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

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Part I — Section 4, Chapter 3, Appendix C I-4-3-App C-5<br />

3.2.3.2 Influence <strong>of</strong> the flight technical tolerances<br />

a) On the nominal outbound turn, locate points “dl” <strong>and</strong> “d2” after 75 <strong>and</strong> 85 degrees <strong>of</strong> turn from “b”.<br />

b) From “dl” <strong>and</strong> “d2”, draw the tangents to the outbound turn <strong>and</strong> locate points “el” <strong>and</strong> “e2” on these tangents<br />

(Table <strong>II</strong>I-C-3, line 11).<br />

c) With a centre on “f2” at a distance r from “e2” on the perpendicular line to d2e2, draw the inbound turn at “e2”.<br />

Locate points “g”, “h”, “i” <strong>and</strong> “j” after 45, 90, 135 <strong>and</strong> 180 degrees <strong>of</strong> turn from “e2”.<br />

d) With a centre on “fl”, draw the inbound turn beginning at “el” <strong>and</strong> locate points “k”, “l” <strong>and</strong> “m” after 180, 225<br />

<strong>and</strong> 270 degrees <strong>of</strong> turn from “el”.<br />

3.2.3.3 Influence <strong>of</strong> the wind<br />

a) The wind effect is calculated for each point by multiplying the wind speed w by the flying time from the point<br />

“a”, beginning <strong>of</strong> the turn.<br />

b) Draw arcs with centres “e2”, “g”, “h”, “i”, “j”, “k”, “l” <strong>and</strong> “m” <strong>and</strong> radii We2, Wg, Wh, Wi, Wj, Wk <strong>and</strong> Wl<br />

(Table I-4-3-App C-3, lines 12 to 19).<br />

3.2.3.4 Drawing <strong>of</strong> the outline <strong>of</strong> the template. The outline <strong>of</strong> the template is composed <strong>of</strong>:<br />

a) the spiral envelope <strong>of</strong> the arcs centred on “e2”, “g”, “h”, “i” <strong>and</strong> “j”;<br />

b) the spiral envelope <strong>of</strong> the arcs centred on “k”, “l” <strong>and</strong> “m”;<br />

c) the common tangent to the spirals a) <strong>and</strong> b);<br />

d) the tangent passing through “a” to the spiral a); <strong>and</strong><br />

e) the tangent passing through “a” to the spiral b).<br />

3.2.4 Drawing <strong>of</strong> the protection area <strong>of</strong> the procedure turn<br />

3.2.4 (Reference Diagram I-4-3-App C-5)<br />

3.2.4.1 Tolerance area <strong>of</strong> the beginning <strong>of</strong> the outbound turn<br />

3.2.4.1.1 From the facility, point 0, draw the radial <strong>of</strong> the procedure <strong>and</strong> its two protection lines. These lines make<br />

an angle <strong>of</strong> 6.9° if the facility is NDB, 5.2° if the facility is a VOR, or 2.4° if the facility is a localizer, on each side <strong>of</strong><br />

the radial.<br />

3.2.4.1.2 Locate point A on the nominal beginning <strong>of</strong> the outbound turn.<br />

3.2.4.1.3 According to the type <strong>of</strong> facility at 0 <strong>and</strong> eventually at A or 0, draw the tolerance area <strong>of</strong> point A Al A2<br />

A3 A4 as described on the Figures I-4-3-App C-1 to I-4-3-App C-5.<br />

23/11/06

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