BASEM AL-KHATIB

Page * Cell: 316-***-****

home:316-***-****

acc05n@r.postjobfree.com

m

JOB OBJECTIVE

Seeking a position in the engineering field that benefits from my

educational background and extensive application of solid modeling, sheet

metal and drafting workbenches using CATIA V5 along with LCA ENOVIA, VPM,

and PDM with 15 years of experience in advanced aircraft structural design

and production support.

EDUCATION

( Bachelor of Science in Mechanical Engineering.

The Wichita State University Wichita, KS

PROFESSIONAL EXPERIENCE:

Bombardier, learjet, Wichita, KS- Contract Dec 2011 -

May 2013

Structural Design Engineer, (CATIA V5)

Learjet 85

( Develop secondary structure, equipment and racks/panels

To support the installation of electrical components

( Seat track and Pressure floor detail and installation drawings

GOODRICH AEROSTRUCTURES, Chula Vista, CA-Contract July 2011 - Dec

2011

Structural Design Engineer, C (CATIA V5)

SERIES

( Detail and installation drawings for the RH Nacelle

Boeing, Everett Seattle, WA- Contract Oct 2010 - May 2011

Structural Design Engineer, 787-9 (CATIA V5)

( Fix leading edge slat 6 Tri-Ribs detail and installation drawings

Spirit Aerosystems, Wichita, KS- Contract Aug 2005 - June 2010

Structural Design Engineer, Sikorsky (CATIA V5) Oct 2008 - June 2010

CH-53K

( 522 transition cabin frame & ramp hinge fitting design

Structural Design Engineer, Boeing (CATIA V5) Aug 2005 - Oct 2008

787-8

( 787 Fuselage Section 41 termination fitting and integrated Stringer design

( System bracket detail and installation drawings

LOCKHEED MARTIN, Forth worth, TX - Contract Oct 2003 - Aug 2005

Structural Design Engineer, JSF (CATIA V4)

( Design and detailing landing gear door hinges and fuel probe fitting.

VOUGHT AIRCRAFT, Grand Prairie (CATIA V4) June 2003 - Oct

-Contract 2003

Structural Design Engineer, 767GTTA Program

( Design and detailing forward lower lobe section 48 stringers and stringer

clips.

CESSNA AIRCRAFT COMPANY, Wichita, KS June 1998 - May 2003

Structural Design Engineer, Citation (CATIA V4) Jan 2002 - Mar 2003

Jet 3

( Flight Control system: Responsible for the auto pilot servo bracket,

aileron trim system, control system gust lock and emergency gear release

details and installations.

( Tail cone Section: Responsible for the tail cone frames, stringers and skin

structural design that includes preliminary design, detail and installation

drawings, coordinate and interface with different support groups.

Page 2

Structural Design Engineer, Sovereign (CATIA V4) Feb 2000 - Jan 2002

( Wing Section: Responsible for the wing leading edge design, detail and

installation drawings that includes leading edge skin, closeout end rib,

heat shield, diffuser, and landing lights. Provide technical design support

and incorporate latest engineering and manufacturing technologies into the

design.

( Flap and Flap Support Structure: Responsible for the flap skin, flap track

and flap track attach fitting design, detail and installation drawings.

( Fatigue Group: Responsible for detail drawings used to define a cyclic and

residual strength test article and test fixture for a monolithic spar.

Structural Design Engineer, Citation (CATIA V4) Jun 1998 - Feb 2000

Jet 2

( Wing: Responsible for the wing lower spar, strap attachment, ribs and

surround structure/fitting re-design.

Citizenship: U.S Citizen.

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