- Registered owner
- Umb Bank Na Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 10088
- Year built
- 2020
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- October 8, 2020
- Certificate issued
- October 9, 2020
- Expires
- October 31, 2027
- Mode S code
- A01B56
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 N106DNMatched 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 N106DNMatched 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 · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DALA2026080404499Hinge Fitting · wornWEAR BEARING HINGE FITTING 1,2,3,4,5 ON LT ELEVATOR HORIZONTAL. REPLACED FITTING 1,2,3,4,5 ON LH ELEVATOR HORIZONTAL AS PER FAM AMM 55-16-42-000-001-A AND AS PER A320 FAM AMM 55-16-42-400-001-A. (LP 1732785 - AIRCRAFT WAS GROUNDED)SDR DALA2026073004396Bushing · migratedMIGRATED BUSHING AFT LUG RH MLG ACTUATOR FITTING. CORRECTIVE ACTION: REPAIRED PER ERA 635754-14AD REV ORIGINAL. (1727287) AIRCRAFT WAS GROUNDED.SDR DALA2026073004398Strut · corrodedCORROSION INTERCONNECTING STRUT IB FLAP ON LH WING. CORRECTIVE ACTION: REPLACED STRUT PER A321 AMM 27-51-44. (1695840) AIRCRAFT WAS GROUNDED.SDR DALA2025050803566Skin · damagedSHIP 1006 WHILE SEARCHING FOR L/L MON OF LIGHTNING STRIKE FOUND UNDOCUMENTED LIGHTNING STRIKE FWD OF FR 52 NEAR STGR 6R. CORRECTIVE ACTION: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 014-0001:00-0505-8-8536/005 00024 SDR DALA2025050803565Skin · damagedSHIP ER/A 626079-14 SECTION I REPAIRED LIGHTNING STRIKE DAMAGE ON LAP SPLICE S-6R, BETWEEN FR\47.5 AND FR57. CORRECTIVE ACTION: ER/A 626079-14 SECTION II REPAIR TO BE ACCOMPLISHED WITHIN 200 FLIGHT CYCLES FROM SECTION I ACCOMPLISHMENT. (0943413)SDR DALA2025041502943Battery · no testSHIP 1006 DURING C PLUS MOD FOUND EMERGENCY PATH LIGHTS OUT AT 15ABC AND 16ABC. CORRECTIVE ACTION: PERFORMED BITE. FOUND 11WL EMERG BATT INOP. R/R 11WL BATT PER A321 AMM 33-51. EMERGENCY PATH LIGHT OPS NML. (6541996)SDR DALA2024082008285Light · damagedAIRCRAFT 1006, EPL ASSEMBLY DAMAGED AND HANGING AT SEAT 36ABC. CORRECTIVE ACTION: REPLACED EPL ASSEMBLY AT 36ABC. (LP 0512001)SDR DALA2023011200240Unknown · odorJUST PRIOR TO TOP OF DESCENT, F/A'S REPORTED THE RETURN OF THE BURNT PLASTIC, POSSIBLY FROM ROW 3 AND 4. MCC NOTIFIED 2210Z. FL360. PERFORMED T/S OF ODOR IN CABIN PER AMDS W/C 0550-2002 FOR TYPE 9 MISCELLANEOUS CONDITION FWD CABIN, FIGURE 2. NO TROUBLE FOUND. SDR DALA2023011000202Unknown · odorLEVEL FLIGHT FL350 FA REPORTED A BURNING ODOR IN FC CABIN POSSIBLE ROW 3CD. NO EVIDENCE OF ODOR ON ARRIVAL. DEBRIEFED CREW AND ODOR LOCALIZED TO ROW 4CD. NO TROUBLE FOUND. C/W ODI STEPS PER A321 2172. C/W WORK CARDS 0550-2002 TYPE 9 FWD CABIN. ALL CKS GOOD.SDR DALA2022071204852None · noneFCTL FLAPS LOCKED ALIGNMENT FAULT FLAPS STUCK AT FLAPS 2 QRH PROCEDURES COMPLETED. LAST LEG FAULTS FLP1 CHK LH MECH DRIVE AND FLP2 CHK MECH DRIVE AND CHECK LH DRIVE INTEGRITY. T/S PER A-321 TSM 27-51-00-810-818 -A NO TROUBLE FOUND(273001). FLAP TRANSMISSION SESDR DALA2021111607074None · noneON CLIMB OUT HAD LOUD POPPING SOUND AND SMALL VIBRATION START AND CONTINUE TO GET LOUDER AS WE CLIMBED. ALL ENGINE PARAMETERS WERE NORMAL. GEAR DOORS WERE UP AND LOCKED. ON DESCENT WHEN ENGINES WENT TO IDLE, POPPING SOUND WENT AWAY AND CAME BACK WHEN ENGINE POSDR DALA2021070103602Unknown · odorDURING DESCENT SMOKE LAV SMOKE ECAM MOMENTARILY. LAV INDICATION LIGHT DID NOT ILLUMINATE HOWEVER PAX SAID MID-LAV SMELLED OF SMOKE. LAV INSPECTED, NO RESIDUE NOTED. INSPECTED MID LAV. NO TRACE FOUND. FALSE ALARM AS NOTED BY FLT CREW. OPS TESTED LAV SMOKE DETEC
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