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Q1 Plans Chapter 9 Page 9-6

Construction begins by glassing the aileron slots on both inboard pieces. When the layups are cured, cut the BL52 and BLOO templates at the 18-A-B-C-18 line. Use these templates to hot wire the inboard foam cores into two pieces each in preparation for laying in the shear web.


Quickie BL52 and BL100

Before doing that, however, the wing must be jigged upside down on the layout table.

Make some wood templates roughly cut to represent female versions of the top portions of the hot wire templates. Full size drawings for these are included. These templates are used to jig the wing cores with the correct dihedral.

To help in getting the trailing edge of the main wing straight(i.e. perpindicular to BL00), the following procedure has been developed:

  1. Run a taut string from one end of the table to the other. To get it taut, you may want to let it extend over the side of the table and hang weights from it. Its location should be at the aft end of the BL100 female jigging template.
  2. Study the full size female jigging templates for BL100, BL52, and BLOO. Notice that a deminsion is given from the string to the aft edge of each female jigging template; e.g. the distance is 0” for BL100 because you set it that way.
  3. By using the distance given, you can set the inboard female jigging templates to give a straight trailing edge when the foam cores are placed in position.

Quickie Main Wing Jigging

As you are locating the cores in position, check to verify that the level lines on the cores are level. This is important so be careful.

At BL00, you will have to bevel the two inboard wing foam cores to allow them to fit together flush at the proper dihedral angle.

Also, stand back and cight spanwise along the wing to verify that the wing is not bowed or kinked. A straight edge laid spanwise is also useful for this.

Don’t be concerned if the templates need to be moved inboard or outboard - slightly to remove any bows or kinks. When everything is satisfactory, mix up some bondo and bondo the templates to the table top in the proper locations. After that is accomplished, the foam cores should be just resting on the templates.


Quickie Main Wing Jigging

The next step is to join the foam cores together with micro slurry. Check each level line as you do this. Before stopping, 5-.MIN the foam cores to the templates with small dabs and being careful not to move the cores.

CAUTION! The foam cores must fit within 1/16”, and the slow epoxy must be used to join them, or exotherm damage will result.

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Q1 Plans Chapter 9 Page 9-7

When the micro has cured, rotate the table 90 deg nose down so that the shear web can be done.


Quickie Rotate Table 90 Degrees

The shear web extends from BL52 left to BL52 right.


Quickie Shear Web

Note that the glass wraps around both the top and the bottom of the wing, so that the shear web corner will have to be rounded slightly to get the glass to lay down. Also, at L52, the layup turns 90 deB, and follows to the trailing edge of the wing, still wrapping up over the top and bottom surface(which, therefore must be ‘scooped’ out .026” so that the two plies will fit flush with the rest of the core.

After laying up the two BID at 45 deg. for the shear web, the rear half of the 18-A-B-C-18 hot-wired piece can be reattached with micro. Use tape to hold the combination together until it cures.




TRIMMING THE FOAM CORE

At this point, the wing should be jigged on your layout table upside down. Using a hard block on the foam core) clean up all joggles, excess micro, and bumps. At BLOO, round that joint so that the glass can flow smoothly across BLOO.

Read over the section on “Mounting the Main wing” to understand how the wing fits on the fuselage.

The shear web that you previously laid u fits against the forward face of the FS89 bulkhead. Measure the width of the fuselage at that point and mark it on the wing foam core with a pen. Mark BL9.3 on each side at the trailing edge of the foam cores and connect up the BL marks. before cutting out this section of the foam core, measure the fuselage to verity that after the cutting, the foam core will project inside the fuselage to the aft of the FS89 bulkhead. If not, change the BL9.3 mark so that the core will project inside the fuselage in that area.

Next, you need to cut off the “nose” of the main wing so that it will fit against the seatback bulkhead. Measure the distance from FS89 bulkhead to the seatback bulkhead on each side of the fuselage, and place marks on the foam at the corresponding locations. Connect the points spanwise with a pen. Tq


Quickie Trimming the Foam Core

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