Collaborating with cross-functional teams to design, implement, and certify the Enhanced Angle of Attack (EAOA) system for the 737 MAX -10 /9/8/7 airplanes• Leading the design and certification of the Enhanced AOA system for 737 MAX series, focusing on Development Assurance.• Developed a comprehensive test infrastructure for meticulous verification of system requirements and performance.• Defining avionics system specifications; managing requirements traceability, validation, and verification processes to ensure FAA/EASA compliance.

Responsible for Maintenance, Repairs and Overhaul (MRO) and for Reliability, Availability, Maintainability and Safety (RAMS) of avionics on Boeing 737s and Airbus 320s operated at the airline:• Reviewed and coordinated of MRO and RAMS service bulletins and service letters received from OEMs and suppliers and advisory circulars and airworthiness directives from the FAA;• Developed, revised and released changed requests, work cards, engineering controls and supporting tech docs, diagrams and drawings, and updated maintenance and operating manuals for installation of new systems or modification of existing systems;• Managed projects: scheduled, actioned and evaluated repairs and alterations/modifications to avionics of the fleet;• Facilitated and conducted avionics prototype testing and evaluations;• Assisted other departments in planning and coordination of MRO programs;• Liaised with Airbus and the FAA on issues and routines.

● Designed and set up a test environment for hardware and software● Provided test application training and support to Contract Manufacturer test engineering teams● Developed test plans, execute testing, and created test reports during hardware development for Linux-devices (Payment Terminals)● Worked with the engineering development team on power design, voltage regulator design, system bring-up and design validation● Supported the team in debugging, troubleshooting, and failure analysis investigation

Program: Avionics Retrofit for Mi-8, Mi-17 and Mi-171 helicopters:• Contributed to re-definition and requirements specification of the avionics system architecture under upgrade• Developed the system requirements documentation for the installation and integration of the subsystems on board• Reviewed and revised maintenance and engineering documentation to ensure the helicopters remain within the aviation regulations

● Developed High-Level system requirements (as defined in ARP4754, DO-160, DO-178), systems architecture, electronic hardware for projects: Integrated Modular Avionic for Aircraft MC-21, Superjet; Touch-Screen Glass Cockpit for Next generation Civil Aircraft; next-gen DME/VOR/ILS onboard radio navigation system● Updated/implemented the design and testing phases, including design and testing of prototypes, test benches, orchestration and sign-off on acceptance test results to ensure design integrity● Developed block definition diagrams, airborne wiring diagrams, system performance descriptions, GUI, software requirements specifications and network protocols● Defined flight control strategies and contributed to the description of pilot use cases and flight operation scenarios● Developed requirements of next-gen DME/VOR/ILS onboard radio systems based on distributed-integrated modular architectures, and of next-gen avionics concepts providing capabilities of dynamic reconfiguration-in-operation based on distributed-but-still-integrated modular architectures● Developed a Nonparametric diagnostics and failure detection method in flight control actuation system (use the measurements of aircraft control and states only) – Ph.D. thesis

• Defined avionics concepts and systems architecture for aircraft, documented evaluation summaries for An-124 Cargo Airplane Retrofit program• Contributed to planning of aircraft modification scenarios, affordability, and feasibility assessment of the program• Collaborated with the certification team on the development of the application and certification basis

• Identified aircraft system requirements and designed systems architecture to meet the requirements (sensors, onboard computers, displays, FLIR, onboard networking and for flight simulators)• Developed block definition diagrams, airborne wiring diagrams, system performance descriptions, and software requirements specifications• Installed, commissioned, and repaired the aircraft systems and sub-systems• Prepared technical aircraft documents and developed aircraft testing and maintenance procedures• Designed aircraft integration, avionics equipment integration, and electrical aircraft interior testing• Provided installation, maintenance instructions, and guidelines to junior staff• Supported the project and technical lead in estimating budget and cost requirements

• Designed and implemented hardware and software of embedded devices and systems from initial requirements to production and commercial deployment: ­ - Customized automotive electronics (coded in С++, C#)­ - Embedded devices and systems (coded in C)­ - Smartphone Apps for automobile remote control (coded in Java, Objective-C)• Designed PCB for security systems and remote controls with OLED displays• Supported software QA and optimize stability and performance• Ensured proper technical and user documentation for the systems and software• Conducted process improvement and participated in defect reduction programs

• Identified aircraft system requirements and designed systems architecture of onboard computers and graphics systems, helmet mounted display, MFD, ILS, VOR/DME and TACAN (for Su-30MKI, Su-32, Su-34, Su-35, Su-57 aircrafts)• Prepared technical aircraft documents and developed aircraft testing and maintenance procedures (the bench, ground, and flight tests)

• Designed and constructed of computer networks.• Administered of networks, IT and laboratory equipment.• Administered and configurated software.