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Tommys RV8 Site
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Date: 9-27-2014
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Number of Hours: 5.00
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Manual Reference:
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Brief Description: Forward Top Skin
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Edged and final drilled #30 the holes in the forward baggage door hinge brace holes that attach to the firewall, then dimple countersunk forward holes
Clecoed hinge support brace and spacer in place on fuselage and final drilled #30 holes in aft end of hinge brace
Final drilled #40 holes in forward top skin that are common with instrument panel flange, upper baggage bulkhead, firewall, baggage door hinge brace and associated support spacers and strips
Separated and edged the F-8104 skin support ribs, then positioned support ribs in place per plans
and drilled holes #40
UNclecoed F821-1 foreward top skin and removed all associated braces and ribs
Final drilled holes common to right and left upper longerons
Edged sides of top skin and dimpled tops skin, spacers, hinge support, support ribs, and baggage door support strips.
Primed all associated parts
Deburred and dimple countersunk instrument panel flange, F866 bulkhead, and forward firewall webbing
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Baggage door parts
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top skin clecoed on
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final drilling every other hole and move clecos
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