Fatigue and Damage Tolerance Engineer

GENERAL QUALIFICATIONS

• Bachelor’s degree in Mechanical, Aircraft or Aerospace Engineering.
• Preferably a master’s degree in relevant field.
• Having at least 2 years of experience in fatigue (crack initiation) and damage tolerance (crack propagation)
• Having knowledge about composites and analysis method of these materials.
• Having knowledge about fatigue (crack initiation) and damage tolerance (crack propagation) of metal and composite structures.
• Being proficient in at least one of the finite element analysis software (nCode, MSC Patran/Nastran, Abaqus).
• Having knowledge about static, dynamic and vibration.
• Preferably making hand calculations for fatigue (crack initiation) and damage tolerance (crack propagation) analysis.

JOB DESCRIPTION

• Making life analysis and reporting of aircraft components and the aircraft as a whole to ensure continuity
• Following test process
• Following the maintenance processes of aircraft components.