---
title: "CS 23.2625 Instructions for Continued Airworthiness — CS-23 · Avioverse"
description: "The applicant must prepare Instructions for Continued Airworthiness that are appropriate for the certification level and performance level of the…"
url: "https://avioverse.aero/regulations/easa/cs-23/subpart-g/cs-23-2625"
---

# CS 23.2625 Instructions for Continued Airworthiness

Normal-Category Aeroplanes (CS-23) · CS-23 · EAR revision 13 May 2026

IR Implementing rule

## CS 23.2625 Instructions for Continued Airworthiness

(a) The applicant must prepare Instructions for Continued Airworthiness that are appropriate for the certification level and performance level of the aeroplane.

(b) If Instructions for Continued Airworthiness are not supplied by the manufacturer of an appliance or product installed in the aeroplane, the Instructions for Continued Airworthiness for the aeroplane must include the information essential to the continued airworthiness of the aeroplane.

(c) The Instructions for Continued Airworthiness must contain a Section titled ‘Airworthiness limitations’ that is segregated and clearly distinguishable from the rest of the document. This Section must set forth each mandatory replacement time, structural inspection interval, and related structural inspection procedure required for type certification. This Section must contain a legible statement in a prominent location that reads: ‘The Airworthiness limitations Section is approved and variations must also be approved’.

(d) The applicant must develop and implement procedures to prevent structural failures due to foreseeable causes of strength degradation, which could result in serious or fatal injuries, loss of the aeroplane, or extended periods of operation with reduced safety margins. The Instructions for Continued Airworthiness must include procedures developed under CS 23.2255.

IR · CS 23.2625 — CS-23 · ED Decision 2017/013/R · CS-23 Easy Access Rules · EAR revision 13 May 2026

AMC Acceptable means of compliance

## AMC1 23.2625 Instructions for Continued Airworthiness

ASTM F44 F3264 Standard Specification for Normal Category Aeroplanes Certification

10.6 Instructions for Continued Airworthiness

F3120/F3120M-20 Standard Specification for Ice Protection for General Aviation Aircraft F3117/F3117M-24a Standard Specification for Crew Interface in Aircraft

F3408/F3408M-21 Standard Specification for Aircraft Emergency Parachute Recovery Systems \[AMC\&GM to CS-23: Issue 4]

\[AMC & GM to CS-23: Issue 5]

AMC · AMC1 23.2625 — CS-23 · ED Decision 2026/003/R · CS-23 Easy Access Rules · EAR revision 13 May 2026

AMC Acceptable means of compliance

## AMC2 23.2625 Instructions for Continued Airworthiness

CS-23 Amdt 4

23.1529 Instructions for Continued Airworthiness (With Appendix G)

AMC · AMC2 23.2625 — CS-23 · ED Decision 2017/025/R · CS-23 Easy Access Rules · EAR revision 13 May 2026

AMC Acceptable means of compliance

## AMC3 23.2625 Instructions for Continued Airworthiness

CS VLA Amdt 1

VLA.1529 Instructions for Continued Airworthiness

AMC · AMC3 23.2625 — CS-23 · ED Decision 2017/025/R · CS-23 Easy Access Rules · EAR revision 13 May 2026

[All rules in SUBPART G — FLIGHT CREW INTERFACE AND OTHER INFORMATION](https://avioverse.aero/regulations/easa/cs-23/subpart-g)

Consolidated from the EASA Easy Access Rules (revision 13 May 2026, 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.