Summary
We are adopting a new airworthiness directive (AD) for all Airbus SAS Model A310-304, -322, -324, and -325 airplanes. This AD was prompted by an evaluation by the design approval holder (DAH) indicating that certain wing skin stringer joints are subject to widespread fatigue damage (WFD). This AD requires a rototest inspection of the fastener holes in the affected areas and repair if necessary, and modifying the fastener holes. We are issuing this AD to address the unsafe condition on these products.
Directive Details
AD Number
FAA-2018-0906
Document Number
2019-02925
Type
Rule
Publication Date
February 22, 2019
Effective Date
March 29, 2019
Affected Manufacturer
Airbus SAS
Criticality
routine
Emergency
No
Docket ID
Docket No. FAA-2018-0906
Topics
Official Documents
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