text: ‘An excessive angle of attack during the ap- 
  proach and landing implies that the airplane is 
  being operated at too low an airspeed. Of 
  course, excessive angle of attack may cause the 
  airplane to stall or spin and the low altitude 
  may preclude recovery. Also, the low aspect 
  ratio configuration at an excessively low air- 
  speed will 
  incur very high induced drag and 
  will necessitate a high power setting or other- 
  wise incur an excessive rate of descent. An 
  additional problem is created by an excessive 
  angle of attack for the airplane which exhibits 
  a large dihedral effect at high lift coefficients. 
  In this case, the airplane would be more sensi- 
  tive to crosswind.s and adequate lateral control 
  may not be available to effect a safe landing at 
  a critical value of crosswind. 