Loading
Loading
Your feedback directly shapes Sporos.
Sign in to track your feedback history
The FAA is adopting a new airworthiness directive (AD) for all Embraer S.A. Model EMB-120, -120ER, -120FC, -120QC, and -120RT airplanes. This AD was prompted by a structural assessment, which found that the fuselage longitudinal skin splice and panel between certain frames are susceptible to cracking. This AD requires performing repetitive inspections of the fuselage center I longitudinal skin splice and applicable corrective actions, as specified in an Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC) AD, which is incorporated by reference (IBR). The FAA is issuing this AD to address the unsafe condition on these products.
Published
Feb 11, 2025
Effective
Mar 18, 2025
Citation
90 FR 9283
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-2024-2140
Project Identifier MCAI-2024-00242-T
Amendment 39-22942
AD 2025-02-09
2120-AA64
14 CFR 39