WEIGHTS AND THE CENTRE OF GRAVITY POSITION
When additional equipment
is
fitted, or after repairs, or a new gel/paint finish or any
other weight change of the
glider, the empty weight and centre of gravity position
is
to
be
determined.
If the ranges of the empty weight, and the centre of gravity position (table below), and
the cockpit loading limits, are satisfied, the flying weight limitations
will
be
in
the
permitted range.
Unloaded weight (kg)
CG
range (mm aft)
245 697 - 756
250
690-
750
255
683 - 745
260
675 - 740
265
654-
735
270
633-
730
275
612 - 726
280
593-
721
285
574 - 717
CONTROL DEFLECTIONS - RIGGING ANGLES
Glider wings level, with fuselage upper surface at a slope of 1000 : 40 tail down from
the horizontal, measured
300mm forward of fin.
Elevator
Up
60
±6mm
Down
54
± 6mm
Rudder
Left
190 ± 10mm
Right
190 ± 10mm
Aileron
Up
93±10mm
Down
48 ± 5mm
Rigging
Angle
wing chord to fuselage longitudinal axis
2 degrees
Tail chord to fuselage longitudinal axis
0 degrees
14
To Next Page
Loading...
Need help?
General
