Aerospool WT-9 Dynamic - Page 43

WT-9 Dynamic Club S
Type:
WT - 9
DYNAMIC
Type landing
-
gear
FIXED
Type of Scale
3 x 500 NDS
Weighing Point
Scale Reading(kg)
Nose wheel
110,9
Right main wheel
111,7
Left main wheel
111,5
Total Weight
334,1
Fuel
Weight =
334,1 kg
Oil and coolant including
C.G. position from DP = Moment / Weight
71259,8
X
T
(mm) 334,1 - 77
=
32627,8 1185
Permitted C.G. range of empty aeroplane X
Calculated position of C.G. is within an
Place, Date: 22
.06.2006
Prievidza 26.01.2011
Date: 1.12.2001
FLIGHT MANUAL
Section 6 Page 6
gear
:
Registration:
S/N:
Date of production:
Calibration valid till
01.06.201
Scale Reading(kg)
Distant from DP (mm)
Moment (kg mm)
a =
-
7
22
-
80069,8
b =
67
8
75732,6
b =
67
8
75597,0
Total Moment =
71259,8
240
Moment =
71259,8
C.G. position from DP = Moment / Weight
- 77
136
=
136 mm X
CT
% MAC 1185
32627,8 1185
Permitted C.G. range of empty aeroplane X
CT
is from 10 to 14 % MAC.
Calculated position of C.G. is within an
permitted range.
.06.2006
Prievidza 26.01.2011
........................................
Supervisor
Section 6 Page 6
-
3
Date of production:
01.06.201
2
Moment (kg mm)
80069,8
75732,6
75597,0
71259,8
71259,8
8 kg/mm
x 100 = 11,5 %
32627,8 1185
........................................
Supervisor
/ Signature