Fuselage — Frame No.9 — Inspection / Repair

Published: Sep 19, 2019
Effective: Oct 3, 2019

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

What to do

Operators and maintenance teams should implement the inspection and repair procedures for Frame No.9 as outlined in the document. They should schedule inspections according to the guidance and carry out repairs promptly if any damage is found. No specific compliance deadlines are stated, so stakeholders should monitor for further updates or instructions.

Summary

The document titled 'Fuselage — Frame No.9 — Inspection / Repair' pertains to AIRBUS HELICOPTERS models SA/AS 365 and EC 155. It addresses inspection and repair procedures specifically for Frame No.9 of the fuselage structure on these helicopter types. The document provides guidance to ensure structural integrity and airworthiness of the affected aircraft.

What changed

This document introduces inspection and repair requirements for the fuselage Frame No.9 on AIRBUS HELICOPTERS SA/AS 365 and EC 155 models. It establishes protocols for identifying damage and performing necessary repairs to maintain safety standards. As the extracted content was unavailable, no amendments or prior versions are referenced.

Why it matters

This document is important for aviation professionals because it ensures the continued structural safety of AIRBUS HELICOPTERS SA/AS 365 and EC 155 aircraft. Operators and maintenance organizations must follow these inspection and repair guidelines to prevent potential structural failures. Compliance helps maintain regulatory airworthiness and reduces the risk of in-service incidents related to fuselage integrity.

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