Rectangular Course
A  principle  ground  reference  maneuver  is  the  rectangular  
course. The  rectangular  course  is  a  training  
maneuver in which the airplane maintains an equal distance 
from  all  sides  of  the  selected  rectangular  references.  The  
maneuver  is  accomplished  to  replicate  the  airport  traffic  
pattern that an airplane typically maneuvers while landing. 
While performing the rectangular course maneuver, the pilot 
should maintain a constant altitude, airspeed, and distance 
from the ground references. The maneuver assists the pilot 
in practicing the following:
•Maintaining  a  specific  relationship  between  the  
airplane and the ground.
•Dividing  attention  between  the  flightpath,  ground-
based  references,  manipulating  the  flight  controls,  
and  scanning  for  outside  hazards  and  instrument  
indications.
•Adjusting the bank angle during turns to correct for 
groundspeed  changes  in  order  to  maintain  constant  
radius turns. 
•Rolling  out  from  a  turn  with  the  required  wind
correction angle to compensate for any drift cause by 
the wind.
•Establishing and correcting the wind correction angle 
in order to maintain the track over the ground.
•Preparing the pilot for the airport traffic pattern and 
subsequent landing pattern practice.
First,  a  square,  rectangular  field,  or  an  area  with  suitable  
ground references on all four sides, as previously mentioned 
should  be  selected  consistent  with  safe  practices.  The  
airplane should be flown parallel to and at an equal distance 
between  one-half  to  three-fourths  of  a  mile  away  from  
the  field  boundaries  or  selected  ground  references.  The  
flightpath should be positioned outside the field boundaries 
or selected ground references so that the references may be 
easily  observed  from  either  pilot  seat.  It  is  not  practicable  
to  fly  directly  above  the  field  boundaries  or  selected  
ground  references.  The  pilot  should  avoid  flying  close  to  
the  references,  as  this  will  require  the  pilot  to  turn  using  
very  steep  bank  angles,  thereby  increasing  aerodynamic  
load factor and the airplane’s stall speed, especially in the 
downwind to crosswind turn.
The  entry  into  the  maneuver  should  be  accomplished  
downwind. This places the wind on the tail of the airplane 
and results in an increased groundspeed. There should be no 
wind  correction  angle  if  the  wind  is  directly  on  the  tail  of  
the airplane; however, a real-world situation results in some 
drift correction. The turn from the downwind leg onto the 
base leg is entered with a relatively steep bank angle. The 
pilot should roll the airplane into a steep bank with rapid, but 
not excessive, coordinated aileron and rudder pressures. As 
the airplane turns onto the following base leg, the tailwind 
lessens and becomes a crosswind; the bank angle is reduced 
gradually with coordinated aileron and rudder pressures. The 
pilot should be prepared for the lateral drift and compensate 
by turning more than 90° angling toward the inside of the 
rectangular course.
The  next  leg  is  where  the  airplane  turns  from  a  base  leg  
position to the upwind leg. Ideally, the wind is directly on 
the nose of the airplane resulting in a direct headwind and 
decreased  groundspeed;  however,  a  real-world  situation  
results  in  some  drift  correction.  The  pilot  should  roll  the  
airplane into a medium banked turn with coordinated aileron 
and rudder pressures. As the airplane turns onto the upwind 
leg, the crosswind lessens and becomes a headwind, and the 
bank angle is gradually reduced with coordinated aileron and 
rudder pressures. Because the pilot was angled into the wind 
on the base leg, the turn to the upwind leg is less than 90°.
The next leg is where the airplane turns from an upwind leg 
position to the crosswind leg. The pilot should slowly roll 
the airplane into a shallow-banked turn, as the developing 
crosswind drifts the airplane into the inside of the rectangular 
course with coordinated aileron and rudder pressures. As the 
airplane turns onto the crosswind leg, the headwind lessens 
and becomes a crosswind. As the turn nears completion, the 
bank angle is reduced with coordinated aileron and rudder 
pressures. To compensate for the crosswind, the pilot must 
angle  into  the  wind,  toward  the  outside  of  the  rectangular  
course, which requires the turn to be less than 90°.
The final turn is back to the downwind leg, which requires 
a  medium-banked  angle  and  a  turn  greater  than  90°.  The  
groundspeed  will  be  increasing  as  the  turn  progresses  and  
the bank should be held and then rolled out in a rapid, but 
not excessive, manner using coordinated aileron and rudder 
pressures.
 
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