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

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Part <strong>II</strong> — Section 1, Chapter 1, Appendix A <strong>II</strong>-1-1-App A-3<br />

MOC is the margin applicable to turns (in metres) <strong>and</strong><br />

d (in metres) = distance (threshold to TP) + do<br />

In the case <strong>of</strong> a turn at an altitude:<br />

do is the shortest distance from obstacle to the turn initiation area boundary <strong>and</strong><br />

d = distance (threshold to earliest TP) + do<br />

Inthecase<strong>of</strong>turnatadesignatedTP:<br />

do is the shortest distance from the obstacle to the earliest TP (line K-K).<br />

3.2 Calculation <strong>of</strong> OCH from an amount <strong>of</strong><br />

altitude missing above an obstacle<br />

This method is applicable whenever it has been established that one obstacle is a problem. This means that the nominal<br />

altitude above the obstacle will not be adequate for an airplane climbing at the SOC from the previously calculated<br />

OCH. If we express the difference in altitude as dif (alt), the necessary increase <strong>of</strong> OCH (dif (OCH)) will be obtained<br />

by the formula:<br />

dif (OCH) =<br />

dif (alt) cot Z<br />

cot Z + cot θ<br />

This method may also be applied for turns at altitude, when an obstacle in the turn initiation area is higher than (turn<br />

altitude – MOC). Then the necessary increase <strong>of</strong> OCH (see 2.1.3, “Obstacle in the turn initiation area”, item b)) will be<br />

obtained by the formula above where:<br />

dif (alt) = obstacle elevation + MOC – previous turn altitude.<br />

4. TECHNIQUE FOR REDUCTION OF THE TURN AREA FOR A TURN AT<br />

AN ALTITUDE FROM INSIDE THE PRECISION SEGMENT<br />

4.1 Turn initiation area<br />

The turn initiation area can be more precisely defined by plotting an area which consists <strong>of</strong> two parts. The first part is<br />

the area enclosed by the turn altitude OAS contour truncated at the turn point as described in Chapter 1, 1.5.3.2.1. The<br />

second part <strong>of</strong> the area is bounded by:<br />

a) the 300 m OAS contour truncated by the line joining the D” points; <strong>and</strong><br />

b) two lines DTL defined as follows:<br />

DT = (HL – RDH) cot θ + 900 m SI units<br />

where DT is the distance from a missed approach point on GP to the corresponding SOC on GP'.<br />

23/11/06

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