airworthiness · Rule · Final rule. · Published 2020-09-03 · Effective 2020-10-08 · 85 FR 54893
Document
Document number
2020-19401
Federal Register citation
85 FR 54893
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus SAS
Publication date
2020-09-03
Effective date
2020-10-08
FAA docket
Docket No. FAA-2020-0332
Abstract
The FAA is adopting a new airworthiness directive (AD) for certain Airbus SAS Model A318 series airplanes; Model A319-111, -112, - 113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes; and Model A321-111, -112, - 131, -211, -212, -213, -231, and -232 airplanes. This AD was prompted by a report that cracks were detected on the left-hand (LH) and right- hand (RH) sides of the first rivet hole of the frame (FR) 43 foot coupling during scheduled maintenance. This AD requires a rotating probe test of the fastener holes at FR43 on the LH and RH sides for any cracking, and on-condition actions if necessary, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.