---
title: "CS-E 700 Excess Operating Conditions — CS-E · Avioverse"
description: "(See AMC E 700) Where any of the operating conditions (e.g. air or gas pressure, thrust, gas temperature) substantiated elsewhere in this subpart could…"
url: "https://avioverse.aero/regulations/easa/cs-e/subpart-e/cs-e-700-excess-operating-conditions"
---

# CS-E 700 Excess Operating Conditions

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

IR Implementing rule

## CS-E 700 Excess Operating Conditions

(See AMC E 700)

Where any of the operating conditions (e.g. air or gas pressure, thrust, gas temperature) substantiated elsewhere in this subpart could be exceeded in any of the normal and likely emergency conditions within the flight envelope declared by the Engine constructor, it must be established to the satisfaction of the Agency that the most severe conditions likely to occur will have no unacceptable effects on the Engine.

\[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 E – TURBINE ENGINES: TYPE SUBSTANTIATION](https://avioverse.aero/regulations/easa/cs-e/subpart-e)

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.