- Registered owner
- Wilmington Trust Co Trustee
- Location
- Wilmington, DE
- Owner type
- Corporation
- Serial number
- 7097
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- April 29, 2016
- Certificate issued
- July 12, 2018
- Expires
- July 31, 2028
- Mode S code
- A9768A
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56 model are included below.
On this page
Airworthiness directives that may apply · 325
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1985 | 1 |
|---|---|
| 1986 | 1 |
| 1990 | 1 |
| 1991 | 1 |
| 1996 | 2 |
| 1997 | 7 |
| 1998 | 11 |
| 1999 | 6 |
| 2000 | 13 |
| 2001 | 12 |
| 2002 | 16 |
| 2003 | 5 |
| 2004 | 17 |
| 2005 | 15 |
| 2006 | 14 |
| 2007 | 16 |
| 2008 | 10 |
| 2009 | 13 |
| 2010 | 9 |
| 2011 | 12 |
| 2012 | 10 |
| 2013 | 15 |
| 2014 | 18 |
| 2015 | 19 |
| 2016 | 23 |
| 2017 | 25 |
| 2018 | 31 |
| 2019 | 22 |
| 2020 | 24 |
| 2021 | 17 |
| 2022 | 22 |
| 2023 | 18 |
| 2024 | 14 |
| 2025 | 22 |
| 2026 | 17 |
See all 480 ADs
Information bulletins that may apply · 8
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.Historical bulletins · 5
SAIB NE-13-33R1Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle VanesSAIB NE-13-33Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle VanesSAIB NE-08-17R2Turbine Section - Propulsion Technology LLC Unapproved RepairSAIB NE-08-17R1Propulsion Technology LLC Unapproved RepairSAIB NE-08-17Propulsion Technologies International Unapproved Repair
NTSB investigations
No NTSB investigations matched to N709FRMatched 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 N709FRMatched 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 · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR F3LA2023051000056Sensor · inoperativeDISCREPANCY: REFERENCE LP 317013 ITEM 1 AIRCRAFT WAS GROUNDED AS A RESULT OF THE SDR REPORTABLE EVENT. AFTER T.O. L/G SHOCK ABSORBER FAULT.
CORRECTIVE ACTION: REMOVED AND REPLACED PROX SENSOR 25GA ON NLG ON LP317014 ITEM 2. PER TSM 32-31-00-851-A. MX ACTION ISDR F3LA2022111400149Power Supply · no testEPSU 10WLFAILED EPSU TEST. REMOVED AND REPLACED L1 DOOR SLIDE ASSEMBLY PER AMM 25-62-44-000-012-A, AMM 25-62-44-400-007-A. OPS CHECK GOOD. AC OK FOR SERVICE.SDR F3LA2022092600122Coffeemaker · failedFA REPORTED BURNING WIRE SMELL IN FWD LAV ON DESCENT. - CORRECTION ACTION: FOUND FWD COFFEE MAKER CAUSING BURNING SMELL. PLACED ON NEF 25-99-40 AD CN#1186814. PLACARDS INSTALLED WITH MCC ABM 430781N REFERENCE TSM 05-50-00-810-831-A AC OK FOR SERVICE.SDR F3LA2022041100025Floorbeam · corrodedDISCREPANCY: REFERENCE PEMCO N/R# 12278N0220, AFT CABIN STRUCTURE, LEFT FUSELAGE HAS CORROSION RESIDUE TOP SURFACE AT FR66 WHERE PANELS 261LG, 261KF, 261MF INTERSECT.
CORRECTIVE ACTION: REMOVED CORRODED FLOORBEAM. INSTALLED NEW FLOOR BEAM IAW A321 SRM
51-72-SDR F3LA2021090300065Power Supply · failedLP171662 ITEM 2, UPSU TEST FAILED. REMOVED AND REPLACED EPSU ABOVE L1 DOOR. OPS CHECK IS GOOD AT THIS TIME. REF AMM 33-51-38-000-001-A AND 33-51-38-400-002-ASDR F3LA2016091900060Relay · stuckLANDING GEAR NOT DOWNLOCKED ON FINAL APPROACH. PERFORMED 260 KNOT CHECK WITH NO DEFECTS IAW AMM 32-31-00-710-005. PERFORMED GEAR SWING WITH NO DEFECTS. REPLACED RELAY 62GA IAW TSM 32-31-00-865-067-A3.B.D.1 AND TSM 32-31-00-810-059-B4.A.4. OPS CHECKED GOOD.
STCs that may be installed · 230
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 230 STCs