FlyingFoam Nurf Instruções gerais de montagem - Página 3
Procurar online ou descarregar pdf Instruções gerais de montagem para Aeronaves FlyingFoam Nurf. FlyingFoam Nurf 11 páginas.
Spar Installation
7. The carbon fiber spars are joined at the wing panel joints with the pre-bent joiner
wires that are found in the small parts bag. The spars will also be wrapped at the joint
with ~1.5" of the 3" wide fiberglass tape. Start by dry fitting the joiners and spars; de-
burr the ends of the joiners/spars with sandpaper if required. Test fit the spars in the
wing cores and adjust the joiners and spar slots as required. Once the dry fit is
satisfactory use epoxy to join the carbon fiber spars with the bent wire spar joiner and
wrap the spars at the joints with the fiberglass tape.
8. The spars can be glued into the EPP cores with CA glue, epoxy or 3M Spray contact
adhesive. To use 3M glue, spray a medium coat of 3M into the spar slot of the cores
and let dry for 5 to 10 minutes. Spray a light coat of 3M on 1 side of the glued together
spar assembly and IMMEDIATELY place the spar in the spar slot in the wing core. DO
NOT WAIT. The wet 3M glue will allow you to position the spar in the slot. IF YOU WAIT
TOO LONG YOU WILL NOT BE ABLE TO MOVE IT!!
9. Weight the spars and wing so they remain flat in the beds while the glue dries.
NOTE: Moving the wing before the glue fully dries may allow the spars to slide in the
foam and result in a twisted/warped wing.
10. Repeat the process for the bottom spars.
Servo Installation
10. After installation of the bottom spars you should have the wing cores in the top beds
with the bottom of the wing facing up.
11. Locate the pockets for your servos (we recommend metal gear servos with the
mounting ears removed). Measure 17" out along the elevon hinge line from the wing
panel joint formed by the center and outer wing panels. From that mark measure
forward and perpendicular from the elevon hinge line to just behind the location of the
Rev 2.0 10/21/13
3