Work Location | Kinston, Mobile |
Duration (in months) | Permanent |
Skillset | - Proficiency with Fatigue and Damage Tolerance Analysis for structure.
- Advanced Static and non-linear analysis experience.
- Knowledge of hand calculations and FE analysis.
- Knowledge of Airbus processes and procedures relating to design (RSDP, SIDP, AP, ABD, AIPI, AIPS, etc..).
- Understanding of aerospace design principles and airworthiness requirements.
- Experience of using Airbus Supply (DocMaster, Airnavx etc.).
- Ensuring the safe operation of Airbus aircraft with respect to structural integrity.
- Airbus stress Signatory experience (Checker/approver).
- Valid Airbus training certificates in AIRBUS SAP, ISAMI, VPM and PASS SSI.
- Bi-lingual (French and English).
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Tools | PATRAN, NASTRAN, ISAMI Analyst, ABAQUS, SAP PAC, GISEH, Hyper Works, PASS SSI, VPM, SRM/ASR, ADL, Python, MS Visual Basic, JIRA, MTS, HSB |
Job Description | - Lead and Perform Static, Fatigue and Damage Tolerance (FDT) stress analysis of primary and secondary aircraft structures using classical hand calculation and Finite Element Analysis (FEA).
- Should be having metallic and composite structure stress analysis working experience.
- Understanding of load paths, extraction of loads from Finite Element Models (GFEM/DFEM).
- Determination of critical failure modes and performing analysis to ensure structural integrity.
- Mitigation techniques for low margins of safety
- Preparation of stress dossiers as per certification requirements
- Review and validate Stress analysis output and Stress Dossiers to ensure compliance with technical requirements.
- Drive issue resolution by interfacing with cross functional teams (Design, manufacturing, quality, configuration management, etc.).
- Serve as a technical representative for onsite offshore coordination, addressing queries, clarifications, and technical escalations.
- Applicant should preferably be familiar with and have prior working experience on Airbus Stress Tools, including ISAMI.
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Required Qualifications (Non-negotiable requirements) | - BE / BTECH/MTECH/MS or equivalent degree (Aerospace/ Mechanical Engineering)
- 5–10 years of hands‑on experience in aerospace structural stress analysis.
- Proven experience working on Airbus aircraft programs (A320, A330, A350, A380, etc.).
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