Actuator Lead

Archer Aviation
San Jose, California, United States$172k – $230kPosted 2 March 2026

Job Description

<div class="content-intro"><p><span style="font-weight: 400;">Archer is an aerospace company based in San Jose, California building an all-electric vertical takeoff and landing aircraft with a mission to advance the benefits of sustainable air mobility. We are designing, manufacturing, and operating an all-electric aircraft that can carry four passengers while producing minimal noise.</span></p> <p><span style="font-weight: 400;">Our sights are set high and our problems are hard, and we believe that diversity in the workplace is what makes us smarter, drives better insights, and will ultimately lift us all to success. We are dedicated to cultivating an equitable and inclusive environment that embraces our differences, and supports and celebrates all of our team members.</span></p></div><p>Archer is seeking an experienced <strong>Actuator Mechanical Development Manager</strong> to lead the design, integration, and validation of high-performance electromechanical actuators for flight-critical applications. This role requires a deep understanding of actuator system architecture, dynamic modeling, and performance analysis, as well as multidisciplinary integration across electrical, controls, and thermal domains. The ideal candidate is a hands-on technical leader with a strong foundation in mechanism design, high-reliability mechanical systems, and aerospace qualification processes—capable of driving concepts from requirements definition through flight-ready hardware on an aggressive schedule.</p> <h2><strong>What You’ll Do</strong></h2> <h3><strong>Design</strong></h3> <ul> <li>Lead a team of design and mechanical system engineers to design and develop high-performance, flight-critical electromechanical actuation systems from concept through production</li> <li>Own overall actuator mechanical design and integration of motors, geartrains, rolling-element screws, bearings, brakes, housings, sensors, and electronics</li> <li>Perform trade studies to optimize system architecture and mass while meeting performance and fault-tolerance requirements</li> <li>Create and review CAD models, drawings, and engineering specifications</li> <li>Develop actuator-system and detailed component specifications and requirements</li> <li>Build and maintain system-level models to validate actuator performance</li> </ul> <h3><strong>Leadership</strong></h3> <ul> <li>Act as single point focal for custom actuation development</li> <li>Work side-by-side with program manager to development and maintain milestone and schedule strategies</li> <li>Develop strong relationships and work seamlessly with internal functional groups for custom motor, controller, and thermal designs</li> <li>Partner with peer design owners including actuator controller, flight controls, GNC, power systems, airframe, and software to deliver an optimized integrated system for the aircraft</li> <li>Drive cross-functional project teams, coordinating with manufacturing, quality, sourcing, and test engineering</li> <li>Lead design reviews and provide technical expertise for key decisions</li> <li>Lead by example through hands-on problem solving, engineering rigor, and accountability</li> <li>Demonstrate best practices in documentation, testing, and design validation</li> <li>Mentor and oversee junior engineers, fostering professional growth</li> <li>Collaborate with systems, safety, and reliability teams to inform DFMEA and ensure requirements are fully validated and understood</li> <li>Lead and oversee technical performance of partnerships and suppliers for varied levels of subassemblies and critical components<br><br></li> </ul> <h2><strong>What You’ll Need</strong></h2> <ul> <li>Bachelor’s degree in Mechanical or Aerospace Engineering (or related field)</li> <li>8+ years of experience in actuated mechanism or electromechanical system design</li> <li>Strong communication and presentation skills at any level within the organization</li> <li>Proven ability to take ownership of complex engine ... (truncated, view full listing at source)