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Aircraft Projects
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Date:  11-18-2007
Number of Hours:  2.00
Manual Reference:  
Brief Description:  Left Elevator - 08 - Trim Tab Hinge & Leading Edge

- Placed trim tab (with hinge drilled and clecoed to the trim tab) on the left elevator.
- Aligned it and final drilled it to the spar and skin (E-606 to E-701).
- Took the trim tab and hinge off.
- Deburred, cut hinge to size, radiused ends and dimpled all holes. I decided to dimple the holes in the hinge and spar instead of countersinking. I thought that the material was too thin to take anymore away.
- Rolled the leading edge of the left elevator. I rolled the heck out of it and it still didn't quite line up right. The skins overlapped so I know they were rolled enought but it looks as though the final 3/4" needs to be bent and no matter how much I rolled it, it wouldn't bend. Just like the other side, I duct taped and clecoed the piece together. I'm hoping that if the skins are forced into that shape for a period of time they will become formed (it's a theory, not a great one but still it's a theory, I'll let you know how it turns out).
- Put the completed trim tab on the elevator and re-checked it for alignment. The trim tab spar moved a little during riveting, so it's a little off but it's close enough for government work.
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Putting the trim tab on the elevator to check for alignment.

Putting the trim tab on the elevator to check for alignment.

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Left Elevator leading edge rolled and clecoed together.

Left Elevator leading edge rolled and clecoed together.

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Checking Trim Tab for alignment and movement. Works great lasts long time.

Checking Trim Tab for alignment and movement. Works great lasts long time.

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