AD 2017-21-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B4-600 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Cracks were found in the door sill area, from frame (FR) 60 to FR63, including the sill beam flag, lock fitting, door sill web, and torsion door panel. This condition could lead to reduced structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct repetitive Special Detailed Inspections (SDI) of the aft cargo door lower torsion box area. Accomplish applicable corrective actions if cracks are detected.
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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; and Model A310 series airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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