AD 2022-19-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | SAS | Airworthiness Directives; Airbus SAS Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus SAS Airplanes |
Unsafe Condition
fatigue cracking, damage, or corrosion in principal structural elements
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness tasks, as specified in EASA AD 2021-0205, which is incorporated by reference. Any differences with EASA AD 2021-0205 are identified as exceptions in the regulatory text of this AD.
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Compliance Time
Before further flight
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Affected Aircraft
All Airbus SAS Model A310-203, -204, -221, -222, -304, -322, -324, and -325 airplanes
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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