Assessor Resource

MEA318B
Inspect aircraft hydro-mechanical, mechanical, gaseous and landing gear systems and components

Assessment tool

Version 1.0
Issue Date: May 2024


This unit requires application of hand skills, standard trade practices and systems knowledge in the inspection of aircraft hydro-mechanical, mechanical, gaseous and landing gear systems and components.

Applications include hydro-mechanical, mechanical, gaseous and landing gear systems and components fitted to fixed wing aircraft.

This unit is part of the Mechanical AME Certificate IV training pathways. It covers the competencies required to inspect aircraft hydro-mechanical, gaseous and landing gear systems and components. Where a CASA licensing outcome is sought this unit forms part of the CASA requirement for the granting of the chosen B1 Aircraft Maintenance Engineer licence under CASR Part 66, in accordance with the licensing provisions in Section 3, Assessment Guidelines.

You may want to include more information here about the target group and the purpose of the assessments (eg formative, summative, recognition)

Prerequisites

MEA302C

Remove and install aircraft hydro-mechanical system and landing gear components

MEA303C

Remove and install aircraft pneumatic system components

MEA305C

Remove and install aircraft fixed wing flight control system components

Employability Skills

This unit contains employability skills.



Evidence Required

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.

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 inspect a range of hydraulic, fuel, gaseous and mechanical system and landing gear components in accordance with relevant maintenance manual instructions while applying all relevant OH&S procedures and standard processes.

Critical aspects for assessment and evidence required to demonstrate competency in this unit

The underlying skills inherent in this unit should be transferable across a range of inspection applications (including the timely involvement of supervisors or other trades) associated with aircraft hydro-mechanical, gaseous, mechanical and landing gear systems and their components. It is essential that system test procedures take into account all safety precautions applicable to the system being maintained, especially where system operation/switching inter-relates to other systems being maintained. Ability to interpret inspection procedures and specifications (allowable limits) and apply them in practice is critical.

Evidence of transferability of skills and knowledge related to inspection is essential. This may be demonstrated through application across a number of aircraft systems or aircraft types. The work plan should take account of applicable safety and quality requirements in accordance with the industry and regulatory standards.

A person cannot be assessed as competent until it can be demonstrated to the satisfaction of the workplace assessor that the relevant elements of this Unit of Competency are being achieved under routine supervision on each type of system and on at least one component of each group listed in the Range Statement, as follows:

Hydraulic systems - a system and at least one component from each of hydro-mechanical system components 3 and 5

Fuel systems - a system and at least one component from each of hydro-mechanical system components 4 and 5

Landing gear systems - each listed system 6 to 8

Landing gear components - one each of 9 to 11

Gaseous systems - each listed system 12 to 15 and at least one component from each of gaseous system components 16 to 19

Mechanical systems - a system applicable to each of system types 20 and 21 and at least one component from each of mechanical system components 22 to 24

This shall be established via the records in the Log of Industrial Experience and Achievement or, where appropriate, an equivalent Industry .

Context of and specific resources for assessment

Competency should be assessed in the work environment or simulated work environment, using procedures, tools and equipment specified in maintenance documentation. It is also expected that general purpose tools, test and ground support equipment found in most routine situations would be used where appropriate.

Method of assessment

Guidance information for assessment

Submission Requirements

List each assessment task's title, type (eg project, observation/demonstration, essay, assingnment, checklist) and due date here

Assessment task 1: [title]      Due date:

(add new lines for each of the assessment tasks)

Assessment Tasks

Copy and paste from the following data to produce each assessment task. Write these in plain English and spell out how, when and where the task is to be carried out, under what conditions, and what resources are needed. Include guidelines about how well the candidate has to perform a task for it to be judged satisfactory.

Required skills

Look for evidence that confirms skills in:

Application of all relevant OH&S procedures

The use of maintenance manuals and documentation to prepare the aircraft and identify requirements for inspection of hydraulic, fuel, gaseous, flight control, landing gear and mechanical systems and components

Use of hand skills and tools in the inspection, adjustment and troubleshooting of hydraulic, fuel, gaseous, flight control, landing gear and mechanical systems

Use of hand skills and tools in the inspection of hydraulic, fuel, flight control, gaseous and mechanical system components

Jacking of the aircraft as required for landing gear system inspection

Use of hand skills and tools in the inspection of landing gear components

The recognition of external defects in hydraulic, fuel, gaseous, flight control, landing gear and mechanical systems and components

Required knowledge

Look for evidence that confirms knowledge of:

How to recognise external defects in hydraulic, fuel, gaseous, flight control, landing gear and mechanical system components

How to configure the aircraft for inspection of hydraulic, fuel, gaseous, flight control, landing gear and mechanical systems and components

Inspection and testing requirements for gears, springs and bearings

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.

Note

Range statements listed below are numbered to facilitate specification of the assessment requirements included in the Evidence Guide.

Hydro-mechanical systems and system components

Hydro-mechanical systems include:

1. Hydraulic systems

2. Fuel systems

Components of hydro-mechanical systems include:

3. Hydraulic accumulators, filters, reservoirs, valves, pumps, motors, actuators, regulators, direct reading gauges

4. Fuel system filters, valves, pumps, rigid and flexible storage cells/tanks

5. Rigid and flexible pipelines, hoses and fittings

Landing gear systems and system components

(components of landing gear retraction, steering and braking systems are covered by hydro-mechanical and mechanical system components)

Landing gear systems include:

6. Retraction systems

7. Steering systems

8. Brake systems, including anti-skid where applicable

Landing gear components include:

9. Wheel assemblies

10. Brake units

11. Struts/oleos

Gaseous systems and system components

Gaseous systems include:

12. Pneumatic

13. Air cycle air conditioning

14. Pressurisation

15. Fire extinguishing

Gaseous system components include:

16. Gauges (direct reading), temperature sensors, pressurisation controllers, temperature controllers

17. Heat exchangers, pressure vessels, condensers, compressors, expansion turbines, humidifiers, valves, actuators

18. Rigid and flexible pipelines and fittings

19. Ducting

Mechanical systems and system components

Mechanical systems include:

20. Mechanical operating and locking systems

21. Mechanical flight control systems or the mechanical elements of power-assisted flight control systems

Mechanical system components include:

22. Cables, pulleys, guides, fairleads, tension regulators, chains, sprockets

23. Control rods, torque tubes, bellcranks, screwjacks, clutches, springs, bearings, gears

24. Control sticks, wheels, columns, trim wheels or handles, rudder pedals

Application of this unit may relate to:

Scheduled or unscheduled maintenance activities

Individual or team related activities

Procedures and requirements

Refer to industry standard procedures specified by manufacturers, regulatory authorities or the enterprise

Copy and paste from the following performance criteria to create an observation checklist for each task. When you have finished writing your assessment tool every one of these must have been addressed, preferably several times in a variety of contexts. To ensure this occurs download the assessment matrix for the unit; enter each assessment task as a column header and place check marks against each performance criteria that task addresses.

Observation Checklist

Tasks to be observed according to workplace/college/TAFE policy and procedures, relevant legislation and Codes of Practice Yes No Comments/feedback
Isolation tags already attached to the system or related systems are checked and aircraft configured for safe system inspection and operation in accordance with specified procedures. 
Hydro-mechanical system and system components are visually or physically checked for external signs of defects in accordance with specified procedures. 
Isolation tags already attached to the system or related systems are checked and aircraft configured, including jacking where necessary, for safe system inspection and operation in accordance with specified procedures. 
Landing gear system and system components are visually or physically checked for external signs of defects in accordance with specified procedures. 
Isolation tags already attached to the system or related systems are checked and aircraft configured for safe system inspection and operation in accordance with specified procedures. 
Gaseous system and system components are visually or physically checked for external signs of defects in accordance with specified procedures. 
Isolation tags already attached to the system or related systems are checked and aircraft configured for safe system inspection and operation in accordance with specified procedures. 
Mechanical system and system components are visually or physically checked for external signs of defects in accordance with specified procedures. 

Forms

Assessment Cover Sheet

MEA318B - Inspect aircraft hydro-mechanical, mechanical, gaseous and landing gear systems and components
Assessment task 1: [title]

Student name:

Student ID:

I declare that the assessment tasks submitted for this unit are my own work.

Student signature:

Result: Competent Not yet competent

Feedback to student

 

 

 

 

 

 

 

 

Assessor name:

Signature:

Date:

Assessment Record Sheet

MEA318B - Inspect aircraft hydro-mechanical, mechanical, gaseous and landing gear systems and components

Student name:

Student ID:

Assessment task 1: [title] Result: Competent Not yet competent

(add lines for each task)

Feedback to student:

 

 

 

 

 

 

 

 

Overall assessment result: Competent Not yet competent

Assessor name:

Signature:

Date:

Student signature:

Date: