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.

I-4-3-App A-4 Procedures — <strong>Aircraft</strong> <strong>Operations</strong> — <strong>Volume</strong> <strong>II</strong><br />

b) start point <strong>of</strong> the turn defined by VOR/DME indication: 7 km (4 NM).<br />

These values are adequate provided that the length <strong>of</strong> the first leg does not exceed 19 km (10 NM); otherwise, they<br />

should be increased by 15 per cent <strong>of</strong> the distance in excess <strong>of</strong> 19 km (10 NM). Example: Start point <strong>of</strong> the turn<br />

defined by VOR intersection; for a 37 km (20 NM) first leg, the length <strong>of</strong> the DR segment shall not be less than<br />

10.5 km or 6.5 NM.<br />

23/11/06<br />

3.3 Characteristics <strong>of</strong> the U-type procedures<br />

3.3.1 Position <strong>of</strong> the initial approach fix (IAF). The IAF can be a facility (VOR or VOR/DME) or a fix from<br />

which track guidance is available. This fix or facility shall be located outside a sector contained between the final<br />

approach path <strong>and</strong> a straight line L (see Figure I-4-3-App A-1). Line L is determined as follows:<br />

a) from the FAP draw line D at an angle to the final approach path.<br />

The length <strong>of</strong> D varies with the type <strong>of</strong> facility. Lengths for each type appear in Table I-4-3-App A-3; <strong>and</strong><br />

b) at the end point <strong>of</strong> line D, draw line L perpendicular to line D.<br />

3.3.1.1 Values for were determined as follows:<br />

a) take the angle (45°) between the dead reckoning segment <strong>and</strong> the ILS axis;<br />

b) add the maximum angle between the first leg <strong>of</strong> the initial segment <strong>and</strong> the dead reckoning segment:<br />

1) 45° + 120° = 165° for VOR/DME; <strong>and</strong><br />

2) 45° + 105° = 150° for VOR/VOR;<br />

c) take the total from steps 1 <strong>and</strong> 2, <strong>and</strong> subtract this from 180. This gives the maximum angle between the first<br />

leg <strong>of</strong> the initial segment <strong>and</strong> the reverse <strong>of</strong> ILS axis:<br />

1) 180° – 165° = 15° for VOR/DME; <strong>and</strong><br />

2) 180° – 150° = 30° for VOR/VOR;<br />

d) subtract the value obtained in c) from 90° in order to have the direction <strong>of</strong> the perpendicular:<br />

1) 90° – 15° = 75° for VOR/DME; <strong>and</strong><br />

2) 90° – 30° = 60° for VOR/VOR; <strong>and</strong><br />

e) subtract a buffer value <strong>of</strong> 5° for technical tolerance to give the following values:<br />

1) 70° for VOR/DME; <strong>and</strong><br />

2) 55° for VOR/VOR.

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

Saved successfully!

Ooh no, something went wrong!