- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 7777
- Year built
- 2017
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- February 4, 2025
- Certificate issued
- September 23, 2021
- Expires
- September 30, 2028
- Mode S code
- A388A9
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 · 226
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 | 1 |
| 2000 | 1 |
| 2001 | 3 |
| 2002 | 2 |
| 2003 | 1 |
| 2004 | 12 |
| 2005 | 8 |
| 2006 | 5 |
| 2007 | 15 |
| 2008 | 8 |
| 2009 | 12 |
| 2010 | 5 |
| 2011 | 11 |
| 2012 | 8 |
| 2013 | 14 |
| 2014 | 16 |
| 2015 | 17 |
| 2016 | 21 |
| 2017 | 24 |
| 2018 | 26 |
| 2019 | 18 |
| 2020 | 21 |
| 2021 | 14 |
| 2022 | 20 |
| 2023 | 18 |
| 2024 | 14 |
| 2025 | 22 |
| 2026 | 17 |
See all 355 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 CFM56-5B3/3 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 N327DNMatched 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 N327DNMatched 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 DALA2026082404784Selector Valve · faultedMIC/DE - DUE TO WHEEL NLG STEERING FAULT AND BRAKES SYS 1 FAULT E/W. FOUND STEERING SELECTOR VALVE (7GC) FAULTING. REPLACED SAME. (LP 8817238 - AIRCRAFT WAS GROUNDED)SDR DALA2026072104275Exciter · faultedDIVERSION, DISPATCHED WITH RT IDG ON MEL, APU AUTO SHUTDOWN IN CRUISE AT FL330. RESTART ATTEMPTS NO HELP. DIVERTED TO JAX. REPLACED ECU. NO HELP. REPLACED EXCITER, LEAD AND IGNITER PLUG. CHECKS OK. REPLACED #2 ENGINE IDG. (LP 8739534 - AIRCRAFT WAS GROUNDED)SDR DALA2026072104276Idg · faultedATB - DUE TO ELEC IDG 2 OIL OVHT ECAM MESSAGE. IDG #2 PLACED ON MEL. OK TO CONTINUE. LATER, REPLACED NBR 2 ENGINE IDG PER A321 AMM 24-21. OPS/LEAK CHECK OK. (LP 8739522 - AIRCRAFT WAS GROUNDED)SDR DALA2025091806855Unknown · fumesATB, PERFORMED AN AIR TURN BACK DUE TO FUMES IN CABIN AND COCKPIT. PERFORMED WATER WASH AND DRY OUT RUNS ON BOTH ENGINES AND REPLACED BOTH RECIRCULATION FILTERS. (LP 7607148)SDR DALA2024050304924Lavatory · fullSHIP 3027 - DIV - TO DEN DUE TO LAVATORIES BEING INOPERATIVE AND LAV TANK SHOWING FULL ON FAP. WASTE TANK FOUND COMPLETELY FULL. SYSTEM OPERATED NORMALLY AFTER BEING DUMPED.SDR DALA2024010400145Unknown · unknownLAVATORY WASTE SYSTEMS WASTE QUANTITY INDICATION SYSTEM. CORRECTIVE ACTION: REPLACED SENSOR, WASTE, TANK LEVEL. STILL NOT WORKING. VERIFIED TANK EMPTY. CONTINUED ON MEL. (5551516) R/R DEU 300RH7 PER A321 AMM 23-73 OPS CHK GOOD.SDR DALA2023092607933Unknown · unknownSHIP 3027 - DIV - TO SDF DUE TO LAV SMOKE DETECT FAULT. CREW DECLARED EMERGENCY ON LANDING. UNABLE TO RESET MESSAGE IN FLIGHT. NO INDICATIONS OF SMOKE/ODOR. CORRECTIVE ACTION: LAV L AND G BOTH SHOWING SMOKE DETECTOR FAULTS. DEFERRED EACH PER MEL AND CONTINUED;SDR DALA2023072806118Unknown · unknownINOP EPSU 12WL AT PASSENGER CABIN. REPLACED EPSU 12WL AT PASSENGER CABIN AS PER A320 FAM AMM 33-51- 38-000-001-A AND AMM 33-51-38-400-001-A. TEST IS GOOD. JOB COMPLETE. (LP# 2888279)SDR DALA2023072806117Unknown · unknownINOP ESPU 12WL AT PASSENGER CABIN. REPLACED ESPU 12WL AT PASSENGER CABIN AS PER A320 FAM AMM 33-51- 38-000-001-A AND AMM AMM 33-51-38-400-001-A, TEST IS GOOD. JOB COMPETE. (LP# 2887555)SDR DALA2023072806116Unknown · unknownPERFORM IN EXTERNAL SKIN REPAIR BTW FR32 TO FR33 AT LEVEL OF STR41R A T LOWER FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN BTW FR32 TO FR33 AT LEVEL OF STR41R AT LOWER FUSELAGE AS PER SRM A32153-21-11-300- 022. TOOL USED DIGITAL CALIPER P/N 700-113-10SDR DALA2023072506029Unknown · unknownIMPROPERLY INSTALLED INTERNAL STRAP ON EXISTING REPAIR LOCATED SLAT 4 LH WING. PERFORMED PERMANENT REPAIR (REINFORCING PLATE) LOC. ON SLAT 4 L /H AS PER A321 SRM 51-42-11 AND A321 SRM 57-40-00-300-067 FIG 001 RECHECK IS NOT REQUIRED DUE TO REPAIR IS CATEGORY ASDR DALA2023072506028Unknown · unknownCRACK SHEAR PLATE STR 23 L LOCATED BETWEEN FR69 TO FR70 AT AFT GALLEY AREA.REPLACED SHEAR PLATE LOC. ON STR 23L BTW FR69 TO FR70 AT AFT GALLEY AREA AS PER A321 SRM 51-42-11, SRM 51-72-11 AND SRM 53-41-17-01A, AND DWG# D534 74180, RELEASE DATE: 14-JUL-22, ISSUESDR DALA2023072506027Unknown · unknownCRACK SHEAR PLATE STR 23 R LOCATED BETWEEN FR69 TO FR70 AT AFT GALLEY AREA. REPLACED SHEAR PLATE STR 23 RH LOCATED BETWEEN FR69 TO FR70 AT AFT GALLEY AREA AS PER A321 SRM 51-42-11, SRM 51-72-11 AND SRM53-41-17-01A, AND DWG D53474180, ISSUE: Z, RELEASE DATE: 14SDR DALA2023071805817Unknown · unknownCORROSION FLOOR BEAM +Y1292 AT FWD GALLEY AREA. REPLACED FLOOR BEAM Y1292 LOC. FRAME 12 TO 24 FWD GALLEY AREA AS PER A321 SRM 51-72-11 AND DRAWING D53135203 RELEASE DATE 12SEP13 ISSUE A00 AND TOOK MEASURES DEEPEST CORROSION ARE: L=0.959INCH,W=0.163INCH,D=0.042SDR DALA2021082705070Skin · dentedLEFT WING SLAT 4 HAS DENT IN UPPER SURFACE. PREPARED , TREATED AND APPLIED EPOXY PRIMER PER A 321 SRM 57-40-00-300-065 . MEASURED DENTED AREA AND FOUND WITHIN LIMITS PER A 321 SRM 57-40-00-283- 001 DEPTH = .167" / CHORD WISE DIMENTION = 5.01". REPAIRED DENT R
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.