l
F.8L Falco Construction Manual
24–16
Revision 4, March 1, 2002
Figure 19
❏
Glue the two 20x20 stringers on the bottom of the fuselage. See Figure 19. At the forward
end, the stringers are glued to the bottom of the main wing spar, and at the aft end they
are glued to the two saddle gussets on the front face of fuselage frame No. 6. The outboard
face of these stringers is at B.L. 140, regardless of what type of wheel well is planned.
These stringers are bowed into place, that is, they take a bend that follows the curve of the
bottom of the fuselage.
Figure 20
❏
Glue the two 20x20 spruce members on the front face of fuselage frame No. 6. See Figure
20—which shows the top of the left wing. These parts must be cut and fitted to the aft
wing spar. The notches in these members must match the seat support required for the
two types of wheel wells. The “open air” wheel well uses four 30x15 seat supports. The
wheel well door installation has two 60x15 seat supports inboard and two 30x15 outboard.
Содержание F.8L Falco
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