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With the airplane
in the downwind position, the maneuver consists
of crossing a straight-line ground reference
at a 90° angle and immediately beginning
a 180° constant radius turn. The pilot will
then adjust the roll rate and bank angle for
drift effects and changes in groundspeed, and
re-cross the straight-line ground reference
in the opposite direction just as the first
180° constant radius turn is completed.
The pilot will then immediately begin a second
180° constant radius turn in the opposite
direction, adjusting the roll rate and bank
angle for drift effects and changes in groundspeed,
again re-crossing the straight-line ground reference
as the second 180° constant radius turn
is completed. If the straight-line ground reference
is of sufficient length, the pilot may complete
as many as can be safely accomplished.
In the same manner as the rectangular course,
it is standard practice to enter ground-based
maneuvers downwind where groundspeed is greatest.
As such, the roll into the turn must be rapid,
but not aggressive, and the angle of bank must
be steepest when initiating the turn. As the
turn progresses, the bank angle and the rate
of rollout must be decreased as the groundspeed
decreases to ensure that the turns radius
is constant. During the first turn, when the
airplane is at the 90° point, it will be
directly crosswind. In addition to the rate
of rollout and bank angle, the pilot must control
the wind correction angle throughout the turn.
Controlling the wind correction angle during
a turn can be complex to understand. The concept
is best understood by comprehending the difference
between the number of degrees that the airplane
has turned over the ground verses the number
of degrees that the airplane has turned in the
air. For example, if the airplane is exactly
crosswind, meaning directly at a point that
is 90° to the straight-lined ground reference.
If the wind, in this example, requires a 10°
wind correction angle (for this example, this
is a left turn with the crosswind from the left)
the airplane would be at a heading that is 10°
ahead when directly over the 90° ground
reference point. In other words, the first 90°
track over the ground would result in a heading
change of 100° and the last 90° track
over the ground would result in 80° of heading
change.
As the turn progresses from a downwind position
to an upwind position, the pilot must gradually
decrease the bank angle with coordinated aileron
and rudder pressure. The pilot should reference
the airplanes nose, wingtips, and the
ground references and adjust the rollout timing
so that the airplane crosses the straight-line
ground reference with the wings level, and at
the proper heading, altitude, and airspeed.
As the airplane re-crosses the straight-lined
ground reference, the pilot should immediately
begin the opposite turnthere should be
no delay in rolling out from one turn and rolling
into the next turn. Because the airplane is
now upwind, the roll in should be smooth and
gentle and the initial bank angle should be
shallow. As the turn progresses, the wind changes
from upwind, to crosswind, to downwind. In a
similar manner described above, the pilot should
adjust the bank angle to correct for changes
in groundspeed. As the groundspeed increases,
the pilot should increase the bank angle to
maintain a constant radius turn. At the 90°
crosswind position, the airplane should also
have the correct wind correction angle. As the
airplane turns downwind, the groundspeed increases;
the bank angle should be increased so that the
rate of turn is used to maintain a constant
radius turn.
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