Document ID: chunk:federal_register_of_legislation:F2024C01173:reg:7:p2
Version: federal_register_of_legislation:F2024C01173
Segment Type: reg
Provision Reference: reg 7 (pt 2/11)
Character Range: 228598–231360

an approved GNSS unit is provided with the automatic barometric aiding options stated in any of the following (the relevant options):
 (a) (E)TSO-129a;
 (b) (E)TSO-C145a;
 (c) (E)TSO-C146a;
 (d) (E)TSO-C196a;
then the relevant options must be connected.
 (4) For paragraph (2)(b), an approved GNSS must not be one authorised in accordance with (E)TSO‑C129 unless:
 (a) the aeroplane is manufactured before 6 February 2014; and
 (b) the approved GNSS fitted to the aeroplane is installed before 6 February 2014.
 (5) The navigation equipment fitted to an aeroplane must be such that, in the event of the failure of any navigation equipment at any stage of a flight, sufficient navigation equipment remains to enable the aeroplane to navigate in accordance with:
 (a) the operational flight plan; and
 (b) the requirements of:
 (i) relevant air traffic services; and
 (ii) the airspace in which the aeroplane is planned to be flown.
 (6) For any aerodrome at which it is planned or intended that an aeroplane may land in IMC, the aeroplane's equipment must be capable of providing guidance to a point from which a safe visual or instrument landing may be conducted.
Note: Section 11.03 of the Part 91 Manual of Standards prescribes, under regulation 91.255 (which is applicable generally) requirements relating to oceanic airspace. When entering oceanic airspace that requires the use of RNP 2, RNP 4 or RNP 10 navigation specification, the crew must check whether at least 2 long range navigation systems (LRNS) are operable. If less than 2 LRNSs are operable, then air traffic control must be informed of the situation.

11.10  Automatic pilot
 (1) Subject to subsection (3), an aeroplane must be fitted with an automatic pilot.
 (2) The automatic pilot must have at least the following modes:
 (a) an altitude holding mode;
 (b) a heading mode.
 (3) Subsection (1) does not apply if the aeroplane is fitted with fully functioning dual controls.

11.11  Equipment to ensure clear view through the windshield
 (1) An aeroplane with a maximum take-off weight of more than 5 700 kg must be fitted with equipment to remove precipitation from the area of windshield directly in front of a pilot's seat.
 (2) An aeroplane with a maximum take-off weight of 5 700 kg or less must:
 (a) meet the requirement under subsection (1) as if it applied to the aeroplane; or
 (b) have a windshield whose design is such that moderate rain will not impair the pilot's view for take-off, landing or normal flight.
Note: Subsection 11.07(2) of the Part 91 Manual of Standards requires RVSM operations to be conducted in accordance with the requirements of the authorised aeronautical information. For an aeroplane that does not have an automatic pilot with the altitude hold function