
Chapter 6 - Fuselage - Translations (includes
mechanics)
6.13 - Extras
Page 119
With very careful adjustment to the plunger lengths, and a tapered metal striker
plate. a system lock slam can be artificial. However, the increased plunger insertion depth
with this current system gives more peace of mind.
.
Test the position of the assembly, and mark the location for the hole where the latch
pin of the latch plunger will have to protrude out through the molding of the inner door
skin. Drill a clearance hole for this pin (about 5/16 inches in diameter) through the inner
door skin and the 1/4 inch aluminum reinforcement section previously glued in. Hold the
assembly in position with the pin protruding through this hole and assemble the Complete
test system hangs and check function.
.
Test the outer skin fit again, and trim all areas for correct fitting (particularly
checking around the cuff). Clean and sand all bonding surfaces. Apply adhesive to both
surfaces (especially the hinge area, be careful around areas around moving parts such as
the door handle). Cover the skin from the outside in place until the adhesive cures. Local
areas that require a secure connection (such as the hinge areas) can be fastened together
with a Cleco, or a small screw as a temporary fixing procedure. Fixing these two surfaces
tightly together can distort the door molds in the hinge area. In this case, fill the void
between the two skins wit a FLOX mixture, and allow it to cure with the proper spacing.
Remove these temporary closures in the same way as for the lines of another fuselage
link. When the bonded joint has healed, make alignment marks for future placement, and
remove doors and trim to fit the opening.
MOUNT DOORS
Reinforce the hinge door pads in the upper fuselage molding by overlaying 4 ply
BID on the inner surface. Use a tapered overlay on the
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