Engineer Engineering

henry marquez

***** **** ******** **.

Dallas, Texas 75287

972-***-**** ? **********@*****.***

MRB and Airframe structure designer

EDUCATION & ACADEMIC EXPERIENCE

Bachelor of Science, Mechanical Engineering - University of Oklahoma, Norman,

Oklahoma - December 1978

Master of Science, Engineering Mechanics - University of Louis, completed 18

Hrs. credit toward Master Degree, St Louis Missouri -

Associate of Science, Civil Engineering - Santa Maria University, Caracas,

Venezuela - July 1974

PROFESSIONAL EXPERIENCE

CTS International (Contract with Gulfstream January 2012 - February

Aerospace) 2014

MRB Structure Engineer Tech Spcl II Savannah, Georgia

. Develop CATIA V Models in data base of G-650 Aircraft, to enhance the

ability to understand how assemblies are installed, to meet program

configuration and enhance an optimum design repair as long as the

structural integrity is maintained and kept within the Primary and

Secondary structures definition, Including other appropriate signatures and

documentation per GAC guidelines and meet FAA polices.

. Provide MRB design repairs maintaining the requirements of design Load

Path without affecting next assembly installation, write Engineering

disposition on non-conforming metal parts, create a schematic proposal

design repair, and ensure the structure integrity of the Airframe is

maintained.

. Perform Engineering disposition on non-conforming on Composite materials,

create a schematic lay-up proposal design repair, and ensure the structure

integrity of the Airframe is maintained.

Assemblies involved:

. Mate Fuselage and Wing: Body Fairing structure, Wing structure LH & RH,

Landing Gear ( Nose and Main landing Gears)

. Fwd / Fwd Mid / Aft Mid / Aft Fuselage Structural sections, Longitudinal

splices, circumferential splices

. Surface control: Leading Edges, Spoilers, Aileron, Flaps and Fix Trailing

Edge.

. Final Assembly: Pre-rigging and rigging Flap operations, Support Outside

Ops. and Modification on 38 Aircraft for C of A, and FAA certification.

Bell Helicopter-Textron June 2008 - January 2012

Sr. Liaison Engineering Specialist Hurst, Texas

Sr. Liaison Engineering Specialist June 2008 - January 2012 Bell Helicopter-

Textron - Hurst, Texas

Develop CATIA IV Models 2D or 3D Models for Liaison Engineering on V-22

Program; including short cuts to develop design repair Models for MRB

Liaison Engineers at Amarillo site. Improve the usage of different

functions applicable to specific design without affecting the next assembly

installation.

. Develop an Engineering disposition on non-conforming parts (Composite and

Metal parts); including sketches or schematic to facilitate Mfg

installation. Hand writing on structure design analysis for MRB Engineers,

coordinated with manufacturing, quality, and Local customer

. Assemblies and installation involved: V-22, H1, 412, Legacy Commercial

and Military.

Lockheed Martin Aeronautics July 2002 - April 2008

Aeronautical Engineer Staff Fort Worth Texas

F-16 Falcon, AFT Fuselage, Wing and Empennage

. Collect and organize engineering disposition from REA (Request

Engineering Action), formulate structural design repairs to maintain

integrity of the structure to the original design envelop. ECN

(Engineering Change Notice) were written to upgrade changes and

Aircraft Retrofits on allied countries to update new system, either

structure, Avionics, depends of next configuration is needed and test.

F-22 Raptor (Mid-Fuselage/Air- Frame).

. CATIA IV Models were used as a research tool to implement the new

requirements of the structure and improve the new design and

Modifications. Responsible for on-site support of F-22 Mid-Fuselage,

support Liaison activities, Manufacturing. Support Producibility

Designs to reduce weight/cost and Configuration Management.

Vought Aero Product April 2000 - July 2002

Liaison Design Engineer (Contract) Dallas, Texas

Responsibilities were to create disposition of non-conforming detail,

assembly and vendor parts to maintain the original design load path and

integrity of the aircraft. Certified Material Review Board for Boeing

Aircraft, and provided interpretation of drawings and specifications for

manufacturing, quality, inspection, procurement quality engineering, buyers

and other groups to assure corrective action had been accomplished to

reduce the numbers of non-conforming parts and assemblies.

. Boeing program (737, 747, 757, 767, 777),

. McDonnell Douglas Aircraft (C-17 Airlifter)

. Northrop-Grumman (Global hawk)

VARO - Electronic Packaging January 2000 - April 2000

Lead Mechanical Engineer Garland, Texas

Review all drawings for each Program from Designers. Check Dimensioning &

Tolerances, Verify the structure integrity for each Electronic Packaging

are maintained by Analyzing Statically, ensuring the Margin Safety is

positive. The requirements for NAVY / SEA Power Supply Enclosure to be

analyzed to 115 G's and the Internal Power Supplies Module to 300G's.

Dynamic Analyses of CCA (Circuit Card Assembly) has its Frequencies

According to NAVY / SEA Specification. Advice for drawing changes to

improve Design maintaining Manufacturing requirements. Completed CDR

(Critical Design Review) successfully with outstanding presentation for

Lockheed Martin Launching System and NAVY / SEA.

Assemblies involved:

. PPS (Programmable Power Supply) for the Cruise Missiles Navy-Ship,

Power Supply for U-2 CIA Aircraft, Power Supply for Navy Submarine,

Proposal Power Supply 5 Units for the F-16 Aircraft (Israel Air

Force), and Proposal for Missile Launcher- Saab Aircraft Sweden Air

Force.

Raytheon System Company June 1998 - September 1999

Lead Mechanical Engineer Arlington, Texas

Lead Mechanical T- 45 OFT / IFT (Operational & Instrument Flight Trainer)

simulator for the NAVY. Supervised 8 detail designers, reviewed drawings,

wrote Engineering Change Notice as required, red line drawings submitted to

a designer to incorporate new changes to meet the baseline requirement. New

designs are created Submitted to a designer to incorporate new changes and

release drawings. Stress analysis (statically) is performed on new or

existing design to ensure the design load is structurally adequate to

maintain the proper margin Safety.

Completed Functional / Physical Configuration Audit for hardware

engineering, maintained 100% on Schedule. Performed MRB (Material Review

Board) engineering on non-conforming details or assemblies. Certified MRB

Engineer.

Assemblies involved:

. T- 45 cockpit OFT / IFT, canopies, trainer instructor platform,

projector platform, HOST computer hardware, safety rails, hand rails,

control loaders for the brake, arresting hook, landing gears, pilot

seat, seat frame, A/C unit, OFT dome structure.

Lockheed Martin Tactical Aircraft March 1997 - June 1998

MRB Airframe Design Engineer (Contract) Fort Worth, Texas

MRB Engineer for the F22 Stealth Fighter. Duties include: Collect and

organize engineering disposition for non-conforming parts and formulate

structural design repairs to maintain integrity of the structure to the

original design envelope. As a Structural Design Engineer, ECN.'s were

written to update changes to meet existing structure. CATIA IV F22 Models

were used as a research tool to implement the new requirements of the

structure and improve the new design drawings on Detail, Sub-assemblies,

installation, and Final Assembly drawings. Assemblies involved:

. F-22 Mid center-aft fuselage (frames, bulkheads, and fittings), side

weapon bay doors.

Vought Aircraft August 1996 - March 1997

Airframe Design Engineer (Contract) Dallas, Texas

Design detail and solid-Engineering model 3-Dimensional from 2-Dimensional

engineering wire-frame through CATIA IV, includes: shear clips, shear webs,

fail-Safe angles, angle-doublers, clips and straps. Build sub-assembly 3-D,

detail (solid E-Models) merged from Engineering -files as needed and

located per engineering Drawing. Checked for interference's using Solid

Functional Clash. Sub-assembly drawing; create a drawing and data set which

includes all Sub-assembly 3-D solid-M Models and fasteners. Maintain Boeing

drafting and ASME (GD&T) standards, assembly:

. 747 Accurate Fuselage Assembly, SPA 2140 that includes the aft bulk

cargo door panels

Lockheed Martin Tactical Aircraft March 1991 - June 1996

Airframe Design Engineer (Contract) Fort Worth, Texas

Design frame station interfacing with Armament, ECS, and Avionics and Fuel

groups to improve the structural frame to accommodate adjacent equipment.

Design F-1 tank (shear webs and fuel floor) to reduce weight and gain fuel

capacity. Conducted trade studies in weight reduction on frames and

bulkheads; frame tabs Vs structural plates, upper frames to minimize weight

to accommodate avionics boxes and lower frames to clear the envelope of the

weapons bay and missiles. Construction of solids of the above frames for

trade studies for final design and installation drawings.

. F-22 Program, Mid-Fuselage working experience in CATIA IV.

Aeronavali-Alenia Aircraft June 1990 - December 1990

Design Stress Liaison Engineer (Contract) Venice, Italy

Modification of cargo floor main cabin, lower fuselage, and installation of

structural doublers to close passenger windows. Fabrication of a new

structure skin, and cargo door assemblies. All design and installation were

revised prior certification. Conducted structural analysis /statically on

individual design repairs. Modification (maintenance, overhaul and repair)

were reviewed prior flight for FAA certification. Assembly: DC-8 cargo

modification and 707 Boeing N.A.T.O.

Arkansas Aerospace Co March 1990 - May 1990

Design Stress Liaison Engineer Little Rock, Arkansas

Redesign Flight deck, Upgrade Avionics, Cabins structures, and Structure

maintenance. Engineering Orders, repair sketches are written to modify

specific structures to meet customer specification. Advance Design Change

Notice is written to change drawings to meet existing structure of aircraft

to accommodate equipment. Provided MRB disposition, for interior initial

installation and modification. Basic structural design analysis is

accompanied to ensure the structure designs are stable and meet Federal

Aviation Administration requirements. Structure analysis reports were

submitted to DER & FAA representatives. Assemblies:

. BAE 125-700, BAE 115-800 (British Aerospace Aircraft) and the G-IV

(Gulfstream Aircraft).

McDonnell Douglas Aircraft December 1987 - December 1989

MRB Liaison Engineer (Contract) St. Louis, Missouri

Certified MRB Engineer, provided MRB design repair, review design

accordingly, write Engineering Change Notice (ECN) to improve design, hands

on structure design analysis coordinated with manufacturing, quality, Local

customer.

Assemblies involved: fuselage, wings, Stabilator, pylons, canopies for

Harrier II; forward-center fuselage, wings, canopies, gun-ammo packs, and

fuel tanks for the F-18; wings, horizontal Stabilator, forward-aft

fuselage, canopies, pylons and landing gear for the F-15; bulkheads, nose

landing gear, cargo floor, flight deck, windshield sill, upper-lower, cargo

doors, ramp assembly for the aft fuselage.

Crew doors, main landing gear pods assembly for the center fuselage. Upper

skip flaps for the wing assembly and parachute storage cylinder for the

stall recovery chute, and tail cone assembly (aft fuselage) for the C-17.

LTV Aero product March 1985 - November 1987

Design Lead Liaison Engineer Dallas, Texas

Assigned to the 747, 757, and DC 10 as Engineering Liaison. Collect and

organize analytical and theoretical information associated with research

study and system performance and Material Review Board including

fabrication and installation problems on the 747 (provide disposition of

non-conforming parts and formulating repairs). Lead Engineer for Liaison

Engineering department on 757 Program. Certified Material Review Board

Engineer.

Followed up on manufacturing for specific structural design repairs are

completed per engineering disposition. Assemblies involved:

. 747 horizontal stabilizer, upper and lower lobes, pressure bulkhead

and body;

. 767 horizontal stabilizer; 757 pressure bulkhead, horizontal and

vertical stabilizer, tail cone and aft fuselage

. DC-10 horizontal stabilizer.

McDonnell Douglas February 1979 - March 1984

MRB Liaison Engineer Tulsa, Oklahoma

Responsible for MRB Liaison engineering activities, including disposition

and repairs of non-conforming parts. Process of parts during manufacturing,

machined, forming welding, spot welding and/ or painting. Engineering

Orders (EO's) were written for necessary changes to improve design.

Certified Material Review Board Engineer.

Worked on the F- 4 Phantom modification program, DC-8 Cargo Modification

and re-engine program. KC-135 Aircraft Modification, F-18 Pylons, F-15

Conformal Tanks and Missiles, Harpoon assembly.

Spartan School of Aeronautics March 1980 - December 1984

Instructor Tulsa, Oklahoma

General Education Dept. teaching Physics I, Physics II, Manufacturing

Process, Quality control analysis, and Lab. Assistant in Non-destructive

testing.

CERTIFICATIONS

McDonnell-Douglas Engineering Training School.

. Military Standards and Military Specifications, ISO 9000, Structural

Analysis, Fracture Mechanics, Composite Analysis, Design Load Path,

Fundamentals of Aircraft Strength Analysis., Tolerances studies:

Assemblies, installation, details, and Fasteners.

Boeing MRB Engineering Training-Tested and Certified

. Hand writing Structural Analysis, Repair Application, Fatigue, fuel

sealing process, MRB Process, Corrosion Protection, Non-Destructive

Testing.

Lockheed Martin Aeronautics, Fort Worth Texas

. Windows 2010 XP, MS-Doc, PowerPoint, and Excel

. CATIA V, Basic, intermediate and Advance at Lockheed Martin

Aeronautics Engineering training school- January thru April, 2008.

. CATIA V Repair design for MRB Engineer at Gulfstream Aerospace

Production Engineering- 2013

. GD & T (Geometry Dimensioning & Tolerances drafting) at Lockheed

Martin Engineering training classes, annually.

ACCOMPLISHMENTS & AWARDS

. Tornado Warning System at University of Oklahoma, 1978

TOOLS & TECHNOLOGY

. CATIA IV completed over 10,000 Hrs.

. Provided CATIA IV training for MRB Design Repair Engineers at Bell-

Helicopter-Textron in Amarillo Texas-site.

. Invented a process in Autoclave to cure cycle to repair Honey Comb

Panels in the V-22 Engine bay, the program was name after my name(

SWIM HENRY), improving the lay-up compaction/every 3 plies, to remove

entrapped air and reduce the core shear strength braze at Bell

Helicopter Textron. Reduce cost and schedule for Mfg.

PUBLICATIONS

. Provided tutorial document for Structural Analysis for Liaison

Engineer on Metal at Bell Helicopter-Textron

. Design structural Titanium radius block to be installed on Composite

material on V-22 Wing area at Bell Helicopter-Textron

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