The "rectangular course" is a practice maneuver in which
the ground track of the airplane is equidistant from all sides of a selected
rectangular area on the ground. While performing the maneuver, the altitude
and airspeed should be held constant.
Like those of other ground track maneuvers, one of the
objectives is to develop division of attention between the flightpath and
ground references, while controlling the airplane and watching for other
aircraft in the vicinity. Another objective is to develop recognition of
drift toward or away from a line parallel to the intended ground track.
This will be helpful in recognizing drift toward or from an airport runway
during the various legs of the airport traffic pattern.
For this maneuver, a square or rectangular field (or an
area bounded on four sides by section lines or roads), the sides of which
are approximately a mile in length, should be selected well away from other
air traffic. (Fig. 11-4). The altitude flown should be approximately 600
to 1,000 feet above the ground (the altitude usually required for airport
traffic patterns).
The airplane should be flown parallel to and at a uniform
distance (about one-fourth to one-half mile away) from the field boundaries,
not above the boundaries. For best results, the flightpath should be positioned
outside the field boundaries just far enough that they may be easily observed
from either pilot seat by looking out the side of the airplane. If an attempt
is made to fly directly above the edges of the field, the pilot will have
no usable reference points to start and complete the turns.
The closer the track of the airplane is to the field boundaries, the steeper the bank necessary at the turning points. Also, the pilot should be able |
Although the rectangular course may be entered from any
direction, this discussion assumes entry on an upwind heading.
While the airplane is on the upwind leg, the next field
boundary should be observed as it is being approached, to plan the turn
onto the crosswind leg. Since the wind is a headwind on this leg, it is
retarding the airplane's groundspeed and during the turn onto the crosswind
leg will try to drift the airplane toward the field. For this reason, the
roll in to the turn must be slow and the bank relatively shallow to counteract
this effect. As the turn progresses, the headwind component decreases,
allowing the groundspeed to increase. Consequently, the bank angle and
rate of turn must be increased gradually to assure that upon completion
of the turn the crosswind ground track will continue the same distance
from the edge of the field. Completion of the turn with the wings level
should be accomplished at a point aligned with the upwind corner of the
field.
Simultaneously, as the wings are rolled level, the proper drift correction must be established with the airplane crabbed into the wind. This requires that the turn be less than a 90 degree change in heading. If the turn has been made properly, the field boundary will again appear to be one-fourth to one-half mile away. While on the crosswind leg the crab angle should be adjusted as necessary to maintain a uniform distance from the field boundary.
As the next field boundary is being approached, the pilot should plan the turn onto the downwind leg. Since a crab angle is being held into the wind and away from the field while on the crosswind leg, this next turn will require a turn of more than 90 degrees. Since the crosswind will become a tailwind, causing the groundspeed to increase during this turn, the bank initially must be medium and progressively increased as the turn proceeds. To complete the turn, the rollout must be timed so that the wings become level at a point aligned with the crosswind corner of the field just as the longitudinal axis of the airplane again becomes parallel to the field boundary. The distance from the field boundary should be the same as from the other sides of the field.
On the downwind leg the wind is a tailwind and results in an increased groundspeed. Consequently, the turn onto the next leg must be entered with a fairly fast rate of roll in with relatively steep bank. As the turn progresses, the bank angle must be reduced gradually because the tailwind component is diminishing, resulting in a decreasing groundspeed.
During and after the turn onto this leg (the equivalent of the base leg in a traffic pattern) the wind will tend to drift the airplane away from the field boundary. To compensate for the drift, the amount of turn must be more than 90 degrees.
Again, the rollout from this turn must be such that as the wings become level, the airplane is crabbed slightly toward the field and into the wind to correct for drift. The airplane should again be the same distance from the field boundary and at the same altitude, as on other legs. The base leg should be continued until the upwind leg boundary is being approached. Once more the pilot should anticipate drift and turning radius. Since drift correction was held on the base leg, it is necessary to turn less than 90 degrees to align the airplane parallel to the upwind leg boundary. This turn should be started with a medium bank angle with a gradual reduction to a shallow bank as the turn progresses. The rollout should be timed to assure paralleling the boundary of the field as the wings become level.
Usually drift should not be encountered on the upwind or the downwind leg, but it may be difficult to find a situation where the wind is blowing exactly parallel to the field boundaries. This would make it necessary to crab slightly on all the legs. It is important to anticipate the turns to correct for groundspeed, drift, and turning radius. When the wind is behind the airplane, the turn must be faster and steeper; when it is ahead of the airplane, the turn must be slower and shallower. These same techniques apply while flying in airport traffic patterns.