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Conrads X-10 Build Log
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Date: 10-28-2009
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Number of Hours: 1.00
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Manual Reference: 31-8 Step 8 to 15
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Brief Description: Section 31 UPPER FORWARD FUSELAGE ASSEMBLY... Pag
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Section 31 UPPER FORWARD FUSELAGE ASSEMBLY... Page 31-8, Step 8 to 15.
Step 8, I dimpled the holes in the flanges of the F-1001A Firewall Bulkhead that are at the top in common with the fuselage skin.
Step 9, I accomplished this previously I believe in chapter 29.
Step 10, I removed the entire assembly and because I have already deburred the parts I skipped this step too.
Step 11, Already accomplished this too.
Step 12, All parts are already primed too.
Step 13, The dimpling has already been accomplished.
Step 14, I already riveted the nutplates to the F-1003D & E.
Step 15, I riveted the F-1044B Angle, F-1044C Spacer and the F-1044D,E and F Angle to the F-1044A Forward Fuselage Rib as shown in figure 2.
Time about 1 hour because I had already accomplished most of the steps.
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Priming Some of the Parts
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The 1044A Forward Fuselage Rib to RivetedF-1044B Angle, F-1044C Spacer and the F-1044D,E and F Angle
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