SB16-03-28 on New Wing
Am I correct in my understanding that the first time I need to be concerned about SB16-03-28 is when installing the aileron hinge brackets?
I'm getting the parts (W-707 D, E, F and G) prepared for the rear spar assembly (page 7-2), and from reading through the service bulletin about seven times, I think that all I have to do is make certain not to rivet the holes used for rib/bracket installation (in other words, the SB doesn't affect anything at this step).
Anything I'm missing? Any provisions I should make during this step to prepare for the SB that I'm not thinking of?