Loading
Loading
Your feedback directly shapes Sporos.
Sign in to track your feedback history
The FAA is adopting a new airworthiness directive (AD) for certain Airbus SAS Model A350-941 and -1041 airplanes. This AD was prompted by an updated stress analysis on the forward (FWD) cargo door and its attachment piano hinges that revealed a risk of cracking and crack propagation on piano hinges 2 and 3, originating from opening- closing fatigue cycles of the FWD cargo door. This AD requires an inspection of the affected parts, and applicable corrective actions, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.
Published
Apr 8, 2025
Effective
May 13, 2025
Citation
90 FR 15114
Agencies
2
Full text not available in our database.
View on Federal Register →Get a plain-English explanation of what this regulation does, which agencies are responsible, and how it affects existing rules.
No document text available yet
Docket No. FAA-2024-2320
Project Identifier MCAI-2024-00268-T
Amendment 39-23006
AD 2025-07-05
2120-AA64
14 CFR 39