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Date:  12-1-2011
Number of Hours:  2.75
Manual Reference:  C07
Brief Description:  Forward fuselage floor structure (complete)

Because I want the bottom skin/floor to be removeable, The only riveting is at the ends of the C06-02 assembly, and the rear angle support for the idler assembly. So when the floor is un-cleco'd, much of this stuff will be hanging in mid air, other than the clecos temporarily holding the forward end of the assembly to the aft spar tunnel angles.

- Tonight I riveted ALL of those floor structure pieces ON MY WORKBENCH, totally outside of the aircraft.

- Then I laid the entire assembly in the fuselage, cleco'd, then riveted as described above in the first paragraph.

Tomorrow I will work on the final details for installing the seat pan.
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Assembly riveted ONLY at the ends (not at the bottom/skin)

Assembly riveted ONLY at the ends (not at the bottom/skin)

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Aft section of the spar tunnel removed

Aft section of the spar tunnel removed

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C06-02 assembly riveted to the sides, but NOT to the bottom/skin

C06-02 assembly riveted to the sides, but NOT to the bottom/skin

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