMatched 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 N350DNMatched 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 · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DALA2025110408055O-Ring · leakingATB- RETURNED TO FLL FOR MUSTY SMELL IN COCKPIT AFTER TAKEOFF. FOUND OIL BEHIND #2 ENGINE NOSE SPINNER, REPLACED NBR 2 ENGINE LPT SHAFT PLUG O'RINGS. COMPLIED WITH ENGINE 2 DECONTAMINATION OF BLEED AIR DUCTING SYSTEM PER A321 AMM 36-11-00-615-801-A01 AND ECSSDR DALA2025010800176Elec Connector · disconnectedAIRCRAFT 3050, ROWS 3,4,17,18,21,22 EELS CLEAR LIGHTS INOP. CORRECTIVE ACTION: RECONNECTED CP TO LIGHTS IN SEAT ROWS 17,18,21,22 CKS GOOD ROWS 3 AND 4 NOT RECIEVING POWER 634270. REPLACED PWR SUPPLY FOR SEATS 3,4 ALL CKS GOOD ON EMERGENCY LIGHTS TEST REF A321 SDR DALA2024041904609Shear Plate · crackedAIRCRAFT 3050, CRACK SHEAR PLATE STR 23 L BTW FR69 TO FR70 AT AFT GALLEY AREA. MEASURES OF CRACK AND MEASURES ARE: L: 0.204 INCHES. CORRECTIVE ACTION: INSTALLED NEW SHEAR PLATE AND BRACKETS (3 E/A) LOCATED STR 23LH BTW FR 69 TO FR 70 AT AFT GALLEY AREA AS PER SDR DALA2024041304392Shear Plate · crackedAIRCRAFT 3050, CRACK SHEAR PLATE STR 23 R BTW FR69 TO FR70 AT AFT GALLEY AREA. MEASURES OF CRACK IS L: 0.911 INCH. CORRECTIVE ACTION: REPLACED SHEAR PLATE AND FASTENERS LOCATED STR 23R BTW FR 69 TO FR 70 AT AFT GALLEY AREA AS PER A321 SRM 51-42-11 AND DWGD5347SDR DALA2024041304391Floor Support · corrodedAIRCRAFT 3050, CORROSION FLOOR BEAM +Y765 BTW FR66 TO FR70 AT AFT GALLEY AREA. MEASURES OF CORROSION ARE: L = 0.908 INCH, W = 0.600 INCH CORRECTIVE ACTION: REPLACED FLOOR BEAM Y765 LOCATED BTW FR66 TO FR70 AT AFT GALLEY AREA AS PER A321 SRM 51-42-11; DWG: D534SDR DALA2024011700684Button · brokenSHIP 3050 LAV 205 O2 DOOR TEST BUTTON BROKEN. CORRECTIVE ACTION: REPLACED TEST LEVER AND SPRING AT LAV 205 O2 GEN DOOR PER CMM 35 -22-40. OPS CHK NML. OK FOR SVC. (KK482624) (4334342)SDR DALA2023092607932Unknown · unknownG4 GALLEY COMPARTMENT #412 HAS AREA SHOWS SMALL DELAMINATION LESS THEN 9"X3" REF. FCN 30-0525-8-0605 / WORK CARD 2530-01591- 01B A/D. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0001:2530-01591-01B/001 00001 C/W ONSDR DALA2023022301371None · noneCORROSION ON ZEE CHANNEL STA 947, RH STR25, WL150. CORROSION ON ZEE CHANNEL STA 947, R/H STR 25 WL150 CHECKS OUT OF LIMITS IAW B737 SRM 53-00-53-1A-2 TABLE 101 PARA 4A DETAIL D FIG 103, REMOVED AND REPLACED ZEE CHANNEL STA 837 TO STA 947 RBL20. (LP# 2637658)SDR DALA2021120607517None · noneSHIP 3050 R2 ENTRY DOOR ARMING LEVER HARD TO OPERATE. CORRECTIVE ACTION: RIGGED R2 DOOR ARMING SYSTEM PER A321 AMM 52-22-00. OK FOR SERVICE (2042188)SDR DALA2021092805832A/C Pack · odorAFTER TAKEOFF BRINING SMELL BEGAN RAN QRH ISOLATED #2 PACK AND SMELL WENT AWAY DURING ADDITIONAL TROUBLESHOOTING PACK 2 CAUSED SMELL TO RETAIN CONTINUED WITH PACK 2 OFF. DISCREPANCY TRANSFERRED RO NRF SEE LOG 1961315 ALL NO GO ODI PROCEDURES C/W. CORRECTIVE ACSDR DALA2021033001898Slat · damagedSHIP 3050 - ATB - DUE TO THE LEADING EDGE SLATS STUCK EXTENDED AT POSITION 1. AIRMAN FAULTED A MECHANICAL SYSTEM JAM. FOUND LEADING EDGE PANEL 522AT HARDWARE BINDING LEFT #2 SLAT. FIRST FLIGHT POST PANEL REMOVAL FOR AD INSPECTION OF LP FUEL S/O VALVE. CORRECTISDR DALA2020061002460Power Supply · no testEPSU (14WL) FAILS EPSU SYSTEM TEST, REPLACED EMERGENCY POWER SUPPLY UNIT 14WLSDR DALA2018100705926Entertain Sys · malfunctionedFLT ATTENDANTS REPORT ELECTRICAL BURNING SMELL FROM PED AT L1 IN FORWARD CABIN, FOUND ARCING ON RIGHT SIDE OF THE HDD-OML COVER R&R HDD OML. IFE SYSTEM PART RD-FA1173-01 SN OFF: Q3977.
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.