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Date:  8-23-2009
Number of Hours:  0.50
Manual Reference:  6-B-1
Brief Description:  Bottom Skin Stiffners Part 02

After fitting bthe horizontal tail frames to the bottom skin, the stiffners were identified and laid out in the correct position.

All work was carried out in accordance with the Zenith Aircraft Company Construction Standards 2007, Zenith Aircraft Company Photo Assembly Guide 2008 and the Zenith Aircraft Company Plan Set Serial Number 65-7512.
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Bottom Skin Stiffners laid out

Bottom Skin Stiffners laid out

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