Document ID: chunk:federal_register_of_legislation:F2024C00332:reg:8:p2
Version: federal_register_of_legislation:F2024C00332
Segment Type: reg
Provision Reference: reg 8 (pt 2/11)
Character Range: 179260–182070

to wear a headset under section 11.30, the flight crew member must use the headset as the primary device to communicate with ATS.

11.09  Navigation equipment
Note: For an aircraft entering oceanic airspace with RNP 2, RNP 4, or RNP 10, navigation specification capability, see subsections 11.03(1B) and (1C) of the Part 91 Manual of Standards in relation to long-range navigation systems (LRNS) operability requirements. The term oceanic airspace is defined in subsection 11.01(2) of the Part 91 Manual of Standards.
 (1) In this section:
approved GNSS means:
 (a) a GNSS system that is authorised in accordance with one of the following:
 (i) (E)TSO-C129;
 (ii) (E)TSO-C145;
 (iii) (E)TSO-C146;
 (iv) (E)TSO-C196a; or
Note: GNSS equipment authorised in accordance with (E)TSO-C129 is unlikely to support ADS-B position source equipment requirements.
 (b) a multi-sensor navigation system that:
 (i) includes GNSS and inertial integration; and
 (ii) is approved, under Part 21 of CASR, as providing a level of performance equivalent to a GNSS system mentioned in subparagraph (a) (ii), (iii) or (iv).
 (2) Without limiting the requirements under subsections (5) and (6), a rotorcraft for a VFR flight at night must be fitted with:
 (a) an approved GNSS; or
 (b) an ADF or VOR.
 (3) Subject to subsections (7) and (8), and without limiting the requirements under subsections (5) and (6), a rotorcraft for an IFR flight must be fitted with at least:
 (a) 2 approved GNSS; or
 (b) 1 approved GNSS and either:
 (i) 1 ADF; or
 (ii) 1 VOR.
 (4) For subsections (2) and (3), if an approved GNSS unit is provided with the automatic barometric aiding options stated in any of the following (the relevant options):
 (a) (E)TSO-C129a;
 (b) (E)TSO-C145a;
 (c) (E)TSO-C146a;
 (d) (E)TSO-C196a;
  then the relevant options must be connected.
 (5) The navigation equipment fitted to a rotorcraft 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 rotorcraft to navigate in accordance with:
 (a) the rotorcraft's operational flight plan; and
 (b)  the requirements of:
 (i) ATS; and
 (ii) the airspace in which the rotorcraft is planned to be flown.
 (6) For any aerodrome at which it is planned, or intended, that a rotorcraft may land in IMC, the rotorcraft's equipment must be capable of providing guidance to a point from which a safe visual, or instrument, landing may be conducted.
 (7) For paragraph (3)(a), an approved GNSS used to comply with that paragraph may not be authorised in accordance with (E)TSO-C129.
 (8) For paragraph (3)(b), an approved GNSS fitted to the rotorcraft must not be one authorised in accordance with (E)TSO-C129, unless:
 (a) the rotorcraft was manufactured before 6 February 2014; and