HB
-28
2
1 Insert the wing's connecting
spar carefully into one wing up
to the V-shaped bend.
2 Hold the spar firmly and push
the wing onto the other side.
Use a slightly screwing motion
if this is difficult. Then push
both wings together
completely with the
servomotor connection cables
hanging downwards.
3 Engage the wing attachment
and connection plate on the
end of the wings and click into
position in the reinforced hole.
When assembling the wing on the fuselage, the
connection of the servo connectors if deflection
servo connectors of the aileron's servomotor must
takes place in the wrong direction.
be joined to the connectors of the cable distributor
Insert the wing using the rear edge of the
in connection point 1 ("AILE" => aileron) the
attachment plate into the fuselage opening until
receiver. Aileron joystick towards the right:
the cut-out on the front edge engages into the
Deflection of right aileron upwards, left aileron
nose on the fuselage. Screw the wings down
downwards. Other side accordingly reversed.
using two screws.
Caution! The motor may start up inadvertently if
operated wrongly.
Keep a firm grip on the fuselage. Switch the
If the nose or tail sections have a tendency to tilt
using double sided tape and should be equally
downwards, the weight is biased in this direction.
balanced. A centre of gravity which is too far
Occasionally the centre of gravity of the aeroplane
rearward (nose too light) will make flying difficult
may have to be corrected e.g. after a repair, by the
and needs to be corrected.
addition of small weights. These should be applied
An airplane's centre of gravity is designed to be in
a certain relation to its lifting areas and the
MINIMOA
it is set up correctly on delivery. The
margin at which the centre of gravity may move in
relation to the ideal set up is very small. You can
check the centre of gravity of the
MINIMOA
by
holding it up at the points shown (140 mm from the
rear edge of the wing) with two fingers. It should
then slightly swing around the horizontal position
and not be inclined to the front or rear.
BALANCING THE CENTRE OF GRAVITY
HB
-28
2
M
IN
IM
0A
HB
-28
2
54
mm
14 MINIMOA CARSON R/C MODEL GLIDER 50 050 5016
GB
GB