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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-19<br />

DL2<br />

e) calculation <strong>of</strong> the horizontal limiting outbound distance: DLs<br />

DLs is the distance between the VOR/DME facility <strong>and</strong> the vertical projection <strong>of</strong> the end <strong>of</strong> the outbound track<br />

onto the horizontal plane passing through S<br />

(DL, hl in km); or<br />

(DLs, DL in NM <strong>and</strong> hl in thous<strong>and</strong>s <strong>of</strong> feet)<br />

2 2<br />

DLs = DL − hl<br />

2 2<br />

DLs = DL − 0.027 hl<br />

3.3.4.2.1.2 Fix tolerance area <strong>and</strong> limiting outbound distance<br />

a) Draw from S the procedure radial “RP” <strong>and</strong> two lines, “RP1” <strong>and</strong> “RP2”, making an angle α (tolerance for a<br />

homing VOR, Part I, Section 2, Chapter 2, Table I-2-2-1) with RP on each side <strong>of</strong> it;<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 />

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

d1 is 0.46 km (0.25 NM) + 0.125 D; <strong>and</strong><br />

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

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

“A1” <strong>and</strong> “A2” at the intersections <strong>of</strong> RP1 with D1 <strong>and</strong> D2; <strong>and</strong><br />

“A3” <strong>and</strong> “A4” at the intersections <strong>of</strong> RP2 with D1 <strong>and</strong> D2.<br />

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

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

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 in the direction <strong>of</strong> the non-manoeuvring side); <strong>and</strong><br />

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

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

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

a) Locate points C1 <strong>and</strong> C’3 at the intersections <strong>of</strong> the extensions <strong>of</strong> curve “l” with the arcs DL1 <strong>and</strong> DL2. If no<br />

intersection occurs a limiting radial shall be specified (see 3.3.4.3 <strong>of</strong> this appendix);<br />

b) locate point C2 between C1 <strong>and</strong> C’3 at a distance (dl + d2 – 1.8) km or (dl + d2 – 1) NM from C’3;<br />

23/11/06

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