Going to taper sand away about half thickness of aluminium at tip 1.
Date: 10/22/2009
Views: 2925
TopFit27ann
Date: 05/29/2004
Views: 2511
DSCN5227
Date: 11/29/1999
Views: 4067
Newest Image
EAA SITE
Date: 08/23/2023
Views: 168546
TopFit20ann
I began to do a final fit of the top to the fuselage. Drilled nine 1/8-inch holes approximately equally spaced across the firewall bond area. Sheet fasteners were installed as the holes were drilled. Each sheet fastener was backed with a small stainless steel washer to spread the load.