Landing Gear System Responsible Engineer Primary role is to support advanced aircraft design efforts with landing gear system design, hardware selection, placement, preliminary sizing, and initial integration into different aircraft configurations. Secondary role is to provide mechanisms design support to other aircraft sub-systems, such as drive systems and door uplocks for in-flight door operation. Responsible for developing landing gear system requirements and creating the associated system specifications, supplier procurement specifications, and supplier SOWs. This will include, but is not limited to, creating functional architecture and activity diagrams, in collaboration with other sub-system engineering disciplines to understand power, cooling, signal, and structural interfaces for the landing gear system. Responsible for identifying existing and/or conceptual landing gear systems to meet requirements, creating 3D models and layouts, and performing trade studies to analyze the impact of integrating proposed mechanisms systems onto aircraft, as well as identify main driver variables that most significantly impact top level program requirements. Responsible for supporting the supplier management team by being the primary technical interface between NGAS and landing gear supplier subject matter experts. Participate in internal program, customer and supplier technical exchange meetings and formal program milestone reviews to provide and/or obtain progress status updates. Provide technical guidance to, and coordinate with, multiple engineering design teams, including the aircraft configuration team, the structures team, sub-systems team, and supplier management teams supporting the conceptual, preliminary, and detail design and development of the aircraft. Principal Landing Gear Engineer:

Bachelor's Degree in STEM (Science, Technology, Engineering or Mathematics) discipline from an accredited university and 5 years of engineering experience OR Master's Degree in STEM (Science, Technology, Engineering or Mathematics) and 3 years of engineering experience Sr. Principal Landing Gear Engineer:

Bachelor's Degree in STEM (Science, Technology, Engineering or Mathematics) discipline from an accredited university and 8 years of engineering experience OR Master's Degree in STEM (Science, Technology, Engineering or Mathematics) and 6 years of engineering experience or PhD and 4 years of engineering experience Prior experience with 3D Computer Aided Design (CAD) software applications Your ability to obtain and/or transfer and maintain the final adjudicated government Secret clearance, and any program access(es) required for the position within a reasonable period of time, as determined by the company Master's Degree in Mechanical or Aerospace Engineering or related discipline Active DoD secret clearance Landing gear placement (both deployed and retracted positions) Landing gear loads and preliminary sizing Shock struts Wheel and tire selection Braking systems Retraction and locking systems Landing gear door sequencing mechanisms Experience with Siemens NX CAD application, including NX Motion module Familiarity with development of landing gear doors, door actuation and door locks, as well as the development of in-flight door opening mechanisms Familiarity with industry standard software application tools such as Microsoft Office (Word, PowerPoint, Excel, Outlook, Visio, etc.), Adobe Acrobat, etc. Prior experience in leading a team of engineers Prior experience in coordinating with multiple Integrated Product Teams (IPTs) within a dynamic program environment Experience with suppliers and supplier coordination