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

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I-4-3-2 Procedures — <strong>Aircraft</strong> <strong>Operations</strong> — <strong>Volume</strong> <strong>II</strong><br />

23/11/06<br />

3.3 INITIAL APPROACH SEGMENTS (OTHER THAN RADAR VECTORS)<br />

UTILIZING STRAIGHT TRACKS AND DME ARCS<br />

3.3.1 Tracks<br />

The angle <strong>of</strong> intersection between the initial approach track <strong>and</strong> the intermediate track should not exceed 120°. When<br />

the angle exceeds 70°, a radial, bearing, radar vector or DME information providing at least 4 km (2 NM) <strong>of</strong> lead<br />

(Cat H, 1.9 km (1 NM)) shall be identified to assist in leading the turn onto the intermediate track (see Figure I-4-3-1).<br />

When the angle exceeds 120°, the use <strong>of</strong> a racetrack or reversal procedure or dead reckoning (DR) track should be<br />

considered. Criteria for such procedures are in 3.4, “Initial approach segment using a racetrack procedure”, 3.5, “Initial<br />

approach segment using a reversal procedure” <strong>and</strong> 3.3.3.3, “Area associated with dead reckoning (DR) track<br />

procedures”.<br />

3.3.2 DME arcs<br />

An arc may provide track guidance for all or for a portion <strong>of</strong> an initial approach. The minimum arc radius shall be<br />

13 km (7 NM) (Cat H, 9.3 km (5 NM)). An arc may join a track at or before the intermediate fix. When joining a track,<br />

the angle <strong>of</strong> intersection <strong>of</strong> the arc <strong>and</strong> the track should not exceed 120°. When the angle exceeds 70°, a radial which<br />

provides at least 4 km (2 NM) (Cat H, 1.9 km (1 NM)) <strong>of</strong> lead shall be identified to assist in leading the turn onto the<br />

intermediate track.<br />

3.3.3 Area<br />

3.3.3.1 The initial approach segment has no st<strong>and</strong>ard length. The length shall be sufficient to permit the altitude<br />

change required by the procedure. The width is divided into:<br />

a) a primary area which extends laterally 4.6 km (2.5 NM) on each side <strong>of</strong> the track; <strong>and</strong><br />

b) a secondary area which adds an additional 4.6 km (2.5 NM) on each side <strong>of</strong> the primary area.<br />

(See Figure I-4-3-2.)<br />

3.3.3.2 Area splay<br />

Where, because <strong>of</strong> an operational requirement, any portion <strong>of</strong> the initial approach is more than 69 km (37 NM) from the<br />

VOR or 52 km (28 NM) from the NDB providing track guidance, the area will start splaying at these distances at an<br />

angle <strong>of</strong> 7.8° for VOR or 10.3° for NDB. Within this splayed area, the width <strong>of</strong> the primary area shall remain one half<br />

<strong>of</strong> the total width <strong>of</strong> the area. (See Figure I-4-3-3.) For calculating secondary area width at a given point, see Section 2,<br />

Chapter 1, 1.2.1, “Calculating secondary area width at a given point”.<br />

Note.— See also Appendix B, “Reduction <strong>of</strong> the width <strong>of</strong> a straight initial approach area after the IAF <strong>and</strong> interface<br />

between straight initial approach area <strong>and</strong> reversal procedure areas” for possible reduction <strong>of</strong> the width <strong>of</strong> straight<br />

initial approach area.<br />

3.3.3.3 Area associated with dead reckoning (DR) track procedures<br />

Where DR track procedures are utilized, the area allocated for the turning portions <strong>of</strong> the dead reckoning segment shall<br />

be calculated to accommodate omnidirectional wind speed (w) derived by the following equation:

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