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Aircraft record

N301DU2021 Airbus BD-500-1A11

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched62 service difficulty reports

Registration
Valid
expires Mar 31, 2028
Based in
Atlanta, GA
owner city / state
Owners
1
since 2021
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
62
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Delta Air Lines INC
Owner type
Corporation
City, state
Atlanta, GA
Certificate issued
Mar 18, 2021
Expires
Mar 31, 2028
Airworthiness
Standard · Transport
Airworthiness date
Mar 18, 2021

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Airbus
Model
BD-500-1A11
Year
2021
Serial number
55069
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
153
Engines
2
Max takeoff weight
20,000 and over lb
Type certificate data sheet
T00008NY
Mode S code
A32367

Engine

Make and model
P & W Pw1521g Serie
Type
Turbo-fan
Power
21,970 lb thrust

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2021 – nowDelta Air Lines INCAtlanta, GA · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (0)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

No ADs published since 1998 matched this airframe or engine model.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (62)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Fuselage · skin · corrodedSep 16, 2026

    CORROSION FOUND ON BOTTOM SKIN AT FWD EDGE OF WTBF, BETWEEN STR36L. COMPLIED WITH ER/A 636395-14 REV 0 PRI REV 0, REV 1, REV 2, REV 3, REV 4, AND FINAL ER/A 636395-14 REV ORIGINAL SECTION I. (LP# 1815433; AIRCRAFT WAS GROUNDED)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · stringer · damagedSep 16, 2026

    WHILE REMOVING DAMAGED SKIN IAW PRI 636395-14, STR 36L BETWEEN FR 34-35 DAMAGED BY CUTOFF WHEEL. COMPLIED WITH ER/A 636395-14 REV 0 PRI REV 0, REV 1, REV 2, REV 3, REV 4, AND FINAL ER/A 636395-14 REV ORIGINAL SECTION I. (LP# 1815437; AIRCRAFT WAS GROUNDED)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedSep 16, 2026

    EVIDENCE OF CORROSION FOUND AT AFT WTB FUSELAGE SKIN, AIRCRAFT CENTERLINE. (M)(P) REF CORROSION SSI: 53-50-02-05. COMPLIED WITH ER/A 636443-14 PRI REV 0, ER/A 636443-14 PRI REV 1, ER/A 636443-14 PRI REV 2, AND FINAL ER/A 636443-14 REV ORIGINAL SECTION I. NOMINAL THICKNESS 0.090", MATERIAL…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · door frame · corrodedSep 16, 2026

    AFT SERVICE DOOR SURROUND - FR74 DOOR FRAME HAS SEVERAL HOLES WITH CORROSION. -M- REFERENCE SSI: 53-61-24-03. NO PRESENCE OF BLUE PAINT FROM PREVIOUS REPAIR. ACCOMPLISHED TASKS FOR ER/A 636471-14 PRI REV. 0, ER/A 636471-14 PRI REV. 1, ER/A 636471-14 PRI REV. 2 AND ER/A 636471-14 REV. ORIGINAL.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · door frame · corrodedSep 16, 2026

    AFT SERVICE DOOR SURROUND - FR76 DOOR FRAME HAS SEVERAL HOLES WITH CORROSION. -M- REFERENCE SSI: 53-61-24-03. NO PRESENCE OF BLUE PAINT FROM PREVIOUS REPAIR. ACCOMPLISHED TASKS FOR ER/A 636471-14 PRI REV. 0, ER/A 636471-14 PRI REV. 1, ER/A636471-14 PRI REV. 2 AND ER/A 636471-14 REV.ORIGINAL. (LP#…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · door frame · corrodedSep 16, 2026

    DURING H CHECK IN MSP, MAINTENANCE WAS ACCOMPLISHING EO WORKCARD 5331-01297-02C (SB BD500-530010 ISSUE 004). DURING MODIFICATION, THE AFT CARGO DOOR SURROUND STRUCTURE C01343028- 103 LOWER SILL WAS FOUND WITH CORROSION. THE CORROSION FOUND IS ON THE OUTER SURFACE OF THE SILL LOCALLY AROUND THE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · waste box · corrodedSep 15, 2026

    WASTE BOX FWD RIGHT CORNER HAS CORROSION MULTIPLE PLACES AND SURROUNDING RIGHT HINGE FITTING. -M- -P- REF. CORROSION SSI: 53- 61-56-02. COMPLIED WITH ER/A 611850-14 ER/A REV A PRI REV 0, 1, AND ERA 611850-14 REV A. ORIGINAL THICKNESS .125'. MATERIAL REMOVED .034". REMAINING THICKNESS .091". (LP…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · waste box · corrodedSep 15, 2026

    WASTE BOX RIGHT SIDE INNER LIP HAS CORROSION. -M- REF. CORROSION SSI: 53-61-56-02. COMPLIED WITH ER/A 611850-14 ER/A REV A PRI REV 0, 1, AND ERA 611850-14 REV A. ORIGINAL THICKNESS .125'. MATERIAL REMOVED .034". REMAINING THICKNESS .091". (LP# 1814774; AIRCRAFT WAS GROUNDED)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · door sill · damagedSep 15, 2026

    FWD CARGO DOOR SURROUND STRUCTURE, LWR SILL AREA (AREA COVERED BY SCUFF PLATES), SKIN PANEL, SILL. COMPLIED WITH ER/A 636422-14 PRI REV 0 AND FINAL ER/A 636422-14 REV ORIGINAL SECTION I PERMANENT REPAIR. PART REPLACED. (LP# 1814859; AIRCRAFT WAS GROUNDED)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · frame · corrodedSep 8, 2026

    CORROSION R/H SIDE FRAME PART # C02382152-102 AT MULTIPLE LOWER PANEL FASTENER HOLES. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0537:2090-2001/007 00307 REMOVED AND REPLACED FRAME PER REF A220 ASRP 51-42-00. (LP# 1800973; AIRCRAFT WAS GROUNDED)

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 62 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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