Document ID: chunk:federal_register_of_legislation:F2018C00889:reg:2:p1
Version: federal_register_of_legislation:F2018C00889
Segment Type: reg
Provision Reference: reg 2 (pt 1/2)
Character Range: 20727–23454

2  GPS RNAV TERMINAL  RNAV 1 or RNP 1

Note   For example, for the purposes of subparagraph 9.3 (b), if the AFM or AFMS for an aircraft states that the aircraft is capable of GPS RNAV TERMINAL (a "GPS capability"), then the aircraft would be approved to navigate in accordance with RNAV 1 (the corresponding "navigation specification").
       9.5 If the AFM or AFMS for an aircraft states that the aircraft is approved for RF Legs and the aircraft:
(a) meets the requirements of paragraph 9.3; and
(b) is equipped with a map display depicting the computed flight path of the aircraft;
       the aircraft is taken to be approved for RF Legs in conjunction with RNP 1 operations.
       9.6 If the AFM or AFMS for an aircraft states that the aircraft is approved for Radius to FRT, and the aircraft:
(a) meets the requirements in paragraph 9.3 above; and
(b) is equipped with a map display depicting the computed flight path of the aircraft;
       the aircraft is taken to be approved for FRT in conjunction with RNP 2 operations.

10 Certain aircraft are deemed to be approved for navigation specifications in Appendices 1, 2, 3, 4 and 6
       10.1Subject to compliance with paragraphs 10.2 and 10.3, 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;
(e) RNP APCH-LNAV;
(f) RNP APCH-LNAV/VNAV;
(g) RNP APCH-LP or RNP APCH-LPV.
       10.2 The aircraft must be equipped with:
(a) a GNSS stand-alone system with en route, terminal and NPA capability having (E)TSO-C129a authorisation for Class A1; or
(b) a GNSS stand-alone system with en route, terminal and NPA capability having (E)TSO-C146 Class Gamma and operational Class 1, 2 or 3; or
(c) an integrated avionics system using a GNSS sensor with (E)TSO‑C129a Class B1 or C1 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 in subparagraph 10.2 (b) 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.
       10.3The aircraft is approved for navigation during a flight in accordance with a navigation specification mentioned in paragraph 10.1 if the AFM or AFMS for the aircraft, as published at the time of the flight, states that the aircraft:
(a)