- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 9360
- Year built
- 2020
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- January 17, 2020
- Certificate issued
- May 19, 2020
- Expires
- May 31, 2027
- Mode S code
- A4A0D9
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 · 281
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 |
| 1999 | 4 |
| 2000 | 10 |
| 2001 | 7 |
| 2002 | 11 |
| 2003 | 3 |
| 2004 | 15 |
| 2005 | 15 |
| 2006 | 14 |
| 2007 | 15 |
| 2008 | 8 |
| 2009 | 13 |
| 2010 | 6 |
| 2011 | 12 |
| 2012 | 10 |
| 2013 | 14 |
| 2014 | 17 |
| 2015 | 17 |
| 2016 | 22 |
| 2017 | 24 |
| 2018 | 27 |
| 2019 | 20 |
| 2020 | 24 |
| 2021 | 16 |
| 2022 | 21 |
| 2023 | 18 |
| 2024 | 14 |
| 2025 | 22 |
| 2026 | 17 |
See all 421 ADs
Information bulletins that may apply · 6
Advisory, not mandatory.
Airframe · Airbus A321-211
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 N398DNMatched 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 A321-211 aircraft
FAA incident reports
No FAA accident or incident reports matched to N398DNMatched 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 A321-211 aircraft
Service difficulty reports · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DALA2025101607570Lens · brokenBROKEN LENS EXIT SIGN IN DOOR FRAME DOOR L3 AND DOOR FRAME DOOR L4 AT PASSENGER CABIN. REPLACED LENS EXIT SIGN IN DOOR FRAME DOOR L3 AND DOOR FRAME DOOR L4 AT PASSENGER CABIN AS PER A320 FAM AMM 33-51-13-000-001-A STEP 4.A(1)(A) AND AS PER A320 FAM AMM 33-51SDR DALA2024012901233Fan · failedAIRCRAFT 3098, IN DESCENT THROUGH 140 SLIGHT ELECTRICAL BURN SMELL IN COCKPIT AND AFT GALLEY, ALSO RECIEVED AN ECAM ELEC BCL 1 FAULT. CORRECTIVE ACTION: REPLACED GALLET AND LAV EXTRACT FAN, BCL 1 AND BAT 1 PUSH BUTTON SWITCH. (LP 4886546)SDR DALA2024012501138Oil System · overservicedAIRCRAFT 3098, SMELLED ELECTRICAL BURNING ODOR DESCENDING THROUGH 11,000 AND AGAIN SHORT FINAL THROUGH ROLLOUT. PILOTS, DOORS 1, 2, AND 4. CORRECTIVE ACTION: FOUND OVER SERVICED APU OIL AND EVIDENCE OF OIL CONTAMINATION IN BLEED SYSTEM. DEFERRED APU REPLACEMEMSDR DALA2023063005247Unknown · unknownEMERGENCY LIGHT ON SEAT 32C INOP. R/R LIGHT ON SEAT 32C PER AMM 33-51. OPS CHECK NO GOOD. FOUND CONNECTOR UNDER SEAT 32A DISCONNECTED. CONNECTED AS REQUIRED AND OPS CHECK GOOD. OK FOR SVC. (LP# 4814695)SDR DALA2023033102468Unknown · unknownEMERGENCY LIGHT AT SEAT 32 FLOOR INOP. FOUND WIRE PULLED BACK FROM PLUG.REINSTALLED PLUG KS OK. (LP# 4123556)SDR DALA2022070604719None · noneCAPTS LEFT HARNESS SHOULDER STRAP INERTIA REEL WILL NOT UNLOCK. REMOVED COVER FROM INERTIA REEL CLEANED DEBRIS AND DUST FROM REEL OPERATES NORMALLY OK FOR SERVICE. (LP# 9177296)SDR DALA2022061504205Sign · missingL1 DOOR MISSING RUNNING MAN EXIT SIGN LENS. RE-INSTALLED EXIT SIGN LENS REF A321 AMM 33-51. OK FOR SVC. (LP# 9177239)SDR DALA2022030401423None · noneERA 595953-14 REV ORIG AND REV A ISSUED FOR REPAIR AND ONE TIME INSPECTION OF GROUND DAMAGE AT S34R-S35R, FRAME 62. ERA REVISED TO REV 'B' WITH STAGE II DTE COMPLETE. FOLLOW ON ACTION REQUIRED. CCOMPLISH SECTION III PRIOR TO 65,600 FLIGHT CYCLES OR 131,300 FLISDR DALA2021122808113None · noneER/A 595953-14 SECTION I WAS ISSUED FOR FUSELAGE SKIN DAMAGE AT THE AFT FRAME OF THE BULK CARGO DOOR OPENING. SECTION I WAS ACCOMPLISHED DURING SPECIAL VISIT IN MSP 10DEC21 ON N/R 8. FOLLOW ON ACTION IS REQUIRED. ACCOMPLISH SECTION II PERMANENT REPAIR WITHIN 2
STCs that may be installed · 223
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 223 STCs