airworthiness · Rule · Final rule. · Published 2018-03-15 · Effective 2018-04-19 · 83 FR 11399
Document
Document number
2018-05018
Federal Register citation
83 FR 11399
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus
Publication date
2018-03-15
Effective date
2018-04-19
FAA docket
Docket No. FAA-2017-0695
Abstract
We are superseding Airworthiness Directive (AD) 2009-18-16, which applied to certain Airbus Model A310-203, -204, -221, -222, -304, -322, -324, and -325 airplanes. AD 2009-18-16 required an inspection for cracking of certain fastener holes on certain frames, and related investigative and corrective actions if necessary; and modification of certain fastener holes. This new AD reduces the compliance times. This AD was prompted by the identification of a structural modification that falls within the scope of the work related to the extension of the service life of the affected airplanes and widespread fatigue damage evaluations. We are issuing this AD to address the unsafe condition on these products.