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

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I-4-6-10 Procedures — <strong>Aircraft</strong> <strong>Operations</strong> — <strong>Volume</strong> <strong>II</strong><br />

b) move SOC back to increase dz. This means that the MAPt <strong>and</strong> consequently earliest TP will be moved <strong>and</strong> the<br />

turn areas extended accordingly; <strong>and</strong><br />

c) increase OCA/H.<br />

6.4.5.6 Safeguarding <strong>of</strong> early turns<br />

If the procedure does not prohibit turns before the MAPt, then an additional area outside the final approach area must<br />

be considered (see Figure I-4-6-14). In this area obstacle elevation shall be less than:<br />

23/11/06<br />

TNA/H + do tan Z – 50 m (164 ft)<br />

(Cat H, TNA/H + do tanZ–40m(132ft))<br />

where do is measured from the obstacle to the nearest point on the edge <strong>of</strong> the final approach area. If this criterion<br />

cannot be met, then the procedure must prohibit turns before the MAPt <strong>and</strong> a note must be added on the pr<strong>of</strong>ile view <strong>of</strong><br />

the approach chart.<br />

6.4.6 Turn initiated at a designated turning point<br />

6.4.6.1 General. A designated TP shall be defined by a fix (see Section 2, Chapter 2, 2.3 <strong>and</strong> 2.4), or by a limiting<br />

radial, bearing or DME distance (see Section 2, Chapter 2, 2.6.5). It is chosen to allow the aircraft to avoid an obstacle<br />

straight ahead. The straight missed approach criteria apply up to the earliest TP. This allows the calculation <strong>of</strong> OCA/H<br />

for final <strong>and</strong> straight missed approach (OCA/Hfm) (see 6.2 “Climb gradient <strong>and</strong> MOC”). SOC is then determined.<br />

6.4.6.2 Turning point tolerance area. The length <strong>of</strong> the TP tolerance area is determined by:<br />

a) the limits <strong>of</strong> the fix tolerance area, plus;<br />

b) an additional distance c (pilot reaction <strong>and</strong> bank establishing time) equivalent to 6 seconds <strong>of</strong> flight at final<br />

missed approach (or maximum published missed approach) speed plus 56 km/h (30 kt) tailwind (see<br />

Figure I-4-6-15). Some example values <strong>of</strong> c are shown in Tables I-4-6-5 <strong>and</strong> I-4-6-6.<br />

If the TP is defined by overheading a facility (e.g. VOR, NDB) the TP fix tolerance can be taken as ± 0.9 km<br />

(± 0.5 NM) up to a height above the facility <strong>of</strong>:<br />

i) 750 m (2 500 ft) for a VOR (with a cone angle <strong>of</strong> 50°); <strong>and</strong><br />

ii) 1 100 m (3 600 ft) for an NDB.<br />

6.4.6.3 <strong>Construction</strong> <strong>of</strong> the turn area<br />

6.4.6.3.1 Turns are executed in the final missed approach area. This area begins at point A, which is located at the<br />

latest limit <strong>of</strong> the TP tolerance area (defined above). Its sides begin at the edges <strong>of</strong> the straight missed approach area.<br />

6.4.6.3.2 TP defined by a fix or by a limiting radial, bearing or DME distance.<br />

a) Outer boundary:<br />

1) On the outside edge <strong>of</strong> the missed approach area, determine point A (see Figure I-4-6-15).

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