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Aircraft Operations. Volume II - Construction of Visual and Instrument ...

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Chapter 4<br />

OFFSET MLS<br />

4.1 USE OF MLS CAT I WITH OFFSET AZIMUTH ALIGNMENT<br />

4.1.1 In certain cases it may not be physically practicable to align the azimuth with the runway centre line because<br />

<strong>of</strong> siting problems, or because airfield construction work dem<strong>and</strong>s a temporary <strong>of</strong>fset location. An <strong>of</strong>fset azimuth shall<br />

not be established as a noise abatement measure.<br />

4.1.2 The zero-degree azimuth shall intersect the runway extended centre line:<br />

a) at an angle not exceeding 5°; <strong>and</strong><br />

b) at a point where the nominal glide path (elevation angle) reaches a height <strong>of</strong> at least 55 m (180 ft) above<br />

threshold. This is called intercept height.<br />

4.1.3 The procedure shall be annotated: “azimuth <strong>of</strong>fset ... degrees” (tenth <strong>of</strong> degrees). The general arrangement is<br />

shown in Figure <strong>II</strong>-1-4-1.<br />

The provisions contained in Chapter 3 apply except that:<br />

4.2 OBSTACLE CLEARANCE CRITERIA<br />

a) all the obstacle clearance surfaces <strong>and</strong> calculations are based on a fictitious runway aligned with the azimuth<br />

specified for the final approach track. This fictitious runway has the same length, the same threshold elevation,<br />

<strong>and</strong> the same distance threshold to intercept point as the real one. The azimuth sector width <strong>and</strong> the MLS<br />

approach reference datum height are based on the threshold <strong>of</strong> the fictitious runway; <strong>and</strong><br />

b) the OCA/H for this procedure shall be at least: intercept altitude/height + 20 m (66 ft).<br />

<strong>II</strong>-1-4-1 23/11/06

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