Document ID: chunk:federal_register_of_legislation:F2020C00605:body:0:p4
Version: federal_register_of_legislation:F2020C00605
Segment Type: other
Provision Reference: 
Character Range: 8029–11078

degrading the accuracy of the computed GPS position of a GNSS-equipped aircraft.
SDA means System Design Assurance as specified in section 2.2.3.2.7.2.4.6 of RTCA/DO‑260B.
SIL means Source Integrity Level as specified in paragraph 2.2.3.2.7.1.3.10 of RTCA/DO‑260B.
SSR means a secondary surveillance radar system that is used by ATC to detect an aircraft equipped with a radar transponder.
TABS means traffic awareness beacon system.
TSO means Technical Standard Order of the FAA.
Note   NAA is defined in regulation 1.4 of the Civil Aviation Safety Regulations 1998.
UK CAP 1391 means Civil Aviation Authority of the United Kingdom document number CAP 1391 titled Electronic conspicuity devices, 2nd edition, dated April 2018, or a later edition as in force from time to time.
VFR has the same meaning as V.F.R. and stands for visual flight rules.
       3Subject to clause 12, if an aircraft carries ADS‑B transmitting equipment for operational use in Australian territory:
       (a)              the equipment must comply with an approved equipment configuration under Schedule 2, 3, 4 or 5 in accordance with the Application provisions of the Schedule; and
       (b)              for Schedule 5, any administrative standard included in the schedule must be complied with.
       4When serviceable ADS‑B transmitting equipment is operated in Australian territory, the equipment must transmit:
       (a)              the current aircraft address; and
       (b) a flight identification that:
           (i) corresponds exactly to the aircraft identification mentioned on the flight notification filed with ATC for the flight; or
           (ii) if a flight notification is not filed for the flight — is the aircraft's registration mark; or
           (iii) is directed or approved by ATC.
       5If an aircraft in flight carries serviceable ADS‑B transmitting equipment, the equipment must be operated:
       (a)              for equipment that complies with an approved equipment configuration set out in Schedule 2 — continuously during the flight in all airspace and at all altitudes, unless the pilot is directed or approved otherwise by ATC; and
       (b)              for equipment that complies with the approved equipment configuration set out in Schedule 3, 4 or 5 — continuously during the flight, within the airspace and within the altitude limits specified for the flight in the applicable Schedule, unless the pilot is directed or approved otherwise by ATC.
       6Subject to clause 7, if an aircraft carries ADS‑B transmitting equipment which does not comply with an approved equipment configuration, the aircraft must not fly in Australian territory unless the equipment is:
       (a)              deactivated; or
       (b)              set to transmit only a value of zero for the NUCp, NACp, NIC or SIL.
Note   It is considered equivalent to deactivation if NUCp, NACp, NIC or SIL is set to continually transmit only a value of zero.
       7The ADS‑B transmitting equipment need not be deactivated for paragraph 6 if the