Electrical and Ice Protection Systems Integration Engineer
The Bell V-280 Future Long-Range Assault Aircraft (FLRAA)
Future Vertical Lift (FVL) Program has an opportunity available for an
Electrical and Ice Protection Systems Integration Engineer within the FLRAA
Vehicle Management Systems Team. The
Electrical and Ice Protection Systems Integration Engineer is responsible for
the design, development, integration, procurement, and test of the Ice
Protection Control System.
Ice Protection System architecture design,
requirements management, systems specifications, interface management, system
schematics, and integration with other vehicle management / aircraft systems
Coordinating with and managing electrical and
avionics system suppliers in the development, integration, and testing of ice
protection system components to include processor-based control units,
software, high power electrical distribution and switching, anti-ice and de-ice
System and software integration, requirements
management, systems specifications, interface management, system safety
assessment, validation and verification testing in systems integration labs,
aircraft flight test, and aircraft/system qualification and certification.
Development of test requirements to drive
systems integration lab and flight test aircraft instrumentation design
Perform hardware and software integration
testing of multiple systems operating together in a systems integration lab
Creation of system performance specifications,
interface control documents, and test plans/procedures.
Support all phases of development from design,
qualification, integration testing, flight test, and production.
Coordinating with teams from other disciplines
including aerodynamics, propulsion, airframe structures, and rotors
At least 8 years of relevant experience in
aerospace industry is required
Familiarity with RTCA DO-160, MIL-STD-704,
MIL-STD-810, MIL-STD-461, MIL-STD-464, RTCA DO-178, RTCA DO-254, SAE ARP4754A,
SAE ARP4761, 14 CFR Part 27 and Part 29 for commercial and military
qualification and certification of aircraft systems
Experience designing system architecture and
Experience with creation of system
specifications, requirements traceability, and verification.
Experience with avionics / electrical system
development testing and integration testing in a systems integration lab
Experience with aircraft installation,
functional testing, and troubleshooting
Work collaboratively in multi-disciplinary
teams to define cross-functional interfaces and conduct air vehicle level trade
studies as designs move from concept to production
Analyze and resolve hardware/software
integration issues as they arise
Experience with avionics electrical interfaces
including analog, digital, discrete I/O
Familiarity with multiple data protocols; ARINC
429, MIL-STD-1553, CAN, Ethernet
Understanding of current system engineering and
configuration management processes.
The preferred candidate will have:
Experience with high voltage DC systems; 270VDC
Experience with high power switching, circuit
protection, solid state switching devices
Experience with Enovia, DOORS, and Serena
Experience with schematic creation using Mentor
Graphics Capital Suite is preferred.
Familiarity with model based systems
Experience with System Safety Assessments,
Failure Hazard Analysis, and Certification and Test plans.
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