The important thing to remember when gathering evidence is that the more evidence the better - that is, the more evidence you gather to demonstrate your skills, the more confident an assessor can be that you have learned the skills not just at one point in time, but are continuing to apply and develop those skills (as opposed to just learning for the test!). Furthermore, one piece of evidence that you collect will not usualy demonstrate all the required criteria for a unit of competency, whereas multiple overlapping pieces of evidence will usually do the trick!
From the Wiki University
What evidence can you provide to prove your understanding of each of the following citeria?
Inspect rotor and rotor control systems and components
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Isolation and warning signs are fitted/installed to the system or related systems and the aircraft configured for safe system inspection and operation in accordance with relevant aircraft publications/maintenance regulations orders and standards and practices Completed |
Evidence:
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Rotor and rotor control system is visually or physically checked/inspected for external signs of defects in accordance with relevant aircraft publications maintenance regulations/orders and standards and practices 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) Completed |
Evidence:
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Defects are identified and recorded in accordance with standard enterprise procedures Completed |
Evidence:
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Inspect basic rotary wing airframe systems
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Relevant maintenance documentation and modification status, including system defect reports, where relevant, are used to identify specific inspection requirements Completed |
Evidence:
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Isolation tags are checked and aircraft configured for safe system inspection and operation in accordance with the applicable maintenance manual Completed |
Evidence:
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Airframe system components are visually or physically checked for external signs of defects in accordance with applicable maintenance manual while observing all relevant WHS requirements, including the use of MSDS and items of PPE Completed |
Evidence:
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Defects are correctly identified and reported Completed |
Evidence:
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Ground test rotor and rotor control systems
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Aircraft and system are prepared in accordance with relevant aircraft publications/maintenance regulations orders and standards and practices for the operation of engine and rotor system Completed |
Evidence:
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Rotor and rotor control system are functionally tested in accordance with relevant aircraft publications maintenance regulations/orders and standards and practices for evidence of malfunction Completed |
Evidence:
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System calibration or adjustments are performed in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices Completed |
Evidence:
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Test/adjust basic rotary wing airframe systems and components
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Aircraft and system are prepared in accordance with applicable maintenance manual for the application of power/system operation Completed |
Evidence:
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Airframe system is functionally tested in accordance with maintenance manual for evidence of serviceability or malfunction Completed |
Evidence:
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System adjustment is performed in accordance with maintenance manual |
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Completed |
Evidence:
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Troubleshoot rotor and rotor control systems
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Available information from aircraft maintenance documentation, inspection and test results is used to assist in fault determination Completed |
Evidence:
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Relevant aircraft publication fault diagnosis guide and logical processes are used to ensure efficient and accurate troubleshooting to line replacement level Completed |
Evidence:
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Specialist advice is obtained to assist with the troubleshooting process Completed |
Evidence:
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Rotor and rotor control system faults are located and the causes of the faults are clearly identified and recorded in aircraft maintenance documentation in accordance with standard enterprise procedures Completed |
Evidence:
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Fault rectification requirements are determined Completed |
Evidence:
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Troubleshoot basic rotary wing airframe systems
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Available information from maintenance documentation, inspection and test results is used, where necessary, to assist in fault determination Completed |
Evidence:
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Maintenance manual fault diagnosis guides and logic processes are used to ensure efficient and accurate troubleshooting Completed |
Evidence:
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Specialist advice is obtained, where required, to assist with the troubleshooting process Completed |
Evidence:
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Airframe system faults are located and the causes of the faults are clearly identified and correctly recorded in maintenance documentation, where required, in accordance with standard enterprise procedures Completed |
Evidence:
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Rectification requirements are determined Completed |
Evidence:
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Remove and install rotary wing rotor and rotor system components
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System is rendered safe and prepared in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices, and isolation and warning signs are installed/fitted to ensure personnel safety Completed |
Evidence:
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Rotor and rotor system component removal is carried out in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices while observing all relevant WHS requirements, including the use of MSDS and items of PPE Completed |
Evidence:
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Required aircraft maintenance documentation is completed and processed in accordance with standard enterprise procedures Completed |
Evidence:
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Removed components are labelled, sealed and packaged in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices Completed |
Evidence:
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Rotor or rotor system component to be installed is checked to confirm correct part or model numbers, modification status and serviceability Completed |
Evidence:
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Mass balance of rotor blades/head is checked in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices Completed |
Evidence:
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Installation is carried out in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices Completed |
Evidence:
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Support/safety equipment is removed at the appropriate time to ensure personnel safety and freedom from structural damage Completed |
Evidence:
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Remove and install rotor control system components
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System is rendered safe and prepared in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices, and isolation and warning signs are installed/fitted to ensure personnel safety Completed |
Evidence:
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Rotary wing flight control system component removal is carried out in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices while observing all relevant WHS requirements, including the use of MSDS and items of PPE Completed |
Evidence:
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Required aircraft maintenance documentation is completed and processed in accordance with standard enterprise procedures Completed |
Evidence:
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Removed components are labelled, sealed and packaged in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices Completed |
Evidence:
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Rotary wing flight control system components to be installed are checked to confirm correct part or model numbers, modification status and serviceability Completed |
Evidence:
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Installation is carried out in accordance with relevant aircraft publications/maintenance regulations/orders and standards and practices Completed |
Evidence:
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Support/safety equipment is removed at the appropriate time to ensure personnel safety and freedom from structural damage Completed |
Evidence:
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Required aircraft maintenance documentation is completed and processed in accordance with standard enterprise procedures Completed |
Evidence:
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Remove and install basic rotary wing airframe system components
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System is rendered safe in accordance with the applicable maintenance manual and isolation tags are fitted, where necessary, to ensure personnel safety Completed |
Evidence:
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Airframe system component removal is carried out in accordance with the applicable maintenance manual while observing all relevant WHS requirements, including the use of MSDS and items of PPE Completed |
Evidence:
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Required maintenance documentation is accurately completed and correctly processed Completed |
Evidence:
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Removed components are tagged, sealed and packaged in accordance with specified procedures Completed |
Evidence:
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Components to be installed are checked to confirm correct part numbers, serviceability and modification status Completed |
Evidence:
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Mass balance of control surfaces to be installed is checked in accordance with the applicable maintenance manual, if required Completed |
Evidence:
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Installation is carried out in accordance with the applicable maintenance manual Completed |
Evidence:
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Required maintenance documentation is completed and processed in accordance with standard enterprise procedures Completed |
Evidence:
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