The step numbers below take off from log #10 of the assembly.
34. Locate F23-09 & F23-11 on the bulkheads. Do not rivet, Rivets will be installed later when the push rod is installed. For that reason I only pilot drilled 2 holes in each end just to hold them in the measured locations.
35. Rivet/bolt the following parts onto Shear Web F22-03 (see all 3 photos below). If you don't you will never be able to get them riveted inside the fuselage: - Rivet angle F23-03 - Rivet bulkhead F23-02 - Bolt the F23-01 Tail Wheel/Skid Mount onto the bottom of bulkhead F23-02 and thru angle F23-04. Torque the nuts.
36. Place the entire assembly from Step 35 into the tailcone and make sure everything aligns as it should, and pieces to be connected are flush. DO NOT CLECO IN PLACE, YET. You need to be able to spread the end of the taicone to get some of the angles around some of the rivet ends already in the lower longerons.
All the items in Step 35 cleco'd together
All the items in Step 35 riveted and bolted into a single assembly.