305 Impact Analysis Jobs - Page 2

About The Role Project Role : Business Analyst Project Role Description : Analyze an organization and design its processes and systems, assessing the business model and its integration with technology. Assess current state, identify customer requirements, and define the future state and/or business solution. Research, gather and synthesize information. Must have skills : Guidewire ClaimCenter BA Good to have skills : NA Minimum 7.5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Business Analyst, you will analyze an organization and design its processes and systems, assessing the business model and its integration with technology. You will assess the current state, identify customer requirements, and define the future state and/or business solution. Additionally, you will research, gather, and synthesize information. Roles & Responsibilities:- Expected to be an SME.- Collaborate and manage the team to perform.- Responsible for team decisions.- Engage with multiple teams and contribute on key decisions.- Provide solutions to problems for their immediate team and across multiple teams.- Lead requirements gathering sessions.- Conduct gap analysis and document findings.- Facilitate communication between business stakeholders and IT teams. Professional & Technical Skills: - Must To Have Skills: Proficiency in Guidewire ClaimCenter BA.- Strong understanding of business process analysis.- Experience in requirements gathering and documentation.- Knowledge of Agile methodologies.- Experience in conducting impact analysis. Additional Information:- The candidate should have a minimum of 7.5 years of experience in Guidewire ClaimCenter BA.- This position is based at our Bengaluru office.- A 15 years full-time education is required. Qualification 15 years full time education

About The Role Job Summary : Aligned to the strategic priorities of our clients, we are committed to activating human potential to drive enterprise transformation across industries. At Capability Network, we help clients navigate disruption, accelerate growth and create value while staying agile in an ever-changing business environment. As a part of our high-impact Talent & Organization / human potential team, you will help drive the following: Although no two days at Accenture are the same, as a Change Management Analyst in our T&O practice , a typical day might include: Discovering stakeholders challenges and expectations and defining a Change Management strategy to support business transformational change programs Leveraging social and digital technologies in change management and communications Assisting clients in developing their change capability and becoming more agile businesses Co-creating solutions and conducting user review sessions, and running stakeholder agreement meetings Conducting a Change Management Impact Analysis and developing treatment plans Implementing strategies that prepare an organization to put new business processes into practice Supporting Change Measurement activities via a Change Readiness tool Working with the HR Transformation team to implement HR Systems such as Success Factors and Workday Working across a dynamic, international team where English is the common language Collaborating with the best and brightest minds in the industry Coaching and mentoring junior team members Contributing to practice-building efforts such as recruiting, training and attending community events Traveling globally to work with prestigious clients and deliver large-scale transformational change Roles & Responsibilities: MBA/Masters degree 1 to 3 years of experience in change management-related programs (stakeholder assessment, change impact analysis, organization design, digital communication and engagement, training support and business readiness) Techno-functional experience in the successful delivery of HCM Systems implementation (SaaS, Workday, SuccessFactors, Oracle Peoplesoft, Taleo) or other cloud solutions is a plus Ability to articulate the business value of recommendations/plans/strategies Ability to interpret data, work with analytic models and advanced technologies and digital tools (e.g. cloud HR, behavior change packages, immersive learning) Ability to effectively manage stakeholders ina multi-cultural and global environment Experience of working on Digital transformations, RPA implementations, Shared Service setups and cloud based implementations will be a bonus Foreign language capabilities (eg. Arabic, Japanese, French) will be an added advantage Qualification Professional & Technical Skills: MBA/Masters degree 1 to 3 years of experience in change management-related programs (stakeholder assessment, change impact analysis, organization design, digital communication and engagement, training support and business readiness) Techno-functional experience in the successful delivery of HCM Systems implementation (SaaS, Workday, SuccessFactors, Oracle Peoplesoft, Taleo) or other cloud solutions is a plus Ability to articulate the business value of recommendations/plans/strategies Additional Information: An opportunity to work on transformative projects with key G2000 clients Potential to Co-create with leaders in strategy, industry experts, enterprise function practitioners and, business intelligence professionals to shape and recommend innovative solutions that leverage emerging technologies. Ability to embed responsible business into everythingfrom how you service your clients to how you operate as a responsible professional. Personalized training modules to develop your strategy & consulting acumen to grow your skills, industry knowledge and capabilities Opportunity to thrive in a culture that is committed to accelerate equality for all. Engage in boundaryless collaboration across the entire organization.

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 : 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.

The responsibilities for this position include reviewing and coordinating with business application teams on data delivery requirements. You will be responsible for developing estimation and proposed delivery schedules in coordination with the development team. Additionally, you will develop sourcing and data delivery designs, review data models, metadata, and delivery criteria for solutions, and coordinate with the team on test criteria and testing performance. You will also contribute to the design, development, and completion of project deliverables, conduct in-depth data analysis, and contribute to strategic efforts. It is essential to have a complete understanding of how data is managed and sourced across multiple business areas. The primary goal of this role is to analyze MassMutual operational data and collaborate with the reporting team to provide the required data efficiently. The required knowledge, skills, and abilities for this position are as follows: - Experience with Data Dictionary, Data Lineage, and Critical Data Elements. - Proficiency in Data Warehousing, Impact Analysis, and Reporting Tools. - Familiarity with Informatics and SQL. - Knowledge of vendor management and STM Mapping. - Exposure to Data Warehousing and Dimensional Modeling Concepts. - Understanding of ETL Source to Target Mapping Document. - Ability to validate data using analytics tools. - Hands-on experience and a strong understanding of the Software Development Life Cycle (SDLC).,

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

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

Role Purpose The purpose of this role is to design, develop and troubleshoot solutions/ designs/ models/ simulations on various softwares as per clients/ project requirements Do 1. Design and Develop solutions as per clients specifications Work on different softwares like CAD, CAE to develop appropriate models as per the project plan/ customer requirements Test the protype and designs produced on the softwares and check all the boundary conditions (impact analysis, stress analysis etc) Produce specifications and determine operational feasibility by integrating software components into a fully functional software system Create a prototype as per the engineering drawings & outline CAD model is prepared Perform failure effect mode analysis (FMEA) for any new requirements received from the client Provide optimized solutions to the client by running simulations in virtual environment Ensure software is updated with latest features to make it cost effective for the client Enhance applications/ solutions by identifying opportunities for improvement, making recommendations and designing and implementing systems Follow industry standard operating procedures for various processes and systems as per the client requirement while modeling a solution on the software 2. Provide customer support and problem solving from time to time Perform defect fixing raised by the client or software integration team while solving the tickets raised Develop software verification plans and quality assurance procedures for the customer Troubleshoot, debug and upgrade existing systems on time & with minimum latency and maximum efficiency Deploy programs and evaluate user feedback for adequate resolution with customer satisfaction Comply with project plans and industry standards 3. Ensure reporting & documentation for the client Ensure weekly, monthly status reports for the clients as per requirements Maintain documents and create a repository of all design changes, recommendations etc Maintain time-sheets for the clients Providing written knowledge transfer/ history of the project Mandatory Skills: Technical Support . Experience: 5-8 Years .

Role Purpose The purpose of this role is to design, develop and troubleshoot solutions/ designs/ models/ simulations on various softwares as per clients/ project requirements Do 1. Design and Develop solutions as per clients specifications Work on different softwares like CAD, CAE to develop appropriate models as per the project plan/ customer requirements Test the protype and designs produced on the softwares and check all the boundary conditions (impact analysis, stress analysis etc) Produce specifications and determine operational feasibility by integrating software components into a fully functional software system Create a prototype as per the engineering drawings & outline CAD model is prepared Perform failure effect mode analysis (FMEA) for any new requirements received from the client Provide optimized solutions to the client by running simulations in virtual environment Ensure software is updated with latest features to make it cost effective for the client Enhance applications/ solutions by identifying opportunities for improvement, making recommendations and designing and implementing systems Follow industry standard operating procedures for various processes and systems as per the client requirement while modeling a solution on the software 2. Provide customer support and problem solving from time to time Perform defect fixing raised by the client or software integration team while solving the tickets raised Develop software verification plans and quality assurance procedures for the customer Troubleshoot, debug and upgrade existing systems on time & with minimum latency and maximum efficiency Deploy programs and evaluate user feedback for adequate resolution with customer satisfaction Comply with project plans and industry standards 3. Ensure reporting & documentation for the client Ensure weekly, monthly status reports for the clients as per requirements Maintain documents and create a repository of all design changes, recommendations etc Maintain time-sheets for the clients Providing written knowledge transfer/ history of the project Mandatory Skills: Scala programming . Experience: 5-8 Years .

About this Position : You will be BA for Media domain who will be SPOC between Clients & technical teams. You will help in Product designing & its implementation & demonstrate expertise of Media domain Roles & Responsibilities: Experience with the Media & Advertising industry (MarTech, AdTech, Publishing, Entertainment) Requirement gathering, gap assessment, functional documentation & product backlog management Solution building, pre-sales, working on RFPs and RFIs in the Media & Advertising domain Knowledge of different tools and platforms used in the advertising, publishing and digital marketing eco-system Strong analytical and problem solving skills. Understand business needs and create business requirement documentation Prepare client business cases, requirement understanding documents etc. as required. Understand systems, processes, flow diagrams, as-is v/s to-be functionalities Support projects throughout the development life cycle Participate in UAT Participate in RFPs, RFIs and prospect meetings Build competitive proposals which includes solutioning of Adtech and MarTech ecosystem Proficiency in verbal and written communication. Ability to review other documents, test cases, and test plans. Evaluate business requirements submitted by Product Management. Collaborate with development and other stakeholders to assess requirements. Anticipate and address risks, gaps, and concerns. In addition to functional expertise, demonstrate an inclination toward technical understanding. Willingness to acquire proficiency in new tools and technologies. Provide accurate sizing estimates for new requirements promptly. Review change requests and manage the Product Backlog. Functional Analyst Skillset : - Demonstrate extensive functional knowledge of managed products and projects. Exhibit strong analytical and problem-solving skills with a proactive learning approach. Serve as the functional Single Point of Contact (SPoC) for assigned activities. Identify and pre emotively address risks, devising mitigation strategies in advance. Regularly update and engage stakeholders with timely project/product status reports. Collaborate with technical teams in solution design activities. Analyse processes and ascertain areas for process improvement. Proficiently manage critical situations, driving them towards result. Translate requirements into relevant documents such as Functional Specifications Reports (FSR), Use Cases, and High-Level Sequence Diagrams. Possess excellent communication, documentation, and presentation skills. Demonstrate proficiency in Root Cause Analysis, Gap Analysis, and Impact Analysis.

Description: As Business Analyst, you will be responsible for Understanding the requirements from product champion and product owners, Analyzing the requirements and identify the impact analysis. 5+ years of Business/Technical analysis Experienced in Agile working model Business Exposure - Banking, PCI, Payments DB/SQL - Moderate/good level of hands-on experience - to query and work with data. Experience using Splunk, Power BI Responsibilities: Defining business objects, Defining API specification, working with the product development team, Dividing the requirements into small user story and write scenarios, Creating user stories and Epics for each impact in JIRA, Triaging product defects and assessing the impact and schedule by working with scrum teams, Creating a mapping of services elements to the service providers service elements. Working with a development team to understand application and clarify requirements/refine requirement, Working with QA in providing insights and feedback for test cases, Reviewing test cases and test suite to ensure that enough coverage in place to attain the best quality, Addressing questions from Development and QA Accepting user stories from scrum teams during Demo, Doing research, creating documents, Adhering to technical and functional standards

Role Purpose The purpose of this role is to design, develop and troubleshoot solutions/ designs/ models/ simulations on various softwares as per clients/ project requirements Do 1. Design and Develop solutions as per clients specifications Work on different softwares like CAD, CAE to develop appropriate models as per the project plan/ customer requirements Test the protype and designs produced on the softwares and check all the boundary conditions (impact analysis, stress analysis etc) Produce specifications and determine operational feasibility by integrating software components into a fully functional software system Create a prototype as per the engineering drawings & outline CAD model is prepared Perform failure effect mode analysis (FMEA) for any new requirements received from the client Provide optimized solutions to the client by running simulations in virtual environment Ensure software is updated with latest features to make it cost effective for the client Enhance applications/ solutions by identifying opportunities for improvement, making recommendations and designing and implementing systems Follow industry standard operating procedures for various processes and systems as per the client requirement while modeling a solution on the software 2. Provide customer support and problem solving from time to time Perform defect fixing raised by the client or software integration team while solving the tickets raised Develop software verification plans and quality assurance procedures for the customer Troubleshoot, debug and upgrade existing systems on time & with minimum latency and maximum efficiency Deploy programs and evaluate user feedback for adequate resolution with customer satisfaction Comply with project plans and industry standards 3. Ensure reporting & documentation for the client Ensure weekly, monthly status reports for the clients as per requirements Maintain documents and create a repository of all design changes, recommendations etc Maintain time-sheets for the clients Providing written knowledge transfer/ history of the project Mandatory Skills: Embedded Software Design . Experience: 5-8 Years .

You will be responsible for developing high-quality, enterprise-class software by conducting requirement analysis, impact analysis, and design for assigned tasks. Your role will involve actively participating in various meetings such as SCRUM Team Daily Stand-ups, user-story grooming, sprint planning, retrospective, demos, and other ad hoc meetings. Additionally, you will collaborate with the team lead/project lead to ensure the software development process adheres to applicable CT QMS processes. Your key responsibilities will include developing software using ASP.NET MVC/Web API, Javascripts, "Rx JS", Angular material, Angular forms, and web API programming. You will also work with technologies like C# .NET, Web APIs, Microservices, .NET Core 2.x, and Azure Cloud. Moreover, you will contribute to managing qualities and ensuring that the team aligns with CT QMS processes. Furthermore, your role will involve coordinating with clients and highlighting any issues to the next level. An essential aspect of this position is the willingness to learn new technologies and the ability to work in a hybrid work mode. Strong OOP concepts, experience in MVC, ASP.NET, and a good understanding of design patterns & principles will be valuable in this role. Desired skills for this position include experience in Microservices, Windows Service, RabbitMQ, TFS/ADO, TeamCity, JIRA, SQL Server, Healthcare Coding and Compliances, and exposure to complex enterprise application component development and maintenance. Your role will require you to have excellent communication skills, analytical thinking, and a proactive approach to problem-solving.,

As a Front Office Product Owner Business Analyst in Hedge Funds Accounting, you will be responsible for overseeing various aspects of Front Office Operations, Treasury Management, Cash Management, and Hedge Funds Accounting. With over 14 years of experience in the domain, you will bring expertise in Hedging Strategies, Change Management projects, and Business Transformation projects to adapt to regulatory changes effectively. Your role will involve working with cross-functional teams, utilizing your experience in SDLC and testing projects following both Agile and waterfall methodologies. You will be required to conduct impact analysis, feasibility analysis, and ensure product control, execution, and delivery of regulatory projects. To excel in this position, you must possess strong decision-making skills, critical thinking abilities, and exceptional interpersonal and stakeholder management skills. Your ability to manage conflicting priorities during project delivery will be crucial in ensuring successful outcomes. In-depth knowledge of regulatory rules pertaining to Treasury Management, Cash Management, and Hedge Funds is essential. Proficiency in MS Office tools, particularly Excel and SQL for data analysis, is necessary to perform effectively in this role.,

You are looking for a highly skilled Manager/Sr. Manager Technical (EIA) to lead and oversee Environmental Impact Assessments for Mining, Cement, Pipeline, and Thermal Power projects. You will be responsible for conducting feasibility studies, risk assessments, preparing reports, ensuring compliance with regulations, engaging with regulatory authorities, and providing technical guidance to project teams. Additionally, you will monitor environmental performance, stay updated with relevant laws and industry trends, and promote sustainable development practices. The ideal candidate should have a Masters/Bachelors degree in Environmental Science, Environmental Engineering, Civil Engineering, or a related field with 3 to 10 years of experience in EIAs, preferably in Mining, Cement, Pipeline, and Thermal Power industries. You must possess strong knowledge of EIA guidelines, regulatory frameworks, risk assessment methodologies, and experience working with regulatory bodies. Preferred qualifications include certification in Environmental Management Systems (ISO 14001), knowledge of biodiversity conservation, air and water quality management, carbon footprint analysis, and hands-on experience in Environmental and Social Impact Assessments (ESIA). You should also have excellent project management, communication, and stakeholder engagement skills, ability to analyze complex data, and proficiency in environmental modeling software and GIS tools. If you meet the requirements and are interested in this position, please submit your resume and a cover letter highlighting your experience in EIA for Mining, Cement, Pipeline, and Thermal Power industries to HR at career.aseries@gmail.com.,

Are you passionate about making a positive impact on the planet and driving the energy transition forward If so, SmartHelio invites you to join their team. SmartHelio is a dynamic company backed by Y-Combinator, with locations in Noida, India and Lausanne, Switzerland. The company has been recognized as "Best for the World" by the B-Corporation institute for its significant contribution to the environment. As a member of the SmartHelio team based in Noida, India, you will have the opportunity to work towards creating a more sustainable future and be part of a company that is committed to making a difference in the world. Join us in our mission to drive positive change and accelerate the transition to clean energy.,

Role Java Full Stack Engineer - Associate Responsibilities Understand requirements and translate that to product features. Participate in Scrum meetings and express the work done and the plan clearly. Participate in scrum ceremonies and clearly communicate. Develop applications using Front end, middleware, and database related technologies. Should be hands in developing and implementing best practices and write smart piece of code. Coding standards should be followed, and the code should be highly performant. Should be able to write unit test cases using any of the frameworks and should be completely automated. Should have strong exposure in REST API design and principles and adhere to RAML/Swagger or Open API specification. Should be able to do impact analysis and document the design of the components. Should be able to develop reusable components using proper design patterns as listed by lead/architect so that it is extensible. The Role offers An outstanding opportunity to re-imagine, redesign, and apply technology to add value to the business and operations. An end-to-end project exposure across multiple technical stack and cloud platform An individual who has passion to learn and adapt to new technologies quickly and scale to the next level easily. High visibility, opportunity to interact with multiple groups within the organization, technology vendors and implementation partners.

About The Role - Grade Specific Key Responsibilities and Tasks Managing the lifecycle of an escalated incident including, but not limited to, acting as the single point of contact, incident intake, impact analysis. Act as a bridge between customers, support teams, and other stakeholders (product, engineering, etc.). . Ability to lead investigations for major incidents keeping all the stakeholders updated as necessary. You will follow the escalation process, including ticket assignment, tracking, and communicating the status of escalated cases while identifying areas for improvement in the escalation process and implementing changes to enhance efficiency. Investigate the underlying causes of escalated issues and work towards permanent solutions. Monitor customer satisfaction, feedback, and trends, and report on the performance of the escalation process to ensure support continues to provide the best internal and customer experience possible for escalated incidents. Skills and Qualifications 7+ years of experience handling customer escalations or working in a customer-facing support role in fast paced software/technology environments. Ability to communicate effectively with customers and other stakeholders. Experience working with relevant tooling including ticketing systems such as Zendesk and ServiceNow, and dashboard tools such as Zendesk Explore and Tableau.