Project Engineer II
-
Engineering
Aerospace / Aviation / Avionics, Mechanical Engineer, Systems Engineer, Engineering Design & Technologists
Job Description & How to Apply Below
Project Engineer II
Company: RSA Engineered Products LLC
Primary
Location:
110 West Cochran Street, Unit A, Simi Valley, CA 93065 USA
Workplace Type:
On-site
Employment Type:
Salaried | Full-Time
Function:
Engineering
Equal Opportunity Employer Minorities/Women/Veterans/Disabled
MainDuties & Responsibilities Summary
Penn Aero is hiring a Project Engineer II at our RSA Engineered Products Companyin Simi Valley, CA. RSA provides flight-critical components and assemblies forthe commercial, defense and business jet markets. RSA designs and produces custom-engineered high pressure/high-temperature ducting assemblies for each customer’s specific performance requirements. RSA’s Peri-SealTM is one ofthe most sought after connectors in the aerospace industry. Additionally, RSAdesigns and produces flexible joints and hoses, ozone converters and many complex assemblies to meet stringent customer needs.
AboutPenn Aero
Penn Aero is a leading manufacturer of highly engineered fasteners and specialized components for critical aerospace, defense, space, and advanced energy applications. We partner with customers to solve their most complex challenges, bringing technical depth and disciplined, agile execution when itmatters most. Experience guides our growth—strengthening capabilities and expanding our global platform as markets evolve. To learn more about Penn Aero'scapabilities and commitment to aerospace excellence, visit
Job SummaryAs a direct report to the Engineering Director, the Project Engineer II shallbe responsible to plan, organize, implement and control a variety of activities related to engineering, research and development and design related to customer specifications to ensure company business goals and customer requirements aremet within cost and on schedule. The Project Engineer II may have Junior Engineers supporting them.
Projects will include, but are not limited to:
New Product Development RSA IPdesigns, Build-to-Print, Design to Spec, and other relevant design activities. The Design Engineering Manager shall be responsible to ensurethe completion of projects from the Request for Proposal (RFP) phase thru Contract Award, Detailed Design, Design Validation/Certification, initial
Production, and sustaining engineering efforts.
Duties & Responsibilities
- Organize and schedule engineering activities to ensure they are completed onschedule and within cost.
- Execution and generation of aircraft certification documentation that may include, but not limited to:
Design calculation reports, test procedures,test reports, 3D modeling, 2D engineering drawings, Engineering Orders, etc. - Peer review of detailed design activities including: manufacturing drawing review, stress analysis, project schedules, etc.
- May require support of junior engineers.
- Assure design compliance to customer requirements.
- Schedule design reviews, meetings, and interdepartmental presentations toensure design points are understood and are concurrent with other organization activities.
- Ability to take “hands on” approach.
- Perform other duties as assigned
- Conform to company safety policies and procedures.
- Work in a team environment.
This role is required to be on-site 5days at theSimi Valley, CA location.
Qualifications Required Education & ExperienceBachelor’s degree in ME, Physics, EE, Aeronautical Engineering or IE with preference toward Mechanical Engineering. Advanced degree preferred.
Understanding of a broad range of engineering skills. Preferably in aircraft/aerospace design and structural analysis. Product development background necessary.
3 – 7+ years of experience in metallic or composite ducting and motioncompensator design per ARP 699 guidelines as Project / Systems Engineer, or equivalent experience in ECS (Environmental Control System), bleed air, or AMS(air management system) system or component design in the following industries:
- Valves (pneumatic or electro mechanical)
- Heat Exchangers
- Turbo Machinery
- Fuel Tank Inert Systems (FTIS, OBIGGS, OBOGGS, NGS, etc.)
- Wing-Anti Ice Systems
- Ram Air Systems
- High Pressure or Low Pressure pneumatic systems
- Structural design
Preferred to have experience with analysis tools such as FEA / FEM tools MSCNASTRAN / PATRAN, ANSYS, ATA NASTRAN / FEMAP
Experience with aircraft certification to EASA, Transport Canada, and/or FAA 14
CFR FAR 25 requirements.
Experience from program award (kick-off) to Milestones such as: PDR(Preliminary Design Review), CDR (Critical Design Review), PRR (Production Readiness Review), SOF (Safety of Flight), EIS…
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