Publication: Magyar Közlöny
Issue: MK-2007-70 (Year: 2007, Number: 70)
Era: 2004-2010
Section: Melléklet a 2007. évi XLVI. törvényhez
Paragraph Index: 3494

(1) when associated approach performance designator indicates APV-I (APD coded as 0) 0 to 50.8 m 0.2 m performance designator does not indicate APV-I (APD A 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I able ype predicted ranging source a ailability message Data content Bits used Range of values Resolution Modified -count 0 to 1 199.9 s 0.1 s Spare — — Number of impacted sources (N) 0 to 31 For N impacted sources Ranging source ID 1 to 255 this A 1 to 31 For NA impacted ranging sources for this approach Ranging source ID 1 to 255 Source availability sense — — Source availability duration 0 to 1 270 s 10 s Number of obstructed approaches (A) 0 to 255 For A obstructed approaches Reference path data selector 0 to 48 — Number of impacted sources for approach (N ) Source availability sense — — Source availability duration 0 to 1 270 s 10 s able AS S accuracy re uirement parameters Ground accuracy designator letter șn (degrees) a0 (metres) a1 (metres) ș0 (degrees) a2 (metres) A  5 0.5 1.65 14.3 0.08 B  5 0.16 1.07 15.5 0.08 C 0.15 0.84 15.5 0.04 5 to 35 0.24 — 0.04 able AS O ASS accuracy re uirement parameters designator letter șn (degrees) a0 (metres) a1 (metres) ș0 (degrees) a2 (metres) Ground accuracy A  5 1.58 5.18 14.3 0.078 B  5 0.3 2.12 15.5 0.078 C 0.3 1.68 15.5 0.042 5 to 35 0.48 — 0.042 3.6.7.1.1.2 The RMS of the ground subsystem contribution to the corrected pseudo-range accuracy for SBAS satellites all be: sh 23/11/06 A 2007/70/II. szám A endix Annex 10 — Aeronautical Communications pr _ gnd 1.8 RMS (metres) M d where M is as defined in 3.6.7.1.1.1. Note AD classifications for S AS ranging sources are under development 3.6.7.1.2.1.1 Category I precision approach and AP For a GBAS ground subsystem that provides the Category I rec h. of tellite signal monitoring re uired in and the integrity ris associated with the monitoring in Note AS signal in space integrity ris is defined as the probability that the ground subsystem provides information which when processed by a fault free receiver using any AS data that could be used by the aircraft results in an out of tolerance lateral or vertical relative position error without annunciation for a period longer than the maximum me to alert An out of tolerance lateral or vertical relative position error is defined as an error that exceeds the Category I 3.6.7.1.2.1.1.1 The GBAS ground subsystem maximum time-to-alert shall be less than or equal to 3 seconds when yp time to alert above is the time between the onset of the out of tolerance lateral or vertical relative position rror and the transmission of the last bit of the message that contains the integrity data that reflects the condition 3.6.7.1.2.1.1.3 For Category I precision approach, the value FASLAL for each FAS block, as defined in the FAS S block, s defined in the FAS vertical alert limit field of the Type 4 message, shall be no greater than 10 metres. 2.1.1.4 For APV, the value FASLAL and FASVAL shall be no greater than the lateral and vertical alert limits iven in Annex 10, Volume I, 3.7.2.4. . For GBAS ground subsystem that provides the GBAS positioning service, tegrity risk shall be less than 9.9 10 8 per hour. excluded and the effects of all other AS S AS and ore satellite constellations failures are included The AS ground subsystem integrity ris includes the integrity ris of tellite signal monitoring re uired in and the integrity ris associated with the monitoring in Note AS signal in space integrity ris is he ground subsystem provides infor hich when processed using any AS data that coul results in a nce hori ontal rela ut annunciation for a period long to ale defined as an error that exceeds both the hori ontal protection lev h 3.6.7.1.2 Integrity 3.6.7.1.2.1 AS ground subsystem integrity ris p ision approach or APV, the integrity risk shall be less than 1.5 10 7 per approac Note The integrity ris assigned to the AS ground subsystem is a subset of the AS signal in space integrity ris where the protection level integrity ris ( ) has been excluded and the effects of all other AS S AS and core satellite constellations failures are included The AS ground subsystem integrity ris includes the integrity ris sa ti precision approach or AP protection level and if additional data bloc is broadcast the ephemeris error position bound T e 1 messages are broadcast. Note The e 3.6.7.1.2.1.1.2 The GBAS ground subsystem maximum time-to-alert shall be less than or equal to 5.5 seconds when Type 101 messages are broadcast. lateral alert limit field of the Type 4 message shall be no greater than 40 metres, and the value FASVAL for each FA a 3.6.7.1. g 3.6.7.1.2.1.2 AS positioning service in Note The integrity ris assigned to the AS ground subsystem is a subset of the AS signal in space integrity s where the protection level integrity ris ( ) has been ri c sa defined as the probability that t mation w n out of tolera by a fault free receiver tive position error witho d be used by the aircraft er than the maximum time rt An out el and the of tolerance hori ontal relative position error is ori ontal ephemeris error position bound A 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I 3.6.7.1.2.1.2.1 The GBAS ground subsystem maximum time-to-alert shall be less than or equal to 3 seconds when Type 1 messages are broadcast and less than or equal to 5.5 seconds when Type 101 messages are br adcast. N T between the onset of the hori ontal relative position error and th ansm ge that contains the integri ndition 3.6.7.1 .2 P 3. 1.2.2.1 For a GBAS ground subsystem that provides the Cate ction el integrity risk shall be less than 5 10 8 per approach. d asurement conditions defined in data broadcast field strength is within the specified range and the protection levels are lower than the alert limits unless configuration changes occur due to the space segment 3.6.7.1.3.2 Continuity of service for positioning service Note For AS ground subsystems that provide the AS positioning service there may be additional continuity re uirements depending on the intended operations .6. em shall not broadcast both Type 1 and Type 101 messages. o ote he time to alert above is the time ssion of the last bit of the messa out of tolerance data that reflects the co e tr i ty .2 rotection level integrity ris 6.7. gory I precision approach or APV, the prote lev Note The Category I precision approach and AP protection level integrity ris is the integrity ris due to undetecte errors in position relative to the AS reference point greater than the associated protection levels under the two following conditions

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