Aircraft Fatigue and Fracture Mechanic Engineer

ALI YUSNI

Teuku Umar street no ** Tegal Regency, Central Java Province – 52192 INDONESIA

Mobile : +62-821-****-****

Email : ***.*****.******@*****.***

Date of Birth : March 16, 1983

EDUCATION

Institut Teknologi Bandung (2003 - 2008)

B.Eng in Aeronautics & Astronautics Engineering – Mechanical Structure

Institut Teknologi Bandung (2015 - 2018)

Magister in Electrical Engineering – High Voltage Engineering

PERSONAL PROFILE STATEMENT

I am personally who can adapt easily in adjusting organizational culture. In my current job, I work as an aircraft structure Design Engineer especially in field of Fatigue and Damage tolerance analysis since February, 2010. In every opportunity I intend to improve these abilities on myself so I can become a better worker.

WORK EXPERIENCES

1. PT. Dirgantara Indonesia (Persero) / Indonesian Aerospace (IAe)Co., Ltd (2010-Now)

• CN-235 Turkish Aircraft Civil to Military Utility Conversion (February 2010 - 2015)

Prepare fatigue and damage tolerance analysis document for CN-235 Turkish military aircraft due to aircraft structural modification. The flight loads on this aircraft involve vibrational loads due to the modification of the addition of several mission systems that cause vibrations.

• CN-235 Military Korean Coast Guard (2013 - 2015)

Prepare fatigue and damage tolerance analysis document for CN-235 Korean Coast Guard aircraft due to aircraft structural modification.

• N-219 Aircraft (2015 - Now)

Analyse the new N219 aircraft structure design to ensure the principal structure elements of aircraft are safe from catastrophic failure during the economic life (design goal life) of the aircraft. Some of the analysis performed includes: Spectra Development, Full Scale Fatigue Test Articles, Test Measurements, Test Requirements.

• CN-235 Structure Life Extended Program - UAE Air force (August 2019)

Supervise the NDT inspection team to guide the inspected area and conduct evaluation (fatigue and damage tolerance analysis) for inspected area.

• CN-235 Structure Life Extended Program - Royal Malaysian Air force (Sept - Nov 2020)

Supervise the NDT inspection team to guide the inspected area and conduct evaluation (fatigue and damage tolerance analysis) for inspected area.

• MALE Surveillance and Tactical Drone (2020 - Now)

Prepare an allowable damage tolerance stress analysis for the principal structure elements of the MALE aircraft to predict the structures durability of the aircraft. Some of the principal structure element includes: Fuselage to Wing Joint, Fuselage to VTP, Landing Gear attachment, Engine mount.

2. PT. LAPI ITB (Part Time)

• Design Engineer (2014-2015)

Conduct the initial concept design drawing (CATIA Based) of training aircraft for 4 passengers.

COURSES

• Basic Aircraft – Indonesian Aerospace (March 01 – April 29, 2010)

• Aircraft Design Process – Indonesian Aerospace (February 22 – March 09, 2012)

• Human Factor Initial – Indonesian Aerospace (August 06 – August 10, 2018)

• Design Organization Approval Panel 3 (Structure) – Indonesian Aerospace (August 05 – August 09, 2019)

• Introduction to Non Destructive Test – Indonesian Aerospace (January 27 – January 30, 2020)

• Basic Airworthiness – Indonesian Aerospace (February 17 – February 21, 2020)

DOCUMENT RESPONSIBILITIES

• CN-235-100M MPA/MSA MELTEM II Damage Tolerance Evaluation Criteria and Guidelines (2012)

• CN-235-100M MPA MELTEM II ADF Antenna Installation Fatigue and Damage Tolerance Analysis (2013)

• CN-235-100M MPA Fatigue Loading Matrix To Support Fatigue and Damage Tolerance Analysis (2013)

• CN-235-100M MPA MELTEM II Reinforcement Upper Ceiling Installation Fatigue and Damage Tolerance Analysis (2013)

• CN-235-100M MPA MELTEM II Cargo Spot Light Relocation Installation Fatigue and Damage Tolerance Analysis (2013)

• CN-235-100M MPA MELTEM II PSE F016 Fatigue and Damage Tolerance Analysis (2013)

• CN-235-100M MSA MELTEM II Spectra Development (2013)

• CN-235-100M MPA MELTEM II UV Sensor Bottom Installation Fatigue and Damage Tolerance Analysis (2014)

• CN-235-100M MPA MELTEM II HF1 Equipment Installation Fatigue and Damage Tolerance Analysis (2014)

• CN-235-100M MPA MELTEM II Ramp Door Hinge Back-Up Structure On Ramp Door Fatigue and Damage Tolerance Analysis (2014)

• CN-235-100M MPA MELTEM II ADFU 3&4 Fatigue and Damage Tolerance Analysis (2014)

• CN-235-100M MPA MELTEM II PSE F040 Fatigue and Damage Tolerance Analysis (2014)

• CN-235-100M MSA MELTEM II PSE F016 Fatigue and Damage Tolerance Analysis (2014)

• CN-235-100M MSA MELTEM II PSE F030 Fatigue and Damage Tolerance Analysis (2014)

• CN-235-100M MSA MELTEM II ICS And Converter Installation Fatigue and Damage Tolerance Analysis (2014)

• CN-235-100M MPA MELTEM II Outer Wing Box Fatigue and Damage Tolerance Analysis Due To Torpedo Installation (2014)

• CN-235-100M MSA MELTEM II Fuel Dump Pump Installation On Center Wing Fatigue and Damage Tolerance Analysis (2014)

• CN-235-100M MPA MELTEM II Ramp Door Hinge Back-Up Structure On Fuselage Fatigue and Damage Tolerance Analysis (2014)

• CN235-110 KCG Airworthiness Limitation Instructions (2014)

• N219 Full Scale Fatigue Test Requirement (2017)

• N219 Main Landing Gear Full Scale Fatigue Test Requirement (2017)

• N219 Full Scale Fatigue Test Article (2018)

• N219 Full Scale Fatigue Test Measurement (2018)

• NC212 NAU9 Navigation Training Fatigue and Damage Tolerance Justification (2020)

• CN235-220M NMA1 Modification Installation Fatigue and Damage Tolerance Justification Volume 1 (2020)

• CN235-220M NMA1 Modification Installation Fatigue and Damage Tolerance Justification Volume 2 (2020)

• MALE Damage Tolerance Stress Allowable Analysis (2020)

• CN235-220M NAL3 Fatigue and Damage Tolerance Justification (2021)

FINITE ELEMENT MODEL RESPONSIBILITIES

• MALE Engine Mount Bar (2020)

• MALE Engine Mount Frame Bulkhead (2021)

COMPUTER SKILL : Microsoft Office, FORTRAN, Visual Basic, MATLAB, Nastran-Patran, CATIA V5

LANGUAGE : Indonesian (native), English (fair)

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