MARK BURTON

571-***-****

acz5ro@r.postjobfree.com

SUMMARY: Mechanical Design Engineer with 25 years’ Aerospace Design and Production experience

EXPERTISE: CAD/CAM: 18,000+ hours CATIA V4 & V5 in Composites, Solid Modeling & Surfacing

Structures & Payloads: Primary & Secondary Fuselage, Wing, Empennage, Interiors

Systems: Hydraulic, Electrical, ECS, Air Ducting, Fuel, Powerplant, Avionic Rack and Panels

MRB Liaison: Dispositioned Discrepant Metallic and Composite Detail Parts and Assemblies

EXPERIENCE:

SIKORSKY AIRCRAFT CORP, Jupiter, FL, March 2016 to present

Mechanical Design Engineer – Performing design support for CH-53K King Stallion heavy lift cargo helicopter for United States Marines testing and certification program. Designing and modifying primary structures to incorporate flight test instrumention for loads pallets for both internal cargo and troop carrying missions. Incorporated modifications to titanium frames and composite bulkheads for external heavy lift cabling and winching systems. Utilizing CATIA V5 for 3-D for concept and design and 2-D for drawings and installation plans and instructions, and SAP for Bills of Materials.

GULFSTREAM AEROSPACE, Savannah, GA, Aug 2015 to Nov 2015

Mechanical Design Engineer – Concept and design of static and fatigue test fixtures for primary structures of G500 and G550 business aircraft. Projects include Composite Aft Engine Beam and Aft Upper and Lower Composite Bulkhead test fixtures. Designed Wing Tip with Winglet box for static test fixture. Designed 2 Point (Wing) Roll test fixture for complete test aircraft in floor mounted welded/bolted steel structure incorporating numerous Wiffle Trees. Utilized CATIA V5 3-D for concept and design, 2-D for drawings and SmarTeam for Bills of Materials.

HONDAJET, Greensboro, NC, June 2014 to July 2015

Mechanical Design Engineer – Performing the incorporation of Engineering Revisions for the HA-420 HondaJet aircraft ECS, Fuel, and Powerplant systems. Responsible for creating Modification (MOD) Routers including MBOM’s (Manufacturing Bill of Material) which include complete work instructions for Production Floor Technicians. Duties include MRB review and approval Engineering CR’s (Change Requests) ensuring manufacturability of parts, assemblies and installations. Additional tasked to ECS systems for Wing Anti-Ice, Bleed Air, Cabin and Cockpit Oxygen, A/C, Ducting, and Water & Waste Systems to revise Master Routers for all new Engineering changes. Attended daily CCB (Change Control Board) reviews for manufacturability and producibility. Utilized CATIA V5 3-D for design and 2-D for drawings, SAP and Teamcenter for Bills of Materials, planning and work instructions.

TRIUMPH AEROSTRUCTURES – VOUGHT AIRCRAFT DIVISION, Grand Prairie, TX, Feb 2013 to May 2014

Mechanical Design Engineer – Performed investigation and resolution of manufacturing issues for Boeing 747-8 Horizontal Stabilizer build center. Work coordinated with MRB group to create predispositions then submitted to expedited disposition process. Tasks included resolution of skin to stringer mill-pad and fastener drilling mis-locations including detailed 3-D Clash and Clearance studies. Provided corrective action documentation for skins, hinge ribs, actuator ribs, and rib chords. Created and modified production tooling and drilling templates including shop aids and drilling guides for skin fastener locations. Created numerous CATIA V5 3-D models and assemblies from Boeing 2-D drawings and 3-D models. Utilized CATIA and SAP for planning and inventory investigations of outdated, superseded, and obsolete parts & assemblies.

BOEING AIRPLANE COMPANY, Charleston, SC, Feb 2012 to Jan 2013

Mechanical Design Engineer – Providing Shipside Engineering Liaison support for the Aft Fuselage, ECS, and hydraulics for 787 Dreamliner composite aircraft. Tasks included MRB support to resolve recurring and repetitive line issues. Investigated and resolved integration and assembly issues for build team mechanics. Provided corrective action resolutions (ARF), modified work instructions (SOI), and parts lists (MBOM). Performed Clash and Clearance analysis to resolve part interferences and assembly drilling and machining errors. Previously assigned to MARM Group for the creation and maintenance of sub-assembly and detail part documentation provided to supplier partners. Graduated Boeing ME Academy Training. Utilized Delmia and 3DVIA to red-line shop floor orders and issue line tags in Velocity system.

BOMBARDIER LEARJET, Wichita, KS, Dec 2009 to Apr 2011

Mechanical Design Engineer – Provided Engineering Liaison support, integration and design support for primary structures, hydraulics, Environmental Control Systems (ECS) of new Learjet 85 all-composite business jet. Interfaced with on-site vendors to coordinate design and manufacturing plans. Projects included fuselage and fairing frames, longerons, gussets, brackets and clips. Designed fairing access doors and hinges. Responsible for design of mounting brackets, tie-rods, and attachment hardware for ECS, fuel inerting, bleed air, anti-ice, and fire suppression systems and components. Attended daily team meetings. Utilized CATIA V5 and Enovia.

GOODRICH AEROSPACE, Oldsmar, FL, Dec 2007 to Jun 2008

Mechanical Design Engineer – Design support for High Intensity Discharge (HID) fuselage mounted electro-mechanical lighting systems for Boeing 787 (Dreamliner) aircraft. Investigated and resolved integration issues involving brackets, fasteners, gaskets, and labeling. Created and reviewed processes and procedures to conform to Boeing (BAC) requirements including vibration, explosion, Safety of Flight (SOF), and maintainability.

LOCKHEED MARTIN AERONAUTICS CO., Fort Worth, TX, May 2006 to Aug 2007

Mechanical Design Engineer – Provided engineering support for F-35 Joint Strike Fighter (JSF) Aft-Fuselage IPT. Responsibilities included Material Review Board (MRB) dispositions and redesigns. Created corrective action documentation for discrepant composite skin panels and metallic machined and forged parts including hydraulics, titanium bulkheads, formers, frames, and brackets. Created and maintained manufacturing plans, Bills of Materials (BOM’s), and illustrated work instructions. Investigated and resolved manufacturing issues providing onsite engineering support for factory floor. Attend weekly design review meetings. All 3-D analysis performed on CATIA V5. Utilized Metaphase PDM Lifecycle for planning and dataset releases.

BOEING DEVELOPMENT CENTER, Tukwila, WA, Jul 2005 to Feb 2006

Tool Design Engineer – Designed test fixtures for 747 Large Cargo Freighter (LCF) certification program including Whiffle Tree load distribution rigs for fuselage static and fatigue tests. Designed floor-mounted

assembly fixtures for 787 Dreamliner Wing-to-Body Joint test fixture including Assembly Jigs (FAJ) and lap splice joint Drill Jigs (DJ). Designed wing tip test box for X-45J Unmanned Combat Air Systems (UCAS) test program for fatigue and static testing. Design tasks utilized CATIA V4 & V5.

GOODRICH AEROSTRUCTURES, Chula Vista, CA, Aug 2004 to Jun 2005

Mechanical Design Engineer – Assigned to Lockheed C-5M Re-Engine Re-Pylon (RERP) program. Provided engineering support for machined fittings, brackets, composite panels and fairings. Interfaced with stress and manufacturing groups to resolve production discrepancies. Created and maintained manufacturing plans, Bills of Material (BOM), and work instructions. Investigated and resolved manufacturing issues. Provided producibility inputs to design. All 3-D analysis performed on CATIA V4 and V5. Utilized Metaphase PDM.

Tool Design Engineer – Designed Assembly Tooling for manufacture of C-5M Pylon sub-assemblies. Utilized CATIA V4 and V5, and PDM Metaphase TeamCenter for release of product structures and tooling.

LOCKHEED MARTIN AERONAUTICS CO., Fort Worth, TX, July 2003 to Mar 2004

Tool Design Engineer – Assigned to F-22 Raptor & F-35 Joint Strike Fighter (JSF) Fuel Test Lab. Supported design of hydraulically articulated full-scale fuel system test stand. Designed airframe structural test fixture components such as bulkheads, shear webs, spars and ribs. Interfaced with fuel and electrical system groups to resolve routing conflicts and interferences. Design tasks performed on CATIA V4 and V5.

1986 to 1996 Experience at other companies – Boeing, Canadair, Space Data, and Motorola Aerospace

EDUCATION:

Mechanical Engineering – University of Arizona, Tucson, AZ

Computer Aided Design – ITT Technical Institute, Phoenix, AZ

Geometric Dimensioning and Tolerancing – Boeing Airplane Company, Seattle, WA

CATIA V5 and V4 Training Matrix - Boeing Airplane Company, Seattle, WA

CATIA V5 Composite Part Design – Keltia Design, Seattle WA

Contact this candidate