Document ID: chunk:federal_register_of_legislation:F2025C00050:body:0:p366
Version: federal_register_of_legislation:F2025C00050
Segment Type: other
Provision Reference: 
Character Range: 1270120–1273859

if installed.
24.5.4          Describe the brake system components and normal and non-normal operation.
24.6                Pneumatic system
24.6.1          Describe the aircraft pneumatic system components and methods of operation.
24.6.2          Describe system limitations and safety devices.
24.7                Environmental/pressurisation system
24.7.1          Describe aircraft pressurisation system components and methods of normal and non-normal operation.
24.7.2          Explain the aircraft pressurisation limitations and safety features.
24.7.3          Describe the differences between gradual and rapid depressurisation experienced by the occupants of the aircraft.
24.7.4          Describes the reason for pressurisation limitation for take-off and landing.
24.7.5          Explain why a pressurised aircraft is fitted with a cabin altimeter.
24.7.6          Describe how to determine that the pressurisation system is functioning correctly.
24.8                Flight controls
24.8.1          Describe primary and secondary flight controls and their method of operation.
24.8.2          Describe the operation of speed-sensing devices that limit or operate flight controls where installed.
24.8.3          Describe degraded modes of operation for aircraft fitted with fly-by-wire flight control systems, the degraded protection provided and the effects on longitudinal stability with changes in aircraft speed.
24.8.4          Knowledge of limitations and safety features that prevent structural damage to the aircraft.
24.9                Ice and rain protection
24.9.1          Describe the aircraft ice protection system/s, detection systems and explain their operation.
24.9.2          Describe anti-ice system limitations.
24.10            Fire and overheat protection
24.10.1      Describe the fire and overheat protection system/s installed on the aircraft, including indicators and extinguishing agents used.
24.10.2      Can determine the serviceability of the system/s.
24.10.3      Describe the power sources necessary for system operation.
24.11            Flight instruments
24.11.1      Describe the system/s that provide data to the primary flight instruments.
24.11.2      Describe the power sources for the primary flight instruments/displays.
24.11.3      Describe the operation of the stall avoidance and/or warning systems.
24.11.4      Knowledge of alternative sources of operation.
24.12            Navigation
24.12.1      Knowledge of the operation of the aircraft navigation system/s, including transponder/s and flight director/s and limitations.
24.12.2      Describe the operation of the aircraft navigation receivers and how to determine their working status.
24.12.3      Knowledge of the aircraft's weather detection system/s and safety precautions.
24.12.4      Operation of the aircraft FMS and cane determine signals used to determine aircraft position.
24.12.5      Describe the operation of the aircraft TCAS system.
24.12.6      Understanding of the aircraft windshear detection system, if installed.
24.13            Autoflight
24.13.1      Knowledge of autopilot and autothrottle, if installed, in flight operation in all modes.
24.13.2      Describe failure annunciations and pilot actions.
24.13.3      Understanding of interface with aircraft navigation systems.
24.13.4      Describe autoflight limitations.
24.14            Communications
24.14.1      Can operate all the aircraft communication systems, voice and data when installed.
24.14.2      Describe operation of aircraft intercommunication systems.
24.14.3      Describe operation of the communications system in the event of depressurisation or use of emergency oxygen system.
24.14.4      Explain operation of the CVR