Perform static, dynamic, and DaDT structural analyses of metallic and composite airframe structures, mechanical systems, and equipment by hand and by using the automated methods and procedures approved for the program
Ensure that structural repairs meet program requirements and are the lightest, lowest cost, and highest quality products consistent with schedule and budget objectives
The analyst may also be expected to derive non-flight applied loads, create, extract and distribute internal loads, and perform weight and stiffness optimization
Tools utilized may include FEMAP, NX, AFGROW, Teamcenter, and other software applications.10 years minimum, 15 years preferred.