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Electrical Design

Location:
San Francisco, CA
Posted:
March 18, 2015

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Resume:

PHILIP LEE WILLIAMS

**** **** **** **

Auburn, WA 98092

253-***-**** (home)

253-***-**** (cell)

E-MAIL: ***************@*****.***

Thirty-four years (34) Electrical Engineering aerospace experience in

system design, application and testing of commercial, military and

government electronic, power and avionic systems. A quality-conscious

system design engineer with strong interpersonal skills and "can do"

attitude who works efficiently and communicates well with multi-disciplined

people. Major strengths in electrical system design, wire design, and

troubleshooting and FAA certification of avionics and electrical systems.

Over 60,000 hours in computer-aided design such as Microsoft, IBM,

Unigraphic II, Tricad, CADAM/CATIA and AutoCAD 12-14, 2000 and 2010.

(Inactive Secret Clearance - NATO - COMSEC)

Boeing/Everett, Washington 2012-2014

Electrical Engineering Design (contract)

Cabin Systems - Design engineer of the Wireless Emergency Lighting System

(WELS) for the customer introduction on the 787-8/-9/-10 programs,

comprised of the Power, Galleys, Lavatories, Crew rests, test bench

development, troubleshooting, shipside support, FAA certification.

Heath Tecna/Bellingham, Washington 2012-2012

Electrical Engineering Design (contract)

Electrical Power systems and wiring design for the modification programs of

commercial and business aircraft, comprised of the Power systems, IFE

systems, Lavatories, Crew rests, test bench development, flight testing,

troubleshooting, shipside support, FAA certification.

Boeing/Everett/Kent, Washington 2000-2011

Electrical Engineering Design

Electrical Power systems design focal for the 737 AEW&C program, comprised

of the Power Distribution Panels, SPDA (secondary power), test bench

development, flight testing, troubleshooting, shipside support, FAA

certification, modification focal and System Functional Tests - domestic

and international. Tested the Scan Eagle Drone capabilities in accordance

with the Australian military activities. Flight Deck Avionics Focal for

the 737 AEW&C program. Responsible for the interface of the avionic

systems in the Flight Deck, which included power, fuel, indication, self-

protection, communications and navigation systems. Assisted in design for

the Large Format Display System (LFDS) avionic interface system for 767-

400 airplane. Led efforts in defining the System Control Document (SCD)

and Interface Control Document (ICD). Coordinated all interface

disciplines for the Flight Deck Upgrade for the 767-200/300 airplane.

Equipment Manager for the FLIR program on the 737 Technology Demonstrator

airplane.

1. Led the interface of the avionic systems in the Flight Deck, which

included power, fuel, indication, self-protection, communications and

navigation systems which produced a new multi-role pilot interface.

2. Mentored and coordinated training of domestic Australian, Turkish and

Korean customers for the 737 AEW&C program in the power, electrical

system and avionics functional tests and provided troubleshooting

experience that improved program time response and efficiency for all

customers.

Aim Aviation/ Renton, Washington 2000-2000

Electrical Engineering Design

Design, build, install, test and troubleshoot the electrical system of a

retractable crew rest station and lavatories for the Delta MD-11 and Boeing

767 Alitalia aircraft. This includes lighting, intercommunication and PSU.

Jet Aviation/ Basel, Switzerland 1997-1999

Electrical Engineering Design (contract)

Boeing/Everett, Washington 1996-1997

Electrical Engineering Design (contract)

PHILIP LEE WILLIAMS PAGE 2

Stevens Aviation/Atlanta, Georgia 1996-1996

Electrical Engineering Design (contract)

Gulfstream/Savannah, Georgia 1994-1996

Electrical Engineering Design (contract)

Design, installation, test and troubleshoot electrical and avionics

interface systems, which includes GPWS, FMS, Entertainment and

Communication systems for Gulfstream, Boeing, Airbus, Learjet and Falcon

aircraft modifications.

. Aid in design for all electrical and avionic interface, components,

panel design, wire routing and layouts, weight reductions,

troubleshooting and testing for the Gulfstream V business jet and 747

aircraft. Led all electrical, communication, testing and avionic

design in building a functional full-scale training mock-up of the

(GV) aircraft, which produced a test lab for the avionics and pilot

training.

E-Systems, Inc./Greenville, Texas 1991-1994

Engineering Specialist

Design of all electrical interface systems to update the military

classified special aircraft for the Air Force. Led project effort in

research, budget, design and development of special systems that were

updated and added to Big Safari program that amounted to over $2 million

each.

3. Researched and implemented new electrical, communication and avionic

design procedures which improved design, manufacturing and

communication efforts with other disciplines.

4. Led and coordinated efforts for complete programs of electrical system

design that improved engineering time response and efficiency.

General Dynamics/Fort Worth, Texas 1981-1991

Engineering Specialist

Project Manager in research, budget, design, layout and development of the

unique electrical interface design for the Navy Advanced Tactical (A-12)

Aircraft, which was awarded the contract. Performed lead-engineering tasks

in writing, bidding and scheduling major engineering proposals for the F-16

program. Worked with other engineering disciplines and manufacturing from

development through delivery on several Air Force and Army contracts, which

amounted to over $2 Million each.

5. Led tooling, manufacturing, wiring and installation efforts between

vendors, co-producers and clients during all (A-12) development phases

which led to highly effective avionic equipment and wiring harness

placement.

6. Trained and managed engineers and support personnel by effectively

utilizing individual capabilities which increased departmental

efficiency through better time utilization and fewer errors.

7. Improved and implemented new design and installation which reduced 25%

weight, 20% manufacturing procedures and $20,000 per year in

engineering costs.

8. Coordinated efforts with Electronic Support Systems in developing

hardware and software which substantially reduced the number of

component parts in the flight simulators.

9. Directed the electrical and installation modifications on the F-16

Thunderbirds, which resulted in a new smoke generation system for the

show team.

EDUCATION

BACHELOR OF SCIENCE IN ELECTRICAL ENGINEERING 1981

TEXAS TECH UNIVERSITY, LUBBOCK, TEXAS



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