Section 171.313 14 CFR Ch. I (1-1-19 Edition) the coverage requirement is reduced to 14 nm beyond Section40Section. (2) Vertically between: (i) A conical surface originating 2.5 meters (8 feet) above the runway centerline at threshold inclined at 0.9 degree above the horizontal. (ii) A conical surface originating at the azimuth ground equipment antenna inclined at 15 degrees above the horizontal to a height of 6,000 meters (20,000 feet). (iii) Where intervening obstacles penetrate the lower surface, coverage need be provided only to the minimum line of sight. (3) Runway region: (i) Proportional guidance horizontally within a sector 45 meters (150 feet) each side of the runway centerline beginning at the stop end and extending parallel with the runway centerline in the direction of the approach to join the approach region. This requirement does not apply to offset azimuth installations. (ii) Vertically between a horizontal surface which is 2.5 meters (8 feet) above the farthest point of runway centerline which is in line of sight of the azimuth antenna, and in a conical surface originating at the azimuth ground equipment antenna inclined at 20 degrees above the horizontal up to a height to 600 meters (2,000 feet). This requirement does not apply to offset azimuth installations. (4) Within the approach azimuth coverage sector defined in paragraphs (a) (1), and (2) and (3) of this section, the power densities must not be less than those shown in Table 9 but the equipment design must also allow for: (i) Transmitter power degradation from normal by Section1.5 dB; TABLE 9 - MINIMUM POWER DENSITY WITHIN COVERAGE BOUNDARIES(DBW/M 2) Data signals Function Angle signals for various antenna beamwidths 1Section Approach azimuth ....................................................................... High rate approach azimuth ........................................................ Back azimuth ............................................................................... Approach elevation ..................................................................... (ii) Rain loss of Section2.2 dB at the longitudinal coverage extremes. (b) Siting requirements. The approach azimuth antenna system must, except as allowed in paragraph (c) of this section: (1) Be located on the extension of the centerline of the runway beyond the stop end; (2) Be adjusted so that the zero degree azimuth plane will be a vertical plane which contains the centerline of the runway served; (3) Have the minimum height necessary to comply with the coverage requirements prescribed in paragraph (a) of this section; (4) Be located at a distance from the stop end of the runway that is consistent with safe obstruction clearance practices; (5) Not obscure any light of an approach lighting system; and Section89.5 Section89.5 Section89.5 Section89.5 Section88 Section88 Section88 Section88 1.5Section .......... .......... .......... Section88 2Section Section85.5 Section88 Section85.5 Section88 Section82 Section86.5 Section82 .............. 08:20 May 17, 2019 Jkt 247048 PO 00000 Frm 00878 Fmt 8010 Section88 Section88 Section88 .................... (6) Be installed on frangible mounts or beyond the 300 meter (1,000 feet) light bar. (c) On runways where limited terrain prevents the azimuth antenna from being positioned on the runway centerline extended, and the cost of the land fill or a tall tower antenna support is prohibitive, the azimuth antenna may be offset. (d) Antenna coordinates. The scanning beams transmitted by the approach azimuth equipment within Section40Section of the centerline may be either conical or planar. (e) Approach azimuth accuracy. (1) The system and subsystem errors shall not exceed those listed in Table 10 at the approach reference datum. At the approach reference datum, temporal sinusoidal noise components shall not exceed 0.025 degree peak in the frequency band 0.01 Hz to 1.6 Hz, and the CMN shall not exceed 0.10 degree. From the approach reference 868 VerDate Sep<11>2014 Clearance signals 3Section Sfmt 8010 Y:\SGML\247048.XXX 247048