AD 2014-12-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B4-600 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Fatigue cracking of the aft cargo door sill beam, lock fitting, and torsion box plate could result in the loss of the door locking function and subsequently, complete loss of the cargo door in flight with the risk of rapid decompression.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the external area of the aft cargo door sill beam for cracking, and repair if necessary. Depending on findings, corrective actions such as repair may be required.
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Compliance Time
Before further flight
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Affected Aircraft
Airbus Model A300 B4-600, B4-600R, F4-600R series airplanes, Model A300 C4-605R Variant F airplanes (collectively called Model A300-600 series airplanes), and Airbus Model A310 series airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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