ALEXANDER Z GRUZMAN

**** ***** *** ** #**

Redmond WA 98052, USA

Tel. 425-***-****

514-***-**** Cell

E-mail: acbbgc@r.postjobfree.com

EDUCATION

Ms. MECHANICAL ENGINEER

SUMMARY OF EXPERIENCE

AIRCRAFT STRUCTURE DESIGN AND INSTALLATION ENGINEER

Twenty five years experience in aircraft engineering

o Primary and Secondary Structure design and modification

o Electrical units and wire bundles installation

o ECS, hydraulic system and APU installation

o Liaison engineering

COMPUTER SKILLS

* CATIA V5

* ENOVIA

* CATIA V4

* UG-NX4

* TEAM CENTER

PROFESSIONAL EXPERIENCE

BOMBARDIER AEROSPACE MONTREAL, CANADA

April 29, 2013 to November 22, 3013

Senior Design Engineer contract

Global 7000/8000 program

Conceptual and detailed design of Secondary Structure

for ECS and AIS installation in AFT fuselage:

Machined and sheet metal design of sub frame, intercostals,

drag links, lugs and support brackets.

BOEING EVERETT, WA

January 2011 to March 2013

Senior Design Engineer - contract

Tanker Boeing 767-2C - Section 46 Lower Fwd

Truss Keel Frames and Systems Interface design:

Architectural, concept and detailed design of 7 Truss Keel frames.

Systems Interfaces design:

Fuel Tank supports interface

Electrical and Fuel drain systems interface.

AGE Engineering Services LLC REDMOND, WA

March 2010 to January 2011

Mechanical Design Group Leader

Boeing 737-700BBJ - Structural modification and Antimissile System Integration:

Technical study at the customer site.

Conceptual Design and CDR.

Preliminary design and PDR.

Detailed design and manufacturing support.

Pod from Composite Materials for Antimissile System:

Preliminary and Detailed Design, manufacturing support and pod integration with

737-700BBJ structure and electrical systems.

Pod and Systems installation on the aircraft.

BOEING EVERETT, WA

October 2007 to January 2010

Senior Structure Design Engineer - contract

Boeing 787 - Ship Side Support Section 46 - 48,

Frames, Fittings and Systems brackets Installation support:

Problem investigation, Solution definition, Engineering revision

Boeing 747-8I Section 46.

Preliminary design of Structure Integration at STA 1741.1

Inner Skin Surface definition.

Circumferential Splice Strap, Stringers Splice Fittings, Shear Ties design

BE AEROSPACE - FLIGHT STRUCTURE DEVISION MARYSVILLE, WA

March 2006 to September 2007

Senior Structure Design Engineer - contract

Airbus300-600 - structural modification from passenger to freighter configuration.

Over wing beams and portal beams reinforcement.

Courier area ceiling design.

BOEING EVERETT, WA

September 2004 to March 2006

Senior Structure Design Engineer - contract

Boeing 747-400 - structural modification from passenger to freighter configuration.

Upper deck floor beams and frames modification.

BEDEC IAI, ISRAEL

October 2002 to September 2004

Senior Structure Design Engineer - contract

Boeing 767-200 - structural modification from passenger to freighter configuration.

Frames reinforcement - Section 43;

Floor beams design and reinforcement - Sections 41 & 43;

Electrical bundles routing, disconnect panels & bracket installation.

S.G.D. Engineering ISRAEL

December 1998 to September 2002

Mechanical Design Group Leader

Elint System Installation on TU-142M aircraft.

Wing leading edge modification to allow LRUs installation and maintenance.

Wing tip modification to allow Spiral antennas and LRUs installation.

Navigator Bay modification.

Copilot instrument panel and console modification.

Instrument bay structural modification.

Electrical bundles routing.

A kit production support

Installation at the customer site.

Chaff & Flare System installation on Cheetah helicopter.

Helicopter structural modification to allow Dispensers installation.

Tail boom reinforcement to allow the Firing controller installation.

Flight deck Central console modification.

Pilot collective modification.

Electrical bundles routing.

A kit production support

Installation at the customer site.

Elint System Installation on MI-17 helicopter.

Operator rack and Instrument rack design.

Tail Instrument box design.

Cockpit structural modification to allow forward antennas installation.

GPS antenna Installation

Passenger bay floor reinforcement.

Electrical bundles routing.

A kit production support

Installation at the customer site.

Phantom F-4RF modification to allow LOROP Pod Installation.

Aft. Cockpit structural modification to allow the MFD installation

Instrument panel and console modification

A kit production support

Installation at the customer site.

Light aircraft PA-42/42-720 structural modification to allow Radar installation.

Frames reinforcement

Radar adapter design and installation

Data Link installation

Instrument and operator racks design and installation.

Under contract to "LAHAV", IAI, ISRAEL

Leader of Engineering Support Group

Phantom F-4E flight test airplane

Acting within MRB ( Material Review Board )

Defining the ways of repairing and corrective action.

Drawing and Route Card revision.

BOEING EVERETT, WA

April 1998 - November 1998

Electrical Installation Design Engineer - contract

Responsible for sections 41 & 42 wiring modification of 747 - 400 in order to meet customer requirements. ( NWA )

Wire bundles, disconnect panels & bracket installation

Electrical unit installation

BEDEC IAI, ISRAEL

July 1995 - April 1998

Senior Structure Design Engineer - contract

Boeing 747-200 - structural modification from passenger to freighter configuration:

Frames and floor beams reinforcement;

Cargo plug and main cargo door modification;

Control panel and cargo door control switches installation

F-4E fighter plane upgrading

Structure modification - to meet new electrical system requirements:

LRU installation;

Wire bundles, disconnect panels & bracket installation;

Flight test units installation.

CANADAIR, BOMBARDIER Inc. MONTREAL, CANADA

December 1988 - January 1992

STAFF SPECIALIST

Regional Jet project

Preliminary design of the wing extension:

Front spar and Rear spar modification,

Landing gear fairing layout and detailed design

Layout and detail design of the wing - fuselage fairing, using the composite materials.

Airbus project

Liaison engineering:

Acting within MRB ( Material Review Board )

Defining the ways of repairing and corrective action.

Drawing and Route Card revision.

IAI, ISRAEL

January 1984 - December 1988

Structure Design and Installation Engineer

Lavi fighter plane project

Aft. Fuselage primary structure detail design.

Electrical, hydraulic and fuel systems units installation

Wire bundle and hydraulic routing

EPU and ECS installation

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