Date:	5-4-2018
Number of Hours:	4.50
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.