Advanced Design System Safety Engineer Staff

Overview The AD&D System Safety Engineer defines andleads system safety strategy for early‑phase aircraft and system concepts andis responsible for ensuring the safety and reliability of designs beingdeveloped by the Advanced Design & Development team. This role will focus on the initial phases ofaircraft development—ideation, hypothesis generation, stakeholder engagement,technology maturation, and conceptual design [BS1] . This role will develop safety‑drivenarchitectures, allocates safety and reliability requirements, and establishesre‑usable safety cases and analysis patterns that can be carried forward intodetailed design and certification programs. This position involves acting as a safety architect and technical leader and collaborating with cross-functionalteams, including aero, airframe, systems, software, and certification engineersas well as flight test, flight operations, and IT, to ensure that noveltechnologies and operating concepts can be matured into certifiable,operationally viable products.This role will work with small, agile teams toexplore new user value propositions, challenge the status quo, and evolve ideasinto developed systems with validated architectures and requirements ready fordetailed design and certification planning. Responsibilities Define AD&D safety engineering strategy, processes, and methods aligned with core Product Development's System Safety and Systems Engineering practices. Conduct system safety analyses to support early development design decisions such as system architectures, availability, integrity, monitoring, and other safety requirements. Conduct and document Functional Decompositions. Conduct and document aircraft and system level safety analyses – specifically Aircraft Functional Hazard Assessments, Preliminary Aircraft Safety Assessments, System Functional Hazard Assessments, Preliminary System Safety Assessments, Particular Risk Assessments, Common Cause Assessments, and Particular Risk Assessments. Develop and review system schematics. Develop and validate reliability, maintenance, and safety requirements. Participate in trade studies and design reviews. Perform reliability and safety trade studies for alternative architectures and design concepts. Establish and maintain safety cases, including explicit documentation of assumptions, open issues, and certification risks for transition into development programs. Mentor and coach AD&D and Systems Engineers in safety driven design practices, including early phase use of ARP4754B/4761A and runtime assurance. Perform reliability analysis of electrical and/or mechanical assemblies using RIAC NPRD-2011, NSWC-11, RIAC Reliability Toolkit, and/or equivalent. Perform reliability analysis of electrical assemblies using MIL-HDBK-217-F2, RIAC NPRD-2011, RIAC Reliability Toolkit, and/or equivalent . Perform Failure Modes and Effects Analysis (FMEA ) of electrical and/or mechanical assemblies per MIL-STD-1629A, SAE ARP4761, RIAC FMD-2013, RIAC Reliability Toolkit, and/or equivalent. Support safety of flight determination for first of type flights or first flights of significantly modified aircraft. Identify Failure Modes and Effects Test (FMET) cases and support simulation and flight FMET Review vendors' reliability analysis and FMEA submittals for completeness and accuracy. Perform Fault Tree Analysis (FTA) and common cause analyses (CCAs) of electrical and/or mechanical systems per SAE ARP4761. Development of tasks and procedures for flight crew and periodic maintenance requirements necessary for ensuring compliance with all regulatory requirements. Coordinate closely with and support the work of system and software architects, systems development assurance, systems engineering, electrical and mechanical systems design, flight deck designers, human factors engineers, and flight test. Travel up to 25% may be required. Qualifications Bachelor's degree in Mechanical, Aerospace, Electrical, Systems Engineering, or relevant technical discipline., Master's degreee preferred. 8+ years of experience with Systems Safety Analyses – specifically AFHA, PASA, SFHA, PSSA, CCA, and FMEAs Must have a strong understanding of ARP 4761 and ARP 4754A Must be able to conduct quick assessments and provide feedback on designs or architectures with only verbal direction or minimal documentation (whiteboard sketches, preliminary schematics, etc.) Must be able to work effectively in early product development phases, before full requirements or system descriptions are documented. Must be able to work with highly iterative or frequently changing designs Must be able to demonstrate the ability to read, write and speak the English language Ability to communicate technical knowledge in a clear and understandable manner Intrinsic motivation to drive progress - to explore, challenge, and innovate – and to minimize administrative overhead Must be innovation minded and willing to try new and different methods or approaches Must be comfortable operating under tight deadlines with minimal direction and in a shop or lab environment. Must be proficient in reading and creating engineering design definition - 3D models, 2D drawings, sketches, schematics, BOMs. Ability to work both independently and across a variety of functional disciplines Ability to efficiently learn new skills and manage multiple tasks Proficient with Microsoft Office (Outlook, Excel, PowerPoint, Word, Visio) Must demonstrate excellent verbal and written communication skills. Preferred Qualifications:  Previous aircraft development program experience, from early concepts to entry into service Private pilot certificate or personal aviation experience Familiarity with ARP 4761A and ARP 4754B. Familiarity with advanced software functions (AI, ML, etc.) and Run Time Assurance methods Working understanding of the FAA's Safety Continuum concepts Knowledgeable of or experienced with STPA