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

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I-4-7-2 Procedures — <strong>Aircraft</strong> <strong>Operations</strong> — <strong>Volume</strong> <strong>II</strong><br />

b) from the extremities <strong>of</strong> the adjacent arcs draw lines tangent to the arcs; <strong>and</strong><br />

c) connect the tangent lines.<br />

The area thus enclosed is the visual manoeuvring (circling) area. See Figures I-4-7-1 <strong>and</strong> I-4-7-2.<br />

7.2.1.2 Note that in Figure I-4-7-1, as an example, the radius for Category E aircraft is used. An operational<br />

advantage is gained by casting arcs only from those runways usable by Category E aircraft.<br />

7.2.1.3 In Figure I-4-7-2 all runways are used because they are available to Category A aircraft. However, since<br />

the radius for Category A is less than that for Category E the total area for all aircraft is slightly smaller than it would<br />

be if Category E criteria were applied completely.<br />

23/11/06<br />

7.2.2 Parameters<br />

The parameters on which visual manoeuvring (circling) radii are based are as follows:<br />

a) speed: speed for each category as shown in Tables I-4-1-1 <strong>and</strong> I-4-1-2 in Chapter 1;<br />

b) wind: ± 46 km/h (25 kt) throughout the turn; <strong>and</strong><br />

c) bank: 20° average achieved or the bank angle producing a turn rate <strong>of</strong> 3° per second, whichever is the lesser<br />

bank. (See Figures <strong>II</strong>-4-1-App A-2 <strong>and</strong> <strong>II</strong>-4-1-App A-3 in Part <strong>II</strong>, Section 4, Appendix A to Chapter 1,<br />

“Parameters for holding area construction”).<br />

7.2.3 Determination method<br />

The radius is determined using the formulas in Section 2, Chapter 3, “Turn area construction”, by applying a 46 km/h<br />

(25 kt) wind to the true airspeed (TAS) for each category <strong>of</strong> aircraft using the visual manoeuvring IAS from<br />

Tables I-4-1-1 <strong>and</strong> I-4-1-2 in Chapter 1. The TAS is based on:<br />

a) altitude: aerodrome elevation + 300 m (1 000 ft); <strong>and</strong><br />

b) temperature: ISA + 15°.<br />

7.2.4 Visibility <strong>and</strong> lowest OCA/H<br />

It is assumed that the minimum visibility available to the pilot at the lowest OCA/H will be as shown in Table I-4-7-3.<br />

This information is not required for the development <strong>of</strong> the procedure, but is included as a basis for the development <strong>of</strong><br />

operating minima.<br />

7.3 OBSTACLE CLEARANCE<br />

See 5.4.4, “OCA/H for visual manoeuvring (circling)”, <strong>and</strong> Table I-4-7-3.

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