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

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<strong>II</strong>I-2-3-2 Procedures — <strong>Aircraft</strong> <strong>Operations</strong> — <strong>Volume</strong> <strong>II</strong><br />

designed. This distance is the sum <strong>of</strong> the minimum stabilization distances required at the IAF <strong>and</strong> IF <strong>and</strong> can be derived<br />

from Table <strong>II</strong>I-2-1-3 or Table <strong>II</strong>I-2-1-9.<br />

Note.— The optimum length <strong>of</strong> 9.3 km (5.0 NM) ensures that the minimum segment length for aircraft IAS up to<br />

390° km/h (210 kt) below 3 050 m (10 000 ft) will be accommodated.<br />

3.2.3 Descent gradient. The optimum descent gradient is 4% (Cat H, 6.5%). Where a higher gradient is necessary<br />

to avoid obstacles, the maximum permissible is 8% (Cat H, 10%). Descent gradient is based on the shortest possible<br />

track distance (TRD) for the fastest category <strong>of</strong> aircraft, <strong>and</strong> not the segment length.<br />

3.2.4 Calculation <strong>of</strong> track distance (TRD). The TRD between two fly-by waypoints is defined as the segment<br />

length reduced by the stabilization distance at both turns (r tan /2) <strong>and</strong> increased by the distance flown in the turn from<br />

abeam the waypoint to the tangent point (2r ×0.5/360).<br />

TRD = segment length – r(tan 1/2 + tan 2/2) + r(1 + 2)/360<br />

where:<br />

23/11/06<br />

1 = turn angle (degrees) at the beginning <strong>of</strong> the segment<br />

2 = turn angle (degrees) at the end <strong>of</strong> the segment<br />

r = turn radius at 25° bank angle<br />

Example for a first 110° turn <strong>and</strong> a second 70° turn:<br />

TRD = segment length – 0.56r<br />

3.2.5 Shortest initial approach segments. For the <strong>of</strong>fset initial approach segments, the shortest possible track<br />

distance will occur when a 110° turn is made at the IAF <strong>and</strong> a 70° turn is made at the IF for a Y-bar procedure <strong>and</strong> when<br />

a 90° turn is made at either the IAF or the IF for a T-bar procedure. For the central initial approach segment, the<br />

shortest possible track distance will occur when a 90° turn is made at the IAF.<br />

3.2.6 Procedure entry altitude. The procedure is entered at the 46 km (25 NM) minimum sector altitude or<br />

terminal arrival altitude. Where the initial approach waypoint forms part <strong>of</strong> an air route, the procedure should be entered<br />

at the minimum en-route altitude applicable to the route segment.<br />

3.2.7 Reversal procedures. When all three initial segment legs are implemented there is no need for reversal<br />

procedures. Should one <strong>of</strong> the legs not be implemented, a racetrack pattern may be established at either or both <strong>of</strong> the<br />

other IAFs. In the event that the central IAF leg is one <strong>of</strong> the remaining legs, its capture region is adjusted to<br />

accommodate normal sector entries into a reversal procedure (see Figure <strong>II</strong>I-2-3-3).<br />

3.2.8 Holding. A holding pattern may be provided at any IAF <strong>and</strong> should be aligned with the initial segment track.<br />

3.3 INTERMEDIATE APPROACH SEGMENT<br />

3.3.1 Alignment. The intermediate approach segment should be aligned with the final approach segment whenever<br />

possible. If a turn at the FAF is necessary it shall not exceed 30°.

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