21.03.2013 Views

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

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

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

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

Part <strong>II</strong> — Section 3, Chapter 1 <strong>II</strong>-3-1-3<br />

width <strong>of</strong> the buffer area is progressively reduced to zero, ending in an area without track guidance where the full MOC<br />

is applied (see Figure <strong>II</strong>-3-1-8).<br />

1.4 CONSTRUCTION OF AREAS FOR VOR AND NDB ROUTES<br />

1.4.1 General<br />

This section contains methods for calculating the areas used for en-route obstacle clearance purposes. The statistical<br />

derivation <strong>of</strong> these calculations, which are based on a root sum square method <strong>of</strong> the navigation system use accuracy,<br />

appears in Appendix B.<br />

1.4.2 Straight areas<br />

1.4.2.1 Area descriptions. The obstacle clearance areas consist <strong>of</strong> a primary area <strong>and</strong> two lateral buffer areas on<br />

each side.<br />

1.4.2.2 Width abeam the facility. Abeam the facility, the total area has a constant width <strong>of</strong> 18.5 km (10.0 NM),<br />

which is comprised <strong>of</strong> the primary area <strong>and</strong> a buffer area. The primary area maintains a constant width <strong>of</strong> 9.3 km<br />

(5.0 NM) on either side <strong>of</strong> the nominal track. The buffer area also maintains a constant width <strong>of</strong> 9.3 km (5.0 NM) on<br />

either side <strong>of</strong> the primary area.<br />

1.4.2.3 Angular limits. When the distance from the facility is greater than:<br />

a) 92.3 km (49.8 NM) for VOR; <strong>and</strong><br />

b) 60 km (32 NM) for NDB,<br />

the areas diverge, following the angular tolerance lines <strong>of</strong> their respective facilities (See Table <strong>II</strong>-3-1-1).<br />

1.4.2.4 Width after the point <strong>of</strong> divergence. After the limiting distance stated in 1.4.2.3, “Angular limits”, the<br />

width <strong>of</strong> the primary area is increased by the angle <strong>of</strong> splay. The buffer area is determined by the angle <strong>of</strong> splay plus an<br />

additional fixed width on the outside <strong>of</strong> the buffer area, parallel to its edge (see Figures <strong>II</strong>-3-1-2 <strong>and</strong> <strong>II</strong>-3-1-3). This<br />

width is:<br />

a) 3.7 km (2.0 NM) for VOR; <strong>and</strong><br />

b) 4.6 km (2.5 NM) for NDB.<br />

1.4.2.5 Longitudinal limits. The longitudinal limits <strong>of</strong> the area associated with a straight segment are determined<br />

as follows:<br />

a) the earliest limit <strong>of</strong> the area is a half circle, centred on the first fix <strong>and</strong> tangent to the lateral limits <strong>of</strong> the total<br />

area; <strong>and</strong><br />

b) the latest limit <strong>of</strong> the area is a half circle, centred on the second fix <strong>and</strong> tangent to the lateral limits <strong>of</strong> the total<br />

area.<br />

1.4.2.6 Combination <strong>of</strong> VOR <strong>and</strong> NDB criteria. In case <strong>of</strong> a straight segment based on a VOR at one end <strong>and</strong> an<br />

NDB at the other end, the area is designed as shown in Figure <strong>II</strong>-3-1-4.<br />

23/11/06

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!