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Elements and Performance Criteria

  1. Remove fixed wing flight control system components
  2. Install fixed wing flight control system components

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.

Flight control system components include:

Ailerons, elevators, rudders, trim tabs, speed brakes, spoilers, flaps and slats

Actuators – mechanical, hydraulic, pneumatic or electric

Mechanical flight control components (cables, pulleys, guides, fairleads, tension regulators, control rods, bellcranks, torque tubes, chains, sprockets, control sticks, wheels or columns, trim wheels or handles, rudder pedals)

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 practices

using relevant maintenance documentation and aircraft manuals to:

remove flight control surfaces

check the mass balance of control surfaces, where required

install flight control surfaces

remove power flight control system components

install power flight control system components

remove mechanical flight control system components

install mechanical flight control system components.

It is essential that safety precautions applicable to the fixed wing flight control system being maintained are fully observed, understood and complied with (especially flight control system inter-relationships with other systems where applicable). An awareness of dual inspection requirements associated with work on flight controls and systems must also be demonstrated.

Evidence of transferability of skills and knowledge related to removal and installation is essential. This may be demonstrated through removal and installation of a representative range of the fixed wing flight control system components listed in the Assessment Conditions.


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:

flight control surface and system component attachment methods

connection hardware and couplings

electrical circuit isolation and plug removal and installation

requirements for balancing of control surfaces

flight control system rigging requirements

requirements for independent inspection of work performed on flight control systems and components

relevant WHS practices

relevant maintenance manuals

relevant regulatory requirements and standard procedures.