Technical aspects:
Domain:
Airframe fuselage (metallic parts):
Frame,
Panel,
Stringer,
Cross Beam,
Frame coupling,
Skin doubler,
System brackets

Carry out the design checking,
Examples of previous experience required in the domain:
Design solutions from a clean sheet:
- Single parts,
- Assemblies,

Design improvements by suggesting alternative solutions,
Realisation of static predimisionning,
Modification of existing solutions to:
New system installation,
Structural reinforcement,
Weight optimisation,

Coupling definition for structural parts based of the section or
type of loading:
Definition of the type and number of fasteners,
Design of coupling parts,

An awareness of common manufacturing constrains,
Experience in cabin interior and/ or system definition would be
appreciated but not necessary.