Airworthiness Directive

AD 2019-08-07 84 FR 23461 Active

Federal Aviation Administration · 14 CFR part 39

Requires those actions, adds Model A320-216 airplanes, and requires a detailed inspection for, and replacement of, certain rivets, and corrective actions if necessary.

FR document
2019-10653
Amendment
39-19628
Published
2019-05-22
Effective
2019-06-26
Models covered
1

Last live check: 2026-10-04

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AD

2019-08-07

FR doc 2019-10653 · 84 FR 23461

AD 2019-08-07Published 2019-05-22Effective 2019-06-26

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires those actions, adds Model A320-216 airplanes, and requires a detailed inspection for, and replacement of, certain rivets, and corrective actions if necessary.

Supersedes an earlier directive that is not in our index. See the official text.

Full official 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.

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All Bell 205 / 212 directives

Applies to 1 model in our index