Grob G 103 TWIN II User Manual

FLIGHT MANUAL GROB G 103 tl
Empty weight . e .. ., . about 380 kg(837,7 lbs)
Maximum flying weight . . 580 kc(1278,67 lbs)
Maxlmwn qewltted wight of non iiftln~ parts 400 kg(881 ,a4 ibs
/
The approved range of cenlre of gravity posliona during lllght is
1
260 mm (10.24 lnohes) to 480 mm (15.11 indzes) behind the datum
li P. e uivalent to 24.7% to 43.5% of the M.A.c.'~~ the wing.
A?; a(ltitude: incidence. board of 600:Z
anele.
I
ths datum line I8 Uudront adge ot tho wlng st the dng root.
.
The spprovd centre ot grsvity rango does not gel exceeded by the
payload dMrkwtion rpscltied in the loadlng
plan 11.8.
, Th. exact posltlon of the centre of gravlty at flying WiQht can be
c@lcuiated eocordlng to41
5.
Mkimum load In ih. hont rul for all lllght .
. 70 kg (154 ibs)
Mulmum
lo& In ihr lront wnl . . . . 110 kg (242 ibs)
Maximum load In
the brdc wat . . . 110 kg (242 ibs)
Maximum 1o.d In
~u' baggog. comp~~t .
10 kg ( 22 lbs)
The maximum flying weight of 580 kg (1278,67 lbs)
must not be exceeded.
Trim weights must be ueed at the suspensions
in front
of stick bulkhead to compensate if
the front seat load 18 lower than 70 kg
( 154 lbs ). See page 14.
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Grob G 103 TWIN II Specifications

General

Brand	Grob
Model	G 103 TWIN II
Category	Aircrafts
Language	English