Job Description

POSITION SUMMARY:

Support the Lead Engineer and the overall product development Integrated Product Team (IPT) in the structural analysis discipline. This position will entail the development of detail analysis, creation of documentation and substantiation reports, and general coordination of stress and fatigue analysis within the IPT and Core Engineering.

ESSENTIAL JOB FUNCTIONS:

Review drawings, specifications, service bulletins, reports, etc. for compliance with applicable regulations

Static strength assessment, fatigue life assessment, and damage tolerance assessment using both manual analysis and finite / boundary element analysis modeling

Prepare FAA required aircraft type certification reports showing compliance with the appropriate FAA or Foreign regulations on all structural components by either analysis or test

Perform complex finite element analysis and modeling

Perform preliminary analysis on Marketing ideas and concepts effecting the aircraft structure and /or weight in coordination with FAA regulations

Conduct aircraft loads analyses, weight investigations and preparation of a structural design criteria report of new/preliminary aircraft designs in coordination with FAA regulations

Perform Aircraft flight and ground loads analyses, and preparation of a required FAA certification loads report

Support the execution of static or fatigue tests of structural components, prepare test procedures, observe and document static or fatigue test results in coordination with FAA type certification report

Document compliance with the applicable regulations covering the structural strength, crash protection, interiors, basic loads, weight balance, stress analysis, static test, dynamic test, fatigue analysis/assessment, and evaluation of the processes and fabrication methods required to produce aircraft structure

Analysis or test of flight test instrumentation racks, test equipment, etc. to Company Engineering Policy requirements

Prepare Company required equipment lists for each aircraft model

Support the IPT in the preparation of material for presentation at design and program reviews

Perform other related duties as required

SUPERVISORY RESPONSIBILITIES:

This position will not have any direct supervisory responsibilities

May be required to train and assist other employees

QUALIFICATIONS:

To perform this job successfully, an individual must be able to perform each essential duty satisfactorily. The requirements listed are representative of the knowledge, skill, and/or ability required. Reasonable accommodations may be made to enable individuals with disabilities to perform the essential functions.

EDUCATION AND EXPERIENCE:

Required:

An understanding and working knowledge of Federal Aviation Regulations (FAR) Part 23 is necessary to perform the duties of this position

Requires a bachelors degree in mechanical or aerospace engineering and a minimum of seven (7) years in structural analyses, test and design or equivalent education and experience.

Detailed knowledge of aircraft with respect to structure, materials and processes specifications, and certification requirements is essential.

Working knowledge of Federal Aviation Regulation (FAR) 21 and 23, related Joint Aviation Requirement (JAR), and Civil Aviation Authority (CAR) 3 required

Preferred:

Familiarity with FORTRAN, Visual Basic, and C+ computer programming; and experience in Finite Element analysis and modeling preferred

Familiarity with extracting CAD models using Siemens NX

LANGUAGE SKILLS:

The employee must possess the ability to communicate effectively with all internal and external customers in both written and oral form

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