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

I-4-3-App C-20 Procedures — Aircraft Operations — Volume II
c) draw a parallel line to the inbound track through C2 and locate point C3 at the intersection of this line with arc
DL2;
d) do the same thing as in a), b) and c) above, with the line “3” instead of curve “l” and points C4, C’6, C5 and C6
instead of C1, C’3, C2 and C3 (see Figure I-4-3-App C-16 a)); and
e) if the aeroplane intercepts the VOR radial before reaching the limiting outbound distance, the pilot is assumed
to follow the indications of the VOR without drifting any further from the procedure axis, so:
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where C5 and C6 are further from the procedure axis than RP2 (see Figure I-4-3-App C-16 b)), replace C5 and
C6 by the intersections of RP2 with line “3” and DL2, and the end of the outbound leg is contained in the area
C1,C2,C3,C4,C5,andC6;
where C4, C5 and C6 are further from the procedure axis than RP2 (see Figure I-4-3-App C-16 c)), replace C4
and C6 by the intersections of RP2 with DL1 and DL2, and the end of the outbound leg is contained in the area
Cl, C2, C3, C4, and C6.
3.3.4.2.1.5 Protection of the inbound turn. Rotate the template 180°, then:
a) place template point “a” on C2 and C3, with axis parallel to the inbound track, and draw curves “4” and “5”
(part of the protection line of a turn of more than 180°) and their common tangent;
b) move the template point “a” along arc DL2 from C3 to C6, with axis parallel to the inbound track, and draw
curve “6”;
c) place template point “a” on C6, C4 and eventually on C5 and draw curves “7”, “8” and eventually “9” and their
common tangents; and
d) draw the tangent to curves “8” and “2”.
3.3.4.2.2 Construction of the entry area. It is assumed that all entries are executed along the VOR radial or the
DME arc defining the fix. The entries made along the radial inbound to the fix or along the DME arc from the nonmanoeuvring
side are protected by the basic area. The protection of the entries made along the reciprocal to inbound or
along the DME arc from the manoeuvring side needs, in addition to the basic area, the area constructed as follows. The
entry along the DME arc from the manoeuvring side is a sector 1 entry procedure. As the reciprocal to the inbound
track is the dividing line between entry sectors 1 and 2, it is assumed that both sector 1 and sector 2 entry procedures
may be executed when entering along the reciprocal to inbound.
3.3.4.2.2.1 Protection of sector 1 entry procedure. When entering along the DME arc, it is assumed that having
passed the fix the aircraft turns and follows a track parallel to the inbound track and on reaching the DME limiting
outbound distance, turns inbound onto the manoeuvring side. For entries along the DME arc, the entry area is drawn as
follows:
a) take a tracing of the template, turn it over and place point “a” on A3 with axis on the line Al A3 to draw curve
“14”;
b) draw the line “15” parallel to line “3” (used in the construction of the basic area) and tangent to curve “14”, and
locate point C10 at the intersection of this line with arc DL2; and
Note.— If no intersection occurs, either the specified DME distances should be adjusted or the sector 1
entry along the DME arc shall not be allowed.