Veloce 400, Руководство пользователя, Страница: 120 / 160

Chapter 6 - Fuselage - Translations (includes
mechanics)
6.13 - Extras Page 115
Prepare two 1.5 by 4 1/4 inch pieces of plywood. Drill a 3-16 hole through the
center of the bottom and a washer glue on the top surface centered in this hole. drill a 1/4
inch hole and install the #10 TEE nut in the center of the other plywood section.. Cut the
appropriate handle for this door (see drawing), and fit for the hole on the inner surface,
locate and drill the 3/16 hole in the bottom leg of the skin door’s inner channel in such a
way that using this pivot point will place the outer surface of that handle flush with the
outer skin. using a #10-32 screw and latch as a fixturing, bond to the two 1/4 inch sections
of plywood on the inner side of each channel leg with a FLOX/MICRO mix. Make sure
the handle will be free to operate.
At this time the reinforcement locations for the door armrest air mounts must also
be added to the inner door panels. Lay four BID ply at the bottom of the window frame
front hat hardening frame section centered about 17 inches above the bottom of the door
frame and about 6 iches long. This offering should be big enough to wrap the sides about
1/4 inch. This will provide local stiffness in this area and provide enough “flesh” for the
self tapping screws that will be used to mount the air arm bracket.
Door opening trim in the upper half of the fuselage. Cut along a line about 1/2 inch
inside the insertion angle, which defines the opening area. Test the inner door shelf fit for
this opening to ensure fit, and trim any interference.
Inner door grip panel in effect on the door opening in the fuselage using 5 minutes
or Bondo epoxy, and thickened to match the outer fuselage outline, small 1/4 inch
plywood blocks can be used to simulate the perimeter thickness of the door seal (it is
probably best to do one side at a time to allow greater accessibility to work on both sides.