AD 2023-03-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | SAS | Airworthiness Directives; Airbus SAS Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus SAS Airplanes |
Unsafe Condition
An interference was detected between the installed nut and the foot radius of frame (FR) 96, between stringer 6 and stringer 7, on the right-hand side. This condition, if not addressed, may affect the structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Remove the affected fasteners and inspect the affected area for damage, including detailed, high frequency eddy current, and rototest inspections for superficial or non-superficial damage. Apply applicable corrective actions if necessary, such as installing new fasteners and nuts with adapted aluminum washers and repair.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the compliance times specified in EASA AD 2022-0093, unless already done.
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Affected Aircraft
Airbus SAS Model A350-941 airplanes, certificated in any category, as identified in EASA AD 2022-0093.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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