Responsibilities
- Lead the design and integration of electronic airborne subsystems.
- Define and manage system interface requirements, including generation of EICD (Electrical Interface Control Documents).
- Support system engineering tasks related to integration planning and coordination.
- Lead lab and platform-level testing activities throughout the integration lifecycle.
- Author test plans, test procedures, and formal documentation.
- Work closely with hardware, software, and mechanical teams to ensure system compatibility.
- Support and guide the integration and verification process in both lab environments and flight platforms.
Qualifications
- B.Sc. or higher in Electrical Engineering or a related field
· Minimum of 8 years of proven experience in electronic airborne systems integration.
- Familiarity with communication protocols such as MIL-STD-1553, RS485, and others.
- Solid understanding of electrical design principles and interface definitions.
- Experience writing test plans and test procedures.
- Strong leadership and communication skills for guiding multidisciplinary integration processes.
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