This unit applies to selecting and applying aeronautical system design principles and techniques appropriate to aeronautical engineering applications. Computer techniques, graphical methods and mathematical calculations should complement scientific principles chosen and include unit analysis, appropriate precision and accuracy, and use conservative estimations. |
Apply basic scientific principles and techniques in aeronautical engineering |
1 | Identify the range of aeronautical system design principles and techniques relevant to aeronautical engineering | 1.1 | Research and report on aeronautical system design principles using appropriate sources of information |
1.2 | Identify the aeronautical system design principles relating to aeronautical engineering applications | ||
1.3 | Research and report on aeronautical system design techniques and associated technologies, software and hardware associated with implementing scientific principles relating to aeronautical engineering applications using appropriate sources of information | ||
2 | Select aeronautical system design principles and techniques relevant to aeronautical engineering applications | 2.1 | Select the relevant aeronautical system design principles for particular aeronautical engineering situations |
2.2 | Select the relevant aeronautical system design techniques and associated technologies, software and hardware for particular aeronautical engineering situations | ||
3 | Apply the relevant aeronautical system design principles and techniques appropriately | 3.1 | Apply the aeronautical system design principles in a consistent and appropriate manner to obtain any required solution |
3.2 | Use appropriate calculations and correct units to establish quantities | ||
3.3 | Use coherent units in equations in a systematic manner to ensure meaningful solutions | ||
3.4 | Use significant figures are used in engineering calculations | ||
3.5 | Apply the aeronautical system design techniques and associated technologies, software and hardware in a consistent and appropriate manner to obtain required solutions | ||
4 | Quote the results of the application of the aeronautical system design principles and techniques correctly | 4.1 | Quote solutions for applications involving engineering calculations in an appropriate style |
4.2 | Quote solutions for applications not involving engineering calculations in an appropriate style |
Required knowledge includes: aeronautical engineering techniques and related technologies, software and hardware associated with implementing scientific principles in engineering solutions and related to appropriate engineering applications the limitations of aeronautical engineering techniques and associated technologies, software and hardware the relevance of scientific principles to aeronautical engineering the applicability and limitations of an extensive range of aeronautical engineering techniques and associated technologies, software and hardware the choice of aeronautical engineering scientific principles for particular applications the applicability of particular aeronautical engineering techniques and associated technologies, software and hardware to specific applications the choice of aeronautical engineering techniques and associated technologies, software and hardware for particular applications the method of application of the scientific principles fundamental and derived quantities common systems of units the procedure for converting between systems of units common prefixes used with units and their values the procedure for ensuring coherent units for meaningful solutions to equations the concept of significant figures the uncertainty of computations based on experimental data procedures for determining the significance of figures in calculations procedures for estimating errors in derived quantities the method of application of the aeronautical engineering techniques and associated technologies, software and hardware the significance of the calculation solution style in relation to the original task the significance of the non-calculation solution style in relation to the original task Required skills include: applying advanced scientific principles relevant to aeronautical engineering analysing the given situation to determine what is required in the manner of a solution analysing the given situation to determine which aeronautical engineering scientific principles are selected selecting appropriate aeronautical engineering techniques and associated technologies, software and hardware to suit the application/s applying appropriate aeronautical engineering principles in determining the required solution applying and manipulating formulas and calculations for engineering applications using the correct units to solve engineering calculations checking the validity of equations using a systematic method for ensuring coherent units applying aeronautical engineering techniques and associated technologies, software and hardware in a manner appropriate to the application and identified scientific principles referring solutions to the original aim of the application quoting solutions in appropriate units and using appropriate significant figures presenting solutions referring to the original aim of the application |
Overview of assessment | A person who demonstrates competency in this unit must be able to apply aeronautical system design principles and techniques in mechanical engineering situations. Competency in this unit cannot be claimed until all prerequisites have been satisfied. |
Critical aspects for assessment and evidence required to demonstrate competency in this unit | Assessors must be satisfied that the candidate can competently and consistently perform all elements of the unit as specified by the criteria, including required knowledge, and be capable of applying the competency in new and different situations and contexts. Assessors should gather a range of evidence that is valid, sufficient, current and authentic. Evidence can be gathered through a variety of ways including direct observation, supervisor’s reports, project work, samples and questioning. Questioning techniques should not require language, literacy and numeracy skills beyond those required in this unit of competency. |
Context of and specific resources for assessment | This unit may be assessed on the job, off the job or a combination of both on and off the job. Where assessment occurs off the job, that is the candidate is not in productive work, then an appropriate simulation must be used where the range of conditions reflects realistic workplace situations. The competencies covered by this unit would be demonstrated by an individual working alone or as part of a team. The assessment environment should not disadvantage the candidate. The candidate must have access to all tools, equipment, materials and documentation required. The candidate must be permitted to refer to any relevant workplace procedures, product and manufacturing specifications, codes, standards, manuals and reference materials. |
Method of assessment | This unit could be assessed in conjunction with any other units addressing the safety, quality, communication, materials handling, recording and reporting associated with applying aeronautical system design principles and techniques in aeronautical engineering situations or other units requiring the exercise of the skills and knowledge covered by this unit. |
Guidance information for assessment |
Aeronautical systems | Aeronautical systems may include: hydraulic systems (utility and flight control) pneumatic systems mechanical systems air and vapour cycle air conditioning systems pressurisation systems fuel storage and distribution systems fire extinguishing systems |
Sources of information | Sources of information include: reference texts manufacturer catalogues and industrial magazines websites use of phone, email and fax information gathering |
Aeronautical engineering | Aeronautical engineering refers to: the engineering discipline concerned with the conceptual development, research, design, manufacture, implementation, installation, commissioning and maintenance of aerospace mechanical, hydraulic, pneumatic, fuel and fire products, processes, systems or services for civil and military applications |
Aeronautical engineering situations | Aeronautical engineering situations may include: working as a member of a design team developing repair schemes developing modifications designing test equipment developing fault trees/diagnosis guides |
Engineering science
This unit contains employability skills
Not applicable.