Mahindra GIPPSAERO GA8-TC 320 - Page 89

C01-01-08 5 Feb 2009 Page 6-5
Section 6
Weight & Balance /
Model GA8-TC 320 Equipment List
D
D
X
Level Points
Datum
Firewall
Station 0
WEIGHING ON JACKS
M
T
Aircraft Registration:____________________ Date:______________
MEASURED DATA
Load Cell Position Distance (mm) Reading (kg)
Adjustment
(±kg)
Nett Load (kg)
Left Wing Jack
D
W
= 1285
L =
Right Wing Jack R =
Tail Jack D
T
= 6093 T =
Sum of Nett Loads S =
X = C of G position = [(L + R) x D
W
+ T x D
T
] / S
i.e. X = [(____+____) x ___ + ___x____] / ____
X = _________mm
Item Weight (kg) Arm (mm) Moment (kg.mm)
Aircraft as weighed S = X =
Add unusable fuel (sump) 6.3
(wings) 5.6
705
1829
4442
10242
Empty Weight
Figure 6-1A Aircraft Weighing Form
D
W
01 Aug 2011