Reports to: Chief Engineer
Role Purpose: Structural substantiation analytically and empirically for all Company products
Key Authorities and Responsibilities:
Produce technical documents, namely interface loads analysis, SEI substantiation, stress reports, Static test plans and reports.
Witness and provide documentary support, for product weight assessment and measurement.
Attain familiarity with technical specifications, aircraft regulations and company procedures and have the ability to review these and apply relevant criteria to the task in hand.
Implement technical specifications, aircraft regulations and company procedures to the task in hand
Demonstrate an understanding for fundamental engineering principles, their application to structures and material, especially related to the aerospace field.
Be able to recognise the most applicable method of structural substantiation required for a given task. Have an appreciation of the physical behaviour of metal and composite material under loading conditions.
Have used FEM, specifically NISA.
Liaise with external sub-contract companies when required.
Prime Working Relationships:
EASA/CAA/NAA/Airframe manufactures.
Provide support and liaise with design, manufacturing and quality departments. Provide guidance to the test laboratory on structural testing.
Demonstrate the ability to work within a team environment.
Preferred Experience and Qualifications:
Degree or HNC/D or equivalent in Engineering discipline
Experience in aircraft cabin interior detailed structural analysis and composites.
Experience in FEM of aircraft cabin interiors.
Previously held signatory position for aircraft structures
Other Conditions:
Willingness and ability to travel within the UK and abroad, sometimes at short notice.
"Due to the high volume of applications we currently receive, we are unable to respond to all candidates. If you do not hear from a Consultant within 5 working days unfortunately you have been unsuccessful on this occasion"
