AD 2024-01-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | SAS | Airworthiness Directives; Airbus SAS Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus SAS Airplanes |
Unsafe Condition
Cracked or ruptured aft LDCD frames, which could allow loads to be transferred to the remaining structural elements, leading to the rupture of one or more vertical aft LDCD frames and reduced structural integrity of the aft LDCD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Retain the actions in AD 2019-16-11, correct the HFEC inspection threshold, modify the LDCD frame forks, and prohibit the installation of affected LDCDs under certain conditions, as specified in EASA AD 2023-0117.
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Compliance Time
Before further flight
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Affected Aircraft
Airbus SAS Model A300 F4-605R and F4-622R airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2023-0117, dated June 13, 2023.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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