9 Damage Tolerance Jobs

Exposure to Aero Repairs/Concession Activities Proficiency in MS Office (Word, Excel, PPT) Hands-on experience with Tools NASTRAN, PATRAN & ISAMI Education Requirements BE / MTech in Aerospace or Mechanical Engineering Skills Required to Succeed in This Job Experience in Aero-structure, preferably with wing and high-lift devices Knowledge of concession treatment process Ability to provide stress assessment for various manufacturing non-conformities Strong knowledge in Strength of Materials, Aircraft Materials, and stress justification using hand calculations (classical methods) Experience working on AIRBUS A350 or legacy programs Familiarity with AIRBUS concession processes and methods Knowledge of AIRBUS-specific tools like ISAMI Experience with SAP PR3/PAC Fatigue and Damage Tolerance experience is an added advantage Able to meet tight deadlines and handle customer demands Willing to work early or late shifts based on project needs

Project Role : Manufacturing Engineering Practitioner Project Role Description : Define processes to fabricate, assemble, inspect and test new products and machines based on production engineering and design principles. Define the supporting tools and fixtures needed for production. Develop procedures, product specifications and define the quality standards and inspection methods. Must have skills : Fatigue & Damage Tolerance F&DT Good to have skills : NAMinimum 3 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Manufacturing Engineering Practitioner, you will define processes to fabricate, assemble, inspect, and test new products and machines based on production engineering and design principles. You will also define supporting tools and fixtures needed for production, develop procedures, product specifications, and define quality standards and inspection methods. Roles & Responsibilities:- Expected to perform independently and become an SME.- Required active participation/contribution in team discussions.- Contribute in providing solutions to work-related problems.- Develop innovative manufacturing processes to improve efficiency.- Collaborate with cross-functional teams to optimize production workflows. Professional & Technical Skills: - Must To Have Skills: Proficiency in Fatigue & Damage Tolerance F&DT.- Strong understanding of structural analysis and material properties.- Experience in CAD software for designing manufacturing processes.- Knowledge of industry standards and regulations for product quality assurance. Additional Information:- The candidate should have a minimum of 3 years of experience in Fatigue & Damage Tolerance F&DT.- This position is based at our Bengaluru office.- A 15 years full-time education is required. Qualification 15 years full time education

Key Responsibilities: Perform fatigue and damage tolerance analysis of metallic and composite structures in accordance with regulatory and OEM standards (e.g., FAA, EASA). Utilize tools like NASGRO , DARWIN , or other proprietary applications for crack growth and fracture mechanics analysis. Conduct life prediction assessments under static and dynamic loading conditions, including variable amplitude loading. Support aircraft certification programs by providing substantiation reports and analysis documentation. Work closely with design, stress, materials, and manufacturing teams to define inspection intervals and structural integrity requirements. Interpret test data and validate analytical models against physical test results. Develop and review fatigue test plans and evaluate test outcomes. Document assumptions, methodologies, and results in clear, traceable technical reports. Required Skills & Qualifications: Bachelor’s or Master’s degree in Mechanical, Aerospace, or Structural Engineering. 3 to 7 years of experience in fatigue and damage tolerance analysis. Hands-on experience with at least one of the following tools: NASGRO , DARWIN , or equivalent. Solid understanding of fracture mechanics , crack growth behaviour , and fatigue life prediction methodologies. Familiarity with aerospace materials, especially metallic alloys used in aircraft structures. Experience working in a regulated environment with exposure to FAA/EASA certification processes . Strong analytical, problem-solving, and documentation skills. Excellent communication skills and ability to work collaboratively in a multidisciplinary team. Attention to detail and accuracy in calculations and reporting. Proactive attitude towards continuous improvement and learning. Preferred: Experience in aircraft structural analysis . Knowledge of residual strength , multiple-site damage (MSD) , or widespread fatigue damage (WFD) assessments. Familiarity with probabilistic analysis techniques . Experience with scripting or automation (e.g., Python, VBA).

Perform fatigue and damage tolerance analysis of metallic and composite structures in accordance with regulatory and OEM standards (e.g., FAA, EASA). Utilize tools like NASGRO , DARWIN , or other proprietary applications for crack growth and fracture mechanics analysis. Conduct life prediction assessments under static and dynamic loading conditions, including variable amplitude loading. Support aircraft certification programs by providing substantiation reports and analysis documentation. Work closely with design, stress, materials, and manufacturing teams to define inspection intervals and structural integrity requirements. Interpret test data and validate analytical models against physical test results. Develop and review fatigue test plans and evaluate test outcomes. Document assumptions, methodologies, and results in clear, traceable technical reports. Bachelor’s or Master’s degree in Mechanical, Aerospace, or Structural Engineering. 7 to 15 years of experience in fatigue and damage tolerance analysis. Hands-on experience with at least one of the following tools: NASGRO , DARWIN , or equivalent. Experience on Stress Concentration evaluation fro Joints and Notches Solid understanding of fracture mechanics , crack growth behavior , and fatigue life prediction methodologies. Ability to use FE tools like HM and Patran for Extraction of Loads/stress for FDT analysis. Familiarity with aerospace materials, especially metallic alloys used in aircraft structures. Experience working in a regulated environment with exposure to FAA/EASA certification processes . Strong analytical, problem-solving, and documentation skills. Excellent communication skills and ability to work collaboratively in a multidisciplinary team.

Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Fatigue & Damage Tolerance F&DT Good to have skills : NAMinimum 5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As an Engineering Services Practitioner, you will assist with end-to-end engineering services to develop technical engineering solutions, solve problems, and achieve business objectives. You will work across structural and stress design, qualification, configuration, and technical management. Roles & Responsibilities:- Expected to be an SME.- Collaborate and manage the team to perform.- Responsible for team decisions.- Engage with multiple teams and contribute on key decisions.- Provide solutions to problems for their immediate team and across multiple teams.- Lead technical discussions and provide guidance to team members.- Develop innovative engineering solutions to address complex challenges.- Conduct regular reviews and assessments to ensure project success. Professional & Technical Skills: - Must To Have Skills: Proficiency in Fatigue & Damage Tolerance F&DT.- Strong understanding of structural and stress analysis.- Experience in technical management and configuration control.- Knowledge of scientific and socio-economic principles in engineering.- Hands-on experience in developing engineering solutions.- Good To Have Skills: Experience with Finite Element Analysis (FEA). Additional Information:- The candidate should have a minimum of 5 years of experience in Fatigue & Damage Tolerance F&DT.- This position is based at our Bengaluru office.- A 15 years full-time education is required. Qualification 15 years full time education

Role & responsibilities : Extraction of material data, geometry details and fastener specifications from part and assembly drawings. Extraction of loads, stresses from GFEM. Generate detailed finite element models Static stress analysis of primary and secondary Aircraft structural components Sizing of primary and secondary structural parts for static, fatigue & DT requirements Mitigation techniques for low margins of safety Preparation of stress certification reports Preferred candidate profile: Candidate should have good working experience on Static, Fatigue & Damage tolerance analysis of Aircraft structural components. Should have good working experience on plant engineering concessions of Aircraft structural (Primary and Secondary) components. Profound knowledge on Stress analysis, aircraft loads and aircraft structures are expected. Should be aware of certification requirements and should have experience with static & fatigue stress certification reports. Candidate should be able to co-ordinate with design and stress teams. Sound knowledge of structural design principles, aircraft loads and aircraft structures are expected Must have experience in static analysis & sizing of Aircraft structural components for metallic and composites Must have experience in the preparation of stress certification reports Working experience in concessions Must have experience in the preparation of stress reports. Having experience in Fatigue & damage tolerance analysis is an added advantage

Role & responsibilities: Identification of PSE ( Principal Structural Elements ) Calculate Stress Concentration Factor. Wide Spread Fatigue Damage Factor, effect in fatigue due to Size, Material, joints, Machining quality, technology process, etc. Fatigue Index Calculation Fatigue Equivalent Stress Calculation and extraction of Reference Stresses Fatigue Spectrum Analysis for various mission and Damage Stimulation Analysis Fatigue Life Estimation and Damage Tolerance Analysis Damage Tolerance Analysis for SLP (Single Load Path), MLP (Multiple Load Path), and DCF (Damage Contaminant Feature) structures Initial Crack definition and determination of Critical Crack Length for Airworthiness Limitation Item, Threshold and Inspection Interval Low Life Mitigation, various low life mitigation techniques based on OEM based process Preparation of Fatigue and Damage Tolerance Analysis Documentation like ACD/ACS, SCNs and Stress Dossiers Candidate Should have good hand-on work experience in Fatigue and Damage Tolerance Analysis of Airframe Structural Analysis Candidate should have in depth knowledge of Fatigue Design Philosophies Knowledge and experience in Structural Failure and Fatigue Failure Characteristics Aware of various types of fatigue, Fatigue assessment Principles and Methods Calculate Fatigue Life (High Cycle Fatigue, Low Cycle Fatigue and Very High Cycle Fatigue) Fatigue Analysis of Metallic and Fastener parts. Composite Fatigue Analysis experience Candidate should have experience in Damage Tolerance Analysis and Crack Propagation Analysis of Airframe Structures Preferred candidate profile: Must have Knowledge of Fatigue Design Guidelines, Principles and Methods Fatigue Life Calculation Crack Propagation Analysis / Damage Tolerance Analysis Aware of DT calculation in several different stages like corner crack , through crack, etc. Fatigue Criteria for Crack Propagation Analysis to determine the critical crack length Awareness and knowledge about the Inspection Techniques for Crack Propagation Analysis Detectable Crack Length Determination Tools: NASGRO, MSC NASTRAN, PATRAN, HyperMESH. OEM Specific Fatigue Tools Basic Knowledge on CATIA V5

At Boeing, we innovate and collaborate to make the world a better place. We’re committed to fostering an environment for every teammate that’s welcoming, respectful and inclusive, with great opportunity for professional growth. Find your future with us. Overview As a leading global aerospace company, Boeing develops, manufactures and services commercial airplanes, defense products and space systems for customers in more than 150 countries. As a top U.S. exporter, the company leverages the talents of a global supplier base to advance economic opportunity, sustainability and community impact. Boeing’s team is committed to innovating for the future, leading with sustainability, and cultivating a culture based on the company’s core values of safety, quality and integrity. Technology for today and tomorrow The Boeing India Engineering & Technology Center (BIETC) is a 5500+ engineering workforce that contributes to global aerospace growth. Our engineers deliver cutting-edge R&D, innovation, and high-quality engineering work in global markets, and leverage new-age technologies such as AI/ML, IIoT, Cloud, Model-Based Engineering, and Additive Manufacturing, shaping the future of aerospace. People-driven culture At Boeing, we believe creativity and innovation thrives when every employee is trusted, empowered, and has the flexibility to choose, grow, learn, and explore. We offer variable arrangements depending upon business and customer needs, and professional pursuits that offer greater flexibility in the way our people work. We also believe that collaboration, frequent team engagements, and face-to-face meetings bring together different perspectives and thoughts – enabling every voice to be heard and every perspective to be respected. No matter where or how our teammates work, we are committed to positively shaping people’s careers and being thoughtful about employee wellbeing. Position Overview Boeing India Engineering is currently looking for Lead Structural Analysis Engineer ( Service Engineering ) to support Airframe Service Engineering Capability at Boeing India, Bangalore. This position will focus on providing 24/7 support to Boeing commercial airplane customers. This position offers a unique opportunity to work complex technical challenges in support of safety operation and return to service. Our team of engineers support over 14,000 aircraft around the globe, and work closely with our customers to ensure that their fleet is operating safely, efficiently, and reliably. Join us today and help shape the future of commercial aviation. Position Responsibilities Primary responsibilities for this position include: Responsible for performing structural analysis of aircraft components, assemblies, and systems while working as an integrated team Responsible to collaborate with Service Engineers to perform root cause analysis and corrective actions on In-Service issues for Airframe and other Mechanical systems. Performs detailed structural analysis (static strength, durability/fatigue and damage tolerance) to determine structural integrity (margins of safety), using classical techniques and Boeing tools. Evaluate structural integrity of aircraft components by way of classical hand calculations and, finite element method Generate documentation to report analysis and test results to support certification/Qualification Support Gated Reviews to validate the quality and completeness of work packages Familiar with regulatory framework (FAA and Mil-Spec), for warranting safety and regulatory compliance. Guides structural design and configuration development. Supports in-service products by investigating failures and analyzing improvements Performs trade studies to optimize structure and meet program requirements. Researches and prepares data to support definition of structural design requirements. Willing to support a 24/7 on-call rotation schedule and the ability to work variable shifts, including weekends or overtime. Basic Qualifications (Required Skills/Experience) Bachelor’s degree in Mechanical/Aerospace/Applied Mechanics/Structural engineering and 12+ years of experience in stress analysisin Services related to Fleet Support. Preferred Qualifications (Desired Skills/Experience) Experience in structural analysis of various airframe structures Experience of Aircraft maintenance and service procedures Experience with structural analysis of metallic and composite structures (good experience with composite structures) Experience with static, fatigue and damage tolerance analysis Knowledge of airplane operating environments Robust understanding of engineering fundamentals such as material properties, Free-body diagrams, structural loads and analysis methods Experience in utilizing FEM software (e.g., ABAQUS, PATRAN/NASTRAN, Hyperworks) Experience or training with computer programming languages (e.g., Matlab, Python, Visual Basic) Experience in utilizing industry CAD systems (e.g., NX/Teamcenter and CATIA/ENOVIA) Candidate demonstrates excellent analytical and problem-solving skills Good verbal and written communication skills to liaise with several Stakeholders Ability to work across functional teams and organizations Willingness to expand into technical areas without prior experience Desire to continuously improve our airplanes Typical Education & Experience Education/experience typically acquired through advanced education (e.g. Bachelor) and typically 12+ years' related work experience or an equivalent combination of education and experience (e.g. Masters+11 years' related work experience etc.) Relocation This position does offer relocation based on candidate eligibility within INDIA. Applications for this position will be accepted until Jun. 06, 2025 Export Control This is not an Export Control position. Education Bachelor's Degree or Equivalent Required Relocation This position offers relocation based on candidate eligibility. Visa Sponsorship Employer will not sponsor applicants for employment visa status. Shift Not a Shift Worker (India) Equal Opportunity Employer: We have teams in more than 65 countries, and each person plays a role in helping us become one of the world’s most innovative, diverse and inclusive companies. We are proud members of the Valuable 500 and welcome applications from candidates with disabilities. Applicants are encouraged to share with our recruitment team any accommodations required during the recruitment process. Accommodations may include but are not limited toconducting interviews in accessible locations that accommodate mobility needs, encouraging candidates to bring and use any existing assistive technology such as screen readers and offering flexible interview formats such as virtual or phone interviews.

Role & responsibilities 1.F&DT Engineer Good Understanding of Various OEM F&DT Method and Tools Experience in F&DT Analysis for Aero structural components and Dossier write up 2. Stress Engineer- Static Stress Justification of Airframes using classical Method Good Hands-on experience in Hypermesh, NASTRAN Experience in dossier checking and write up Email id: basavanagowda.gowder@quest-global.com Experience: 2 to 6 Years Location: Bangalore Interview Date :24 May 2025 Timing : 9.00 AM Contact Person name : Basavaraj 9071717179 Venue Addresss Quest Global Engineering Services Private Limited PRIMROSE 7B, Embassy Tech Village, Sarjapura Marathahalli Outer Ring Road, Devarabeesanahalli, Bengaluru 560103, India Note: Pls ignore if you're not working above skills.