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:
|
SC-VTOL |
CS-27 Amdt. 6 |
|
VTOL.2260 (a) |
CS 27.603 Material CS 27.613 (c) Material strength properties and design values |
|
VTOL.2260 (b) |
CS 27.605 Fabrication methods |
|
VTOL.2260 (c) |
CS 27.613 (a) & (b) Material strength properties and design values |
|
VTOL.2260 (d) |
CS 27.613 (a) Material strength properties and design values |
|
VTOL.2260 (e) |
CS 27.603 (c) Materials |
|
VTOL.2260 (f) |
CS 27.613 (e) Material strength properties and design values |
|
VTOL.2260 (g) |
CS 27.613 Material strength properties and design values |
(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.
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