Note from the editor

• found in: CS-29 Amdt 10 - Large Rotercraft (Jan 2023)
• n/a found in: CS-29 Amdt 12 - Large Rotorcraft (Mar 2026)

# Note from the editor The content of this document is arranged as follows: the cover regulation (recitals and articles) of the implementing rule (IR) or delegated rule (DR) appears first, then the IR or DR annex points, followed by the related acceptable means of compliance (AMC) and guidance material (GM). In case of certification specifications (CSs), a CS is followed by the related AMC and GM. All elements (i.e. articles, IRs, DRs, AMC, CSs, and GM) are colour-coded and can be identified according to the illustration below. The EU regulation or EASA Executive Director (ED) decision through which the article, IR, DR, CS, AMC, or GM was introduced or last amended is indicated below the article, IR, DR, CS, AMC, or GM title in italics. <table border="1" cellpadding="0" cellspacing="0" width="603"><tr><td valign="top" width="603"><p>Certification specification</p><p>ED decision</p><p>Acceptable means of compliance</p><p>ED decision</p><p>Guidance material</p><p>ED decision</p></td></tr></table> This document will be updated regularly to incorporate further amendments. The format of this document has been adjusted to make it user-friendly and for reference purposes. Any comments should be sent to erules@easa.europa.eu. # Note from the editor The content of this document is arranged as follows: the cover regulation (recitals and articles) of the implementing rule (IR) or delegated rule (DR) appears first, then the IR or DR annex points, followed by the related acceptable means of compliance (AMC) and guidance material (GM). In case of certification specifications (CSs), a CS is followed by the related AMC and GM. All elements (i.e. articles, IRs, DRs, AMC, CSs, and GM) are colour-coded and can be identified according to the illustration below. The EU regulation or EASA Executive Director (ED) decision through which the article, IR, DR, CS, AMC, or GM was introduced or last amended is indicated below the article, IR, DR, CS, AMC, or GM title in italics. <table border="1" cellpadding="0" cellspacing="0" width="603"><tr><td valign="top" width="603"><p>Certification specification</p><p>ED decision</p><p>Acceptable means of compliance</p><p>ED decision</p><p>Guidance material</p><p>ED decision</p></td></tr></table> This document will be updated regularly to incorporate further amendments. The format of this document has been adjusted to make it user-friendly and for reference purposes. Any comments should be sent to erules@easa.europa.eu. # Note from the editor The content of this document is arranged as follows: the cover regulation (recitals and articles) of the implementing rule (IR) or delegated rule (DR) appears first, then the IR or DR annex points, followed by the related acceptable means of compliance (AMC) and guidance material (GM). In case of certification specifications (CSs), a CS is followed by the related AMC and GM. All elements (i.e. articles, IRs, DRs, AMC, CSs, and GM) are colour-coded and can be identified according to the illustration below. The EU regulation or EASA Executive Director (ED) decision through which the article, IR, DR, CS, AMC, or GM was introduced or last amended is indicated below the article, IR, DR, CS, AMC, or GM title *in italics*. <table cellpadding="7" cellspacing="0"> <col/> <tr> <td valign="top"><h4><a name="_Toc256000003"></a> Certification specification</h4> <p align="right"> <i>ED decision</i></p> <h5><a name="_Toc256000004"></a> Acceptable means of compliance</h5> <p align="right"> <i>ED decision</i></p> <h5><a name="_Toc256000005"></a> Guidance material</h5> <p align="right"> <i>ED decision</i></p> </td> </tr> </table> This document will be updated regularly to incorporate further amendments. The format of this document has been adjusted to make it user-friendly and for reference purposes. Any comments should be sent to erules@easa.europa.eu.