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

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Part <strong>II</strong>I — Section 3, Chapter 6 <strong>II</strong>I-3-6-11<br />

c) Determine which <strong>of</strong> the obstacles identified in steps a) <strong>and</strong> b) is the highest. This will give the controlling<br />

obstacle.<br />

d) Add the appropriate aircraft category related margin (Table <strong>II</strong>I-3-6-3) to the height <strong>of</strong> the highest controlling<br />

obstacle.<br />

ha =<br />

hma cot Z + (–xz +x)<br />

cot Z + cot θ<br />

where: ha = height <strong>of</strong> equivalent approach obstacle<br />

hma = height <strong>of</strong> missed approach obstacle<br />

θ = glide path angle<br />

Z = angle <strong>of</strong> missed approach surface<br />

x = range <strong>of</strong> obstacle relative to l<strong>and</strong>ing threshold point (negative after LTP)<br />

xz = distance from threshold to origin <strong>of</strong> Z surface (–900 m, –700 m for Cat H)<br />

6.4.8.8.3 Adjustments for high airfield elevations <strong>and</strong> steep glide path angles.<br />

6.4.8.8.3.1 The margins shall be adjusted as follows:<br />

a) for airfield elevation higher than 900 m (2 953 ft), the allowances shall be increased by 2 per cent <strong>of</strong> the radio<br />

altimeter margin per 300 m (1 000 ft) airfield elevation; <strong>and</strong><br />

b) for glide path angles greater than 3.2° in exceptional cases, the allowances shall be increased by the 5 per cent<br />

<strong>of</strong> the radio altimeter margin per 0.1° increase in glide path angle between 3.2° <strong>and</strong> 3.5°.<br />

6.4.8.8.3.1.1 Procedures involving glide paths greater than 3.5° or any angle when the nominal rate <strong>of</strong> descent (Vat<br />

for the aircraft type × the sine <strong>of</strong> the glide path angle) exceeds 5 m/sec (1 000 ft/min), are non-st<strong>and</strong>ard. They require<br />

the following:<br />

a) increase <strong>of</strong> height loss margin (which may be aircraft type specific);<br />

b) adjustment <strong>of</strong> the origin <strong>of</strong> the missed approach surface;<br />

c) adjustment <strong>of</strong> the slope <strong>of</strong> the W surface;<br />

d) re-survey <strong>of</strong> obstacles; <strong>and</strong><br />

e) the application <strong>of</strong> related operational constraints.<br />

Such procedures are normally restricted to specifically approved operators <strong>and</strong> aircraft, <strong>and</strong> are associated with<br />

appropriate aircraft <strong>and</strong> crew restrictions. They are not to be used as a means to introduce noise abatement procedures.<br />

6.4.8.8.3.1.2 Part <strong>II</strong>, Section 1, Chapter 1, Appendix B shows the procedure design changes required <strong>and</strong> the<br />

related operational/certification considerations.<br />

23/11/06

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