The document describes the design and optimization of an airplane bearing bracket using Inspire software. The initial design was optimized to reduce the mass by 23% while meeting the design envelope requirements and withstanding three load cases. Modifications made during optimization included allowing movement of fastener footprints and modifying cross-sectional changes. The final optimized design had a mass of 228 grams and stress levels under 100% of the yield stress. The bracket is intended to be manufactured using additive manufacturing.