- Registered owner
- Alc A321 8640 LLC
- Location
- Camden, DE
- Owner type
- LLC
- Serial number
- 8640
- Year built
- 2018
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 18, 2018
- Certificate issued
- December 18, 2018
- Expires
- December 31, 2028
- Mode S code
- A9AF3E
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 N723FRMatched 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 N723FRMatched 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 · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR F3LA2024061200091Shear Plate · crackedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. AFT CABIN R/H LATERAL SHEER PLATE CRACKED AT FR 69. REMOVED AND REPLACED AFT CABIN L/H LATERAL SHEAR PLATE IAW A321 SRM 51-72-11-911-001. MX ACTION IS ACCEPTABLE.SDR F3LA2024061000090Shear Plate · crackedREFERENCE AIRBORNE/PEMCO N/R 15334.0295 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. AFT CABIN L/H LATERAL SHEER PLATE CRACKED AR FR 69. AFT CABIN L/H LATERAL SHEAR PLATE DAMAGED REMOVED AND REPLACED IAW A321 SRM 51-42-11. APPLIED TOP COAT IAWSDR F3LA2024051700067Battery · no testEPSU TEST FAILED, EPSU BATTERY 11WL FAULT. THIS FAILURE WAS DURING OVERNIGHT MAINTENANCE AND DID NOT CAUSE A FLIGHT DELAY. REPLACED BATTERY EPSU 11WL. EPSU TEST PASS. AMM 33-51-3R-400-002-A./END/SDR F3LA2022102100138Carriage · stuckECAM F/CTL FLAPS LOCKED, LESS THAN FLAPS ONE, QRH PROCEDURES APPLIED INCREASED APPROACH SPEED. EMERGENCY DECLARED. PERFORMED TSM 27-51-00-810-818-A STEP # 1 AND FOUND FLAP CARRIAGE REQUIRED LUBE LUBRICATED L/H AND R/H FLAP CARRIAGES IAW AMM 12-22-27-640-004SDR F3LA2021090100063Control Lever · inoperativeLGCIU 1 FAULT. LANDING GEAR WOULD NOT EXTEND, USED GRAVITY GEAR EXTENSION PER QRL. REMOVED AND INSTALLED LANDING GEAR NORMAL CONTROL LEVER. OPS CHECK GOOD. REF TSM 32-31-00-810-809-A AND AMM 32-31-11-400-001-A.SDR F3LA2021021100008Wire · disconnectedDISCREPANCY: EXIT LIGHT AT 4R DOES NOT ILLUMINATE. CORRECTIVE ACTION: FOUND EMERGENCY LIGHT NOT CONNECTED TO WIRING. RECONNECTED EXIT LIGHT 4R AND OPS CHECK GOOD REF AMM 25-23-49-400-010-A. AMM 33-51-00-710-804ASDR F3LA201912120152Trim System · bindingSTAB TRIM BINDING // PERFORMED OPERATIONAL TEST OF LOGISTICS ACTUATION ELAC 1&2 & SEC STANDBY POWER SUPPLY & ABILITY OF SEC 1&2 TO ACHIEVE PITCH CTL & ABILITY OF SIDE STICK PRIORITY FUNCTION, OPS CHECKS GOOD. A/C OK FOR SERVICE PER E/C 279000-05-1, WO# 394380 SDR F3LA201910070122Oxygen Mask · brokenFIRST OFFICER`S OXYGEN MASK HAS A BROKEN CONNECTOR TO HOSE. SWAPPED THE FIRST OFFICER`S OXYGEN MASK WITH 4TH OBSERVER`S.SDR F3LA201909100112Oxygen Mask · brokenCAPTAINS O2 MASK MAIN HOSE CAME OFF DURING PREFLIGHT SYSTEM CHECK. SWAP PILOTS O2 MASK W/4TH OBSERVER MASK OP CHECKS NORMAL AIRCRAFT OK TO CONTINUE. 4TH OBSERVERS O2 MASK INOP. DEFERRED PER MEL 25-11-07A CT# 1154512 DUE DATE 07-07-2020.
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