
Chapter 6 - Fuselage - Translations (includes
mechanics)
6.11 - LINE INSTALLATION BRAKE
Page 109
misalignment noted. If significant shimming is required, build the mounting surface in
the box area of local mounting gear with 3 inch BID pre-lam width. Lightly torque the
screws holding the equipment in place and correct any positioning before BID cure. Wipe
off excess resin or glass before it becomes fully cured.
Final assembly will employ a 1/4 inch rubber band provided (approximately 2
inches wide) both at the top of the gear leg, and either as a band or large washers on the
other side (inside the fuselage) of the composite gear box to avoid concentrated loading
of compost locations. Rubber should provide to facilitate the separation of the recess gears
as well as provide cushioning against the destructive effects of point loads to the
compound.
The gear legs are supplied pre-drilled to the top shafts. Trim off excess material
from the ends of the gear legs for a finished look, and also to provide space for proper
installation and operation of the brake mounting plate, which may have to be drilled for
the mounting bolts (drill the corresponding positions and sizes) . Select the proper bolts
to complete this set (note that with many shaft sets the bottom bolts are larger than the
top bolts).
It may be convenient at this point to install a temporary replacement nose gear to
allow the fuselage over wheeling, This can be as simple as a two-by-four section attached
to the firewall, or you can put a caster at the bottom if you like. Ballast will be needed to
keep the nose down.
6.11
LINE INSTALLATION BRAKE
Содержание 400
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