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

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

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

a) From “c” draw two lines at 5 degrees on each side <strong>of</strong> the nominal outbound leg.<br />

b) Locate points “d1”, “d2”, “d3” <strong>and</strong> “d4” on these lines (Table I-4-3 App C-2, lines 12 <strong>and</strong> 13).<br />

c) With a centre on “e2” at a distance r from “d2” on the perpendicular line to the nominal outbound leg (line<br />

passing through d2 <strong>and</strong> d4), <strong>and</strong> a radius r, draw the inbound turn beginning at “d2”. Locate points “f” <strong>and</strong> “g”<br />

after 50 <strong>and</strong> 100 degrees <strong>of</strong> turn from “d2”. With centres on “e3” <strong>and</strong> “e4”, draw the corresponding arcs<br />

beginning at “d3” <strong>and</strong> “d4”. Locate points “h”, “i” <strong>and</strong> “j” after 100, 150 <strong>and</strong> 200 degrees from “d4” <strong>and</strong> points<br />

“k” <strong>and</strong> “l” after 200 <strong>and</strong> 250 degrees <strong>of</strong> turn from “d3”.<br />

3.2.2.3 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 point “a”.<br />

b) Draw arcs with centres “c”, “d2”, “f”, “g”, “h”, “i”, “j”, “k” <strong>and</strong> “l” <strong>and</strong> radii Wc, Wd2, Wf, Wg, Wh, Wi, Wj, Wk<br />

<strong>and</strong> Wl (Table I-4-3 App C-2, lines 14 to 21).<br />

3.2.2.4 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 tangent passing through “a” to the arc centred on “c”;<br />

b) the common tangent to the arcs centred on “c” <strong>and</strong> “d2”;<br />

c) the spiral envelope <strong>of</strong> the arcs centred on “d2”, “f” <strong>and</strong> “g”;<br />

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

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

f) the common tangent to the spirals c) <strong>and</strong> d);<br />

g) the common tangent to the spirals d) <strong>and</strong> e); <strong>and</strong><br />

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

3.2.3 <strong>Construction</strong> <strong>of</strong> the 80° — 260° procedure turn template<br />

3.2.3 (Reference Table I-4-3-App C-3 <strong>and</strong><br />

3.2.3 Diagram I-4-3-App C-4)<br />

3.2.3.1 Nominal track. Draw a line representing the axis <strong>of</strong> the procedure <strong>and</strong> locate points “a” <strong>and</strong> “b” on it<br />

(Table I-4-3-App C-3, line 10). With a centre “c” at a distance r (Table I-4-3-App C-3, line 5) from “b” on the<br />

perpendicular line to the procedure axis passing through “b”, draw the nominal outbound turn <strong>of</strong> 80° <strong>and</strong> locate point<br />

“d” at the end <strong>of</strong> this turn. From “d” draw the tangent to the nominal outbound turn <strong>and</strong> locate point “e” on this tangent<br />

(Table I-4-3-App C-3, line 11). With a centre on “f” <strong>and</strong> a radius r, draw the nominal inbound turn <strong>of</strong> 260° beginning<br />

at “e”.<br />

23/11/06

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