- Registered owner
- Delta Air Lines Inc
- Location
- Atlanta, GA
- Owner type
- Corporation
- Serial number
- 55192
- Year built
- 2023
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- February 24, 2023
- Certificate issued
- February 24, 2023
- Expires
- February 28, 2030
- Mode S code
- A3560B
Airbus Canada LP BD-500-1A11TCDS T00008NYAirframe · Airbus Canada LP BD-500-1A11Engine modelPratt & Whitney PW1521G SERIE
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 71
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2017 | 1 |
|---|---|
| 2019 | 1 |
| 2020 | 4 |
| 2021 | 10 |
| 2022 | 11 |
| 2023 | 11 |
| 2024 | 17 |
| 2025 | 16 |
| 2026 | 10 |
Airframe · Airbus Canada LP BD-500-1A11
AD 2026-15-14Engine fuel and controlAD 2026-13-52PneumaticEmergency ADAD 2026-13-02NavigationInformation bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Airbus Canada LP BD-500-1A11
SAIB NE-19-03Escape Slide Maintenance Tasks and Intervals - JASC 2565NTSB investigations
No NTSB investigations matched to N314DUMatched 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 Canada LP BD-500-1A11 aircraft
FAA incident reports
No FAA accident or incident reports matched to N314DUMatched 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 Canada LP BD-500-1A11 aircraft
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DALA2026072104268Fire Warning · false activationUPON BLOCKING IN TO GATE, A MX TECHNICIAN TOLD GROUND CREW TO TELL US TO BLOW FIRE EXT. ON ENGINE #1 DUE TO TAILPIPE FIRE. FIRED BTL 1 ON NR 1 ENG . HAD NO INDICATIONS OF FIRE/FIRE WARNING. UPON INSPECTION #1 ENG. NO VISIBLE DAMAGE OBSERVED. PERFORMED TURBINESDR DALA2026010100002Light · damagedEMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE, EMERGENCY DOWN LIGHT AT 2L MISSING ITS COVER / INTERIOR. REPLACED LENS AFT/LEFT. (LP 1379266)SDR DALA2025122609409Engine · odorAFTER STARTING RT ENG WITH AIR START CART, SMELLED DIRTY SOCK ODOR, STARTED LEFT ENGINE SMELL WORSENED RAN QRH FOR SMOKE FIRE FUMES NO NOTICEABLE CHANGE ISOLATED EACH SYSTEM LEFT SEEMS WORSE , SHUTDOWN ALL BLEED AND PACK SOURCE. RAN BOTH ENGINES WITH SNIFFER HSDR DALA2025121709179Bleed Air Sys · odorATB, RETURNED TO BNA CREW REPORTED DIRTY SOCK SMELL AFTER TAKEOFF. COMPLIED WITH TASK CARD 0550-2001. FOUND FAINT ODOR ONLY AT 20% N1 AND ABOVE. RT ENGINE BLEED DEFERRED. (LP# 7699534)SDR DALA2025120408877Unknown · odorCREW REPORTED DIRTY SOCK SMELL ON DESCENT. PILOTS ON O2 AND EMERGENCY DECLARED. T/S PER MSI WORKCARDS. ISOLATED PNEUMATIC SYSTEM, RAN ENGINES USING P-TRAK. NO ABNORMAL ODORS PRESENT. REPLACED RECIRC FILTERS. NO ODORS. ACFT RTS. (LP# 8035472)SDR DALA2025111308342O-Ring · failedDIVERTED TO MSP DUE TO DIRTY SOCK SMELL IN CABIN. COMPLETED AMDS CARD 0550-2001, 0550- 2003 AND 0550-9001-A220. COMPLETED MD LOG #1299655 STEP 1-5. #1 & #2 ENGINES SPINNER O-RINGS REPLACED. REPLACED RECIRCULATION FILTERS, JOB COMPLETE. (LP# 8035421, 1301555, SDR DALA2025042403227Skin · corrodedFUSELAGE SKIN HAS CORROSION AROUND THE FORWARD PASSENGER DOOR SCUFF PLATE ATTACH FASTENER HOLES 6OL, 8OL . SUMMARY SEE NR FOR ADDITIONAL INFORMATION 038-0001:5331-01297- 01A/001 00181 REPAIRED PER PRI 625637-14 REV 0, PRI 625637-14 REV 1, PRI 625637-14 REV 2, SDR DALA2025042403226Skin · corrodedFUSELAGE SKIN HAS CORROSION AROUND THE AFT CARGO DOOR LOWER SCUFF PLATE ATTACH FASTENER HOLE 6OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 016-0001:5331-01297- 02C/001 00180 REPAIRED PER PRI 625644-14 REV 0, PRI 625644-14 REV 1, PRI 625644 REV 2, AND FINAL ERSDR DALA2025042403224Skin · corrodedFUSELAGE SKIN HAS CORROSION AROUND THE FORWARD CARGO DOOR LOWER SCUFF PLATE ATTACH FASTENER HOLES 18OL. COMPLIED WITH ER/A 625638-14 REV. A PRI REV. 0 AND FINAL ER/A 625638-14 REV. A SECTION I. (LP# 0923463)SDR DALA2025041703026Slat Track · damagedLT WING SLAT TRACK #3, LOWER INBOARD SIDE OF TRACK, HAS DAMAGE, SHARP CORNER EDGE. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 032-0001:5742-01028-02A/001 00197 EVALUATED AND BLENDED SLAT TRACK REF 5742-01028-02A. NDT SDR DALA2025040802752Bottle · low pressureWING SLIDE CAUTION LEFT WING SLIDE. T/S PER A220 EFIM SOL.# 2-29563.PERFORMED VISUAL VERIFICATION OF SLIDE CYLINDER PRESS PER A220 AMP 25-63, FOUND SLIDE PRESS BELOW LIMITS. R/R LT OWEED SLIDE PER W/C: 2563-4002. ALL RII C/W 2563-4002 LH DELTA QC 2086. VERIFIESDR DALA2024092009271Diverter · faultedSHIP 8314 - DIV - TO PHX DUE TO ALL LAVS INOP IN FLIGHT. CORRECTIVE ACTION: REMOVE AND REPLACED WASTE TANK DIVERTER. (LP# 6049036)SDR DALA2023122010425Unknown · unknownGROUND CREW HIT NOSE GEAR DOOR. C/W ERA 607191-14 SECTION 1. TAPE APPLIED. INSP REQUIRED EVERY 7 DAYS. TERMINATING ACTION DUE WITHIN 850 FH FROM FLT 1189 20TH MAR 23. C/W REPEAT INSP OF THE FWD RH NLG DOOR REF ERA 607191-14 REV ORI. SECT II. NO FURTHER DEFECTS
STCs that may be installed · 13
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Airbus Canada LP BD-500-1A11
STC ST04254NYInstallation of Viasat Satcom SoftwareSTC ST04818NYInstallation of a Passenger Seat Re-PitchSTC ST00030IBInstallation of Test Tech ELTSTC ST11389DSInstallation of Delta Comfort Passenger Seating SectionSTC ST04803NYInstallation of a Panasonic Avionics In-Flight Entertainment SystemSTC ST00079IBIntegration of Halon-free Portable Fire Extinguisher HAFEXSTC ST00215IBInstallation of saf-Tglo ECO Photoluminescent Aisle Path Marking SystemsSTC ST04792NYUpdate of Intelsat 2KuSTC ST04562NYInstallation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking SystemsSTC ST03422NYUpdate of Intelsat componentsSTC ST04483ATInstallation of the Avionics Support Group Constant Friction Mount (cfMount) with CradleSTC ST03972NYInstallation of Honeywell Satcom SBB Upgrade and WiFi Network ActivationSTC ST04073NYInstallation of navAero Electronic Flight Bag provisions