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Aircraft Operations

Doc 8168 Aircraft Operations, Volume I Flight Procedures

Doc 8168 Aircraft Operations, Volume I Flight Procedures

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Chapter 1<br />

EN-ROUTE CRITERIA<br />

1.1 GENERAL<br />

1.1.1 Procedures developed utilizing en-route criteria assume normal aircraft operations. Any requirements to<br />

satisfy Annex 6 aeroplane performance operating limitations must be considered separately by the operator.<br />

1.1.2 Two methods can be used to determine en-route obstacle clearance areas:<br />

a) a simplified method, which is the standard method; and<br />

b) a refined method, which can be used when the simplified method is too constraining.<br />

1.2 OBSTACLE CLEARANCE AREAS<br />

1.2.1 In the simplified method, the obstacle clearance area is divided into a central primary area and two lateral<br />

buffer areas. In the refined method, the obstacle clearance area is divided into a central primary area and two lateral<br />

secondary areas. The width of the primary area corresponds to 95 per cent probability of containment (2 SD). The total<br />

width of the area corresponds to 99.7 per cent probability of containment (3 SD).<br />

1.2.2 Reductions to secondary area widths<br />

Secondary areas for en-route operations may be reduced when justified by factors such as:<br />

a) relevant information on flight operational experience;<br />

b) regular flight inspection of facilities to ensure better than standard signals; and/or<br />

c) radar surveillance.<br />

1.2.3 Area without track guidance<br />

When track guidance is not provided, for example, outside the coverage of navigation facilities along the route, the<br />

primary area splays at an angle of 15° from its width at the last point where track guidance was available. The width of<br />

the buffer area (simplified method) or the secondary area (refined method) is progressively reduced to zero, ending in<br />

an area without track guidance where the full minimum obstacle clearance (MOC) is applied.<br />

I-5-1-1 23/11/06

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