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RV-6A - GBC
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Date:  9-7-2015
Number of Hours:  5.00
Manual Reference:  
Brief Description:  Rear Spar - and fairings

Worked through the same tasks from the left, but now on the right wing to set Angle of Incidence, Sweep, and 'square' with fuselage. Then progressively drilled the rear spar on the right wing but only up to .250 inch, awaiting a final pass to make slight alignment tweaks on the alignment of both wing bolt holes. (ordered bolts today).

Used the previously mark alignment offsets to drill the overlapping bottom fuselage skin then enlarged to final size.Holes aligned well with wing flange for nutplate positions.

Enlarged the fairing holes for the #8 screws, and deburred/dimpled.

Need to make a detailed task list to ascertain that everything is ready to pull out the wing for final clean-up (only about 4-5 inches.
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Drilled the Rt Rear Spar

Drilled the Rt Rear Spar

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Drilled the fuselage overlap

Drilled the fuselage overlap

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Dimpled & deburred

Dimpled & deburred

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