Google Links

Follow the links below to find material targeted to the unit's elements, performance criteria, required skills and knowledge

Elements and Performance Criteria

  1. Research and identify the range of basic scientific principles and techniques relevant to aeronautical engineering
  2. Select basic aeronautical scientific principles and techniques relevant to particular aeronautical engineering applications
  3. Apply the relevant basic aeronautical scientific principles and techniques appropriately
  4. Quote the results of the application of the basic aeronautical scientific principles and basic techniques correctly

Required Skills

Look for evidence that confirms knowledge of

basic aeronautical scientific principles including

statics complete tasks requiring analysis and application of

forces and moments of forces

systems of concurrent and nonconcurrent forces

dry sliding friction

dynamics complete tasks requiring analysis and application of

Newtons Laws

kinematics and kinetics of uniformly accelerated linear motion

kinematics and kinetics of uniformly accelerated rotation

curvilinear motion and centrifugal force

work energy power and torque

mechanical advantage and efficiency

strength of materials

axial tension and compression

direct shear

bolted riveted bonded and welded connections

shear in beams

bending stresses and bending deflections by standard formulas only

torsion

aerodynamics

Bernoullis Theorem

the atmosphere

aerodynamic forces lift drag weight and thrust

stability and control to a level not requiring the application of calculus

airscrews and propulsion to a level not requiring the application of calculus

aircraft performance to a level not requiring the application of calculus

fluid mechanics

properties of fluids including mineral and synthetic hydraulic fluids

fluid statics Archimedes Principle and Pascals Principle

fluid flow continuity and energy conservation

fluid power pumps

thermodynamics

heat transfer principles conduction convection and radiation

perfect gas laws

kinetic theory of gases

laws of thermodynamics

control concepts including closed and open loop control

electricity and electronics

basic electrical concepts

Ohms Law

Kirchhoffs Current and Voltage Laws

basic DC circuits

basic power supply transformer rectifier filter and regulator

PLC concepts IO timing counting programming

electronic devices discrete resistors diodes capacitors inductors transistors and rectifiers

microprocessor concepts

light sound and vibration

wave behaviour standing vs travelling waves transverse and longitudinal

light reflection absorption refraction diffraction spectrum infrared visible ultraviolet transmission medium and engineering applications

sound pitch frequency intensity power decibel scale noise dose spectrum infrasound audible ultrasound speed natural frequency resonance transmission medium and engineering applications

vibration sources balancing shaft alignment measurement damping and engineering applications

basic aeronautical techniques and related technologies software and hardware associated with implementing scientific principles in mechanical engineering solutions

the applicability and limitations of basic aeronautical scientific principles

the applicability and limitations of basic aeronautical techniques and associated technologies software and hardware

appropriateness of calculations

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 carrying out dimensional analysis

the concept of significant figures

the uncertainty of computations based on experimental data

the procedures for determining the significance of figures in calculations

the procedures for estimating errors in derived quantities

Look for evidence that confirms skills in

selecting appropriate basic aeronautical scientific principles to suit specific applications

selecting appropriate basic aeronautical techniques and associated technologies software and hardware to suit specific applications

applying basic aeronautical scientific principles to particular engineering situations

applying and manipulating appropriate formulas for applications involving engineering calculations

applying appropriate calculations to engineering situations

checking the validity of equations is using dimensional analysis

applying basic aeronautical 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 using appropriate significant figures

quoting limitations of solutions due to assumptions scientific principles and techniques used

presenting solutions referring to the original aim of the application

Evidence Required

The evidence guide provides advice on assessment and must be read in conjunction with the performance criteria required skills and knowledge range statement and the Assessment Guidelines for the Training Package

Overview of assessment

A person who demonstrates competency in this unit must be able to apply basic scientific principles and techniques in aeronautical engineering situations

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 supervisors 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 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 basic scientific 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


Range Statement

The range statement relates to the unit of competency as a whole. It allows for different work environments and situations that may affect performance. Bold italicised wording, if used in the performance criteria, is detailed below. Essential operating conditions that may be present with training and assessment (depending on the work situation, needs of the candidate, accessibility of the item, and local industry and regional contexts) may also be included.

Sources of information

Sources of information include:

reference texts

manufacturer catalogues and industrial magazines

international aerospace organisation publications

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

Relevant basic aeronautical scientific techniques and principles

Candidates should apply appropriate basic techniques supported by their mathematical skills and introductory knowledge of scientific principles to design, manufacturing, commissioning and maintenance related tasks and projects relating to metal and composite structure, aerodynamic loads, stability, control and performance, mechanical systems and related components, hydraulic systems and related components, pneumatic systems and related components, air cycle air conditioning and pressurisation systems and related components, power plant systems and components, and the application and interfacing of electrical and electronic system control.

The applications may require the use of one or two basic aeronautical scientific principles together with a fundamental mathematical calculation leading to process, resources and system choices from a limited range of options.

Basic techniques include:

basic hand and power tool operations

machining

fitting

welding

moulding

fabricating

wiring and programming techniques