Document ID: chunk:federal_register_of_legislation:F2025C00050:body:0:p357
Version: federal_register_of_legislation:F2025C00050
Segment Type: other
Provision Reference: 
Character Range: 1239927–1243776

brakes;
(c)           flaps and slats.
5.1.5              Determine the airspeeds to meet performance requirements for different configurations and phases of flight.
5.1.6              Describe stall characteristics and limits of normal operating envelope.
5.1.7              Discuss the meteorological performance limiting factors.
5.1.8              Discuss any unique operational characteristics, including runway requirements/limitations.

6.                       Fuel and engine oil systems
6.1.1              Describe the following in relation 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              Determine level of engine oil.
6.1.3              Describe oil system indicators and grade of oil required.
6.1.4              Describe fuel and oil system limitations.

7.                       Engines
7.1.1              Describe type of engine/s installed, the main components, rated thrust or 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 feathering and unfeathering the propeller/s, where 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          Explain operation of the anti-skid system and limitations.
10.1.6          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 system
12.1.1          Explain the operation of aircraft heating, demisting, and airconditioning systems, normal and emergency modes of operation and