Engineer High School

SHANNON EILEEN HUNT

**** ********** *** ** #***

Seattle, WA 98136

Home: *****************@*****.***

Mobile: 425-***-****

EDUCATION

Embry Riddle Aeronautical University Graduation: September 2017

Enrolled in Masters of Aeronautics

University of Alabama

Introduction to Flight Test June 2015

University of Washington

Completed 2/3 of Medical Devices & Commercialization certificate program June 2010

Completed Basic Medical Science certificate program June 2009

Completed Modern Aircraft Structures certificate program June 2008

University of Southern California

Completed Systems Architecture December 2006

Michigan State University, East Lansing, Michigan

Bachelor of Science in Mechanical Engineering Graduation: May 8, 2006

3.127/4.00 GPA

University Scholars Scholarship (applied to 4 years)

COURSEWORK COMPLETED

Finite Element Analysis, Fluid Mechanics, Thermodynamics, Mechanics of Deformable Solids, Aerodynamics for Engineers, Design & Analysis of Aircraft Structures I and II (UW), Fatigue and Failure Analysis (UW), Physiology (UW), Anatomy (UW), Medical Device Design (Human Factors), Introduction to Flight Test (UAH), Aircraft Composite Structures: Materials and Mechanics (Ed Wells), Hydraulics Analysis (Ed Wells), Human Factors in Aviation (ERAU), Aviation/ Aerospace System Safety (ERAU), Aviation/ Aerospace Accident Investigation and Analysis (ERAU)

TECHNICAL SKILLS

CATIA V4/ V5, NASTRAN, Patran, UNIX, ANSYS, CSW, Abaqus, SolidWorks, Matlab, Minitab, Unigraphics, All Microsoft Office, Abaqus

OTHER SKILLS

Completed 5 years of French (middle school/ high school), 2 years of Latin (high school), and 1 year of German (college)

EXPERIENCE

Boeing Company, Boeing Field, WA

Engineer/ Scientist, Level 2, promoted to Level 3- Stress Analyst

Flight Test Instrumentation Stress Analyst

11/2010 to Present

- Support various airplane programs including 747-8I, 747-8F, P-8I, 787-9, 757ECO, 737MAX, KC46A, 787-10

- Review and correct stress analysis notes submitted by design engineers and other stress analysts in order to make sure all load

factors and loads are considered

- Compile data and create lab report for Rapid Prototyping Material allowables

- Coordination with various groups about Flight Test Equipment installations

Focal for coordinating floors with 787-9 Production, 737 MAX/ Spirit Aerosystems, KC46A, and 787-10 Production

Perform analysis and answer questions regarding water barrels, fin cone winch, ballast plates and rails, seats, laptop table, raised floor, etc. Explain LOPAs to Production when coordinating the floors and discuss any issues that arise regarding the floors to other interested parties.

Participate in discussions with Floors, Weights, Flutter, Ground Operations etc to make sure the Flight Test envelope is met

Facilitate discussions between designers and other groups about FTI equipment by creating coordination sheets, participating in meetings, and ensuring that everyone understands the FARs and their applicability to FTI equipment

Resolve factory issues/ tags – non-Production MRB authority

- Create stress training for design engineers

- Identified safety critical parts to ensure first flight is on time; perform analysis and coordinate with affected groups to gather all needed

information

- Develop Flight Test Stress Notes Library and Flight Test Coord Sheet Library

- ECSLib focal for BT&E

Troubleshooting issues from users across the BT&E organization

Grant access for users as needed

Explain how to use the system/ help provide introduction

Boeing Company, Everett, WA

Engineer/ Scientist, Level 1, promoted to Level 2- Stress Analyst

Door Design Center (737/747/757/767/777)

08/2008 to 11/2010

- Supported fleet problems as they come up by evaluating repair proposals from the airlines, adjusting them as needed, performing analysis to be reviewed by ARs, and providing appropriate forms to the airline customers

- Gathered and provide required information for BBJ3 certification with JAA to provide to ARs

- Supported needed actions for compliance with FAA’s Aging Aircraft Safety Rule (AASR)

Screened and categorized all Door group related service bulletins and SRMs

Reviewed current Structural Repair Manual procedures for all models and revised them to meet AASR/ Damage Tolerance requirements

Performed analysis and provided substantiation for changes made to all Structural Repair Manuals/select Service Bulletins

- Work on escapement issues to support problems from suppliers

Developed and executed plan for removing fasteners from 777 fatigue article

Created presentations/ information to share and led meetings with ARs, MP&T, SDT, other groups to discuss and develop solution

Performed analysis comparing test data with fleet experience

- Supported PD efforts for KC-X proposal

Collaborate with appropriate groups to gather needed data and perform trade studies

Review existing analysis and newly developed documentation to help coordinate certification efforts

- Substantiated 747-8 Cargo Door Tests by processing test notes, videos, and data as part of validation/ substantiation package

Boeing Company, Everett, WA

Engineer/Scientist, Level 1- Stress Analyst

777 Freighter Sections 43/ 44

11/2006 to 08/2008

- Analyzed drawings and discussed drawing packages with designers in order to support release deadlines on the program

- Provide thorough documentation of all analysis performed electronically and in paper/ hardcopy

- Major analyses performed include Rotor Burst, Windmilling, Viewport Window Damage Tolerance, SRM allowables, Shoring, PDU roller loads

Performed analysis by collecting previous analyses and reverse engineering as appropriate for Rotor Burst and Windmilling

Developed original Viewport Window notes by relating the geometry to passenger window geometries, examining previous

methods and discussing with SDT & ARs to ensure method/ solution used is reasonable

Coordinated with Section 48 to revise PDU roller loads

Created coordination sheet for Rotor Burst to provide to Propulsion/ discuss analysis and answer questions as needed

-Supported KBE efforts to develop a stress check automated tool of stringer, skin, shear ties, and frames

Developed and executed a testing methodology for checking the stress check results to the drawings

Worked with designers to determine where the measurements used by the stress check tool were being taken from and how to mimic them in CATIA V4

Proposed changes to make it more user friendly

Ensured that the definitions being used by KBE for the stress check output were correct

-Supported 777F certification efforts by updating tables and providing write-ups for Fuselage formal documentation sections in accordance with deadlines

Boeing Company, Everett, WA

Engineer/ Scientist, Level 1

Post Prod 737/747/767/777 Internal Loads

06/15/06 to 11/2006

-Use of Windows/ Unix platforms: elfexceed

-Mapping of internal and external models to compare how they lined up

-Stall buffet and nose gear balancing forces

Create force cards using NASTRAN and determine if the OLOAD conditions are met

Took moments around 0,0,0 and calculated the cross products

Use of EXCEL and macros to make automated

Worked on floor beam fix in Patran – determined what CBARs, PBARs, CSHEARs, PSHEARs are needed

Boeing/ Mid-western Aircraft Systems / Spirit AeroSystems, Inc Intern

05/05 to 08/05

Wichita, Kansas

- 787 Pylon Design Intern

- Created and maintained list of existing parts in ENOVIA by collaborating with manufacturing, systems, structures, and drafters to catalogue parts

- Use of CATIA V5 to design side fairing supports and to solve systems problems

SPECIAL PROJECTS/ EDUCATION RELATED EXPERIENCE

Opportunities for New Engineers: Morphing Wind Tunnels

August 2010- August 2012

-Selected as part of a team; goal of project is to remotely automate the flaps on wind tunnel models using mechatronics

Evaluate potential actuation methods and materials; ie, piezo-electrical, hydraulic, SMA alloys using a design matrix

Research potential measurement methods, such as photogrammetry, laser tracking, manual measurements

Assist with developing solution, implementing, and testing it

2005 Michigan Space Grant Consortium Undergraduate Fellowship

April 2005- August 2006

- Exploration of thin walled pressure vessels composed of composite materials, impact of slots on performance, and how rupture can be minimized

- Research background information, obtain materials from suppliers, fabricate vessel, compile and present data, publish results, and monitor budget of the project

- Presented at Fall 2005 Michigan Space Grant Consortium Conference

- Presented at 2006 AIAA Region III Conference at Ohio State University in the undergraduate division

Senior Capstone/ Siemens Dematic Corporation

January- May 2006

- Test, design, and create prototypes of solutions to reduce vibration transmission in powered roller

- Collaborate with company and group in testing and creating prototypes that will be cost effective and meet European industrial sound level standards

- Consideration of DFM/A principles and use of a design matrix to evaluate potential designs

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