AD 2019-19-17
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 on the forward fittings in the radius of frame 40, adjacent to the tension bolts in the center section of the wings, which could result in reduced structural integrity of the wings.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
initial and repetitive ultrasonic (UT) and high frequency eddy current (HFEC) inspections and applicable corrective actions, including reworking the fuselage lateral panel at frame 40, blending out around cracks, and repair.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 flight hours
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Affected Aircraft
Airbus SAS Model A300 B4-600 series, Model A300 B4-600R series, Model A300 F4-605R, and Model A300 C4-605R Variant F airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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