- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 7381
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- February 3, 2025
- Certificate issued
- May 21, 2020
- Expires
- May 31, 2027
- Mode S code
- A3524E
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 N313DNMatched 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 N313DNMatched 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 DALA2025062004648Proximity Sensor · faultedDECLARED EMERGENCY DUE TO LANDING GEAR NOT EXTENDING AFTER SELECTOR HANDLE WAS MOVED DOWN. SYSTEM WAS FAULTING THE RH GEAR DOOR OPEN PROX SENSOR. ALT. GEAR EXTENSION PERFORMED. CORRECTIVE ACTION: DEFERRED GEAR RETRACTION SYSTEM PER MEL. AIRCRAFT WILL POSITION SDR DALA2024111911022Unknown · odorSHIP 3013 -ATB- DUE TO DIRTY SOCK SMELL. CORRECTIVE ACTION: APU INSPECTED, RAN ENGINES SEVERAL MINUTES AND UNABLE TO DUPLICATE SMELL. R/R RECIRCULATION FILTERS. OK FOR SERVICE. (LP 6516092)SDR DALA2024032603834Light · no testAIRCRAFT 3013, EMERGENCY SEAT MOUNTED LIGHTING INOP. CORRECTIVE ACTION: RESECURED LIGHTS IAW A321 AMM 33-52. OPS CKS NORMAL. (LP 0262012)SDR DALA2023021701235None · noneAT GATE FLT ATTENDANT CALLED AND SAID UPON LANDING BACK BY 2L HAZE AND SMELL LIKE BURNED PLASTIC AND DOORS BETWEEN 3L AND 4L WERE WORST.RAN PACKS AND CONFIGURED CABIN FWD & AFT AND COCKPIT TEMP. SELECTORS TO FULL HOT, FULL COLD AND 60 DEG., RAN THOSE CONFIGURASDR DALA2022122808447Door · missingTOILET SERVICING AND DRAINAGE DOOR MISSING.SDR DALA2022120107686Skin · scratchedSCRATCH ON EXTERNAL SKIN LOC. FR 23 TO FR 24 BTW STR 42 L TO STR 43 AT LOWER FUSELAGE. COMPLIED WITH ER/A 603753-14 REV ORIGINAL. APPROVED DATE 27 NOV 22, MATCHES WITH ALL STEP ON PRI 603753-14 REV 0 AND REV 1. IT ISBEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONSDR DALA2022120107685Skin · scratchedSCRATCH ON EXTERNAL SKIN LOC. FR 25 TO FR 26 BTW 39 L TO STR 40 L AT L OWER FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOC. FR 25 TO FR 26 BTW 39 L TO STR 40 L AT LOWER FUSELAGE AS PER A321 SRM53-11-11 -300-090 FIG. 001 SHEET 01 MESURES OF REWORKED SDR DALA2022112907612Support · corrodedCORROSION LOWER SILL LOC. FR 68 AT LEVEL STR 23 R/H AT AFT GALLEY AREA. PERFORMED REPAIR ON LOWER SILL AREA FR68 AT LEVEL STR23 RH SIDE AS PER A321 SRM 53-41-14-300-001 REPAIR PRINCIPLE 7 FIGURE 001SHEET 04. MEASURED OF CORROSION IS DEPTH: 0.033 INCH TOOL USEDSDR DALA2022112907613Damper · no testDONT PASS TEST DAMPER PASSENGER CREW DOOR 831 IN PASSENGER CABIN. REPLACED DOOR DAMPER ON PASSENGER CREW DOOR 831 AS PER A 320 FAM AMM 52-11-14-000-001-B AND 52-11-14-400-001-B TOOL USED TORQUEP /N QD2R200 S/N 0219122698 DUE DATE 08-OCT-23 HIGH REGULATOR P/N 8SDR DALA2022090705974None · noneWHILE PERFORMING BIRDSTRIKE INSPECTION REF LOG 9180304 FOUND DENT DAMAGE RT SIDE FWD FUSELAGE. ASSOCIATED ER/A 14-602057 ADDED FOR AC 3013 C/W FUSELAGE SKIN DENT ERA 602057-14 REV A. ON NR. 1, 2, & 3. (LP# 9180308)SDR DALA2022062904535None · noneELECTRICAL/BURNING SMELL BEGAN ABOUT 10 MINS PRIOR TO PUSHBACK. PRESENT IN COCKPIT AND FORWARD GALLEY AREA. NO OTHER ABNORMALITIES NOTED. FUMES DISAPATED IN ABOUT 10 MINS. ACCOMPLISHED WORK CARD 0550-2002, IDENTIFY AND TROUBLESHOOT SMOKE AND FUMES IN COCKPIT ASDR DALA2021070703762Bottle · leakingDOOR ASSIST BOTTLE DOSENTAT HOLD PRESSUR. REMOVED DOOR DAMPENER (EMER DPER CYLINDER PER A319-320-321 AMM 52-11 (977514) DEPT 525-RII -OK TO INSTALL DOOR ASSIST ACTUATOR QC 1506 845686, INSTALLED L1 DOOR DAMPENER /EMER- OPS CYLINDER PER A321 AMM 52-11 (460188) SDR DALA2022042803010None · noneR 1 DOOR LOWER AFT CORNER HAS BEEN PERMEMANT REPAIRED PER RI 577423-14 DATED 18 APR 19 15:00 AND PER A 321 SRM 52-10-00-300- 003 AND REF LOG 5808112. FWD TO MONITOR REF A321 SRM 52-10-00-300-003 REPAIR CATEGORY B REQUIRES INSPECTION AT 60,000 FC PER A321 SRI 5SDR DALA2018061944065Lens · missingL1 DOOR ENTRANCE LOWER EMERGENCY EXIT LENS MISSING, INSTALLED A LENSSDR DALA2018033102170Connector · disconnectedFLOOR EMERGENCY LIGHT AT SEAT 11ABC INOPERATIVE. CONNECTOR FOUND DISCONNECTED AT THE SEAT TRACK RACE WAY CONDUIT, CONNECTED THE CONNECTOR.
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.