11 Isami 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

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

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

• Own GFEM updates, FEM validation, and DMU optimization. • Define mesh strategies for complex stress/F&DT analyses. • Lead load extraction, hand calcs, and crack growth assessments. • Conduct fatigue life predictions (rainflow/Miner) and damage tolerance evaluations. • Validate composite/metallic material performance in ISAMI. • Manage complex static and fatigue analysis, including crack growth and DTA for metallic and composite structures. • Ensure compliance with Airbus structural analysis methods and tools. • Develop Excel VBA tools for process automation. • Drive and ensure Airframe certification requirements and resolve critical structural issues. • Guide junior engineers and review analysis reports. • Review technical reports, Liaise with Technical committee for design verification and changes. • conduct technical audits, and support management decisions. Qualifications: • Masters in Aerospace/Mechanical Engineering (PhD a plus). • 9+ years in airframe stress/F&DT (fuselage sub-assemblies: frames, panels, junctions). • Expert in Airbus methods, ISAMI, HyperWorks, Nastran/Patran. • Deep knowledge of composite/metallic fatigue and crack growth. • Advanced Excel/VBA/Python for analytical automation. • Good Communication skills

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

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

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