UniKL VLE

Hi All!

This is the introductory course to the aircraft landing gear systems and maintenance, such as the component of shock strut, aircraft brakes, aircraft wheel, aircraft tube and tires and anti skid brake control system.

Upon completion of this course students should be able to:

2.    DESCRIBE and EXPLAIN the operations, constructions, systems layout and components of the AIRCRAFT LANDING GEAR SYSTEM using appropriate drawings or schematic diagrams.

3.    CARRY OUT AIRCRAFT LANDING GEAR SYSTEM components removal & installation as per AMM procedures.

4.    CARRY OUT AIRCRAFT LANDING GEAR SYSTEMS servicing as per AMM procedures.

All the best!!!

LEARNING OUTCOMES:

Upon completion of this course students should be able to.

1. IDENTIFY (C1) and DESCRIBE (Cl) the appropriate regulatory requirements relating to turbine engines constructions

2. EXPLAIN (C2) the constructions of the turbine engine using appropriate drawings or schematic diagrams

3. EXAMINE (C3) the operations, working principles and their related components using appropriate drawings and schematic diagrams

4. TROUBLE-SHOOT (P4), INSPECT (P1) and CARRY OUT (P4) replacements of the turbine engine components as per the relevant technical documents

5. PERFORM (P4) servicing of the turbine engine components as per the relevant technical documents.

6. PERFORM (C3) all documentations relevant to the rnaintenance tasks carried out on an aircraft in accordance with the appropriate regulatory requirements

Upon completion of this course students should be able to:

1.     Identify and describe the appropriate regulatory requirements relating to turbine engines’ systems.

2.     Describe typical examples of the constructions, systems layout and components of the turbine engines’ systems using appropriate drawings or schematic diagrams.

3.     Describe the operations of the turbine engines’ systems and their related components using appropriate drawings and schematic diagrams.

4.     Perform inspections, trouble-shooting and replacements of the turbine engines’ systems and components as per the relevant technical documents.

5.     Perform servicing of the turbine engines’ systems and components as per the relevant technical documents.

6.     Effect the documentations and certifications for maintenance tasks carried out on an aircraft in accordance with the appropriate regulatory requirements.

This is part two study on gas turbine engines. As a continuation of part one, this part two describes the bearings used in gas turbine engines, the lubrication and air sealing of the bearings, and how the same air system cools the hot section components of the engine. The study looks at how the fuel metering, starting, and ignition system support the operation of gas turbine engines. To read engine power and monitor engine operation from the flight deck, the study covers the various engine instrumentation system

LEARNING OUTCOMES:

Upon completion of this course students should be able to.

1. IDENTIFY (C1) and DESCRIBE (Cl) the appropriate regulatory requirements relating to turbine engines constructions

2. EXPLAIN (C2) the constructions of the turbine engine using appropriate drawings or schematic diagrams

3. EXAMINE (C3) the operations, working principles and their related components using appropriate drawings and schematic diagrams

4. TROUBLE-SHOOT (P4), INSPECT (P1) and CARRY OUT (P4) replacements of the turbine engine components as per the relevant technical documents

5. PERFORM (P4) servicing of the turbine engine components as per the relevant technical documents.

6. PERFORM (C3) all documentations relevant to the rnaintenance tasks carried out on an aircraft in accordance with the appropriate regulatory requirements