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

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Chapter 3<br />

TURN AREA CONSTRUCTION<br />

3.1 GENERAL<br />

3.1.1 This chapter describes the general criteria for the construction <strong>of</strong> turn areas for use in the different segments<br />

<strong>of</strong> instrument flight procedures. The methodologies presented — wind spiral <strong>and</strong> bounding circle — apply to the phases<br />

<strong>of</strong> flight shown below. All other turns are constructed by means <strong>of</strong> arcs (see the appropriate chapters).<br />

a) Departure.<br />

b) Missed approach.<br />

c) Final approach fix (turns > 10 degrees).<br />

d) RNAV turns at the IAF <strong>and</strong> IF (turns > 30 degrees).<br />

3.1.2 Turn parameters<br />

3.1.2.1 This section shows the parameters on which the turn areas are based, together with the variables which<br />

represent them in the drawings. The values for the following parameters vary according to the phase <strong>of</strong> flight. Their<br />

values are listed in Table I-2-3-1, “Turn construction parameter summary”. For the specific application <strong>of</strong> the<br />

parameters in the table, see the applicable chapters. Tables I-2-3-2 <strong>and</strong> I-2-3-3 show example calculations <strong>of</strong> various<br />

turning parameters for a selection <strong>of</strong> IAS.<br />

a) Altitude.<br />

b) Indicated airspeed (IAS).<br />

c) Wind.<br />

d) Bank angle.<br />

e) Flight technical tolerances.<br />

3.1.2.2 Other turn factors <strong>and</strong> calculations used in turn construction<br />

a) Fix tolerance. As appropriate for the type <strong>of</strong> fix. See Section 2, Chapter 2, “Terminal area fixes”. See also<br />

Part <strong>II</strong>, Section 3, “En-route criteria”.<br />

b) Rate <strong>of</strong> turn (R) in degrees/second. This is calculated as follows:<br />

1) R = (6 355 tan α)/π V, where V is the TAS in km/h; <strong>and</strong><br />

I-2-3-1 23/11/06

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