CS ACNS.D.ADSB.100 Integrity

• ED Decision 2013/031/R found in: GM Remote Aerodrome Air Traffic Services (ED 2019/004/R) Issue 2 (Jul 2020)

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.