Specifications

6-6 Information Manual
Section 6 Cirrus Design
Weight & Balance SR20
Figure 6-3
Airplane Weighing Form
Weighing
Point
Scale
Reading
- Tare = Net Weight X Arm = Moment
L Main A=
R Main A=
Nose B=
Total
As Weighed
CG=
CG = Total Moment / Total Weight
Space below provided for additions or subtractions to as weighed condition
Empty Weight
CG=
Engine Oil (if oil drained)
15 lb at FS 78.4, moment = 1176
Unusable Fuel 26.4 153.95 4064
Basic Empty Weight CG=
SR20_FM06_1441
x
WL 100.0
y
A
B
FS 100.0 FS 145.0
A = x + 100
B = A - y
y = ____________ Measured
x = ____________ Measured
REF DATUM
FS 0.0
Airplane Weighing Form
March 2010