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

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

23/11/06<br />

2) R = (3 431 tan α)/πV, where V is the TAS in kt;<br />

up to a maximum value <strong>of</strong> 3 degrees/second.<br />

c) Radius <strong>of</strong> turn (r) at a designated angle <strong>of</strong> bank in still air, in km or NM as appropriate. The turn radius for a<br />

given value <strong>of</strong> R is derived as follows:<br />

r=V/(20π R) where V is the TAS.<br />

d) Wind effect (Eθ) for the time taken to change heading θ degrees, in km or NM as appropriate.<br />

e) Gravity. The value used implicitly in the formulae is 9.80665 m/s 2 (68 625 NM/hour 2 ).<br />

f) c = 6 seconds pilot reaction time.<br />

3.2 TURN INNER BOUNDARY CONSTRUCTION<br />

3.2.1 Turn at an altitude/height<br />

The inner boundary normally originates at the beginning <strong>of</strong> the turn initiation area from whichever edge <strong>of</strong> the area<br />

provides the best lateral protection (inner edge if turn < 75°, outer edge if turn ≥ 75°). It then diverges outwards in the<br />

direction <strong>of</strong> the nominal track with a splay <strong>of</strong> 15 degrees (see Figures I-2-3-1 a) <strong>and</strong> b)).<br />

3.2.2 Turns at a designated turning point<br />

On the inner edge <strong>of</strong> the turn, the primary area boundary starts at the K-line. The edges <strong>of</strong> the primary <strong>and</strong> secondary<br />

areas are connected to their counterparts in the subsequent sections. For these connections, the following rules apply:<br />

a) if the point to connect is outside the protection area associated with the subsequent section, then the boundary<br />

converges with the nominal track after the turn at an angle equal to half the angle <strong>of</strong> turn (A/2); <strong>and</strong><br />

b) if the point to connect is inside the protection area associated with the subsequent section, then the boundary<br />

diverges from the nominal track at an angle <strong>of</strong> 15 degrees.<br />

3.3.1 <strong>Construction</strong> is as follows:<br />

3.3 TURN OUTER BOUNDARY CONSTRUCTION<br />

a) Point A (see Figure I-2-3-2) is where the curve begins. The parameters that determine its location are:<br />

1) fix tolerance; <strong>and</strong><br />

2) flight technical tolerance;<br />

b) from this point there are two methods for constructing the curving portion <strong>of</strong> the turn outer boundary:

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