Document ID: chunk:federal_register_of_legislation:F2018C00889:reg:5:p2
Version: federal_register_of_legislation:F2018C00889
Segment Type: reg
Provision Reference: reg 5 (pt 2/2)
Character Range: 26420–27445

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:
(a) is capable of the navigation specification; or
(b) has the GPS capability mentioned in an item in the Table that corresponds to the navigation specification.

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