Document ID: chunk:federal_register_of_legislation:F2024C01173:reg:3:p3
Version: federal_register_of_legislation:F2024C01173
Segment Type: reg
Provision Reference: reg 3 (pt 3/4)
Character Range: 318905–321859

other than subparagraph (1)(b)(iii) which is optional.
Note: The following GNSS receivers meet the requirements of this section, namely, those certified to (E)TSO-C145a or (E)TSO-C146a, or later versions; or those manufactured to comply with (E)TSO-C196a. Some later versions of GNSS receivers certified to (E)TSO-C129 may also meet the requirements, i.e. those having FDE and HPL features incorporated.

11.70  Alternate ADS-B OUT equipment configuration—requirements
 (1) An alternate ADS-B OUT equipment configuration is acceptable if:
 (a) it has been certified by CASA or the national aviation authority of a recognised country, during type certification, as meeting the standards of EASA AMC 20-24 or EASA CS‑ACNS; and
 (b) the aircraft flight manual or flight manual supplement attests to the certification; and
 (c) the GNSS system meets the performance requirements mentioned in subsection 11.69(1).
 (2) An alternate ADS-B OUT equipment configuration is acceptable if:
 (a) it has been certified by EASA, during type certification, as meeting the standards of EASA AMC 20-24; and
 (b) the aircraft flight manual attests to the certification; and
 (c) the GNSS system meets the performance requirements mentioned in subsection 11.69(1).
 (3) For an aeroplane first certificated in its country of manufacture on or after 8 December 2016, an equipment configuration is acceptable if:
 (a) it has been certified by the FAA, during type certification, as meeting the standards of 14 CFR 91.227; and
 (b) the aircraft flight manual attests to the certification; and
 (c) the GNSS system meets the performance requirements mentioned in subsection 11.69(1).
 (4) For an aeroplane first certificated in its country of manufacture before 8 December 2016, an equipment configuration is acceptable if:
 (a) it has been certified by the FAA, during type certification, as meeting the standards of 14 CFR 91.227; and
 (b) the aircraft flight manual attests to the certification; and
 (c) the GNSS system meets the performance requirements mentioned in subsection 11.69(2).

11.71  Aeroplane flown with no operative surveillance equipment
  Where this Chapter requires surveillance equipment to be fitted to an aeroplane, the equipment may be inoperative at the beginning of a flight if the flight:
 (a) begins from an aerodrome at which there is no facility for the surveillance equipment to be repaired or replaced; and
 (b) ends not more than 72 hours after the time the surveillance equipment was found to be inoperative.
Note: See also section 11.06 for additional requirements related to a flight with inoperative equipment. For a flight with no operative surveillance equipment, within controlled airspace or at a controlled aerodrome, Division 11.2 of the Part 91 Manual of Standards has requirements related to air traffic control clearances. Whether a clearance is issued, or when a clearance may be issued, could be affected by the flight not being