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Grob ASTIR CS User Manual

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MASS AND RESIDUAL MOMENT LIMITS OF THE CONTROL SURFACES
After repainting
or
a repair the hinge moments and weights may not exceed the
following values:
ASTIR CS (S/N 1002 - 1536)
Elevator:
Rudder:
10.0 to 15.0kgcm
13.65kgcm
± 10%
Aileron:
16.0kgcm ± 12%
ASTIR CS 77 (S/N 1601 - 1698)
ASTIR CS JEANS (S/N 2001 - 2092)
Elevator:
Rudder:
10.0 to 15.0kgcm
16.5kgcm
± 10%
Aileron:
16.0kgcm ± 12%
ASTIR CS 77 (starting from S/N 1699)
ASTIR CS JEANS (starting from S/N 2093)
Elevator
Rudder
Aileron
10.0
to 15.0kgcm
Oto 5kgcm
Oto 1kgcm
2.40 to 3.25kg
3,2kg
± 10%
4,1kg ± 12%
2.40 to 3.25kg
4,5kg
± 10%
4,1kg ± 12%
2.40 to 3.25kg
max.6.0kg
max.
6.0kg
For the measurement
of
the hinge moments the controls must be removed from the
glider. For the determination of the hinge moment
(M
= P.
r)
the control hinge should be
as friction free as
possible. The force P can be measured with a spring balance. If the
values are exceeded, then the balance weight should be increased. Before a repair
of
the control surfaces and/or a replacement
of
the balance weight, the manufacturer
is
to
be contacted.
p
----r
18

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Grob ASTIR CS Specifications

General IconGeneral
BrandGrob
ModelASTIR CS
CategoryAircrafts
LanguageEnglish

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