ANTHONY ZEMANOVICH, Eng.

Rosemere, Quebec

450-***-**** u acq2vs@r.postjobfree.com

PROFILE

Bilingual Aerospace Engineer, trustworthy, detail-oriented, persevering, versatile, and customer oriented. Able to complete projects on time and to cost. Capabilities include:

Aircraft Hydro-mechanical, Flight Control Systems

Aircraft Liaison, Catia v4 + v5 proficient

Aircraft Component Design & Installation

Gas Turbine Externals Design

Customer Support Engineering

Worked on the following aircraft programs:

Airbus A380

Boeing 747-8

Bell 429

Bombardier Dash 8-100/300/400

Bombardier CRJ 700/900/1000

Bombardier Global Express 5000/6000/7000/8000

Bombardier CSeries

Falcon F7X

Gulfstream G500/G550

Hawker 450XP

PROFESSIONAL EXPERIENCE

Bombardier Inc., Saint Laurent/Mirabel, Quebec 2009 - 2014

Systems Engineer

Hydraulics/Flight Controls, Hydro-mechanical Systems/Customer Support

For Hydraulic System:

- Completed review of 25 component drawings to ASME Y14.5 – 1994

- Completed review of System Definition Drawing (SDD) set

- Completed Integrated System Test and Component Rig (ISTCR) SDD installation review

- Reviewed 9 Flight Test Equipment Requirements (FTER) documents for aircraft certification testing

- Day to day liaison with hydraulic supplier

For Flight Controls/Hydro-mechanical Systems:

- Achieved Flight Controls/Hydro-mechanical systems integration

- Developed and monitored ground spoiler panel actuator (GSA) endurance test program

- Conducted aircraft brake improvement program with supplier

- Conducted slat disconnect sensor (SDS) design improvement program with supplier

- Completed new flap actuator design integration with supplier

- Completed aircraft component environmental testing to RTCA DO-160 & MIL-STD-810standards

- Reviewed Qualification Test Procedures (QTP) & Qualification Test Reports (QTR) for environmental

testing

For Customer Support:

- Provided customer support maintenance assessment and solutions during CSeries aircraft development,

Electrical Wiring and Interconnection System (EWIS), halon system, Auxiliary Power Unit (APU)

Pratt & Whitney Canada, Longueuil, Quebec, 2008 - 2009 - Contractor

Systems Engineer

Designed 10 main engine electrical harnesses, gas turbine engine, accessories design

Qualified 19 components for new Boeing 747-8 Auxiliary Power Unit (APU) for environmental qualification

to specification RTCA DO-160E

Reviewed QTP & QTR documents

Achieved technical liaison with 12 suppliers

Created 15 Equipment Specifications, functional and performance criteria

Developed 30 environmental test procedures to RTCA/DO-160

Assessed gas turbine engine component design of permanent magnet alternator

Innotech Execaire, Montreal, Quebec 2007

Design Engineer

For Bombardier business jet Global Express model G5000/6000, created Environmental Control System

(ECS) interior integration with Catia v5

Completed ducting, blower, air pack integration and installation

Gulfstream Aerospace, Savannah, Georgia, 2006 - 2007 - Contractor

Design Engineer

For Gulfstream model G500/G550, completed ECS mechanical integration for an air quality R & D project

using Catia software

Achieved component assembly of new process ECS system as a drop-in package with input and output

aircraft interfaces

Achieved both minimal footprint design and system volume

Bell Helicopter Textron, Mirabel, Quebec, 2005 - Contractor

Design Engineer

For Bell model 429, completed EWIS harness installation using Catia software

Completed battery installation

Selected appropriate retention brackets, p-clips, and stand-off hardware

Maintained minimum distance requirements between harnesses

Ensured a clash free installation with other components

Created wire harness solid models and 2d drawings

Airbus, Toulouse, France, 2004 - 2005 - Contractor

Liaison Engineer

For Airbus A380 FAL formulated liaison division solutions, thereby ensuring continuous EWIS production

of certification aircraft

Ensured aircraft structural modifications formulated to accommodate EWIS retention as necessary

Resolved component installation clashes on FAL

Documented Request For Change (RFC) FAL solutions with instructions and diagrams as necessary

Interfaced FAL RFQ solutions with aircraft master solid models

Airbus, Hamburg, Germany, 2004 - Contractor

Design Engineer

For aircraft A380, completed EWIS harness installation using Catia software

Selected appropriate retention brackets, p-clips, stand-offs

Ensured minimum allowable spacing between wire harnesses

Ensured no clashes with other aircraft components

Resolved clashes with appropriate stake-holders to harmonize an optimal solution

Ensured minimum wire harness bend radii

Goodrich Aerospace Canada Limited, Oakville, Ontario, 2003 - Contractor

Design Engineer

For aircraft A380 landing gear, completed components drawing set with Catia software

Created assembly drawings

Created fabrication drawings

Honeywell Canada, Mississauga, Ontario, 2003 - Contractor

Design Engineer

As part of the Dassault Aircraft F7X Environmental Control System (ECS), designed a wing slat skin

temperature Sensor using Pro Engineer design software, resistive temperature detector (RTD) sensing

elements, stainless steel housing

Produced 5 Technical Specifications for absolute, gage and differential Pressure Sensors including:

Design and Performance Requirements, Quality Assurance Provisions

Produced 5 Technical Specifications for Temperature Sensors, RTD and Thermistor sensing elements

including: Design and Performance Requirements, Quality Assurance Provisions

Assessed environmental test requirements for all ECS Temperature and Pressure sensors to RTCA/DO-

160D

Design For Six Sigma (DFSS) trained

Pratt & Whitney Canada, Mississauga, Ontario, 2001 - 2002 - Contractor

Design Engineer

Developed environmental test procedures to RTCA/DO-160

Designed 5 gas turbine engine external components using CATIA

Assessed 20 suppliers component proposals for functional and performance requirements

Assessed gas turbine engine component design of: fuel pump, starter motor, ignition exciter, heat

exchanger, IGV actuator, rate sensor, engine control box, structural support brackets, temperature &

pressure sensors, pressure relief valve, bypass filter

Guided new temperature sensor probe design with supplier, material selection, functional and

performance requirements

Bombardier Inc., Toronto, Ontario 1996 - 2001

Design Engineer

Created 25 CATIA designs for experimental test rig ground platforms for certification and for structures

Formulated Liaison Division Solutions, thereby ensuring continuous production of Bombardier Dash 8-400 certification aircraft

Created approximately 150 CATIA 3D models & 2D drawings with GD&T for the following aircraft systems: mechanical, air, flight controls, avionics, and hydraulic

Created 24 flight control system CATIA models for Bombardier CRJ900 regional jet certification aircraft

Revised engine installation drawings for Dash 8-400 aircraft

Lockheed Martin Canada Inc., Ottawa, Ontario 1994 – 1996

Design Engineer

Completed electronic packaging design work with CAD

Completed fixture design for functional and environmental testing

Systemex Automation, Laval, Quebec 2014 - 2015

HVAC Design Engineer

For Port Of Montreal Grain Elevator, conducted validation and verification of ducting layout and pressure drop calculations.

Reviewed duct diameters and air velocity

Saint John Shipbuilding Ltd., Saint John, New Brunswick 1984 - 1985

HVAC Project Engineer

Organized air conditioning design, selection of fans, motors, compressors, evaporators

Performed HVAC design and verification, Canadian Patrol Frigates (CPF) Naval Program

Calculated cooling loads, ventilation requirements, pipe sizing, obtained municipal approval

Verified HVAC and refrigeration designs and equipment selection

SNC-Lavalin Inc., Montreal, Quebec 1981 – 1983, 1986 - 1989

HVAC Design Engineer, Noise Control Engineer

Supervisor, Mechanical Design, of damage control systems for the Canadian Patrol Frigates (CPF) and Tribal Class Upgrade and Maintenance (TRUMP) shipbuilding programs

Performed console, electronic enclosure design, material selection, stress, thermal analysis

Conducted an environmental test program for product qualification

Wrote technical specifications for a wide variety of mechanical equipment including pumps, valves, transducers, level sensors, pressure vessels; worked to CSA, MIL, AQAP QA levels

Designed fire detection and suppression systems: AFFF, dry chemical, sprinkler and halon

Vendor assessment, selection and technical interface

Conducted refinery noise and vibration control studies and remedial design

Carried out HVAC energy conservation studies, generated a building load computer model

Verified HVAC and refrigeration designs and equipment selection, building and food production

Performed air-tightness studies of new housing construction in Canada

Bendix Canada, Ville Saint Laurent, Quebec 1979 - 1981

Project Engineer – Materials & Processes

Project leader of a manufacturing improvement and cost reduction program, aviation sector

Investigated and assessed automated de-burring processes; this R&D study resulted in internal de-burring cost savings of 50% and improved process consistency

Supported metal finishing department, designed electrochemical process tooling

Investigated manufacturing operation sheets for clarity and improvements

.

Martin Marietta Canada Ltd., Ottawa, Ontario 1989 – 1994

Facility Engineer

Formulated operating solutions for Transport Canada air traffic control facilities including Area Control Centres, Flight Service Stations, and Flight Control Towers

EDUCATION, ASSOCIATIONS, TECHNICAL SKILLS

B.Eng. Mechanical, Concordia University, Montreal, Quebec

Member of Ordre des ingenieurs du Quebec

Software: MS Office, CATIA v4 & v5, Solidworks, Autocad, VPM

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