- Registered owner
- Delta Air Lines Inc
- Location
- Altanta, GA
- Owner type
- Corporation
- Serial number
- 8713
- Year built
- 2019
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- January 31, 2019
- Certificate issued
- January 30, 2019
- Expires
- January 31, 2029
- Mode S code
- A426A5
From the FAA registry file of October 22, 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 N367DNMatched 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 N367DNMatched 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 · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DALA2025010200025Solenoid Valve · faultedSHIP 3067 -ATB- RETURNED TO SLC AND DECLARED AN EMERGENCY DUE TO LEFT ENGINE COMPRESSOR STALL. CORRECTIVE ACTION: REPLACED NBR 1 ENGINE PRV, PRV CONTROL SOLENOID, TLT, AND IP CHECK VALVE. (LP 6692554)SDR DALA2024120811520Light · damagedAIRCRAFT 3067, EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:605. CABIN BY LAV 3 IS BLINKING ON AND OFF. BOTH SMALL CEILING LIGHTS OVER 18 AND 28 ARE BLINKING AS WELL. SEATS 19- 24 EMERGENCY LIGHTS ARE ALSO BLINKING. CORRECTIVE ACTION: EPSU SYS TSDR DALA2024112511212Battery Pack · failedAIRCRAFT 3067, L3 DOOR AND OVERHEAD #3 EMERGENCY EXIT LIGHTS INOP. CORRECTIVE ACTION: FOUND BATTERY PACK BAD. R/R 11WL BATTERY PACK AS PER A321 AMM 33-51. (LP 6492630)SDR DALA2024102710418Floorbeam · corrodedAIRCRAFT 3067, CORROSION ON FLOOR BEAM -Y160.5 AT LEVEL FRAME 68 AFT GALLEY AREA. (SSI: 534147). CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y160.5 AND FASTENERS LOCATED BETWEEN FRAME 67 TO FRAME 70 IN AFT GALLEY AREA AS PER A321 SRM 51-42-11, A321 SRM 51-72-11 DWSDR DALA2024102710417Floorbeam · corrodedAIRCRAFT 3067, CORROSION ON FLOOR BEAM Y765 BETWEEN FRAME 67 AND FRAME 68 AT AFT GALLEY AREA. (SSI 534147). CORRECTIVE ACTION: REPLACED FLOOR BEAM Y765 AND FASTENER BETWEEN FRAME 66 AND FRAME 70 AT AFT GALLEY AREA AS PER A321 SRM 51-42-11, A321 SRM 51-72-11, DSDR DALA2024102100279Shear Plate · crackedAIRCRAFT 3067, CRACK ON SHEAR PLATE LOCATED BETWEEN FRAME 69 TO FRAME 70 AND STRINGER 23 LEFT AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SHEAR PLATE AND FASTENERS LOCATED BETWEEN FRAME 69 TO FRAME 70 AND STRINGER 23 LEFT AT AFT GALLEY AREA AS PER A321 SRMSDR DALA2024102110279Support · corrodedAIRCRAFT 3067, CORROSION LOWER SILL AT FRAME 68 AND STRINGER 23 LEFT AT AFT GALLEY AREA (SSI 534147). CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON LOWER SILL AREA AT FRAME 68 AND STRINGER 23 LEFT AT AFT GALLEY AREA AS PER A321 SRM 53-41-14-300-001. FIGURE SDR DALA2024091609028Lens · misinstalledAIRCRAFT 3067, FOUND SEVERAL EMERGENCY EXIT SIGNS WITH THE LENSES SWAPPED. CORRECTIVE ACTION: REMOVED AND REINSTALLED LENSES IN CORRECT LOCATIONS REF A321 AMM 33-51. (LP 0558533)SDR DALA2024072207316Power Supply · inoperativeAIRCRAFT 3067, FOUND EMERGENCY LTS INOP ON SVC CHK. CORRECTIVE ACTION: REPLACED EPSU (11WL). (LP 6129518)SDR DALA2023070705508Unknown · unknownAFT ENTRY DOOR CUT-OUT IN FUSELAGE HAS WEAR DAMAGE DUE TO CONTACT WITH UPPER DOOR SKIN PLATE. REWORKED DAMAGE PER A321 SRM 53-41-11-283-041 PG. 32 OF 37 ( 468743) BLENDED DAMAGED AREA PER SAME SRM REF. (963834) NOMINAL SKIN THICKNESS IS .236. REMAINING THICKNESDR DALA2021082004873Bpcu · faultedON LANDING ROLLOUT LOST NWS STEERING UPON SHUT DOWN GOT BRAKES/N /S MINOR FAULT. BSCU PER A321 AMM 32-42 PERFROMED NWS TEST, BSCU BITE BOTH CHECK GOOD. NO FAULTS PRESENT AT THIS TIME. (LP# 7765762)SDR DALA202008112765Unknown · unknownEMERGENCY EXIT SIGNS INOPERATIVE. PERFORMED AMM 32-51. ALL EMERGENCY LIGHTS CHECKED NORMAL.SDR DALA202008112764Unknown · unknownEMERGENCY EXIT SIGNS WERE INOPERATIVE. PERFORMED AMM 32-51. ALL EMERGENCY LIGHTS CHECKED NORMAL.SDR DALA2019070704163Cover · missingPDA PART DEPARTING AIRCRAFT 3067 LOG 5428765, DURING SERVICE CHECK FOUND 532CB INBOARD FLAP TRACK MOVABLE FAIRING PIVOT COVER MISSING, INSTALLED 532CB INBOARD FLAP FAIRING PIVOT COVER.
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