Summary
We are adopting a new airworthiness directive (AD) for certain Airbus SAS Model A350-941 airplanes. This AD was prompted by a review of the Airbus A350 structure design principles database for type definition that revealed that the balancer fitting part, installed on the tail cone, on a certain frame (FR) has several corrosion-resistant stainless steel nuts that do not meet the requirements for protection against corrosion. This AD requires application of a new additional overcoat sealant and elastic varnish on the affected nuts and fasteners. We are issuing this AD to address the unsafe condition on these products.
Directive Details
AD Number
FAA-2018-0758
Document Number
2018-24683
Type
Rule
Publication Date
November 14, 2018
Effective Date
December 19, 2018
Affected Manufacturer
Airbus SAS
Criticality
routine
Emergency
No
Docket ID
Docket No. FAA-2018-0758
Topics
Official Documents
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