Staff Engineer, Landing Gear Systems (RX) (R5372)

Job description

Job responsibilities

• Architecture and Kinematic Trades: Lead landing gear architecture definition and trade studies (e.g., electro-mechanical vs. hydro-mechanical actuation, fixed vs.
• Mechanism and Structural Design: Own the full CAD design lifecycle from initial concept through drawing release, including complex linkage kinematics, clearance envelopes, structural load paths, material selection, and…
• Structural and Dynamic Sizing: Perform first-principles classical stress and fatigue hand calculations, backed by finite element analysis (linear/non-linear, modal, buckling) and dynamic landing load assessments.
• Subsystem Sizing and Selection: Size and select wheels, tires, brakes, shock absorption systems, actuators, and nose wheel steering mechanisms tailored to vehicle landing and taxi envelopes.
• Component Sourcing and Vendor Management: Author technical specifications and statements of work (SOW) for landing gear components, evaluate vendors, and drive supplier technical execution.
• Test, Drop Qualification, and Validation: Define verification test plans, design mechanical test fixtures, support drop test campaigns, and execute functional validation against performance requirements.
• Integration and Flight Test Support: Support prototype assembly, ground taxi testing, and flight test operations to identify discrepancies, resolve mechanism anomalies via root-cause investigation, and implement rapid…

Job requirements

• Clearance: US Citizens Only; must have an active Secret or higher clearance.
• Experience: minimum 7 years (L4) to 12 years (L5) of direct experience in aerospace mechanism design, aircraft landing gear systems, or primary structural development.
• Education: B.S. or M.S. in Mechanical Engineering, Aerospace Engineering, or a related technical discipline.
• Core Fundamentals: Deep mastery of classical solid mechanics, kinematics, dynamics, fatigue, materials selection (alloys, heat treatments, surface treatments, allowables), and GD&T/tolerance stack-up methodologies.
• Analysis and Modeling: Demonstrated capability performing closed-form hand calculations and FEA analysis (linear, non-linear, buckling, modal) for high-load mechanism and structural components.
• CAD and PLM: Extensive experience in 3D CAD modeling, mechanism layout, and drawing release (Siemens NX preferred, or equivalent like CATIA/Creo) with PLM workflows.
• Hardware and Supplier Execution: Proven track record sourcing aerospace hardware, collaborating with specialized mechanism/actuator suppliers, and supporting physical builds and test rigs.
• Autonomy: Demonstrated ability to self-direct, prioritize technical tasks without oversight, and deliver functional hardware under tight timelines.