Document ID: chunk:federal_register_of_legislation:F2024C01173:reg:7:p5
Version: federal_register_of_legislation:F2024C01173
Segment Type: reg
Provision Reference: reg 7 (pt 5/11)
Character Range: 236047–238875

until the time the engines are shut down at the end of the flight.
 (4) For anti-collision light equipment comprising white strobe lights only, the lights must be displayed as follows:
 (a) for a turbine-engine aeroplane—from immediately before the engines are started until the time the engines are shut down at the end of the flight;
 (b) for any other aeroplane—from immediately after the engines are started until the time the engines are shut down at the end of the flight.
 (5) For anti-collision light equipment comprising a combination of red beacon lights and white strobe lights, the lights must be displayed as follows:
 (a) for the red beacon lights—in accordance with the requirements in subsection (3);
 (b) for the white strobe lights, in accordance with the following:
 (i) if the aeroplane, on its way to the runway from which it will take off, or on its way from the runway on which it has landed, crosses any other runway that is in use for take-offs or landings (an active runway)—while the aeroplane is crossing the active runway;
 (ii) from the time the aeroplane first enters the runway from which the aeroplane will take off until the time the aeroplane leaves the runway on which it has landed.
 (6) Subsections (3), (4) and (5) do not apply if the pilot in command reasonably believes that, in the circumstances, reflection or glare from the anti-collision light system may cause a hazard to an aircraft.

11.17  Landing lights
  An aeroplane operating by night must be fitted with at least:
 (a) 2 landing lights; or
 (b) a single landing light having 2 independent and separately energised illumination sources.

       11.18  Navigation lights
        (1) An aeroplane operating by night must be fitted with navigation lights.
        (2) If required to be fitted under subsection (1), the navigation lights must be displayed during a flight and when operating on the movement area of an aerodrome.

Division 6—Alerting and warning system requirements

11.19  Altitude alerting system and assigned altitude indicator
 (1) The following aeroplanes must be fitted with altitude alerting equipment in accordance with subsection (2):
 (a) a piston-engine aeroplane operating in controlled airspace above FL 150;
 (b) a turbine-engine aeroplane.
 (2) For subsection (1), the altitude alerting equipment must:
 (a) include an assigned altitude indicator; and
 (b) alert the flight crew if the aeroplane approaches a preselected altitude; and
 (c) alert the flight crew, including by an aural or visual warning, if the aeroplane deviates from a preselected altitude.
 (3) An aeroplane that is not required to be fitted with altitude alerting equipment under subsection (1) must be fitted with altitude alerting equipment at least in the form of an assigned altitude indicator.

11.20  Aeroplane flown with