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Date:  6-12-2012
Number of Hours:  2.00
Manual Reference:  F02
Brief Description:  Continue rear spar carry through

Continued with the rear spar carry through instructions on F02.

- Put the shear angle back on the fuselage to drill the remaining holes that had not yet been drilled.

- Put the shear angle on the rear spar carry through assembly and updrilled everything. Then of course there was the disassembly and deburring.

- Drilled the 1/4" holes through the vertical attach angles (just above the bottom cleco in photo #3).

- Assembled all the parts of the rear spar carry through and riveted and bolted per plans.

- I did NOT rivet the vertical attach angles. The rear spar carry through won't fit around the "stuff" inside the fuselage if you do. So I put the rear spar carry through assembly in place, THEN cleco'd the vertical attach angles in place.

- Tomorrow I will rivet the shear angle to the fuselage structure (the empty holes across the bottom of the angle in photo #2).
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Rear spar carry through assembly to the right

Rear spar carry through assembly to the right

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From below...

From below...

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Vertical angles had to be placed AFTER the carry though or the carry through would not fit

Vertical angles had to be placed AFTER the carry though or the carry through would not fit

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