21 Patran Jobs

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 : Aircraft Structural Analysis Good to have skills : NAMinimum 3 year(s) of experience is required Educational Qualification : 15 years full time education Summary :We are seeking an experienced Aircraft Structures Engineer to join our dynamic aerospace engineering team. The successful candidate will be responsible for the analysis, evaluation, and optimization of aircraft structural components, ensuring compliance with industry standards, safety regulations, and performance specifications. The role involves utilizing advanced engineering software and analytical methods to conduct structural analysis and stress evaluations. A strong background in aerospace structural engineering is essential, including extensive knowledge of materials, structural mechanics, and finite element analysis (FEA) tools. The ideal candidate will possess, Excellent problem-solving skills, Strong attention to detail and strong ability to manage multiple projects simultaneously Roles & Responsibilities:Serve as team lead (45 members) for structural analysis and stress evaluationsTechnical customer liaison; deliver training and guide teamPerform analysis using HyperWorks, ISAMI, Nastran/PatranPrepare and review stress certification dossiersCreate, validate, and integrate GFEM/DFEM modelsA350/A350F experience with OEM tools/methods preferred Professional & Technical Skills: Proficient in primary and secondary structural analysis for A320SA, A350, and A350F programs.Experienced in stress analysis of metallic and composite aircraft structures using ISAMI (CFH, MFH, CFA/MFA, MSP, CSPS, DT TI, DT EI, Unfolding, Crippling Junctions and Joints) as well as classical hand calculations.Extensive hands-on experience with HyperWorks, ISAMI, and Nastran/Patran for structural analysis and simulation.Proficient in the creation, validation, and condensation of GFEM/DFEM models.Adept at technical communication and coordination with customers, ensuring alignment with engineering requirements.Experienced in mentoring and technically guiding team members, including delivering training sessions.Competent in the preparation and peer-review of stress certification dossiers in compliance with regulatory and customer requirements.Additional skills include programming with VBA/Python and proficiency in CATIA, enhancing automation and CAD integration capabilities.Strong ability to perform and accurately interpret both automated and manual stress calculations.Demonstrated understanding of static compliance with customer and airworthiness authority requirements.Proficient in metallic/composite structure stress analysisExpertise in specific tools/methodologies for the OEMStrong manual/automated stress calculation and airworthiness complianceEffective communication, mentoring, and leadershipProgramming (VBA/Python) and CATIA knowledge is advantageous Additional Information:5-8 years' aerostructure stress analysis experience15 years full-time educationBased in Bengaluru Qualification 15 years full time education

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 : Aircraft Structural Analysis Good to have skills : NAMinimum 2 year(s) of experience is required Educational Qualification : 15 years full time education Summary :We are seeking an experienced Aircraft Structures Engineer to join our dynamic aerospace engineering team. The successful candidate will be responsible for the analysis, evaluation, and optimization of aircraft structural components, ensuring compliance with industry standards, safety regulations, and performance specifications.The role involves utilizing advanced engineering software and analytical methods to conduct structural analysis and stress evaluations. A strong background in aerospace structural engineering is essential, including extensive knowledge of materials, structural mechanics, and finite element analysis (FEA) tools. The ideal candidate will possess, Excellent problem-solving skills, Strong attention to detail and strong ability to manage multiple projects simultaneously Roles & Responsibilities:Serve as key team member for structural analysis and stress evaluationsIndependent technical; deliveries, training and guide teamPerform analysis using HyperWorks, ISAMI, Nastran/PatranPrepare and review stress certification dossiersCreate, validate, and integrate GFEM/DFEM modelsA350/A350F experience with OEM tools/methods preferred Professional & Technical Skills: Proficient in primary and secondary structural analysis for A320SA, A350, and A350F programs.Experienced in stress analysis of metallic and composite aircraft structures using ISAMI (CFH, MFH, CFA/MFA, MSP, CSPS, DT TI, DT EI, Unfolding, Crippling Junctions and Joints) as well as classical hand calculations.Extensive hands-on experience with HyperWorks, ISAMI, and Nastran/Patran for structural analysis and simulation.Proficient in the creation, validation, and condensation of GFEM/DFEM models.Adept at technical communication and coordination with customers, ensuring alignment with engineering requirements.Experienced in mentoring and technically guiding team members, including delivering training sessions.Competent in the preparation and peer-review of stress certification dossiers in compliance with regulatory and customer requirements.Additional skills include programming with VBA/Python and proficiency in CATIA, enhancing automation and CAD integration capabilities.Strong ability to perform and accurately interpret both automated and manual stress calculations.Demonstrated understanding of static compliance with customer and airworthiness authority requirements.Proficient in metallic/composite structure stress analysisExpertise in specific tools/methodologiesStrong manual/automated stress calculation and airworthiness complianceEffective communication, mentoring, and leadershipProgramming (VBA/Python) and CATIA knowledge is advantageous Additional Information:2-5 years' aerostructure stress analysis experience15 years full-time educationBased in Bengaluru Qualification 15 years full time education

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 : Aircraft Structural Analysis Good to have skills : NAMinimum 5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :We are seeking an experienced Aircraft Structures Engineer to join our dynamic aerospace engineering team. The successful candidate will be responsible for the analysis, evaluation, and optimization of aircraft structural components, ensuring compliance with industry standards, safety regulations, and performance specifications. The role involves utilizing advanced engineering software and analytical methods to conduct structural analysis and stress evaluations. A strong background in aerospace structural engineering is essential, including extensive knowledge of materials, structural mechanics, and finite element analysis (FEA) tools. The ideal candidate will possess, Excellent problem-solving skills, Strong attention to detail and strong ability to manage multiple projects simultaneously Roles & Responsibilities:Serve as SME and team lead (1015 members) for structural analysis and stress evaluationsTechnical customer liaison; deliver training and guide teamPerform analysis using HyperWorks, ISAMI, Nastran/PatranPrepare and review stress certification dossiersCreate, validate, and integrate GFEM/DFEM modelsA350/A350F experience with OEM tools/methods preferred Professional & Technical Skills: Proficient in primary and secondary structural analysis for A320SA, A350, and A350F programs, with strong expertise in OEM-specific tools and methodologies.Experienced in stress analysis of metallic and composite aircraft structures using ISAMI (CFH, MFH, CFA/MFA, MSP, CSPS, DT TI, DT EI, Unfolding, Crippling Junctions and Joints) as well as classical hand calculations.Skilled in leading and managing teams of 1015 engineers, ensuring project milestones and quality standards are met.Extensive hands-on experience with HyperWorks, ISAMI, and Nastran/Patran for structural analysis and simulation.Proficient in the creation, validation, and condensation of GFEM/DFEM models.Adept at technical communication and coordination with customers, ensuring alignment with engineering requirements.Experienced in mentoring and technically guiding team members, including delivering training sessions.Competent in the preparation and peer-review of stress certification dossiers in compliance with regulatory and customer requirements.Additional skills include programming with VBA/Python and proficiency in CATIA, enhancing automation and CAD integration capabilities.Strong ability to perform and accurately interpret both automated and manual stress calculations.Demonstrated understanding of static compliance with customer and airworthiness authority requirements.Proficient in metallic/composite structure stress analysisStrong manual/automated stress calculation and airworthiness complianceEffective communication, mentoring, and leadershipProgramming (VBA/Python) and CATIA knowledge is advantageous Additional Information:8+ years' aerostructure stress analysis experience15 years full-time educationBased in Bengaluru Qualification 15 years full time education

Job Description (Meshing): Role: • Understanding the client’s design and analysis requirements. • Giving estimates to the designer/client. • Meshing the models in Hypermesh and setting decks for Optistruct. Required Skills: • The candidate should have 3 – 5 years of hands on experience on Hypermesh. • Should have worked on Heavy equipment structural domain. • The candidate should be in a position to work independently with minimum guidance from the team lead. • Giving estimates to the designer/client. Desired Skills: • Good written and oral communication skills. • Experience in Rail Transportation /Aerospace/Automotive/Heavy Engineering. Experience in analysis by using Optistruct solver. Education Qualification: B.E/B.Tech., in Mechanical Engineering with atleast 60% of marks.

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

Dear Candidate: Greetings from Metrics Numero Talent Acquisition Team!!! MetricsNumero was founded with the goal of creating a centre of excellence that provides high-quality services in Aerospace , Mechanical, SAP, Microsoft, AI/ML, EDW-BI & Data Analytics, Cloud services Mechanical Engineering & Design, ERP and Banking solutions to a wide range of industries globally. Our driving force is to provide innovative solutions to complex business problems. We are specialized in Software Advisory & Consultation. We are a growing and dynamic MNC having head office in Kolkata, India with branch offices in Bengaluru, Kolkata and international offices in Chicago (USA) and Toronto (Canada). We are serving and delivering IT solutions to customers in India and worldwide. Experience: 8+ Yrs Location: Bangalore Job Description: Good experience in Stress Analysis experience in Aerospace Domain. Should have good experience in Aerostructure Analysis Able to analyse stress (Static and Fatigue) and perform hand calculation Experience with FEM tool (Hyperworks /Nastran /Patran) Good technical leadership and delivery management skill Preferred Experience : Experience in DTA (Damage Tolerance Analysis)

Role & responsibilities This position is responsible for supporting Lead Engineers and/or senior level Engineers in the structural substantiation of the mechanical / payloads / systems and structures design within the Technical Services Engineering departments utilizing established modeling and analysis standards (such as Bruhn, Niu, BDM, JA Stress Manuals, etc.). The Stress Engineer will support design and structural substantiation of aircraft engineering packages based on customer and OEM requirements for production, retrofit applications and product development. Work independently and/or under the direction of an experienced engineer, review/analyze basic mechanical/structural/payloads/systems based on defined requirements using approved processes and tools, with knowledge and hands-on experiences in Aircraft monument: FEM, interface load report, substantiation plan, stress analysis, partial static test plan and report, full scale static test plan and report, wind milling analysis Aircraft seating system: FEM, stress analysis, interface load report, dynamic test plan and report, static test plan and report, dynamic simulations Airframe: airframe (fuselage) stress analysis, aircraft fatigue and damage tolerances, Materials: Allowable test plan and report, metallic and composite material properties, material and process specification Regulation and Certification: FAR, CS, SAE, TSO, ACs +Assigned tasks include but not limited to: assemblies/components structural review/analysis, mechanical/structural/payloads/ systems installations review/analysis, specifications review (such as materials specifications and manufacturing process specifications), basic test plans/reports (such as tie-rods tension/compression testing) and associated testing support as needed. Participates in teams to support the development of designs. Supports the documentation of design implementation. Perform engineering design reviews and sign drawings and/or documents. Obtain, interpret, and analyze OEM airplane install drawings using approved processes and tools. Provides technical, design and informational support for airplane modifications (including full-time on-site modification support and on-call home-team support), manufacturing support and/or in-service issues. Troubleshoots basic mechanical/structural/payloads/systems problems associated with structural requirements. Actively support engineering department goals and initiatives. Coordinate with other departments as necessary. Utilize internal analysis/drawing/document standards per customer or regulatory agency requirements. Fast produce error-free engineering documents per engineering document standard. Preferred candidate profile Education and/or Experience Degree in Mechanical Engineering, Aerospace Engineering or related Engineering field and 3-8 years of relevant working experience. Knowledge and Skills: Design: Able to read and understand Computer Aided Design (CAD) designs, drawings and specifications. Knowledge of design techniques, tools and principles involved in production of precision technical plans, drawings, and models. Tools: Proficient in CAE/CAD modeling tools used by the department (such as Catia, AutoCAD, Patran/Nastran, Femap/Nastran). Administration: Knowledge of business and management principles involved in strategic planning, equipment allocation/management, basic leadership techniques and coordination of people and resources. Able to work in a team environment and accept required roles, responsibilities and accountability. Aircraft Fundamental Knowledge: basic knowledge of FAA requirements for the installation and structural substantiation of mechanical/structural/payloads/systems components (14 CFR Part 25, MMPDS, etc.) and OEM Design requirements (Boeing Design Manual, Standard Interface Documents, etc.) is required. Basic understanding of aircraft terms, design and structural analysis requirements is desirable. Engineering: Knowledge of the practical application of engineering science and technology. This includes applying principles, techniques, procedures, and equipment to the design review and structural analysis of various systems, goods and services. Skills Problem Solving: Identifying complex problems and reviewing related information to develop and evaluate options and implement solutions. Critical Thinking: Using logic and reasoning to identify the strengths and weaknesses of alternative solutions, conclusions or approaches to problems. Using scientific rules and methods to solve problems is required. Mathematical: College level mathematics required. Ability to use various formulas embedded and linkage amongst cells in spreadsheet program. Basic statistics required to be able to examine/reduce data and identify results/trends. Finite Elements Method (FEM) mathematics understanding. Customer Orientation: Must demonstrate concern and take actions to meet requirements and high standards of quality of both internal and external customers. Must display courtesy and sensitivity. Manage difficult situations. Meet commitments. Respond promptly to customer needs. Solicit customer feedback to improve service. Communication: Giving full attention to what other people are saying, taking time to understand the points being made, asking questions as appropriate and not interrupting at inappropriate times. Communicating effectively in writing as appropriate for the needs of the audience. Talking to others to convey information effectively. Good oral and written communication skills. Language: Ability to read, analyze, and interpret general business periodicals, procedures, drawings, technical data, engineering documentations, and governmental regulations. Ability to write engineering documentations and formal business correspondence. For situations concerning Japanese customer assignments, Japanese language skills may also be required. Judgment and Decision Making: Considering the relative costs and benefits of potential actions to choose the most appropriate one. Time Management : Managing one's own time. Able to multitask and work independently. Attitude: Demonstrate continuous skill improvement. Positive attitude is required. Other General Requirements: High attention to detail. Able to work in a team environment and accept required roles, responsibilities, and accountability. Able to multitask and work independently. Working knowledge of Windows based computers, particularly MS Office products (Word, Excel Access & PowerPoint). Demonstrate continuous skill improvement. Language Skill: Ability to read and interpret documents such a safety rules, operating and maintenance instructions and procedure manuals. Ability to write routine reports and correspondence. Ability to speak effectively before groups of customers of employees of organization. Reasoning Ability: Ability to apply common sense understanding to carry out instructions furnished in written, oral, or diagram form. Ability to deal with problems involving several concrete variables in standardized situations. Customer Orientation: Must demonstrate concern and take actions to meet requirements and high standards of quality of both internal and external customers. Must display courtesy and sensitivity. Manage difficult situations. Meet commitments. Respond promptly to customer needs. Solicit customer feedback to improve service.

About The Role 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 : Aircraft Structural Analysis Good to have skills : NAMinimum 3 year(s) of experience is required Educational Qualification : 15 years full time education Summary :We are seeking an experienced Aircraft Structures Engineer to join our dynamic aerospace engineering team. The successful candidate will be responsible for the analysis, evaluation, and optimization of aircraft structural components, ensuring compliance with industry standards, safety regulations, and performance specifications.The role involves utilizing advanced engineering software and analytical methods to conduct structural analysis and stress evaluations. A strong background in aerospace structural engineering is essential, including extensive knowledge of materials, structural mechanics, and finite element analysis (FEA) tools. Roles & Responsibilities:-Expected to be an SME, collaborate and manage the team to perform.-Capable of handling the customer technically.-Technical Training and guiding the team.-Handling the team of min 10 to 15 members.-Highly preferred A350/A350F primary and secondary structure experience with good knowledge of Excellent problem-solving skillsStrong attention to detailThe ability to manage multiple projects simultaneously-Good Experience in Hyperworks, ISAMI and Nastran/Patran-Experience in GFEM/DFEM creation, validation, and condensation-Preparation/Checking of Stress Certification Dossiers.-Having VBA/Python programming, Catia is an added advantage. Professional & Technical Skills: Proficient in primary and secondary structural analysis for A320SA, A350, and A350F programs, with strong expertise in Airbus-specific tools and methodologies.Experienced in stress analysis of metallic and composite aircraft structures using ISAMI (CFH, MFH, CFA/MFA, MSP, CSPS, DT TI, DT EI, Unfolding, Junctions and Joints) as well as classical hand calculations.Skilled in leading and managing teams of 1015 engineers, ensuring project milestones and quality standards are met.Extensive hands-on experience with HyperWorks, ISAMI, and Nastran/Patran for structural analysis and simulation.Proficient in the creation, validation, and condensation of GFEM/DFEM models.Adept at technical communication and coordination with customers, ensuring alignment with engineering requirements.Experienced in mentoring and technically guiding team members, including delivering training sessions.Competent in the preparation and peer-review of stress certification dossiers in compliance with regulatory and customer requirements.Additional skills include programming with VBA/Python and proficiency in CATIA, enhancing automation and CAD integration capabilities.Strong ability to perform and accurately interpret both automated and manual stress calculations.Demonstrated understanding of static compliance with customer and airworthiness authority requirements. Additional Information:- The candidate should have a minimum of 8 years of experience in Aerostructure stress analysis.- This position is based at our Bengaluru office.- A 15 years full time education is required. Qualification 15 years full time education

About The Role 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 : Aircraft Structural Analysis Good to have skills : NAMinimum 5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :We are seeking an experienced Aircraft Structures Engineer to join our dynamic aerospace engineering team. The successful candidate will be responsible for the analysis, evaluation, and optimization of aircraft structural components, ensuring compliance with industry standards, safety regulations, and performance specifications.The role involves utilizing advanced engineering software and analytical methods to conduct structural analysis and stress evaluations. A strong background in aerospace structural engineering is essential, including extensive knowledge of materials, structural mechanics, and finite element analysis (FEA) tools. Roles & Responsibilities:-Expected to be an SME, collaborate and manage the team to perform.-Capable of handling the customer technically.-Technical Training and guiding the team.-Handling the team of min 10 to 15 members.-Highly preferred A350/A350F primary and secondary structure experience with good knowledge of Excellent problem-solving skillsStrong attention to detailThe ability to manage multiple projects simultaneously-Good Experience in Hyperworks, ISAMI and Nastran/Patran-Experience in GFEM/DFEM creation, validation, and condensation-Preparation/Checking of Stress Certification Dossiers.-Having VBA/Python programming, Catia is an added advantage. Professional & Technical Skills: Proficient in primary and secondary structural analysis for A320SA, A350, and A350F programs, with strong expertise in Airbus-specific tools and methodologies.Experienced in stress analysis of metallic and composite aircraft structures using ISAMI (CFH, MFH, CFA/MFA, MSP, CSPS, DT TI, DT EI, Unfolding, Junctions and Joints) as well as classical hand calculations.Skilled in leading and managing teams of 1015 engineers, ensuring project milestones and quality standards are met.Extensive hands-on experience with HyperWorks, ISAMI, and Nastran/Patran for structural analysis and simulation.Proficient in the creation, validation, and condensation of GFEM/DFEM models.Adept at technical communication and coordination with customers, ensuring alignment with engineering requirements.Experienced in mentoring and technically guiding team members, including delivering training sessions.Competent in the preparation and peer-review of stress certification dossiers in compliance with regulatory and customer requirements.Additional skills include programming with VBA/Python and proficiency in CATIA, enhancing automation and CAD integration capabilities.Strong ability to perform and accurately interpret both automated and manual stress calculations.Demonstrated understanding of static compliance with customer and airworthiness authority requirements. Additional Information:- The candidate should have a minimum of 8 years of experience in Aerostructure stress analysis.- This position is based at our Bengaluru office.- A 15 years full time education is required. Qualification 15 years full time education

Perform detailed static analysis using classical Hand calcualtion, on aerostructures, including wings, fuselage, landing gear, Floor beam, Doors and other aircraft components. Utilize Finite Element Analysis (FEA) software, such as HYPERMESH, NASTRAN, PATRAN to model and analyze structural performance under various loading conditions. Ensure compliance with aerospace industry standards, including FAA, EASA, and military regulations, and participate in design reviews. Experience on Airbus and Boeing Aircraft structures is an added advantage. Develop and validate analytical methods using excel and Macros techniques to predict the behavior of structural components. Work closely with design engineers to provide input on material selection, design changes, and manufacturing processes to optimize structural performance and minimize weight while maintaining safety. Lead technical reports and documentation to communicate analysis results, design recommendations, and compliance to regulatory bodies and customers. Preparing the certification standard report with detailed explanations of procedures followed for analyzing a structure to support PDR and CDR. Include all the mitigations and summarize Reserve factor in the report Mentor and provide guidance to junior engineers and analysts. Collaborate with cross-functional teams (materials, design, systems, etc.) to ensure integrated, efficient, and safe structural designs. Identify and address structural performance risks, and provide solutions to improve the overall reliability and performance of aerostructures. Participate in customer-facing discussions and presentations related to structural design and analysis. Conduct optimization studies to enhance structural efficiency, reduce weight, and improve manufacturability of fuselage components. Explore design alternatives to achieve optimal performance Bachelor's, Master's, in Aerospace Engineering, Mechanical Engineering, or a related field. 10+ years of experience in stress analysis and design of aerostructures, preferably in the aerospace industry. In-depth knowledge of structural analysis methods, including finite element modeling (FEM), classical hand calculations, and failure theories. Proficient in FEA tools such as NASTRAN/PATRAN/HM similar software. Strong understanding of aerospace materials, including composites, metals, and advanced alloys. Familiarity with aircraft systems and the integration of structures with other aircraft systems. Solid understanding of aerospace loads and regulatory standards and certifications (e.g., FAA, EASA). Strong problem-solving skills, attention to detail, and ability to manage multiple projects simultaneously. Excellent written and verbal communication skills, including technical report writing and presentations. Ability to work in a fast-paced, multidisciplinary team environment.

Key Responsibilities: Perform high-quality mesh generation for structural analysis using Hypermesh and Patran . Develop and refine GFEM and DFEM models for various components and assemblies, ensuring mesh quality and compliance with CAE standards. Prepare models for static, dynamic, and thermal FEA simulations. Interpret and apply engineering drawings and CAD data to build accurate finite element models. Ensure mesh quality and convergence to meet analysis requirements. Ensure adherence to customer-specific FEM guidelines and industry best practices. Collaborate closely with design, simulation, and test teams to validate and iterate FE models. Document meshing processes, model assumptions, and preprocessing methodologies. Troubleshoot and resolve issues related to meshing and model setup. Familiarity with optimization techniques for FE modeling. Required Skills & Qualifications: Bachelor's or Master's degree in Mechanical, Aerospace, or related engineering field. 3 to 7 years of relevant CAE experience , with a focus on meshing and preprocessing. Strong command of Hypermesh and Patran for shell and solid meshing. Hands-on experience in GFEM and DFEM meshing techniques and standards. Solid understanding of FEA fundamentals, material properties, and boundary conditions. Familiarity with CAD software (e.g., CATIA, NX) for model extraction and cleanup. Excellent problem-solving and communication skills. Ability to manage multiple tasks and meet tight deadlines. Proactive attitude towards continuous improvement and learning. Preferred: Exposure to solver environments like OPTISTRUCT , NASTRAN , ABAQUS for FE model set-up Experience with scripting or automation (e.g., TCL, Python) in preprocessing. Knowledge of aerospace or automotive domain-specific CAE workflows.

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).

Bachelor's or Master's degree in Mechanical, Aerospace, or related engineering field. 7 to 15 years of relevant CAE experience , with a focus on meshing and preprocessing. Strong command of Hypermesh and Nastran/ Patran for shell and solid meshing. Hands-on experience in GFEM and DFEM meshing techniques and standards. Perform Strcutural Analysis Hand calculation for static stress checks like Buckling, crippling, Lug analysis, fastener check using classical methods Solid understanding of FEA fundamentals, material properties, and boundary conditions. Familiarity with CAD software (e.g., CATIA, NX) for model extraction and cleanup. Excellent problem-solving and communication skills. Ability to manage multiple tasks and meet tight deadlines.

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 : Aircraft Structural Analysis Good to have skills : Airbus Configuration ToolsMinimum 2 year(s) of experience is required Educational Qualification : 15 years full time education Summary :We are seeking a skilled and detail-oriented Stress Engineer to support the structural analysis of aircraft wing components. The role involves performing static and fatigue & damage tolerance (F&DT) analyses to support in-service structural repairs on aircraft wings. Roles & Responsibilities:Perform detailed static stress analysis of wing structures to support repair solutions for in-service damage.Conduct fatigue and damage tolerance (F&DT) analysis in line with EASA requirements to assess the continued airworthiness of repairs.Develop and validate analytical models (hand calculations, FEM) for primary and secondary structural components.Provide technical substantiation reports and stress dossiers to support repair design and regulatory approval.Collaborate with design engineers to ensure repair feasibility, manufacturability, and certification compliance.Use OEM tools, methods, and allowable (preferably Airbus) for substantiation.Participate in peer reviews, design/stress reviews, and sign-off assigned activities. Professional & Technical Skills: Strong knowledge of static strength, fatigue life estimation, and fracture mechanics.Proficiency in industry-standard tools such as ISAMI, Mathcad, PATRAN.Proficient in engineering documentation systems relevant to Repair.(Tech Request, ICARUS, Airbus World)Familiarity with EASA regulations, structural repair manuals (SRMs), and OEM guidelines (preferably Airbus)Strong problem-solving abilities and an analytical mindset.Good communication and stakeholder management skills.Prior experience in MRO or airline engineering support roles in Repairs will be desirable.Previous experience with Airbus wing structure analysis tools and standards will be desirable. Additional Information:- The candidate should have a minimum of 2 to 8 years of experience in aircraft structures design or repair, preferably with a focus on wings.- This position is based at our Bengaluru office.- A 15 years full-time education is required. Qualification 15 years full time education

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

Support the DIC by accomplishing efficient On time Delivery of design release, First time right, and Continual Improvement on skill in Design for Composite parts. Responsibilities Accountabilities Support the DIC by accomplishing efficient On time Delivery of design release, First time right, and Continual Improvement on skill in Design and Analysis. Support the DIC In manging the budget for Engineering department and ensuring that resources are used efficiently. Suggest innovative ideas to reduce cost and improve productivity and efficiency. Control the rejections so as to save costs and produce outputs that are as per specified quality standards and as per customer requirements. Enable customer satisfaction by driving efficiency in internal processes within the department. Ensure appropriate, suitable actions towards customer complaints, so as to facilitate both customer retention as well as identify methods that helps in preventing such breakdowns from recurring. Stress analysis (Composite Metallic) and to checking the detail as per any OEM standards. To work with various analysis types such as linear statics, nonlinear statics (contact, material and large deformation), dynamics (normal modes and cyclic modal). Working knowledge of PATRAN/NASTRAN is most essential requirement. Familiarity with other FEA software will be an advantage Designing of composite parts through Composite Design (CPD) in Catia. Performing FE Modeling (Shell and Solid), FE Analysis for various structural Components. Good exposure on Material properties and allowable. Experience in Hand calculations. Providing design Suggestion /Modification based on failure. Interpreting and understanding FEA results, post-processing and preparing comprehensive analysis reports. Plan and promote continuous improvements in material, machine utilization and process to improve section individual productivity, and quality of the product. Coordinate with the automation team to identify use cases and drive automation / process improvement initiatives within the Section

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.

Required Domain Expertise (skills): Graduate / Post Graduate Engineer (Aerospace Engineering / Mechanical Engineering). Experience working with Aerospace OEM / Tier / Suppliers on Specific Design activities. Tools : Patran/Nastran, Hypermesh, ISAMI (preferred) Experience: 3 - 10 years Soft skills: Ability to work independently & in a team ( including overseas teams) Ability to communicate effectively (oral, written & presentation) Flexibility & adaptability to changing project scenarios and requirements Key skills: Sound knowledge of structural design principles, aircraft loads and aircraft structures Experience in static, fatigue and damage tolerance analysis of aircraft structural components (Airbus methods and tools would be preferable) Background in design and sizing of aircraft primary structure components and parts Ability to liaise/negotiate with design, stress, EU teams and customer services Certification requirements and experience with stress dossiers Finite element method / finite element analysis (FEM / FEA) Very good analytical and reasoning skills Job Description: Stress analysis of metallic and composite aircraft structures using hand calculations, ISAMI, GFEM and DFEMs Extraction of loads, stresses, generation of spectra and mission files Extraction of material data, geometry details and fastener specifications from part & assembly drawings Application of appropriate static, fatigue and damage tolerance design values from standard references. Creation of FEMs using geometric data from part & assembly drawings Sizing of primary and secondary parts for static and fatigue requirements. Fastener load extraction and joint analysis. RF calculation for different failure modes such as strength, buckling, shear panel failure, damage tolerance etc. Low RF mitigations using classical or numerical methods. Preparation of stress certification dossiers, ACD4 and ACD6

Greetings from Metrics Numero Talent Acquisition Team !!! Metrics Numero and Alpha Numero are group companies , offering top-of-the-line Avionics/Aerospace technology services and Solutions, ERP consulting and SMA/SME services, AI Data and Analytics, Software Consulting, Mechanical Engineering and Design Services, as well as Product Design and Engineering. Experience : 7+ Yrs Location : Bangalore Job Description : Good experience in Stress Analysis experience in Aerospace Domain. Able to analyse stress (Static and Fatigue) and perform hand calculation Experience with FEM tool (Hyperworks /Nastran /Patran) Experience in DTA (Damage Tolerance Analysis) would be preferred Good technical leadership and delivery management skill