Requirements

• Aircraft structural knowledge
o Assembly and Joining Processes
o Model Based Definition Interrogation
o Software: CATIA

• Composites Analysis
o Static Analysis, CLPT, Bearing/Bypass, Radius Bending, Peak Strain
o Software: IAS, CSW, GKJOINT, FKBEND/UBEND

• Metallic Analysis
o Classical Static Stress Methods (FBD, BDMs)
o Book 2 Fatigue Methods
o Book 3 Damage Tolerance Methods
o Software: IAS, CSW, IDTAS, DTANAL

• Bolt Bending Analysis (Static and Fatigue)

• Documentation and Archival
o Stress Notes Documentation
o Software: MS Word, ENOVIA

Education/experience typically acquired through advanced technical education from an accredited course of study in engineering, computer science, mathematics, physics or chemistry (e.g. Bachelor) and typically 5 or more years' related work experience or an equivalent combination of technical education and experience (e.g. PhD, Master+3 years' related work experience). In the USA, ABET accreditation is the preferred, although not required, accreditation standard.