Mahindra GIPPSAERO GA8-TC 320 - Page 90

Section 6
Weight & Balance /
Model GA8-TC 320 Equipment List
Page 6-6 5 Feb 2009 C01-01-08
Aircraft Registration:____________________ Date:______________
MEASURED DATA
Load Cell Position Distance (mm) Reading (kg)
Adjustment
(±kg)
Nett Load (kg)
Left Main Wheel
D
M
= 1943
L =
Right Main Wheel R =
Nose Wheel D
N
= -356 N =
Sum of Nett Loads S =
X = C of G position = [(L + R) x D
M
+ N x D
N
] / 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 6-1B Aircraft Weighing Form
D
D
X
Level Points
Datum
Firewall
Station 0
WEIGHING ON WHEELS
M
T
D
N
01 Aug 2011