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

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Part I — Section 2, Chapter 2 I-2-2-7<br />

Table I-2-2-1. System use accuracy (2SD) <strong>of</strong> facility providing track guidance <strong>and</strong><br />

facility not providing track guidance<br />

VOR 1<br />

ILS NDB<br />

System use accuracy <strong>of</strong> facility NOT providing track +/– 4.5° +/– 1.4° +/– 6.2°<br />

System use accuracy <strong>of</strong> facility providing track +/– 5.2° +/– 2.4° +/– 6.9°<br />

1. The VOR values <strong>of</strong> +/– 5.2° <strong>and</strong> +/– 4.5° may be modified according to the value <strong>of</strong> a) in Table I-2-2-2, resulting from flight tests.<br />

Table I-2-2-2. Tolerances on which system use accuracies are based<br />

The values in Table I-2-2-1 are the result <strong>of</strong> a combination, on a root<br />

sum square basis, <strong>of</strong> the following tolerances<br />

VOR ILS NDB<br />

a) ground system tolerance +/– 3. 6° +/– 1° 1<br />

+/– 3°<br />

b) airborne receiving tolerance +/– 2.7° +/– 1° +/– 5.4°<br />

c) light technical tolerance 2<br />

1. Includes beam bends.<br />

+/– 2.5° +/– 2° +/– 3°<br />

2. Flight technical tolerance is only applied to navigation aids providing track. It is not applied to fix intersecting navigation aids.<br />

Parameter<br />

Table I-2-2-3.<br />

TAR<br />

within 37 km (20 NM)<br />

RSR<br />

within 74 km (40 NM)<br />

Video map accuracy 1.1 km 0.6 NM 2.2 km 1.2 NM<br />

Azimuth accuracy 0.7 km 0.4 NM 1.5 km 0.8 NM<br />

Flight technical<br />

tolerance<br />

0.7 km<br />

(5 s at 500 km/h)<br />

0.3 NM<br />

(5 s at 250 kt)<br />

1.4 km<br />

(10sat500km/h)<br />

0.7 NM<br />

(10sat250kt)<br />

Controller technical<br />

tolerance 0.6 km 0.3 NM 1.1 km 0.6 NM<br />

Total fix tolerance (RSS'd) ± 1.6 km ± 0.8 NM ± 3.2 km ± 1.7 NM<br />

23/11/06

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