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Proposed rule 2025-17731

Airworthiness Directives; Airbus SAS Airplanes

The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus SAS Model A318-111, -112, and -122; A319-111, -112, -113, -114, -115, -131, -132, and -133; A320-211, -212, -214, -216, - 232, -233, -251N, -252N, -253N, -271N, -272N, and -273N; and A321-211, -212, -213, -231, -232, -251N, -252N, -253N, -271N, -272N, -251NX, - 252NX, -253NX, -271NX, -272NX airplanes. This proposed 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 proposed AD would require 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 proposing this AD to address the unsafe condition on these products.

Source: FederalRegister.gov API v1Recently refreshed. Last successful refresh: 2026-07-31 22:30:24 UTC.

Source-supplied record

Document details

Document number
2025-17731
Published
Sep 15, 2025
Effective
Not supplied
Comments close
Oct 30, 2025
Federal Register citation
90 FR 44350

Docket identifiers

  • Docket No. FAA-2025-2544
  • Project Identifier MCAI-2025-00531-T

CFR references

  • Title 14, part 39