Summary
We are adopting a new airworthiness directive (AD) for all Airbus Model A321 series airplanes. This AD was prompted by a determination from fatigue testing that cracks could develop in the cabin floor beam junction at certain fuselage frame locations. This AD requires repetitive inspections for cracking in the cabin floor beam junction at certain fuselage frame locations, and repair if necessary. We are issuing this AD to address the unsafe condition on these products.
Directive Details
AD Number
FAA-2016-9498
Document Number
2017-14588
Type
Rule
Publication Date
July 19, 2017
Effective Date
August 23, 2017
Affected Manufacturer
Airbus
Criticality
routine
Emergency
No
Docket ID
Docket No. FAA-2016-9498
Topics
Official Documents
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