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

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<strong>II</strong>-1-3-2 Procedures — <strong>Aircraft</strong> <strong>Operations</strong> — <strong>Volume</strong> <strong>II</strong><br />

23/11/06<br />

Note 2.— The dimensions shown are those which encompass current aircraft types. They are chosen to<br />

facilitate OCA/H calculations <strong>and</strong> promulgation <strong>of</strong> aircraft category related minima. It is assumed that these<br />

dimensions are not intended to be used for other purposes than the OCA/H calculations in other ICAO<br />

documents. The use <strong>of</strong> OAS surfaces to calculate OCA/H may result in significant differences between aircraft<br />

categories because <strong>of</strong> small differences in size. For this reason, it is always preferable to use the Collision Risk<br />

Model (3.4.9) which will allow for more realistic assessment for both height <strong>and</strong> position <strong>of</strong> obstacles.<br />

Note 3.— Current Category E aircraft are not normally civil transport aircraft <strong>and</strong> their dimensions are not<br />

necessarily related to Vat at maximum l<strong>and</strong>ing mass. For this reason, they should be treated separately on an<br />

individual basis.<br />

b) Category <strong>II</strong>/<strong>II</strong>I is flown autocoupled (for Category <strong>II</strong> flown with flight director, see 3.4.8.7.6).<br />

c) Missed approach climb gradient 2.5 per cent.<br />

d) The approach azimuth deviation information is displayed using sensitivity characteristics in accordance with the<br />

following table (Annex 10, <strong>Volume</strong> I, Attachment G to Part I, 7.4.1.1).<br />

Approach azimuth antenna<br />

to threshold distance (ATT) Nominal course width<br />

0 – 400 m ± 3.6 degrees<br />

500 – 1 900 m ± 3.0 degrees<br />

2 000 – 4 100 m<br />

(105)<br />

± arctan degrees<br />

ATT<br />

4 200 – 6 300 m ± 1.5 degrees<br />

Note.— The displacement sensitivity characteristics given above for the ATT distances from 2 000 m to<br />

4 100 m are based upon a nominal course width <strong>of</strong> 210 m at the MLS approach reference datum.<br />

e) Glide path (elevation angle):<br />

1) minimum: 2.5°;<br />

2) optimum: 3.0°; <strong>and</strong><br />

3) maximum: 3.5° (3° for Cat <strong>II</strong>/<strong>II</strong>I operations).<br />

Note.— The glide path angle <strong>of</strong> the procedure must be greater than or equal to the minimum glide path<br />

(see Annex 10, Part I, 3.11.1 — Definitions).<br />

f) MLS approach reference datum height 15 m (50 ft).<br />

g) All obstacle heights are referenced to threshold elevation.<br />

h) For Cat <strong>II</strong> <strong>and</strong> Cat <strong>II</strong>I operations the Annex 14 inner approach, inner transitional <strong>and</strong> balked l<strong>and</strong>ing surfaces<br />

have not been penetrated. Where the Cat <strong>II</strong> OCA/H is higher than the level <strong>of</strong> the inner horizontal surface, but<br />

below 60 m, the inner approach <strong>and</strong> balked l<strong>and</strong>ing surfaces should be extended to the Cat <strong>II</strong> OCA/H level to<br />

accommodate Cat <strong>II</strong>I operations.

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