16 Isami Jobs

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: Develop finite element models, perform FEA simulations and interpret FEA results Should be Well versed with 1D, 2D meshing and stress report preparation. Hand calculation knowledge through classical approach using strength of materials and free body concepts. Knowledge on Airbus methods and Should be able to create IRAMT Sheets, SDL and Justification reports. Knowledge on VBA Macros is added advantage Technical Skills: SOM-Practitioner FEA-Practitioner Stress reports-Practitioner Tools: MSC Nastran & Patran, Hyper Mesh, Hyper View and Catia, IRAMT Share CV on preetid@hrworksindia.com Regards, Preeti Dahotre 8788148794

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

Job Responsibilities Develop finite element models, perform FEA simulations and interpret FEA results Should be Well versed with 1D, 2D meshing and stress report preparation. Hand calculation knowledge through classical approach using strength of materials and free body concepts. Knowledge on Airbus methods and Should be able to create IRAMT Sheets, SDL and Justification reports. Knowledge on VBA Macros is added advantage Technical Skills Required SOM FEA Stress reports MSC Nastran & Patran, Hyper Mesh, Hyper View and Catia, IRAMT

Minimum 5-15 years experience in aerostructure analysis, with minimum of 3 years of experience in composite analysis. Excellent knowledge of Aircraft Primary and Secondary structureal components. Hands-on experience with relevant tools (ISAMI, NASGRO, MSC Nastran/Patran and Altair Hypermesh). Experience on Simcenter 3D is an advantage. Knowledge on CATIA is desirable Strong experience in Static Strength, Fatigue & Damage Tolerance Analysis of aircraft primary structures A strong theoretical and practical foothold on analyses of metallic and composite structures Domain-wide experience from initial sizing to aftermarket services A well-balanced expertise including a sound understanding of basic structural concepts, hand calculations Knowledge of concessions and MRB

Entity:- Accenture Industry X Practice:- Aero Engineering (Aerostructure) Title:-Engineering Services Senior Analyst - L10 Role:- Stress Analysis Job location:- Bangalore About Industry X:- Industry X combines Accenture's powerful digital capabilities with deep engineering and manufacturing expertise. We use the power of data and digital to help our clients reimagine the products they make, and how they make them. By connecting engineering and manufacturing operations every step of the way - from how products are designed and engineered, sourced and supplied, manufactured, to how they are serviced and renewed, we help them achieve greater productivity, drive growth and meet their sustainability commitments Know more:- www.youtube.com/watch?v=XaLxTEI3atI WHAT'S IN IT FOR YOU? Performs static stress analysis or fatigue and damage tolerance analysis of aircraft structures using a broad range of standard hand, legacy and harmonized methods, responsible for checking various types of aircraft components and assemblies:Door Surround Structures, Side and Lower Shells, Pax and Cargo Floors, Skins, stringers, various clips, fasteners, joints and fittings etc. To support Sizing & Justification phase. What you would do in this role Experience in Sizing and justification of metallic/Composite primary and secondary aircraft structural components. Experience in Door Surround Structures/Side shells/PAX floors. Experience in GFEM/DFEM(2D and3D) creation, validation, and condensation Good knowledge of airframe static stress analysis including analytical calculation methods (HSB/Niu/Bruhn) and finite element-based analysis. Stress analysis of Metallic and Composite Aircraft Structural components using FEM, ISAMI and Hand Calculations. Experience in ISAMI based analysis (CFH, MFH, CFA, CSPS, LUG, DT TI and EI, Notch sensitivity/Open Hole, Unfolding). Experience in Buckling and Modal Analysis. Experience in engineering tools, (ISAMI, Hypermesh, NASTRAN, PATRAN, MS Office). Experience Sizing/Justification of aircraft components by providing the solution to the problem. Good Knowledge on CATIA and experience in reading assembly drawings Strong Technical Report (Stress Dossier) writing skills. Training and Guiding the Juniors to execute the tasks. Stress tasks quality check Qualification Who are we looking for? 5 to 9 years of Aerostructure Stress Analysis Experience Location:Bangalore Education:BE/M.Tech in Mechanical, Aerospace, Aeronautical Engineering or relevant subject Ability to work individually and Guide the team. Supporting continuous improvement initiatives to increase team efficiency. Highly preferred primary and secondary structure experience with good knowledge of tools and methods. Hypermesh, Nastran/Patran, ISAMI Having VBA/Python programming is an added advantage. Accenture is an equal opportunities employer and welcomes applications from all sections of society and does not discriminate on grounds of race, religion or belief, ethnic or national origin, disability, age, citizenship, marital, domestic or civil partnership status, sexual orientation, gender identity, or any other basis as protected by applicable law.

Entity:- Accenture Industry X Practice:- Aero Engineering (Aerostructure) Title:-Engineering Services Senior Analyst - L10 Role:- Stress Analysis Job location:- Bangalore About Industry X:- Industry X combines Accenture's powerful digital capabilities with deep engineering and manufacturing expertise. We use the power of data and digital to help our clients reimagine the products they make, and how they make them. By connecting engineering and manufacturing operations every step of the way - from how products are designed and engineered, sourced and supplied, manufactured, to how they are serviced and renewed, we help them achieve greater productivity, drive growth and meet their sustainability commitments Know more:- www.youtube.com/watch?v=XaLxTEI3atI WHAT'S IN IT FOR YOU? Performs static stress analysis or fatigue and damage tolerance analysis of aircraft structures using a broad range of standard hand, legacy and harmonized methods, responsible for checking various types of aircraft components and assemblies:Door Surround Structures, Side and Lower Shells, Pax and Cargo Floors, Skins, stringers, various clips, fasteners, joints and fittings etc. To support Sizing & Justification phase. What you would do in this role Experience in Sizing and justification of metallic/Composite primary and secondary aircraft structural components. Experience in Door Surround Structures/Side shells/PAX floors. Experience in GFEM/DFEM(2D and3D) creation, validation, and condensation Good knowledge of airframe static stress analysis including analytical calculation methods (HSB/Niu/Bruhn) and finite element-based analysis. Stress analysis of Metallic and Composite Aircraft Structural components using FEM, ISAMI and Hand Calculations. Experience in ISAMI based analysis (CFH, MFH, CFA, CSPS, LUG, DT TI and EI, Notch sensitivity/Open Hole, Unfolding). Experience in Buckling and Modal Analysis. Experience in engineering tools, (ISAMI, Hypermesh, NASTRAN, PATRAN, MS Office). Experience Sizing/Justification of aircraft components by providing the solution to the problem. Good Knowledge on CATIA and experience in reading assembly drawings Strong Technical Report (Stress Dossier) writing skills. Training and Guiding the Juniors to execute the tasks. Stress tasks quality check

Entity:- Accenture Industry X Practice:- Aero Engineering (Aerostructure) Title:- Engineering Services Specialist - L9 Role:- Stress Analysis Job location:- Bangalore About Industry X:- Industry X combines Accenture's powerful digital capabilities with deep engineering and manufacturing expertise. We use the power of data and digital to help our clients reimagine the products they make, and how they make them. By connecting engineering and manufacturing operations every step of the way - from how products are designed and engineered, sourced and supplied, manufactured, to how they are serviced and renewed, we help them achieve greater productivity, drive growth and meet their sustainability commitments Know more:- www.youtube.com/watch?v=XaLxTEI3atI WHAT'S IN IT FOR YOU? Performs static stress analysis or fatigue and damage tolerance analysis of aircraft structures using a broad range of standard hand, legacy and harmonized methods, responsible for checking various types of aircraft components and assemblies:Door Surround Structures, Side and Lower Shells, Pax and Cargo Floors, Skins, stringers, various clips, fasteners, joints and fittings etc. To support Sizing & Justification phase. What you would do in this role Experience in Sizing and justification of metallic/Composite primary and secondary aircraft structural components. Experience in Door Surround Structures/Side shells/PAX floors. Experience in GFEM/DFEM(2D and3D) creation, validation, and condensation Good knowledge of airframe static stress analysis including analytical calculation methods (HSB/Niu/Bruhn) and finite element-based analysis. Stress analysis of Metallic and Composite Aircraft Structural components using FEM, ISAMI and Hand Calculations. Expertise in ISAMI based analysis (CFH, MFH, CFA, CSPS, LUG, DT TI and EI, Notch sensitivity/Open Hole, Unfolding). Expertise in Buckling and Modal Analysis. Strong technical aptitude, including applicable engineering tools, (ISAMI, Hypermesh, NASTRAN, PATRAN, MS Office). Expertise in Sizing/Justification of aircraft components by providing the mitigation solution for critical components. Good Knowledge on CATIA and experience in reading assembly drawings Strong Technical Report (Stress Dossier) writing and checking skills. Building, Leading, and guiding the team to execute the tasks. Stress quality check and Delivery responsibility. Training the resources to fill the knowledge gap. Qualification Who are we looking for? Overall 9 to 12 years of experience in Aerostructure domain Minimum 9 years of Aerostructure Stress Experience Location:Bangalore Education:BE/M.Tech in Mechanical, Aerospace, Aeronautical Engineering or relevant subject Ability to Guide, work and lead the team. Supporting continuous improvement initiatives to increase team efficiency. Ability to liaise and with the teams across the department including Design and Stress. Highly preferred A350/A350F primary and secondary structure experience with good knowledge of tools and methods. Hypermesh, Nastran/Patran, ISAMI Having VBA/Python programming is an added advantage. Accenture is an equal opportunities employer and welcomes applications from all sections of society and does not discriminate on grounds of race, religion or belief, ethnic or national origin, disability, age, citizenship, marital, domestic or civil partnership status, sexual orientation, gender identity, or any other basis as protected by applicable law.

Entity:- Accenture Industry X Practice:- Aero Engineering (Aerostructure) Title:- Engineering Services Specialist - L9 Role:- Stress Analysis Job location:- Bangalore About Industry X:- Industry X combines Accenture's powerful digital capabilities with deep engineering and manufacturing expertise. We use the power of data and digital to help our clients reimagine the products they make, and how they make them. By connecting engineering and manufacturing operations every step of the way - from how products are designed and engineered, sourced and supplied, manufactured, to how they are serviced and renewed, we help them achieve greater productivity, drive growth and meet their sustainability commitments Know more:- www.youtube.com/watch?v=XaLxTEI3atI WHAT'S IN IT FOR YOU? Performs static stress analysis or fatigue and damage tolerance analysis of aircraft structures using a broad range of standard hand, legacy and harmonized methods, responsible for checking various types of aircraft components and assemblies:Door Surround Structures, Side and Lower Shells, Pax and Cargo Floors, Skins, stringers, various clips, fasteners, joints and fittings etc. To support Sizing & Justification phase. What you would do in this role Experience in Sizing and justification of metallic/Composite primary and secondary aircraft structural components. Experience in Door Surround Structures/Side shells/PAX floors. Experience in GFEM/DFEM(2D and3D) creation, validation, and condensation Good knowledge of airframe static stress analysis including analytical calculation methods (HSB/Niu/Bruhn) and finite element-based analysis. Stress analysis of Metallic and Composite Aircraft Structural components using FEM, ISAMI and Hand Calculations. Expertise in ISAMI based analysis (CFH, MFH, CFA, CSPS, LUG, DT TI and EI, Notch sensitivity/Open Hole, Unfolding). Expertise in Buckling and Modal Analysis. Strong technical aptitude, including applicable engineering tools, (ISAMI, Hypermesh, NASTRAN, PATRAN, MS Office). Expertise in Sizing/Justification of aircraft components by providing the mitigation solution for critical components. Good Knowledge on CATIA and experience in reading assembly drawings Strong Technical Report (Stress Dossier) writing and checking skills. Building, Leading, and guiding the team to execute the tasks. Stress quality check and Delivery responsibility. Training the resources to fill the knowledge gap.

Entity:- Accenture Industry XPractice:- Aero Engineering (Aerostructure)Title:- Engineering Services AnalystRole:- F&DT EngineeringJob location:- BangaloreAbout Industry X:- Industry X combines Accenture's powerful digital capabilities with deep engineering and manufacturing expertise. We use the power of data and digital to help our clients reimagine the products they make, and how they make them. By connecting engineering and manufacturing operations every step of the way - from how products are designed and engineered, sourced and supplied, manufactured, to how they are serviced and renewed, we help them achieve greater productivity, drive growth and meet their sustainability commitments.Know more:- www.youtube.com/watch?v=XaLxTEI3atI WHAT'S IN IT FOR YOU? Performs Fatigue and Damage Tolerance analysis of aircraft structures using a broad range of standard hand, legacy and harmonized methods, responsible for checking various types of aircraft components and assemblies:Door Surround Structures, Side and Lower Shells, Pax and Cargo Floors, Skins, stringers, various clips, fasteners, joints and fittings etc. To support Sizing & Justification phases.What you would do in this role Experience in Sizing and justification of metallic/Composite primary and secondary aircraft structural components. Experience in Door Surround Structures/Side shells/PAX and Cargo floors. Analysis of metallic and composite structures (Plain Strength checks, Buckling, Bolted joint analysis) Experienced in spectrum generation. Calculation of Fatigue life by using or DFEM or ISAMI modules. Understanding of mission profiles, calculating rain flow counting, Preparation of stress files and FESPS databases Knowledge on Material and surface protection treatment to be used for fatigue calculations. Experience on Damage tolerance, crack propagation analysis on aircraft components. Should have strong foundation in the area of load/stress analysis with abilities to formulate "free body diagrams" and identify load path of structures. Knowledge on Non-destructive testing approaches. Experience with the use of both Finite Element (NASTRAN/PATRAN/HYPER MESH) and classical methods to perform structural load/Fatigue stress analysis for primary airframe structures is preferred. Continuous learning ability to understanding best practices in analysis and methodologies. Good Knowledge on CATIA and experience in reading assembly drawings. Strong Technical Report (Dossier) writing skills. Training and Guiding the Juniors to execute the tasks. F&DT tasks quality check. Qualifications Who are we looking for? 5 to 9 years of Aerostructure F&DT Analysis Experience Location:Bangalore Education:BE/M.Tech in Mechanical, Aerospace, Aeronautical Engineering or relevant subject Ability to Guide, work and lead the team. Supporting continuous improvement initiatives to increase team efficiency. Ability to liaise and with the teams across the department including Design and Stress. Highly preferred primary and secondary structure experience with good knowledge of tools and methods. Hypermesh, Nastran/Patran, ISAMI Having VBA/Python programming is an added advantage.Accenture is an equal opportunities employer and welcomes applications from all sections of society and does not discriminate on grounds of race, religion or belief, ethnic or national origin, disability, age, citizenship, marital, domestic or civil partnership status, sexual orientation, gender identity, or any other basis as protected by applicable law.

Entity:- Accenture Industry X Practice:- Aero Engineering (Aerostructure) Title:- Engineering Services Senior Analyst - 10 Role:- F&DT Engineering Job location:- Bangalore About Industry X:- Industry X combines Accenture's powerful digital capabilities with deep engineering and manufacturing expertise. We use the power of data and digital to help our clients reimagine the products they make, and how they make them. By connecting engineering and manufacturing operations every step of the way - from how products are designed and engineered, sourced and supplied, manufactured, to how they are serviced and renewed, we help them achieve greater productivity, drive growth and meet their sustainability commitments. Know more:- www.youtube.com/watchv=XaLxTEI3atI WHAT'S IN IT FOR YOU Performs Fatigue and Damage Tolerance analysis of aircraft structures using a broad range of standard hand, legacy and harmonized methods, responsible for checking various types of aircraft components and assemblies:Door Surround Structures, Side and Lower Shells, Pax and Cargo Floors, Skins, stringers, various clips, fasteners, joints and fittings etc. To support Sizing & Justification phases. What you would do in this role Experience in Sizing and justification of metallic/Composite primary and secondary aircraft structural components. Experience in Door Surround Structures/Side shells/PAX and Cargo floors. Analysis of metallic and composite structures (Plain Strength checks, Buckling, Bolted joint analysis) Experienced in spectrum generation. Calculation of Fatigue life by using or DFEM or ISAMI modules. Understanding of mission profiles, calculating rain flow counting, Preparation of stress files and FESPS databases Knowledge on Material and surface protection treatment to be used for fatigue calculations. Experience on Damage tolerance, crack propagation analysis on aircraft components. Should have strong foundation in the area of load/stress analysis with abilities to formulate "free body diagrams" and identify load path of structures. Knowledge on Non-destructive testing approaches. Experience with the use of both Finite Element (NASTRAN/PATRAN/HYPER MESH) and classical methods to perform structural load/Fatigue stress analysis for primary airframe structures is preferred. Continuous learning ability to understanding best practices in analysis and methodologies. Good Knowledge on CATIA and experience in reading assembly drawings. Strong Technical Report (Dossier) writing skills. Training and Guiding the Juniors to execute the tasks. F&DT tasks quality check. Qualifications Who are we looking for 5 to 9 years of Aerostructure F&DT Analysis Experience Location:Bangalore Education:BE/M.Tech in Mechanical, Aerospace, Aeronautical Engineering or relevant subject Ability to Guide, work and lead the team. Supporting continuous improvement initiatives to increase team efficiency. Ability to liaise and with the teams across the department including Design and Stress. Highly preferred primary and secondary structure experience with good knowledge of tools and methods. Hypermesh, Nastran/Patran, ISAMI Having VBA/Python programming is an added advantage. Accenture is an equal opportunities employer and welcomes applications from all sections of society and does not discriminate on grounds of race, religion or belief, ethnic or national origin, disability, age, citizenship, marital, domestic or civil partnership status, sexual orientation, gender identity, or any other basis as protected by applicable law.

Entity:- Accenture Industry X Practice:- Aero Engineering (Aerostructure) Title:- Engineering Services Specialist Role:- F&DT Engineering Job location:- Bangalore About Industry X:- Industry X combines Accenture's powerful digital capabilities with deep engineering and manufacturing expertise. We use the power of data and digital to help our clients reimagine the products they make, and how they make them. By connecting engineering and manufacturing operations every step of the way - from how products are designed and engineered, sourced and supplied, manufactured, to how they are serviced and renewed, we help them achieve greater productivity, drive growth and meet their sustainability commitments Know more:- www.youtube.com/watch?v=XaLxTEI3atI WHAT'S IN IT FOR YOU? Performs Fatigue and Damage Tolerance analysis of aircraft structures using a broad range of standard hand, legacy and harmonized methods, responsible for checking various types of aircraft components and assemblies:Door Surround Structures, Side and Lower Shells, Pax and Cargo Floors, Skins, stringers, various clips, fasteners, joints and fittings etc. To support Sizing & Justification phases. What you would do in this role Experience in Sizing and justification of metallic/Composite primary and secondary aircraft structural components. Experience in Door Surround Structures/Side shells/PAX and Cargo floors. Expertise of Fatigue life calculation by using DFEM or ISAMI modules, Crack Propagation Analysis. Expertise in ISAMI modules (Metallic Filled Hole, Composite Filled Hole, Lug analysis, Corin Analysis, Notch, Sensitivity, Damage Tolerance, Tension Fitting, Fatigue Spectrum Analysis (1D & 2D), Fatigue DFEM Initiation Modules, etc.,) Experience with the use of both Finite Element (NASTRAN/PATRAN/HYPER MESH) and classical methods to perform structural load/Fatigue stress analysis for primary airframe structures is preferred. Expertise in Sizing/Justification of aircraft components by providing the mitigation solution for critical components. Experienced in documents (like PDR/CDR/Certification reports, Concessions, Repairs) and report creation and getting validated. High level of customer and quality orientation together with strong abilities in consulting and implementation. Experience on to industry standard verification & validation methods Good written and oral communication skills in English. Perform in a pressure environment and make quick yet meaningful decisions. Continuous learning ability to understanding best practices in analysis and methodologies. Good Knowledge on CATIA and experience in reading assembly drawings. Strong Technical Report (Dossier) writing and checking skills. Building, Leading, and guiding the team to execute the tasks. F&DT quality check and Delivery responsibility. Good experience in planning the training for freshers and experienced resources to fill the knowledge gap. Qualifications Who are we looking for? Overall 8 to 12 years of experience in Aerostructure domain Minimum 9 years of Aerostructure F&DT Experience Location:Bangalore Education:BE/M.Tech in Mechanical, Aerospace, Aeronautical Engineering or relevant subject Ability to Guide, work and lead the team. Supporting continuous improvement initiatives to increase team efficiency. Ability to liaise and with the teams across the department including Design and Stress. Highly preferred A350/A350F primary and secondary structure experience with good knowledge of tools and methods. Hypermesh, Nastran/Patran, ISAMI Having VBA/Python programming is an added advantage. Accenture is an equal opportunities employer and welcomes applications from all sections of society and does not discriminate on grounds of race, religion or belief, ethnic or national origin, disability, age, citizenship, marital, domestic or civil partnership status, sexual orientation, gender identity, or any other basis as protected by applicable law.

Entity:- Accenture Industry XPractice:- Aero Engineering (Aerostructure)Title:- Engineering Services Associate Manager - L8Role:- F&DTJob location:- BangaloreAbout Industry X:- Industry X combines Accenture's powerful digital capabilities with deep engineering and manufacturing expertise. We use the power of data and digital to help our clients reimagine the products they make, and how they make them. By connecting engineering and manufacturing operations every step of the way - from how products are designed and engineered, sourced and supplied, manufactured, to how they are serviced and renewed, we help them achieve greater productivity, drive growth and meet their sustainability commitmentsKnow more:- www.youtube.com/watch?v=XaLxTEI3atI WHAT'S IN IT FOR YOU? Performs Fatigue and Damage Tolerance analysis of aircraft structures using a broad range of standard hand, legacy and harmonized methods, responsible for checking various types of aircraft components and assemblies:Door Surround Structures, Side and Lower Shells, Pax and Cargo Floors, Skins, stringers, various clips, fasteners, joints and fittings etc. To support Sizing & Justification phases.What you would do in this role Experience in Sizing and justification of metallic/Composite primary and secondary aircraft structural components. Experience in Door Surround Structures/Side shells/PAX and Cargo floors. Expertise of Fatigue life calculation by using DFEM or ISAMI modules, Crack Propagation Analysis. Expertise in ISAMI modules (Metallic Filled Hole, Composite Filled Hole, Lug analysis, Corin Analysis, Notch, Sensitivity, Damage Tolerance, Tension Fitting, Fatigue Spectrum Analysis (1D & 2D), Fatigue DFEM Initiation Modules, etc.,) Experience with the use of both Finite Element (NASTRAN/PATRAN/HYPER MESH) and classical methods to perform structural load/Fatigue stress analysis for primary airframe structures is preferred. Expertise in Sizing/Justification of aircraft components by providing the mitigation solution for critical components. Experienced in documents (like PDR/CDR/Certification reports, Concessions, Repairs) and report creation and getting validated. High level of customer and quality orientation together with strong abilities in consulting and implementation. Experience on to industry standard verification & validation methods Good written and oral communication skills in English. Perform in a pressure environment and make quick yet meaningful decisions. Continuous learning ability to understanding best practices in analysis and methodologies. Good Knowledge on CATIA and experience in reading assembly drawings. Strong Technical Report (Dossier) writing and checking skills. Good Experience in preparing effort estimation, Planning of the project deliverables and risk assessment. Customer interaction regarding technical discussion and project status. Capable of handling multiple projects. Building, Leading, and guiding the team to execute the tasks. F&DT quality Qualifications Who are we looking for? Overall 14+ years of experience in Aerostructure domain Minimum 12 years of Aerostructure F&DT Experience Location:Bangalore Education:BE/M.Tech in Mechanical, Aerospace, Aeronautical Engineering or relevant subject Ability to Guide, work and lead the team. Supporting continuous improvement initiatives to increase team efficiency. Ability to liaise and with the teams across the department including Design and Stress. Highly preferred A350/A350F primary and secondary structure experience with good knowledge of tools and methods. Hypermesh, Nastran/Patran, ISAMI Having VBA/Python programming is an added advantage.Accenture is an equal opportunities employer and welcomes applications from all sections of society and does not discriminate on grounds of race, religion or belief, ethnic or national origin, disability, age, citizenship, marital, domestic or civil partnership status, sexual orientation, gender identity, or any other basis as protected by applicable law.

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 : NA Minimum 3 year(s) of experience is required Educational Qualification : Bachelors or Masters degree in Mechanical or Aerospace or Structural engineering Summary :As an Aircraft Structural Analysis Manufacturing Engineering Practitioner, you will be responsible for defining processes to fabricate, assemble, inspect, and test new products and machines based on production engineering and design principles. Your typical day will involve developing procedures, product specifications, and defining quality standards and inspection methods for aircraft structural analysis. WHAT'S IN IT FOR YOU? Performs static stress analysis or fatigue and damage tolerance analysis of aircraft structures using a broad range of standard hand, legacy and harmonized methods, responsible for checking various types of aircraft components and assemblies:Door Surround Structures, Side and Lower Shells, Pax and Cargo Floors, Skins, stringers, various clips, fasteners, joints and fittings etc. To support Sizing & Justification phase. What you would do in this role Experience in Sizing and justification of metallic/Composite primary and secondary aircraft structural components. Experience in Door Surround Structures/Side shells/PAX floors. Experience in GFEM/DFEM(2D and3D) creation, validation, and condensation Good knowledge of airframe static stress analysis including analytical calculation methods (HSB/Niu/Bruhn) and finite element-based analysis. Stress analysis of Metallic and Composite Aircraft Structural components using FEM, ISAMI and Hand Calculations. Experience in ISAMI based analysis (CFH, MFH, CFA, CSPS, LUG, DT TI and EI, Notch sensitivity/Open Hole, Unfolding). Experience in Buckling and Modal Analysis. Experience in engineering tools, (ISAMI, Hypermesh, NASTRAN, PATRAN, MS Office). Experience Sizing/Justification of aircraft components by providing the solution to the problem. Good Knowledge on CATIA and experience in reading assembly drawings Strong Technical Report (Stress Dossier) writing skills. Training and Guiding the Juniors to execute the tasks. Stress tasks quality check Who are we looking for? 5 to 9 years of Aerostructure Stress Analysis Experience Location:Bangalore Education:BE/M.Tech in Mechanical, Aerospace, Aeronautical Engineering or relevant subject Ability to work individually and Guide the team. Supporting continuous improvement initiatives to increase team efficiency. Highly preferred primary and secondary structure experience with good knowledge of tools and methods. Hypermesh, Nastran/Patran, ISAMI Having VBA/Python programming is an added advantage. Qualification Bachelors or Masters degree in Mechanical or Aerospace or Structural engineering

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