Starboard flange will be reduced to prevent so much seal bulging out. Y9-11-27
Date: 11/18/2009
Views: 5533
Flugzeugabsturz_22_08_2008_Marchtrenk_014
Date: 08/22/2008
Views: 8110
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EAA SITE
Date: 08/23/2023
Views: 807568
WingSet31Ann
Completed the fitting of the W26 (aft) lift pin sockets. Ran the wings on and measured the gap between the fore and aft sockets and the fuselage. About 1.5mm at the front of the W27 (fore) lift pin sockets. No space at the back. A couple more plies of BID are all that are needed there.