---
title: "CS 25.681 Limit load static tests — CS-25 · Avioverse"
description: "Compliance with the limit load requirements of this CS-25 must be shown by tests in which – (1) The direction of the test loads produces the most severe…"
url: "https://avioverse.aero/regulations/easa/cs-25/subpart-d/cs-25-681"
---

# CS 25.681 Limit load static tests

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

IR Implementing rule

## CS 25.681 Limit load static tests

(a) Compliance with the limit load requirements of this CS-25 must be shown by tests in which –

(1) The direction of the test loads produces the most severe loading in the control system; and

(2) Each fitting, pulley, and bracket used in attaching the system to the main structure is included.

(b) Compliance must be shown (by analyses or individual load tests) with the special factor requirements for control system joints subject to angular motion.

IR · CS 25.681 — CS-25 · ED Decision 2003/2/RM · CS-25 Easy Access Rules · EAR revision 26 Jan 2023

[All rules in SUBPART D – DESIGN AND CONSTRUCTION](https://avioverse.aero/regulations/easa/cs-25/subpart-d)

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.