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Proposed rule 2025-08784

Airworthiness Directives; Airbus SAS Airplanes

The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus SAS Model A319-112 and -132 airplanes, and Model A320-214, -232, -233, -251N, and -271N airplanes. This proposed AD was prompted by rivet holes being left unplugged after bracket relocation or removal accomplished during certain modifications, potentially resulting in fatigue damage starting from those rivet holes. This proposed AD would require a one-time special detailed inspection (SDI) of the rivet holes and applicable corrective actions; and would also allow the installation of certain modifications, provided rivets are installed after the modification; as specified in a European Union Aviation Safety Agency (EASA) AD, which is proposed for incorporation by reference (IBR). 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 22:49:02 UTC.

Source-supplied record

Document details

Document number
2025-08784
Published
May 19, 2025
Effective
Not supplied
Comments close
Jul 3, 2025
Federal Register citation
90 FR 21247

Docket identifiers

  • Docket No. FAA-2025-0907
  • Project Identifier MCAI-2024-00634-T

CFR references

  • Title 14, part 39