11Certain other aircraft deemed to be approved for navigation authorisations in Appendices 1, 2, 3, 4 and 6

11 Certain other aircraft deemed to be approved for navigation authorisations in Appendices 1, 2, 3, 4 and 6

11.1Subject to compliance with paragraphs 11.2 and 11.3, an Australian aircraft is deemed to be approved for navigation in accordance with any of the following navigation specifications:

(e) RNP APCH-LNAV;

(f) RNP APCH-LNAV/VNAV;

(g) RNP APCH-LP or RNP APCH-LPV.

11.2 The aircraft must be equipped with:

(a) a GNSS stand-alone system with en route, terminal, NPA and LPV capability having (E)TSO-C146 ( ) authorisation for Class Gamma and operational Class 3; or

(b) an integrated avionics system using GNSS sensors with (E)TSO‑C145 ( ) Class Beta and operational Class 3 authorisation as the only primary sensor input to the area navigation function is deemed to be 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.

11.3The aircraft is approved for navigation during a flight in accordance with a navigation specification mentioned in paragraph 11.1 if the AFM or AFMS for the aircraft, as published at the time of the flight, states that the aircraft:

(b) has the GPS capability mentioned in an item in the Table that corresponds to the navigation specification.

Note For example, for the purposes of subparagraph 11.3 (b), if the AFM or AFMS for an aircraft states that the aircraft is capable of GPS RNAV NON-PRECISION APPROACH (a “GPS capability”), then the aircraft would be approved to navigate in accordance with RNP APCH-LNAV (the corresponding “navigation specification”).