Quickie Q2 Lite, Руководство по монтажу

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rear shell core is only 1/411 thick, bevel the forward shell to match
the aft core at the joint. Also, sand dull the inside skin glass within
2.5" of either side of the joint, in preparation for the inside joint
lamination later. Prepare some scrap lumber for use in holding the
jigged position. Mix up flox and spread it on both edges of the shells
where they will join. Place the two shells together, hold them in
position with the lumber and Bondo, and permit to cure.
..... Next, laminate the 3 BID tapes shown on the outside of the skin
after you have sanded dull the existing glass. Note that the three tapes
have the following widths: 5", 4", and 3" and that the orientation
should be at 45 degrees to the joint itself. Wherever it is necessary to
overlap BID in order to laminate around the entire circumference,
overlap the BID by a minimum of 1.5".
..... Once that lamination has cured, craw1 inside the fuselage and
perform the inside skin lamination as shown, wherever possible. The 4
BID tapes have the following widths: 5",4",3", and 2" with a 45 degree
orientation to the joint. The extra BID is to make up for the glass
strength lost when the foam was beveled.
END OF CHAPTER
Q2 Plans - Chapter 13 - Page 13-01