Analyst Mechanical Engineering

ARIS HARDJENDRO 425-***-**** ***************@*******.***

AEROSPACE STRUCTURE ANALYSIS ENGINEER WITH 20 YEARS OF EXPERIENCE

( B.S. in Mechanical Engineering, Green Card Holder )

SKILLED AND EXPERIENCED IN,

*Aircraft Structural analysis and test for both metal and composite structure

* Classic hand calculation

* Computer based analysis, FEM( NASTRAN, FEMAP, PATRAN )

* Computer programming language- Visual basic, Delphi

* MS Office application- Visual Basic for Application (EXCEL, WORD,)

SUMMARY OF PROFESSIONAL EXPERIENCE

• Stress analyst aerospace industry, 20 years’ experience. Performed strength analysis and optimizing

aircraft structures and used both traditional and computer analysis, both metal and composite structure.

• Structure analyst for “blow down” panel – leading edge airbus A380 aircraft (Composite)

• Structure analyst for lay-out design and support detail drawings for Fairchild-Dornier J728 aircraft.

• Composite integral stiffened panel development, IPTN – Hawker de Havilland Australia (Composite)

• Technically responsible for aircraft fuselage structure. Working both for N250, N250-100 aircraft.

• Structure analyst for lay-out design and support detail drawings for CN235 aircraft.

WORK HISTORY

D3 TECHNOLOGIES DECEMBER 2004 TO OCTOBER 2012 Mukilteo, W

• Structural analyst of 747 – Freighter/Passenger Program ( Boeing On-site Support)

Static and fatigue analysis of Fuselage structure

• Structural analyst of 777 - Freighter Program ( Boeing On-site Support)

Static and fatigue analysis of Fuselage/Wing structure

• Structural analyst of 747LCF Large Cargo Freighter Program ( Boeing On-site Support)

Static and fatigue analysis of Fuselage structure

• Structural analyst of 757-200 Fuselage for Winglet Modification Program ( D3 Technologies Office )

Substantiated monocoque and various Fuselage components for increased loads.

INDONESIAN AEROSPACE JANUARY 2003 TO DECEMBER 2004 BANDUNG, INDONESIA

• Bubble window, CN 235 military version

• Nose radome, CN 235 military version (composite structure)

• Super rebel 2500 crash investigation

• Wing to body fairing CN 235 Justification(Composite Structure)

AIRBUS NOVEMBER 2001 TO SEPTEMBER 2002 BRISTOL, ENGLAND

• Structure analyst worked on blow down panel – leading edge A380 (composite structure)

FAIRCHILD DORNIER MAY 1999 TO OCTOBER 2001 MUNCHEN, GERMANY

• Stress analysis for layout, detail drawings for Fuselage J728 aircraft and support designers.

INDONESIAN AEROSPACE (IAE) JULY 1998 TO MAY 1999 BANDUNG, INDONESIA

• N250 – Stress Analysis for design support and stress report

ARIS HARDJENDRO 425-***-**** ***************@*******.***

HAWKER DEHAVILLAND AUGUST 1997 TO JULY 1998 BANKSTOWN, AUSTRALIA

• Composite integral stiffened panel development (composite structure)

INDONESIAN AEROSPACE (IAE) –IPTN MARCH 1992 TO AUGUST 1997 BANDUNG, INDONESIA

• Airframe fuselage structure analysis (skins / stringer, frame, circumferential splice, passenger and

baggage door surrounds, system penetration, etc.), from preliminary to detail design phase. Released

layout and production drawings including stress report preparations and structural test plans for

certification of N250 airplane.

• Skin stringer development test

EDUCATION

Bachelor of Science degree from Mechanical Engineering department,

Bandung Institute of Technology (ITB), Bandung, Indonesia

Other information

Green Card Holder

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