1. A line was marked at 12 7/16 on both F-01255. 2. The corner of both F-01255 was trimmed leaving 1/8 at the aft end. 3. The angle of both F-01255 was opened to achieve a total 95.4 degrees. 4. F-01255 were twisted 2.7 degrees in order to achieve a planar face. 5. F-01234 was deburred. 6. F-01234 were positioned on top of each F-01255 and with a piece of aluminum we simulated a side fuselage skin. 7. Both F-01255 were match-drilled #30, a total of 27 holes on each one. 8. F-01255 were deburred. 9. same for F-01255-L-1
