MAP Structures & Cargo Stress Engineer

Job Description:

The job holder will be part of MAP Structure & Cargo TADAX1 within the Stress team.

MAP Structure & Cargo is composed of a multidisciplinary cross-functional and international team of highly skilled and motivated engineers involved on the complete Aircraft

Its mission is developed at the intersection of the Program Industrial and Engineering domains acting as a principal actor during the FAL Build Process Ground Testing Flight Testing and Delivery Process

In this position you will have a unique opportunity to be as close as possible to the physical Aircraft and deeply involved trough the complete Aircrafts design build test process Aircraft operations and Delivery to the Customers.

This role requires the ability to adapt to MAP environment and to develop strong links with all Engineering DTO FAL Flight Tests Flight Line Flight Crews Quality Delivery and Production teams.

Additionally in recent years the MAP has been developing skills in Specific Design Workpackage like the Firefighter and other specific additional Capabilities where you will be a key actor.

As a stress member you will have the unique opportunity to be involved in different projects from the Specific Design Workpackage to supporting Production & Flight Test activities

MAP Structures & Cargo mains tasks:

MAP Structures & Cargo in FAL A400M Sevilla is responsible in front of manufacturing organization to:

• Provide Engineering support and expertise to manufacturing organization involved in FAL Sevilla.
• Provide engineering disposition to Concession and DQN (Where we are competent including Partners & Subcontractor).
• Issue Special Instructions to cover temporary design solutions or Configuration Changes.
• Provide engineering statement on Technical/Quality logbook.
• Develop & certify new Aircraft Capabilities for Specific Design Workpackage

Within MAP Structures & Cargo Stress team the job holder:

Support to Specific Design Workpackage

• Stress analysis and validation of metallic composite & hybrid structures using Airbus Defence & Space methods to assess design solutions for a whole range of tasks potentially from concept and structural development to certification and in-service maintenance.
• Static sizing and detailed analysis of the structural components parts and assemblies as well as integration of systems and equipment.
• Analysis and validation at component level for static strength producing relevant strength margins or reserve factors according to validated and applicable Airbus methods & sizing processes.
• Stress analysis by means of FEM techniques (preparation validation and assessment of results) and application of traditional stress justification methods and tools.
• Definition and establishment of the certification/qualification stress documents.
• Structural test definition support and analysis of the tests

Support to Production & Flight Test

• Ensure safe operations of the Product with respect to structural integrity and operational effectiveness
• Liaise with and support stakeholders such as Final Assembly Line Flight Line Delivery Centre Flight Test Centre Design Office Chief Engineers Airworthiness Authorities and other MAP offices for daily business and for improvement projects
• Define and deliver technical solutions in support of build test and delivery of aircraft on Non-Conformities
• Involved in Static&FDT justifications on composite & metallic structures for NCN concessions & Special Instructions following deviation from the definition & need of A/C Configuration change within Flight Test Campaign
• Develop towards getting CoC delegations and autonomy on the complete A/C.
• Be part of various projects (NCs Eradication CSDM digital tools...) in close relation within projects teams and stakeholders so as to continuously improve our efficiency hence our financial and operational performances.
• Opportunities to get more familiar with Flight Tests activities and the creation of Special Instructions (SIs)

Requested skills:

• University Aeronautical Engineering Degree or equivalent
• 5 years experience in Structural analysis of airframe components metallic & composite structures.
• Knowledge of structural analysis in general and design details of airframe including tools.
• Knowledge of Airbus Tools & Methods (ISAMI ISAMI Xpress SRM)
• Ability to understand and perform static calculation within metallic & composites structure according to Airbus methods and sizing processes including FEM techniques.
• Ability to provide stress analyses for the repair/acceptance of metallic & composite damaged structures.
• Ability to understand and integrate technologies in the domain of metallic & composite materials
• Fluent English language Good level of Spanish required
• Good autonomous decision making based on technical experience is essential for this role.
• Strong team working skills and a proven ability to work in a multicultural environment are required in order to build relationships with stakeholders at all levels of the business.

This job requires an awareness of any potential compliance risks and a commitment to act with integrity as the foundation for the Companys success reputation and sustainable growth.

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