Look for evidence that confirms knowledge of: aircraft construction principles and the causes of structural damage, including metal fatigue and corrosion structural fatigue preventative measures structural corrosion removal and preventative measures aircraft repair schemes and modification data/drawings procedures for the design and approval of repair schemes and modifications material specifications for aluminium alloys and steel alloys used in aircraft structure structural material identification by markings and numbering systems material identification by chemical, electrical and mechanical methods material storage requirements hardware types and specifications identification of hardware sealants used in aircraft structure and their application and handling chemical surface treatments electroplating paints and finishes OHS precautions associated with repair of aircraft structure MSDS PPE Look for evidence that confirms skills in: applying relevant OHS procedures, including the use of MSDS and applicable items of PPE using approved maintenance documentation and aircraft publications relating to aircraft structure identifying various aircraft metals and their basic metallurgy properties by interpretation of markings, numbering systems or visual, chemical or mechanical means identifying various aircraft composite materials and their basic properties by interpretation of markings and visual means handling and storing aircraft metals and composite materials, including sealing agents, to industry standards identifying aircraft structural assembly fasteners (metal and composite) by interpretation of markings, numbering systems, size, shape and colour correctly assessing and describing the extent of damage correctly interpreting and/or producing repair scheme/modification drawings (including third angle projection, isometric, sectional formats and hand sketches) using appropriate hand tools and machines to remove and assemble aircraft structural components, parts, sections and skin, including riveting equipment, drilling equipment, aligning tools and material fasteners (grip pins) applying correct removal, installation and repair techniques for: a range of rivets (blind and solid) using hand, squeeze and pneumatic situations a range of close tolerance fasteners (standard and oversize – hilocks, taper locks), including hole preparation threaded devices, including internal and external thread cutting, helicoil inserts and damaged stud replacement hardware assembled by close tolerance fits using heat, cooling and force methods, including bearings, bushes and inserts correct support of the aircraft structure by jacking, trestling and/or jigging methods performing a range of metal structure repair techniques, including: metal scab patch, flush, splice, lap and formed section repair metal to metal and metal to composite bonding applying structural corrosion removal/treatment techniques restoring aircraft structure sealing and surface finishes |