60 Patran Jobs

We are seeking a skilled and detail-oriented Design Engineer – Aero Structures to join our aerospace engineering team. The ideal candidate will be responsible for the conceptual and detailed design of structural components such as fuselage, wings, nacelles, and empennage. You will use advanced CAD tools like CATIA V5 & V6 to develop and validate designs that meet strength, weight, cost, and regulatory requirements. This role requires collaboration with cross-functional teams including stress analysis, manufacturing, and certification groups to ensure optimal design solutions throughout the product lifecycle.

Position: Stress Engineer Location: Bengaluru Responsibilities: Experience in static analysis of aircraft interiors, structural components, secondary brackets, and other structures Experience in IFL & Static Test Plan (preferably commercial aircrafts). Sound knowledge of structural design principles, and aircraft structures. Finite element method / finite element analysis (FEM / FEA). Experience in composite & metallic structural analysis. Certification requirements and experience with stress dossiers. Hand Calculations & MS Office Experience working with Aerospace interiors and structures (Both Metallic & Composite). Ability to work independently & co-ordinate with the team. Stress methods understanding and providing critical design solutions. Ability to communicate effectively (Oral, Written & Presentation) Flexibility & adaptability to changing project scenarios and requirements. Technical Skills Required: NASTRAN PATRAN Hypermesh FEMAP

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 : 7+ Years Job Location : Bangalore Preferred Skills : Must have relevant Stress Analysis experience in Aerospace Domain. Should have good experience in Aero Structure Analysis Able to analyse stress (Static or Fatigue) and perform hand calculation Experience with FEM (Hyper works /Nastran /Patran)

Job Description 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 : NA Minimum 5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Execution of comprehensive fatigue and damage tolerance analysis for metallic and composite structural parts related to design and development of rotary wing aircrafts primary and secondary structures. Provide execution insight and facilitate the team with interpretation of static analysis results for defining the fatigue critical location, number of calculation points, fatigue sensitive area, primary and secondary load path identification, design philosophy identification, scatter factor selection in alignment with client and regulatory guidelines FAR/CS 25.571, 29.571, MIL-STD-1530 etc. Understand the meshing and analysis guidelines for static and fatigue analysis and ensure the FE models created by team for F&DT justifications are compiled to the guidelines and are of high quality. Ensure that the V&V documents capture the required checks for the FE models. Also ensure the specific considerations for the fatigue evaluation is correctly captured and simulated in the FE models and if required use your expertise and guidance to align with the requirements. Develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Identify the fatigue critical locations based on highly stressed areas from static analysis results, safety critical parts and the standard features which irrespective of stress value need to be checked. Down select the number of calculation points and align with the client on this. Decision basis for selection of reliable concepts out of multiple concepts based on the static and F&DT justification validations and compliance including future operational and maintenance and repair considerations. Enable F&DT team with expertise for generation of fatigue test plan (full scale and component level test), interpretation of test results and correlation with analysis in the test report. Review the outputs. Level II checker approver signatory for F&DT analysis certification reports, F&DT test plan, test orders and F&DT test reports. Enable team engagements and knowledge sharing for distributed teams across the programs and locations. Technically lead and guide the team for mitigating the low fatigue and crack growth life and F&DT performance non-compliance issues based on your expertise and experience. Align these methods with clients and document it as reference documents. Incorporate features and design aspects covering the downstream manufacturing and inspection processes, accessibility and in-service replacement/repair. Technically lead for aligning customer expectations with engineering deliverables and strategic goals. Collaborate and lead cross-functionally with design manufacturing quality, and systems teams. Technical interface with the client, ensuring timely issue resolutions, aligning design mitigations and any deviations needed w.r.t processes, methods, inputs, and deliverables. Professional & Technical Skills:Expertise and work experience in the design/development and integration of metallic, sheet metal, and composite helicopter aircraft structures for both primary and secondary components from F&DT point of view. Experience of implementing the weight optimization techniques, load path optimization, fatigue and damage tolerance analysis for helicopter/aircraft certification and testing activities. Knowledge of airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Experience in preparation of F&DT test plan, test orders, test load derivation and test to analysis correlation reports for component level and full-scale structural tests for rotary wing aircrafts. Exposure to certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with drawing standards. Any experience in process automation using MS excel VBA/Python etc Proficient in FEA and F&DT tools is essential with experience in NASGRO FRANC 3D MSC FATIGUE, MSC NASTRAN/PATRAN, HyperMesh/Optistrucut. or similar tools is a strong plus. Automation experience using Excel MACROS & VBA Python and CATIA V5 is a plus. Proven experience for structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Working experience related to aircraft materials, fatigue phenomenon, fracture mechanics concepts, fatigue spectrum derivation, probabilistic fatigue and crack growth assessments. Sound knowledge of primary and secondary load paths, structural classification and their relevance for the F&DT justification. Expertise in structural classification, related F&DT compliance, calculation points and their down selection, selection of scatter factors. Deep knowledge of FEA considerations and their incorporation in the meshing requirements for F&DT Analysis. Experience in end-to-end concept to design validation, manufacturability, certification and F&DT certification test and test correlation activities for preferably rotary wing aircraft helicopter certification. In-depth understanding of helicopter/aircraft load-bearing structures, structural response with focus on structural integrity, stiffness, and load path optimization under both static and Fatigue conditions. Knowledge of failure modes relevant to metallic and composite airframe components. Experience for low cycles and high cycle fatigue analysis for fixed wing or rotary wing aircrafts. Exposure to functional considerations like telescopic, foldability swivel and reversal of structure. Any specialization/certification in F&DT/Fracture mechanics/fatigue life extension etc will be a plus. Additional Information:- The candidate should have 9 to 12 years of practical experience in the Aerostructures fatigue and damage tolerance analysis domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Qualification 15 years full time education

Job Description 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 : NA Minimum 5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Design and develop primary and secondary structural componentsboth metallic and compositefor rotary-wing aircraft, ensuring compliance with airworthiness regulations, structural integrity requirements, and OEM-specific design standards. Understand the meshing and analysis guidelines for static, dynamic and impact analysis and ensure the FE models created by team are complied to the guidelines and are of high quality. Ensure that the V&V documents capture the required checks for the FE models. Also ensure the physics of the problem is correctly simulated in the FE models and if required use your expertise and guidance to align with the requirements. Ensure alignment and compliance to the client specific and regulatory guidelines as per FAR 27/29CS/JAR/Military MIL-STD-1530 etc Enable team engagements and knowledge sharing for distributed teams across the programs and locations. Validate the design of structural through Classical and FE Analysis, and assist in detailed load path analysis, optimal material selection based on Analysis results and operational design environmental conditions. Owning optimum design by static stress analysis Dynamic analysis and impact analysis evaluation of multiple structural design concepts through detailed trade-off analyses. Develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Perform weight estimation, its tracking, and control across all design phases, ensuring alignment with weight budgets and performance criteria. Technically lead and guide the team for mitigating the low RF Low life and performance non-compliance issues. Create the test FE models incorporating the failure, features and boundary conditions as per standard procedure and test fixture. Creating the method register, Method document, check lists and report templates in compliance with regulatory and client specific requirements. Front end and act as the technical interface with the client, ensuring alignment on deviations and processes, methods, inputs, overall objectives and deliverables. Interact with clients on a regular basis to track and classify the issues and ensure timely resolution of the issues as per SLA. Assist in during customer technical audits, program quality gate reviews, and change control reviews. Support and mentor junior team members by providing technical guidance, sharing best practices, and fostering their growth in design methodologies, tools, and domain knowledge. Actively contributes to skill development, knowledge transfer, and team capability building through hands-on support and constructive feedback. Professional & Technical Skills:Expertise in the design/development and integration of metallic, sheet metal, and composite helicopter aircraft structures for both primary and secondary components from Static point of view. Experience of static dynamic and impact analysis for sizing of large, fixed wing or rotary wing aircraft. Experience in weight optimization techniques, load path optimization for helicopter/aircraft certification and testing activities. Any experience in process automation using MS excel VBA/Python etc Strong knowledge of airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Experience in preparation of full scale and component level certification test plan, test orders, test load derivation and test to analysis correlation reports for component level for fixed wing or rotary wing aircrafts. Certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with GD & T and drawing standards. Proficiency over the structural static dynamic and impact analysis tools like general MSC NASTRAN/PATRAN/ABAQUS/ HyperMesh/ OptistructLS DYANA is must, Automation experience using Excel MACROS & VBA Python and Catia V5 is a plus. FEA considerations and meshing requirements for different types of structural analyses like static, dynamic, buckling and impact analyses. End to end validation, certification compliance, manufacturing support and certification test & test correlation activities specifically for rotary wing aircraft helicopter. High level skills and experience in the 2D/3D mesh creation and meshing guidelines, FE Modelling, and Assembly integration methodologies. Experience of aerospace material selection, structural feature simulation, analyses and meshing guidelines and procedures. Capability to solve day to day analysis problem in Analysis and post processing of Analysis results. Sound knowledge of helicopter/aircraft load-bearing structures, with focus on structural integrity, stiffness, and load path optimization under both static, dynamic, and impact conditions. Familiarity with Fatigue requirement is plus. High experience aligned with the rotary wing or fixed wing structural arrangement, primary, secondary and support structures, load path, sizing procedures for metallic and composite structures. Strong awareness of static dynamic and impact strength justification analyses and failure modes relevant to metallic and composite airframe components. Introductory knowledge about the analysis considerations for the any of the Innovative design and functional considerations like telescopic structures, foldability swivel and reversal of structure. Expertise for structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Familiar with structural analysis considerations related to assembly line constraints, ergonomic considerations, and sequence planning to ensure seamless integration in high-rate production environments. Additional Information:- The candidate should have a 8 to 9 years of practical experience static analysis/Dynamic analysis/ Impact Analysis in the Aerostructures domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering 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 : Aircraft Structural Analysis Minimum 7.5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:Join a mid-level leadership role within the Aerostructure Engineering team, supporting both strategy and technical execution across the full engineering lifecyclefrom concept through production, certification, and sustainment. Play a pivotal role in leading engineering delivery, technical governance, and client interactions for high-impact aerospace programs spanning rotary- and fixed-wing platforms. Opportunity to drive digital engineering initiatives including MBD, MBSE, and digital twin integration within legacy and next-gen design environments. Own design and development tasks for aircraft structural components. Apply advanced aircraft structural analyses Approach to Validate the design concepts through Classical and FE Analysis, and assist in detailed load path analysis, optimal material selection and operational design environmental conditions compliant to the airworthiness regulations, structural integrity requirements, and OEM-specific design standards. Preparation of method register, Method document, check lists, report templates, SLA in alignment with client. Guide the team for selection of optimum design by stress evaluation of multiple structural design concepts through detailed trade-off analyses for required dimensions and weight constraints. Maintaining scope requirement log, Input enabler and query trackers and coordinating with respective client stakeholders to get the resolutions on-time, ensuring high-quality output. Lead the team to develop complex 2D and 3D FE models, their integration, properties allocation, create validation and verification reports for the FE models, Analysis deck preparation/editing, perform structural Analyses, result extraction and interpretations, Error removal, post process and assist in developing automation using inhouse macros. Finalize the meshing and analyses requirements for different types of structural analyses in alignment with client. Mitigation in case of low RF/MOS, Alternative concepts analyses, compilation of inputs for the review and certification reports. Analyse complex design challenges and propose optimal engineering solutions. Level II and Level III checker and signatory for the analysis and certification reports from Accenture side. Certification test support creation of FE models incorporating the failure, features and boundary conditions as per standard procedure and test fixture. Ensuring alignment with weight budgets and performance criteria. Collaborate and lead cross-functionally with design team, manufacturing, quality, and systems teams; actively engage in design reviews, issue resolution, and integration discussions. Act as the primary technical interface with the client, ensuring alignment on design objectives and deliverables. Support and mentor junior team members by providing technical guidance, sharing best practices, and fostering their growth in design methodologies, tools, and domain knowledge. Actively contributes to skill development, knowledge transfer, and team capability building through hands-on support and constructive feedback. Professional & Technical Skills:Expertise in the design, development and integration of metallic, and composite helicopter aircraft structures for both primary and secondary components from static Dynamic/ Impact point of view. Experience of static dynamic and impact analysis for sizing of large, fixed wing or rotary wing aircraft. Experience in weight optimization techniques, load path optimization for helicopter/aircraft certification and testing activities. Working knowledge of airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Experience in preparation of full scale and component level certification test plan, test orders, test load derivation and test to analysis correlation reports for component level for fixed wing or rotary wing aircrafts. Familiarity with GD&T and industry drawing standards, Proficiency over the structural static dynamic and impact analysis tools like general MSC NASTRAN/PATRAN/ABAQUS/ HyperMesh/ OptistructLS DYANA is must, Can guide the team for automation using Excel MACROS & VBA Python and Catia V5 is a plus. FEA considerations and meshing requirements for different types of structural analyses like static, dynamic, buckling and impact analysis. End to end concept to design validation, certification, manufacturing support and certification test & test correlation activities specifically for rotary wing aircraft helicopter. Command over the 2D/3D mesh creation and meshing guidelines, FE Modelling, and Assembly integration methodologies. Strong grasp of aerospace material selection, structural feature simulation, analyses and meshing guidelines and procedures. Capability to solve day to day analysis problem in Analysis and post processing of Analysis results. In-depth understanding of helicopter/aircraft load-bearing structures, with focus on structural integrity, stiffness, and load path optimization under both static, dynamic, and impact conditions. Familiarity with Fatigue requirement is plus. Deep knowledge of rotary wing or fixed wing structural arrangement, primary, secondary and support structures, load path, sizing procedures for metallic and composite structures. Strong awareness of static dynamic and impact strength justification analyses and failure modes relevant to metallic and composite airframe components. Analysis considerations for the any of the Innovative design and functional considerations like telescopic structures, foldability swivel and reversal of structure. Expertise for structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Familiar with structural analysis considerations related to assembly line constraints, ergonomic considerations, and sequence planning to ensure seamless integration in high-rate production environments. Additional Information:- The candidate should have a 12 to 15 years of experience in the Aerostructure Analysis domain preferably for the rotary wing aircrafts, in a technical managerial & program manager role for OEM/service providers. This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering 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 : Aircraft Structural Analysis Minimum 5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Design and develop primary and secondary structural componentsboth metallic and compositefor rotary-wing aircraft, ensuring compliance with airworthiness regulations, structural integrity requirements, and OEM-specific design standards. Understand the meshing and analysis guidelines for static, dynamic and impact analysis and ensure the FE models created by team are complied to the guidelines and are of high quality. Ensure that the V&V documents capture the required checks for the FE models. Also ensure the physics of the problem is correctly simulated in the FE models and if required use your expertise and guidance to align with the requirements. Ensure alignment and compliance to the client specific and regulatory guidelines as per FAR 27/29CS/JAR/Military MIL-STD-1530 etc Enable team engagements and knowledge sharing for distributed teams across the programs and locations. Validate the design of structural through Classical and FE Analysis, and assist in detailed load path analysis, optimal material selection based on Analysis results and operational design environmental conditions. Owning optimum design by static stress analysis Dynamic analysis and impact analysis evaluation of multiple structural design concepts through detailed trade-off analyses. Develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Perform weight estimation, its tracking, and control across all design phases, ensuring alignment with weight budgets and performance criteria. Technically lead and guide the team for mitigating the low RF Low life and performance non-compliance issues. Create the test FE models incorporating the failure, features and boundary conditions as per standard procedure and test fixture. Creating the method register, Method document, check lists and report templates in compliance with regulatory and client specific requirements. Front end and act as the technical interface with the client, ensuring alignment on deviations and processes, methods, inputs, overall objectives and deliverables. Interact with clients on a regular basis to track and classify the issues and ensure timely resolution of the issues as per SLA. Assist in during customer technical audits, program quality gate reviews, and change control reviews. Support and mentor junior team members by providing technical guidance, sharing best practices, and fostering their growth in design methodologies, tools, and domain knowledge. Actively contributes to skill development, knowledge transfer, and team capability building through hands-on support and constructive feedback. Professional & Technical Skills:Expertise in the design/development and integration of metallic, sheet metal, and composite helicopter aircraft structures for both primary and secondary components from Static point of view. Experience of static dynamic and impact analysis for sizing of large, fixed wing or rotary wing aircraft. Experience in weight optimization techniques, load path optimization for helicopter/aircraft certification and testing activities. Any experience in process automation using MS excel VBA/Python etc Strong knowledge of airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Experience in preparation of full scale and component level certification test plan, test orders, test load derivation and test to analysis correlation reports for component level for fixed wing or rotary wing aircrafts. Certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with GD & T and drawing standards. Proficiency over the structural static dynamic and impact analysis tools like general MSC NASTRAN/PATRAN/ABAQUS/ HyperMesh/ OptistructLS DYANA is must, Automation experience using Excel MACROS & VBA Python and Catia V5 is a plus. FEA considerations and meshing requirements for different types of structural analyses like static, dynamic, buckling and impact analyses. End to end validation, certification compliance, manufacturing support and certification test & test correlation activities specifically for rotary wing aircraft helicopter. High level skills and experience in the 2D/3D mesh creation and meshing guidelines, FE Modelling, and Assembly integration methodologies. Experience of aerospace material selection, structural feature simulation, analyses and meshing guidelines and procedures. Capability to solve day to day analysis problem in Analysis and post processing of Analysis results. Sound knowledge of helicopter/aircraft load-bearing structures, with focus on structural integrity, stiffness, and load path optimization under both static, dynamic, and impact conditions. Familiarity with Fatigue requirement is plus. High experience aligned with the rotary wing or fixed wing structural arrangement, primary, secondary and support structures, load path, sizing procedures for metallic and composite structures. Strong awareness of static dynamic and impact strength justification analyses and failure modes relevant to metallic and composite airframe components. Introductory knowledge about the analysis considerations for the any of the Innovative design and functional considerations like telescopic structures, foldability swivel and reversal of structure. Expertise for structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Familiar with structural analysis considerations related to assembly line constraints, ergonomic considerations, and sequence planning to ensure seamless integration in high-rate production environments. Additional Information:- The candidate should have a 8 to 9 years of practical experience static analysis/Dynamic analysis/ Impact Analysis in the Aerostructures domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering 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 : Aircraft Structural Analysis Minimum 3 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Design and develop primary and secondary structural componentsboth metallic and compositefor rotary-wing aircraft, ensuring compliance with airworthiness regulations, structural integrity requirements, and OEM-specific design standards. Use meshing and analysis guidelines for static, dynamic and impact analysis and ensure the FE models created by team are compiled to the guidelines and are of high quality. Perform the checks and prepare FEA V&V documents, capture the required checks for the FE models. Also ensure the physics of the problem is correctly simulated in the FE models and if required use your expertise and guidance to align with the requirements. Perform FEA analysis for static dynamic and impact analysis in alignment and compliance to the client specific and regulatory guidelines as per FAR 27/29CS/JAR/Military MIL-STD-1530 etc Take up team engagements and knowledge sharing sessions for distributed teams across the programs and locations. Design validation of structural through Classical and FE Analysis, and assist in detailed load path analysis, optimal material selection based on Analysis results and operational design environmental conditions. Document the details for presenting into the certification reports and certifying agencies. Provide supporting evidence for the selection of optimum design by static stress analysis Dynamic analysis and impact analysis evaluation of multiple structural design concepts through detailed trade-off analyses. Comply to schedule, weight requirement and cost compliance by efficiently tracking methods. Follow escalation mechanism to ensure compliance. Develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Provide analysis results for the decision process of selection of reliable concepts out of multiple concepts based on the static, dynamic and impact stress analysis validation with future operational and maintenance and repair considerations. Provide details from FE models for the weight estimation, its tracking, and control across all design phases, ensuring alignment with weight budgets and performance criteria. Perform the task of mitigating the low RF Low life and performance non-compliance issues based on discussion with SME/Leads or your expertise and experience. Align relevant details of these methods to SME/Leads to align with the client. Documentation of iterations and outcomes for future reference. Create the test FE models incorporating the failure, features and boundary conditions as per standard procedure and test fixture. Design validate through analysis or classical calculations the Incorporated features and design aspects covering the downstream manufacturing and inspection processes, accessibility and in-service replacement/repair. Prepare detailed presentation for reference and review. Assist in during customer technical audits, program quality gate reviews, and change control reviews by providing the required analysis results and justifications. Professional & Technical Skills:Experience with Aerospace projects for the design/development and integration of metallic, and composite helicopter aircraft structures for both primary and secondary components. Knowledge of Aerospace structures, their classification as primary, secondary and support structures based on load bearing capacities. Experience of static dynamic and impact analysis for sizing of large, fixed-wing or rotary wing aircraft for major OEMs. Exposure to weight optimization techniques, load path optimization for helicopter/aircraft certification and testing activities. Experience in process automation using MS excel VBA/Python etc Exposure to airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Knowledge of Preparation of full scale and component level certification test plan, test orders, test load derivation and test to analysis correlation reports for component level for fixed wing or rotary wing aircrafts. Knowledge of certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with drawing standards. Proficiency over the structural static dynamic and impact analysis tools like general MSC NASTRAN/PATRAN/ABAQUS/ HyperMesh/ OptistructLS DYANA is must, Automation experience using Excel MACROS & VBA Python and Catia V5 is a plus. FEA considerations and meshing requirements for different types of structural analyses like static, dynamic, buckling and impact analyses. FEA V&V methods, analysis as per the certification compliance, manufacturing support and certification. Create inputs for the test & test correlation activities specifically for rotary wing aircraft helicopter. Experience in the 2D/3D mesh creation and meshing guidelines, FE Modelling, and Assembly integration methodologies. Experience of aerospace material, structural feature simulation, analyses as per meshing guidelines and procedures. Capability to solve day to day analysis problem in Analysis, analysis error and post processing of Analysis results. knowledge of helicopter/aircraft load-bearing structures Experience aligned with the rotary wing or fixed wing structural arrangement, primary, secondary and support structures, load path, sizing procedures for metallic and composite structures. Familiarity with Fatigue requirement is plus. Experience in static dynamic and impact strength justification analyses and failure modes relevant to metallic and composite airframe components. Exposure to Innovative design and functional considerations like telescopic structures, foldability swivel and reversal of structure. Knowledge of structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Additional Information:- The candidate should have a 5 to 8 years of practical experience static analysis/Dynamic analysis/ Impact Analysis in the Aerostructures domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering 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 : Aircraft Structural Analysis Good to have skills : NA Minimum 3 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Design and develop primary and secondary structural componentsboth metallic and compositefor rotary-wing aircraft, ensuring compliance with airworthiness regulations, structural integrity requirements, and OEM-specific design standards. Use meshing and analysis guidelines for static, dynamic and impact analysis and ensure the FE models created by team are compiled to the guidelines and are of high quality. Perform the checks and prepare FEA V&V documents, capture the required checks for the FE models. Also ensure the physics of the problem is correctly simulated in the FE models and if required use your expertise and guidance to align with the requirements. Perform FEA analysis for static dynamic and impact analysis in alignment and compliance to the client specific and regulatory guidelines as per FAR 27/29CS/JAR/Military MIL-STD-1530 etc Take up team engagements and knowledge sharing sessions for distributed teams across the programs and locations. Design validation of structural through Classical and FE Analysis, and assist in detailed load path analysis, optimal material selection based on Analysis results and operational design environmental conditions. Document the details for presenting into the certification reports and certifying agencies. Provide supporting evidence for the selection of optimum design by static stress analysis Dynamic analysis and impact analysis evaluation of multiple structural design concepts through detailed trade-off analyses. Comply to schedule, weight requirement and cost compliance by efficiently tracking methods. Follow escalation mechanism to ensure compliance. Develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Provide analysis results for the decision process of selection of reliable concepts out of multiple concepts based on the static, dynamic and impact stress analysis validation with future operational and maintenance and repair considerations. Provide details from FE models for the weight estimation, its tracking, and control across all design phases, ensuring alignment with weight budgets and performance criteria. Perform the task of mitigating the low RF Low life and performance non-compliance issues based on discussion with SME/Leads or your expertise and experience. Align relevant details of these methods to SME/Leads to align with the client. Documentation of iterations and outcomes for future reference. Create the test FE models incorporating the failure, features and boundary conditions as per standard procedure and test fixture. Design validate through analysis or classical calculations the Incorporated features and design aspects covering the downstream manufacturing and inspection processes, accessibility and in-service replacement/repair. Prepare detailed presentation for reference and review. Assist in during customer technical audits, program quality gate reviews, and change control reviews by providing the required analysis results and justifications. Professional & Technical Skills:Experience with Aerospace projects for the design/development and integration of metallic, and composite helicopter aircraft structures for both primary and secondary components. Knowledge of Aerospace structures, their classification as primary, secondary and support structures based on load bearing capacities. Experience of static dynamic and impact analysis for sizing of large, fixed-wing or rotary wing aircraft for major OEMs. Exposure to weight optimization techniques, load path optimization for helicopter/aircraft certification and testing activities. Experience in process automation using MS excel VBA/Python etc Exposure to airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Knowledge of Preparation of full scale and component level certification test plan, test orders, test load derivation and test to analysis correlation reports for component level for fixed wing or rotary wing aircrafts. Knowledge of certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with drawing standards. Proficiency over the structural static dynamic and impact analysis tools like general MSC NASTRAN/PATRAN/ABAQUS/ HyperMesh/ OptistructLS DYANA is must, Automation experience using Excel MACROS & VBA Python and Catia V5 is a plus. FEA considerations and meshing requirements for different types of structural analyses like static, dynamic, buckling and impact analyses. FEA V&V methods, analysis as per the certification compliance, manufacturing support and certification. Create inputs for the test & test correlation activities specifically for rotary wing aircraft helicopter. Experience in the 2D/3D mesh creation and meshing guidelines, FE Modelling, and Assembly integration methodologies. Experience of aerospace material, structural feature simulation, analyses as per meshing guidelines and procedures. Capability to solve day to day analysis problem in Analysis, analysis error and post processing of Analysis results. knowledge of helicopter/aircraft load-bearing structures Experience aligned with the rotary wing or fixed wing structural arrangement, primary, secondary and support structures, load path, sizing procedures for metallic and composite structures. Familiarity with Fatigue requirement is plus. Experience in static dynamic and impact strength justification analyses and failure modes relevant to metallic and composite airframe components. Exposure to Innovative design and functional considerations like telescopic structures, foldability swivel and reversal of structure. Knowledge of structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Additional Information:- The candidate should have a 5 to 8 years of practical experience static analysis/Dynamic analysis/ Impact Analysis in the Aerostructures domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering 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 : NA Minimum 3 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Independently execution of comprehensive fatigue and damage tolerance analysis for metallic and composite structural parts related to design and development of rotary wing aircrafts primary and secondary structures. Perform the static FEA independently for fatigue loading to facilitate the team with interpretation of static analysis results for defining the fatigue critical location, number of calculation points, fatigue sensitive area, primary and secondary load path identification, design philosophy identification, scatter factor selection in alignment with client and regulatory guidelines FAR/CS 25.571, 29.571, MIL-STD-1530 etc. Follow the meshing and analysis guidelines for static and fatigue analysis and ensure the FE models created by team for F&DT justifications are compiled to the guidelines and are of high quality. Perform the FEA V&V checks and prepare the V&V documents capture the required checks for the FE models. Also ensure the specific considerations for the fatigue evaluation is correctly captured and simulated in the FE models and if required use your expertise and guidance to align with the requirements. Independently develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Prepare detailed output which will help to Identify the fatigue critical locations based on highly stressed areas from static analysis results, safety critical parts and the standard features which irrespective of stress value need to be checked. Perform the low RF/MOS mitigation, Alternative concepts analyses, compilation of inputs for the review and certification reports. Down select the number of calculation points and align with the client on this in alignment with SME/Team leads. Perform the required analyses checks to enable decision basis for selection of reliable concepts out of multiple concepts based on the static and F&DT justification validations compliance including future operational and maintenance and repair considerations. Enable F&DT team with required inputs for generation of fatigue test plan (full scale and component level test), interpretation of test results and correlation with analysis in the test report. Review the outputs. Peer checker for F&DT analysis certification task. Enable team engagements and knowledge sharing for distributed teams across the programs and locations. Perform the mitigation task for the low fatigue, crack growth life and F&DT performance non-compliance issues based on your expertise and experience. Align these methods with SMEs team leaders and document it as reference documents. Perform tasks as required based on the outcomes of Collaboration with cross-functional discussions with design manufacturing quality, and systems teams; actively support with relevant detailed results and observations to engage in design reviews, issue resolution, and integration discussions. Assisting customer technical audits, program quality gate reviews, and change control reviews. Support and mentor junior team members by providing technical guidance, sharing best practices, and fostering their growth in design methodologies, tools, and domain knowledge. Enable aligning customer expectations with engineering deliverables and strategic goals. Ensure engineering activities meet cost, schedule, target weight and performance objectives while maintaining traceability and regulatory compliance. Professional & Technical Skills:Expertise in the design/development and integration of metallic, sheet metal, and composite helicopter aircraft structures for both primary and secondary components from F&DT point of view. Experience of static and F&DT analysis for sizing of large, fixed wing or rotary wing aircraft. Experience in weight optimization techniques, load path optimization, fatigue and damage tolerance analysis for helicopter/aircraft certification and testing activities. Strong knowledge of airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Experience in preparation of F&DT test plan, test orders, test load derivation and test to analysis correlation reports for component level and full-scale structural tests for rotary wing aircrafts. Certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with drawing standards. Proficient in FEA and F&DT tools is essential with experience in NASGRO FRANC 3D MSC FATIGUE, MSC NASTRAN/PATRAN, HyperMesh/Optistrucut. or similar tools is a strong plus. Automation experience using Excel MACROS & VBA Python and Catia V5 is a plus. Expertise for structural sizing of aerospace structural parts meeting certification, testing and manufacturability requirements. Sound work experience related to aircraft materials, fatigue phenomenon, fracture mechanics concepts, fatigue spectrum derivation, probabilistic fatigue and crack growth assessments. Must have knowledge of structural classification, primary and secondary structure design requirements, load path and structural response. Perform the low RF/MOS mitigation, Alternative concepts analyses, compilation of inputs for the review and certification reports. Expertise in structural classification, related F&DT compliance, calculation points and their down selection, selection of scatter factors. FEA considerations and their incorporation in the meshing requirements for F&DT Analysis. In-depth understanding of helicopter/aircraft load-bearing structures, structural response with focus on structural integrity, stiffness, and load path optimization under both static and Fatigue conditions. Knowledge of failure modes relevant to metallic and composite airframe components. Proven experience for low cycles and high cycle fatigue analysis for fixed wing or rotary wing aircrafts. Exposure to functional considerations like telescopic, foldability swivel and reversal of structure. Additional Information:- The candidate should have 5 to 8 years of practical experience in the Aerostructures fatigue and damage tolerance analysis domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering 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 : NA Minimum 5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Execution of comprehensive fatigue and damage tolerance analysis for metallic and composite structural parts related to design and development of rotary wing aircrafts primary and secondary structures. Provide execution insight and facilitate the team with interpretation of static analysis results for defining the fatigue critical location, number of calculation points, fatigue sensitive area, primary and secondary load path identification, design philosophy identification, scatter factor selection in alignment with client and regulatory guidelines FAR/CS 25.571, 29.571, MIL-STD-1530 etc. Understand the meshing and analysis guidelines for static and fatigue analysis and ensure the FE models created by team for F&DT justifications are compiled to the guidelines and are of high quality. Ensure that the V&V documents capture the required checks for the FE models. Also ensure the specific considerations for the fatigue evaluation is correctly captured and simulated in the FE models and if required use your expertise and guidance to align with the requirements. Develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Identify the fatigue critical locations based on highly stressed areas from static analysis results, safety critical parts and the standard features which irrespective of stress value need to be checked. Down select the number of calculation points and align with the client on this. Decision basis for selection of reliable concepts out of multiple concepts based on the static and F&DT justification validations and compliance including future operational and maintenance and repair considerations. Enable F&DT team with expertise for generation of fatigue test plan (full scale and component level test), interpretation of test results and correlation with analysis in the test report. Review the outputs. Level II checker approver signatory for F&DT analysis certification reports, F&DT test plan, test orders and F&DT test reports. Enable team engagements and knowledge sharing for distributed teams across the programs and locations. Technically lead and guide the team for mitigating the low fatigue and crack growth life and F&DT performance non-compliance issues based on your expertise and experience. Align these methods with clients and document it as reference documents. Incorporate features and design aspects covering the downstream manufacturing and inspection processes, accessibility and in-service replacement/repair. Technically lead for aligning customer expectations with engineering deliverables and strategic goals. Collaborate and lead cross-functionally with design manufacturing quality, and systems teams. Technical interface with the client, ensuring timely issue resolutions, aligning design mitigations and any deviations needed w.r.t processes, methods, inputs, and deliverables. Professional & Technical Skills:Expertise and work experience in the design/development and integration of metallic, sheet metal, and composite helicopter aircraft structures for both primary and secondary components from F&DT point of view. Experience of implementing the weight optimization techniques, load path optimization, fatigue and damage tolerance analysis for helicopter/aircraft certification and testing activities. Knowledge of airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Experience in preparation of F&DT test plan, test orders, test load derivation and test to analysis correlation reports for component level and full-scale structural tests for rotary wing aircrafts. Exposure to certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with drawing standards. Any experience in process automation using MS excel VBA/Python etc Proficient in FEA and F&DT tools is essential with experience in NASGRO FRANC 3D MSC FATIGUE, MSC NASTRAN/PATRAN, HyperMesh/Optistrucut. or similar tools is a strong plus. Automation experience using Excel MACROS & VBA Python and CATIA V5 is a plus. Proven experience for structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Working experience related to aircraft materials, fatigue phenomenon, fracture mechanics concepts, fatigue spectrum derivation, probabilistic fatigue and crack growth assessments. Sound knowledge of primary and secondary load paths, structural classification and their relevance for the F&DT justification. Expertise in structural classification, related F&DT compliance, calculation points and their down selection, selection of scatter factors. Deep knowledge of FEA considerations and their incorporation in the meshing requirements for F&DT Analysis. Experience in end-to-end concept to design validation, manufacturability, certification and F&DT certification test and test correlation activities for preferably rotary wing aircraft helicopter certification. In-depth understanding of helicopter/aircraft load-bearing structures, structural response with focus on structural integrity, stiffness, and load path optimization under both static and Fatigue conditions. Knowledge of failure modes relevant to metallic and composite airframe components. Experience for low cycles and high cycle fatigue analysis for fixed wing or rotary wing aircrafts. Exposure to functional considerations like telescopic, foldability swivel and reversal of structure. Any specialization/certification in F&DT/Fracture mechanics/fatigue life extension etc will be a plus. Additional Information:- The candidate should have 9 to 12 years of practical experience in the Aerostructures fatigue and damage tolerance analysis domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering 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 : Aircraft Structural Analysis Minimum 5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Design and develop primary and secondary structural componentsboth metallic and compositefor rotary-wing aircraft, ensuring compliance with airworthiness regulations, structural integrity requirements, and OEM-specific design standards. Understand the meshing and analysis guidelines for static, dynamic and impact analysis and ensure the FE models created by team are complied to the guidelines and are of high quality. Ensure that the V&V documents capture the required checks for the FE models. Also ensure the physics of the problem is correctly simulated in the FE models and if required use your expertise and guidance to align with the requirements. Ensure alignment and compliance to the client specific and regulatory guidelines as per FAR 27/29CS/JAR/Military MIL-STD-1530 etc Enable team engagements and knowledge sharing for distributed teams across the programs and locations. Validate the design of structural through Classical and FE Analysis, and assist in detailed load path analysis, optimal material selection based on Analysis results and operational design environmental conditions. Owning optimum design by static stress analysis Dynamic analysis and impact analysis evaluation of multiple structural design concepts through detailed trade-off analyses. Develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Perform weight estimation, its tracking, and control across all design phases, ensuring alignment with weight budgets and performance criteria. Technically lead and guide the team for mitigating the low RF Low life and performance non-compliance issues. Create the test FE models incorporating the failure, features and boundary conditions as per standard procedure and test fixture. Creating the method register, Method document, check lists and report templates in compliance with regulatory and client specific requirements. Front end and act as the technical interface with the client, ensuring alignment on deviations and processes, methods, inputs, overall objectives and deliverables. Interact with clients on a regular basis to track and classify the issues and ensure timely resolution of the issues as per SLA. Assist in during customer technical audits, program quality gate reviews, and change control reviews. Support and mentor junior team members by providing technical guidance, sharing best practices, and fostering their growth in design methodologies, tools, and domain knowledge. Actively contributes to skill development, knowledge transfer, and team capability building through hands-on support and constructive feedback. Professional & Technical Skills:Expertise in the design/development and integration of metallic, sheet metal, and composite helicopter aircraft structures for both primary and secondary components from Static point of view. Experience of static dynamic and impact analysis for sizing of large, fixed wing or rotary wing aircraft. Experience in weight optimization techniques, load path optimization for helicopter/aircraft certification and testing activities. Any experience in process automation using MS excel VBA/Python etc Strong knowledge of airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Experience in preparation of full scale and component level certification test plan, test orders, test load derivation and test to analysis correlation reports for component level for fixed wing or rotary wing aircrafts. Certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with GD & T and drawing standards. Proficiency over the structural static dynamic and impact analysis tools like general MSC NASTRAN/PATRAN/ABAQUS/ HyperMesh/ OptistructLS DYANA is must, Automation experience using Excel MACROS & VBA Python and Catia V5 is a plus. FEA considerations and meshing requirements for different types of structural analyses like static, dynamic, buckling and impact analyses. End to end validation, certification compliance, manufacturing support and certification test & test correlation activities specifically for rotary wing aircraft helicopter. High level skills and experience in the 2D/3D mesh creation and meshing guidelines, FE Modelling, and Assembly integration methodologies. Experience of aerospace material selection, structural feature simulation, analyses and meshing guidelines and procedures. Capability to solve day to day analysis problem in Analysis and post processing of Analysis results. Sound knowledge of helicopter/aircraft load-bearing structures, with focus on structural integrity, stiffness, and load path optimization under both static, dynamic, and impact conditions. Familiarity with Fatigue requirement is plus. High experience aligned with the rotary wing or fixed wing structural arrangement, primary, secondary and support structures, load path, sizing procedures for metallic and composite structures. Strong awareness of static dynamic and impact strength justification analyses and failure modes relevant to metallic and composite airframe components. Introductory knowledge about the analysis considerations for the any of the Innovative design and functional considerations like telescopic structures, foldability swivel and reversal of structure. Expertise for structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Familiar with structural analysis considerations related to assembly line constraints, ergonomic considerations, and sequence planning to ensure seamless integration in high-rate production environments. Additional Information:- The candidate should have a 8 to 9 years of practical experience static analysis/Dynamic analysis/ Impact Analysis in the Aerostructures domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering 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 : Aircraft Structural Analysis Minimum 3 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Design and develop primary and secondary structural componentsboth metallic and compositefor rotary-wing aircraft, ensuring compliance with airworthiness regulations, structural integrity requirements, and OEM-specific design standards. Use meshing and analysis guidelines for static, dynamic and impact analysis and ensure the FE models created by team are compiled to the guidelines and are of high quality. Perform the checks and prepare FEA V&V documents, capture the required checks for the FE models. Also ensure the physics of the problem is correctly simulated in the FE models and if required use your expertise and guidance to align with the requirements. Perform FEA analysis for static dynamic and impact analysis in alignment and compliance to the client specific and regulatory guidelines as per FAR 27/29CS/JAR/Military MIL-STD-1530 etc Take up team engagements and knowledge sharing sessions for distributed teams across the programs and locations. Design validation of structural through Classical and FE Analysis, and assist in detailed load path analysis, optimal material selection based on Analysis results and operational design environmental conditions. Document the details for presenting into the certification reports and certifying agencies. Provide supporting evidence for the selection of optimum design by static stress analysis Dynamic analysis and impact analysis evaluation of multiple structural design concepts through detailed trade-off analyses. Comply to schedule, weight requirement and cost compliance by efficiently tracking methods. Follow escalation mechanism to ensure compliance. Develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Provide analysis results for the decision process of selection of reliable concepts out of multiple concepts based on the static, dynamic and impact stress analysis validation with future operational and maintenance and repair considerations. Provide details from FE models for the weight estimation, its tracking, and control across all design phases, ensuring alignment with weight budgets and performance criteria. Perform the task of mitigating the low RF Low life and performance non-compliance issues based on discussion with SME/Leads or your expertise and experience. Align relevant details of these methods to SME/Leads to align with the client. Documentation of iterations and outcomes for future reference. Create the test FE models incorporating the failure, features and boundary conditions as per standard procedure and test fixture. Design validate through analysis or classical calculations the Incorporated features and design aspects covering the downstream manufacturing and inspection processes, accessibility and in-service replacement/repair. Prepare detailed presentation for reference and review. Assist in during customer technical audits, program quality gate reviews, and change control reviews by providing the required analysis results and justifications. Professional & Technical Skills:Experience with Aerospace projects for the design/development and integration of metallic, and composite helicopter aircraft structures for both primary and secondary components. Knowledge of Aerospace structures, their classification as primary, secondary and support structures based on load bearing capacities. Experience of static dynamic and impact analysis for sizing of large, fixed-wing or rotary wing aircraft for major OEMs. Exposure to weight optimization techniques, load path optimization for helicopter/aircraft certification and testing activities. Experience in process automation using MS excel VBA/Python etc Exposure to airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Knowledge of Preparation of full scale and component level certification test plan, test orders, test load derivation and test to analysis correlation reports for component level for fixed wing or rotary wing aircrafts. Knowledge of certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with drawing standards. Proficiency over the structural static dynamic and impact analysis tools like general MSC NASTRAN/PATRAN/ABAQUS/ HyperMesh/ OptistructLS DYANA is must, Automation experience using Excel MACROS & VBA Python and Catia V5 is a plus. FEA considerations and meshing requirements for different types of structural analyses like static, dynamic, buckling and impact analyses. FEA V&V methods, analysis as per the certification compliance, manufacturing support and certification. Create inputs for the test & test correlation activities specifically for rotary wing aircraft helicopter. Experience in the 2D/3D mesh creation and meshing guidelines, FE Modelling, and Assembly integration methodologies. Experience of aerospace material, structural feature simulation, analyses as per meshing guidelines and procedures. Capability to solve day to day analysis problem in Analysis, analysis error and post processing of Analysis results. knowledge of helicopter/aircraft load-bearing structures Experience aligned with the rotary wing or fixed wing structural arrangement, primary, secondary and support structures, load path, sizing procedures for metallic and composite structures. Familiarity with Fatigue requirement is plus. Experience in static dynamic and impact strength justification analyses and failure modes relevant to metallic and composite airframe components. Exposure to Innovative design and functional considerations like telescopic structures, foldability swivel and reversal of structure. Knowledge of structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Additional Information:- The candidate should have a 5 to 8 years of practical experience static analysis/Dynamic analysis/ Impact Analysis in the Aerostructures domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering 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 Minimum 12 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:Lead strategic aerospace engineering engagements for rotary wing platforms, driving technical delivery, innovation, and client satisfaction. Play a key role in shaping engineering processes, delivery governance, and team capability development. Engage directly with aerospace OEMs, Tier-1 suppliers and regulatory bodies, influencing design decisions, compliance strategies, and product lifecycle outcomes. Drive digital engineering transformation, championing initiatives around MBSE, MBD, and digital continuity. Lead and oversee the execution of comprehensive fatigue and damage tolerance analysis for metallic and composite structural parts related to design and development of rotary wing aircrafts primary and secondary structures. Guide the team with interpretation of static analysis results for defining the fatigue critical location, number of calculation points, fatigue sensitive area, primary and secondary load path identification, design philosophy identification, scatter factor selection in alignment with client and regulatory guidelines FAR/CS 25.571, 29.571, MIL-STD-1530 etc. Establish and govern engineering F&DT analysis best practices, design review frameworks, and technical quality gates across the program lifecycle. Provide technical oversight related to F&DT across multiple concept development, structural architecture, F&DT requirement compliance for detailed design, integration, certification and certification test support. Support in generation and review of fatigue test plan (full scale and component level test), interpretation of test results and correlation with analysis in the test report. Level II and level III checker approver signatory for F&DT analysis certification reports, F&DT test plan, test orders and F&DT test reports. Lead root cause investigations, risk assessments, and resolution strategies for stress/F&DT related issues, non-conformances, schedule variance and airworthiness deviations. Finalize the F&DT technical requirements, limitations and associated tasks within defined timelines, ensuring high-quality output with minimal errors. Analyse complex design challenges and propose optimal engineering solutions aligned with project goals and constraints. Provide high level competency for the fatigue spectrum derivation for analysis and the subsequent service load and the test load spectrum derivation. Document the procedure as a signed document for reference. Supervision and approval of method register, F&DT method document, Analysis tools alignment, F&DT certification analysis check lists, certification test report templates and SLA in alignment with client during the initial execution phase. Act as the technical voice of the program, aligning customer expectations with engineering deliverables and strategic goals. Drive end-to-end scope definition, requirements management, and traceability across the engineering structural lifecycle related to F&DT justification. Ensure effective planning, milestone tracking, and schedule variance analysis to maintain alignment with program delivery goals and importantly internal deal construct parameters or solution baselines. Lead effective engineering change management by proactively tracking evolving inputs and shifting requirements. Evaluate and mitigate the impact of delays on schedule variance, resource planning, costs, and milestone achievement through a structured change control process aligned with client approvals and established governance protocols. Represent engineering during customer technical audits, program quality gate reviews, and change control reviews. Ensure engineering activities meet cost, schedule, target weight and performance objectives while maintaining traceability and regulatory compliance. Act as the primary technical/program level interface with the client, ensuring alignment on F&DT compliance objectives and deliverables. Professional & Technical Skills:Expertise in design, development, and integration of metallic and composite helicopter/aircraft structures (primary and secondary) from F&DT perspective. Experience with static and F&DT analysis for sizing large fixed or rotary wing aircraft. Skilled in weight and load path optimization, fatigue, and damage tolerance for certification and testing. Strong knowledge of airworthiness regulations (CS-27/29, FAR 23/25), OEM standards, and FAA/EASA certification. Experienced in test plan preparation, test orders, load derivation, and test-to-analysis correlation for component and full-scale tests. Familiar with certification testing, life extension, and fatigue-resistant structure design. Knowledge of GD&T and drawing standards is a plus. Proficient in FEA and F&DT tools is essential with experience in NASGRO FRANC 3D MSC FATIGUE, MSC NASTRAN/PATRAN, HyperMesh/Optistruct. or similar tools is a strong plus. Can guide the team for automation using Excel MACROS & VBA Python and Catia V5 is a plusDeep understanding of aircraft materials, fatigue, fracture mechanics, fatigue spectrum derivation, and probabilistic crack growth assessment. Familiar with FEA considerations and meshing for F&DT analysis. Experience from concept through design validation, manufacturability, certification, and F&DT test correlation, preferably for rotary wing aircraft. Strong knowledge of helicopter/aircraft load-bearing structures, focusing on integrity, stiffness, and load path optimization under static and fatigue loads. Awareness of failure modes in metallic and composite airframe parts. Skilled in structural classification, F&DT compliance, calculation points, down-selection, and scatter factor selection. Proven expertise in low and high cycle fatigue analysis for fixed or rotary wing aircraft. Acoustics and noise separation knowledge is a plus. Competent in structural sizing to meet certification, test, and manufacturability requirements. Proven experience in static and F&DT sizing for design and integration of rotary-wing and/or fixed-wing aircraft structures across end-to-end design lifecycle phases. Demonstrated experience collaborating with cross-functional teamsincluding design, stress analysis, manufacturing, systems and qualitywithin complex delivery frameworks for aerostructure development programs. Additional Information:- The candidate should have minimum 15 years of engineering experience in the Aerostructures F&DT domain preferably for the rotary wing aircrafts, technical managerial & program manager role for OEM/service providers. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering 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 : Aircraft Structural Analysis Good to have skills : NA Minimum 5 year(s) of experience is required Educational Qualification : 15 years full time education Summary : As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities: You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Design and develop primary and secondary structural componentsboth metallic and compositefor rotary-wing aircraft, ensuring compliance with airworthiness regulations, structural integrity requirements, and OEM-specific design standards. Understand the meshing and analysis guidelines for static, dynamic and impact analysis and ensure the FE models created by team are complied to the guidelines and are of high quality. Ensure that the V&V documents capture the required checks for the FE models. Also ensure the physics of the problem is correctly simulated in the FE models and if required use your expertise and guidance to align with the requirements. Ensure alignment and compliance to the client specific and regulatory guidelines as per FAR 27/29CS/JAR/Military MIL-STD-1530 etc Enable team engagements and knowledge sharing for distributed teams across the programs and locations. Validate the design of structural through Classical and FE Analysis, and assist in detailed load path analysis, optimal material selection based on Analysis results and operational design environmental conditions. Owning optimum design by static stress analysis Dynamic analysis and impact analysis evaluation of multiple structural design concepts through detailed trade-off analyses. Develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Perform weight estimation, its tracking, and control across all design phases, ensuring alignment with weight budgets and performance criteria. Technically lead and guide the team for mitigating the low RF Low life and performance non-compliance issues. Create the test FE models incorporating the failure, features and boundary conditions as per standard procedure and test fixture. Creating the method register, Method document, check lists and report templates in compliance with regulatory and client specific requirements. Front end and act as the technical interface with the client, ensuring alignment on deviations and processes, methods, inputs, overall objectives and deliverables. Interact with clients on a regular basis to track and classify the issues and ensure timely resolution of the issues as per SLA. Assist in during customer technical audits, program quality gate reviews, and change control reviews. Support and mentor junior team members by providing technical guidance, sharing best practices, and fostering their growth in design methodologies, tools, and domain knowledge. Actively contributes to skill development, knowledge transfer, and team capability building through hands-on support and constructive feedback. Professional & Technical Skills: Expertise in the design/development and integration of metallic, sheet metal, and composite helicopter aircraft structures for both primary and secondary components from Static point of view. Experience of static dynamic and impact analysis for sizing of large, fixed wing or rotary wing aircraft. Experience in weight optimization techniques, load path optimization for helicopter/aircraft certification and testing activities. Any experience in process automation using MS excel VBA/Python etc Strong knowledge of airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Experience in preparation of full scale and component level certification test plan, test orders, test load derivation and test to analysis correlation reports for component level for fixed wing or rotary wing aircrafts. Certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with GD & T and drawing standards. Proficiency over the structural static dynamic and impact analysis tools like general MSC NASTRAN/PATRAN/ABAQUS/ HyperMesh/ OptistructLS DYANA is must, Automation experience using Excel MACROS & VBA Python and Catia V5 is a plus. FEA considerations and meshing requirements for different types of structural analyses like static, dynamic, buckling and impact analyses. End to end validation, certification compliance, manufacturing support and certification test & test correlation activities specifically for rotary wing aircraft helicopter. High level skills and experience in the 2D/3D mesh creation and meshing guidelines, FE Modelling, and Assembly integration methodologies. Experience of aerospace material selection, structural feature simulation, analyses and meshing guidelines and procedures. Capability to solve day to day analysis problem in Analysis and post processing of Analysis results. Sound knowledge of helicopter/aircraft load-bearing structures, with focus on structural integrity, stiffness, and load path optimization under both static, dynamic, and impact conditions. Familiarity with Fatigue requirement is plus. High experience aligned with the rotary wing or fixed wing structural arrangement, primary, secondary and support structures, load path, sizing procedures for metallic and composite structures. Strong awareness of static dynamic and impact strength justification analyses and failure modes relevant to metallic and composite airframe components. Introductory knowledge about the analysis considerations for the any of the Innovative design and functional considerations like telescopic structures, foldability swivel and reversal of structure. Expertise for structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Familiar with structural analysis considerations related to assembly line constraints, ergonomic considerations, and sequence planning to ensure seamless integration in high-rate production environments. Additional Information:- The candidate should have a 8 to 9 years of practical experience static analysis/Dynamic analysis/ Impact Analysis in the Aerostructures domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering 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 : Aircraft Structural Analysis Good to have skills : NA Minimum 7.5 year(s) of experience is required Educational Qualification : 15 years full time education Summary : As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities: Join a mid-level leadership role within the Aerostructure Engineering team, supporting both strategy and technical execution across the full engineering lifecyclefrom concept through production, certification, and sustainment. Play a pivotal role in leading engineering delivery, technical governance, and client interactions for high-impact aerospace programs spanning rotary- and fixed-wing platforms. Opportunity to drive digital engineering initiatives including MBD, MBSE, and digital twin integration within legacy and next-gen design environments. Own design and development tasks for aircraft structural components. Apply advanced aircraft structural analyses Approach to Validate the design concepts through Classical and FE Analysis, and assist in detailed load path analysis, optimal material selection and operational design environmental conditions compliant to the airworthiness regulations, structural integrity requirements, and OEM-specific design standards. Preparation of method register, Method document, check lists, report templates, SLA in alignment with client. Guide the team for selection of optimum design by stress evaluation of multiple structural design concepts through detailed trade-off analyses for required dimensions and weight constraints. Maintaining scope requirement log, Input enabler and query trackers and coordinating with respective client stakeholders to get the resolutions on-time, ensuring high-quality output. Lead the team to develop complex 2D and 3D FE models, their integration, properties allocation, create validation and verification reports for the FE models, Analysis deck preparation/editing, perform structural Analyses, result extraction and interpretations, Error removal, post process and assist in developing automation using inhouse macros. Finalize the meshing and analyses requirements for different types of structural analyses in alignment with client. Mitigation in case of low RF/MOS, Alternative concepts analyses, compilation of inputs for the review and certification reports. Analyse complex design challenges and propose optimal engineering solutions. Level II and Level III checker and signatory for the analysis and certification reports from Accenture side. Certification test support creation of FE models incorporating the failure, features and boundary conditions as per standard procedure and test fixture. Ensuring alignment with weight budgets and performance criteria. Collaborate and lead cross-functionally with design team, manufacturing, quality, and systems teams; actively engage in design reviews, issue resolution, and integration discussions. Act as the primary technical interface with the client, ensuring alignment on design objectives and deliverables. Support and mentor junior team members by providing technical guidance, sharing best practices, and fostering their growth in design methodologies, tools, and domain knowledge. Actively contributes to skill development, knowledge transfer, and team capability building through hands-on support and constructive feedback. Professional & Technical Skills: Expertise in the design, development and integration of metallic, and composite helicopter aircraft structures for both primary and secondary components from static Dynamic/ Impact point of view. Experience of static dynamic and impact analysis for sizing of large, fixed wing or rotary wing aircraft. Experience in weight optimization techniques, load path optimization for helicopter/aircraft certification and testing activities. Working knowledge of airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Experience in preparation of full scale and component level certification test plan, test orders, test load derivation and test to analysis correlation reports for component level for fixed wing or rotary wing aircrafts. Familiarity with GD&T and industry drawing standards, Proficiency over the structural static dynamic and impact analysis tools like general MSC NASTRAN/PATRAN/ABAQUS/ HyperMesh/ OptistructLS DYANA is must, Can guide the team for automation using Excel MACROS & VBA Python and Catia V5 is a plus. FEA considerations and meshing requirements for different types of structural analyses like static, dynamic, buckling and impact analysis. End to end concept to design validation, certification, manufacturing support and certification test & test correlation activities specifically for rotary wing aircraft helicopter. Command over the 2D/3D mesh creation and meshing guidelines, FE Modelling, and Assembly integration methodologies. Strong grasp of aerospace material selection, structural feature simulation, analyses and meshing guidelines and procedures. Capability to solve day to day analysis problem in Analysis and post processing of Analysis results. In-depth understanding of helicopter/aircraft load-bearing structures, with focus on structural integrity, stiffness, and load path optimization under both static, dynamic, and impact conditions. Familiarity with Fatigue requirement is plus. Deep knowledge of rotary wing or fixed wing structural arrangement, primary, secondary and support structures, load path, sizing procedures for metallic and composite structures. Strong awareness of static dynamic and impact strength justification analyses and failure modes relevant to metallic and composite airframe components. Analysis considerations for the any of the Innovative design and functional considerations like telescopic structures, foldability swivel and reversal of structure. Expertise for structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Familiar with structural analysis considerations related to assembly line constraints, ergonomic considerations, and sequence planning to ensure seamless integration in high-rate production environments. Additional Information:- The candidate should have a 12 to 15 years of experience in the Aerostructure Analysis domain preferably for the rotary wing aircrafts, in a technical managerial & program manager role for OEM/service providers. This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering 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 : NA Minimum 12 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:Lead strategic aerospace engineering engagements for rotary wing platforms, driving technical delivery, innovation, and client satisfaction. Play a key role in shaping engineering processes, delivery governance, and team capability development. Engage directly with aerospace OEMs, Tier-1 suppliers and regulatory bodies, influencing design decisions, compliance strategies, and product lifecycle outcomes. Drive digital engineering transformation, championing initiatives around MBSE, MBD, and digital continuity. Lead and oversee the execution of comprehensive fatigue and damage tolerance analysis for metallic and composite structural parts related to design and development of rotary wing aircrafts primary and secondary structures. Guide the team with interpretation of static analysis results for defining the fatigue critical location, number of calculation points, fatigue sensitive area, primary and secondary load path identification, design philosophy identification, scatter factor selection in alignment with client and regulatory guidelines FAR/CS 25.571, 29.571, MIL-STD-1530 etc. Establish and govern engineering F&DT analysis best practices, design review frameworks, and technical quality gates across the program lifecycle. Provide technical oversight related to F&DT across multiple concept development, structural architecture, F&DT requirement compliance for detailed design, integration, certification and certification test support. Support in generation and review of fatigue test plan (full scale and component level test), interpretation of test results and correlation with analysis in the test report. Level II and level III checker approver signatory for F&DT analysis certification reports, F&DT test plan, test orders and F&DT test reports. Lead root cause investigations, risk assessments, and resolution strategies for stress/F&DT related issues, non-conformances, schedule variance and airworthiness deviations. Finalize the F&DT technical requirements, limitations and associated tasks within defined timelines, ensuring high-quality output with minimal errors. Analyse complex design challenges and propose optimal engineering solutions aligned with project goals and constraints. Provide high level competency for the fatigue spectrum derivation for analysis and the subsequent service load and the test load spectrum derivation. Document the procedure as a signed document for reference. Supervision and approval of method register, F&DT method document, Analysis tools alignment, F&DT certification analysis check lists, certification test report templates and SLA in alignment with client during the initial execution phase. Act as the technical voice of the program, aligning customer expectations with engineering deliverables and strategic goals. Drive end-to-end scope definition, requirements management, and traceability across the engineering structural lifecycle related to F&DT justification. Ensure effective planning, milestone tracking, and schedule variance analysis to maintain alignment with program delivery goals and importantly internal deal construct parameters or solution baselines. Lead effective engineering change management by proactively tracking evolving inputs and shifting requirements. Evaluate and mitigate the impact of delays on schedule variance, resource planning, costs, and milestone achievement through a structured change control process aligned with client approvals and established governance protocols. Represent engineering during customer technical audits, program quality gate reviews, and change control reviews. Ensure engineering activities meet cost, schedule, target weight and performance objectives while maintaining traceability and regulatory compliance. Act as the primary technical/program level interface with the client, ensuring alignment on F&DT compliance objectives and deliverables. Professional & Technical Skills:Expertise in design, development, and integration of metallic and composite helicopter/aircraft structures (primary and secondary) from F&DT perspective. Experience with static and F&DT analysis for sizing large fixed or rotary wing aircraft. Skilled in weight and load path optimization, fatigue, and damage tolerance for certification and testing. Strong knowledge of airworthiness regulations (CS-27/29, FAR 23/25), OEM standards, and FAA/EASA certification. Experienced in test plan preparation, test orders, load derivation, and test-to-analysis correlation for component and full-scale tests. Familiar with certification testing, life extension, and fatigue-resistant structure design. Knowledge of GD&T and drawing standards is a plus. Proficient in FEA and F&DT tools is essential with experience in NASGRO FRANC 3D MSC FATIGUE, MSC NASTRAN/PATRAN, HyperMesh/Optistruct. or similar tools is a strong plus. Can guide the team for automation using Excel MACROS & VBA Python and Catia V5 is a plusDeep understanding of aircraft materials, fatigue, fracture mechanics, fatigue spectrum derivation, and probabilistic crack growth assessment. Familiar with FEA considerations and meshing for F&DT analysis. Experience from concept through design validation, manufacturability, certification, and F&DT test correlation, preferably for rotary wing aircraft. Strong knowledge of helicopter/aircraft load-bearing structures, focusing on integrity, stiffness, and load path optimization under static and fatigue loads. Awareness of failure modes in metallic and composite airframe parts. Skilled in structural classification, F&DT compliance, calculation points, down-selection, and scatter factor selection. Proven expertise in low and high cycle fatigue analysis for fixed or rotary wing aircraft. Acoustics and noise separation knowledge is a plus. Competent in structural sizing to meet certification, test, and manufacturability requirements. Proven experience in static and F&DT sizing for design and integration of rotary-wing and/or fixed-wing aircraft structures across end-to-end design lifecycle phases. Demonstrated experience collaborating with cross-functional teamsincluding design, stress analysis, manufacturing, systems and qualitywithin complex delivery frameworks for aerostructure development programs. Additional Information:- The candidate should have minimum 15 years of engineering experience in the Aerostructures F&DT domain preferably for the rotary wing aircrafts, technical managerial & program manager role for OEM/service providers. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Qualification 15 years full time education

Job Description 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 : NA Minimum 3 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Design and develop primary and secondary structural componentsboth metallic and compositefor rotary-wing aircraft, ensuring compliance with airworthiness regulations, structural integrity requirements, and OEM-specific design standards. Use meshing and analysis guidelines for static, dynamic and impact analysis and ensure the FE models created by team are compiled to the guidelines and are of high quality. Perform the checks and prepare FEA V&V documents, capture the required checks for the FE models. Also ensure the physics of the problem is correctly simulated in the FE models and if required use your expertise and guidance to align with the requirements. Perform FEA analysis for static dynamic and impact analysis in alignment and compliance to the client specific and regulatory guidelines as per FAR 27/29CS/JAR/Military MIL-STD-1530 etc Take up team engagements and knowledge sharing sessions for distributed teams across the programs and locations. Design validation of structural through Classical and FE Analysis, and assist in detailed load path analysis, optimal material selection based on Analysis results and operational design environmental conditions. Document the details for presenting into the certification reports and certifying agencies. Provide supporting evidence for the selection of optimum design by static stress analysis Dynamic analysis and impact analysis evaluation of multiple structural design concepts through detailed trade-off analyses. Comply to schedule, weight requirement and cost compliance by efficiently tracking methods. Follow escalation mechanism to ensure compliance. Develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Provide analysis results for the decision process of selection of reliable concepts out of multiple concepts based on the static, dynamic and impact stress analysis validation with future operational and maintenance and repair considerations. Provide details from FE models for the weight estimation, its tracking, and control across all design phases, ensuring alignment with weight budgets and performance criteria. Perform the task of mitigating the low RF Low life and performance non-compliance issues based on discussion with SME/Leads or your expertise and experience. Align relevant details of these methods to SME/Leads to align with the client. Documentation of iterations and outcomes for future reference. Create the test FE models incorporating the failure, features and boundary conditions as per standard procedure and test fixture. Design validate through analysis or classical calculations the Incorporated features and design aspects covering the downstream manufacturing and inspection processes, accessibility and in-service replacement/repair. Prepare detailed presentation for reference and review. Assist in during customer technical audits, program quality gate reviews, and change control reviews by providing the required analysis results and justifications. Professional & Technical Skills:Experience with Aerospace projects for the design/development and integration of metallic, and composite helicopter aircraft structures for both primary and secondary components. Knowledge of Aerospace structures, their classification as primary, secondary and support structures based on load bearing capacities. Experience of static dynamic and impact analysis for sizing of large, fixed-wing or rotary wing aircraft for major OEMs. Exposure to weight optimization techniques, load path optimization for helicopter/aircraft certification and testing activities. Experience in process automation using MS excel VBA/Python etc Exposure to airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Knowledge of Preparation of full scale and component level certification test plan, test orders, test load derivation and test to analysis correlation reports for component level for fixed wing or rotary wing aircrafts. Knowledge of certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with drawing standards. Proficiency over the structural static dynamic and impact analysis tools like general MSC NASTRAN/PATRAN/ABAQUS/ HyperMesh/ OptistructLS DYANA is must, Automation experience using Excel MACROS & VBA Python and Catia V5 is a plus. FEA considerations and meshing requirements for different types of structural analyses like static, dynamic, buckling and impact analyses. FEA V&V methods, analysis as per the certification compliance, manufacturing support and certification. Create inputs for the test & test correlation activities specifically for rotary wing aircraft helicopter. Experience in the 2D/3D mesh creation and meshing guidelines, FE Modelling, and Assembly integration methodologies. Experience of aerospace material, structural feature simulation, analyses as per meshing guidelines and procedures. Capability to solve day to day analysis problem in Analysis, analysis error and post processing of Analysis results. knowledge of helicopter/aircraft load-bearing structures Experience aligned with the rotary wing or fixed wing structural arrangement, primary, secondary and support structures, load path, sizing procedures for metallic and composite structures. Familiarity with Fatigue requirement is plus. Experience in static dynamic and impact strength justification analyses and failure modes relevant to metallic and composite airframe components. Exposure to Innovative design and functional considerations like telescopic structures, foldability swivel and reversal of structure. Knowledge of structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Additional Information:- The candidate should have a 5 to 8 years of practical experience static analysis/Dynamic analysis/ Impact Analysis in the Aerostructures domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Qualification 15 years full time education

Job Description 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 : NA Minimum 5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Design and develop primary and secondary structural componentsboth metallic and compositefor rotary-wing aircraft, ensuring compliance with airworthiness regulations, structural integrity requirements, and OEM-specific design standards. Understand the meshing and analysis guidelines for static, dynamic and impact analysis and ensure the FE models created by team are complied to the guidelines and are of high quality. Ensure that the V&V documents capture the required checks for the FE models. Also ensure the physics of the problem is correctly simulated in the FE models and if required use your expertise and guidance to align with the requirements. Ensure alignment and compliance to the client specific and regulatory guidelines as per FAR 27/29CS/JAR/Military MIL-STD-1530 etc Enable team engagements and knowledge sharing for distributed teams across the programs and locations. Validate the design of structural through Classical and FE Analysis, and assist in detailed load path analysis, optimal material selection based on Analysis results and operational design environmental conditions. Owning optimum design by static stress analysis Dynamic analysis and impact analysis evaluation of multiple structural design concepts through detailed trade-off analyses. Develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Perform weight estimation, its tracking, and control across all design phases, ensuring alignment with weight budgets and performance criteria. Technically lead and guide the team for mitigating the low RF Low life and performance non-compliance issues. Create the test FE models incorporating the failure, features and boundary conditions as per standard procedure and test fixture. Creating the method register, Method document, check lists and report templates in compliance with regulatory and client specific requirements. Front end and act as the technical interface with the client, ensuring alignment on deviations and processes, methods, inputs, overall objectives and deliverables. Interact with clients on a regular basis to track and classify the issues and ensure timely resolution of the issues as per SLA. Assist in during customer technical audits, program quality gate reviews, and change control reviews. Support and mentor junior team members by providing technical guidance, sharing best practices, and fostering their growth in design methodologies, tools, and domain knowledge. Actively contributes to skill development, knowledge transfer, and team capability building through hands-on support and constructive feedback. Professional & Technical Skills:Expertise in the design/development and integration of metallic, sheet metal, and composite helicopter aircraft structures for both primary and secondary components from Static point of view. Experience of static dynamic and impact analysis for sizing of large, fixed wing or rotary wing aircraft. Experience in weight optimization techniques, load path optimization for helicopter/aircraft certification and testing activities. Any experience in process automation using MS excel VBA/Python etc Strong knowledge of airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Experience in preparation of full scale and component level certification test plan, test orders, test load derivation and test to analysis correlation reports for component level for fixed wing or rotary wing aircrafts. Certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with GD & T and drawing standards. Proficiency over the structural static dynamic and impact analysis tools like general MSC NASTRAN/PATRAN/ABAQUS/ HyperMesh/ OptistructLS DYANA is must, Automation experience using Excel MACROS & VBA Python and Catia V5 is a plus. FEA considerations and meshing requirements for different types of structural analyses like static, dynamic, buckling and impact analyses. End to end validation, certification compliance, manufacturing support and certification test & test correlation activities specifically for rotary wing aircraft helicopter. High level skills and experience in the 2D/3D mesh creation and meshing guidelines, FE Modelling, and Assembly integration methodologies. Experience of aerospace material selection, structural feature simulation, analyses and meshing guidelines and procedures. Capability to solve day to day analysis problem in Analysis and post processing of Analysis results. Sound knowledge of helicopter/aircraft load-bearing structures, with focus on structural integrity, stiffness, and load path optimization under both static, dynamic, and impact conditions. Familiarity with Fatigue requirement is plus. High experience aligned with the rotary wing or fixed wing structural arrangement, primary, secondary and support structures, load path, sizing procedures for metallic and composite structures. Strong awareness of static dynamic and impact strength justification analyses and failure modes relevant to metallic and composite airframe components. Introductory knowledge about the analysis considerations for the any of the Innovative design and functional considerations like telescopic structures, foldability swivel and reversal of structure. Expertise for structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Familiar with structural analysis considerations related to assembly line constraints, ergonomic considerations, and sequence planning to ensure seamless integration in high-rate production environments. Additional Information:- The candidate should have a 8 to 9 years of practical experience static analysis/Dynamic analysis/ Impact Analysis in the Aerostructures domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Qualification 15 years full time education

Job Description 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 : NA Minimum 3 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Design and develop primary and secondary structural componentsboth metallic and compositefor rotary-wing aircraft, ensuring compliance with airworthiness regulations, structural integrity requirements, and OEM-specific design standards. Use meshing and analysis guidelines for static, dynamic and impact analysis and ensure the FE models created by team are compiled to the guidelines and are of high quality. Perform the checks and prepare FEA V&V documents, capture the required checks for the FE models. Also ensure the physics of the problem is correctly simulated in the FE models and if required use your expertise and guidance to align with the requirements. Perform FEA analysis for static dynamic and impact analysis in alignment and compliance to the client specific and regulatory guidelines as per FAR 27/29CS/JAR/Military MIL-STD-1530 etc Take up team engagements and knowledge sharing sessions for distributed teams across the programs and locations. Design validation of structural through Classical and FE Analysis, and assist in detailed load path analysis, optimal material selection based on Analysis results and operational design environmental conditions. Document the details for presenting into the certification reports and certifying agencies. Provide supporting evidence for the selection of optimum design by static stress analysis Dynamic analysis and impact analysis evaluation of multiple structural design concepts through detailed trade-off analyses. Comply to schedule, weight requirement and cost compliance by efficiently tracking methods. Follow escalation mechanism to ensure compliance. Develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Provide analysis results for the decision process of selection of reliable concepts out of multiple concepts based on the static, dynamic and impact stress analysis validation with future operational and maintenance and repair considerations. Provide details from FE models for the weight estimation, its tracking, and control across all design phases, ensuring alignment with weight budgets and performance criteria. Perform the task of mitigating the low RF Low life and performance non-compliance issues based on discussion with SME/Leads or your expertise and experience. Align relevant details of these methods to SME/Leads to align with the client. Documentation of iterations and outcomes for future reference. Create the test FE models incorporating the failure, features and boundary conditions as per standard procedure and test fixture. Design validate through analysis or classical calculations the Incorporated features and design aspects covering the downstream manufacturing and inspection processes, accessibility and in-service replacement/repair. Prepare detailed presentation for reference and review. Assist in during customer technical audits, program quality gate reviews, and change control reviews by providing the required analysis results and justifications. Professional & Technical Skills:Experience with Aerospace projects for the design/development and integration of metallic, and composite helicopter aircraft structures for both primary and secondary components. Knowledge of Aerospace structures, their classification as primary, secondary and support structures based on load bearing capacities. Experience of static dynamic and impact analysis for sizing of large, fixed-wing or rotary wing aircraft for major OEMs. Exposure to weight optimization techniques, load path optimization for helicopter/aircraft certification and testing activities. Experience in process automation using MS excel VBA/Python etc Exposure to airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Knowledge of Preparation of full scale and component level certification test plan, test orders, test load derivation and test to analysis correlation reports for component level for fixed wing or rotary wing aircrafts. Knowledge of certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with drawing standards. Proficiency over the structural static dynamic and impact analysis tools like general MSC NASTRAN/PATRAN/ABAQUS/ HyperMesh/ OptistructLS DYANA is must, Automation experience using Excel MACROS & VBA Python and Catia V5 is a plus. FEA considerations and meshing requirements for different types of structural analyses like static, dynamic, buckling and impact analyses. FEA V&V methods, analysis as per the certification compliance, manufacturing support and certification. Create inputs for the test & test correlation activities specifically for rotary wing aircraft helicopter. Experience in the 2D/3D mesh creation and meshing guidelines, FE Modelling, and Assembly integration methodologies. Experience of aerospace material, structural feature simulation, analyses as per meshing guidelines and procedures. Capability to solve day to day analysis problem in Analysis, analysis error and post processing of Analysis results. knowledge of helicopter/aircraft load-bearing structures Experience aligned with the rotary wing or fixed wing structural arrangement, primary, secondary and support structures, load path, sizing procedures for metallic and composite structures. Familiarity with Fatigue requirement is plus. Experience in static dynamic and impact strength justification analyses and failure modes relevant to metallic and composite airframe components. Exposure to Innovative design and functional considerations like telescopic structures, foldability swivel and reversal of structure. Knowledge of structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Additional Information:- The candidate should have a 5 to 8 years of practical experience static analysis/Dynamic analysis/ Impact Analysis in the Aerostructures domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering 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 2 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Support in the design validation through static dynamic and impact analysis of rotary wing aircraft structural components. Work under the guidance of the Lead Engineer to develop complex 2D and 3D FE models, their integration, properties allocation, validation and verification of FE models, Analysis deck preparation/editing, perform different structural Analyses, result extraction and post processing using inhouse macros. Use meshing and analysis guidelines for static, dynamic and impact analysis FE model creation and ensure the FE models created by team are compiled to the guidelines and are of high quality. Perform the checks and prepare FEA V&V documents, capture the required checks for the FE models. Also ensure the physics of the problem is correctly simulated in the FE models and if required use your expertise and guidance to align with the requirements. Perform the required analyses task under supervision for the low RF/MOS mitigation, Alternative concepts analyses, creation of inputs for the review and certification reports. Address design challenges and implement the proposed optimal engineering solutions aligned with project goals and constraints. Apply basic principles of aerospace structures design /sizing and material selection. Interpret technical requirements and execute assigned tasks within defined timelines, ensuring high-quality output with minimal errors. Assist in interpreting technical requirements and validate it through justification analyses. Participate in design reviews and incorporate feedback into iterative improvements. Collaborate with cross-functional teams to ensure alignment with structural and performance goals. Engage in training sessions to enhance technical knowledge and skillsets relevant to the role. Professional & Technical Skills: Good experience of 2D/3D mesh creation and meshing guidelines, FE Modeling, and Assembly integration methodologies. Experience of static dynamic and impact analysis for sizing of large, fixed-wing or rotary wing aircraft for major OEMs. Knowledge of classical hand calculations for simple structural parts Command over MSC NASTRAN/PATRAN/ Hypermesh/ Optistruct is must F&DT knowledge, Excel MACROS using VBA / Python and Catia V5 is a plus Understanding of Engineering Drawings and Analysis data extraction from CAD models. Must have knowledge of structural classification, primary and secondary structure design requirements, load path and structural response Additional Information:- The candidate should have a 2 to 4 years of experience in the Aerostructure Analysis domain. This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering 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 : Fatigue & Damage Tolerance F&DT Good to have skills : NAMinimum 2 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Support in the design validation through static dynamic and impact analysis of rotary wing aircraft structural components. Work under the guidance of the Lead Engineer to develop complex 2D and 3D FE models to be used for the fatigue evaluations, their integration, properties allocation, validation and verification of FE models, Analysis deck preparation/editing, perform different structural Analyses, result extraction and post processing using inhouse macros. Use meshing and analysis guidelines for fatigue and DT analysis FE model creation and ensure the FE models created by team are compiled to the guidelines and are of high quality. Perform the checks and prepare FEA V&V documents, capture the required checks for the FE models. Also ensure the physics of the problem as applicable for the fatigue life and crack growth estimations is correctly simulated in the FE models and if required use your expertise and guidance to align with the requirements. Perform the required analyses task under supervision for the low LIFE/RF/MOS mitigation, Alternative concepts analyses, creation of inputs for the review and certification reports. Use Excel macros and program codes to extract and post process the required data from FEA output files for further F&DT evaluation. Address design challenges and implement the proposed optimal engineering solutions aligned with project goals and constraints. Apply basic principles of aerospace structures design /sizing and material selection to meet the project goals. Familiarize with the structural classification, primary and secondary structure design requirements, load path and structural response. Interpret technical requirements and execute assigned tasks within defined timelines, ensuring high-quality output with minimal errors. Assist in interpreting technical requirements and validate it through justification analyses. Participate in design reviews and incorporate feedback into iterative improvements. Participate in the cross-functional teams to ensure alignment with structural and performance goals. Engage in training sessions to enhance technical knowledge and skillsets relevant to the role. Professional & Technical Skills: Technical Skills: Strong command over the 2D/3D mesh creation and meshing guidelines, FE Modeling, and Assembly integration methodologies. Command over MSC NASTRAN/PATRAN/ HyperMesh/ Optistruct is must and F&DT knowledge, Excel MACROS using VBA / Python and Catia V5 is a plus Understanding of Engineering Drawings and Analysis data extraction from CAD models. Professional Attributes:Self-motivated, quick to learn, well-organized, and capable of independently planning and executing tasks with minimal supervision. Additional Information:- The candidate should have 2 to 4 years of experience in the Aerostructure Analysis domain. This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering 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 : Fatigue & Damage Tolerance F&DT Good to have skills : NAMinimum 7.5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:Join a mid-level leadership role within the Aerostructure Engineering team, supporting both strategy and technical execution across the full engineering lifecyclefrom concept through production, certification, and sustainment. Play a pivotal role in leading engineering delivery, technical governance, and client interactions for high-impact aerospace programs spanning rotary- and fixed-wing platforms. Opportunity to drive digital engineering initiatives including MBD, MBSE, and digital twin integration within legacy and next-gen design environments. Lead fatigue and damage tolerance (F&DT) analysis for metallic/composite parts in primary and secondary rotary wing structures. Guide interpretation of static analysis to define fatigue-critical areas, calc points, load paths, design intent, and scatter factors per FAR/CS 25.571/29.571, MIL-STD-1530, etc. Prepare method registers, F&DT documents, tool alignment, certification checklists, test report templates, and SLAs per scope and client needs. Manage project scope, constraints, and alignments with client during project initiation. Apply standard F&DT methods and best practices, documenting limitations based on NDE/NDI, manufacturing constraints, and design criteria. Provide expertise in deriving fatigue and test load spectra and formalize via documented procedures. Offer technical oversight across concept design, structural layout, compliance checks, integration, certification, and test phases. Support fatigue test plan creation (full/component level), test result interpretation, and correlation; review team outputs. Act as Level II/III checker, approver, and signatory for F&DT analysis, plans, test orders, and reports. Lead root cause investigations, risk assessments, and resolution of stress/F&DT issues, non-conformances, and airworthiness gaps. Analyze complex design issues and recommend optimal engineering solutions aligned with program goals. Support delivery manager and act as the technical voice of the program, enable aligning customer expectations with engineering deliverables and strategic goals. Front face Accenture in all technical discussions and lead the discussion. Drive end-to-end scope definition, requirements management, and traceability across the engineering structural lifecycle related to F&DT justification. Ensure effective planning, milestone tracking, and schedule variance analysis to maintain alignment with program delivery goals and importantly internal deal construct parameters or solution baselines. Drive robust engineering change management by closely monitoring evolving inputs and requirement changes. Assess and manage the impact of delays on schedule variance, resource allocation, cost, and milestone delivery through a structured change control process aligned with client approvals and governance protocols. Ensure engineering activities meet cost, schedule, target weight and performance objectives while maintaining traceability and regulatory compliance. Collaborate and lead cross-functionally with design/analysis team, manufacturing, quality, and systems teams; actively engage in design reviews, issue resolution, and integration discussions. Act as the technical interface with the client, ensuring alignment of F&DT compliance objectives and deliverables. Professional & Technical Skills: Expertise in design, development, and integration of metallic and composite helicopter/aircraft structures (primary and secondary) from F&DT perspective. Experience with static and F&DT analysis for sizing large fixed or rotary wing aircraft. Skilled in weight and load path optimization, fatigue, and damage tolerance for certification and testing. Strong knowledge of airworthiness regulations (CS-27/29, FAR 23/25), OEM standards, and FAA/EASA certification. Experienced in test plan preparation, test orders, load derivation, and test-to-analysis correlation for component and full-scale tests. Familiar with certification testing, life extension, and fatigue-resistant structure design. Knowledge of GD&T and drawing standards is a plus. Proficient in FEA and F&DT tools is essential with experience in NASGRO / FRANC 3D / MSC FATIGUE, MSC NASTRAN/PATRAN, HyperMesh/Optistruct. or similar tools is a strong plus. Can guide the team for automation using Excel MACROS & VBA / Python and Catia V5 is a plusDeep understanding of aircraft materials, fatigue, fracture mechanics, fatigue spectrum derivation, and probabilistic crack growth assessment. Familiar with FEA considerations and meshing for F&DT analysis. Experience from concept through design validation, manufacturability, certification, and F&DT test correlation, preferably for rotary wing aircraft. Strong knowledge of helicopter/aircraft load-bearing structures, focusing on integrity, stiffness, and load path optimization under static and fatigue loads. Awareness of failure modes in metallic and composite airframe parts. Skilled in structural classification, F&DT compliance, calculation points, down-selection, and scatter factor selection. Proven expertise in low and high cycle fatigue analysis for fixed or rotary wing aircraft. Acoustics and noise separation knowledge is a plus. Competent in structural sizing to meet certification, test, and manufacturability requirements. Proven experience in static and F&DT sizing for design and integration of rotary-wing and/or fixed-wing aircraft structures across end-to-end design lifecycle phases. Demonstrated experience collaborating with cross-functional teamsincluding design, stress analysis, manufacturing, systems and qualitywithin complex delivery frameworks for aerostructure development programs. Additional Information:- The candidate should have 12 to 15 years of engineering experience in the Aerostructures F&DT domain preferably for the rotary wing aircrafts, technical managerial & program manager role for OEM/service providers. This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering 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 12 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:Lead strategic aerospace engineering engagements for rotary wing platforms, driving technical delivery, innovation, and client satisfaction. Play a key role in shaping engineering processes, delivery governance, and team capability development. Engage directly with aerospace OEMs, Tier-1 suppliers and regulatory bodies, influencing design decisions, compliance strategies, and product lifecycle outcomes. Drive digital engineering transformation, championing initiatives around MBSE, MBD, and digital continuity. Oversee static, dynamic, and impact sizing analysis for primary/secondary rotary wing structures. Establish engineering best practices, review frameworks, and quality gates. Provide oversight across concept development, stress validation, integration, and certification. Plan analysis/test requirements for metallic and composite materials, ensuring structural integrity and compliance. Act as Level II/III checker or approver for analysis reports and test documentation. Integrate cost, weight, safety, and manufacturability into design lifecycles. Lead root cause investigations, risk assessments, and corrective actions for structural issues. Finalize technical requirements within timelines and ensure high-quality outputs. Developing L3 level planning compliant to program milestones and driving scope / requirements and Input management accordingly to meet defined planning. Establish method documents, report templates, and SLAs during project setup. Drive scope definition, requirement traceability, and analysis across the structural lifecycle. Represent Accenture in technical discussions, aligning deliverables with client expectations. Lead discussions on analysis methods, meshing, and sizing guidelines. Track milestones, manage schedules, and ensure alignment with program goals. Monitor evolving requirements, manage changes, and ensure compliance with cost/schedule targets. Act as the key technical liaison, ensuring clarity and alignment on project deliverables. Build and mentor a high-performance engineering team with clear vision and growth plans. Conduct coaching, reviews, and succession planning. Contribute to internal initiatives, including design automation and digital workflows. Proven experience in static dynamic and impact analysis / sizing for design and integration of rotary-wing and/or fixed-wing aircraft structures across end-to-end design lifecycle phases. Demonstrated experience collaborating with cross-functional teamsincluding design, stress analysis, manufacturing, systems integration and quality within complex delivery frameworks for aerostructure development programs. Bachelors / masters degree (BE/MTech) in Aerospace, Aeronautical, or Mechanical Engineering. Certifications in project management (PMP/Prince2), Six Sigma, or Digital Engineering will be plus. FEA considerations and meshing requirements for different types of structural analyses like static, dynamic, buckling and impact analysis. In-depth understanding of helicopter/aircraft load-bearing structures, with focus on structural integrity, stiffness, and load path optimization under both static, dynamic, and impact conditions. Strong awareness of static dynamic and impact strength justification analyses and failure modes relevant to metallic and composite airframe components. Familiarity with structural analysis considerations related to assembly line constraints, ergonomic considerations, and sequence planning to ensure seamless integration in high-rate production environments. Proficient in configuration management principles, including part lifecycle management, engineering change control, version tracking, and release processes will be plus. Professional & Technical Skills: Expertise in the design/development and integration of metallic, sheet metal, and composite helicopter / aircraft structures for both primary and secondary components. Experience in weight optimization techniques, load path optimization, helicopter/aircraft certification and testing activities. Strong knowledge of airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Experience in preparation of test plan, test orders, test load derivation and test to analysis correlation reports for component level and full-scale structural tests for rotary wing / fixed wing aircrafts. Experience managing design-to-cost, design-to-weight, and sustainability considerations across the design lifecycleProficient in common FEA tools is essential with experience in MSC NASTRAN/PATRAN, ABAQUS, HyperMesh/Optistruct. LS DYANA or similar tools is a strong plus. Technically sound, solution-driven leader with strong decision-making skills. Capable of guiding teams through complexity and ambiguity. Strong communicator and client interface, capable of aligning stakeholders. Passionate about mentoring and driving engineering excellence. Strategic mindset focused on quality, optimization, and best practices. Additional Information:- The candidate should have a minimum of 15 years of engineering experience in the Aerostructures domain, with at least 5 years in a technical leadership or program governance role. This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Qualification 15 years full time education

As a Lead Associate-FE Analysis at Genpact, you will play a crucial role in maintaining and creating Tableau dashboards while ensuring data accuracy and resolving any report extraction issues. Your rich experience in FE modeling using ANSYS (Workbench & APDL) and HYPERMESH, along with expertise in Static (Linear and Non-Linear) Analysis, Dynamic analysis, and HCF/LCF fatigue analysis will be instrumental in analyzing various mechanical components" systems and sub-systems. Additionally, knowledge of Composites and Fatigue analysis would be advantageous. Your responsibilities will include utilizing your skills in FE modeling, dynamic analysis, and fatigue analysis to enhance the performance and reliability of mechanical components. Excellent communication and presentation skills will be key in effectively conveying your findings and recommendations to stakeholders. To excel in this role, you should hold a Bachelor's degree in Mechanical Engineering or an equivalent field. Preferred skills include knowledge of ABAQUS, Patran, and Nastran, which will further strengthen your capabilities in FE analysis. Join us at Genpact, where you will have the opportunity to work with a global team of professionals dedicated to delivering innovative solutions that drive business outcomes. If you are passionate about leveraging your expertise in FE analysis to make a meaningful impact, we invite you to apply for this exciting opportunity. Genpact is committed to creating a world that works better for people, and as a Lead Associate-FE Analysis, you will be at the forefront of shaping a future where data, technology, and AI converge to transform leading enterprises. Take the next step in your career with us and be part of a dynamic team that values curiosity, agility, and the pursuit of lasting value for our clients.,