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Job Role:
Maintenance Repair Operations, Avionics Engineer
Location:
United States
Type:
Permanent
Job description
General Summary: The DER Avionics Engineer will be responsible for the design, development, and integration of the assigned avionic systems for the HondaJet aircraft. Duties and Responsibilities: Define, plan, and develop complex systems level requirements to support the avionic systems for the HondaJet aircraft. Perform systems level integration activities for aircraft avionic systems including: Control and Display Systems; Navigations Systems; Communication Systems; Surveillance Systems; and Cabin Management Systems. Interface with suppliers to ensure technical requirements are met to support aircraft development need dates. Provide technical assistance to production and customer service departments for support of system technical inquires and issue resolution. Perform system evaluation and analysis to verify the system design compliance with functional requirements. Coordinate with cross-functional team members to complete assignments/projects as defined and on schedule. Develop targeted system level enhancements to address customer feedback and product improvement initiatives. Conduct system lab testing and aircraft functional testing. Prepare presentations on avionics system design/development status. Support system analyses for avionic systems. "Honda Aircraft Is An Equal Opportunity Employer" Education, Work Experience, Certification and/or Licensure: Bachelors' degree in Engineering from an accredited college or university; (preferably in Electrical/Electronic Engineering.) Minimum of 8 years Engineering experience; 4 years of experience working with integrated aircraft avionic/electrical systems in the areas of design engineering, system analysis, and system test. Masters' Degree in Engineering from an accredited college or university; (preferably in Electrical/Electronic Engineering.) Minimum of 6 years Engineering experience; 4 years of experience working with integrated aircraft avionic/electrical systems knowledge of aircraft design requirements of 14 CFR Part 23. DER authorization required. Knowledge, Skills and Abilities: Proficiency in writing technical requirements, documentation, and reports involving test data and analysis. Familiarity with avionics/electrical test laboratories and lab equipment. Working knowledge of system qualification requirements including DO-160F/G for environmental, DO-178B/C for software, and DO-254 for complex electronic hardware. Familiarity with SAE ARP 4754 and ARP 4761 desirable Proficiency in Microsoft Office suite (Word, Excel, Project, PowerPoint is required. Proficiency in requirements management tools such as DOORS, PLM tools such as TeamCenter and SAP is preferred. Ability to manage and complete complex work assignments. Ability to work independently and within a multi-functional team environment. Ability to support production and customer service to trouble shoot and recommend solutions to aircraft issues
Requirements
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