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MOC VTOL.2260 Materials and processes
Available versions for ERULES-1963177438-22433
n/a
found in: Small Category VCA (Revision 0) SC-VTOL (Oct 2024)
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Small Category VCA... (Oct 2024)
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MOC VTOL.2260 Materials and processes n/a (a) The following combination of CS-27 Amdt. 6 requirements, with their corresponding guidance material, is accepted as a means of compliance with [VTOL.2260](#_DxCrossRefBm1877490473): <table border="1" cellpadding="0" cellspacing="0" width="567"><tr><td valign="top" width="142"><p>SC-VTOL</p></td><td valign="top" width="425"><p>CS-27 Amdt. 6</p></td></tr><tr><td valign="top" width="142"><p><a href="#_DxCrossRefBm1877490473">VTOL.2260</a> (a)</p></td><td valign="top" width="425"><p>CS 27.603 Material </p><p>CS 27.613 (c) Material strength properties and design values</p></td></tr><tr><td valign="top" width="142"><p><a href="#_DxCrossRefBm1877490473">VTOL.2260</a> (b)</p></td><td valign="top" width="425"><p>CS 27.605 Fabrication methods</p></td></tr><tr><td valign="top" width="142"><p><a href="#_DxCrossRefBm1877490473">VTOL.2260</a> (c)</p></td><td valign="top" width="425"><p>CS 27.613 (a) & (b) Material strength properties and design values</p></td></tr><tr><td valign="top" width="142"><p><a href="#_DxCrossRefBm1877490473">VTOL.2260</a> (d)</p></td><td valign="top" width="425"><p>CS 27.613 (a) Material strength properties and design values </p></td></tr><tr><td valign="top" width="142"><p><a href="#_DxCrossRefBm1877490473">VTOL.2260</a> (e)</p></td><td valign="top" width="425"><p>CS 27.603 (c) Materials </p></td></tr><tr><td valign="top" width="142"><p><a href="#_DxCrossRefBm1877490473">VTOL.2260</a> (f)</p></td><td valign="top" width="425"><p>CS 27.613 (e) Material strength properties and design values </p></td></tr><tr><td valign="top" width="142"><p><a href="#_DxCrossRefBm1877490473">VTOL.2260</a> (g)</p></td><td valign="top" width="425"><p>CS 27.613 Material strength properties and design values </p></td></tr></table> (b) For composite structures, additional guidance can be found in AMC 20-29 chapter 6 and MOC VTOL.2240 (a) & (b). (c) For additive manufacturing, additional guidance can be found in the EASA Certification Memorandum CM-S-008.