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

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Chapter 6<br />

PRECISION APPROACH PROCEDURES — GBAS<br />

6.1 INTRODUCTION<br />

6.1.1 Application<br />

The GBAS criteria in this chapter are based on ILS criteria <strong>and</strong> are related to the ground <strong>and</strong> airborne equipment<br />

performance <strong>and</strong> integrity required to meet the Category I operational objectives described in Annex 10. An illustration<br />

<strong>of</strong> the specific definitions used in this chapter is given in Figure <strong>II</strong>I-3-6-1.<br />

Note.— While specific GBAS Category I criteria are in preparation, the criteria contained in this chapter are based<br />

on an ILS Category I equivalency method. Development <strong>of</strong> Annex 10 requirements for Category <strong>II</strong> <strong>and</strong> <strong>II</strong>I approaches<br />

is in progress; pending their finalization, procedure design criteria will be made available.<br />

6.1.2 Procedure construction<br />

The procedure from en route to the GBAS final approach segment <strong>and</strong> in the final missed approach phase conforms<br />

with the general criteria. The differences are found in the physical requirements for the GBAS precision segment which<br />

contains the final approach segment as well as the initial <strong>and</strong> intermediate phases <strong>of</strong> the missed approach segment.<br />

These requirements are related to the performance <strong>of</strong> the GBAS Cat I system.<br />

6.1.3 St<strong>and</strong>ard conditions<br />

The following list contains the st<strong>and</strong>ard assumptions on which procedures are developed. Provisions are made for<br />

adjustments where appropriate. Adjustments are m<strong>and</strong>atory when conditions differ adversely from st<strong>and</strong>ard conditions<br />

<strong>and</strong> are optional when so specified (see 6.4.8.7, “Adjustment <strong>of</strong> OAS constants”).<br />

a) Maximum aircraft dimensions are assumed to be the following:<br />

<strong>Aircraft</strong> category Wing span<br />

Vertical distance between the flight<br />

paths <strong>of</strong> the wheels <strong>and</strong> the GBAS antenna<br />

(m)<br />

H 30 3<br />

A, B 60 6<br />

C, D 65 7<br />

DL 80 8<br />

Note 1.— OCA/H for Cat DL aircraft is published when necessary.<br />

<strong>II</strong>I-3-6-1 23/11/06

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