---
title: "AMC No. 1 to 25.301(b) Loads — CS-25 · Avioverse"
description: "The engine and its mounting structure are to be stressed to the loading cases for the aeroplane as a whole."
url: "https://avioverse.aero/regulations/easa/cs-25/subpart-c/amc-no-1-to-25-301-b-loads"
---

# AMC No. 1 to 25.301(b) Loads

Large Aeroplanes (CS-25) · CS-25 · EAR revision 26 Jan 2023

AMC Acceptable means of compliance

## AMC No. 1 to 25.301(b) Loads

The engine and its mounting structure are to be stressed to the loading cases for the aeroplane as a whole.

\[Amdt 25/1]

AMC — CS-25 · ED Decision 2005/006/R · CS-25 Easy Access Rules · EAR revision 26 Jan 2023

[All rules in SUBPART C – STRUCTURE](https://avioverse.aero/regulations/easa/cs-25/subpart-c)

Consolidated from the EASA Easy Access Rules (revision 26 Jan 2023, extracted 13 Oct 2026) for convenience. Not the official publication — verify against the Official Journal of the European Union and the EASA publications before operational use.