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

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Part <strong>II</strong> — Section 1, Chapter 3 <strong>II</strong>-1-3-7<br />

Note.— Guidance material for determining the distance to the descent fix from the threshold is contained in<br />

Chapter 1, Appendix C.<br />

3.4.3.2 Obstacle clearance at the descent fix. When a descent fix is provided , the precision approach surfaces<br />

start at the earliest point <strong>of</strong> the FAF tolerance area (see Figure <strong>II</strong>-1-3-3). The provisions <strong>of</strong> Part I, Section 2, Chapter 2,<br />

2.7.4, “Obstacle close to a final approach fix or stepdown fix” which allow obstacles close to the fix to be ignored,<br />

apply in the area below the 15 per cent gradient within the precision surfaces (Cat H, 15 per cent gradient or the<br />

nominal gradient multiplied by 2.5, whichever is greater). Where a descent fix is not provided at the FAP, no<br />

curtailment <strong>of</strong> the precision surfaces is permitted (see Figure <strong>II</strong>-1-3-4). If the precision surfaces are extended into the<br />

preceding segment, they shall not be extended beyond the intermediate approach segment.<br />

3.4.4 Glide path verification check<br />

A DME fix is necessary so as to permit comparison between the indicated glide path (elevation angle) <strong>and</strong> the aircraft<br />

altimeter information. The fix shall not have a fix tolerance exceeding ± 0.9 km (± 0.5 NM). The range shall be stated<br />

in tenths <strong>of</strong> kilometres (nautical miles).<br />

Note.— Guidance material for determining the height crossing the DME fix is contained in Chapter 1, Appendix C.<br />

3.4.5 Missed approach<br />

The missed approach point is defined by the intersection <strong>of</strong> the nominal glide path <strong>and</strong> the decision altitude/height<br />

(DA/H). The DA/H is set at or above the OCA/H, which is determined as specified in 3.4.7 to 3.4.9 <strong>and</strong> 3.5.<br />

3.4.6 Termination<br />

The precision segment normally terminates at the point where the final phase <strong>of</strong> the missed approach commences (see<br />

Part I, Section 4, Chapter 6, 6.1.2, “Phases <strong>of</strong> missed approach segment”) or where the missed approach climb surface<br />

Z (starting 900 m past threshold) reaches a height <strong>of</strong> 300 m (984 ft) above threshold, whichever is lower.<br />

3.4.7 Obstacle clearance in the precision segment application <strong>of</strong> basic ILS surfaces<br />

3.4.7.1 General. The area required for the precision segment is bounded overall by the basic ILS surfaces defined<br />

in 3.4.7.2, below. In st<strong>and</strong>ard conditions there is no restriction on objects beneath these surfaces (see 3.1.3, “St<strong>and</strong>ard<br />

conditions”). Objects or portions <strong>of</strong> objects that extend above these surfaces must be either:<br />

a) minimum mass <strong>and</strong> frangible; or<br />

b) taken into account in the calculation <strong>of</strong> the OCA/H.<br />

3.4.7.2 Definition <strong>of</strong> basic ILS surfaces. The surfaces to be considered correspond to a subset <strong>of</strong> Annex 14<br />

obstacle limitation surfaces as specified for precision approach runway code numbers 3 or 4 (see Figure <strong>II</strong>-1-3-7).<br />

These are:<br />

a) the approach surface, continuing to the final approach point (FAP) (first section 2 per cent gradient, second<br />

section 2.5 per cent as described in Annex 14);<br />

b) the runway strip assumed to be horizontal at the elevation <strong>of</strong> the threshold;<br />

23/11/06

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