- Registered owner
- Delta Air Lines Inc
- Location
- Atlanta, GA
- Owner type
- Corporation
- Serial number
- 12724
- Year built
- 2025
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- August 21, 2025
- Certificate issued
- August 20, 2025
- Expires
- August 31, 2032
- Mode S code
- A7BF22
Airbus S A S A321-271NXTCDS A28NMAirframe · Airbus S A S A321-271NXTCDS E00087ENEngine · IAE PW1133GA-JM
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 83
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2018 | 5 |
|---|---|
| 2019 | 8 |
| 2020 | 19 |
| 2021 | 14 |
| 2022 | 12 |
| 2023 | 15 |
| 2024 | 13 |
| 2025 | 22 |
| 2026 | 19 |
See all 127 ADs
Information bulletins that may apply · 2
Advisory, not mandatory.
Airframe · Airbus S A S A321-271NX
SAIB NE-19-03Escape Slide Maintenance Tasks and Intervals - JASC 2565Engine · IAE PW1133GA-JM
SAIB 2026-11Theft of Turbofan Engine Parts before MutilationNTSB investigations
No NTSB investigations matched to N599DAMatched 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 S A S A321-271NX aircraft
FAA incident reports
No FAA accident or incident reports matched to N599DAMatched 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 S A S A321-271NX aircraft
Service difficulty reports
No reports matched to N599DAGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Airbus S A S A321-271NX aircraft
Reports on N599DA not matched to an aircraft · 6
They name N599DA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR UG82005F00008Probe · dented(REF CNTRL NR: PA 05-004) ALTITUDE SPLIT BETWEEN NR 1 AND NR 2 ALTIMETERS OF 250 FT AT 17000 FT. THE RT PITOT/STATIC PROBE HAS IMPACT DAMAGE. REPLACED THE RT PITPT/STATIC PROBE. COMPLETED ALTITUDE AND LEAK CHECKS IAW MM. RETURNED AIRCRAFT TO SERVICE. (K)SDR UG82005F00005Probe · damaged(REF CNTRL NR: PA05004) ALTITUDE SPLIT BETWEEN NR 1 AND NR 2 ALTIMETERS OF 250 FT AT 17,000 FT. THE RT PITOT/STATIC PROBE HAS IMPACT DAMAGE. (K)SDR 2003F00271Switch · malfunctionedRIGHT THRUST REVERSER UNLOCKED ON ENGINE START. BOTH THRUST REVERSER STOW SWITCHES WERE LEFT IN THE DEPRESSED POSITION. PLACED BOTH THRUST REVERSER STOW SWITCHES IN THE NORMAL POSITION. THRUST REVERSERS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
STCs that may be installed · 91
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Airbus S A S A321-271NX
STC ST12461IBInstallation of Cockpit Voice Recorder with optional RIPS UpgradeSTC ST00885LAInstallation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.STC ST02528LAInstallation of the Thales Avionics, Inc. Data Transfer Device (DTD) or Solid State Drive (SSD) into the existing Cabin Media Loader (CML)