21.03.2013 Views

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

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

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

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

Part <strong>II</strong> — Section 3, Chapter 1 <strong>II</strong>-3-1-5<br />

b) Outer edge <strong>of</strong> the turn. The outer edge <strong>of</strong> the turn area is composed <strong>of</strong>:<br />

1) a straight extension <strong>of</strong> the outer edge <strong>of</strong> the segment before the turn;<br />

2) the arc <strong>of</strong> a circle having a radius <strong>of</strong> T, which is centred on the turning point (nominal fix or facility); <strong>and</strong><br />

3) the tangent <strong>of</strong> the arc <strong>of</strong> this circle which makes an angle <strong>of</strong> 30° with the following segment.<br />

The value <strong>of</strong> T is described by the following equation:<br />

where: r = radius <strong>of</strong> turn<br />

T=SA+2*r+E165°<br />

E165° = wind effect to account for 120° course change plus 30° convergence angle plus 15° drift<br />

SA = area semi-width<br />

This method is based on the assumption that the size <strong>of</strong> the tolerance associated with the turn point is included<br />

in the area corresponding to a straight segment.<br />

Note 1.— Use the highest minimum altitude <strong>of</strong> all the segments intersecting at the turning point.<br />

Note 2.— Maximum turn angle is 120°.<br />

Note 3.— A constant wind effect (E165°) needs to be applied for all turn angles.<br />

Example calculation for an altitude <strong>of</strong> 4 500 m. Given the turn parameters as stated in 1.4.3.3, “Turn<br />

parameters” <strong>and</strong> area semi-width <strong>of</strong> 18.5 km, it follows that:<br />

the radius <strong>of</strong> turn (r) = 16.77<br />

wind effect (E165°) = 9.00<br />

T = 18.5 + 33.54 + 9.00 = 61.04 km<br />

c) Inner edge <strong>of</strong> the turn. From point K <strong>of</strong> the turn, draw a line making an angle <strong>of</strong> α/2 with the nominal track in<br />

segment 2 (the segment following the turn). This line ends where it intersects the edge <strong>of</strong> segment 2.<br />

d) End <strong>of</strong> turn area. The arc as described under (2) also denotes the end <strong>of</strong> the turn area.<br />

1.4.3.5 Bidirectional routes. The method <strong>of</strong> construction <strong>of</strong> the turn area assumes a direction <strong>of</strong> flight. When the<br />

route is to be flown in both directions, it is necessary to construct both turn areas to account for both directions <strong>of</strong> flight<br />

<strong>and</strong> to apply the minimum obstacle clearance over the whole combined turn area (see Figure <strong>II</strong>-3-1-6).<br />

1.5 MINIMUM ALTITUDES FOR SIGNAL RECEPTION<br />

The minimum altitude en route based on VOR or NDB navigation, providing a minimum obstacle clearance, shall<br />

allow a proper reception <strong>of</strong> the relevant facilities. The following formula can be used for planning purposes.<br />

23/11/06

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!