CS ACNS.D.ADSB.100 Integrity
ED Decision 2013/031/R
(a) The ADS-B Out system integrity is designed commensurate with a ‘major’ failure condition for the transmission of the following parameters:
(1) ICAO 24-bit aircraft address;
(2) Airborne Horizontal Position — Latitude and Longitude;
(3) Airborne Navigation Integrity Category: NIC;
(4) Airborne/Surface Navigation Accuracy Category for Position: NACp;
(5) Airborne/Surface Source Integrity Level: SIL;
(6) Airborne/Surface System Design Assurance: SDA;
(7) 1090 ES Version Number;
(8) Airborne velocity over Ground — East/West and North/South;
(9) Airborne/Surface Navigation Accuracy Category for Velocity: NACv;
(10) Emitter Category;
(11) Surface Horizontal Position — Latitude and Longitude;
(12) Surface Navigation Integrity Category: NIC;
(13) Surface Ground Track;
(14) Movement (surface ground speed);
(15) Length/width of Aircraft;
(16) GPS Antenna Offset;
(17) Geometric Altitude;
(18) Geometric Altitude Quality: GVA;
(b) The ADS-B Out system integrity is designed commensurate with a ‘minor‘ failure condition for the transmission of other data parameters.
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