- Lead, manage and resource the wing engineering team, providing strategic direction and fostering a culture of collaboration and innovation.- Oversee the design, development, and certification of wing structure and components, ensuring compliance with regulatory requirements and industry standards.- Guide problem-solving efforts and driving continuous improvement initiatives in wing design and engineering.- Manage project execution, coordinate with internal and external stakeholders, and monitor progress to ensure successful outcomes.- Foster collaboration with internal teams and external partners, and engage with stakeholders to drive innovation and influence industry standards.- Drive a culture of continuous improvement and innovation to enhance productivity, efficiency, and safety in wing engineering processes and methodologies.

Established company vision, culture and decision-making.Delivered business strategy and product development.Defined market opportunities and resource/financial estimations.Formed, led and monitored the company performance.

• Accountable for all the Hydraulic and Pneumatic technical deliverables of wing systems installation across all Airbus Fleet (A220, SA, A330, A350, A380, A400M, R&T) meeting requirements to Time, Cost and Quality;• Developing and implementing team strategy to achieve the overall vision of Wing Systems Installation;• Managing team's financial performance, workload planning and overall productivity improvement;• Responsible for the recruitment, training, technical development and skill-set management of the team;• Integrating globally across all Airbus Aircrafts' Systems Installation teams to ensure that the scope of any tasks are fully understood and enabled;• Engaging external Supplier/RSP support with complete workload scoping and definition using SOW/PO documentation;• Leading an internal team of WP Leaders, Technical Signatories and Professionals;• Representing Wing Fluid Systems Installation in stakeholder meetings and reviews.

Functional Aspect:• Technically Led Leading Edge and Midbox Wing Work Packages;• AP1020 Stress Approver rights delegation holder;• Control the overall technical delivery quality in compliance with EASA CS 25, FAA JAR 25 strength justification according to Airbus Methods;• Led and technically guided/enabled to UK/International Internal and External teams, RSPs and Sub-Contracting companies to ensure the overall IDR/PDR/CDR/CS requirements/deliveries are achieved;• Secured Wing structure certification technical coverage and documentation completeness (Stress Dossiers, SSR, ACD/ACS, ALS Part 1/Part 2, SRM);• Effective data control using tool capabilities and module functionalities of MSC Patran/Nastran, HyperMesh/HyperView, ISAMI Analyst, CATIA V5, MS WPs etc. Operational Aspect:• Project Managed Internal and External technical deliveries with regular weekly monitoring of all activity progress;• Managed resource and monitored spend for an accurate cost and quality delivery;• Monitored all enablement requirements and appropriate on-time deliveries for a continuous overall delivery progress; Product Evolution Aspect:• Technically improved product performance and maintenance via Weight Saving and DTC improvement definition;• Developed Business Cases ROMs and ROIs for further Wing WP evolution towards a more aircraft efficient structure;• Reduced NRCs via modification of drawing configurations, analysis and documentation scope;• Reduction RCs via modifications of manufacturing processes, tooling designs and assembling configuration time and complexities;• Reduced ALI locations and maintenance intervals increase for lower operating costs. Testing and Manufacturing Aspect:• Involved in Full Scale test findings to support strength justification and enable further structural optimisations;• Monitored manufacturing processes in order to drive potential improvements and overall product evolution.

• Delivered WING Focal Functional/Operational Role for a First Ever A350 Russian Runway Certification Delivery;• Delivered leadership of multiple WING Work Packages (LE, MIDBOX, TE, WINGTIP/WINGLET, High Lift, MLG) and Integration with Fuselage WP on an overall Airframe delivery aspect;• Provided business development and integration on an International level (UK, France, Germany, USA, India);• Strategically planned activity and resource aspect, followed by appropriate monitoring and red-flagging issues on resource or budget level;• E2E Product and Project Managed Internal/External teams and technical deliveries with regular weekly progress monitoring of all activities;• Monitored the enablement requirements and SOW/PO deliveries;• Communicated with customers and stakeholders in order to achieve an appropriate level of expectations for an overall successful target delivery;• Identified gaps and issues in technical justification process, engaging and delivering the problem solving sessions for further progress;• Delivered leadership with ability to develop, influence and coach less experienced engineers;• Dealt with difficult conversations and team members with additional level of support and guidance provided, as well as monitoring;• Provided technical performance evaluation of all team members.

Demonstrated Integration Coverage via:- Integration and quality control of delivered data by relevant work packages;- Technical guidance, resource support and resolutions on internal and sub-contractor team requests;- Detail investigation on critical queries, appropriately flagged risks and discussions with Local Stress Authorities;- Presentation content creation / presenting skills used in IDR/PDR/CDR supporting program progress;- Manufacturing and Testing teams support, supervising the activities and seeking for process improvements.Demonstrated F&DT Technical Coverage via:- Overall structure concept and flight behavior understanding;- Aircraft mission files, conversion tables and relevant spectrum files coverage;- Component pseudo, max fatigue and equivalent stress understanding and derivation;- AM documentation, ISAMI Analyst, ISAMI Series, DAMTOL;- Fatigue and SEI Analysis / Top and Bottom cover, Rib 27, Rib 27A, Sharklet Device, Root Joint;- DT and SEI DT Analysis, Threshold and Inspection Interval derivation / Top and Bottom cover (Skin to Stringer, SWJ, Manholes), Rib 27, Rib 27A, Sharklet Device, Root Joint;- Stress Dossier and Preliminary Stress Sheet documentation write up;- Structural modifications coverage, assembling and structural performance improvements;- GFEM FESPS Quality Gate-Reviews assessments / exceedance evaluation assessments, expected Fatigue performance impact confirmations;- Interface component load input derivation and quick data manipulation;- Lean projects, cutting costs with team work ideas, tools and innovations.Demonstrated FEM Technical Coverage via:- Component DFEM and GFEM manipulation skillset demonstrated;- Structural modifications, performance improvements, complex structure assembly modeling for a correct load re-distribution scenarios prediction in failure cases;- DFEM Validation checking procedure and documentation write up, using AM 2036;- Achieved AUK Internal CATIA V5 Instructor Qualification.

Technical Innovation Engineering Projects:- Preliminary and detailed design and stressing- Documentation production;- Manufacturing and testing supervision;- Results analysis.Project: ATRO-X VTOL UAV / Hot Cycle Tip Jet Propulsion System for UASYSTEMS- Main Rotor Head, Rotor Blades and Main Rotor Head to Rotor Blade interface;- Conceptual, Preliminary and Detail Design;- Preliminary and Detail Stress Analysis;- Static FE analysis using MSC Patran/ Nastran;- Thermal FE analysis of Rotor Blade assembly (spars, ribs, ducts, nozzles) and thermal expansion effects on aerodynamic design;- Hand calculation on welded joints and fastener sets , structure bearing capabilities.Project: Rocket Engine- Conceptual and Preliminary Design / Structure and Tooling;- Preliminary and Detail FE Analysis / Tooling;- Non-linear FE simulation / component forming for targeted combustion chamber, throat and throttle geometry;- Complex production technology target / component buckling effect during forming, caused by complex geometry, component internal thermal stress issues, resolutions and further on development;- Tool development for final assembling and testing.