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

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Appendix to Chapter 6<br />

REFINED METHOD FOR CALCULATING MAPt AND<br />

TRANSITIONAL TOLERANCES FOR A MISSED APPROACH POINT<br />

DEFINED BY A DISTANCE FROM THE FAF<br />

1. INTRODUCTION<br />

1.1 This appendix shows the full Root Sum Square (RSS) method for calculating:<br />

a) distance from earliest MAPt to nominal MAPt;<br />

b) distance from nominal MAPt to latest MAPt; <strong>and</strong><br />

c) distance from nominal MAPt to SOC,<br />

when the MAPt is defined by a distance from the FAF.<br />

1.2 The criteria contained in Part I, Section 4, Chapter 6, 6.1.6.3, “Determining SOC with an MAPt defined by a<br />

distance from the FAF (simplified method)” are conservative in certain cases. To overcome this conservatism,<br />

distances may be calculated precisely using the formulas in this appendix.<br />

1.3 The equations shown in Chapter 6, Table I-4-6-1, “Values for Z (Earliest <strong>and</strong> latest MAPt for MAPt<br />

determined by distance from the FAF)” <strong>and</strong> Chapter 6, Table I-4-6-2, “Computation <strong>of</strong> transitional distance” were<br />

derived by linear interpolation from the accurate RSS calculations at the extreme values quoted (i.e. aircraft Categories<br />

A to D <strong>and</strong> for all aerodrome elevations up to 4 000 m (13 000 ft)).<br />

2. CALCULATION<br />

2.1 General<br />

The calculation <strong>of</strong> each <strong>of</strong> the relevant distances is done in two steps, using the maximum <strong>and</strong> minimum final approach<br />

speeds for the category <strong>of</strong> aircraft. The considered distance is the higher <strong>of</strong> the two found.<br />

2.2 Factors<br />

The empirical RSS method takes into account the following factors:<br />

a) the fix tolerance at the FAF (assumed as 1.9 km (1.0 NM) to develop the simplified equations in the body <strong>of</strong><br />

this chapter);<br />

b) the minimum permissible speed at ISA – 10°C or the maximum permissible speed at ISA + 15°C, whichever is<br />

the more critical for each category <strong>of</strong> aircraft considered;<br />

I-4-6-App-1 23/11/06

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