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

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Part <strong>II</strong> — Section 4, Chapter 1, Appendix A <strong>II</strong>-4-1-App A-13<br />

Altitude in thous<strong>and</strong>s <strong>of</strong> metres<br />

Altitude<br />

feet<br />

x 1 000<br />

42<br />

39<br />

36<br />

33<br />

30<br />

27<br />

24<br />

21<br />

18<br />

15<br />

12<br />

9<br />

6<br />

3<br />

55°<br />

Example Number 3<br />

Example Number 1<br />

Example Number 2<br />

0<br />

0<br />

0 1 2 3 4 5 6 7 8 9 10<br />

Distance in nautical miles<br />

For distances over 10 miles <strong>and</strong>/or altitudes in excess <strong>of</strong> 35 000 ft, multiply chart values by 10 (e.g. read as<br />

1 mile at 4 000 ft, or as 10 miles at 40 000 ft).<br />

To determine slant range, extend altitude line to a point vertically above ground distance. Follow arc down to<br />

base line <strong>and</strong> read slant range (Example No. 1).<br />

To determine ground distance, read slant range arc upward to selected altitude line. Follow vertically down to<br />

ground distance line (Example No. 2).<br />

To determine minimum usable ground distance to VOR/DME fix, enter with the maximum altitude for the<br />

procedure. Ground distance is found vertically below intersection with diagonal (Example No. 3).<br />

Figure <strong>II</strong>-4-1-App A-7. DME slant range vs. ground distance/<br />

Minimum usable ground distance to a VOR/DME fix (non-SI units)<br />

___________________<br />

Slant range<br />

Altitude<br />

feet<br />

x 1 000<br />

42<br />

39<br />

36<br />

33<br />

30<br />

27<br />

24<br />

21<br />

18<br />

15<br />

12<br />

9<br />

6<br />

3<br />

23/11/06

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