Specifications

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Section 9 Cirrus Design
Supplements SR20
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 15.0 154.9 2324
Basic Empty Weight CG=
SR20_FM06_2539
x
WL 100.0
y
A
B
FS 100.0 FS 142.5
A = x + 100
B = A - y
y = ____________ Measured
x = ____________ Measured
REF DATUM
FS 0.0
Revision 01: 08-26-09