---
title: "CS-E 525 Continued Rotation — CS-E · Avioverse"
description: "(see AMC E 525) If any of the Engine’s main rotating systems will continue to rotate after the Engine is shutdown for any reason while in flight, and…"
url: "https://avioverse.aero/regulations/easa/cs-e/subpart-d/cs-e-525-continued-rotation"
---

# CS-E 525 Continued Rotation

Engines (CS-E) · CS-E · EAR revision 7 Dec 2023

IR Implementing rule

## CS-E 525 Continued Rotation

(see AMC E 525)

If any of the Engine’s main rotating systems will continue to rotate after the Engine is shutdown for any reason while in flight, and means to prevent that continued rotation, are not provided, any continued rotation during the maximum period of flight and in the flight conditions expected to occur with that Engine inoperative must not result in effects that would be unacceptable under CS-E 510.

\[Amdt. No.: E/1]

IR — CS-E · ED Decision 2007/015/R · CS-E Easy Access Rules · EAR revision 7 Dec 2023

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

Consolidated from the EASA Easy Access Rules (revision 7 Dec 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.