Tamarack Aerospace Group, a dynamic and fast paced aircraft modification company, is seeking a highly motivated Stress Analyst Engineer who desires to become part of a company involved in providing revolutionary improvements in the performance of business jets and beyond.

As a Stress Analyst Engineer with Tamarack Aerospace Group you can expect to work on aircraft structures from early development stages through to field support.

Sandpoint, Tamarack’s US business home base, is known as a destination resort town and is part of several historic small towns in the area with active communities rich with arts and culture and numerous noteworthy restaurants. Sandpoint is positioned on the scenic Lake Pend Oreille, the largest body of water in Idaho, yielding several types of summer recreational activities and boating. With the surrounding mountains and geographical location, Sandpoint has exceptional snowboarding, skiing, and snowmobiling opportunities. In close proximity, the national forests contain notable species of wildlife, expanding the outdoor activities. Sandpoint is close to destination cities with the renowned Coeur d’Alene, Idaho just 45 miles to the south and Spokane, Washington 72 miles to the southwest.

Tamarack Aerospace’s unique corporate culture is one that strives towards achieving excellence in challenging and stimulating work while offering ample opportunities for professional development. The ideal candidate will be a self-starter inspired by the excitement of creating innovative solutions in a diverse and dynamic multi-disciplinary team environment.

If your goal is to become a significant member, working with an elite, highly experienced development and production support team, send your resume to jobs@tamarackaero.com for consideration. You’ll find we offer competitive compensation/benefits commensurate with your experience.

Your privacy is important to us so your information will remain confidential.

Job Description:

  • Perform structural analysis work on aircraft modification programs addressing metallic or composite designs. Analysis may include primary or secondary airframe structures to substantiate that positive margins are in place for aspects including static strength, fatigue, and aero-elastic behavior.
  • Develop internal loads information and free body diagrams for structural assemblies. Perform strength and stability checks of structural details using industry standard finite element methods and classical hand calculations.
  • Create specialized finite element models of structural details as needed to support stress analysis work.
  • Support drawing release by documenting static and fatigue stress analyses for new designs and design changes.
  • Compile margin of safety summaries and document analysis results in formal report format for approval from FAA or EASA certifying authority under Part 23 or Part 25 regulations.
  • Review and approve supplier drawings, stress reports, and test reports.
  • Coordinate with the design groups, manufacturing, loads, test and others as required.

Specific tasks include:

  • Build or modify FEM models
  • Validation of FEM based on test or other data
  • Conduct sizing sensitivity studies for initial design
  • Produce stress calculations supporting compliance reports
  • Compose reports documenting compliance to FAA or EASA Part 23 or Part 25 requirements

Qualifications:

  • 8+ years’ applied aerospace industry experience required.
  • Must be familiar with FAA or EASA Part 23 and Part 25 certification requirements.
  • High proficiency with NX NASTRAN and FEMAP is required.
  • Proficient understanding of aerospace industry engineering principles and concepts for aircraft primary structure.
  • Must be proficient in traditional (hand) calculations through to full computer simulations, testing, and documentation supporting certification.
  • Must possess excellent verbal and written communication skills and must function well within a multi-disciplinary team.
  • High proficiency in MS Word and Excel is required.

Education & Experience:

  • B.S. in Aerospace or Mechanical Engineering required
  • Minimum of 8 years of experience in the aerospace industry with emphasis on primary airframe structural analysis.

 

Email your application to jobs@tamarackaero.com