Composite Secondary and Tertiary Structure for Landing Gear
This document will contain guidance and considerations for the use of composite materials on non-primary structure for landing gear systems. Content to include design considerations, conditions and applications where composites are feasible/beneficial, high-level descriptions of various manufacturing processes, and certification/validation considerations.
Rationale: This document is intended to address the use of composites in landing gear applications where they are or may become common in such a way that is not done by AIR5552. There currently are no documents pertaining to composite secondary/tertiary structure on LG components.