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Elements and Performance Criteria

  1. Remove general aircraft electrical hardware
  2. Install general aircraft electrical hardware

Range Statement

This field allows for different work environments and conditions that may affect performance. Essential operating conditions that may be present (depending on the work situation, needs of the candidate, accessibility of the item, and local industry and regional contexts) are included.

Removal and installation of electrical hardware includes one or more of the following connection methods:

Bolted

Plug connectors

Electrical hardware includes:

Switches

Relays

Lamps

Terminal blocks

Current limiters

Circuit breakers

Fuses

Sockets

Potentiometers

Capacitors

Inductors

Magnetic amplifiers

Transformers

Rheostats

Miscellaneous sensors and minor components hard mounted throughout the aircraft

Busbars

Lugs

Ferrules

Splices

Connectors and electrical, electronic cables and looms

Procedures and requirements include:

Industry standard procedures specified by manufacturers, regulatory authorities or the enterprise


Performance Evidence

Evidence required to demonstrate competency in this unit must be relevant to and satisfy all of the requirements of the elements and performance criteria under the specified conditions of assessment, and must include:

applying relevant WHS procedures

using approved maintenance documentation and aircraft publications relating to miscellaneous aircraft electrical hardware and components

recognising defects in and deterioration of electrical cables to aircraft industry standards, including crimped and soldered joints

correctly interpreting aircraft wire markings, terminal block identification and plug/socket pin numbering systems

inspecting electrical looms and harness pre and post-removal and installation to ensure minimum bends are maintained, cable is not in tension, plugs are correctly aligned, security of route ensures no chaffing of insulation, adequate clipping and cable ties have been utilised and construction complies with aircraft industry standards

positive identification of miscellaneous electrical hardware and/or components in all aircraft systems

plug connector pin removal and insertion.

It is essential that applicable cleanliness requirements and WHS precautions are fully observed, including awareness of electrostatic discharge procedures.

Evidence of transferability of skills and knowledge related to removal and installation is essential.


Knowledge Evidence

Evidence required to demonstrate competency in this unit must be relevant to and satisfy all of the requirements of the elements and performance criteria and include knowledge of:

component attachment methods

connection of hardware and plugs

relevant WHS procedures

electrical wiring used in aircraft and wire marking

plug/socket pin numbering and terminal block identification

cable and loom installation requirements

crimping tools and crimp terminals

procedures for removal and insertion of plug connector pins

electrical fundamentals and related mathematical and physics principles.