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 : abnx55@r.postjobfree.com

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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