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

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Part <strong>II</strong> — Section 4, Chapter 1, Appendix A <strong>II</strong>-4-1-App A-3<br />

where: α = angle<strong>of</strong>bankindegrees;<br />

or<br />

V = true airspeed in metres per second; <strong>and</strong><br />

R = rate <strong>of</strong> turn in degrees per second.<br />

where: α = angle<strong>of</strong>bankindegrees;<br />

tan <br />

R= 0.055V<br />

V = true airspeed in nautical miles per minute; <strong>and</strong><br />

R = rate <strong>of</strong> turn in degrees per second.<br />

where: V = true airspeed in metres per second;<br />

or<br />

R = rate <strong>of</strong> turn; <strong>and</strong><br />

r = radius <strong>of</strong> turn in kilometres<br />

6.3 Radius <strong>of</strong> turn (r)<br />

0.18V<br />

r=<br />

π R<br />

3V<br />

r=<br />

π R<br />

where: V = true airspeed in nautical miles per minute;<br />

R = rate <strong>of</strong> turn; <strong>and</strong><br />

r = radius <strong>of</strong> turn in nautical miles.<br />

6.4 Cone effect area radius calculation formula<br />

z=hltanγl<br />

where: hl = height above the facility in thous<strong>and</strong>s <strong>of</strong> metres;<br />

or<br />

γl = 1/2 cone angle in degrees; <strong>and</strong><br />

z = radius <strong>of</strong> the cone effect area in kilometres<br />

z = 0.164 h1 tan γ1<br />

23/11/06

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