Used a 1/8" piloted 100 degree counterbore to counterbore hinges.
Date: 10/14/2009
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EAA SITE
Date: 08/23/2023
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DSCN9936
Approximate position Stbd side behind D panel, prior to fuselage closure. Note the plethora of lightening holes (also
serving as pass throughs for Redux. Angle held is approximately in line with deceleration stress of harness.