Description

Integrate engine control systems into airframe or OEM platforms for gas turbine development.

This role is hybrid.

Responsibilities

• Address requirements and resolve integration issues between engine control systems and airframe/OEM teams.
• Define, design, develop, test, and certify engine control system interfaces.
• Support engine test, systems test rig, and simulation development activities.
• Manage requirements using DOORS and configuration via JIRA or Integrity.

Required Skills

• U.S. Citizenship is required.
• Bachelor’s or Master’s degree in Electrical, Aerospace, or Mechanical Engineering.
• Gas turbine experience with integration of ARINC 429, RVDT/LVDT, and discrete communication systems.
• Knowledge of power bus management and analog systems.
• Experience with FAA Part 33 and Part 25 certifications.
• Proficiency in SAE ARP4754 development and V&V processes.
• Minimum 10 years in system development lifecycle.

Preferred Skills

• Experience with RTCA DO-178, DO-254, and DO-160 certifications.
• Control law development using Matlab/Simulink.

Key Skills

Education

Any Graduate