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Final rule 2025-16404

Airworthiness Directives; Airbus SAS Airplanes

The FAA is superseding Airworthiness Directive (AD) 2017-14- 14, which applied to all Airbus SAS Model A321-111, -112, -131, -211, - 212, -213, -231, and -232 airplanes. AD 2017-14-14 required repetitive inspections for cracking in the cabin floor beam junction at certain fuselage frame locations and repair if necessary. Since the FAA issued AD 2017-14-14, further analysis determined that the compliance times for the inspections must also be based on flight hours. This AD continues to require the actions in AD 2017-14-14, revises compliance times, and adds a provision for optional modifications. The FAA is issuing 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
2025-16404
Published
Aug 27, 2025
Effective
Oct 1, 2025
Comments close
Not supplied
Federal Register citation
90 FR 41773

Docket identifiers

  • Docket No. FAA-2025-0213
  • Project Identifier MCAI-2024-00385-T
  • Amendment 39-23115
  • AD 2025-17-05

CFR references

  • Title 14, part 39