..
-.
FLIGHT
MANUAL
GR00
G
103
31
If the limits of the empty weight
C.
of
G.
poaltions and the loading
lirnltatlons drari are adhered to the
C.
of
G.
ot the loaded glider
will
be within the permitted range.
It should be noted that to make use of the maxlmum load the maximum
admissable load for non-llftlng parts must not be exceeded.
Empty Weight
kg lb8
360 794
365 805
370 81.6
375 827
380 838
385 849
390 860
395
871
400 882
-.
:'
j
The weight of the non-lifting parts is the sum of the fuselage, tallplane
and mexlmum load In the funelage and must not exceed
400
kgs
(882
ib).
Otherwise the
maximum
load permitted
Range ot
C.
of
G.
behind Datum
Forward Aft
mm inches mrn inches
758 29.84
773 30.43
748
29. 45 769 30. 28
739
29.09
765 30.12
729
28. 70
761 29. 96
720
28.
35
757
29.
80
711
27. 99
753 29.
65
703
27. 68 749
29.49
694 27.
32
745
29.
33
686 27.01
742 29.21
in the fuselage must be correspondingly decreased.
me Centre of Gravity should
be
recalculstd alter repair, repainting,
the inatallation of addltlonel equipment or when a period of
4
years
hm elapsed after the laat weighing.
The empty weight, empty welght
C.
of
Q.
positlon and maximum load,
should be recorded after
each
weighing on page
S
of the Flight Hand-
book.
17
th
march
1982
'L
7.
#&77
:'-2
ir.J
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