Finished updrilling the AN3 holes in the elevator control rod idler, F19-08. Torqued nuts to 24lb-in and applied torque seal. Oriented the bolt heads inboard so the bolts can be removed since there is insufficient clearance to remove the bolts with the bracket mounted near the skin. This has a disadvantage of not being able to readily see if the nuts are backing off, but I also added torque seal to the bolt heads to monitor for any movement.
Started doing some more trimming of the aft fuselage verticals for control rod and rudder cable clearance.
