High-strength aluminum, stainless steel, and titanium structural flight hardware engineered to withstand high aerodynamic fatigue, vibration, and multi-axis g-force loads.
Airframe structural clips, fuselage frame brackets, and fuel tank baffle gussets must withstand continuous cyclic fatigue without crack initiation.
Our CAM programmers strictly control sheet nesting orientation relative to the rolling grain of 7075 and 2024 alloys, ensuring bend lines cross transverse to grain to eliminate micro-cracking.
Cutting with 99.999% pure high-pressure nitrogen gas prevents oxygen recast layers, ensuring pristine cut edges ready for deburring, chemical conversion, or fusion welding.
Every bracket batch is accompanied by raw material Mill Test Reports (MTRs), Certificates of Conformance (COC), and AS9102 First Article Inspection reports archived in our secure digital vault.
Speak directly with Garret Maino and our Plainville manufacturing engineers. Submit STEP, DXF, or PDF drawings for comprehensive DFM review and production quotation.