EASA AD US-2024-24-01: Fuselage - Upper Frame at the Frame Splices between Stringers - Inspections | RegNotify

Airworthiness DirectiveEASA AD US-2024-24-01

Fuselage - Upper Frame at the Frame Splices between Stringers - Inspections

Published: Dec 10, 2024
Effective: Jan 13, 2025

Boeing 757

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

What to do

Operators and maintenance organizations should implement the specified inspection procedures for the fuselage upper frame splices as outlined in the document. They must schedule inspections according to the defined intervals and report findings as required. No specific compliance deadlines are stated in the document.

Summary

The document titled 'Fuselage - Upper Frame at the Frame Splices between Stringers - Inspections' is a regulatory directive focusing on inspection requirements for the upper fuselage frame splices located between stringers. It addresses structural integrity concerns relevant to aircraft fuselage maintenance. Specific aircraft types, engine models, or part numbers are not explicitly mentioned in the document.

What changed

This document introduces mandatory inspection procedures for the fuselage upper frame at the frame splices between stringers. It establishes new inspection criteria and intervals to detect potential structural issues early. There are no amendments or superseded regulations indicated.

Why it matters

This directive is critical for aviation maintenance professionals and operators to ensure the continued airworthiness of aircraft fuselage structures. Early detection of frame splice issues helps prevent structural failures and enhances flight safety. Compliance with these inspections supports regulatory adherence and reduces the risk of costly repairs or operational disruptions.

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