Adam M. Spencer 955 Harbor Island DriveSan Diego, CA 92101Ph 438-496-1910skixxx@msn.com

General experience: 25 Years in New Aircraft composite and metal structures and systems detail design; for Bombardier, Boeing, Gulfstream, IAI, Grumman, Lockheed Martin Skunk Works, Aeronca, Precision Conversions, ROHR, Fairchild Republic and ATG.10 Years in Flight test instrumentation design for; ATG, Boeing, and Bombardier3 Years in Computer mechanical design for IBM.2 Years in Vehicle design for Freightliner and J I Case5 Years in Single/ Multiple family home design and construction

US Secret clearance 1980 -1983, Fairchild RepublicUS Secret clearance 1997-1998, LMSW

Citizen of USA and Canada

EDUCATION University of Washington Certification in Virtual World …………..2010 Duke University....................... Industrial Design studies……. 2000 University of Washington.............. …Engineering studies ………1976 Mesa Community College................. Computer Science .……….1994 Edmonds Community College............. Mathematics studies…. 1974 Everett Community College……Aerospace design certificate…… 1973 Yakima Community College....General Engineer studies……….…1972

EMPLOYMENT

Bombardier in Montreal QuebecSN Flight Test Design Engineer, on our Corporation has contract with July 2012 to present. I am creating the flight test instrumentation layout drawings designing flight test equipment and wire harness installations for the; G7000 and G8000, FT aircraft using CATIA v5 and VPM navigator.

Gulfstream Aircraft in Savannah GaDesign Tech II, On contract to Oct 2011 to April 2012. I Designed systems for the next generation G650 series aircraft, Designing ESC, Hydraulic, water and fuel lines using CATIA V5 tubing and sheet metal programs, ensuring GD & T tolerances met

ANSI Y14.5M-1982 for 3d parts. I conceptualized a new ECS hot/cold air manifold, which reduced cost and weight. CATIA V5 500 hours.

Boeing Aerospace Corp. in the Puget Sound, WAFlight test Design and Manufacturing EngineerSept 2008 to Aug 2011. Designed and planned Flight test installations for wire harnesses, instrumentation and modified support structure for 737, 747, 777, and 787 and converted CATIA V4 datasets to 3d CATIA V5 ensuring the data, GD & T annotation and tests conformed to FAA specifications. CATIA V4 & V5, ENOVIA, IVT, DELMIA,VELOCITY, REDARS 3000 hours

ONSNO LLC / owner Inventor / San Diego, CA Dec 2006 to present.Designed and patented a ski device with my wife Vanessa Spencer. We designed, fabricated and built 2 prototypes from Aluminum material. Created the NC programs and milled all the parts on a 4 axis end mill. Tested the device and converted the design to plastic injection molded parts.

Learjet in Wichita/MontrealLead Design Engineer/ Mar 2008 to Aug 2008 Using ENOVIA to create the skeleton file structure used to develop the Digital mock up of the new composite Learjet. I reviewed all the preliminary datasets created by various Engineering firms and department. Then organized and filed each system or structure into the ENOVIA driven DMU. Created installation reports and calculated and verified load factors, review stress reports, and GD & T notes to insure the design met Learjet specifications. CATIA, ENOVIA V5, 600 hours

Boeing Flight Test in Seattle, WAFlight test Engineer/ Boeing 787, Sept 2006 to Feb 2008.On contract to, Boeing to review engineering data and defined the location in 3D DMU of 787 for all the strain gages, thermocouples, wire harnesses and other electronic test systems required to certify the 787 per FAA and Boeing standard regulations. Designed and planned test installations for 747F insuring the data and tests conformed to FAA specifications. CATIA V5, ENOVIA, 4000 hours

Aviation Technology Group in Englewood ColoradoSpecial Projects Engineer Javelin VLJT Feb 2005 to Aug 2006. I worked as a direct employee at ATG as the Lead Designer on the Prototype aircraft in charge of the DMU and aircraft prototype. As the lead I coordinated 28 different companies design

efforts loading the DMU with model files and creating presentations used to determine production configuration, review tolerance studies using GD& T per ANSI Y14.5M-1982. Solidworks, UG NX-3, CATIA V 5 and Team center 2500 hours

Precision Conversions in Everett WAAircraft Door Design Specialist, Jan 2003 to Jan 2005, On contract to design and analyze a Crew Entry Door and Sub systems design for 757 cargo conversion from Passenger Aircraft. The crew entry door, I designed to be a one piece Aluminum machined part which held all the mechanical parts in exacting position. Using Solid works as a design tool created 3D Models of the 757- 41 section primary and secondary structures, Crew Station and Crew Entry Door. Prepared Maintenance manual and meet the FAA FAR 25 requirements. Solidworks 2000 and Cosmos-works 2000 hours

IBM in Research Triangle Park, NCMechanical Design consultant, May 1999 to December 2001: on contract to responsible for new product design and Production configuration management. I worked directly with the Industrial design "Richard Sapper" and marketing to generate Computer Desktop / Server designs and coordinated the design with the subcontractors using CATIA and PRO-E.

Lockheed Martin Skunk Works in Palmdale CASenior Engineer / Lockheed Martin Skunk Works, Palmdale CA, I worked Configuration Design and Support x-35 known now as the JSF Aircraft, , Sept 1997 TO Aug 1998: On Contract to LMSW in Palmdale, CA. Configuration Management" for Joint Strike fighter 'JSF' aircraft X35, I used CATIA 3d advanced surfacing and kinematics, to define and integrate the Aircraft Systems into the primary structure. I Designed parts of the Main landing Gear, Flight Control Actuators, Engine Mounts, Fuel System, Arresting Hook and onboard Computer installations.

Nordam Industries in Tulsa, OKSenior Design Specialist DORNIER 328-300 Nacelles May 97 to Sept 97: On Contract, I was responsible for the design and analysis of Nacelle cowl and Engine Wire-harness designs for Pratt& Whitney Turbine Jet Engine used on the Dornier 328-300.

ROHR Industries in San Diego, CANacelle Design Specialist, MD 95.Boeing 717 Aircraft. Nov 1996 to Mar 1997: On contract, I created 3d models using CATIA V4 of Sheet metal parts used on the MD-95 Engine Cowl and Thrust reverser, all the documents met FAA FAR 25 certification regulations. Designed Space shuttle surface tile geometry definition used to build the heat shield tiles for the X-33.

Boeing in Wichita, KS,Nacelle Design Engineer April 1996 to Oct 1996: On contract, I used CATIA Advanced Surfaces to produce tooling models used to produce the Composite Nacelle Structure for 777 and manufacturing specifications. Design 3d models of the thrust reverser mechanisms.

Freightliner, in Portland, OregonChassis Engineer I used CATIA to design modules for Chassis and Configuration management for Trucks Freightliner Trucks Portland Oregon. Nov 1995 to Mar 1996: On contract, I Designed 3d models of the: Chassis, Exhaust System, suspension and Drive axles, and Engine firewall Compartment ensuring GD & T tolerances met ANSI Y14.5M-1982 using CATIA.

AERONCA, Middletown, OhioNacelle Design Consultant, Boeing 737 Engine Cowl. Jun 95 to Oct 1995: on Contract to I redesigned the 737 Composite Cowlings into Sheet Metal type construction for SWA ensuring GD & T tolerances met ANSI Y14.5M-1982 using CATIA.

Gulfstream in Savannah, GALead Engineer Mar 1995 to Jun 1995: on Contract to design the G5 Engine Pylon and configuration management of the G5 composite Pylon Structure and Engine Mount to Meet FAA, FAR 23 Certification using CATIA

Boeing, in Everett, WALead Design Specialist Mar 1994 to Feb 1995: on Contract to Lead the creation of 3D solid mockup models of the 767 Aircraft primary and secondary structure from 2d drawings ensuring GD & T tolerances met ANSI Y14.5M-1982.

JI CASE, Hinsdale, ILMechanical Engineer Apr 1992 to Nov 1992: on Contract, I designed the mechanical parts and configurations for the Combines and the Automatic and manual transmissions using CATIA V3 3d models. I created 3d model of each gear, bearing, spacer, and sand casing used on various off-road Equipment such as tractors, combines and implements.

Boeing in Renton, WAInteriors Door Designer / Sept 1991 to Feb 1992: on Contract to Boeing, Renton, WA. Using surfaces and volume solids I designed solid models of the 777 Interior Composite panel entry door and secondary support Structure.

Boeing in Wichita, KSInstrumentation Structures Engineer / Jan 1990 to Sept 1991: On Contract to Boeing, Wichita, KS. I redesigned all the 777 cockpit structure from Aluminum to Titanium structure on in the Cockpit of the 777 CATIA V3 500 hours. I created kit parts for the 737, Cargo Door Mechanisms using INK and MYLAR ensuring GD & T tolerances met ANSI Y14.5M-1982.

Canada Air Montreal, PQ, CanadaComposite Engineer / May 1988 to Dec 1989: On Contract I designed the Tail cone and Wheel-well using composite Kevlar and graphite/carbon fibers, and molded antenna housing ensuring GD & T tolerances met ANSI Y14.5M-1982.Cadam1500 hours, CATIA v2 400 hours

McDonnell Douglas Helicopter, Mesa AZComposite Structure Consultant /, Jun 1987 to Apr 1988: On Contract, I Created design layouts and concepts for preliminary design proposals for all the composite parts and coordinated the Configuration Management of the Aft Spar with Long Beach CA., using the CADD-3 system 2500 hours.

McDonnell Douglas, Long Beach, CAStructures Engineer Dec 1986 to May 1987: On Contract designed the Precision forging for the Primary Structure on the MD11 Wing to Body interface and wing to body composite fairings. CADD3 1000 hours

ROHR Industries, San Diego, CANacelle Design Consultant Jun 1986 to Nov 1986: On Contract to. I designed a common Metal and Composite Nacelle to be used on Boeing, AIRBUS, MD aircraft, for all Rolls Royce, Pratt & Whitney and G.E., Turbine Jet Engine

Boeing, in Renton WACorrosion EngineerBoeing, Renton, WA: Nov 1985 to May 1986: On contract, I designed a Configuration management system to apply Corrosion protection treatments for the 757 737,727 and 707 aircraft. I created the aircraft specifications and Centerline diagrams for 100 Seat 737-400. CV4x 1400 hours

Grumman, long Island, NYLead Engineer Apr 1984 to Dec 1985 on Contract, I designed the G4 and F100 Thrust Reverse doors and the Composite Pylon Structure and secondary structure for systems on the G4. I supervised 10 designers to complete the detail work on CADAM for the Gulf-stream G4 Fokker F100 Aircraft ensuring GD & T tolerances met ANSI Y14.5M-1982.

Israeli Aircraft Industries, Tel Aviv, IsraelEngineer /, Sep 1983 to Mar1984: On Contract to I used the Nikki Computer System to design primary and secondary structure, systems and Ventral Fins for Aft Fuselage of the LAVI Aircraft. Nikki system 2200 hours

Republic Fairchild Industries, Farmingdale, NYStructures Designer / Jan 1980 to June 1983: On Contract I Designed the Primary Engine support structure and Cowl for the Saab 340 aircraft, and I created the ejection seat installation A-10B, a two-seat version and I redesigning the ballistic Foam around the A10 Flight controls. CADAM 1000 hours

Boeing, Everett, WALead Drafter / April 1971 to Dec 1979: Direct employee and student at U of W. I designed primary and secondary structure used on the 747SP fuselage and wings ensuring GD & T tolerances met ANSI Y14.5M-1982 using INK and MYLAR.

Also spent many summers building designing and building single and multiple family residents, last project was 12 condo’s I designed and built at 610 East Lake Stevens Road in Lake Stevens Washington in early 1990’s.

Computer program hours CATIA V5, 15k+, CATIA V4, 8,700 hours, CATIA V3, 8,600 hours, CATIA V2, 1,400 hours, , CATIA: 3D Solids, Advanced surfaces 10,000+ HoursTotal CATIA hours= 28,300

ENOVIA 5000 hours, MILLMASTER NC MILL 2000 hours, SOLIDWORKS 5,000 hours COSMOS Stress and loads 4000 hours, CADAM 3000 hours, UG 2 certified at Motorola University, NX 3 certified at ATG , SL design and build 1000 hours.