Figure 20-1: Chart preparation using 10-degree lines
THE FLIGHT PLANNING FORM
As information relating to the proposed flight is accumulated, enter it in the appropriate sections of a flight planning form. Figure 20-2a shows how the planned flight from Melfort to Humboldt would be entered. The cruise altitude of 4,500 feet, and true airspeed, track, and wind velocity can be entered, and the remaining figures can be added as they are obtained through measurement or calculation. Other pertinent information, particularly weather and landing details, can be added for current and future use.
Figure 20-2a: Flight planning form
TRACK LINE MEASUREMENT
One of the properties of a Transverse Mercator Projection is that scale can be considered constant all over the chart. Because of this the meridians of longitude, (the vertical lines), converge at a point above the top of the chart, and for that reason a straight line drawn on the chart meets each meridian at a slightly different angle. To offset these differences, place the protractor at the midpoint of the track line when measuring that angle. This is particularly important when the track line is long and runs parallel to the parallels of latitude.
AIRSPEED CORRECTIONS
True Airspeed (TAS) is used for navigation computations since indicated Airspeed (IAS) varies with temperature, pressure, and altitude. Conversion of IAS to TAS (or vice-versa) can be done very rapidly on your circular navigation computer. Because most helicopter operations are conducted at relatively low altitude, quite often IAS is used, as the differences are minimal.
WIND VELOCITY (W/V)
In aviation terminology, the term wind velocity, usually abbreviated to W/V, implies both the direction of the wind and its speed. Wind velocities normally change with altitude and, in planning a cross-country flight, this must be taken into account when preparing the flight planning form. Many factors affect the selection of the altitude(s) at which a flight will be conducted and W/V is a major one.
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