SOFTWARE SAFETY STANDARDS AND REQUIREMENTS ACROSS THE FULL DEVELOPMENT LIFECYCLE FROM HAZARD IDENTIFICATION THROUGH DEVELOPMENT TO SYSTEM/SOFTWARE QUALIFICATION TEST IS DESIRED (E.G. DO-178C, MIL-STD-822, AMCOM385-17, JOINT SOFTWARE SAFETY ENGINEERING HANDBOOK)

Proven analytical and problem-solving skills with the ability to work with cross functional teams in resolving complex highly integrated functional systems problems.
Must be familiarity with the civil safety process defined in Society of Automotive Engineers (SAE) ARP-4761 and ARP-4754 and/or defense safety process defined in MIL-STD-882.

MUST HAVE DIRECT EXPERIENCE IN SAE ARP4761 ANALYSES:

• Aircraft and System Functional Hazard Assessments (AFHA/SFHAs)
• Aircraft and System Safety Assessment (PASA, PSSA. ASA, SSA)
• Particular Risk Analysis (PRA)
• Zonal Safety Analysis (ZSA)
• Common Mode Analysis (CMA)
• Direct Experience in MIL-STD-882 analyses:
• Preliminary Hazard Analysis (PHA)
• Operational & Support Hazard Analysis (O&SHA)
• Health Hazard Analysis (HHA)
• System/Subsystem Hazard Analysis (SHA/SSHA)
• Hazardous Materials
• Failure Modes and Effects Criticality Analyses (FMECA)
• Safety Assessment Report (SAR)
  Experience or training in the?development and application of model-based systems engineering (MBSE), and model-based safety analysis (MBSA) is desired.
  Technical and functional understanding of aircraft and aircraft systems.
  Operational understanding of aircraft, aircraft systems, and related support systems is highly desirable.
  BS and 2+ plus years of experience on aircraft or system development/sustainment programs that have utilized structured safety program processes or plans.
  Related degrees with relevant experience such as military rotorcraft/powered life aviator or mechanic qualification will be considered.
  Job Type: Contract
  Pay: $84.00 - $86.00 per hour
  Expected hours: 40 per week

Benefits:

• 401(k)
• Dental insurance
• Health insurance
• Vision insurance

Work Location: In perso