AD 2020-23-11
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, which could result in reduced structural integrity of the fuselage
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
repetitive inspections for discrepancies of certain areas in and around the fuselage, as specified in two European Union Aviation Safety Agency (EASA) ADs, repairing discrepancies
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within the compliance times specified
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
all Airbus SAS Model A300 series airplanes; and Airbus SAS Model A300-600 series airplanes
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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