(definition, implementation/and functional validation). Especially in avionics and electrical
FAA/EASA/Part 25/MILS-STD regulations knowledge and application
ATA 25/ATA 24 knowledge
2D->3D conversion
Limited
knowledge and experience about Structural Design and Stress Analysis
, Product design and developments, Technology Development. Design optimization.
Work Experience
Education
:
Bachelors degree in Mechanical or Aerospace Engineering
.
6
- 10 years of
experience
in Aerospace sector working in OEMs Final Assembly Lines (FALs) or Aircraft Systems related Tier-1s. Familiarity with international environments.
Experience in
managing OEMs technical/process documentation.
*
Fluent English level
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