AD 2025-16-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | SAS | Airworthiness Directives; Airbus SAS Airplanes |
Unsafe Condition
Rivet holes being left unplugged after bracket relocation or removal accomplished during certain modifications, potentially resulting in fatigue damage starting from those rivet holes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct a one-time special detailed inspection (SDI) of the rivet holes for discrepancies (missing or incorrect rivets and cracks). Accomplish applicable corrective actions, including repairing cracks, obtaining instructions for addressing incorrect rivets, and installing oversized rivets. Allow installation of certain modifications, provided rivets are installed after the modification.
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Compliance Time
Before further flight
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Affected Aircraft
Airbus SAS Model A319-112 and -132 airplanes, and Model A320-214, -232, -233, -251N, and -271N airplanes, certificated in any category, as identified in EASA AD 2024-0204.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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