List the assessment methods to be used and the context and resources required for assessment. Copy and paste the relevant sections from the evidence guide below and then re-write these in plain English.
Elements describe the essential outcomes. | Performance criteria describe the performance needed to demonstrate achievement of the element. |
1. | Prepare to undertake repair or modification | 1.1 | Modification or the repair scheme is identified in accordance with structural repair manual and/or approved data |
| | 1.2 | Specialist advice is obtained in establishing an approved repair scheme where a standard repair scheme cannot be identified or where damage is beyond specified limits |
| | 1.3 | All materials and equipment required are organised |
| | 1.4 | Structure is supported and prepared in accordance with the applicable maintenance manual to ensure personnel safety and freedom from damage |
| | 1.5 | Jigs, fixtures or bracing are used, as required, to maintain shape and/or alignment |
2. | Repair/modify aircraft structure | 2.1 | Structural repairs/modifications are performed, in accordance with approved repair scheme or modification drawings and instructions, ensuring that aircraft standard practices are used and process requirements are carried out while observing all relevant work health and safety (WHS) requirements, including the use of material safety data sheets (MSDS) and items of personal protective equipment (PPE) |
| | 2.2 | Work area is cleaned of all waste material or contaminants |
| | 2.3 | Required mensuration/alignment checks are completed and components are adjusted, where necessary, to operate within prescribed specifications |
| | 2.4 | Repaired components or assemblies are tagged, sealed and packaged or cradled in accordance with specified procedures, where required |
| | 2.5 | Required maintenance documentation is completed and processed in accordance with standard enterprise procedures |
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 regulations and practices, including the use of MSDS and PPE
using approved maintenance documentation and aircraft publications relating to aircraft structure
identifying aircraft structural assembly fasteners by interpretation of markings, numbering systems, size, shape and colour
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 – hillocks and 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
correctly supporting the aircraft structure by jacking, trestling and/or jigging methods
performing mensuration checks after structure reassembly.
It is essential that the procedures take into account all aircraft and personal safety precautions relating to aircraft structure.
Evidence of transferability of skills and knowledge related to the major repair and modification of aircraft structure is essential. This may be demonstrated through application across a number of aircraft systems or aircraft types. Ability to interpret repair/modification procedures and specifications and apply them in practice is critical. The application of the procedures should also clearly indicate knowledge of structural flight loads and aerodynamic requirements.
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:
aircraft construction principles and structural component attachment methods for primary structure:
fuselage
wings and attachment fittings
horizontal and vertical stabilisers and attachment fittings
pylons and attachment fittings
flight control surfaces
engine mounts and nacelles and attachment fittings
undercarriage attachments
procedures for replacement of primary structure components, such as:
fuselage frames and longerons
wing spars or spar caps
wing-to-fuselage attachment fittings
tailplane attachment fittings
undercarriage attachment fittings
aircraft mensuration checks – when required and methodology
repair of integral fuel tanks and sealing of faying surfaces, including specific WHS and PPE requirements
surface finishes and methods of restoration
how to obtain MSDS
relevant maintenance and structural repair manuals and modification data
relevant regulatory requirements and standard procedures.
Competency should be assessed in the work environment or simulated work environment using tools and equipment specified in maintenance documentation. It is also expected that general-purpose tools and test equipment found in most routine situations would be used where appropriate.
The following conditions of assessment represent the requirements of the Regulators (ADF and CASA) and maintenance stakeholders and must be rigorously observed.
A person cannot be assessed as competent until it can be demonstrated to the satisfaction of the workplace assessor that the relevant elements and performance criteria of the unit of competency are being achieved under routine supervision on tasks involving repairing by replacement or modifying major load-carrying structural members, such as skins, longerons, spars, frames and bulkheads.
This shall be established via the records in the Log of Industrial Experience and Achievement or, where appropriate, an equivalent Industry Evidence Guide (for details refer to the Companion Volume Assessment Guidelines).
Assessors must satisfy the requirements of the National Vocational Education and Training Regulator (Australian Skills Quality Authority, or its successors).
Where the unit is to be used for CASA licensing purposes the Assessor must also meet the criteria specified in the CASR Part 147 Manual of Standards.