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<strong>II</strong>-1-1-6 Procedures — <strong>Aircraft</strong> <strong>Operations</strong> — <strong>Volume</strong> <strong>II</strong><br />

23/11/06<br />

1.4 PRECISION SEGMENT<br />

1.4.1 General<br />

The precision segment is aligned with the localizer course <strong>and</strong> contains the final descent for l<strong>and</strong>ing as well as the<br />

initial <strong>and</strong> intermediate phases <strong>of</strong> the missed approach segment See Figure <strong>II</strong>-1-1-5.<br />

1.4.2 Origin<br />

The precision segment starts at the final approach point (FAP), that is, the intersection <strong>of</strong> the nominal glide path <strong>and</strong> the<br />

minimum altitude specified for the preceding segment. The FAP should not normally be located more than 18.5 km<br />

(10.0 NM) before threshold, unless adequate glide path guidance beyond the minimum specified in Annex 10 is<br />

provided.<br />

1.4.3 Descent fix<br />

1.4.3.1 A descent fix may be located at the FAP to overcome certain obstacles located before the FAP as an<br />

alternative to increasing the glide path (GP) angle. When so located, it becomes the final approach fix. The extension <strong>of</strong><br />

the precision surfaces into the precision segment is then terminated. The descent fix should not normally be located<br />

more than 18.5 km (10.0 NM) before threshold, unless adequate GP guidance beyond the minimum specified in Annex<br />

10 is provided. The maximum fix tolerance is ± 0.9 km (± 0.5 NM). Where DME is used to identify the fix, the range<br />

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

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

Appendix C.<br />

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

at the earliest point <strong>of</strong> the FAF tolerance area (see Figure <strong>II</strong>-1-1-2). The provisions <strong>of</strong> Part I, Section 2, Chapter 2, 2.7.4,<br />

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

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

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

precision surfaces is permitted (see Figure <strong>II</strong>-1-1-3). If the precision surfaces are extended into the preceding segment,<br />

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

1.4.4 Glide path verification check<br />

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

altimeter information. The fix shall not have a fix tolerance exceeding ± 0.9 km (± 0.5 NM). When DME is used to<br />

identify the fix, the range shall be stated in tenths <strong>of</strong> kilometres (nautical miles).<br />

Note.— Guidance material for determining the height crossing the outer marker is contained in Appendix C.<br />

1.4.5 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 1.4.7 to 1.4.9 <strong>and</strong> 1.5.

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