Document ID: chunk:federal_register_of_legislation:F2025C00050:body:0:p360
Version: federal_register_of_legislation:F2025C00050
Segment Type: other
Provision Reference: 
Character Range: 1250414–1254232

to the aircraft's fuel system:
(a)           location of fuel tank/s and capacity;
(b)           normal and non-normal fuel system operation and distribution;
(c)           location and type of pumps used;
(d)           vents system and location of vents and drains;
(e)           system controls and indicators;
(f)             minimum grades, colour and additives required, if any;
(g)           minimum fuel temperature;
(h)           indications of reduced or loss of fuel flow.
6.1.2              Minimum level of engine oil.
6.1.3              The aeroplane's oil system indicators and grade of oil required.
6.1.4              Fuel and oil system limitations for the aeroplane.

7.                       Engines
7.1.1              Describe type of engine/s installed, the main components, rated horsepower and indicators required for operation.
7.1.2              State engine start limits, as applicable.
7.1.3              Describe engine controls and their function.
7.1.4              Describe normal and non-normal engine operation.
7.1.5              Describe operation of the ignition system.
7.1.6              Describe the method of rotor engagement, as applicable.

8.                       Electrical system
8.1.1              Describe core components of the aircraft's electrical system.
8.1.2              Describe the system design and operation, including use of AC or DC power, as applicable.
8.1.3              Explain the methods of power generation.
8.1.4              Describe the electrical system protections and locations of key components.
8.1.5              Explain the indications of normal and degraded system operation.
8.1.6              Describe the location of connections for external sources of power, if applicable.
8.1.7              Describe the use of the APU when used to provide a source of electrical power.

9.                       Hydraulic system
9.1.1              Describe core components of the aircraft hydraulic system/s and their method of operation, including alternative sources of operation.
9.1.2              Describe normal system operating pressure and system protections to prevent damage to components or system.
9.1.3              Explain method of determining sufficient system capacity, indicators and controls.
9.1.4              Describe systems operated by the hydraulic system/s.

10.                   Undercarriage and brakes
10.1.1          Describe the undercarriage system components and safety systems.
10.1.2          Explain normal and alternative method of undercarriage operation.
10.1.3          Describe operation of the nosewheel steering system, if installed.
10.1.4          Describe the brake system components and normal and non-normal operation.
10.1.5          Determine brake energy limits and brake cooling requirements.

11.                   Pneumatic system
11.1.1          Describe the aircraft pneumatic system components and methods of operation.
11.1.2          Describe system limitations and safety devices.

12.                   Environmental/pressurisation system
12.1.1          Explain the operation of aircraft heating, demisting, and airconditioning systems, if applicable, normal and emergency modes of operation and limitations.

13.                   Flight controls
13.1.1          Describe primary and secondary flight controls and their method of operation.
13.1.2          Knowledge of limitations and safety features that prevent structural damage to the aircraft.

14.                   Ice and rain protection
14.1.1          Describe the aircraft ice protection system/s, detection systems and explain their operation.
14.1.2          Describe anti-ice system limitations, if applicable.

15.                   Fire and overheat protection
15.1.1          Describe the fire and overheat protection