---
title: "CS-E 210 Failure Analysis — CS-E · Avioverse"
description: "(See AMC E 210) (a) A Failure analysis of the Engine, including the control system for a typical installation must be made to establish that no single…"
url: "https://avioverse.aero/regulations/easa/cs-e/subpart-b/cs-e-210-failure-analysis"
---

# CS-E 210 Failure Analysis

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

IR Implementing rule

## CS-E 210 Failure Analysis

(See AMC E 210)

(a) A Failure analysis of the Engine, including the control system for a typical installation must be made to establish that no single Fault, or double Fault if one of the Faults may be present and undetected during pre-flight checks, could lead to unsafe Engine conditions beyond the normal control of the flight crew.

(b) In certain cases the Failure analysis will depend on assumed installation conditions. Such assumptions must be stated in the analysis.

\[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 B — PISTON ENGINES: DESIGN AND CONSTRUCTION](https://avioverse.aero/regulations/easa/cs-e/subpart-b)

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.