Hours for 9/15 and 9/16 combined. Finished reattaching repaired aileron: Bolts torqued and sealed, Unriveted the damaged flap, just for fun. Will order a new QB flap on Monday from Vans.
Measured prop tracking with a dial indicator (image 1): TIR = 0.088-0.089". Well within 0.125" (+/- 1/16") recommended by AC 90-89B.
Test alternator belt tension by torque wrench method i.a.w. Lycoming SI-1129B. Was way too loose. Small pulley should hold at 11-13 ft-lb turning clockwise. After redo, torque wrench clicked when set to 132 in-lb, but slipped at 156 in-lb. Safety wire job took three tries to get tight (images 2 and 3).
Checked and reset Pmag timing i.a.w.Emagair manual. Set the prop a skosh past TDC and blew in disconnceted the manifold pressure line. All set.
Taped the electronic level to the left flap. Full-up to full-down travel is 32 degrees--right at Van's lower limit for the RV-9A. Marked 10 and 20 deg intermediate flap deployments with a 90 deg combo square resting on top of the wing with its blade touching the edge. Will need a helper to set the lines back a skosh to be read from the cockpit.
Looked at gap between Al fairings and bottom of horizontal stab. It's 1/8" or less all the way around, but the Van's supplied weather stripping needed so much trimming around vertical fin attach structure and the longerons that I'll look for something more suitable.