221 

Federal Aviation Administration, DOT 

§ 23.441 

(2) The rudder must be suddenly dis-

placed from the maximum deflection to 
the neutral position. 

(c) The yaw angles specified in para-

graph (a)(3) of this section may be re-
duced if the yaw angle chosen for a par-
ticular speed cannot be exceeded in— 

VerDate Mar<15>2010 

10:12 Mar 18, 2014

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pmangrum on DSK3VPTVN1PROD with CFR