Setting the Wing Incidence – 2

After the F-796A was bolted, temporarily, to the fuselage, the clamp could be removed. I located the center of the 1/4” hole on the flange of the angle, double checking to be sure that there was sufficient edge distance on both T-405 and F-796A. I drilled the 1/4” hole through T-405.

I finished the bracket installation after the wings were removed by installing the nutplate on T-405 as shown in DWG 38 Detail F and Section E-E. I noted the orientation of the platenut as it was important.

Time: 8 hours.