Structural Analysis Engineer II

Structural Analysis Engineer II (Full Time)
Department: All Openings, Engineering

Job Title:

Responsibilities involve performing stress analysis for new and derivative designs of Part 23 aircraft structures and other related activities. This includes review of Engineering drawings, preparing load calculations and writing substantiation reports in collaboration with the Structural Engineering group and Structural Unit Members providing approvals.

ESSENTIAL JOB FUNCTIONS:

Perform static and dynamic structural analysis of metallic and composite structures and fatigue life assessment using both manual (textbook theory) analysis and finite element analysis modeling to guide product design and design changes.

Use the latest analysis tools and techniques including Finite and Boundary Element tools.

Build Finite Element Models to determine internal loads, locate stress concentrations and perform analysis on components.

Create stress analysis reports and/or test plans for substantiation.

Support static/fatigue test execution and test results.

Review drawings, specifications, service bulletins, reports, etc.

Review new drawings as required for determination of compliance to all part 23 structures requirements.

Prepare FAA required aircraft type certification reports showing compliance with FAA regulations covering structural strength, crash protection, interiors item, basic loads, weight balance, fatigue life, and flight test instrumentation.

Determine and develop approaches to solutions that are lightest, lowest in cost and high quality and consistent with schedule and budget objectives.

Contribute to developing plans for engineering substantiation projects.

Acts in collaboration with representatives in other disciplines (design, mass properties, manufacturing, materials & processes, etc.) and with Senior Structural Analysis Engineers.

Perform other related duties as required.

Minimum Position Qualifications

To perform this job successfully, an individual must be able to perform each essential function satisfactorily. The requirements listed below are representative of the knowledge, skill, and/or ability required.

Education and Experience

Requires a Bachelors degree in mechanical or aerospace engineering; a minimum of 3 years in structural analysis and test or equivalent education and experience is desired, preferably in aerospace or aircraft manufacturing environment.

Detailed knowledge of aircraft with respect to structure, materials and processes specifications, and certification requirements is essential. Working knowledge of Code of Federal Regulations (CFR) Part 23 is an asset.

Experience in Finite Element analysis and modeling is required.

Knowledge of computer programming such as VBA is preferred.

Excellent communication and interpersonal abilities to collaborate effectively with internal teams, industry partners, and customers.

Working knowledge of Windows based computer programs such as Word, Excel, and Outlook.

Physical Demands

The physical demands described here are representative of those that must be met by an employee to successfully perform the essential functions of this job.

Reasonable accommodations may be made to enable individuals with disabilities to perform the essential functions.

While performing the duties of this job, the employee is occasionally required to stoop, kneel, crouch, or crawl; and frequently required to stand; walk, use hands to finger, handle, or feel; reach with hands and arms; and talk or hear.

Specific vision abilities required by this job include close vision, peripheral vision, depth perception, and ability to adjust focus.

Requires moderate physical effort consisting of occasionally lifting and/or moving light to moderately heavy weight material up to 35 lbs.

Mental Demands

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