EASA AD 2025-0174R1: Fuselage — Rear Structure / Rear Frame — Inspection | RegNotify

Airworthiness DirectiveEASA AD 2025-0174R1

Fuselage — Rear Structure / Rear Frame — Inspection

Published: Sep 22, 2025
Effective: Sep 29, 2025

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

What to do

Operators and maintenance teams of AIRBUS HELICOPTERS DEUTSCHLAND EC135 and EC635 helicopters should review and implement the inspection procedures outlined in this document. They must schedule and perform the required inspections within the specified intervals to maintain compliance and ensure aircraft safety. No explicit compliance deadlines are provided in the extracted content.

Summary

Fuselage — Rear Structure / Rear Frame — Inspection is a regulatory document concerning the inspection requirements for the rear structure and rear frame of AIRBUS HELICOPTERS DEUTSCHLAND EC135 and EC635 helicopter models. It provides guidance on maintaining the structural integrity of these specific helicopter fuselage components to ensure continued airworthiness and safety.

What changed

This document introduces inspection protocols specifically targeting the rear fuselage structure and rear frame of the EC135 and EC635 helicopters. It establishes new or updated inspection criteria to detect potential structural issues that could affect the safety and performance of these aircraft models.

Why it matters

This document is critical for aviation professionals because it helps operators and maintenance organizations identify and address potential structural weaknesses in the rear fuselage area of EC135 and EC635 helicopters. Compliance ensures continued airworthiness, reduces the risk of structural failure, and supports safe flight operations.

More for Airbus Helicopters EC135

All 49

Get the next one by email

New ADs and bulletins for Airbus Helicopters EC135 and Helicopters 635, summarized like this page, every Monday.