EASA AD US-2025-05-16: Fuselage - Skin under the Drag Link Assembly - Inspection | RegNotify

Airworthiness DirectiveEASA AD US-2025-05-16

Fuselage - Skin under the Drag Link Assembly - Inspection

Published: Mar 25, 2025
Effective: Apr 22, 2025

Boeing 737

AI-generated summary of the official EASA document. Verify against the PDF before acting.

What to do

Affected stakeholders should implement the specified inspection procedures for the fuselage skin under the drag link assembly as outlined in the directive. Maintenance schedules should be updated accordingly to include these inspections at the prescribed intervals. No specific compliance deadlines are provided in the document.

Summary

The document titled 'Fuselage - Skin under the Drag Link Assembly - Inspection' is a regulatory directive focusing on the inspection requirements for the fuselage skin located beneath the drag link assembly. The document aims to ensure the structural integrity of this specific aircraft component, although no specific aircraft types, engine models, or part numbers are mentioned.

What changed

This directive introduces mandatory inspection procedures for the fuselage skin under the drag link assembly to detect potential damage or wear. It establishes inspection criteria and intervals to maintain airworthiness and prevent structural failures. No amendments or prior regulations are referenced.

Why it matters

This directive is important for aviation professionals as it helps maintain the safety and reliability of the aircraft structure by identifying possible issues early. Operators and maintenance organizations must incorporate these inspections into their routine maintenance programs to ensure compliance and avoid operational disruptions. Compliance teams need to track these requirements to meet regulatory standards.

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