Using fore and aft the supplied by Europa for push-rod jam nuts that are .155" thick
Date: 12/13/2013
Views: 7157
Newest Image
EAA SITE
Date: 08/23/2023
Views: 804391
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.