Analysis Engineer
Resume:
CURRICULUM VITAE
NAME : Mohamad Firdaus
: August 21th,1963
DATE OF BIRTH
NATIONALITY : Indonesian
ADDRESS : Jl. Batununggal Mulia Raya No.6
Bandung 40267 – Indonesia
Phone : +628********
EDUCATION : Civil Engineering Graduate
Parahyangan Catholic University, Bandung Indonesia
E-MAIL : **********@*****.***
QUALIFICATION : Stress Analysis Engineer
SUMMARY OF WORK EXPERIENCE
Over fifteen years, - Performed stress, strength and stability of structures Aircraft and Interior
Equipment, design allowable development, structural modeling, strength checking and formal
analysis preparation, structural drawing approval, approval of modification notice
Involved and participated to different Aircraft programs, like: Commuter Aircraft N250 PA1 and
PA2, CN235-220M Joint with TAI (Tusas Aerospace Industry) Program, NMX Air Taxi With 6-8
Passengers, CN235-220M NRK1-2-3 (ROKAF) military version, CN235-220M VIP (TUDM)
military version, Interior Development of A330 VVIP Configuration, Structure Development of
Fokker 28 Shoulder Harness,NC212-200 Patmar, F.28 (Fokker ) PELITA Airline,HESA Program
Antonov AN 140.
COMPUTER SKILL
1. Finite element analysis using of PATRAN, PC NASTRAN,CATIA
2. MS Office Application ( Word, Excel etc )
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HISTORY OF EMPLOYMENT
JOB EXPERIENCE :
JAN 2012 – PRESENT,
Indonesia Aerospace Industries( IAe ), Bandung, Indonesia
TAI (Tusas Aerospace Industry) Program
Prepared Stress and Strength Analysis Documents:
- FE Model and Stress Analysis of Torpedo Support Structure Installation
on Wing Structure of CN 235 Aircraft
- FE Model and Stress Analysis of Bubble Window Structure Installation
on Fuselage Structure of CN 235 Aircraft
- FE Model and Stress Analysis of Ballast Installation on Fuselage Structure
of CN 235 Aircraft
- Observer Oxygen Tube Routing Modification Stress Analysis Installation
of CN 235 Aircraft
HESA ( Iran Aircraft Industries ) and Indonesia Aerospace Industries( IAe ),
Bandung, Indonesia, ( March to April 2012 )
Prepared Stress and Strength Analysis Documents:
- Mechanism System Control Horizontal Tail Stress and Strength Analysis
of AN 140 Aircraft
JAN 2011 – DEC 2011,
Indonesia Aerospace Industries( IAe ), Bandung, Indonesia
TAI (Tusas Aerospace Industry) Program
Prepared Stress and Strength Analysis Documents:
- FE Model and Stress Analysis of Liferaft Rack Storage CN 235 Aircraft.
HESA ( Iran Aircraft Industries ), ( April to Juni 2011 ), Isfahan Iran
Prepared Stress and Strength Analysis Documents:
- FE Model and Stress Analysis of Cargo Door Structure of AN 140 Aircraft
- FE Model Horizontal Stabilizer of AN 140 Aircraft
- FE Model Elevator of AN 140 Aircraft
- FE Model Trim of AN 140 Aircraft
- FE Model Validation of Centre Fuselage, Rear Fuselage of AN 140 Aircraft
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JAN 2010 – DEC 2010,
Indonesia Aerospace Industries( IAe ), Bandung, Indonesia
TAI (Tusas Aerospace Industry) Program
Prepared Stress and Strength Analysis Documents:
- FE Model and Stress Analysis of Liferaft Laucher Rack Structure Installation
of CN 235 Aircraft Ramp Door.
- FE Model and stress Analysis of Liferaft Rack Storage CN 235 Aircraft.
- Additional Hole of Wing Rear Spar Stress and Strength Justification
Analysis of CN 235 Aircraft
HESA ( Iran Aircraft Industries ), ( March to April 2010 ), Isfahan Iran
Prepared Stress and Strength Analysis Documents:
- FE Model and Stress Analysis of Sliding Door Structure of AN 140 Aircraft
- FE Model and Stress Analysis of FLIR structure installation of AN 140 Aircraft
- FE Model and Stress Analysis of FLIR Composite Fairing of AN 140 Aircraft
JUL 2007 – JAN 2010,
Indonesia Aerospace Industries( IAe ), Bandung, Indonesia
TAI (Tusas Aerospace Industry) Program
Prepared Stress and Strength Analysis Documents:
- FE Model and Stress Analysis of Torpedo and Depth Charge Support Structure
Installation on Wing Structure of CN 235 Aircraft
- FE Model and Stress Analysis of Side Console Structure Installation of CN 235
Aircraft
- V/UHF2 Antenna Installation, GPS antenna Installation on CN 235 Aircraft
- FE Model and Stress Analysis of liferaft Laucher Rack structure Installation on CN
235 Aircraft Ramp Door
- Smoke Marker Installation Stress and Strength of CN 235 Aircraft.
April 2007 – JUL 2007
Ankara, Turkye
TAI (Tusas Aerospace Industry) Program
Prepared Stress and Strength Analysis Documents:
- FE Model and Stress Analysis of ATR 70 Mission Rack Structure Installation
JUN 2006 – APRIL 2007,
Indonesia Aerospace Industries ( IAe ), Bandung, Indonesia
TAI (Tusas Aerospace Industry) Program
Prepared Stress and Strength Analysis Documents:
- Skin and stringer fuselage Stress Analysis of CN 235 Aircraft
- Obdas and Artist Rack Structure Stress Analysis of CN 235 Aircraft
- Stress Analysis of Oxygen Bottle Installation, V/UHF2 Antenna Installation, GPS
antenna Installation of CN 235 Aicraft
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JAN 2006 – JUN 2006
Indonesia Aerospace Industries ( IAe ), Bandung, Indonesia
NMX Air Taxi With 6-8 Passenger Aircraft
Prepared Stress and Strength Analysis Documents :
- Skin and stringers Aft fuselage analysis of NMX, formed typical,
- FE Model and Stress Analysis of Cabin and Cockpit Floor Fuselage beam
Structure of NMX Aircraft
1992 - 2005
Indonesia Aerospace Industries ( IAe ), Bandung, Indonesia
CN235-220M VIP (TUDM) military version
Prepared Certification Documents :
- Interior Support & Fitting Stress and Strength analysis
- Interface Load Analysis of Interior Modules – Geven Doc.
- Review of Flammability Test Plan and Report of Interior Modules – Geven Doc.
- Review of Static Test Plan and Report of Passenger Seat – Geven Doc.
CN235-220M NRK2-3 VIP (ROKAF) military version
Prepared Certification Documents :
- Interior Support & Fitting Stress and Strength analysis
- Interface Load Analysis of Interior Modules – AIM Aviation Doc.
- Review of Flammability Test Plan and Report – AIM Aviation Doc.
- Review of Static Test Plan and Report of Passenger Seat – AIM Aviation Doc.
CN235-220M NRK1 (ROKAF) military version
Prepared Certification Documents :
- Interior Support & Fitting Stress and Strength analysis
- Review of Interface Load Analysis of Lavatory – B/E Aerospace Doc.
- Additional Equipment Support and Fitting Stress and Strength Analysis
- Review of Static Test Plan of Lavatory
- Review of Fire Properties of Galley and Lavatory Test Plan and Report
Fokker F-28 (PT. GARUDA & PELITA) civil version
Prepared Certification Documents;
- Additional Support Structure of Fokker F-28 Shoulder Harness Stress and
Strength Analysis.
A330-341 VVIP (PT. GARUDA) civil version
Prepared Certification Documents;
- Interior Development of A330-341 VVIP Configuration
CN235-220M (MOAC) military version
Prepared Certification Documents :
- Interior Support & Fitting Stress and Strength analysis
- Review of Static Test Plan and Report of Seats – Aviointeriors Doc.
- Review of Interface Load Analysis and Stress Analysis of
Galley, Lavatory, Emergency Stowage, Attendant Seat, Passenger Seat,
Overhead Stowage Bin at Aerosoft S.r.l Napoli, Italy
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N250 – PA ll A/C Program
Prepared Stress and Strength Analysis Documents :
- Cargo Restraint, Cargo Ceiling, Cabin Ceiling installation Structure
- PSU, Wind Screen Installation structure
- Cargo Floor Structure
- Stowage Bin ( Hatrack ) installation structure
N250 – PA I A/C Program
Prepared Stress and Strength Analysis Documents :
- Cargo Restraint, Compartment Lighting, Cabin Lighting installation
- PSU, Cargo Floor, Internal Lighting installation
- Stowage Bin ( Hatrack ) installation structure
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