FAA-H-8083-25C · Source PDF page 396

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Effect of Wind · PHAK page 16-9

Original FAA PHAK page 16-9
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• Movement of the air mass in reference to the ground mass of air is moving westward at 20 knots, the airspeed of the aircraft remains the same, but GS becomes 120 minus • Forward movement of the aircraft through the air mass 20 or 100 knots. Actually, these two motions are independent. It makes no Assuming no correction is made for wind effect, if an aircraft difference whether the mass of air through which the aircraft is heading eastward at 120 knots and the air mass moving is flying is moving or is stationary. A pilot flying in a 70- southward at 20 knots, the aircraft at the end of 1 hour is knot gale would be totally unaware of any wind (except for almost 120 miles east of its point of departure because of its possible turbulence) unless the ground were observed. In progress through the air. It is 20 miles south because of the reference to the ground, however, the aircraft would appear motion of the air. Under these circumstances, the airspeed to fly faster with a tailwind or slower with a headwind, or to remains 120 knots, but the GS is determined by combining drift right or left with a crosswind. the movement of the aircraft with that of the air mass. GS can be measured as the distance from the point of departure to As shown in Figure 16-13, an aircraft flying eastward at the position of the aircraft at the end of 1 hour. The GS can an airspeed of 120 knots in still air has a groundspeed (GS) be computed by the time required to fly between two points a exactly the same—120 knots. If the mass of air is moving known distance apart. It also can be determined before flight eastward at 20 knots, the airspeed of the aircraft is not by constructing a wind triangle, which is explained later in affected, but the progress of the aircraft over the ground is this chapter. [Figure 16-14] 120 plus 20 or a GS of 140 knots. On the other hand, if the The direction in which the aircraft is pointing as it flies is WINDS ARE CALM called heading. Its actual path over the ground, which is a combination of the motion of the aircraft and the motion of the air, is called track. The angle between the heading and 090° the track is called drift angle. If the aircraft heading coincides with the TC and the wind is blowing from the left, the track does not coincide with the TC. The wind causes the aircraft to drift to the right, so the track falls to the right of the desired course or TC. [Figure 16-15] Groundspeed 120 knots The following method is used by many pilots to determine WINDS 270° AT 20 KNOTS 090° compass heading: after the TC is measured, and wind correction applied resulting in a TH, the sequence TH ± variation (V) = magnetic heading (MH) ± deviation (D) = compass heading (CH) is followed to arrive at compass heading. [Figure 16-16] By determining the amount of drift, the pilot can counteract the effect of the wind and make the track of the aircraft Groundspeed 140 knots coincide with the desired course. If the mass of air is moving across the course from the left, the aircraft drifts to the WINDS 090° AT 20 KNOTS right, and a correction must be made by heading the aircraft sufficiently to the left to offset this drift. In other words, if the wind is from the left, the correction is made by pointing 090° the aircraft to the left a certain number of degrees, therefore correcting for wind drift. This is the wind correction angle (WCA) and is expressed in terms of degrees right or left of the TC. [Figure 16-17] Groundspeed 100 knots Figure 16-13. Motion of the air affects the speed with which aircraft move over the Earth’s surface. Airspeed, the rate at which an aircraft moves through the air, is not affected by air motion. 16-9