Publication: Magyar Közlöny
Issue: MK-2007-70 (Year: 2007, Number: 70)
Era: 2004-2010
Section: Melléklet a 2007. évi XLVI. törvényhez
Paragraph Index: 3297

c) way-point data words shall define the location and sequence of way-points for the procedures. Note The structure and coding of auxiliary words through are defined in Appendix A Tables A through A uidance material concerning the coding of M S RNA procedures is given in Attachment 2007/70/II. szám C a ter Annex 10 — Aeronautical Communications 23/11/06 3.11.4.9 System accuracy The accuracy standards specified herein shall be met on a 95 per cent probability basis unless otherwise stated. Note The overall error limits include errors from all causes such as those from airborne e uipment ground e uipment and propagation effects Note It is intended that the error limits are to be applied over a flight path interval that includes the approach reference datum or bac a imuth reference datum Information on the interpretation of M S errors and the measurement of these errors over an interval appropriate for flight inspection is provided in Attachment Note To determine the allowable errors for degradation allowances at points other than the appropriate reference datum the accuracy specified at the reference datum should first be converted from its linear value into its e uivalent angular value with an origin at the antenna 3.11.4.9.1 M S approach reference datum The height of the MLS approach reference datum shall be 15 m (50 ft). A tolerance of plus 3 m (10 ft) shall be permitted. Note The operational objective of defining the height of the M S approach reference datum is to ensure safe guidance over obstructions and also safe and efficient use of the runway served The heights noted in assume Code or Code runways as defined by Annex Note At the same time the reference datum is to provide a convenient point at which the accuracy and other parameters of the function may be specified Note In arriving at the above height values for the M S approach reference datum a maximum vertical distance of m ( ft) between the path of the aircraft M S antenna selected for final approach and the path of the lowest part of the wheels at the threshold was assumed For aircraft exceeding this criterion appropriate steps may have to be ta en either to maintain ade uate clearance at threshold or to adjust the permitted operating minima 3.11.4.9.2 M S bac a imuth reference datum The height of the MLS back azimuth reference datum shall be 15 m (50 ft). A tolerance of plus 3 m (10 ft) shall be permitted. Note The objective of defining the M S bac a imuth reference datum is to provide a convenient point at which the accuracy and other parameters of the function may be specified 3.11.4.9.3 The PFE shall be comprised of those frequency components of the guidance signal error at the output of the airborne receiver which lie below 0.5 rad/s for azimuth guidance information or below 1.5 rad/s for elevation guidance information. The control motion noise shall be comprised of those frequency components of the guidance signal error at the output of the airborne receiver which lie above 0.3 rad/s for azimuth guidance or above 0.5 rad/s for elevation guidance information. The output filter corner frequency of the receiver used for this measurement is 10 rad/s. 3.11.4.9.4 Approach a imuth guidance functions At the approach reference datum, the approach azimuth function shall provide performance as follows:

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