Summary
The FAA is adopting a new airworthiness directive (AD) for certain Airbus SAS Model A318 and A319 series 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 frame (FR) 16 and FR 20 web holes and passenger door intercostal fitting holes at the door stop fitting locations. This AD requires repetitive rototest inspections of the holes at the door stop fittings for any cracking, and corrective actions if necessary, as specified in a European Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.
Directive Details
AD Number
FAA-2019-0254
Document Number
2019-24508
Type
Rule
Publication Date
November 13, 2019
Effective Date
December 18, 2019
Affected Manufacturer
Airbus SAS
Criticality
routine
Emergency
No
Docket ID
Docket No. FAA-2019-0254
Topics
Official Documents
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