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

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I-4-3-8 Procedures — <strong>Aircraft</strong> <strong>Operations</strong> — <strong>Volume</strong> <strong>II</strong><br />

23/11/06<br />

2) for base <strong>and</strong> procedure turns, however, the area for 165 km/h (90 kt) should be checked. An additional<br />

template for these procedures is incorporated in the Template Manual for Holding, Reversal <strong>and</strong> Racetrack<br />

Procedures (Doc 9371).<br />

3.6.4.1 Statistical area construction<br />

3.6.4 Area construction<br />

If statistical methods are used to combine the variables <strong>and</strong> then to extrapolate distributions to develop areas, the<br />

probability level associated with that extrapolation should meet an acceptable level <strong>of</strong> safety.<br />

3.6.4.2 Additive tolerance area construction<br />

A variety <strong>of</strong> methods may be used to construct areas. Whichever method is selected, the procedure design criteria<br />

specified in 3.5, “Initial approach segment using a reversal procedure”, <strong>and</strong> the area parameters specified in 3.6.2,<br />

“Area parameters”, apply. One additive tolerance method, the template tracing technique (TTT), is described in<br />

Appendix C.<br />

Note.— For applications where airspace is not critical, a method <strong>of</strong> constructing a simplified rectangular area<br />

(based on the TTT areas) is also contained in Appendix C.<br />

3.6.5 Area reduction<br />

The area may be reduced under special circumstances. Methods <strong>of</strong> reduction include:<br />

a) reduction <strong>of</strong> the maximum speed(s) specified for the procedure. Speeds below the minimum value for initial<br />

approach in a given aircraft category shall not be specified (see Tables I-4-1-1 <strong>and</strong> I-4-1-2 <strong>of</strong> Section 4,<br />

Chapter 1). If procedures are developed which exclude specific aircraft categories due to speed, this must be<br />

stated explicitly;<br />

b) restricting use <strong>of</strong> the procedure to specified categories <strong>of</strong> aircraft;<br />

c) restricting procedure entry to specific track(s); <strong>and</strong><br />

d) use <strong>of</strong> DME or radial/bearing to limit outbound track (see 3.6.6, “Use <strong>of</strong> DME or intersecting radial/bearing”).<br />

3.6.6 Use <strong>of</strong> DME or intersecting radial/bearing<br />

If a DME distance or an intersecting radial or bearing is used to limit the outbound leg, the area may be reduced by<br />

applying the appropriate adjustments described in Appendix C, in this case the limiting distance or radial/bearing shall<br />

allow adequate time for the descent specified. The distance on the outbound track is thereby limited by the timing or by<br />

reaching the limiting DME distance or radial/bearing, whichever occurs first.<br />

3.6.7 Secondary areas<br />

Secondary areas shall be added to the outer boundary <strong>of</strong> all areas calculated using the criteria in 3.6.4, “Area<br />

construction”. The width <strong>of</strong> the secondary area is 4.6 km (2.5 NM).

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