- Registered owners
- Delta Air Lines IncDept 595 Aircraft Registrations
- Location
- Atlanta, GA
- Owner type
- Corporation
- Serial number
- 8388
- Year built
- 2018
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 26, 2022
- Certificate issued
- August 24, 2018
- Expires
- August 31, 2028
- Mode S code
- A40CA4
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56-5B2 model are included below.
On this page
Airworthiness directives that may apply · 236
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 |
| 2000 | 3 |
| 2001 | 4 |
| 2002 | 5 |
| 2003 | 1 |
| 2004 | 12 |
| 2005 | 8 |
| 2006 | 5 |
| 2007 | 15 |
| 2008 | 9 |
| 2009 | 12 |
| 2010 | 6 |
| 2011 | 11 |
| 2012 | 8 |
| 2013 | 14 |
| 2014 | 16 |
| 2015 | 17 |
| 2016 | 21 |
| 2017 | 24 |
| 2018 | 26 |
| 2019 | 19 |
| 2020 | 21 |
| 2021 | 15 |
| 2022 | 20 |
| 2023 | 18 |
| 2024 | 14 |
| 2025 | 22 |
| 2026 | 17 |
See all 368 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 CFM56-5B2 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 N360DNMatched 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 N360DNMatched 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 · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DALA2026062603804Plenum · odorAFTER ENGINE START WITH BLEED ON ENGINE AFT FA'S REPORTED STRONG FUEL/EXHAUST ODOR AT ROW 38/39. SWITCHED TO APU BLEED AND ODOR DISAPATED. NO ODOR IN FLIGHT DECK. REPLACED AIR PLENUM IAW AMM 21-52, LOWER Y-DUCT ON MIXING UNIT IAW AMM 21-21. (LP 8742730, 16618SDR DALA2026033002055Wire Harness · shortedDIVERSION TO ATL DUE TO RIGHT ENGINE EGT EXCEEDANCE. ECU FAULTING T495 SENSOR. INSPECTED WIRING HARNESS AND FOUND JUNCTION BOX SHORTED. REPLACED MAIN JUNCTION BOX, OPS CHECK OK. (LP 8377943)SDR DALA2025072805618Tail Cone · ground damageAIRCRAFT 3060, WHILE BEING TOWED TO THE GATE IN PNS, THE SUBJECT A321 TAIL CONE (P/N D0007000510000) WAS DAMAGED WHEN THE LH ELEVATOR ON AIRCRAFT 3060 CONTACTED AN ADJACENT BUILDING. THE TAIL CONE SKIN WAS DENTED, DAMAGING THE UNDERLYING STRUCTURE IN THE AREA SDR DALA2025073105727Structure · ground damageAIRCRAFT 3060, DURING GROUND OPERATIONS IN PNS, THE HORIZONTAL STABILIZER IMPACTED A BUILDING CAUSING DAMAGE TO THE RH SIDE OF THE ASSEMBLY. THERE IS ALSO POTENTIAL DAMAGE TO THE NOSE LANDING GEAR FROM AN OVERLOAD CONDITION DUE TO THE ABRUPT IMPACT. CORRECTIVESDR DALA2025012600630Pump · leakingSHIP 3060 - MISC/DE - DUE TO LOSS OF BLUE HYDRAULIC SYSTEM (HYD B RSVR LO LVL ECAM MESSAGE). CORRECTIVE ACTION: FOUND LEAK IN BLUE ELECTRIC PUMP. REPLACED BLUE HYDRAULIC SYSTEM ELECTRIC PUMP (2075GJ). OK FOR SERVICE. (LP 6778398)SDR DALA2024082008284Power Supply · inoperativeAIRCRAFT 3060, INOP EMERGENCY POWER SUPPLY UNIT (EPSU) 10WL AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED EPSU 10WL IN FORWARD GALLEY AREA. (LP 0511381)SDR DALA2024081208055Shear Plate · crackedAIRCRAFT 3060, CRACK SHEAR PLATE LOCATED STR 23 L FROM FR69 TO FR70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SHEAR PLATE LOCATED STR 23 L FROM FR69 TO FR70 AT AFT GALLEY AREA AS PER A321 SRM 51-72-11 AND DWG D53474180 RELEASE DATE: 14-JUL-22 ISSUE: Z ANSDR DALA2024080807917Fitting · corrodedAIRCRAFT 3060, CORROSION CENTER FITTING LOCATED FROM FR66 TO FR68 LH SIDE AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED CENTER FITTING AND FASTENERS LOCATED FROM FR66 TO FR68 LH SIDE AFT GALLEY AREA AS PER A321 SRM 51-42-11, A321 SRM51-72-11 AND DWG D53480505 RSDR DALA2024011200536Unknown · unknownSHIP 3060 R4 DOOR ASSIST CYL REQUIRES SVC. CORRECTIVE ACTION: SERVICED R4 DOOR ASSIST CYL IAW A321 AMM 52-10-00, NO LEAKS NOTED AT THIS TIME, OK TO CONTINUE. (5525421)SDR DALA2024011200535Unknown · unknownSHIP 3060 R3 DOOR ASSIST BOTTLE REQUIRES SVC. CORRECTIVE ACTION: SERVICED R3 DOOR ASSIST CYL IAW A321 AMM 52-22-00. NO LEAKS NOTED AT THIS TIME, OK TO CONTINUE. (5525420)SDR DALA2023030701684None · noneAFT FLOOR PROXIMITY EMER ESCAPE PATH AT SEAT 5B INOP. R&R PROXIMITY LIGHT PER A321 AMM 33-52. OPS CHK GOOD. OKAY FOR SVC. MEL AND PLACARD REMOVED. (LP# 9885892)SDR DALA2019091705379Splice · brokenSEAT MOUNTED EMERGENCY LIGHT INOP @ ROW 5A, FOUND 2 SPLICES BROKEN ON FWD LIGHT OF SEAT 5A. INSTALLED 2 EACH NEW SPLICES
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.