Quickie Q2 Lite Construction Manual - page 80
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The external visual inspection capability provided by the
materials allow inspection of all primary structures at any point
before finishing. All primary structures are at the surface,
eliminating the requirement for “pre-cover” or “closure” inspections.
Opaque filler materials are used throughout the airplane in
finishing, and inspection must take place before any areas are
obscured. Some areas may have opaque materials applied to one surface
where the structure is inspectible from the opposite side (wing
trailing edge for' example).
3.0 DEFECTS
3.1 VOIDS
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Interlaminar voids in a new layup may be due to small air
bubbles trapped between plies during the layup. These void areas look
white and are distinctly visible even deep in a cured layup.
Interlaminary voids up to 1 inch in diameter do not require repair,
as long as they do not consist of more than 5% of the surface area.
Interlaminar voids (air bubbles) up to 2 inches in diameter are
acceptable when repaired as follows: A small hole is drilled into the
void and epoxy is injected into the void area. Small voids such as
this may occupy up to 5% of the laminate surface area.
Voids greater than 2 inches in diameter should be repaired as shown
in paragraph 4.
CONTINUED ON NEXT PAGE
PAGE 3-20
Q2 Plans - Chapter 3 - Page 3-19