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

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I-4-3-App C-14 Procedures — <strong>Aircraft</strong> <strong>Operations</strong> — <strong>Volume</strong> <strong>II</strong><br />

b) with a centre on S, draw arcs “Ds” with a radius Ds, “Dl” with a radius Ds – dl, “D2” with a radius Ds + dl,<br />

“DLs”, “DL1” <strong>and</strong> “DL2” with radii DLs, DLs – d2 <strong>and</strong> DLs + d2<br />

23/11/06<br />

where dl <strong>and</strong> d2 are the DME tolerance associated with D <strong>and</strong> DL:<br />

dl is 0.46 km (0.25 NM) + 0.0125 D;<br />

d2 is 0.46 km (0.25NM) + 0.0125 DL<br />

c) locate points “A” at the intersection <strong>of</strong> “RP” <strong>and</strong> “Ds”<br />

“Al” <strong>and</strong> “A2” at the intersections <strong>of</strong> “RP1”<br />

with “Dl” <strong>and</strong> “D2”<br />

“A3” <strong>and</strong> “A4” at the intersections <strong>of</strong> “RP2”<br />

with “D1” <strong>and</strong> “D2”.<br />

3.3.4.1.1.3 Protection <strong>of</strong> the outbound turn <strong>and</strong> outbound leg<br />

a) Place racetrack template point “a” on Al, with axis parallel to the inbound track, <strong>and</strong> draw curve “1” (part <strong>of</strong> the<br />

outline <strong>of</strong> the template);<br />

b) place template point “a” on A3, with axis parallel to the inbound track, <strong>and</strong> draw curve “2” (part <strong>of</strong> the outline<br />

<strong>of</strong> the template) <strong>and</strong> line “3” (protection <strong>of</strong> the outbound leg on the non-manoeuvring side); <strong>and</strong><br />

c) draw the common tangent to curves “1” <strong>and</strong> “2” <strong>and</strong> extend the straight part <strong>of</strong> curve “1” <strong>and</strong> the line “3” in the<br />

direction <strong>of</strong> the outbound end.<br />

3.3.4.1.1.4 Area containing the end <strong>of</strong> the outbound leg<br />

a) Locate points Cl <strong>and</strong> C’3 at the intersection <strong>of</strong> the extension <strong>of</strong> curve “l” with the arcs DL1 <strong>and</strong> DL2;<br />

b) locate point C2 between Cl <strong>and</strong> C’3 at a distance (dl + d2 – 1.8) km or (dl + d2 – 1) NM from C’3;<br />

c) draw a parallel line to the inbound track through C2 <strong>and</strong> locate points C3 at the intersection <strong>of</strong> this line with arc<br />

DL2;<br />

d) do the same thing as in a), b) <strong>and</strong> c) with the line “3” instead <strong>of</strong> curve “l” <strong>and</strong> points C4, C’6, C5 <strong>and</strong> C6 instead<br />

<strong>of</strong> Cl, C’3, C2 <strong>and</strong> C3 (see Figure I-4-3-App C-13 a)); <strong>and</strong><br />

e) if the aircraft intercepts the VOR radial before reaching the limiting outbound distance, the pilot is assumed to<br />

follow the indications <strong>of</strong> the VOR without drifting any further from the procedure axis, so:<br />

where C5 <strong>and</strong> C6 are further from the procedure axis than RP2 (see Figure I-4-3-App C-13 b)), replace C5 <strong>and</strong><br />

C6 by the intersections <strong>of</strong> RP2 with line “3” <strong>and</strong> DL2, <strong>and</strong> the end <strong>of</strong> the outbound leg is contained in the area<br />

Cl, C2, C3, C4, C5 <strong>and</strong> C6; <strong>and</strong><br />

where C4, C5 <strong>and</strong> C6 are further from the procedure axis than RP2 (see Figure I-4-3-App C-13 c)), replace C4<br />

<strong>and</strong> C6 by the intersections <strong>of</strong> RP2 with DL1 <strong>and</strong> DL2, <strong>and</strong> the end <strong>of</strong> the outbound leg is contained in the area<br />

Cl, C2, C3, C4 <strong>and</strong> C6.<br />

3.3.4.1.1.5 Protection <strong>of</strong> the inbound turn. Rotate the template 180°, then:<br />

a) place template point “a” on C2 <strong>and</strong> C3, with axis parallel to the inbound track, <strong>and</strong> draw curves “4” <strong>and</strong> “5”<br />

(part <strong>of</strong> the protection line <strong>of</strong> a turn <strong>of</strong> more than 180°) <strong>and</strong> their common tangent;

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