AD 2023-04-09
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | SAS | Airworthiness Directives; Airbus SAS Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus SAS Airplanes |
Unsafe Condition
Fatigue damage in principal structural elements could result in reduced structural integrity of the airplane.
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Required Actions
Revise the existing maintenance or inspection program to incorporate new or more restrictive airworthiness limitations specified in EASA AD 2022-0172. Include new actions (e.g., inspections) in operator maintenance documents. Comply with these actions as required by 14 CFR 91.403(c).
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Compliance Time
Within the compliance times specified in EASA AD 2022-0172.
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Affected Aircraft
Airbus SAS Model A310 series airplanes, including A310-203, A310-204, A310-221, A310-222, A310-304, A310-322, A310-324, and A310-325. Excludes A310-203C and A310-308 airplanes, which are not certificated by the FAA.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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