- Registered owner
- Umb Bank Na Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 9582
- Year built
- 2020
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- November 13, 2020
- Certificate issued
- November 13, 2020
- Expires
- November 30, 2027
- Mode S code
- A01F0D
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 N107DNMatched 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 N107DNMatched 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 · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DALA2026081004599Seat Track · corrodedCORROSION SEAT TRACK -Y765 BTW FR64 TO FR66 AT AFT GALLEY AREA (SSI 5 34147). REPLACED SEAT TRACK -Y765 AND FASTENERS LOC. BTW FR64 TO FR66, AS PER SRM 51-72-11, A321 SRM 51-42-11, DWG D53472909, ISSUE: K, AND D53472903, ISSUE: Q. (LP 1748028 - AIRCRAFT WAS SDR DALA2026080904591Seat Track · corrodedCORROSION SEAT TRACK -Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA (SSI 534147). REPLACED SEAT TRACK - Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA IAW SRM 51-42-11 AND DWG D53472001, ISSUE: Y, DWG D53474250, ISSUE: V, DWG D53474180, . (LSDR DALA2025092306949Oven · failedAIRCRAFT 1007, OVEN 104 IN FWD GALLEY WAS USED TO WARM UP BREAD FOR ONLY 5 MINUTES. STARTED TO SMELL AN ELECTRICAL BURNING SMELL, THEN THE SCREEN GAVE AN ERROR MESSAGE. SHUT OVEN 104 DOWN. CORRECTIVE ACTION: REPLACED OVEN 104 REF A321 AMM 25-35-19. OPS CHK NMLSDR DALA2024062606520Door · damagedAIRCRAFT 1007, WHILE ON THE LINE AT BOS, MTC REPORTED DAMAGE TO THE L4 (REAR LEFT) PASSENGER/SERVICE DOOR. THE DAMAGE CONSISTS OF A SINGLE DENT ON THE AFT LOWER CORNER OF THE DOOR, CAUSING A 0.5-INCH DEFLECTION INWARD AND SPANNING AN AREA 5 INCH LONG AND 1 5/1SDR DALA2023101808587Unknown · unknownLH FLAP INTERCONNECT STRUT HAS CORROSION. REQUIRES REPLACEMENT. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0229:2751-9202/002 00267 REPLACED LH FLAP INTERCONNECT STRUT PER A321 AMM 27-51-44 . UNSUCCESSFUL PARTS CHANGE SENT TO RECORDS 32583 FORCED PARTS RECOSDR DALA2023101808586Unknown · unknownRH FLAP INTERCONNECT STRUT HAS CORROSION. REQUIRES REPLACEMENT. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0229:2751-9202/001 00266 REPLACED RH FLAP INTERCONNECT STRUT PER A321 AMM 27-51-44. STRUT, INTERCON OFF 30-2751-9-0002 11007 ON 30-2751-9-0002 20776. SDR DALA2023040402602Unknown · unknownSHIP 1007 - ATO - DUE TO BRAKES SYS 2 FAULT. CORRECTIVE ACTION: CREW COMPLIED WITH QRH PROCEDURES AND RESET SYSTEM. OK TO CONTINUE. (4124242)SDR DALA2022100506483None · noneSHIP 1007 -ATB- DUE TO SUSPECTED #2 ENGINE STALL. CORRECTIVE ACTION: PERFORMED BORESCOPE INSPECTION OF 4TH STG LPC, HPC, HPT AND 1ST STG LPT PER AMM WITH NO FINDINGS. INSPECTED MCD'S AND 4TH STG LPT WITH NO FINDINGS. REPLACED IP CHECK VALVE AS PRECAUTIONARY. (
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