Brief Description: Cont'd assembling control linkage components
Completed assembly of flap handle (installed internal components) This required making a jig to center drill a 0.250 solid rod while ensuring it matched the supplied flap slider and, then, while holding all in place, press fit a roll pin.
Since the bearing lock (adhesive) came in, also installed the bearings in the control column.
Test fit/installed the flap handle assembly in the fuselage weldment. There may be an issue here, more to follow.
Cleaned and prepared the aluminum prep tanks (alodine system) for use tomorrow.
