Alexey I. ZHUKOV

109443, Volgogradsky avenue, 143-2, Moscow, Russia

Born: November 15, 1982 in Moscow, Russia

Nationality: Russia

Cellular phone: +7 926 557-01-72, +49 152 574-102-52

E-mail: ksey.zhukov@gmail.com

Married, 2 children

SUMMARY

Stress Engineer / Task Leader. Experience in aircraft industry since 2007. Participated in major AIRBUS programs: A330-200GMF, A350XWB, BelugaXL (Development), Long Range and Single Aisle (Serial Activity), able to perform tasks autonomously. Self-motivated and self-directed. I have an experience of working at AIRBUS side (business trips to Bremen and Hamburg, Germany). Recommendations are available upon request.

EDUCATION

09.1989 to 06.1999

Regular school (advanced English language / Mathematics study), Moscow, Russian Federation;

High school equivalency.

09.1999 to 02.2005

Moscow Power Engineering Institute (Technical University) / Power Plant Engineering and Mechanics Institute, Moscow, Russian Federation;

Mechanical Engineer; Specialization: Dynamics and Strength of the Machines;

University Diploma, topic “Crack growth criteria definition for Rails”.

WORK EXPERIENCE (beginning from the most recent)

02.2007 to present

Stress Engineer / Stress Leader in ECAR (Engineering Center of AIRBUS in Russia),

Moscow, Russian Federation

Major Projects: 07.2016 to present

AIRBUS Single Aisle family Floor Structure S15 – S19.1 stress team on-site support in Hamburg, Germany, CEO/NEO + Retrofit activity

Stress Engineer / Stress Focal

• Integration to Airbus Stress team, on-site support;

• Workload/workflow coordination of stress team in Moscow;

• Retrofit modifications: reports writing and cross-checking;

• Non-regular task: Overweight PAX Seats static stress justification for all SA Family (screening

of all Stress Reports since MSN0001 under Airbus Deutschland responsibility for the Floor

Structure S15 – S17 in order to identify critical zones, finding possible solutions: changing of

calculation methods / ASSACOS and other recalculations / applying engineering judgement /

providing reinforcement recommendations);

• SA Family Static Stress and F&DT documentation (Reports, Technical Memorandums,

Coordination Memos) electronic storing;

03.2014 to present (since 07.2016 – only as a stress coordinator)

AIRBUS A320/A330/A340 families: Long Range and Single Aisle Serial Activity (fuselage sections, both German and French perimeters)

Stress Leader / Stress Engineer

• Static stress and F&DT (Fatigue and Damage Tolerance) support of modifications for Serial

Activity projects: Primary and Secondary Structure of Forward, Central and Afterward

Sections, Center Wing Box, Floor areas, Mechanical / Electrical Systems and Equipment

Installation, Hat rack / Galley fittings, Racks (for example, Ku/Ka-band Aircraft Networking

Data Unit (KANDU) and Ku/Ka-band Radio Frequency Unit (KRFU) installation),

circumferential and longitudinal joints;

• Workload, hours estimation, target dates and calculation methods coordination with

customer. Communication with ECAR subcontractors;

• Constructions development and optimization in close cooperation with Design Department;

• Providing of quick technical solutions in order to support the Manufacturing (e.g. Design

Query Note / Beanstandungsmeldung / Works Query Note);

• Technical and Certification documents creation, updating and cross-checking (Stress

Statements, Stress Sheets, Stress Reports, ACD4/6 sheets, Stress manuals);

• Stress validation in compliance with FAR/JAR/CS regulations;

• ACD4/6 sheets checking/creating/updating and transformation to ACD Toolbox software;

• FE estimative and detailed modeling, analytical calculations;

• Working with CATIA V5 solid models (parts and assemblies);

10.2013 to 02.2014

AIRBUS A350XWB-900. S16-18 Integration & A-brackets

Stress Engineer

• Static stress calculations of A-brackets. FEM modeling and Certification reporting (Fixed and

Movable Systems Attachment Brackets, Water Tank Attachment Structure, Catwalks in Bulk

Area, Support Structure for Connectivity and IFEC Rack). Working in Hamburg, Germany

(08.10 – 06.12.2013) in cooperation with customer;

• FEM and hand calculations of X-Y-Z- fittings for Hat racks and monuments in the Crown Module Structure - Upper and Lateral (standard and CCRC – Cabin Crew Rest Compartment - versions);

• Constructions development and optimization in close cooperation with Design Department;

10.2011 to 09.2013

AIRBUS A350XWB-900. PAX, Cargo and Bulk Cargo Doors Integration.

Stress Engineer

• Static and F&DT calculations of all Frame Side Interface Fittings (see picture below) and

Counter Balance Mechanism of Bulk Cargo Door;

• Passing through all the phases from early maturity calculations and FEM modeling of all

Fittings to Certification Reporting, business trip to AIRBUS Bremen (05.08 – 23.08.2013);

Frame Side Fittings (PAX Door example)

• Workload, target dates and calculation methods coordination with customer (written, spoken

forms), creating of Coordination Memos, Minutes of Meetings;

• FEM producing, updating and checking according to AIRBUS standards and rules

(Linear/Non-Linear, thermal, modal analyses), analytical calculations;

• Constructions development and optimization in close cooperation with Design Department,

weight saving.

10.2010 to 10.2011

AIRBUS Long Range and Single Aisle families (including NEO and Sharklets)

Stress Engineer

• ASSACOS calculations (circumferential and longitudinal joints, cross beams etc.) and

checking, certification reporting; creation of ACD4 sheets. Communication with ECAR

subcontractors;

07.2009 to 09.2010

AIRBUS A350XWB-900 Sections 16/18 integration

Stress Engineer

• Hand and ISAMI calculations of non-regular metallic zones: X-Paddles, Doors Surrounding,

Corner Fittings, Cross Beams junctions;

• ISAMI composite modeling of Z-struts;

02.2007 to 06.2009

AIRBUS A330-200 GMF AFT and FWD sections.

Stress Engineer

• Justification and certification phases. Calculation of regular and non-regular fuselage zones -

Doors surrounding, stringer and frame couplings, corner fittings, cut-outs, Lugs, latch fittings

etc. Regular fuselage zones – circumferential and longitudinal junctions ISSY calculations.

03.2005 to 02.2007

Stress Engineer in Federal State Unitary Enterprise “NPO Mashinostroyenia” (military

space and rocketry company),

Reutov city, Moscow District, Russian Federation

Stress Engineer

• FEM and analytical calculations of cruise missile launch equipment;

• Stress documentation preparation (stress reports, Stress sheets, Office memorandums);

• Constructions development and optimization in close cooperation with Design Department;

• Preparation of Strength Test Manuals and support of the Tests process in the Laboratory.

07.2003 to 02.2005

Stress Engineer in JSC “Russian Railways”,

Moscow, Russian Federation

Stress Engineer

• Static stress, F&DT and analytical calculations of Rails;

• FEM analyses, working with SolidWorks;

• Crack growth in Rails criteria definition.

Russian: mother-tongue; English: upper-intermediate; German: elementary.

LANGUAGES

SKILLS

• Windows 95, 98, 2000, NT, Vista, XP, 7, 8;

• Mac OS, Linux, Unix;

• PATRAN/NASTRAN (Linear, Non-linear modules), ANSYS, FEMAP;

• ISAMI, ISSY, ASSACOS;

• SAFE;

• CATIA V4/V5;

• SolidWorks;

• TREND;

• ASSIST;

• MS ECXEL, POWEPOINT, WORD (Stress Dossier), VBA;

• HSB (Handbuch Struktur Berechnung);

• TAKSY, GILDA, PDM Link;

• ACD ToolBox;

• Zamiz, Docmaster, Copedoc.