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Design of primary, secondary and tertiary airframe structures, work-stations, hard-points and other similar structural installations in metallic and composite materials for a variety of airborne platforms.

Production of parts, assemblies and installation drawings using Solid Works in compliance with the Design Office Handbook (DOH) and relevant Certification Basis e.g. CS-27.

Provision of support to the avionics/electrical design engineers in matters relating to mechanical/structural design.

Provision of support to the production and installation engineers in matters relating to mechanical/structural design.

Carry out aircraft surveys to define design solutions as required.

Knowledge of, and the ability to select, appropriate mechanical/structural techniques and solutions for aerospace applications e.g. fuselage hard-points, cabin structures. (E)

Knowledge of aerospace structural manufacturing processes. (E)

Conceptual structures/mechanical design. (E)

Understanding of cockpit/cabin ergonomics. (D)

EASA Part 21 Subpart J (DOA) requirements. (D)

EASA Part 21 Subpart G (POA) requirements. (D)

Ability to work to a high and consistent level of accuracy (E)

Proficient user of Solid Works CAD (D – training can be provided)

Proficient user of Microsoft Office (Word, Excel, Outlook) (E)

Ability to work as part of a team (E)

HNC, HND, Degree in a relevant engineering subject. (E)

An engineering apprenticeship with relevant experience. (D)

Experience working within an Aerospace Design Office. (E)

Experience of the full design life-cycle from conception to delivery of the design package. (D)