EAD 2026-0119-E: 16 A380s sorted by serial number

EASA Emergency AD 2026-0119-E, issued on 22 June 2026 and effective on 24 June 2026, applies to sixteen A380s designated by their manufacturer serial number: five in Group 1, barred from all flight before a special detailed inspection of the wing mid spars, save for a controlled ferry flight to the inspection site, eleven in Group 2, to be inspected within 25 flight cycles of the effective date. Whether your aircraft is affected comes down to a single datum: its MSN, compared against the AD's literal list, not its registration nor its age.

This article works from the text of the EAD, not from press coverage. All quotations are taken from the official EAD 2026-0119-E page and its reference PDF, checked line by line on 18 September 2026.

What the EAD requires, text in hand

Status first. AD 2026-0119-E is an Emergency Airworthiness Directive: its remark 2 states that "the results of the safety assessment have indicated the need for immediate publication and notification, without the full consultation process". It is issued under Part 21.A.3B of Regulation (EU) 748/2012, on type certificate EASA.A.110, with no supersedure and no corresponding foreign AD. Published on 22 June 2026, effective on 24 June 2026: it took effect immediately, without the comment phase that PAD 25-170 had run for AD 2025-0280.

The reason. The EAD does not start from an incident but from the results of inspections already ordered: "EASA issued several ADs requiring inspection of wing spars, last one being EASA AD 2025-0280. Following the review of the results of those inspections, it has been determined that the cracks found on certain aeroplanes could reduce the structural integrity of the wing." The logical next step: "To address this potential unsafe condition, Airbus determined that an additional special detailed inspection has to be accomplished." The required action is therefore an investigation, not a repair: contact Airbus for special detailed inspection instructions for the wing mid spars, accomplish them, then report the results. The AD describes itself as an "interim action": "further AD action may follow".

The scope. The applicability lists neither a range nor a production date: it names sixteen manufacturer serial numbers, MSN 30, 42, 55, 56, 105, 142, 184, 187, 190, 202, 203, 208, 209, 227, 228 and 234, across three models, the A380-841, A380-842 and A380-861. Chapter ATA 57, wings, wing mid spars.

The identity card of EAD 2026-0119-E, from the official EASA PDF.

The list of sixteen MSNs: a literal sort

The passage that decides everything else fits in two lines of definitions: "Group 1 are aeroplanes MSN 190, 202, 203, 209 and 228. Group 2 are aeroplanes MSN 30, 42, 55, 56, 105, 142, 184, 187, 208, 227 and 234." No range, no presumption, no entry-into-service criterion: membership is determined by comparing one integer, your aircraft's MSN, to a closed list of sixteen numbers.

Two practical consequences. First, the identifier that matters is the manufacturer serial number, not the registration mark: an A380 may have changed registration and operator, but its MSN is engraved for life on the data plate and reported on the certificate of registration, the certificate of airworthiness and the whole technical file. Second, the sort is binary: an aircraft is either on the list or it is not. MSN 235, built immediately after 234, falls outside the EAD's applicability while remaining, like every other, inside that of AD 2025-0280.

Specialist media have mapped these sixteen MSNs to their operators: according to the tally published by Flightradar24 on 24 June 2026, updated 26 June, fifteen are flown by Emirates and one by Qantas, registered VH-OQI. That attribution is useful context; it does not replace the AD's list, which remains the only probative reference for your file.

The sixteen MSNs and the two regimes of EAD 2026-0119-E, from its definitions and Table 1.

The required regime, sequence by sequence

The exact sequence, paragraphs (1) to (4):

Inspection, paragraph (1) and Table 1. Within the Table 1 compliance time, "contact Airbus for instructions for special detailed inspection of the Wing Mid Spars and accomplish those instructions accordingly". Group 1: "Before next flight after the effective date of this AD", i.e. before the first flight after 24 June 2026. Group 2: "Within 25 Flight Cycles (FC) after the effective date of this AD". This is not a standard EASA inspection: it is a "special detailed inspection" whose content is set by Airbus, in instructions that are not public.

Ferry flight, paragraph (2). For Group 1 only: "A ferry flight (up to 3 FC, non-ETOPS, no passengers) is permitted to position the aeroplane to a location where the inspection can be accomplished." A grounded aircraft may therefore reach the inspection site, provided it flies without passengers, outside ETOPS and in no more than three cycles.

Corrective action, paragraph (3). "If, during the inspection as required by paragraph (1) of this AD, any discrepancy is detected, before next flight, contact Airbus for applicable repair instructions and, within the compliance time specified in those instructions, accomplish those instructions accordingly." A discrepancy holds the aircraft on the ground until Airbus repair instructions arrive and are accomplished within their specified time.

Reporting, paragraph (4). "Within 7 days after the inspection as required by paragraph (1) of this AD, or after the effective date of this AD, whichever occurs later, report the inspection results, including no findings, to Airbus." Seven days, even when nothing was found: an absence of findings is reported too.

The chain of ADs that led to the EAD

The EAD did not arrive alone. The reference it cites, AD 2025-0280, issued on 11 December 2025 and effective on 18 December 2025, had ordered repetitive inspections of the mid spars on all A380-841, -842 and -861, with no MSN restriction. Its parts scope was precise: the Wing Mid Rear Spar (MRS) between ribs 17 and 33, the Wing Inner Mid Front Spar (IMFS) between ribs 14 and 29, the Wing Outer Mid Front Spar (OMFS) between ribs 29 and 38, left and right hand sides. Its deadlines: before return to service after each storage lasting more than twelve months, or within 39 months of the effective date, whichever comes first, then at intervals not exceeding 36 months, per Airbus Alert Operators Transmission A57R027-25 of 4 November 2025, with results reported to Airbus within 30 days.

It is the feedback from those inspections that triggered the EAD: the cracks found "on certain aeroplanes" led Airbus to define a deeper inspection, limited to the sixteen airframes whose situation required it. The mechanics are legible: a fleet-wide AD harvests results, an EAD targets the MSNs whose results call for a specific investigation. For a continuing airworthiness manager, the lesson is that paragraph (4) reporting of AD 2025-0280 was not a formality: it is what feeds the sort.

The documentary chain: AOT, consultation, fleet-wide AD, results, targeted EAD.

Proving your aircraft is in, or out: the documents that count

For an operator, a CAMO or a buyer, the question comes up twice. When the EAD lands: is my MSN on the list? Months later, as today: can I prove the requirement was accomplished, or that it never applied to me?

Proof of membership hangs on one integer. The MSN is read on the aircraft's data plate, and appears on three reference documents: the certificate of registration, the certificate of airworthiness, and as the primary identifier of the airworthiness records. That is the number to compare against the list, verbatim. Two distinct decisions then come into play: applicability is read in the MSN list; enforceability rests with the state of registry. The EAD is issued by EASA on the type certificate; for the sixteen aircraft, none of which is registered in the EU according to the press tally, the state-of-registry authorities make the directive enforceable, generally by adopting such requirements or by imposing them through their own instruments.

Proof of accomplishment hangs on four documents: the special detailed inspection instructions received from Airbus, the work order and release evidence accomplished within the Table 1 time, the results report sent to Airbus within seven days, including a "no findings" report, and, where a discrepancy was found, the repair instructions and their accomplishment before the next flight. For a Group 1 aircraft ferried to the inspection site, the ferry record matters too: three cycles at most, non-ETOPS, no passengers, to the inspection location.

Proof of exclusion is drafted the same way: a dated note in the records, signed and archived, showing the MSN was compared to the list turns "we are not in it" into a verifiable fact. It is the same reflex as the P/N and S/N qualification under the tail gearbox AD 2026-0168, or the "affected part" presumption of the FAA AD 2026-17-10: the records prove the status, not memory.

A worked example: two files on one desk

Take a fully fictional case to see the mechanics. A CAMO tracks two A380-841s for a lessor. The first file shows MSN 208: it is on the list, Group 2. The CAMO verifies the special inspection was accomplished within the 25 cycles following 24 June 2026, that the report was sent to Airbus within seven days, and archives evidence of both in the airworthiness records. The second aircraft carries MSN 190: Group 1. There, the question is not only "did the inspection happen" but "did the aircraft fly between 24 June and its inspection": every flight was barred, not only revenue flights; if it flew outside an authorised ferry flight, the operator was out of compliance and the finding must be documented, not hidden. If the aircraft was positioned by ferry flight, the CAMO checks the three conditions of paragraph (2): three cycles at most, non-ETOPS, no passengers. In both cases, the file speaks for the aircraft.

What this article cannot establish

• The content of the Airbus instructions is not public. The exact nature of the "special detailed inspection", its precise zones and acceptance criteria sit in the instructions Airbus sent to the affected operators; the EAD mandates them without publishing them. This article reproduces only what the text cites.
• The operator split comes from the press. The mapping of the sixteen MSNs between Emirates and Qantas, including registration VH-OQI for the Qantas airframe, is the tally published by Flightradar24 on 24 June 2026, updated 26 June; the EAD names no operator.
• Inspection results are not public. Which cracks were found, on which precise spar and on which MSN, is not detailed in the EAD, which refers to "cracks found on certain aeroplanes" without further granularity.
• The sequel is unwritten. The EAD is an "interim action": a further AD, an expansion or a narrowing of scope may follow; nothing in the text says which decision will come.
• No MSN-to-severity mapping is published. The text does not say why a given number sits in Group 1 and another in Group 2; the sort reflects inspection results, not a production rule.

Kepler's take: when sixteen integers set the regime

Kepler's take: EAD 2026-0119-E is a textbook case of what we build: a directive that sorts a fleet by comparing an integer in the records to a published list. An airworthiness register that knows each aircraft's MSN, the applicability of every AD received, and the date and evidence of every accomplishment turns that sort into a query of seconds, and "not listed" into a signed finding rather than a conviction. Kepler Aviation designs traceability and documentation-automation tools for maintenance and airworthiness management, within the Kepler Digitals ecosystem. To assess your records' ability to answer this kind of sort, contact us.

Sources

• EASA, Emergency Airworthiness Directive 2026-0119-E, 22 June 2026 and official PDF: primary source for all quotations (applicability, definitions, reason, required actions (1) to (4), Table 1, remarks), verified line by line on 18 September 2026.
• EASA, Airworthiness Directive 2025-0280, 11 December 2025 and official PDF: repetitive inspections of the affected parts (MRS ribs 17-33, IMFS ribs 14-29, OMFS ribs 29-38, LH and RH) on all A380-841/-842/-861 MSNs, per AOT A57R027-25 of 4 November 2025; PAD 25-170 consultation from 5 November to 3 December 2025 with no comments.
• Flightradar24, "EASA issues emergency directive for some A380 wings", Ian Petchenik, 24 June 2026, updated 26 June: MSN-to-operator mapping (fifteen Emirates, one Qantas VH-OQI), dated secondary source, not used as proof of applicability.
• Regulation (EU) 1321/2014, Annex I (Part-M), points M.A.301 and M.A.303 (EUR-Lex): mandatory accomplishment of applicable ADs, recalled in the EAD's header.