← FAA Federal Register actions

Airworthiness Directives; Airbus SAS Airplanes

airworthiness · Rule · Final rule. · Published 2019-05-22 · Effective 2019-06-26 · 84 FR 23461

Document

Document number
2019-10653
Federal Register citation
84 FR 23461
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus SAS
Publication date
2019-05-22
Effective date
2019-06-26
FAA docket
Docket No. FAA-2018-0795

Abstract

We are superseding Airworthiness Directive (AD) 2014-20-04, which applied to all Airbus SAS Model A318 and A319 series airplanes; Airbus SAS Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; and Airbus SAS Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes. AD 2014-20-04 required repetitive inspections of the titanium angles between the belly fairing and the keel beam side panel, an inspection of the open holes of cracked titanium angles, and corrective action if necessary. This AD continues to require those actions, adds Model A320-216 airplanes, and requires a detailed inspection for, and replacement of, certain rivets, and corrective actions if necessary. This AD was prompted by reports of cracks at the lower riveting of the four titanium angles that connect the belly fairing to the keel beam side panels. We are issuing this AD to address the unsafe condition on these products.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown