§3.233 may be used instead, except that in any case values less than 0.

6 of the specified minimum loads shall not be employed. 3The critical portions of the aileron control system shall also be designed for a single tangential force having a limit value equal to 1.25 times the couple force determined from the above criteria. 4D = wheel diameter. FIG. 3-11 —PILOT CONTROL FORCE LIMITS