Job Title: Systems Safety Engineer

Functional Area: Engineering

Requsition Number: 7315

Work Location: Interiors -(Electronic Systems Center) Phoenix AZ

Job Description Summary: Position Overview
Because of a strategic commitment, Goodrich Corporation has initiated the creation of an Electronic Systems Center (ESC) headquartered in scenic Phoenix, AZ. The ESC will support a wide variety of Goodrich aerospace products with state-of-the-art facilities and expertise. The ESC team will design, test, build, and support electronic components and systems for all parts of the Enterprise. As a system safety engineer you will be working in a focused, cross-functional team of engineers developing avionics products.

Primary Responsibilities

Execution of Engineering Projects:

- Works with other System Engineers to helps to define system architectures by developing and utilizing Fault Hazard Assessments, System Safety Assessments, Fault Tress and Reliability Predictions, and Failure Mode and Effects Analyses.

- Ensures system designs are certifiable to FAA, EASA and other authority requirements.

- Assists with complex system and sub-system trade studies.

- Develops System Safety Assessment (SSA) documentation from guidance including FAA Advisory Circular AC 25.1309, SAE ARP 4754 and ARP 4761.

- Develops Fault Tree Analyses from guidance such as Nuclear Regulatory Commissions Fault Tree Handbook (NUREG-0492) and SAE ARP 4761

Basic Qualifications: Knowledge, Skills and Abilities

Required:

- BS degree in Electrical (preferred), Software, Systems Engineering with at least 8 years of experience in the Aerospace Industry.

- A minimum of 5 years of experience in the RM&S field desired regardless of engineering degree.

- Broad based system design and development background (electronics, software, avionics) with a preferred focus on modern avionics integration.

- System safety documentation experience.

- FAA/EASA certification and audit experience.

Critical competencies: Customer Focus, Drive for Results, Technical Skills, Interpersonal Savvy, Commitment to Continuous Improvement, Effective Teamwork.

Preferred:

- System requirements definition experience taking into account SAE ARP 4754, Fault Tree/System Safety Assessments, FAA/EASA regulations.

- Experience with system modeling to support hardware/software partitioning, trade studies, overall design decisions, and to predict total system performance.

- Development of System Description Documents, Certification Test Plans, Common-Mode Analyses, and other documents required for aircraft certification.

- Understands how Failure Mode, Effects and Criticality Analysis (FMECA) utilizing methodologies such as FMD-97, MIL-STD-1629 and SAE ARP 5580 are constructed.

- Understands how Electrical Stress Analysis and Derating Analysis in accordance with customer supplied or Goodrich Derating Guidelines are constructed.

- Understands Reliability Prediction Analyses utilizing Methodologies such as MIL-HDBK-217, PRISM, 217-Plus, MIL-HDBK-338 Field Data Methods, and NPRD-95 are constructed.

- Complete development life-cycle experience: requirements, design, development, integration, and qualification tested to the requirements of DO-178B.

- DER qualifications or history

% Travel Required: 10 - 20%