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My RV-10
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Date:  1-30-2011
Number of Hours:  2.00
Manual Reference:  Sec 7-9 DWG 13A
Brief Description:  Riveting / Test Assembly Left Aileron

Mounted my brake assembly to the bench and formed the trailing edge.
Turned out nice and straight and ture.
Began test assembly of aileron ribs / spar / leading edge and counter weight.
Final drilling / deburring / dimpling of bottom spar / skin to accomidate the CS4-4 rivets.
Fitted and riveted the count balance weight to leading edge skin.
Prep for the nut plate for the mounting assembly.
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Used Brake to form trailing edge

Used Brake to form trailing edge

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Spar / Rib Assembly

Spar / Rib Assembly

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Leading Edge Assembly

Leading Edge Assembly

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