Flight Controls - Tamarack Active Technology Load Alleviation System (ATLAS) Winglets - Placard Installation / AFM Revision
- Published
- Effective
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Affected stakeholders must install the required placards on the aircraft and update the AFM as specified in the document. Compliance with these requirements should be verified promptly to ensure continued airworthiness and regulatory compliance. No explicit deadlines are provided in the document for these actions.
Summary
The Flight Controls - Tamarack Active Technology Load Alleviation System (ATLAS) Winglets - Placard Installation / AFM Revision is a regulatory document addressing the installation of placards and revisions to the Aircraft Flight Manual (AFM) related to Tamarack ATLAS winglets. It applies to aircraft equipped with these winglets to ensure proper operational awareness and compliance with updated flight control requirements.
What changed
This document introduces requirements for installing specific placards on aircraft fitted with Tamarack ATLAS winglets and mandates corresponding revisions to the AFM. It establishes new operational information and limitations to be included in the AFM to reflect the characteristics of the ATLAS winglets.
Why it matters
The changes are critical for aviation professionals to maintain aircraft airworthiness and operational safety when using Tamarack ATLAS winglets. Operators, maintenance organizations, and compliance teams must ensure that placards are correctly installed and AFM revisions are incorporated to meet regulatory standards and avoid potential flight control issues.
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