airworthiness · Rule · Final rule. · Published 2026-05-29 · Effective 2026-07-06 · 91 FR 31880
Document
Document number
2026-10799
Federal Register citation
91 FR 31880
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus SAS
Publication date
2026-05-29
Effective date
2026-07-06
FAA docket
Docket No. FAA-2025-2544
Abstract
The FAA is adopting a new airworthiness directive (AD) for certain Airbus SAS Model A318-111, -112, and -122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, -216, -232, -233, -251N, -252N, -253N, -271N, - 272N, and -273N airplanes; and Model A321-211, -212, -213, -231, -232, -251N, -252N, -253N, -271N, -272N, -251NX, -252NX, -253NX, -271NX, and -272NX airplanes. This AD was prompted by the detection of a deviation from the manufacturing process during a review of the cold working process in the assembly line. This AD requires repetitive special detailed inspections (SDIs) and rototest or high frequency eddy current (HFEC) and rototest inspections of the affected fasteners and fastener holes, and applicable on-condition actions. The FAA is issuing this AD to address the unsafe condition on these products.