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