Key Responsibilities

Design and develop new complex PCB and CCA hardware, and create alternate solutions using existing designs.
Ensure compliance with EMI/EMC requirements and verify performance at the unit level.
Develop and document DO-254-compliant complex hardware.
Perform system integration , author and execute detailed test procedures.
Design and release Interface Control Documents (EICDs) and other supporting technical documentation.
Support FRACA resolution , engineering changes, and design release processes.
Conduct design verification and testing using appropriate lab equipment to validate integrity and performance.
Perform product life cycle sustaining activities, including troubleshooting and component obsolescence management.

Required Qualifications

Bachelor’s degree in Electrical, Electronics, or related Engineering discipline.
3–6 years of relevant hardware engineering experience , preferably in aerospace or embedded systems.
Strong understanding of analog / linear circuit design , signal conditioning, and data conversion (ADC/DAC).
Experience in Product/LRU and Printed Board Assembly (PBA) design verification and qualification.
Knowledge of DO-254 (Design Assurance for Airborne Electronic Hardware) and RTCA DO-160 (Environmental Qualification).
Proficiency with PCB schematic and layout tools , Mathcad , MS Excel , and LT-Spice for simulation and analysis.
Experience with requirements-based testing and hardware validation.

Familiarity with avionics development life cycle , debugging techniques , and component obsolescence management .