- Registered owner
- Delta Air Lines Inc
- Location
- Atlanta, GA
- Owner type
- Corporation
- Serial number
- 10300
- Year built
- 2021
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- November 4, 2021
- Certificate issued
- November 4, 2021
- Expires
- November 30, 2028
- Mode S code
- A071C2
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 N128DNMatched 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 N128DNMatched 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 · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DALA2025042103036Unknown · odorSHIP 1028 ON PREVIOUS ARRIVAL CABIN CREW REPORTED STRONG CHEMICAL ODOR IN THE CABIN. THE CHEMICAL ODOR PERSISTS IN THE CABIN DURING PREFLIGHT AND NEEDS TO BE INVESTIGATED. POSSIBLE ACETONE ODOR. CORRECTIVE ACTION: T/S PER A321 TSM 05-51 -00-810-831-A. HAD FAINSDR DALA2024020601620Seal · leakingSHIP 1028 - DIV - TO PHX DUE TO AIR R WING LEAK ECAM MESSAGE. CORRECTIVE ACTION: FOUND LEAK AT CLAMP BETWEEN OZONE CONVERTER AND FLOW CONTROL VALVE, AND AT CLAMP BETWEEN ACM AND SECONDARY HEAT EXCHANGER. REPLACED SEALS. LEAK CHECK GOOD. (LP 5398286)SDR DALA2024012401098Skin · damagedAIRCRAFT 1028, GSE RAILING CONTACTED AIRCRAFT SKIN JUST AFT OF THS DOOR. CORRECTIVE ACTION: CRACK .25" LONG IN A 1" DENT FOUND AT FRAME 73/74 AT STR 28/29L. REMOVED DAMAGE AND INSTALLED A DOUBLER PER A321-200 SRM 53-00-11-300-029. FIG 001. PAGE 9. DEFERRED TO SDR DALA2022021500991None · noneEVALUATE AFT EXTERIOR SKIN DAMAGE. DURING SV IN BHM PERFORMED WORK ON NRC #5 COMPLIED WITH PRI 596293-14 REV O-6 (767121) QC 5209 PRI 596293-14 REV O-6 MATCHES ERA 596293-14 REV O (767121) QC 5209 COMPLIED WITH ERA 596293-14 REV O (767121) QC 5209. (LP# 212066SDR DALA2022021500990None · noneSKIN DAMAGED BELOW C3 CARGO DOOR. DURING SV IN BHM PERFORMED WORK ON NRC # 31 COMPLIED WITH PRI 596659-14 REV O-2 (767121) QC 5209 PRI 596659-14 REV O-2 MATCHES ERA 596659-14 REV O (767121) QC 5209 COMPLIED WITH ERA 596659-14 REV O (767121) QC 5209. (LP# 21206SDR DALA2022021500989None · noneSTRINGER 42RH BETWEEN FRAME 60 AND 61 IS BENT. DURING SV IN BHM PERFORMED WORK ON NRC #9 AND #29 COMPLIED WITH PRI 596416-14 REV O-2 (767121) QC 5209 PRI 596416-14 REV O-2 MATCHES ERA 596416-14 REV O (767121) QC 5209 COMPLIED WITH ERA 596416-14 REV O (767121) SDR DALA2022021500988None · noneSTRINGER 42LH BENT BETWEEN FRAME 58 AND 59. DURING SV IN BHM PERFORMED WORK ON NRC #9 AND #29 .COMPLIED WITH PRI 596416-14 REV O-2 (767121) QC 5209.PRI 596416-14 REV O- MATCHES ERA 596416-14 REV O (767121) QC 5209.COMPLIED WITH ERA 596416-14 REV O (767121) QC SDR DALA2022022401221None · none***DTE*** A321 / FUSELAGE / DENT AND GOUGES/ PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 6 MONTHS FROM REPAIR ACCOMPLISHMENT. LOG-PAGE UPDATED @ 09FEB22 1502 UTC 02 DFRD BY GRAY 00495354 BHM 09FEB22 RII: N ENTR 00495354 W REPAIR APPROVAL IS LIMITED TO 6 MOSDR DALA2022022401220None · none***DTE*** A321 / FUSELAGE / FR61-FR62 / STR 40R -STR 41R / DENT / PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 6 MONTHS FROM REPAIR ACCOMPLISHMENT. LOG-PAGE UPDATED @ 09FEB22 1425 UTC 02 DFRD BY GRAY 00495354 BHM 09FEB22 RII: N ENTR 00495354 W REPAIR APPROVSDR DALA2022022401219None · none***DTE*** A321 / FUSELAGE / FR 58 - 61 / STR 42R, 43R, & 42L / DEFORMED. REPAIR APPROVAL IS LIMITED TO 6 MONTHS FROM REPAIR ACCOMPLISHMENT. REPAIR APPROVAL IS LIMITED TO 6 MONTHS AFTER SECTION I (FEB. 9, 2022). ADDITIONAL ENGINEERING AUTHORIZATION (ER/A) REVIS
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