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Flandy Rv-10
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Date:  3-19-2011
Number of Hours:  3.50
Manual Reference:  30-3/ 31-15
Brief Description:  Fwd Fuselage riveting and more dimpling

Dimpled holes in forward fuselage assembly per instructions. Rivetd the F-1044B/C/D/E/F to theF-1044A fwd fuselage rib. Riveted nutplates to F-1083 control cable panel and then attached to F-1068A Center sub-panel. Started riveting F-1068 L+R Sub-panels to F-1068 A center sub panel.

Dimpled bagage floor stiffeners, bagge door skin/frames/and closeout panel.

Sect.29 Inserted vent door into frame and attached with called for hardware except substituted AN3-4 bolt for AN527 screw--- much easier to tighten. Section 29 Complete.


Sect. 30 Set step to correct spanwise insertion and correct sweep back per plans. Match drilled #30. Clecoed baggage floors in place and drilled #30 from bottom through floors. Removed floors and deburred. Match drilled left step #12.
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