F-16 Systems Engineer & NGB A5 Liaison (Airworthiness)

Gauss Management Research & Engineering (GMRE Inc.); Utah; On-site; USD 120,000 - 180,000; Full time

Benefits offered by this job

Health insurance

Dental insurance

Vision insurance

401(k)

Paid time off

Paid holidays

Life insurance

Job summary

Gauss Management Research & Engineering (GMRE Inc.) seeks Systems Engineer support for USAF acquisition programs. You will translate requirements into system-level specs, lead technical teams, and coordinate with government managers and contractors on milestones and reviews.

You will brief leadership on status and risks, ensuring compliance with airworthiness and test criteria while interfacing with aircraft integration designs and lifecycle considerations.

Qualifications

• Proven ability to translate user requirements into system-level specs.
• Experience with acquisition documents, test plans and reviews.
• Strong written and verbal communication skills.

Responsibilities

• Translate user requirements into system-level requirements and acquisition documents for F-16 upgrade programs.
• Assist with program execution, source selection reviews, and technical reports.
• Act as liaison between NGB/A5 and F-16 SPO program management/engineering teams.
• Lead the technical team to meet acquisition milestones, requirements, and reviews.
• Brief program status, risks, and design reviews to leadership and stakeholders.

Skills

Acquisition strategy

Technical program management

Systems engineering

AF Airworthiness

MS Office

Communication skills

Team leadership

Project planning

Vendor interaction

Education

Engineering degree

DoD / USAF experience

Job description

Gauss Management Research & Engineering (GMRE Inc.) seeks Systems Engineer support for USAF acquisition programs. You will translate requirements into system-level specs, lead technical teams, and coordinate with government managers and contractors on milestones and reviews.

You will brief leadership on status and risks, ensuring compliance with airworthiness and test criteria while interfacing with aircraft integration designs and lifecycle considerations.