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DYNAMIC WT9
5.1.6 Fiche de Pesée
Weight and Balance Record of the aeroplane DYNAMIC
Model: DYNAMIC
WT-9
Configuration
: (Empty weight including the operating fluids of the engine and standard equipment ).
Datum point ( DP):
Weighing-machines place Weight (kg)
Nose wheel
Right wheel
Left wheel
Total weight
Fuel
Weight =
Engine oil and coolant including
C.G. position from DP.
X
= M/G = –––––––––––– =
T
C.G. in % MAC
X
= (X
– 77)/ SAT x 100 = –––––––– x 100 =
CT
T
Permitted C.G. range of empty aeroplane X
Calculated position of C.G. is within an permitted range.
Place , date:
Date: Novembre 2003
Registration:
leading edge of wing root section
Distant from DP
G
a = -
N
G
b =
R
G
b =
L
G
Total Moment M =
240
kg
(MAC= 1185 mm)
X
– 77
T
1185
is 12% ± 2 % MAC
CT
DYNAMIC WT9
MANUEL D'UTILISATION, D'ENTRETIEN ET DE REPARATION
S/N:
(mm)
Moment =
Signature / Supervisor Stamp:
Date of production:
Moment M= G ∗ Distant
-
kg/mm
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