Aerospool WT-9 Dynamic - Page 89

TECHNICAL DESCRIPTION, OPERATING, MAINTENANCE AND REPAIR MANUAL
5.1.6 Weight and Balance Record
Weight and Balance Record of the aeroplane WT-9 Dynamic
Model: WT-9
Dynamic
Registration: S/N: Date of production:
Configuration : (Empty weight including the operating fluids of the engine and standard equipment ).
Datum point ( DP): leading edge of wing root section
Type of Scales: Calibration walid up to:
Weighing-machines place
Weight (kg) Distant from DP (mm)
Moment M= G ∗ Distant
Nose wheel G
N
a = - -
Right wheel G
R
b =
Left wheel G
L
b =
Total weight G Total Moment M =
Fuel 240
Weight = kg Moment = kg/mm
Engine oil and coolant including
C.G. position from DP.
X
T
= M/G = –––––––––––– =
C.G. in % MAC (MAC= 1185 mm)
X
T
– 77
X
CT
= (X
T
– 77)/ SAT x 100 = –––––––– x 100 =
1185
Permitted C.G. range of empty aeroplane X
CT
is 12% ± 2 % MAC
Calculated position of C.G. is within an permitted range.
Place , date: Signature / Supervisor Stamp:
Date: 01.03.2002 WT-9 Dynamic Section 5 Page 5 - 8