Document ID: chunk:federal_register_of_legislation:F2018C00889:front:0:p7
Version: federal_register_of_legislation:F2018C00889
Segment Type: other
Provision Reference: 
Character Range: 18260–20680

relevant Appendix); and
(b) complies with each requirement for the flight set out in the relevant Appendix; and
(c) ensures that each member of the flight crew of the aircraft:
           (i) satisfies each flight crew requirement for the flight set out in the relevant Appendix; and
           (ii) conducts the flight in accordance with the navigation authorisation.
       8.4 Operators of foreign registered aircraft holding an RNP AR navigation authorisation must not navigate in accordance with RNP AR procedures in Australia without prior CASA acceptance of that navigation authorisation.

9 Certain aircraft are deemed to be approved for navigation specifications in Appendices 1, 2, 3 and 4
       9.1Subject to compliance with paragraphs 9.2 and 9.3, an Australian aircraft is deemed to be approved for navigation in accordance with any of the following navigation specifications:
(a) RNAV 5;
(b) RNAV 1 and RNAV 2;
(c) RNP 2;
(d) RNP 1.
       9.2 The aircraft must be equipped with a GNSS stand-alone system with en route and terminal navigation capability having:
(a) (E)TSO-C129 ( ) authorisation for Class A1 or A2; or
(b) (E)TSO-C146 ( ) authorisation for Class Gamma and operational Class 1, 2 or 3; or
(c) an integrated avionics system using GNSS sensors with (E)TSO‑C129 ( ) Class B1, B2, C1 or C2 authorisation, or (E)TSO‑C145 ( ) Class Beta and operational Class 1, 2 or 3 authorisation as the only primary sensor input to the area navigation function, that is accepted as a stand-alone system for this subsection.
Note   The integrated avionics systems referred to are those systems typically installed in US 14 CFR/EASA CS Part 23 or Part 27 aircraft that combine flight displays, communications, radio navigation (VOR and ILS) and area navigation into a single integrated system. (E)TSO C115 multi-sensor systems that utilise independent discrete sensor inputs are not addressed under this subsection.
       9.3The aircraft is approved for navigation during a flight in accordance with a navigation specification mentioned in paragraph 9.1 if the AFM or AFMS for the aircraft, as published at the time of the flight, states that the aircraft:
(a) is capable of the navigation specification; or
(b) has the GPS capability mentioned in an item of the Table that corresponds to the navigation specification.

    Table
   GPS capability     Navigation specification
   (Column 1)         (Column 2)