Electrical Hardware Design Engineer/ Hardware Design Engineer

JR-063942 Electrical Hardware Design Engineer/ Hardware Design Engineer Location: Phoenix, AZ- Onsite work only Fulltime Visa: USC/ GC Holder. Keywords to search: Gas turbine engine components Aero Engines PCB Design Circuit Card Assembly (CCA) Printed Board Assembly (PBA) Analog / Linear Circuit Design Signal Conditioning Data Conversion (ADC / DAC) EMI / EMC Compliance DO-254, DO-160 Avionics Hardware Development Hardware Integration & Testing EICD (Interface Control Documents) Design Verification & Validation Product Lifecycle Support Hardware Simulation & Analysis Job Description: Develop new complex PCB and CCA designs /alternate solutions with existing designs. Understand and comply designs with EMI/EMC requirements and verify at unit level. Develop DO-254 compliant complex hardware. Perform system integration based on documentation / author and execute test procedures. Design interfaces and release EICDs (Interface Control Documents Author documents for FRACA resolution and engineering changes / design release. Perform testing with appropriate lab equipment to verify integrity of design. Perform product life cycle sustaining tasks. Qualifications 3-6 years of hardware engineering experience Bachelor's degree from an accredited institution in a technical discipline such as the sciences, technology, engineering or mathematics Required Skills: Electrical Engineer -Aero Engines Develop Acceptance test criteria for electronic control units or other gas turbine engine components. Electrical design experience with aero engine projects or other aero engine manufacturers projects. Rich experience working on aero engine external parts BS degree in Electronic Engineering or related discipline Experience with Engines and power systems. Experience with module level analog / linear circuits including signal conditioning, data conversion (analog-to-digital and digital-to-analog Demonstrated experience performing Product / LRU and Printed Board Assembly (PBA) design verification and qualification. Knowledge of DO-254, Design Assurance Guidance for Airborne Electronic Hardware and RTCA DO-160 Qualification Guidelines. Demonstrated experience designing, simulating, analyzing, and verifying design performance to requirements. Proficiency with PCB schematic / Layout tools, Mathcad, MS Excel, and LT-Spice. Test Engineering experience including requirements-based testing. Familiarity with the avionics development life cycle and troubleshooting / debug capability / component obsolescence